U.S.

Department of Transportation
Federal Aviation Administration
Washington, DC

Master Minimum Equipment List (MMEL)

Revision: 62
Date: 11/28/2022

Boeing 737
B-737-100/200/300/400/500/600/700/800/900/900ER

Richard C. Grundman, Chair

Flight Operations Evaluation Board (FOEB)

Federal Aviation Administration (FAA)

Transport Aircraft Seattle Branch
2200 S. 216th St, 2nd Floor, North Wing
Des Moines, WA 98198

Telephone: (206) 231-3893

Email: 9-AVS-AFS-100@faa.gov
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. I
DATE: 11/28/2022
AIRCRAFT:
TABLE OF CONTENTS AND CONTROL PAGE
Boeing B-737
SYSTEM NO. SYSTEM PAGE NO. REV NO. DATE
-- Cover Page -- 62 11/28/2022
-- Table of Contents and Control Page I 62 11/28/2022
-- Highlights of Change II thru XI 62 11/28/2022
-- FAA MMEL Policy Application Record XII thru XIX 62 11/28/2022
-- Definitions XX 60 02/09/2018
-- Preamble XXI 60 02/09/2018
-- Guidelines for (M) and (O) Procedures XXII 60 02/09/2018
21 Air Conditioning 21-1 thru 68 62 11/28/2022
22 Autoflight 22-1 thru 13 62 11/28/2022
23 Communications 23-1 thru 37 62 11/28/2022
24 Electrical Power 24-1 thru 5 58 10/10/2015
25 Equipment/Furnishings 25-1 thru 27 62 11/28/2022
26 Fire Protection 26-1 thru 31 62 11/28/2022
27 Flight Controls 27-1 thru 17 62 11/28/2022
28 Fuel 28-1 thru 30 62 11/28/2022
29 Hydraulic Power 29-1 thru 4 62 11/28/2022
30 Ice and Rain Protection 30-1 thru 13 62 11/28/2022
31 Indicating/Recording Systems 31-1 thru 8 62 11/28/2022
32 Landing Gear 32-1 thru 8 58 10/10/2015
33 Lights 33-1 thru 19 62 11/28/2022
34 Navigation 34-1 thru 42 62 11/28/2022
35 Oxygen 35-1 thru 5 62 11/28/2022
36 Pneumatic 36-1 thru 5 62 11/28/2022
38 Water/Waste 38-1 thru 2 62 11/28/2022
46 Information Systems 46-1 thru 5 58 10/10/2015
47 Inert Gas System 47-1 55a 02/13/2012
49 Airborne Auxiliary Power 49-1 thru 5 58 10/10/2015
52 Doors 52-1 thru 19 62 11/28/2022
73 Engine Fuel and Control 73-1 thru 2 62 11/28/2022
74 Ignition 74-1 thru 2 58 10/10/2015
75 Bleed Air 75-1 52 04/29/2008
77 Engine Indicating 77-1 thru 3 62 11/28/2022
78 Engine Exhaust 78-1 thru 2 62 11/28/2022
79 Engine Oil 79-1 thru 2 62 11/28/2022
80 Starting 80-1 thru 2 58 10/10/2015
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. II
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737

The following changes are the Highlights of Changes for Revision 62. EFFECTIVE ABOVE DATE, the
Boeing 737 Master Minimum Equipment List has been revised. The changes in this revision were made
to align with FAA policy letters and to increase dispatch flexibility. All changes are reflected in the
highlights of change listed below and are indicated by revision bars in the associated ATA section. For
any change affecting an ATA section, all pages in that associated ATA section are re-dated
accordingly, with the exception of nomenclature changes for ATA chapter headings.

ITEM NO. EXPLANATION OF CHANGE

General Minor editorial corrections and formatting changes were made throughout the
document, indicated with change bars. These editorial corrections may be adopted in
Minimum Equipment Lists (MEL) at the operator’s discretion.

ATA 21 AIR CONDITIONING

21-01-06B Deleted option 21-01-06B.

21-02-03 Added Line Number applicability to item heading, provisos, (O) requirement and
NOTE.

21-02-04 Removed Flow Control Valve part number from the item heading.

21-02-05 Split item 02-05 into new option 02-05A and option 02-05B. Added airplane
applicability for -800/-900ER to the item heading, added (M) procedure requirement
and proviso.

21-02-06 Added new relief item 21-02-06.

21-11-02-01 Removed both options 11-02-01A and 11-02-01B from MMEL as they were deleted in
Revision 57 per PL-31, Revision 3.

21-11-02-02A Removed from MMEL as it was deleted in Revision 57 per PL-31, Revision 3.

21-11-02-02B Removed from MMEL as it was deleted in Revision 57 per PL-31, Revision 3.

21-11-02-03 Restructured proviso for clarification.

21-14-04-02 Added proviso d) for the 737-800BCF and added NOTE.

21-14-04-03 Modified proviso a) for the 737-800BCF.

21-15-03-02 Added proviso d) for the 737-800BCF and added NOTE.

21-15-03-03 Modified proviso a) for the 737-800BCF.

21-21-20 Removed from MMEL per PL-31, Revision 3 as it was moved to item 21-17 in
Revision 34a.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. III
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
21-32 Added “or Pack Flow Controller” to item heading.

21-33C Added NOTE.

21-38 Restructured provisos, added proviso b) for the 737-800BCF and added NOTE.

21-40-01B Removed "for airplanes with" between "and" and "recirculation" in column 4. Added
"if" in front of "installed" and parentheses.

21-40-02-01B Removed "for airplanes with" between "and" and "recirculation" in column 4. Added
"if" in front of "installed" and parentheses.

21-53 Added new relief item 21-53.

ATA 22 AUTOFLIGHT

22-07-01 Removed from MMEL as it was deleted in Revision 61 per PL-31, Revision 3.

22-07-02 Removed from MMEL as it was deleted in Revision 61 per PL-31, Revision 3.

22-09 Removed from MMEL as it was deleted in Revision 61 per PL-31, Revision 3.

22-10 Removed from MMEL as it was deleted in Revision 61 per PL-31, Revision 3.

22-11 Deleted (O) requirement.

22-15-02B Deleted (O) requirement.

22-18-01-02A Added proviso.

22-18-01-02B Deleted (O) requirement.

ATA 23 COMMUNICATIONS

23-01-01A Added NOTE.

23-01-02A Added NOTE.

23-02-01A Revised proviso b) per PL-9, Revision 12.

23-03-01-02B Added NOTE.

23-03-02 Revised number installed from “3” to “-“.

23-03-03 Added new relief item 23-03-03 with options 23-03-03A and 23-03-03B.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. IV
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
23-05 Removed from MMEL per PL-31, Revision 3 as it was moved to item 23-04 in
Revision 27.

23-07-01 Removed from MMEL per PL-31, Revision 3 as it was moved to item 23-04 in
Revision 27.

23-07-02 Removed from MMEL per PL-31, Revision 3 as it was moved to item 25-11 in
Revision 33.

23-08 Removed from MMEL per PL-31, Revision 3 as it was moved to item 25-11 in
Revision 33.

23-11-01 Added new relief item 23-11-01 with options 23-11-01A and 23-11-01B.

23-13-02 Added new relief item 23-13-02.

23-17 Added "***" denoting item 23-17 is optional equipment.

23-18-01 Added new relief item 23-18-01 with options 23-18-01A and 23-18-01B.

23-27 Deleted relief information, indicated options 23-27A and 23-27B have been
incorporated into Items 23-03, 23-11 and 23-18.

23-29 Added new relief item 23-29 with options 23-29A and 23-29B.

23-30 Added new relief item 23-30.

ATA 25 EQUIPMENT/FURNISHINGS

25-01 Revised provisos A and B per PL-132, Revision 0.

25-01-01 Added new relief item 25-01-01 per PL-132, Revision 0.

25-02 Removed from MMEL per PL-31, Revision 3 as it was moved to item 25-11 in
Revision 33.

25-05A Revised provisos per PL-100, Revision 3.

25-05B Revised repair interval and provisos per PL-100, Revision 3.

25-06 Revised item heading, provisos, and NOTES per PL-79, Revision 9.

25-06-02-01 Revised item heading and provisos per PL-79, Revision 9.

25-06-02-02 Revised item heading and proviso per PL-79, Revision 9.

25-06-03 Revised item heading and provisos per PL-79, Revision 9.

25-06-04 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 49.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. V
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
25-06-06 Added new relief item 25-06-06.

25-07 Removed from MMEL per PL-31, Revision 3 as it was moved to item 25-11 in
Revision 30.

25-08 Removed from MMEL per PL-31, Revision 3 as it was moved to item 52-08 in
Revision 30.

25-12-01 Split item 25-12-01 into new options 25-12-01A and 25-12-01B per PL-132,
Revision 0.

25-12 Revised item title.

25-12-01-01 Added new relief item 25-12-01-01 per PL-132, Revision 0.

25-12-02 Split item 25-12-02 into new options 25-12-02A and 25-12-02B per PL-132,
Revision 0.

25-12-02-01 Added new relief item 25-12-02-01 per PL-132, Revision 0.

25-15 Removed from MMEL per PL-31, Revision 3 as it was moved to item 21-41 in
Revision 33.

25-17-01A Revised provisos and added NOTE per PL-132, Revision 0.

25-17-01B Revised proviso per PL-132, Revision 0.

25-17-01-01 Added new relief item 25-17-01-01 per PL-132, Revision 0.

25-17-02A Revised provisos and added NOTE per PL-132, Revision 0.

25-17-02B Revised proviso per PL-132, Revision 0.

25-17-02-01 Added new relief item 25-17-02-01 per PL-132, Revision 0.

25-17-03 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 46.

25-17-04 Revised title per PL-132, Revision 0.

25-17-04A Revised provisos and added NOTE per PL-132, Revision 0.

25-17-04B Revised proviso per PL-132, Revision 0.

25-17-04-01 Added new relief item 25-17-04-01 per PL-132, Revision 0.

25-19 Removed from MMEL per PL-31, Revision 3 as it was moved to item 25-06 in
Revision 39.

25-20-02 Revised proviso to change the deferral period.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. VI
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
25-24A Revised NOTE to NOTE 1, added NOTE 2 per PL-104 Revision 7.

25-24C Added option 25-24C per PL-104 Revision 7.

ATA 26 FIRE PROTECTION

26-02-02 Revised proviso for clarification.

26-03 Removed (M) requirement, revised provisos and added NOTE per PL-132,
Revision 0.

26-03-01 Added new relief item 26-03-01 per PL-132, Revision 0.

26-04A Added proviso a).

26-04B Revised provisos and removed NOTE 1.

26-08-03 Added “***” denoting item 26-08-03 is optional equipment.

26-11 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 27.

26-12-01 Revised proviso a) to clarify “right engine bleed”.

26-12-02 Revised proviso a) to clarify “right engine bleed”.

26-14-04 Added NOTE.

26-20 Removed from MMEL per PL-31, Revision 3 as it was moved to item 26-19 in
Revision 39.

ATA 27 FLIGHT CONTROLS

27-02 Removed from MMEL as it was deleted in Revision 27 per PL-31, Revision 3.

27-04-01B Revised proviso a) for clarification.

27-04-02B Revised proviso a) for clarification.

27-06 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 22-05 in
Revision 27.

27-07-01 Added NOTE.

27-07-03 Added NOTE.

27-09 Removed from MMEL as it was deleted in Revision 61 per PL-31, Revision 3.

27-13 Removed from MMEL as it was deleted in Revision 61 per PL-31, Revision 3.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. VII
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
27-20-01-01A Added NOTE.

27-20-01-02A Added NOTE

27-20-03A Added NOTE.

27-23 Revised Installed and Required Quantity and proviso to clarify “per elevator”.

ATA 28 FUEL

28-02C Revised NOTE.

28-02-01 Added NOTE.

28-13 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 22-05 in
Revision 27.

28-24 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 28-10 in
Revision 47a.

28-25-01A Added NOTE.

28-26 Replaced "deactivated" with "provided Fuel Shutoff Valve Battery and Charger is
deactivated" in column 4.

ATA 29 HYDRAULIC POWER

29-03-01 Revised proviso a) to clarify “associated system”.

29-03-02 Revised proviso a) to clarify “associated system”.

29-06 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 32-13 in
Revision 33.

29-11-01 Revised provisos a) and b) to clarify “associated” quantity and system.

29-11-02 Revised provisos a), b) and c) to clarify “associated” quantity, system and pump.

29-14 Removed from MMEL per PL-31, Revision 3 as it was incorporated into Item 29-07 in
Revision 39.

29-15 Revised provisos a), b) and c) to clarify “associated” quantity, system and pump.

ATA 30 ICE AND RAIN PROTECTION

30-03-02B Added NOTE.

30-03-03B Added NOTE.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. VIII
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
30-04-04 Added NOTE.

30-11-02 Added proviso e).

30-11-03 Added proviso d).

30-18B Added NOTE.

30-22 Added new relief item 30-22, with subitems 30-22-01 and 30-22-02.

ATA 31 INDICATING/RECORDING SYSTEMS

31-03 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 34-41.

31-05 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 23-10.

31-12 Deleted in Revision 62.

31-12A Deleted in Revision 62.

31-12B Deleted in Revision 62.

31-14-01 Removed from MMEL as it was deleted in Revision 57 per PL-31, Revision 3.

31-14-02 Removed from MMEL as it was deleted in Revision 57 per PL-31, Revision 3.

ATA 33 LIGHTS

33-06A Added “winglet” to proviso.

33-06B Added “wingtip” to proviso a).

33-06-01-02 Removed from MMEL per PL-31, Revision 3 as it was incorporated into Item 33-06 in
Revision 45a.

33-11-02-01 Removed from MMEL as it was deleted in Revision 49a per PL-31, Revision 3.

33-13 Removed from MMEL as it was deleted in Revision 27 per PL-31, Revision 3.

33-21-02 Added -800BCF airplane applicability.

33-22-03 Removed from MMEL as it was deleted in Revision 49 per PL-31, Revision 3.

33-22-04 Removed from MMEL as it was deleted in Revision 49 per PL-31, Revision 3.

33-26 Added -800BCF airplane applicability.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. IX
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
ATA 34 NAVIGATION

34-06 Removed from MMEL as it was deleted in Revision 27 per PL-31, Revision 3.

34-10 Removed from MMEL as it was deleted in Revision 27 per PL-31, Revision 3.

34-17-03-03 Removed from MMEL as it was deleted in Revision 52 per PL-31, Revision 3.

34-18A Revised number installed from “-” to “2”.

34-18B Revised number installed from “-” to “2”.

34-18-02 Revised item heading per PL-105 Revision 4.

34-18-02A Revised repair interval and proviso per PL-105 Revision 4.

34-18-02B Removed NOTE and revised proviso per PL-105 Revision 4.

34-18-02C Added new option 34-18-02C per PL-105 Revision 4.

34-20-01-03 Revised NOTE for clarification.

34-24 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 34-01 in
Revision 50.

34-31 Added airplane applicability (-100/-200/-300/-400/-500) to the item heading.

34-34 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 34-03 in
Revision 30.

34-36-02-02-02 Added (M) requirement, proviso and NOTE.

34-39 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 34-01 in
Revision 50.

34-50 Removed from MMEL per PL-31, Revision 3 as it was incorporated into Item 34-17 in
Revision 37.

ATA 35 OXYGEN

35-01 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 27.

35-03-05 Revised number installed from “1” to “-”.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. X
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
35-04 Revised item heading, removed (M) requirement, revised provisos, and added
NOTES per PL-132 Revision 0.

35-04-01 Added new relief item 35-04-01 per PL-132 Revision 0.

35-06 Revised provisos per PL-132 Revision 0.

35-06-01 Added new relief item 35-06-01 per PL-132 Revision 0.

ATA 36 PNEUMATIC

36-05-02 Split item 36-05-02 into new option 36-05-02A and option 36-05-02B.

ATA 38 WATER/WASTE

38-02 Revised item heading per PL-83, Revision 8.

38-02B Deleted proviso b), revised former proviso c) to proviso b) and revised proviso b) per
PL-83, Revision 8.

ATA 46 INFORMATION SYSTEMS

46-01-05 Added "Supply/Power" to item title.

46-01-06A Added "stowed, secured" and comma after "means" in list item a) in column 4.

46-01-06B Added "stowed, secured" and comma after "means" in list item a) in column 4.

ATA 52 DOORS

52-15-01 Added new proviso a).

52-15-02 Added new proviso a).

52-17-04 Corrected spelling of “Flight” in item title.

52-17-05 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 52-20 in
Revision 46.

ATA 73 ENGINE FUEL AND CONTROL

73-09 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 30.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XI
DATE: 11/28/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Boeing B-737
ITEM NO. EXPLANATION OF CHANGE
ATA 77 ENGINE INDICATING

77-04 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 73-05 in
Revision 30.

77-07 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 34-41 in
Revision 30.

77-08 Removed from MMEL per PL-31, Revision 3 as it was moved to Item 73-06 in
Revision 30.

ATA 78 ENGINE EXHAUST

78-03 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 30.

ATA 79 ENGINE OIL

79-03 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 27.

79-04-01 Added new relief item 79-04-01.

79-05 Removed from MMEL per PL-31, Revision 3 as it was deleted in Revision 27.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XII
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737

With this MMEL Revision 62, stated policy from the following list of FAA MMEL Policy Letters (PL) has
been applied to the appropriate items listed on this MMEL, as applicable.

Note: The FAA MMEL Policy Application Record is not required to be incorporated into an operators
MEL submission or final approval.

Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-001 Wide-Body Passenger Airplane Door/Slide Relief Revision 4 N/A
02/27/2010

PL-002 Aural and Visual Speed Warning Policy Revision 1 N/A

08/15/1997

PL-003 DME Systems MMEL Policy Revision 1 34-13

08/15/1997

PL-005 Takeoff Warning Systems Revision 1 N/A

08/15/1997

PL-009 Public Address System, Crewmember Interphone Revision 12 23-02-01,

and Alerting Systems 10/23/2015 23-02-01-01,
23-02-02,
23-02-02-01,
23-04-01-01,
23-04-01-02A,
23-04-01-03-01,
23-04-01-03-02,
23-04-02-01,
23-04-02-02,
23-04-02-03-01,
23-04-02-03-02,
23-20-01-01,
23-20-01-02A,
23-20-02-01,
23-20-02-02,
23-19-01-01,
23-19-01-02,
23-19-01-03,
23-19-01-04,
23-19-02-01,
23-19-02-02,
23-19-02-03,
23-19-02-04

PL-013 Oil Temperature and Pressure Instrument MEL Revision 1 79-04

Policy 08/15/1997
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XIII
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737
Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-024 Lavatory Fire Protection Revision 5 26-15-01,
10/23/2015 26-15-02,
26-16-01,
26-16-02

PL-025 MMEL and MEL Definitions Revision 22 As Applicable

08/19/2021

PL-026 Thrust Reversers on Small Turbojet Airplanes Revision 1 N/A

08/15/1997

PL-029 Master Minimum Equipment List (MMEL) Revision 5 23-10-01

Requirements for Cockpit Voice Recorder (CVR) 08/10/2010

PL-031 MMEL Format Specification Revision 3 As Applicable

01/20/2011

PL-032 Traffic Alert and Collision Avoidance System Revision 7 34-40,

(TCAS) 07/07/2006 34-40-01,
34-40-02,
34-40-03,
34-40-04,
34-40-05

PL-034 MMEL and MEL Preamble Revision 4 As Applicable

08/15/1997

PL-036 FAR Part 91 MEL Approval & Preamble Revision 3 As Applicable

06/16/2020

PL-038 Policy Regarding MMEL Relief for Primary Thrust Revision 1 N/A
Setting Instruments on Two-Engine Airplanes 08/15/1997

PL-039 Altitude Alerting Systems Revision 5 34-25,

01/29/2010 34-25-01,
34-25-02

PL-040 ETOPS and Polar Operations Revision 3 As Applicable

11/10/2020

PL-045 Time Limited Dispatch (TLD) Authorization for Full Revision 2 N/A
Authority Digital Electronic Control (FADEC) 03/04/2004
Engines
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XIV
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737
Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-054 Terrain Awareness and Warning System (TAWS) Revision 10 34-26-01,
10-31-2005 34-26-01-01,
34-26-01-02,
34-26-01-03,
34-26-01-04,
34-26-01-05,
34-26-02,
34-26-03,
34-26-04

PL-056 Flight Deck FWD Observer Seat Revision 5 25-11-01,

01/01/2012 25-11-02,
25-11-04

PL-058 Flight Deck Headsets and Hand Microphones Revision 4 23-14-01,

03/24/2012 23-14-02,
23-14-03,
23-17

PL-063 Instrument and Equipment Items Required for Revision 4 As Applicable

Emergency Procedures 07/05/2012

PL-064 Electrical Power MMEL Policy - Four Engine Revision 1 N/A

Cargo Airplanes 08/15/1997

PL-065 Policy Regarding Cargo Provisions in the MMEL Revision 1 N/A

for Cargo Operations 08/15/1997

PL-067 Windshear Warning and flight Guidance System Revision 4 34-15-03,

(RWS) Windshear Detection and Avoidance 01/15/2012 34-26-01-05
System (PWS)

PL-069 External Door Indication System Revision 2 52-03

09/24/2003

PL-072 Wing Icing Detection Lights Revision 4 33-07

03/12/2012

PL-076 ATC Transponders and Automatic Altitude Revision 7 34-18,

Reporting Systems 12/04/2017 34-18-01

PL-077 Cockpit and Instrument Lighting Systems Revision 4 33-01

12/17/2012
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XV
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737
Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-079 Passenger Seat Relief Revision 9 25-06,
12/05/2017 25-06-02-01,
25-06-02-02,
25-06-03,
25-06-05-01,
25-06-05-02

PL-083 Water and Waste Systems on Air Carrier Aircraft Revision 8 38-01,
05/11/2015 38-02

PL-084 Master Minimum Equipment List (MMEL) for Revision 1 34-25

Reduced Separation Minimum (RVSM) 08/15/1997
Operations

PL-087 Flight Data Recorder (FDR) Revision 10 31-02-01

08/10/2010

PL-089 FASTEN SEAT BELT WHILE SEATED Signs or Revision 2 25-09

Placards 01/31/2009

PL-090 Pitot Heat Indicating System Revision 1 30-05-01,

09/20/2001 30-05-02

PL-093 Autopilot Disconnect MMEL Policy Revision 1 22-01-01-01A,

09/11/2006 22-01-01-02A

PL-094 Liquid or Paste Propeller Deicer Revision 1 N/A

10/08/2004

PL-095 VHF Communications MMEL Requirements Revision 2 23-03,

01/15/2012 23-03-01-01,
23-03-01-02,
23-03-01-03,
23-03-01-04

PL-096 Galley/Cabin Waste Receptacles Access Revision 2 25-22-01

Doors/Covers 01/29/2010

PL-097 Flight Attendant Seat(s) Revision 4 25-03-01,

09/06/2007 25-03-02,
25-03-03

PL-098 Navigation Databases Revision 1 34-36-01-04,

06/01/2017 34-36-02-05,
34-36-03-06
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XVI
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737
Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-099 Door/Slide Relief Policy Revision 2 52-16
02/26/2010

PL-100 MMEL/MEL Relief for Cargo Restraint Revision 3 25-05

Components 10/02/2020

PL-101 Autopilot Relief Revision 2 22-01

12/15/2011

PL-102 Cargo Compartment Smoke Detection and Fire Revision 2 26-19

Suppression Systems 12/17/2012

PL-104 Storage Bins/Cabin, Galley and Lavatory Storage Revision 7 25-24,

Compartments/Closets 06/24/2020 25-24-02

PL-105 Automatic Dependent Surveillance-Broadcast Revision 4 34-18-02

(ADS-B) System 02/08/2021

PL-106 High Frequency (HF) Communications Revision 5 23-11

06/06/2014

PL-107 MMEL Relief for Inoperative APU Generator Revision 1 N/A

05/22/2001
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XVII
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737
Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-108 Carriage of Empty Cargo Handling Equipment Revision 1 21-01-01-05,
10/17/2011 21-01-01-06,
21-01-01-07,
21-01-02,
21-01-02-02,
21-01-04C,
21-01-05B,
21-02-03,
21-04-02-02,
21-06-02-02,
21-10-02-03,
21-12-02-03,
21-13-02-03,
21-14-03-03,
21-14-04-03,
21-15-02-04,
21-15-03-03,
21-16-02-03,
21-26-01,
21-26-02-03,
21-40-02-03,
21-45-02,
21-45-03,
21-45-03-01,
21-45-03-02,
21-45-04A,
25-16,
26-14,
26-19,
52-06-04,
52-10-01

PL-109 Supplemental Type Certificate (STC) MMEL/MEL Revision 1 As Applicable

Relief Process 11/07/2019

PL-111 MMEL Policy for Inoperative Standby Attitude Revision 1 34-07-01

Indicator 01/29/2004

PL-112 Relief for 14 CFR 25.795 Compliant Flight Deck Revision 2 52-18,
Doors 01/18/2012 52-19,
52-20-02

PL-113 MMEL Relief for Anti-Skid Inoperative Revision 0 32-02-01,

12/20/2002 32-02-02
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XVIII
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737
Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-114 Nose Gear Steering Systems Revision 1 32-08
10/09/2012

PL-117 Selective Call System (SELCAL) Revision 0 23-06

10/07/2005 23-06-01

PL-119 Two-Section MMELs (Parts 91, 125, and 135) Revision 4 N/A
12/04/2017

PL-120 Emergency Locator Transmitters (ELT) Revision 3 23-12-01,

04/12/2019 23-12-02,
23-12-02-01,
23-12-02-02

PL-121 (EFB) Electronic Flight Bag Revision 1 46-01-01,

05/05/2021 46-01-04,
46-01-05,
46-01-06

PL-122 Flight Deck Door Surveillance Systems Revision 1 23-21,

10/09/2012 23-21-01,
52-23,
52-23-01

PL-123 Passenger Notice System (Lighted Information Revision 1 33-03-01,

Signs) 04/30/2010 33-03-02

PL-124 Damaged Window/Windshield Relief Revision 0 N/A

01/20/2009

PL-125 Equipment Relief without Passengers Revision 1 N/A

11/27/2012

PL-126 Chelton FlightLogic Electronic Flight Instrument Revision 0 N/A

Systems (EFIS) 05/28/2010

PL-127 Night Vision Imaging Systems (NVIS) Revision 0 N/A

06/07/2010

PL-129 Cockpit Smoke Vision Systems (CSVS) Revision 0 25-28

03/12/2012

PL-130 Flightcrew Rest Facilities (FCRF) Revision 2 N/A

03/12/2021
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. XIX
DATE: 11/28/2022
AIRCRAFT:
FAA MMEL POLICY APPLICATION RECORD
Boeing B-737
Affected Item
PL Revision and Sequence
PL No. Subject
Date Number(s)
PL-131 Radar (Radio) Altimeters for Rotorcraft Revision 0 N/A
10/23/2019

PL-132 Portable Emergency Equipment Revision 0 25-01,

05/03/2021 25-01-01,
25-12-01,
25-12-01-01,
25-12-02,
25-12-02-01,
25-17-01,
25-17-01-01,
25-17-02,
25-17-02-01,
25-17-04,
25-17-04-01,
26-03,
26-03-01,
35-04,
35-04-01,
35-06,
35-06-01
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 60 PAGE NO. XX
DATE: 02/09/2018
AIRCRAFT:
DEFINITIONS
Boeing B-737

Refer to the current FAA MMEL Policy Letter 25, MMEL and MEL Definitions, found on the FAA Flight
Standards Information Management System (FSIMS) website.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 60 PAGE NO. XXI
DATE: 02/09/2018
AIRCRAFT:
PREAMBLE
Boeing B-737

For the MMEL, Preamble used for operations under 14 CFR Parts 121, 125, 129, and 135, refer to the
current FAA Policy Letter PL-34, MMEL and MEL Preamble, or for the preamble used for 14 CFR
Part 91 operations, refer to MMEL Policy PL-36, 14 CFR Part 91 MEL and Preamble. Both preambles
may be found on the FAA Flight Standards Information Management System (FSIMS) website.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 60 PAGE NO. XXII
DATE: 02/09/2018
AIRCRAFT:
GUIDELINES FOR (M) AND (O) PROCEDURES
Boeing B-737

The FOEB has identified a need for certain procedures to provide an adequate level of safety while
providing relief for some items. These procedures must be established by the operator and may be
based on the aircraft manufacturer’s recommended procedures, Supplemental Type Certificate
modifier’s recommended procedures, or equivalent operator procedures. When recommended
procedures are published, the operator should comply with these procedures.

(M) and (O) Procedures are based on the Maintenance and Operational Procedures published in the
Boeing 737 Dispatch Deviations Guide (DDG).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

01-01 All-Passenger
Configuration
(All Models)

01-01-01 (-100/-200/-300/-400/ C 2 1 (O) Except for ER operations, one

-500/-600 and -700/-800 may be inoperative provided flight
without PATS Auxiliary altitude remains at or below FL 250.
Fuel Tanks)

01-01-02 (-700IGW/-800 with C 2 1 (M)(O) Except for ER operations, one

PATS Auxiliary Fuel may be inoperative provided:
Tanks) a) Flight altitude remains at or
below FL 250, and
b) For airplanes with auxiliary
fuel bleed air pressurization
system installed, is verified to
be operational before each
departure.

01-01-03 (-900/-900ER) C 2 1 (M)(O) Except for ER operations, one

may be inoperative provided:
a) Flight altitude remains at or
below FL 250,
b) Forward cargo heat duct is
secured closed, and
c) Airport ambient temperature
does not exceed 103 °F
(39 °C).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-01 All-Passenger
Configuration
(All Models)
(Cont’d)

01-01-04 (-100/-200) C 2 0 (M)(O) Except for ER operations,

both may be inoperative provided
flight is conducted in an
unpressurized configuration.

01-01-05 (-300/-400/-500) C 2 0 (M)(O) Except for ER operations,

both may be inoperative provided:
a) Flight is conducted in an
unpressurized configuration,
and
b) Procedures are established
and used to ensure lower
cargo compartments remain
empty or are verified to
contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-01 All-Passenger
Configuration
(All Models)
(Cont’d)

01-01-06 (-600/-700/-800) C 2 0 (M)(O) Except for ER operations,

both may be inoperative provided:
a) Flight is conducted in an
unpressurized configuration,
b) Recirculation fan(s) operates
normally,
c) Both E/E equipment cooling
exhaust fans operate
normally,
d) Procedures are established
and used to ensure lower
cargo compartments remain
empty or are verified to
contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits,
and
e) Airplanes with Auxiliary tanks
installed, auxiliary tanks
remain empty or auxiliary fuel
is included as part of zero fuel
weight.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-01 All-Passenger
Configuration
(All Models)
(Cont’d)

01-01-07 (-900/-900ER) C 2 0 (M)(O) Except for ER operations,

both may be inoperative provided:
a) Flight is conducted in an
unpressurized configuration,
b) Recirculation fans operate
normally,
c) Both E/E equipment cooling
exhaust fans operate
normally,
d) Procedures are established
and used to ensure lower
cargo compartments remain
empty or are verified to
contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits,
e) Forward cargo heat duct is
secured closed, and
f) Airport ambient temperature
does not exceed 103 °F
(39 °C).

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-02 Combi and All-Cargo C 2 0 (M)(O) Except for ER operations,

Configurations both may be inoperative provided:
(737C, QC, and STCs a) Flight is conducted in an
ST01566LA, unpressurized configuration,
ST01961SE, and and
ST02556SE) b) Procedures are established
and used to ensure main deck
cargo compartment remains
empty or is verified to contain
only empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

01-02-01 Right Pack C 1 0 (O) Except for ER operations, may be

inoperative provided flight altitude
remains at or below FL 250.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-02 Combi and All-Cargo

Configurations
(737C, QC, and STCs
ST01566LA,
ST01961SE, and
ST02556SE)
(Cont’d)

01-02-02 Left Pack C 1 0 (O) Except for ER operations, may be

inoperative provided:
a) Flight Altitude remains at or
below FL 250, and
b) Procedures are established
and used to ensure main deck
cargo compartment remains
empty or is verified to contain
only empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

01-03 All-Cargo Configuration C 2 1 (O) Except for ER operations, may be

(-700C) inoperative provided flight altitude
remains at or below FL 250.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-04 Pemco COMBI

(STC ST03387AT)
and All-Cargo
Configurations

01-04A C 2 1 Except for ER operations, one may

be inoperative provided only flight
deck is occupied.

01-04B C 2 1 (O) Except for ER operations, one

may be inoperative provided flight
altitude remains at or below FL 250.

01-04C C 2 0 (M)(O) Except for ER operations,

may be inoperative provided:
a) Flight is conducted in an
unpressurized configuration,
and
b) Procedures are established
and used to ensure main deck
cargo compartment remains
empty or is verified to contain
only empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-05 All-Cargo Configuration

(STC ST01827LA and
ST00283AT)

01-05A C 2 1 (O) Except for ER operations, one

may be inoperative provided flight
altitude remains at or below FL 250.

01-05B C 2 0 (M)(O) Except for ER operations,

may be inoperative provided:
a) Flight is conducted in an
unpressurized configuration,
and
b) Procedures are established
and used to ensure the main
deck cargo compartments
remain empty or are verified
to contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in the Fly Away Kits
and which materials can be
used as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

01 Air Conditioning Packs

(Cont’d)

01-06 All-Cargo Configuration

(-800BCF)

01-06A C 2 1 (O) Except for ER operations, may be

inoperative provided flight altitude
remains at or below FL 250.

01-06B Deleted in Revision 62. |

02 Pack Air Flow/Shutoff C 2 0 (M)(O) May be inoperative

Valves deactivated closed.
(Includes
STC SA2969SO)

02-01 High Flow Mode C 2 0

(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)

02-02 APU High Flow Mode C 2 0

02-03 Electronic Flow Control C 2 0 (O) May be inoperative provided: |

(-800/-900ER Line a) Appropriate performance |
Numbers 5684, and adjustments are applied, and |
5759 and subsequent) b) Procedures are established |
and used to ensure aft lower |
cargo compartment remains |
empty or is verified to contain |
only empty cargo handling |
equipment, ballast (ballast |
may be loaded in ULDs), |
and/or Fly Away Kits. |

NOTE: Operator MELs must define |

which items are approved for |
inclusion in the Fly Away Kits |
and which materials can be |
used as ballast. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

02 Pack Air Flow/Shutoff

Valves
(Includes
STC SA2969SO)
(Cont’d)

02-04 Position Indicator Switch

Discrete Signal |

02-04A C 2 1 May be inoperative failed open

provided both air conditioning packs
operate normally.

02-04B C 2 1 May be inoperative failed closed

provided both air conditioning packs
operate normally.

02-05 Pack Flow Sensors |

(-800/-900ER Line |
Numbers 5684, and |
5759 and subsequent) |

02-05A C 2 0 (M) May be inoperative provided pack |

inlet pressure sensor(s) for |
associated air conditioning pack(s) is |
verified to operate normally. |

02-05B C 2 0 Maybe inoperative provided |

associated Electronic Flow Control is |
considered inoperative. |

NOTE: Refer to MMEL Item 21-02-03, |

Electronic Flow Control. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 5. REPAIR CATEGORY
6. NO. INSTALLED
Boeing B-737 7. NO. REQUIRED FOR DISPATCH
8. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

02 Pack Air Flow/Shutoff

Valves
(Includes
STC SA2969SO)
(Cont’d)

02-06 Pack Inlet Pressure |

Sensors |
(-800/-900ER Line |
Numbers 5684, and |
5759 and subsequent) |

02-06A C 2 0 (M) May be inoperative provided pack |

flow sensor(s) for associated air |
conditioning pack(s) is verified to |
operate normally. |

02-06B C 2 0 Maybe inoperative provided |

associated Electronic Flow Control is |
considered inoperative. |

NOTE: Refer to MMEL Item 21-02-03, |

Electronic Flow Control. |

03 Pack Trip Warning C 2 0 (M)(O) May be inoperative provided

Systems associated pack is not used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

04 Pack Turbofan
(-100/-200/-300/-400/
-500)

04-01 All-Passenger C 2 0 (O) May be inoperative provided

Configuration associated pack(s) is operated only in
(All Models) flight with flaps retracted.

04-02 Combi and All-Cargo

Configurations
(737C, QC,
STCs SA2969SO,
ST01566LA, and
ST01961SE)

04-02-01 Right Pack Turbofan C 1 0 (O) May be inoperative provided right

pack is operated only in flight with
flaps retracted.

04-02-02 Left Pack Turbofan C 1 0 (O) May be inoperative provided:

a) Left pack is operated only in
flight with flaps retracted, and
b) Procedures are established
and used to ensure main deck
cargo compartment remains
empty or is verified to contain
only empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

04 Pack Turbofan
(-100/-200/-300/-400/
-500)
(Cont’d)

04-03 All-Cargo Configuration C 2 0 (M)(O) May be inoperative closed

(STCs ST01827LA and provided associated pack(s) is
ST00283AT) operated only in flight with flaps
retracted.

05 Pack Ram Air Systems C 2 0 (M)(O) May be inoperative in FLIGHT

OPEN position provided:
a) Operations are not conducted
on runways covered with
slush or on gravel runways,
and
b) Associated pack is not
operated during takeoff or
landing on wet runways or
runways with standing water.

05-01 Exhaust Louver C 2 0 (M)(O) May be inoperative provided:

*** Assemblies a) Actuator(s) is disconnected,
(-100/-200/-300/-400/ and
-500) b) Louver(s) is secured in full
open position.

06 Pack Turbofan Valves

(-100/-200/-300/-400/
-500)

06-01 All-Passenger C 2 0 (M)(O) May be inoperative closed

Configuration provided associated pack(s) is
(All Models) operated only in flight with flaps
retracted.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

06 Pack Turbofan Valves

(-100/-200/-300/-400/
-500)
(Cont’d)

06-02 Combi and All-Cargo

Configurations
(737C, QC,
STCs SA2969SO,
ST01566LA, and
ST01961SE)

06-02-01 Right Pack Turbofan C 1 0 (M)(O) May be inoperative closed

Valve provided right pack is operated only
in flight with flaps retracted.

06-02-02 Left Pack Turbofan C 1 0 (M)(O) May be inoperative closed

Valve provided:
a) Left pack is operated only in
flight with flaps retracted, and
b) Procedures are established
and used to ensure main deck
cargo compartment remains
empty or is verified to contain
only empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

06-03 All-Cargo Configuration C 2 0 (M)(O) May be inoperative closed

(STCs ST01827LA and provided associated pack(s) is
ST00283AT) operated only in flight with flaps
retracted.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

07 RAM DOOR FULL C 2 0

OPEN Indicating Lights

08 Air Mix Valves C 2 0 (M)(O) May be inoperative provided

(-100/-200/-300/-500/ associated pack is not used.
-600/-700)

09 Air Mix Valve Position C 2 0

Indicators
(-100/-200/-300/-500/
-600/-700)

10 Cabin Rate of Climb

Indicator

10-01 Analog Control System

(-100/-200/-300/-400/
-500)

10-01A C 1 0 May be inoperative provided AUTO

and STBY control modes operate
normally.

10-01B C 1 0 (M)(O) May be inoperative provided

flight is conducted in an
unpressurized configuration.

10-02 Digital Control System C 1 0 May be inoperative provided AUTO

(-300/-400/-500/-600/ and ALTN control modes operate
-700/-800/-800BCF/ normally.
-900/-900ER)

10-02-01 (-300/-400/-500) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
and
b) Outflow valve is positioned to
25% open position.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

10 Cabin Rate of Climb

Indicator
(Cont’d)

10-02 Digital Control System

(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

10-02-02 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Prior to a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Outflow valve is positioned to
737-26-1121 and 25% open position, and
737-26-1122, and either c) Recirculation fan(s) operates
737-21-1135, or normally except for -800BCF
737-21-1163 or their airplane.
Production Equivalents)

10-02-03 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Upon a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Procedures are established
737-26-1121 and and used to ensure lower
737-26-1122, and either forward cargo compartment
737-21-1135, or remains empty, or is verified
737-21-1163 or their to contain only empty cargo
Production Equivalents) handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.
c) Outflow valve is positioned to
25% open position, and
d) Recirculation fan(s) operates
normally except for -800BCF
airplane.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

10 Cabin Rate of Climb

Indicator
(Cont’d)

10-02 Digital Control System

(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

10-02-04 (-900/-900ER) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
b) Outflow valve is positioned to
25% open position,
c) Recirculation fan(s) operates
normally,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

11 Cabin Altitude Warning C 1 0 May be inoperative provided flight

System altitude remains at or below
10,000 ft. MSL.

11-01 High Altitude Warning C 1 0 May be inoperative provided

*** System procedures do not require its use.

11-02 CABIN ALTITUDE Light

|
11-02-03 -600/-700/-800/ C 2 1 (O) May be inoperative provided: |
-800BCF/-900/ a) Associated TAKEOFF |
-900ER CONFIG warning light |
(Upon Incorporation of operates normally, and |
Boeing Service Bulletin b) Before engine start for the first |
737-31A1332, or flight of the day, or following |
Production Equivalent) any change of either |
STC ST03312NY flightcrew member, the |
flightcrew performs a briefing |
on cabin altitude warning |
indications and procedures. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

12 Cabin Altitude Indicator

12-01 Analog Control System

(-100/-200/-300/-400/
-500)

12-01A C 1 0 May be inoperative provided:

a) Cabin differential pressure
indicator operates normally,
and
b) A chart is provided to crew to
convert differential pressure to
cabin altitude.

12-01B C 1 0 (M)(O) May be inoperative provided

flight is conducted in an
unpressurized configuration.

12-02 Digital Control System C 1 0 May be inoperative provided:

(-300/-400/-500/-600/ a) Cabin differential pressure
-700/-800/-800BCF/ indicator operates normally,
-900/-900ER) and
b) A chart is provided to crew to
convert differential pressure to
cabin altitude.

12-02-01 (-300/-400/-500) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
and
b) Outflow valve is positioned to
25% open position.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-20
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

12 Cabin Altitude Indicator

(Cont’d)

12-02 Digital Control System

(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

12-02-02 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Prior to a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Outflow valve is positioned to
737-26-1121 and 25% open position, and
737-26-1122, and either c) Recirculation fan(s) operates
737-21-1135 or normally except for -800BCF
737-21-1163 or their airplane.
Production Equivalents)

12-02-03 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Upon a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Procedures are established
737-26-1121 and and used to ensure lower
737-26-1122, and either forward cargo compartment
737-21-1135 or remains empty or is verified to
737-21-1163 or their contain only empty cargo
Production Equivalents) handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.
c) Outflow valve is positioned to
25% open position, and
d) Recirculation fan(s) operates
normally except for -800BCF
airplane.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-21
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

12 Cabin Altitude Indicator

(Cont’d)

12-02 Digital Control System

(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

12-02-04 (-900/-900ER) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
b) Outflow valve is positioned to
25% open position,
c) Recirculation fan(s) operates
normally,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-22
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

13 Cabin Differential
Pressure Indicator

13-01 Analog Control System

(-100/-200/-300/-400/
-500)

13-01A C 1 0 May be inoperative provided:

a) Cabin altitude indicator
operates normally, and
b) A chart is provided to crew to
convert cabin altitude to
differential pressure.

13-01B C 1 0 (M)(O) May be inoperative provided

flight is conducted in an
unpressurized configuration.

13-02 Digital Control System C 1 0 May be inoperative provided:

(-300/-400/-500/-600/ a) Cabin altitude indicator
-700/-800/-800BCF/ operates normally, and
-900/-900ER) b) A chart is provided to crew to
convert cabin altitude to
differential pressure.

13-02-01 (-300/-400/-500) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
and
b) Outflow valve is positioned to
25% open position.

13-02-02 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Prior to a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Outflow valve is positioned to
737-26-1121 and 25% open position, and
737-26-1122, and either c) Recirculation fan(s) operates
737-21-1135 or normally except for -800BCF
737-21-1163 or their airplane.
Production Equivalents)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-23
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

13 Cabin Differential
Pressure Indicator
(Cont’d)

13-02 Digital Control System

(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

13-02-03 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Upon a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Procedures are established
737-26-1121 and and used to ensure lower
737-26-1122, and either forward cargo compartment
737-21-1135 or remains empty or is verified to
737-21-1163 or their contain only empty cargo
Production Equivalents) handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.
c) Outflow valve is positioned to
25% open position, and
d) Recirculation fan(s) operates
normally except for -800BCF
airplane.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

13-02-04 (-900/-900ER) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
b) Outflow valve is positioned to
25% open position,
c) Recirculation fan(s) operates
normally,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-24
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

14 Cabin Pressure Control

System

14-01 Analog Control System C 2 1 (O) One may be inoperative provided

Automatic/Standby manual mode (AC and DC actuators)
Modes operates normally.
(-100/-200/-300/
-400/-500)

14-02 Analog Control C 3 0 (M)(O) May be inoperative for

Automatic/Standby/ unpressurized flight provided:
Manual Modes a) Outflow valve is deactivated
(-100/-200/ open or removed, and
-300/-400/-500) b) Extended overwater flight is
prohibited.

14-03 Digital Control System C 2 1 (M)(O) One may be inoperative

Automatic Modes provided:
(-300/-400/-500/-600/ a) Manual mode operates
-700/-800/-800BCF/ normally,
-900/-900ER) b) Inoperative controller is
deactivated, and
c) For airplanes with auxiliary
fuel bleed air pressurization
system installed, is verified to
be operational before each
departure if the auxiliary fuel
tank system is required for
flight.

14-03-01 (-300/-400/-500) C 2 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed, and
b) Extended overwater flight is
prohibited.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-25
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

14 Cabin Pressure Control

System
(Cont’d)

14-03 Digital Control System

Automatic Modes
(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

14-03-02 (-600/-700/-800/ C 2 0 (M)(O) May be inoperative for

-800BCF Prior to unpressurized flight provided:
Incorporation of Boeing a) Outflow valve is deactivated in
Service Bulletins 25% open position or
737-26-1121 and removed,
737-26-1122, and either b) Recirculation fan(s) operates
737-21-1135 or normally except for -800BCF
737-21-1163 or their airplane,
Production Equivalents) c) Extended overwater flight is
prohibited, and
d) Airplanes with auxiliary tanks
installed, auxiliary tanks
remain empty or auxiliary fuel
is included as part of zero fuel
weight.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-26
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

14 Cabin Pressure Control

System
(Cont’d)

14-03 Digital Control System

Automatic Modes
(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

14-03-03 (-600/-700/-800/ C 2 0 (M)(O) May be inoperative for

-800BCF Upon unpressurized flight provided:
Incorporation of Boeing a) Procedures are established
Service Bulletins and used to ensure lower
737-26-1121 and forward cargo compartment
737-26-1122, and either remains empty, or is verified
737-21-1135 or to contain only empty cargo
737-21-1163 or their handling equipment, ballast
Production Equivalents) (ballast may be loaded in
ULDs), and/or Fly Away Kits,
b) Outflow valve is deactivated in
25% open position or
removed,
c) Recirculation fan(s) operates
normally except for -800BCF
airplane,
d) Extended overwater flight is
prohibited, and
e) Airplanes with auxiliary tanks
installed, auxiliary tanks
remain empty or auxiliary fuel
is included as part of zero fuel
weight.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-27
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

14 Cabin Pressure Control

System
(Cont’d)

14-03 Digital Control System

Automatic Modes
(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

14-03-04 (-900/-900ER) C 2 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed,
b) Recirculation fan(s) operates
normally,
c) Extended overwater flight is
prohibited,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-28
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

14 Cabin Pressure Control

System
(Cont’d)

14-04 Digital Control System

Manual Mode
(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)

14-04-01 (-300/-400/-500) C 1 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed, and
b) Extended overwater flight is
prohibited.

14-04-02 (-600/-700/-800 C 1 0 (M)(O) May be inoperative for

All-Passenger unpressurized flight provided:
Configuration/-800BCF a) Outflow valve deactivated to
Prior to Incorporation of 25% open position or
Boeing Service Bulletins removed,
737-26-1121 and b) Recirculation fan(s) operates
737-26-1122, and either normally except for -800BCF
737-21-1135 or airplane, |
737-21-1163 or their c) Extended overwater flight is
Production Equivalents) prohibited, and |
d) For -800BCF, procedures are |
established and used to |
ensure main deck cargo |
compartment remain empty, |
or are verified to contain only |
cargo handling equipment, |
ballast (ballast may be loaded |
in ULDs), and /or fly away |
kits. |

NOTE: Operator MELs must define |

which items are approved for |
inclusion in Fly Away Kits and |
which materials can be used |
as ballast. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-29
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

14 Cabin Pressure Control

System
(Cont’d)

14-04 Digital Control System

Manual Mode
(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

14-04-03 (-600/-700/-800 C 1 0 (M)(O) May be inoperative for

All-Passenger unpressurized flight provided:
Configuration/-800BCF a) Procedures are established
Upon Incorporation of and used to ensure lower
Boeing Service Bulletins forward cargo compartment, |
737-26-1121 and main deck cargo compartment |
737-26-1122, and either (as applicable) remains empty |
737-21-1135 or or is verified to contain only
737-21-1163 or their empty cargo handling
Production Equivalents) equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits,
b) Outflow valve is deactivated in
25% open position or
removed,
c) Recirculation fan(s) operates
normally except for -800BCF
airplane, and
d) Extended overwater flight is
prohibited.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-30
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

14 Cabin Pressure Control

System
(Cont’d)

14-04 Digital Control System

Manual Mode
(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

14-04-04 (-900/-900ER) C 1 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed,
b) Recirculation fan(s) operates
normally,
c) Extended overwater flight is
prohibited,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-31
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

15 Main Outflow Valve

15-01 Analog Control System

Outflow Valve Actuators
(AC and/or DC)
(-100/-200/-300/-400/
-500)

15-01A C 2 1 One actuator may be inoperative for

pressurized cargo-only flight,
provided airplane is depressurized
before landing.

15-01B C 2 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated
open or removed, and
b) Extended overwater flight is
prohibited.

15-02 Digital Control System

Outflow Valve Automatic
Mode Actuators

15-02-01 (-300/-400/-500)

15-02-01A C 2 1 One may be inoperative provided

manual mode actuator operates
normally.

15-02-01B C 2 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed, and
b) Extended overwater flight is
prohibited.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-32
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

15 Main Outflow Valve

(Cont’d)

15-02 Digital Control System

Outflow Valve Automatic
Mode Actuators
(Cont’d)

15-02-02 (-600/-700/-800/ C 2 1 One may be inoperative provided

-800BCF/-900/ manual mode actuator operates
-900ER) normally.

15-02-03 (-600/-700/-800/ C 2 0 (M)(O) May be inoperative for

-800BCF Prior to unpressurized flight provided:
Incorporation of Boeing a) Outflow valve is deactivated in
Service Bulletins 25% open position or
737-26-1121 and removed,
737-26-1122, and either b) Recirculation fan(s) operates
737-21-1135 or normally except for -800BCF
737-21-1163 or their airplane, and
Production Equivalents) c) Extended overwater flight is
prohibited.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-33
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

15 Main Outflow Valve

(Cont’d)

15-02 Digital Control System

Outflow Valve Automatic
Mode Actuators
(Cont’d)

15-02-04 (-600/-700/-800/ C 2 0 (M)(O) May be inoperative for

-800BCF Upon unpressurized flight provided:
Incorporation of Boeing a) Procedures are established
Service Bulletins and used to ensure lower
737-26-1121 and forward cargo compartment
737-26-1122, and either remains empty or is verified to
737-21-1135 or contain only empty cargo
737-21-1163 or their handling equipment, ballast
Production Equivalents) (ballast may be loaded in
ULDs), and/or Fly Away Kits,
b) Outflow valve is deactivated in
25% open position or
removed,
c) Recirculation fan(s) operates
normally except for -800BCF
airplane, and
d) Extended overwater flight is
prohibited.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-34
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

15 Main Outflow Valve

(Cont’d)

15-02 Digital Control System

Outflow Valve Automatic
Mode Actuators
(Cont’d)

15-02-05 (-900/-900ER) C 2 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed,
b) Recirculation fan(s) operates
normally,
c) Extended overwater flight is
prohibited,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).

15-03 Digital Control System

Outflow Valve Manual
Mode Actuator

15-03-01 (-300/-400/-500) C 1 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed, and
b) Extended overwater flight is
prohibited.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-35
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

15 Main Outflow Valve

(Cont’d)

15-03 Digital Control System

Outflow Valve Manual
Mode Actuator
(Cont’d)

15-03-02 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative for

-800BCF Prior to unpressurized flight provided:
Incorporation of Boeing a) Outflow valve is deactivated in
Service Bulletins 25% open position or
737-26-1121 and removed,
737-26-1122, and either b) Recirculation fan(s) operates
737-21-1135 or normally except for -800BCF
737-21-1163 or their airplane,
Production Equivalents) c) Extended overwater flight is
prohibited, and |
d) For -800BCF, procedures are |
established and used to |
ensure main deck cargo |
compartment remain empty, |
or are verified to contain only |
cargo handling equipment, |
ballast (ballast may be loaded |
in ULDs), and /or fly away |
kits. |

NOTE: Operator MELs must define |

which items are approved for |
inclusion in Fly Away Kits and |
which materials can be used |
as ballast. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-36
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

15 Main Outflow Valve

(Cont’d)

15-03 Digital Control System

Outflow Valve Manual
Mode Actuator
(Cont’d)

15-03-03 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative for

-800BCF Upon unpressurized flight provided:
Incorporation of Boeing a) Procedures are established
Service Bulletins and used to ensure lower
737-26-1121 and forward cargo compartment, |
737-26-1122, and either main deck cargo compartment |
737-21-1135 or (as applicable) remains empty |
737-21-1163 or their or is verified to contain only
Production Equivalents) empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits,
b) Outflow valve is deactivated in
25% open position or
removed,
c) Recirculation fan(s) operates
normally except for -800BCF
airplane, and
d) Extended overwater flight is
prohibited.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-37
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

15 Main Outflow Valve

(Cont’d)

15-03 Digital Control System

Outflow Valve Manual
Mode Actuator
(Cont’d)

15-03-04 (-900/-900ER) C 1 0 (M)(O) May be inoperative for

unpressurized flight provided:
a) Outflow valve is deactivated in
25% open position or
removed,
b) Recirculation fan(s) operates
normally,
c) Extended overwater flight is
prohibited,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).

16 Pressure Relief Valves

16-01 Analog Control System

(-100/-200/-300/-400/
-500)

16-01A C 2 1 (M) One may be inoperative closed

for pressurized flight.

16-01B C 2 0 (M)(O) May be inoperative provided

flight is conducted in an
unpressurized configuration.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-38
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

16 Pressure Relief Valves

(Cont’d)

16-02 Digital Control System C 2 1 (M) One may be inoperative closed

(-300/-400/-500/-600/ for pressurized flight.
-700/-800/-800BCF/
-900/-900ER)

16-02-01 (-300/-400/-500) C 2 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
and
b) Outflow valve is positioned to
25% open position.

16-02-02 (-600/-700/-800/ C 2 0 (M)(O) May be inoperative provided:

-800BCF Prior to a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Outflow valve is positioned to
737-26-1121 and 25% open position, and
737-26-1122, and either c) Recirculation fan(s) operates
737-21-1135 or normally except for -800BCF
737-21-1163 or their airplane.
Production Equivalents)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-39
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

16 Pressure Relief Valves

(Cont’d)

16-02 Digital Control System

(-300/-400/-500/-600/
-700/-800/-800BCF/
-900/-900ER)
(Cont’d)

16-02-03 (-600/-700/-800/ C 2 0 (M)(O) May be inoperative provided:

-800BCF Upon a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins 737-26- b) Procedures are established
1121 and 737-26-1122, and used to ensure lower
and either 737-21-1135 forward cargo compartment
or 737-21-1163 or their remains empty or is verified to
Production Equivalents contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits,
c) Outflow valve is positioned to
25% open position, and
d) Recirculation fan(s) operates
normally except for -800BCF
airplane.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

16-02-04 (-900/-900ER) C 2 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
b) Outflow valve is positioned to
25% open position,
c) Recirculation fan(s) operates
normally,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-40
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

17 Temperature Indicators

17-01 Supply Duct C 1 0 May be inoperative provided both

(-100/-200/-300/-500/ duct overheat warning systems
-600/-700) operate normally.

17-02 Supply Duct C 3 0 May be inoperative provided

(-400/-800/-800BCF/ associated ZONE TEMP light
-900/-900ER) operates normally.

17-03 Pass Cabin C - 0

17-04 Pack (-400/-800/ C 2 0

-800BCF/-900/-900ER)

18 Duct Overheat Warning

Lights

18-01 DUCT OVERHEAT C 2 0 May be inoperative provided supply

(-100/-200/-300/-500/ duct temperature indicators operate
-600/-700) normally.

18-02 ZONE TEMP C 3 0 May be inoperative provided

(-400/-800/-800BCF/ associated supply duct temperature
-900/-900ER) indicator operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-41
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

19 Passenger Cabin
Temperature Control
Systems

19-01 Automatic/Manual
Controls (-100/-200/
-300/-500/-600/-700)

19-01A C 2 1

19-01B C 2 0 (O) May be inoperative provided right

pack is not used.

19-02 FWD/AFT

19-02-01 (-400/-800/-800BCF/ C 2 0 (O) May be dispatched with faults

-900/-900ER) indicated by ZONE TEMP Light(s)
during Master Caution recall provided
associated temperature control
system is checked to operate
normally before each takeoff.

19-02-02 (-400/-800/-800BCF)

19-02-02A C 2 0 (M)(O) May be inoperative provided

Trim Air Pressure Regulating and
Shutoff Valve remains CLOSED.

19-02-02B C 2 0 (M)(O) May be inoperative provided

associated Trim Air Modulating Valve
is deactivated CLOSED.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-42
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

19 Passenger Cabin
Temperature Control
Systems
(Cont’d)

19-02 FWD/AFT
(Cont’d)

19-02-03 (-900/-900ER)

19-02-03A C 2 0 (M)(O) May be inoperative provided:

a) Trim Air Pressure Regulating
and Shutoff Valve remains
Closed,
b) Forward cargo heat duct is
secured closed, and
c) Airport ambient temperature
does not exceed 103 °F
(39 °C).

19-02-03B C 2 0 (M)(O) May be inoperative provided:

a) Associated Trim Air
Modulating Valve is
deactivated CLOSED,
b) Forward cargo heat duct is
secured closed, and
c) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-43
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

|
21 Flight Deck Temperature
Control Systems

21-01 Automatic/Manual
Controls (-100/-200/
-300/-500/-600/-700)

21-01A C 2 1

21-01B C 2 0 (O) May be inoperative provided left

pack is not used.

21-02 Primary/Backup Modes

21-02-01 (-400/-800/-900/ C 2 1 (O) One may be inoperative provided

-800BCF/-900ER) remaining temperature control is
verified to operate normally.

21-02-02 (-400/-800/-800BCF)

21-02-02A C 2 0 (M)(O) May be inoperative provided

Trim Air Pressure Regulating and
Shutoff Valve remains CLOSED.

21-02-02B C 2 0 (M)(O) May be inoperative provided

associated Trim Air Modulating Valve
is deactivated CLOSED.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-44
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

21 Flight Deck Temperature

Control Systems
(Cont’d)

21-02 Primary/Backup Modes

(Cont’d)

21-02-03 (-900/-900ER)

21-02-03A C 2 0 (M)(O) May be inoperative provided:

a) Trim Air Pressure Regulating
and Shutoff Valve remains
CLOSED,
b) Forward Cargo heat duct is
secured closed, and
c) Airport ambient temperature
does not exceed 103 °F
(39 °C).

21-02-03B C 2 0 (M)(O) May be inoperative provided:

a) Associated Trim Air
Modulating Valve is
deactivated CLOSED,
b) Forward cargo heat duct is
secured closed, and
c) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-45
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

22 Forward Outflow Valve

(-100/-200/-300/-400/
-500, including STCs
SA2969SO,
ST01566LA, and
ST01961SE)

22A C 1 0 Except for 737C and STC

ST01566LA and ST01961SE cargo
or cargo/passenger operations, may
be inoperative closed.

22B C 1 0 May be inoperative open provided

both packs operate normally.

22C C 1 0 (O) May be inoperative open with one

pack operating normally provided
flight altitude remains at or below
FL 200.

23 FORWARD OUTFLOW C 1 0
CLOSED Indicating
Light
(-100/-200)

24 Gasper Fan D 1 0
*** (-100/-200/-300/-500/
-600/-700)

25 Water Separator C 2 0 (M)(O) May be inoperative provided

Anti-Icing Systems associated pack is not used.
(-100/-200/-300/-500/
-600/-700)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-46
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

26 Ground Preconditioned C 1 0 May be inoperative closed.

Air Connection Check
Valve

26-01 Analog Control System C 1 0 (M)(O) May be inoperative open

(-100/-200/-300/-400/ provided:
-500) a) Flight is conducted in an
unpressurized configuration,
and
b) Procedures are established
and used to ensure main deck
cargo compartment
(as applicable) remains
empty, or is verified to contain
only empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

26-02 Digital Control System

26-02-01 (-300/-400/-500) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
and
b) Outflow valve is positioned to
25% open position.

26-02-02 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Prior to a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Outflow valve is positioned to
737-26-1121 and 25% open position, and
737-26-1122, and either c) Recirculation fan(s) operates
737-21-1135 or normally except for -800BCF
737-21-1163 or their airplane.
Production Equivalents)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-47
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

26 Ground Preconditioned
Air Connection Check
Valve
(Cont’d)

26-02 Digital Control System

(Cont’d)

26-02-03 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-800BCF Upon a) Flight is conducted in an
Incorporation of Boeing unpressurized configuration,
Service Bulletins b) Procedures are established
737-26-1121 and and used to ensure lower
737-26-1122, and either forward cargo compartment
737-21-1135 or remains empty or is verified to
737-21-1163 or their contain only empty cargo
Production Equivalents) handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits,
c) Outflow valve is positioned to
25% open position, and
d) Recirculation fan(s) operates
normally except for -800BCF
airplane.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

26-02-04 (-900/-900ER) C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted in an
unpressurized configuration,
b) Outflow valve is positioned to
25% open position,
c) Recirculation fan(s) operates
normally,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-48
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

27 Electrical/Electronic
Equipment Cooling
Blowers

27-01 Non-EFIS C 2 1 Except for ER operations, one may

(-100/-200/-300/ be inoperative.
-400/-500)

27-02 EFIS (-300/-400/-500)

27-02-01 Supply Fans C 2 1 Except for ER operations, one may

be inoperative.

27-02-02 Exhaust Fans C 2 1 Except for ER operations, one may

be inoperative.

27-03 CDS B 4 3 (M) One fan may be inoperative

(-600/-700/-800/ provided:
-800BCF/-900/-900ER) a) All remaining fans are verified
to operate normally, and
b) Both low flow detectors are
verified to operate normally.

28 Equipment Cooling D 1 0 May be inoperative open.

*** Check Valve
(-100/-200)

29 Air Cleaner Purge C 2 0

*** Valves
(-100/-200/-300)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-49
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

30 Control Cabin
*** Augmentation Fan
(-200)

30A C 1 0 (M)(O) May be inoperative with fan

wind-milling provided OAT remains at
or below 120 °F (49 °C).

30B C 1 0 (M)(O) May be inoperative with fan

wind-milling provided OAT remains at
or below 115 °F (46 °C) if PDCS is
installed and operates normally.

30C C 1 0 (M)(O) May be inoperative with fan

seized provided:
a) One air conditioning pack
operates normally,
b) OAT remains at or below
100 °F (38 °C), and
c) Window heat operates
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-50
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

31 Recirculation Fan(s)

31-01 (-300/-500) C 1 0 May be inoperative provided left pack

is operating when OAT is above
100 °F (38 °C).

31-02 (-400 and Pemco -400

COMBI)

31-02A C 2 1 One fan may be inoperative provided

left pack is operating when OAT is
above 100 °F (38 °C).

31-02B C 2 0 May be inoperative provided OAT

remains below 100 °F (38 °C).

31-03 (-600/-700) C 1 0 May be inoperative provided:

a) Left pack is operating when
OAT is above 100 °F (38 °C),
b) Flight is conducted
pressurized, and
c) Both packs operate normally.

31-04 (-800/-900/-900ER)

31-04A C 2 1 Left fan may be inoperative provided

left pack is operating when OAT is
above 100 °F (38 °C).

31-04B C 2 1 Right fan may be inoperative

provided:
a) Left pack is operating when
OAT is above 100 °F (38 °C),
and
b) Flight is conducted
pressurized.

31-04C C 2 0 May be inoperative provided:

a) OAT remains below 100 °F
(38 °C), and
b) Flight is conducted
pressurized.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-51
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

31 Recirculation Fan(s)
(Cont’d)

31-04 (-800/-900/-900ER)
(Cont’d)

31-04-01 (-800EF C 1 0 May be inoperative provided:

STC ST02000NY) a) Left pack is operating when
OAT is above 100 °F (38 °C),
b) Flight is conducted
pressurized, and
c) Both packs operate normally.

31-04-02 (-900 With Greenpoint C 1 0 May be inoperative provided:

Technologies, Inc. a) Left pack is operating when
Interior Installation OAT is above 100 °F (38 °C),
G12111000-101 b) Flight is conducted
STC ST11040SE) pressurized, and
c) Both packs operate normally.

31-05 (-300QC/F, -400F) C 1 0 May be inoperative in cargo

(STCs ST01566LA, configuration.
SA2969SO, and
SA2970SO Only)

31-05-01 (STC SA2970SO) C 1 0 May be inoperative in PAX mode

provided OAT remains below 100 °F
(38 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-52
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

32 Pack Temperature C 4 2 (O) One system (primary or standby)

Control System(s) on each pack may be inoperative
(Electronic Pack/Zone provided remaining system on
Controller or Pack Flow associated pack is checked to |
Controller) operate normally. |
(-400/-800/-800BCF/
-900/-900ER)

33 Pack Temperature
Control Valves
(-400/-800/-800BCF/
-900/-900ER)

33A C 2 0 (O) May be inoperative closed

provided associated Standby Pack
Temperature Control Valve(s) is
verified to operate normally.

33B C 2 0 (M)(O) May be inoperative provided:

a) Associated Temperature
Control Valve is deactivated
closed, and
b) Associated Standby Pack
Temperature Control Valve(s)
is verified to operate normally.

33C C 2 0 (M)(O) May be inoperative provided

associated pack is considered
inoperative.

NOTE: Refer to MMEL Item 21-01, |

Air Conditioning Packs. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-53
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

34 Standby Pack
Temperature Control
Valves
(-400/-800/-800BCF/
-900/-900ER)

34A C 2 0 (O) May be inoperative provided

associated Pack Temperature
Control Valve(s) is checked to
operate normally.

34B C 2 0 (M)(O) May be inoperative provided

associated pack is not used.

35 Trim Air Pressure

Regulating and Shutoff
Valve

35-01 (-400/-800/-800BCF) C 1 0 (M) May be inoperative secured

closed.

35-02 (-900/-900ER) C 1 0 (M)(O) May be inoperative secured

closed provided:
a) Forward cargo heat duct is
secured closed, and
b) Airport ambient temperature
does not exceed 103 °F
(39 °C).

36 Trim Air Modulating

Valves

36-01 (-400/-800/-800BCF)

36-01A C 3 0 (M)(O) May be inoperative closed.

36-01B C 3 0 (O) May be inoperative in any

position provided Trim Air Pressure
Regulating and Shutoff Valve
remains closed.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-54
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

36 Trim Air Modulating

Valves
(Cont’d)

36-02 (-900/-900ER)

36-02A C 3 0 (M)(O) May be inoperative closed

provided:
a) Forward cargo heat duct is
secured closed, and
b) Airport ambient temperature
does not exceed 103 °F
(39 °C).

36-02B C 3 0 (M)(O) May be inoperative in any

position provided:
a) Trim Air Pressure Regulating
and Shutoff Valve remains
CLOSED,
b) Forward cargo heat duct is
secured closed, and
c) Airport ambient temperature
does not exceed 103 °F
(39 °C).

37 Outflow Valve Heater C 1 0

*** Gasket
(-100/-200/-300/-400/
-500)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-55
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

38 Outflow Valve Position C 1 0 (M)(O) May be inoperative provided: |

Indicator a) Valve is verified to be |
operating normally, and |
b) For -800BCF, procedures are |
established and used to |
ensure main deck cargo |
compartment remain empty, |
or are verified to contain only |
cargo handling equipment, |
ballast (ballast may be loaded |
in ULDs), and /or fly away |
kits. |

NOTE: Operator MELs must define |

which items are approved for |
inclusion in Fly Away Kits and |
which materials can be used |
as ballast. |

39 Trim Air Check Valves

39-01 (-400/-800/-800BCF/ C 2 1 (M) One may be inoperative provided

-900/-900ER) associated valve is deactivated
closed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-56
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

40 Equipment Cooling
Automatic Flow Control
Valve/Overboard
Exhaust Valve

40-01 Analog Control System

(-100/-200/-300/-400/
-500)

40-01A C 1 0 (M)(O) May be inoperative in open

position provided flight is conducted
in an unpressurized configuration.

40-01B C 1 0 May be inoperative in closed position

provided both packs and recirculation |
fan(s) (if installed) are operated |
during ground taxi operations.

40-02 Digital Control System

40-02-01 (-300/-400/-500)

40-02-01A C 1 0 (M)(O) May be inoperative in open

position provided:
a) Flight is conducted in an
unpressurized configuration,
and
b) Outflow valve is positioned to
25% open position.

40-02-01B C 1 0 May be inoperative in closed position

provided both packs and recirculation
fan(s) (if installed) are operated
during ground taxi operations.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-57
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

40 Equipment Cooling
Automatic Flow Control
Valve/Overboard
Exhaust Valve
(Cont’d)

40-02 Digital Control System

(Cont’d)

40-02-02 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative in open

-800BCF Prior to position provided:
Incorporation of Boeing a) Flight is conducted in an
Service Bulletins unpressurized configuration,
737-26-1121 and b) Outflow valve is positioned to
737-26-1122, and either 25% open position, and
737-21-1135 or c) Recirculation fan(s) operates
737-21-1163 or their normally except for -800BCF
Production Equivalents) airplane.

40-02-03 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative in open

-800BCF Upon position provided:
Incorporation of Boeing a) Flight is conducted in an
Service Bulletins unpressurized configuration,
737-26-1121 and b) Procedures are established
737-26-1122, and either and used to ensure lower
737-21-1135 or forward cargo compartment
737-21-1163 or their remains empty or is verified to
Production Equivalents) contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits,
c) Outflow valve is positioned to
25% open position, and
d) Recirculation fan(s) operates
normally except for -800BCF
airplane.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-58
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

40 Equipment Cooling
Automatic Flow Control
Valve/Overboard
Exhaust Valve
(Cont’d)

40-02 Digital Control System

(Cont’d)

40-02-04 (-900/-900ER) C 1 0 (M)(O) May be inoperative in open

position provided:
a) Flight is conducted in an
unpressurized configuration,
b) Outflow valve is positioned to
25% open position,
c) Recirculation fan(s) operates
normally,
d) Forward cargo heat duct is
secured closed, and
e) Airport ambient air
temperature does not exceed
103 °F (39 °C).

40-02-05 (-600/-700/-800/ C 1 0 (M)(O) Except for ER operations,

-800BCF/-900/-900ER) may be inoperative provided:
a) Actuator is verified to be in
smoke position, and
b) Both packs operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-59
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

41 Door Area Heater

Systems

41-01 Main Deck Cargo Door D - 0

*** Heating
Blankets/Systems
(737C and -700C)

41-02 Entry Door Area and D - 0 (M) May be inoperative deactivated.

Overwing Emergency
Exit Hatch Area Heater
Systems
(-600/-700/-800/
-900/-900ER)

41-03 Main Cargo Door Heater D 1 0 (M) May be inoperative in Quick

System Change cargo configuration.
(STC ST01566LA)

41-04 Mid-Exit Door Area D 1 0 (M) May be inoperative deactivated.

*** Heater System
(-900ER)

41-05 Forward Entry Door Area D 1 0 (M) May be inoperative deactivated.

(-800BCF)

42 Equipment Cooling Low B 2 1 (M)(O) One may be inoperative

Flow Detector Systems provided associated fans (supply or
(-600/-700/-800/ exhaust) are verified to operate
-800BCF/-900/-900ER) normally.

43 Equipment Cooling Air C 1 0 (M) Equipment Cooling System may

Filter be operated with filter removed.
(-600/-700/-800/
-800BCF/-900/-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-60
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

44 Fan Bypass Check

Valves
(-600/-700/-800/
-800BCF/-900/-900ER)

44A C 2 0 May be inoperative open/missing

provided airport ambient temperature
remains below 80 °F (27 °C).

44B C 2 0 May be inoperative open/missing for

an associated inoperative pack.

44C D 2 1 One may be inoperative

open/missing provided pack
associated with remaining fan bypass
check valve operates normally.

45 Air Distribution Riser

Shutoff Valves
(-700C/-800BCF/
STC ST02556SE)

45-01 Passenger Configuration C 2 0 (M) May be inoperative provided

(-700C) valves are deactivated open.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-61
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

45 Air Distribution Riser

Shutoff Valves
(-700C/-800BCF/
STC ST02556SE)
(Cont’d)

45-02 Passenger and Cargo C 2 0 (M)(O) May be inoperative in closed

Configurations position provided:
(-700C) a) Flight is conducted in an
unpressurized configuration,
b) Recirculation fan operates
normally,
c) Both E/E equipment cooling
exhaust fans operate
normally, and
d) Procedures are established
and used to ensure main deck
(as applicable) and lower
cargo compartments remain
empty or are verified to
contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

45-02-01 Right Riser SOV C 1 0 (M)(O) Except for ER operations,

may be inoperative closed provided
operation is limited to left pack only.

45-02-02 Left Riser SOV C 1 0 (M)(O) Except for ER operations,

may be inoperative closed provided
operation is limited to one pack.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-62
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

45 Air Distribution Riser

Shutoff Valves
(-700C/-800BCF/
STC ST02556SE)
(Cont’d)

45-03 Cargo Configuration

(-800BCF)

45-03A C 2 0 (M) Both may be inoperative in open

position provided:
a) Both E/E equipment cooling
exhaust fans operate
normally, and
b) Procedures are established
and used to ensure main deck
(as applicable) and lower
cargo compartments remain
empty or are verified to
contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-63
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

45 Air Distribution Riser

Shutoff Valves
(-700C/-800BCF/
STC ST02556SE)
(Cont’d)

45-03 Cargo Configuration

(-800BCF)
(Cont’d)

45-03B C 2 0 (M)(O) Both may be inoperative in

closed position provided operation is
limited to left pack, and:
a) Flight is conducted in a single
pack configuration,
b) Mix manifold exhaust shutoff
valve is in open position,
c) Both E/E equipment cooling
exhaust fans operate
normally, and
d) Procedures are established
and used to ensure main deck
(as applicable) compartments
remain empty or are verified
to contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-64
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

45 Air Distribution Riser

Shutoff Valves
(-700C/-800BCF/
STC ST02556SE)
(Cont’d)

45-03 Cargo Configuration

(-800BCF)
(Cont’d)

45-03-01 Right Riser SOV C 1 0 (M) Except for ER operations, may be

inoperative open provided:
a) The left main deck riser SOV
is in the open position,
b) Both E/E equipment cooling
exhaust fans operate
normally,
c) Mix manifold exhaust shutoff
valve is in closed position,
and
d) Procedures are established
and used to ensure main deck
compartments (as applicable)
remain empty or are verified
to contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-65
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

45 Air Distribution Riser

Shutoff Valves
(-700C/-800BCF/
STC ST02556SE)
(Cont’d)

45-03 Cargo Configuration

(-800BCF)
(Cont’d)

45-03-02 Left Riser SOV C 1 0 (M) Except for ER operations, may be

inoperative open provided:
a) The right main deck riser SOV
is in the open position,
b) Both E/E equipment cooling
exhaust fans operate
normally,
c) Mix manifold exhaust shutoff
valve is in closed position,
and
d) Procedures are established
and used to ensure main deck
compartments (as applicable)
remain empty or are verified
to contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-66
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

45 Air Distribution Riser

Shutoff Valves
(-700C/-800BCF/
STC ST02556SE)
(Cont’d)

45-04 STC ST02556SE Only

45-04A C 2 0 (M)(O) May be inoperative provided:

a) Valves are deactivated open,
and
b) Procedures are established
and used to ensure main deck
cargo compartment remains
empty or is verified to contain
only empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

45-04B C 2 1 (M)(O) May be inoperative closed

provided operation is limited to left
pack only.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-67
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

46 Air Heater D 1 0 May be inoperative provided

Supernumerary compartment is not occupied.
Compartment
STC ST01566LA
(-300RB), ST01961SE,
and ST02556SE

47 Humidification System C 3 0 May be inoperative provided:

*** (-800EF a) Manual shutoff valve is
STC ST02000NY) closed, and
b) All Humidifier Switches are in
OFF.

48 Zonal Drying System C 1 0 (M) May be inoperative provided:

*** (-800EF a) Humidifiers are switched OFF,
STC ST02000NY) and
b) Dryer/Humidifier power is
removed.

49 Return Air Grille C - - (M) One may be broken or missing

(-600/-700/-800/ provided:
-800BCF/-900/ a) Broken or missing grille is
-900ER) located within a designated
area as defined by Boeing,
and
b) Grille is removed and
replaced with a blanking plate.

50 Flight Deck Foot and C 4 0 May be inoperative provided flight

Shoulder Heater deck temperature is acceptable to
Systems flightcrew.

51 Pack Supply air Cleaner D 2 0 (M) May be inoperative provided

*** System associated air cleaner purge valve is
(-600/-700) deactivated closed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 21-68
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar

52 Integrated Display Unit

*** (IDU) Cooling System
(-300)
(Boeing Service Bulletin
737-31-1435)

52-01 Normal and Alternate C 2 1 May be inoperative provided IDU

Fans COOLING OFF light operates
normally.

52-02 IDU COOLING OFF C 1 0 (M) May be inoperative provided:

Light a) Normal and alternate IDU
cooling fans operate normally,
and
b) IDU cooling fan warning
system is verified to operate
normally.

53 Ozone Converters C 2 0 As required by 14 CFR. |

*** (-600/-700/-800/-900/- |
900ER) |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

01 Autopilot Systems

01A C - 1 May be inoperative provided

approach minimums do not require its
use.

01B B - 0 Except for ER operations, may be

inoperative provided:
a) Approach minimums do not
require their use,
b) Enroute operations do not
require autopilot use, and
c) Number of flight segments
and segment duration is
acceptable to flightcrew.

NOTE 1: Operators should make

every effort to repair
autopilot early in repair
interval, as provided by this
relief statement, in
consideration of such
factors as weather, traffic
density, and effect of other
inoperative systems.

NOTE 2: Any mode which functions

normally may be used. If
CWS is inoperative, do not
use other modes (pitch or
roll).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

01 Autopilot Systems
(Cont’d)

01-01 Control Wheel Autopilot

Disconnect Switches

01-01-01 -100/-200/-300/
-400/-500
Without Autopilot
DISENGAGE Bar

01-01-01A C 2 1 May be inoperative on non-flying

pilot’s side provided:
a) Autopilot is not used below
1,500 ft. AGL, and
b) Approach minimums do not
require use of autopilot.

01-01-01B B 2 0 May be inoperative provided

autopilots are not used.

01-01-02 -100/-200/-300/
-400/-500
With Autopilot
DISENGAGE Bar and
-600/-700/-800/
-800BCF/-900/-900ER

01-01-02A C 2 1 One may be inoperative provided:

a) Mode Control Panel autopilot
DISENGAGE bar operates
normally,
b) Autopilot is not used below
1,500 ft. AGL, and
c) Approach minimums do not
require use of autopilot.

01-01-02B B 2 0 May be inoperative provided

autopilots are not used.

01-02 Autopilot DISENGAGE C 1 0

*** Bar
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

02 Autopilot Disengaged
Warning System

02-01 Lights

02-01A C 2 1 May be inoperative provided autopilot

disengage aural warning system
operates normally.

02-01B B 2 1 Except for ER operations, may be

inoperative provided autopilots are
not used.

02-01C B 2 0 Except for ER operations, may be

inoperative provided autopilots are
not used.

02-02 Aural Warning B 1 0 Except for ER operations, may be

*** inoperative provided autopilots are
not used.

03 Yaw Damper

03-01 (-100/-200/-300/
-400/-500)

03-01-01 Without Rudder C 1 0 (O) May be inoperative provided yaw

Pressure Reducer damper switch remains OFF.
System Installed
NOTE: Refer to AFM Limitations for
SP-77 autopilot.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

03 Yaw Damper
(Cont’d)

03-01 (-100/-200/-300/
-400/-500)
(Cont’d)

03-01-02 With Rudder Pressure

Reducer System
Installed

03-01-02A C 1 0 (M)(O) May be inoperative provided:

a) Yaw damper switch remains
OFF, and
b) Rudder Pressure Reducer
System is verified to operate
normally.

NOTE: Refer to AFM Limitations for

SP-77 autopilot.

03-01-02B C 1 0 (M)(O) May be inoperative provided

yaw damper is deactivated.

NOTE: Refer to AFM Limitations for

SP-77 autopilot.

03-02 (-600/-700/-800/ C 1 0 (O) May be inoperative provided yaw

-900/-900ER) damper switch remains off.

03-03 Yaw Damper Indicator C 1 0

***

04 Autothrottle System C 1 0 May be inoperative provided

*** approach minimums do not require its
use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

05 Mach Trim Systems C - 0 (M)(O) May be inoperative provided:

a) AFM Limitations are
observed, and
b) Mach trim actuator is verified
to be in null/uncommanded
elevator position.

05-01 (-300/-400/-500/-600/ C 2 1 (M) One may be inoperative

-700/-800/-900/-900ER) deactivated provided:
a) Remaining Mach trim system
is verified to operate normally,
and
b) Mach trim fail light operates
normally.

06 SP-77/SP-177/SP-300/ C - 0 Individual mode annunciations may

Collins Flight and be inoperative provided associated
Approach Mode system modes are not used.
Annunciations

06-01 SP-177/SP-300
*** Annunciator Panels
(-200/-300/-400/-500)

06-01A C 2 1 One may be inoperative provided:

a) Engaged system (AP, FD, AT,
PDCS, or FMCS) is at pilot
position with operative mode
annunciator, and
b) Approach minimums do not
require their use.

06-01B C 2 0 May be inoperative provided

associated systems are not used.

NOTE: PDCS or FMCS data on CDU

may be valid when PDC or
FMC annunciator is
inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

06 SP-77/SP-177/SP-300/
Collins Flight and
Approach Mode
Annunciations
(Cont’d)

06-02 SP-77 Approach

Progress Displays
(-100/-200)

06-02A C 2 1 One may be inoperative provided

approach minimums do not require
their use.

06-02B C 2 0 May be inoperative provided

associated system modes are not
used.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

08 Autothrottle Disengage
*** Lights

08A C 2 1 One may be inoperative when

autothrottle is used provided
approach minimums do not require
their use.

08B C 2 0 May be inoperative provided

autothrottle is not used.

11 STAB OUT OF TRIM B 1 0 Except for ER operations, may be |

Light inoperative provided autopilots are
not used.

12 Autopilot Trim Circuit C 1 0 (M) Trim circuit to monitor stabilizer

*** Breaker Monitor trim CB may be inoperative provided
(-100/-200) remaining functions of STAB OUT OF
TRIM light operate normally.

13 Automatic Thrust C 1 0 May be inoperative unless

*** Restoration (ATR) procedures require its use.
System
(-300)

14 Mode Control Panel

Selectors
(-200/-300/-400/-500/
-600/-700/-800/-900/
-900ER)

14-01 V/S Selector C 1 0 May be inoperative provided

*** (DOWN, UP) procedures do not require its use.

14-02 Bank Angle Selector C 1 0

*** (10, 15, 20, 25, 30)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

15 Mode Control Panel

Switches/Paddles
(-200/-300/-400/-500/
-600/-700/-800/-900/
-900ER)

15-01 A/P CWS Engage C 2 0

Switches

15-02 A/P CMD Engage

Switches

15-02A C 2 1 Maybe inoperative provided approach

minimums do not require its use.

15-02B B 2 0 Except for ER operations, may be |

inoperative provided autopilots are
not used.

15-03 Autothrottle Arm Switch C 1 0 May be inoperative provided

*** approach minimums do not require
autothrottle use.

15-04 A/T SPEED Switch C 1 0 May be inoperative provided

*** approach minimums do not require
autothrottle use.

15-05 F/D Switches C 2 0 May be inoperative provided

*** approach minimums do not require
flight director use.

15-06 IAS/MACH Change Over C 1 0

*** Switch

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

15 Mode Control Panel

Switches/Paddles
(-200/-300/-400/-500/
-600/-700/-800/-900/
-900ER)
(Cont’d)

15-07 APP Switch C 1 0 May be inoperative provided

*** approach minimums do not require
autopilot or flight director use.

15-08 EPR/N1, LNAV, VNAV, C - 0 May be inoperative provided enroute

*** LVL CHG, V/S, HDG operations do not require their use.
SEL, ALT HOLD, and
VOR/LOC Switches

15-09 SPD INTV, PDC, and C - 0

*** ALT INTV Switches

16 Mode Control Panel

Windows

16-01 Vertical Speed C 1 0 May be inoperative provided

*** (VERT SPEED) procedures do not require its use.
(-200/-300/-400/-500/
-600/-700/-800/-900/
-900ER)

16-02 (EFIS/PFD/ND)
(-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Includes
STC ST03355AT)

16-02-01 Airspeed C 1 0 May be inoperative and associated

(IAS/MACH) selector used provided selected
airspeed indications operate
normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

16 Mode Control Panel

Windows
(Cont’d)

16-02 (EFIS/PFD/ND)
(-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Includes
STC ST03355AT)
(Cont’d)

16-02-02 Heading (HEADING) C 1 0 May be inoperative and associated

selector used provided selected
heading indications operate normally.

16-02-03 Vertical Speed C 1 0 May be inoperative provided

(VERT SPEED) procedures do not require its use.

16-02-04 Vertical Speed C 1 0 May be inoperative and associated

(VERT SPEED) selector used provided selected
(-600/-700/-800/-900/ vertical speed indications operate
-900ER) normally.

16-02-05 Altitude (ALTITUDE) C 1 0 May be inoperative and associated

(-600/-700/-800/-900/ selector used provided selected
-900ER) altitude indications operate normally.

16-02-06 Course (COURSE) C 2 0 May be inoperative and associated

selector used provided selected
course indications operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

16 Mode Control Panel

Windows
(Cont’d)

16-02 (EFIS/PFD/ND)
(-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Includes
STC ST03355AT)
(Cont’d)

16-02-07 Window Lighting B 1 0 May be inoperative provided:

a) Selected airspeed indications
operate normally,
b) Selected heading indications
operate normally,
c) Selected vertical speed
indications operate normally,
d) Selected altitude indications
operate normally, and
e) Selected course indications
operate normally.

17 Takeoff/Go-Around
(TO/GA) Switches

17A C 2 1 One may be inoperative provided

approach minimums do not require its
use.

17B C 2 0 May be inoperative provided:

a) Both thrust levers are
operated manually for takeoff,
and
b) Autopilot and Flight Director
are not used below Minimum
Descent Altitude or 500 ft.,
whichever is higher.

NOTE: Flight director go-around and

windshear guidance are not
available with both TO/GA
switches inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

18 Mode Control Panel

*** Switch Lights

18-01 Autopilot Engage Switch

Lights

18-01-01 CWS C 2 0

18-01-02 CMD

18-01-02A C 2 1 One may be inoperative provided |

approach minimums do not require its |
use. |

18-01-02B B 2 0 Except for ER operations, may be |

inoperative provided autopilots are
not used.

18-02 Mode Selector Switch C - 0

Lights

18-03 A/T ARM Switch Light C 1 0

19 Thrust Mode C 1 0 May be inoperative provided thrust

Annunciator/ mode limits are observed.
Thrust Mode Display
(-300/-400/-500/-600/
-700/-800/-900/-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 22-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
22. Autoflight
Change
Sequence No. Item 1 2 3 4 Bar

20 Automatic Landing
System

20-01 Fail Passive C 1 0 May be inoperative provided

*** approach minimums do not require its
use.

20-02 Fail Operational C 1 0 May be inoperative provided

*** (LAND 3) approach minimums do not require its
(-600/-700/-800/ use.
-900/-900ER)

20-03 AUTOLAND Light

***

20-03A C 2 0 (O) May be inoperative provided

alternate procedures are established
and used.

20-03B D 2 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

01 Flight Deck Speakers

***

01-01 Airplanes with Audio

Accessory Unit (AAU)

01-01A B - 0 May be inoperative provided:

a) Headset earphones or
headphones associated with
inoperative speaker(s) are
installed and operate normally,
and
b) TCAS audio is considered
inoperative, and
c) TAWS (GPWS) advisory
callouts are considered
inoperative.

NOTE: Refer to MMEL Item 34-26 |

(GWPS advisory callouts) and |
MMEL Item 34-40 (TCAS |
audio) |

01-01B C - 0 (O) May be inoperative provided:

a) Procedures do not require its
use, and
b) Headset earphones or
headphones associated with
inoperative speaker(s) are
installed and operate normally,
and
c) Aural alert voices, TCAS, and
TAWS (GPWS) are verified to
operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

01 Flight Deck Speakers

*** (Cont’d)

01-02 Airplanes with Remote

Electronics Unit (REU)

01-02A B - 0 May be inoperative provided:

a) Headset earphones or
headphones associated with
inoperative speaker(s) are
installed and operate normally,
b) TCAS audio is considered
inoperative,
c) TAWS (GPWS) advisory
callouts area considered
inoperative, and
d) Altitude Alert Tone is
considered inoperative.

NOTE: Refer to MMEL Item 34-26 |

(GWPS advisory callouts), |
MMEL Item 34-40 (TCAS |
audio) and MMEL Item 34-25 |
(Altitude Alerting System – |
Aural Alert) |

01-02B C - 0 (M)(O) May be inoperative provided:

a) Procedures do not require its
use,
b) Headset or earphones
associated with inoperative
speaker(s) are installed and
operate normally, and
c) Aural alert voices, TCAS,
GPWS, and Altitude Alert are
verified to operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

02 Passenger Address
System
(Includes
STC ST10238SC)

02-01 Passenger Configuration

02-01A B 1 0 (O) May be inoperative provided:

a) Alternate, normal, and
emergency procedures and/or
operating restrictions are
established and used, and
b) Flight attendant alerting
system (audio or visual) |
operates normally.

NOTE: Any station function(s) that

operates normally may be
used.

02-01B C 1 0 (O) May be inoperative provided:

a) PA not required by 14 CFR,
and
b) Alternate, normal, and
emergency procedures and/or
operating restrictions are
established and used.

NOTE: Any station function(s) that

operates normally may be
used.

02-01-01 Lavatory Speakers C - 0 (O) May be inoperative provided

alternate procedures are established
and used.

02-01-02 Cabin Speakers C - - May be inoperative provided

inoperative speakers are not adjacent
to each other.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

02 Passenger Address
System
(Includes
STC ST10238SC)
(Cont’d)

02-02 Cargo Configuration

(Courier/Supernumerary
Address System)

02-02A C 1 0 (O) May be inoperative provided

alternate, normal and emergency
procedures and/or operating
restrictions are established and used.

02-02B D 1 0 May be inoperative provided

procedures do not require its use.

02-02-01 Lavatory Speakers

02-02-01A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

02-02-01B D 1 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

03 Communication Systems D - - Any in excess of those required by

(VHF and UHF) 14 CFR may be inoperative provided
it is not powered by Standby Bus and
is not required for emergency
procedures.

03-01 VHF Comm Control C - - One side of VHF Comm Control

*** Panels panel tuning function may be
inoperative provided:
a) Associated transceiver can be
tuned from opposite side of
control panel, and
b) Associated transceiver
operates normally.

03-01-01 Active Frequency Light C - 0

***

03-01-02 Frequency Transfer

Switch

03-01-02A C - 0 May be inoperative provided

associated VHF active frequency can
be selected.

03-01-02B D - - May be inoperative provided

associated VHF radio is considered
inoperative.

NOTE: Refer to MMEL Item 23-03 |

(Communication Systems |
(VHF and UHF)). |

03-01-03 Frequency Selector C - 2

Knob

03-01-04 Frequency Indication C - 2

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

03 Communication Systems
(VHF and UHF)
(Cont’d)

03-02 Radio Tuning Panels C - 2 One may be inoperative provided: |

*** a) Left radio tuning panel
operates normally, and
b) Inoperative radio tuning panel
remains OFF.

03-02-01 Off-Side Tuning Light C - 0

03-03 VHF Data Link |

*** |

03-03A C 1 0 (O) May be inoperative provided |

alternate procedures are established |
and used. |

03-03B D 1 0 May be inoperative provided |

procedures do not require its use. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

04 Crewmember Interphone
System

04-01 Passenger Configuration

04-01-01 Flight Deck to Cabin, B - - (O) May be inoperative provided:

Cabin to Flight Deck a) Flight deck to cabin and cabin
Functions to flight deck interphone
functions operate normally on
at least 50% of cabin
handsets, and
b) Alternate communications
procedures between affected
flight attendant station(s) are
established and used.

NOTE: Any station function(s) that

operates normally may be
used.

04-01-02 Cabin to Cabin Function

04-01-02A B 2 0 (O) May be inoperative provided

alternate communications procedures
between affected flight attendant
station(s) are established and used.

NOTE: Any station function(s) that

operates normally may be
used.

04-01-02B B - - (O) May be inoperative provided:

a) Cabin to cabin interphone
functions operate normally on
at least 50% of cabin
handsets, and
b) Alternate communications
procedures between affected
flight attendant station(s) are
established and used.

NOTE: Any station function(s) that

operates normally may be
used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

04 Crewmember Interphone
System
(Cont’d)

04-01 Passenger Configuration

(Cont’d)

04-01-03 Flight Deck to Ground

Function
(Includes CALL
Functions)

04-01-03-01 Large Turbojet Airplanes

Operating Under 14 CFR
Part 121

04-01-03-01A C 1 0 (O) Flight interphone flight deck to

ground/ground to flight deck function
may be inoperative provided:
a) Alternate procedures are
established and used, and
b) Nose gear/forward fuselage
service interphone jack
operates normally.

04-01-03-01B C 1 0 (O) Service interphone flight deck to

ground/ground to flight deck function
may be inoperative provided:
a) Alternate procedures are
established and used, and
b) Nose gear/forward fuselage
flight interphone jack operates
normally.

04-01-03-01C B - 0 (O) May be inoperative provided

alternate procedures are established
and used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

04 Crewmember Interphone
System
(Cont’d)

04-01 Passenger Configuration

(Cont’d)

04-01-03 Flight Deck to Ground

Function
(Includes CALL
Functions)
(Cont’d)

04-01-03-02 All Other

Aircraft/Operations

04-01-03-02A C - 0 (O) May be inoperative provided

alternate procedures are established
and used.

04-01-03-02B D - 0 May be inoperative provided

procedures do not require its use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

04 Crewmember Interphone
System
(Cont’d)

04-02 Cargo Configuration

04-02-01 Flight Deck to Cabin,

Cabin to Flight Deck
Functions

04-02-01A C - 0 (O) May be inoperative provided

alternate, normal, and emergency
procedures and/or operating
restrictions are established and used.

04-02-01B D - 0 May be inoperative provided

procedures do not require its use.

04-02-02 Cabin to Cabin Function D - 0

04-02-03 Flight Deck to Ground

Function
(Includes CALL
Functions)

04-02-03-01 Large Turbojet Airplanes

Operating Under 14 CFR
Part 121

04-02-03-01A C 1 0 (O) Flight interphone flight deck to

ground/ground to flight deck function
may be inoperative provided:
a) Alternate procedures are
established and used, and
b) Nose gear/forward fuselage
service interphone jack
operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

04 Crewmember Interphone
System
(Cont’d)

04-02 Cargo Configuration

(Cont’d)

04-02-03 Flight Deck to Ground

Function
(Includes CALL
Functions)
(Cont’d)

04-02-03-01B C 1 0 (O) Service interphone flight deck to

ground/ground to flight deck function
may be inoperative provided:
a) Alternate procedures are
established and used, and
b) Nose gear/forward fuselage
flight interphone jack operates
normally.

04-02-03-01C B - 0 (O) May be inoperative provided

alternate procedures are established
and used.

04-02-03-02 All Other

Aircraft/Operations

04-02-03-02A C - 0 (O) May be inoperative provided

alternate procedures are established
and used.

04-02-03-02B D - 0 May be inoperative provided

procedures do not require its use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

04 Crewmember Interphone
System
(Cont’d)

04-03 For an Operator other

than a Holder of an Air
Carrier or Commercial
Operator Certificate

04-03-01 Flight Deck to Cabin,

Cabin to Flight Deck
Functions

04-03-01A C - 0 (O) May be inoperative provided

alternate, normal and emergency
procedures and/or operating
restrictions are established and used.

04-03-01B D - 0 May be inoperative provided

procedures do not require its use.

04-03-02 Cabin to Cabin Function D - 0

|
06 Selective Call System
*** (SELCAL)

06A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

06B D 1 0 May be inoperative provided

procedures do not require its use.

06-01 Channels

06-01A C - 0 (O) May be inoperative provided

alternate procedures are established
and used.

06-01B D - 0 May be inoperative provided

procedures do not require its use.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

09 ACARS System
***

09A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Any portion of system that

operates normally may be
used.

09B D 1 0 May be inoperative provided

procedures do not require its use.

NOTE: Any portion of system that

operates normally may be
used.

09-01 ACARS Printer D - 0

09-02 FMC Interface Function

09-02A C - 0 (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Any portion of system that

operates normally may be
used.

09-02B D 1 0 May be inoperative provided

procedures do not require its use.

NOTE: Any portion of system that

operates normally may be
used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

10 Cockpit Voice Recorder

System (CVR)

10-01 Aircraft without Recorder A 1 0 May be inoperative provided:

Independent Power a) Flight Data Recorder (FDR)
Supply (RIPS) operates normally, and
b) Repairs are made within
3 flight-days.

NOTE: With CVR Datalink enabled,

an inoperative ACARS could
cause a CVR fault, refer to
item 23-09.

10-02 Aircraft with Recorder A 1 0 (M) May be inoperative provided:

*** Independent Power a) Flight Data Recorder (FDR)
Supply (RIPS) operates normally,
(-600/-700/-800/ b) RIPS circuit breaker is pulled
-900/-900ER) and collared,
c) A 15 minute interval after
pulling of the c/b is achieved
before departure, and
d) Repairs are made within
3 flight-days.

NOTE 1: CVR is inoperative with the

RIPS c/b pulled and
collared.

NOTE 2: With CVR Datalink enabled,

an inoperative ACARS
could cause a CVR fault,
refer to item 23-09.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

10 Cockpit Voice Recorder

System (CVR)
(Cont’d)

10-02 Aircraft with Recorder

*** Independent Power
Supply (RIPS)
(-600/-700/-800/
-900/-900ER)
(Cont’d)

10-02-01 Recorder Independent

Power Supply (RIPS)

10-02-01A C 1 0 (M) May be inoperative provided:

a) CVR operates normally, and
b) RIPS battery is removed.

10-02-01B A 1 0 (M) May be inoperative provided:

a) Flight Data Recorder (FDR)
operates normally,
b) RIPS battery is removed, and
c) Repairs are made within
3 flight-days.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

11 High Frequency (HF)

*** Communication System
(Includes STCs
ST02959AT and
ST01837LA)

11A D - - Any in excess of those required by

14 CFR may be inoperative.

11B C - 1 (O) One may be inoperative while

conducting operations that require
two LRCS provided:
a) Aircraft SATVOICE system
operates normally,
b) SATVOICE services are
available as an LRCS over
the intended route of flight,
c) The ICAO flight plan is
updated (as required) to notify
ATC of the communications
equipment status of the
aircraft, and
d) Alternate procedures are
established and used.

11-01 HF Data Link |

*** |

11-01A C 1 0 (O) May be inoperative provided |

alternate procedures are established |
and used. |

11-01B D 1 0 May be inoperative provided |

procedures do not require its use. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

12 Emergency Locator
*** Transmitter (ELT)

12-01 Survival Type ELTs D - - Any in excess of those required by

*** 14 CFR may be inoperative or
missing.

12-02 Fixed ELTs

***

12-02A A - 0 (M) May be inoperative provided:

a) System is deactivated, and
b) Repairs are made within
90 days

12-02B A - 0 (M) May be missing provided:

a) Placard stating “ELT not
installed” is placed in view of
the pilot, and
b) Repairs are made within
90 days.

12-02C D - - (M) Any in excess of those required

by 14 CFR may be inoperative
provided system is deactivated.

12-02D D - - Any in excess of those required by

14 CFR may be missing.

12-02-01 Remote ELT Switch D - - (M) May be inoperative provided:

*** a) Remote ELT switch is
deactivated, and
b) ELT switch is placed in the
ARMED mode.

12-02-02 ELT Indicator Light D - -

***
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

13 Flightcrew Audio A 2 1 (O) Either captain’s or first officer’s

Selector/Control Panels audio control panel may be
inoperative provided:
a) Optional AUDIO transfer
switch is installed and
operates normally,
b) Primary observer’s audio
control panel is located on aft
electronics panel and
operates normally, and
c) Repairs are made within
2 flight-days.

13-01 AUDIO Transfer Switch C 1 0

***

13-02 Switch Lights C - 0 |

14 Flight Deck Headsets

Earphones/Headphones
and Boom Microphones

14-01 Headset Boom

Microphones

14-01A A - 0 May be inoperative provided:

a) Associated hand microphone
is installed and operates
normally, and
b) Repairs are made within
3 flight-days.

14-01B D - - Any in excess of those required by

14 CFR may be inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

14 Flight Deck Headsets

Earphones/Headphones
and Boom Microphones
(Cont’d)

14-02 Headset
Earphones/Headphones

14-02A C - 1 Either captain’s or first officer's

headset may be inoperative provided
associated flight deck speaker
operates normally.

14-02B D - - Any in excess of those required by

14 CFR may be inoperative.

14-03 Active Noise Canceling/ D - 0 May be inoperative provided normal

Reduction Function audio function of headset is
operative.

15 Prerecorded Passenger
*** Announcement System

15A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

15B D 1 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-20
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

16 Push-To-Talk (PTT)
Switches

16-01 Control Wheel PTT C 2 1 (M) One may be inoperative

Switches provided:
a) Associated audio selector
panel PTT switch operates
normally, and
b) Affected switch is either
verified failed open or is
deactivated.

16-02 Flightcrew Audio C 2 1 (M) One may be inoperative

Selector Panel PTT provided:
Switches a) Associated control wheel PTT
switch operates normally, and
b) Affected switch is verified
failed open.

16-03 Glareshield Panel PTT

*** Switch(es)

16-03A C - 0 (M) May be inoperative provided

affected switch is either verified failed
open or is deactivated.

16-03B D - 0 (M) May be inoperative provided:

a) Affected switch is either
verified failed open or is
deactivated, and
b) Procedures do not require its
use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-21
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

16 Push-To-Talk (PTT)
Switches
(Cont'd)

16-04 Pendant Switch(es)

***

16-04A C - 0 (M) May be inoperative provided

affected switch is either verified failed
open or is deactivated.

16-04B D - 0 (M) May be inoperative provided:

a) Affected switch is either
verified failed open or is
deactivated, and
b) Procedures are not based on
its use.

17 Flight Deck Hand

*** Microphones |

17A C - 0 May be inoperative or missing

provided associated boom
microphone operates normally.

17B D - 0 Any in excess of those required by

14 CFR may be inoperative or
missing.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-22
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

18 Satellite Communication
*** System (SATCOM)

18A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

18B D 1 0 May be inoperative provided

procedures do not require its use.

18-01 SATCOM Data Link |

*** |

18-01A C 1 0 (O) May be inoperative provided |

alternate procedures are established |
and used. |

18-01B D 1 0 May be inoperative provided |

procedures do not require its use. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-23
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

19 Alerting System
(Audio/Visual)

19-01 Passenger Configuration

19-01-01 Flight Deck Call Visual B 1 0 May be inoperative provided:

Alerting System a) Audio alerting system
operates normally, and
b) Audio alerting system
differentiates between normal
and emergency calls.

19-01-02 Flight Deck Call Audio B 1 0 May be inoperative provided:

Alerting System a) Flight deck visual alerting
system operates normally,
and
b) Flight deck visual alerting
system differentiates between
normal and emergency calls.

19-01-03 Flight Attendant Visual

Alerting System

19-01-03A B 1 0 (O) May be inoperative provided:

a) PA system operates normally,
b) If affected visual alerting
system is used for lavatory
smoke detector alerting, an
alternate lavatory smoke
detector alert (visual or audio)
is installed and operates
normally, and
c) Alternate procedures for
contacting flight attendants
are established and used.

NOTE 1: Passenger to Attendant Call

System is considered
Nonessential Equipment
and Furnishing (NEF).

NOTE 2: Any visual alerting system

function(s) that operates
normally may be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-24
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

19 Alerting System
(Audio/Visual)
(Cont’d)

19-01 Passenger Configuration

(Cont’d)

19-01-03 Flight Attendant Visual

Alerting System
(Cont’d)

19-01-03B B 1 0 (O) May be inoperative provided:

a) Audio alerting system
operates normally,
b) Audio alerting system
differentiates between normal
and emergency calls,
c) If affected visual alerting
system is used for lavatory
smoke detector alerting, an
alternate lavatory smoke
detector alert (audio or visual)
is installed and operates
normally, and
d) Alternate procedures for
contacting flight attendants
are established and used.

NOTE 1: Passenger to Attendant Call

System is considered
Nonessential Equipment
and Furnishing (NEF).

NOTE 2: Any visual alerting system

function(s) that operates
normally may be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-25
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

19 Alerting System
(Audio/Visual)
(Cont’d)

19-01 Passenger Configuration

(Cont’d)

19-01-04 Flight Attendant Audio

Alerting System

19-01-04A B - 0 (O) May be inoperative provided:

a) PA system operates normally,
b) If affected audio alerting
system is used for lavatory
smoke detector alerting, an
alternate lavatory smoke
detector alert (visual or audio
is installed and operates
normally, and
c) Alternate procedures for
contacting flight attendants
are established and used.

NOTE 1: Passenger to Attendant Call

System is considered
Nonessential Equipment
and Furnishing (NEF).

NOTE 2: Any audio alerting system

function(s) that operates
normally may be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-26
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

19 Alerting System
(Audio/Visual)
(Cont’d)

19-01 Passenger Configuration

(Cont’d)

19-01-04 Flight Attendant Audio

Alerting System
(Cont’d)

19-01-04B B - 0 (O) May be inoperative provided:

a) Visual alerting system
operates normally,
b) Visual alerting system
differentiates between normal
and emergency calls,
c) If affected audio alerting
system is used for lavatory
smoke detector alerting, an
alternate lavatory smoke
detector alert (visual or audio)
is installed and operates
normally, and
d) Alternate procedures for
contacting flight attendants
are established and used.

NOTE 1: Passenger to Attendant Call

System is considered
Nonessential Equipment
and Furnishing (NEF).

NOTE 2: Any audio alerting system

function(s) that operates
normally may be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-27
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

19 Alerting System
(Audio/Visual)
(Cont’d)

19-02 Cargo Configuration

19-02-01 Flight Deck Call Visual B 1 0 May be inoperative provided flight

Alerting System deck audio alerting system operates
normally.

19-02-02 Flight Deck Call System D 1 0 May be inoperative provided

courier/supernumerary compartment
remains unoccupied.

19-02-03 Courier/Supernumerary
Visual Alerting System

19-02-03A B 1 0 (O) May be inoperative provided:

a) Courier/supernumerary
address system operates
normally, and
b) Alternate procedures are
established and used.

19-02-03B D 1 0 May be inoperative provided

courier/supernumerary compartment
remains unoccupied.

NOTE: Any visual alerting system

function(s) that operates
normally may be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-28
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

19 Alerting System
(Audio/Visual)
(Cont’d)

19-02 Cargo Configuration

(Cont’d)

19-02-04 Courier/Supernumerary
Audio Alerting System

19-02-04A B 1 0 (O) May be inoperative provided:

a) Courier/supernumerary
address system operates
normally, and
b) Alternate procedures are
established and used.

19-02-04B D - 0 May be inoperative provided

courier/supernumerary compartment
remains unoccupied.

NOTE: Any audio alerting system

function(s) that operates
normally may be used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-29
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

20 Handset Systems
***

20-01 Passenger Configuration

20-01-01 Flight Deck

20-01-01A C 1 0 (O) May be inoperative provided:

a) Flight deck to cabin
communication operates
normally, and
b) Alternate procedures are
established and used.

20-01-01B D 1 0 May be inoperative provided

procedures do not require its use.

20-01-02 Cabin

20-01-02A B - - (O) May be inoperative provided:

a) 50% of cabin handsets
operate normally, and
b) Alternate communication
procedures between affected
flight attendant station(s) are
established and used.

NOTE 1: An operative handset at an

inoperative flight attendant
seat shall not be counted to
satisfy 50% requirement.

NOTE 2: Any handset functions that

operate normally may be
used.

20-01-02B B 1 0 NOTE: Any handset functions that

operate normally may be
used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-30
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

20 Handset Systems
*** (Cont’d)

20-02 Cargo Configuration

20-02-01 Flight Deck

20-02-01A C 1 0 (O) May be inoperative provided flight

deck to courier/supernumerary
communication operates normally.

20-02-01B D 1 0 May be inoperative provided

procedures do not require its use.

20-02-02 Courier/Supernumerary

20-02-02A D - 1

20-02-02B D - 0 May be inoperative provided

courier/supernumerary compartment
remains unoccupied.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-31
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

21 Electronic Visual
*** Surveillance Systems
(All Installed Systems)

21A A 1 0 (O) May be inoperative and

components may be missing
provided:
a) Alternate procedures are
established and used, and
b) Repairs are made within
3 flight-days.

NOTE: Any portion of the system

which operates normally may
be used.

21B C 1 0 (O) May be inoperative and

components may be missing
provided:
a) The flight deck door viewing
port is installed and operates
normally, and
b) Alternate procedures are
established and used.

NOTE: Any portion of the system

which operates normally may
be used.

21C D 1 0 May be inoperative and components

may be missing provided procedures
do not require its use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-32
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

21 Electronic Visual
*** Surveillance Systems
(All Installed Systems)
(Cont’d)

21-01 All-Cargo Configuration

21-01A C 1 0 May be inoperative provided

courier/supernumerary compartment
remains empty.

21-01B D 1 0 May be inoperative and components

may be missing provided procedures
do not require its use.

22 Electronic Voice C 1 0 (O) May be inoperative provided

*** Checklist alternate procedures are established
and used.

23 Multipurpose Interactive C 1 0 (O) May be inoperative provided

*** Display Unit (MIDU) alternate procedures are established
and used for affected subsystems.

24 Landscape Camera D 1 0
*** System
(-800EF
STC ST02000NY)

24-01 Dome Camera D 1 0 (M) May be inoperative or missing.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-33
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

25 Automated Flight
*** Information Reporting
System (AFIRS)
(STCs ST10345SC and
ST02361NY)

25A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Any portion of system that

operates normally may be
used.

25B D 1 0 May be inoperative provided

procedures do not require its use.

NOTE: Any portion of system that

operates normally may be
used.

25-01 Global Voice SATCOM

*** (ST02361NY)

25-01A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

25-01B D 1 0 May be inoperative provided

procedures do not require its use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-34
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

25 Automated Flight
*** Information Reporting
System (AFIRS)
(STCs ST10345SC and
ST02361NY)
(Cont’d)

25-01 Global Voice SATCOM

*** (ST02361NY)
(Cont’d)

25-01-01 Cockpit Dialer Pad

25-01-01A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

25-01-01B D 1 0 May be inoperative provided

procedures do not require its use.

25-01-02 Flt Compt. Handset

25-01-02A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

25-01-02B D 1 0 May be inoperative provided

procedures do not require its use.

25-01-03 Pax. Compt. Handset

25-01-03A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

25-01-03B D 1 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-35
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

25 Automated Flight
*** Information Reporting
System (AFIRS)
(STCs ST10345SC and
ST02361NY)
(Cont’d)

25-02 Global Messaging

*** (ST02361NY)

25-02A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

25-02B D 1 0 May be inoperative provided

procedures do not require its use.

NOTE: Any portion of the system that

operates normally may be
used.

26 Avionica secureLINK D 1 0 May be inoperative provided

*** Airborne Wireless Router procedures do not require its use.
(STC03151AT)
NOTE: Any mode that operates
normally may be used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-36
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

27 Data Link
*** Communication

27A Incorporated into Items 23-03, 23-11 |

and 23-18 in Revision 62. |

27B Incorporated into Items 23-03, 23-11 |

and 23-18 in Revision 62. |

28 FWD and AFT Attendant C 6 0 (O) May be inoperative provided

*** Control Panel LCD alternate procedures are established
Touch Screen Display, and used.
Display Processor, and
Display Processor NOTE: Any portion of the system that
Over-Temperature LED operates normally may be
Light, Boeing Sky Interior used.
(BSI)
(-600/-700/-800/
-900/-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 23-37
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
23. Communications
Change
Sequence No. Item 1 2 3 4 Bar

29 Passenger Cabin |
*** Medical Communications |
System |

29A C 1 0 (O) May be inoperative and |

components may be missing provided |
alternate procedures are established |
and used. |

NOTE: Any portion of the system that |

operates normally may be |
used. |

29B D 1 0 May be inoperative and components |

may be missing provided procedures |
do not require its use. |

NOTE: Any portion of the system that |

operates normally may be |
used. |

30 Low Frequency D 1 0 Any in excess of those required by |

*** Underwater Locating 14 CFR may be inoperative or |
Device (LF-ULD) missing. |
(-600/-700/-800/-900/- |
900ER upon |
incorporation of Boeing |
Service Bulletin 737-23- |
1605 or production |
equivalent) |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 24-1
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
24. Electrical Power
Change
Sequence No. Item 1 2 3 4 Bar

01 Engine Driven Generator

Systems

01-01 (-100/-200/-300/
-400/-500)

01-01A B 2 1 (M)(O) Except for ER operations,

may be inoperative provided:
a) APU generator operates
normally and is used
throughout flight, and
b) An APU fuel heater is
installed.

01-01B B 2 1 (M)(O) Except for ER operations,

may be inoperative provided:
a) APU generator operates
normally and is used
throughout flight, and
b) Fuel temperature is
maintained at or above 32 °F
(0 °C).

01-02 (-600/-700/-800/ B 2 1 (M)(O) Except for ER operations,

-900/-900ER) may be inoperative provided: APU
generator operates normally and is
used throughout flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 24-2
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
24. Electrical Power
Change
Sequence No. Item 1 2 3 4 Bar

02 APU Generator System C 1 0 Except for ER operations, may be

inoperative.

03 Engine Driven Generator

LOW OIL
PRESSURE/DRIVE
Lights

03-01 (-100/-200/-300/ C 2 0 LOW OIL PRESSURE/DRIVE lights

-400/-500) and associated generator low oil
pressure switches may be inoperative
provided associated HIGH OIL TEMP
light and oil temperature indicator
operate normally.

03-02 (-600/-700/-800/ C 2 0 DRIVE lights and associated

-900/-900ER) generator low oil pressure switches
may be inoperative.

04 Engine Driven Generator C 2 0 May be inoperative provided

Oil Temperature associated LOW OIL
Indicator Systems PRESSURE/DRIVE light and HIGH
(-100/-200/ OIL TEMP light operates normally.
-300/-400/-500)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 24-3
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
24. Electrical Power
Change
Sequence No. Item 1 2 3 4 Bar

05 Engine Driven Generator C 2 0 May be inoperative provided

HIGH OIL TEMP Lights associated LOW OIL
(-100/-200/-300/ PRESSURE/DRIVE light and oil
-400/-500) temperature indicator operate
normally.

06 Transformer Rectifiers

06-01 No. 2 TR B 1 0 Except for ER operations, may be

(-100/-200) inoperative provided:
a) All DC busses and all
generators (including APU
generator) operate normally,
and
b) APU generator can be
electrically connected to either
bus.

07 Frequency Meter C 1 0

08 AC Volts Indication B 1 0 (O) May be inoperative except in

STBY PWR position provided
Standby Power Test is accomplished.

08-01 Residual Voltage C 1 0

Function
(-100/-200/-300/
-400/-500)

09 AC Ammeters C - 0 May be inoperative provided

associated generator off bus lights
operate normally.

10 Generator System C 1 0
Annunciator Panel
(-100/-200/-300/
-400/-500)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 24-4
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
24. Electrical Power
Change
Sequence No. Item 1 2 3 4 Bar

11 External Power System C 1 0 NOTE: Any portion of system which

operates normally may be
used.

11-01 DC Receptacle D 1 0
***

12 GEN OFF BUS Lights C 2 1 One may be inoperative provided

associated generator AC ammeter
operates normally.

13 Galley Load Shed C 1 0 May be inoperative provided GALLEY

*** Sensor Module Power Switch remains OFF when
(-300/-400/-500) APU is being used to power both
generator busses on ground.

14 BAT DISCHARGE Light C 1 0

***

15 TR UNIT Light C 1 0
***

16 ELEC Light
***

16-01 (-300/-400/-500) C 1 0 (O) May be inoperative OFF

provided:
a) Standby Power Test is
accomplished, and
b) Battery Charger is verified to
operate normally.

16-02 (-600/-700/-800/ C 1 0 (O) May be inoperative OFF

-900/-900ER) provided:
a) Standby Power Test is
accomplished once each
flight-day, and
b) Battery Charger is verified to
operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 24-5
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
24. Electrical Power
Change
Sequence No. Item 1 2 3 4 Bar

17 DC Ammeter Indication B 1 0 (O) May be inoperative provided:

a) BAT position operates
normally,
b) Standby Power Test is
accomplished, and
c) Procedures do not require its
use.

18 DC Volts Indication B 1 0 (O) May be inoperative except in

STBY PWR position provided
Standby Power Test is accomplished.

19 APU GEN OFF BUS C 1 0 May be inoperative provided:

Light a) APU frequency meter
operates normally, and
b) APU ammeter operates
normally.

20 Cabin Power Switch B 1 0 (M) May be inoperative provided

*** (Jet Aviation Engineering procedures are established and used
Services (JAES)) to deactivate cabin power.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

01 Megaphones D - - Any in excess of those required by

(Includes STCs 14 CFR may be inoperative or
SA2969SO, and removed provided: |
ST10238SC) a) Inoperative megaphone |
remains in a certified location |
until removed from the aircraft |
at the next suitable |
maintenance facility, |
b) Location placarding is |
removed or obscured, and |
c) Required distribution is
maintained.

NOTE: Not required for all-cargo

operations.

01-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper installation |
and operation is verified at each |
preflight. |
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

03 Flight Attendant Seat

Assembly
(Single or Dual Position)

03-01 Required Flight B - - (M)(O) One seat position or assembly

Attendant Seats (dual position) may be inoperative
provided:
a) Affected seat or seat
assembly is not occupied,
b) Flight attendant(s) displaced
by inoperative seat(s)
occupies either an adjacent
flight attendant seat or
passenger seat which is most
accessible to inoperative
seat(s) so as to most
effectively perform assign
duties,
c) Alternate procedures are
established and used as
published in crewmembers
manuals,
d) Folding type seat stows
automatically or is secured in
retracted position, and
e) Passenger seat assigned to
flight attendant is placarded
“FOR FLIGHT ATTENDANT
USE ONLY”.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

03 Flight Attendant Seat

Assembly
(Single or Dual Position)
(Cont’d)

03-01 Required Flight NOTE 1: An automatic folding seat

Attendant Seats that will not stow
(Cont’d) automatically is considered
inoperative.

NOTE 2: A seat position with an

inoperative or missing
restraint system is
considered inoperative.

NOTE 3: Individual operators, when

operating with inoperative
seats, will consider locations
and combinations of seats
to ensure that proximity to
exits and distribution
requirements of applicable
14 CFR are met.

NOTE 4: If one side of a dual seat

assembly is inoperative and
a flight attendant is
displaced to adjacent seat,
adjacent seat must operate
normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

03 Flight Attendant Seat

Assembly
(Single or Dual Position)
(Cont’d)

03-02 Excess Flight Attendant C - - (M) May be inoperative provided:

Seats a) Affected seat position or seat
assembly is not occupied, and
b) Folding type seat stows
automatically or is secured in
retracted position.

NOTE 1: An automatic folding seat

that will not stow
automatically is considered
inoperative.

NOTE 2: A seat position with an

inoperative or missing
restraint system is
considered inoperative.

03-03 All-Cargo Configuration D - - May be inoperative provided affected

seat or seat assembly is not
occupied.

03-04 Seat Cushion Heating D - 0 (M) May be inoperative provided

*** System heating system is deactivated.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

04 Cabin Window Shades D - 0 May be inoperative in a compartment

used for cargo provided AFM
Limitations are observed.

NOTE: Passenger Cabin Window

Shades in compartments
configured for passengers
only are considered
Nonessential Equipment and
Furnishing (NEF).

05 Cargo Compartment
Restraint Components
(Includes -800BCF and
STC ST02556SE)

05A A - - (M) May be inoperative or missing

provided:
a) Cargo-loading limits from the |
OEM Weight and Balance |
Manual are observed, and |
b) Repairs are made within |
120 consecutive |
calendar -days. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

05 Cargo Compartment
Restraint Components
(Includes -800BCF and
STC ST02556SE)
(Cont’d)

05B A - - May be inoperative or missing |

provided: |
a) Cargo compartment remains |
empty, and |
b) Repairs are made within |
120 consecutive |
calendar-days. |

05C C - - May be inoperative or missing

provided pallet with inoperative
lock(s) is removed.

05-01 Passenger Pallets C - - (M) One lock per pallet may be

(737C, -300 QC, inoperative provided:
and -700C) a) Three seats in group
associated with lock are
blocked by folding and
securing backrests in a
forward position, and
b) If more than one lock is
inoperative, pallet must be
removed.

NOTE: If a pallet lock cover is broken

or missing, associated lock is
considered inoperative.

05-02 Cargo Pallet Locks C - - (M)(O) May be inoperative or missing

(Pemco 737 F/QC provided acceptable cargo loading
and COMBI, limits from an approved source
STC ST02556SE) (i.e., an approved Cargo Loading
Manual, Cargo Handling Manual, or
Weight and Balance Document) are
observed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

06 Passenger Seats D - - May be inoperative provided: |

(Includes all a) Seat does not restrict access |
Configurations and to any emergency exit, egress |
Locations, and route, or main aisle, and |
STC ST10238SC) b) Affected seat(s) is blocked |
and placarded
“DO NOT OCCUPY”.

NOTE 1: A seat with an inoperative

seat belt or shoulder |
harness is considered |
inoperative.

NOTE 2: Affected seat(s) may |

include the seat(s) behind |
and/or adjacent outboard |
seats. |

NOTE 3: Inoperative seats do not

affect the required number
of Flight Attendants.

06-01 Recline Mechanism

06-01A D - - (M) May be inoperative and seat

occupied provided seat is secured in
upright position.

06-01B D - - May be inoperative and seat

occupied provided seat back is
immovable in full upright position.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

06 Passenger Seats
(Includes all
Configurations and
Locations, and STC
ST10238SC)
(Cont’d)

06-02 Armrests

06-02-01 With Seat Positioning D - - (M) May be inoperative or missing |

Controls for Taxi, and seat occupied provided: |
Takeoff, and Landing a) Armrest does not restrict |
(TTL) and/or Other access to any emergency exit, |
Controls egress route, or main aisle, |
and |
b) If Armrest with seat control is |
missing or removed, seat is |
secured in taxi, takeoff, and |
landing (TTL) position. |

06-02-02 Without Seat Positioning D - - May be inoperative or missing and |

Controls for Taxi, seat occupied provided it does not |
Takeoff, and Landing restrict access to any emergency exit, |
(TTL) and/or Other egress route, or main aisle. |
Controls |

06-03 Underseat Baggage C - - (O) May be inoperative provided:

Restraining System a) Baggage is not stowed under |
seat with inoperative
restraining system, |
b) Associated seat is placarded
“DO NOT STOW BAGGAGE
UNDER THIS SEAT”, and
c) Procedures are established to
alert Cabin Crew of
inoperative restraining
system. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

06 Passenger Seat(s)
(Includes
STC ST10238SC)
(Cont’d)
|
06-05 Seat Belt/Air Bag
Restraint Systems

06-05-01 Seat Belt/Air Bag D - - May be inoperative provided affected

Restraint System seat is blocked and placarded
Required By 14 CFR “DO NOT OCCUPY”.

06-05-02 Seat Belt/Air Bag Not D - - (M) May be inoperative or

*** Required by 14 CFR disconnected provided seat belt
operates normally.

06-06 Delethalization Pads D - - May be inoperative or missing |

*** provided affected seat is blocked and |
placarded "DO NOT OCCUPY". |
|
09 “Fasten Seat Belts While C - - One or more signs or placards may
Seated” Signs or be illegible or missing provided a
Placards legible sign or placard is visible from
each occupied passenger seat.

10 Nonessential Equipment - 0 May be inoperative, damaged, or

*** and Furnishing (NEF) missing provided that item(s) is
deferred in accordance with
operator’s NEF deferral program.
NEF program, procedures, and
processes must be outlined in
operator’s appropriate document.
(M) and (O) procedures, if required,
must be available to flightcrew and
included in operator’s appropriate
document.

NOTE: Exterior lavatory door

ashtrays are not considered
NEF items.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

11 Observer Seat(s)

11-01 Primary Observer’s Seat

(Including Associated
Equipment)

11-01A A 1 0 May be inoperative provided:

a) A passenger seat in
passenger cabin is made
available to an FAA inspector
for performance of official
duties, and
b) Repairs are made within
2 flight-days.

11-01B A 1 0 May be inoperative provided:

a) Second observer’s seat is
available to an FAA inspector
for performance of official
duties, and
b) Repairs are made within
2 flight-days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

11 Observer Seat(s)
(Cont’d)

11-01 Primary Observer’s Seat

(Including Associated
Equipment)
(Cont’d)

11-01C A 1 0 May be inoperative provided:

a) Required minimum safety
equipment (safety belt and
oxygen) is available,
b) Seat is acceptable to an
FAA inspector for
performance of official duties,
and
c) Repairs are made within
2 flight-days.

NOTE 1: These provisos are

intended to provide for
occupancy of above seats
by an FAA inspector when
minimum safety equipment
(safety belt and oxygen) is
functional and inspector
determines conditions to be
acceptable.

NOTE 2: Pilot-in-Command will

determine if minimum safety
equipment is functional for
other persons authorized to
occupy any observer
seat(s).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

11 Observer Seat(s)
(Cont’d)

11-02 Second Observer’s Seat D 1 0 NOTE: Pilot-in-Command will

*** (Including Associated determine if minimum safety
Equipment) equipment is functional for
other persons authorized to
occupy any observer seat(s).

11-03 Crotch Straps C - 0

***

11-04 Observer Seat Not D - 0 NOTE: Pilot-in-Command will

Required by 14 CFR determine if minimum safety
(Including Associated equipment is functional for
Equipment) other persons authorized to
occupy any observer seat(s).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

12 Portable Flashlight |
*** Holders/Flashlights

12-01 Cabin |

12-01A C - - May be inoperative or removed |

provided: |
a) Crewmember assigned to the |
affected position has an |
equivalent operative flashlight |
readily available, |
b) Inoperative flashlight remains |
in a certified location or is |
removed from the aircraft, and |
c) Location placarding is |
removed or obscured. |

12-01B D - - Any in excess of those required by |

14 CFR may be inoperative or |
removed provided: |
a) Inoperative flashlight remains |
in a certified location until |
removed from the aircraft at |
the next suitable maintenance |
facility, and |
b) Location placarding is |
removed or obscured. |

12-01-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper installation |
and operation is verified at each |
preflight. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

12 Portable Flashlight
*** Holders/Flashlights
(Cont’d)

12-02 Flight Deck |

12-02A C - - May be inoperative or removed |

provided: |
a) Crewmember assigned to the |
affected position has an |
equivalent operative flashlight |
readily available, |
b) Inoperative flashlight remains |
in a certified location or is |
removed from the aircraft, and |
c) Location placarding is |
removed or obscured. |

12-02B D - - Any in excess of those required by |

14 CFR may be inoperative or |
removed provided: |
a) Inoperative flashlight remains |
in a certified location until |
removed from the aircraft at |
the next suitable maintenance |
facility, and |
b) Location placarding is |
removed or obscured. |

12-02-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper installation |
and operation is verified at each |
preflight. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

13 Emergency Evacuation
*** Signal System

13A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

13B D 1 0 May be inoperative provided

procedures do not require its use.

14 Main Deck Cargo 9G

Barrier Net

14-01 (737F and QC) C 1 1 One net attachment, at any location,

(PEMCO World Air may be broken or missing provided
Services, Inc.) maximum loading on main deck is
reduced to 34,650 lbs. |

NOTE: Not required for all-passenger

operations.

14-02 (-700C and -700 Combi)

14-02A C 1 0 In cargo mode, may be missing or net

attachments may be broken or
missing provided approved cargo
loading limits in Weight and Balance
Control and Loading Manual are
observed.

NOTE: Not required for all-passenger

operations.

14-02B D 1 0 May be missing or net attachments

may be broken or missing provided
associated cargo compartment
remains empty.

NOTE: Not required for all-passenger

operations.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo 9G

Barrier Net
(Cont’d)

14-03 (STC ST01566LA)

14-03A C 1 1 In cargo mode only, one attachment

may be broken or missing provided:
a) There are no visible defects
on remaining net fittings, and
b) Maximum allowable load
limits are observed.

14-03B D 1 0 May be missing or net attachments

may be broken or missing provided
associated cargo compartment
remains empty.

NOTE: Not required for all-passenger

operations.
|
16 Lower Cargo C - - (M)(O) May be damaged or missing
Compartment Lining provided procedures are established
Panels and Floor Panels and used to ensure associated
compartment remains empty or is
verified to contain only empty cargo
handling equipment, ballast (ballast
may be loaded in ULDs), and/or Fly
Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

17 Emergency Medical
Equipment
(Includes
STC ST10238SC)

17-01 First Aid Kit (FAK) and/or

Associated Equipment

17-01A A - - (O) If more than one is required by

14 CFR, only one required FAKs may |
be incomplete or removed provided: |
a) The FAK is labeled or |
placarded in a manner that |
will identify it as a unit that |
can not be mistaken for a fully |
serviceable unit, |
b) Location placarding is |
removed or obscured, and |
c) Repairs or replacements are |
made within one flight. |

NOTE: Medical equipment installed in |

the aircraft as part of an |
Emergency Medical Service |
(EMS) operation is not |
considered part of the normal |
complement of equipment. No |
MMEL relief applies to that |
equipment and 14 CFR |
maintenance and inspection |
requirements do not apply. |

17-01B D - - Any in excess of those required by

14 CFR may be incomplete or |
removed. |

17-01-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper FAK |
servicing is verified at each preflight. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

17 Emergency Medical
Equipment
(Includes
STC ST10238SC)
(Cont’d)

17-02 Emergency Medical Kit

(EMK) and/or Associated
Equipment

17-02A A - 0 (O) May be incomplete or removed |

provided: |
a) EMK is labeled or placarded in |
a manner that will identify it as |
a unit that can not be mistaken |
for a fully serviceable unit, |
b) Location placarding is |
removed or obscured, and |
c) Repairs or replacements are |
made within one flight. |

NOTE: Medical equipment installed in |

the aircraft as part of an |
Emergency Medical Service |
(EMS) operation is not |
considered part of the normal |
complement of equipment. No |
MMEL relief applies to that |
equipment and 14 CFR |
maintenance and inspection |
requirements do not apply. |

17-02B D - - Any in excess of those required by

14 CFR may be incomplete or |
removed. |

17-02-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper EMK |
servicing is verified at each preflight. |
|

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

17 Emergency Medical
Equipment
(Includes
STC ST10238SC)
(Cont’d)

17-04 Automatic External

Defibrillator (AED) and/or |
Associated Equipment

17-04A A - 0 (O) May be incomplete, inoperative or |

removed provided: |
a) AED is labeled or placarded in |
a manner that will identify it as |
a unit that can not be mistaken |
for a fully serviceable unit, |
b) Location placarding is |
removed or obscured, and |
c) Repairs or replacements are |
made within one flight. |

NOTE: Medical equipment installed in |

the aircraft as part of an |
Emergency Medical Service |
(EMS) operation is not |
considered part of the normal |
complement of equipment. No |
MMEL relief applies to that |
equipment and 14 CFR |
maintenance and inspection |
requirements do not apply. |

17-04B D - - Any in excess of those required by

14 CFR may be incomplete, |
inoperative, or removed. |

17-04-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper installation |
and operation is verified at each |
preflight. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-20
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

18 Flotation Equipment D - - Any in excess of those required by

(Crew and Passengers) 14 CFR may be inoperative or
missing provided required distribution
is maintained.
|
20 Exterior Lavatory Door
Ashtrays

20-01 Airplanes with Multiple

Exterior Lavatory Door
Ashtrays Installed

20-01A A - - Up to and including 50% maybe

missing or inoperative for 10 days.

NOTE: Crew lavatories are included

in the total aircraft exterior
lavatory door ashtray count.

20-01B A - - More than 50% may be missing or

inoperative for 3 days.

NOTE: Crew lavatories are included

in the total aircraft exterior
lavatory door ashtray count.

20-02 Airplanes with Only One A 1 0 May be missing provided it is

Exterior Lavatory Door replaced within 10 consecutive |
Ashtray Installed calendar-days. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-21
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

21 Flightcrew Seats

21-01 Recline Mechanism A 2 0 (M) May be inoperative provided:

a) Seat is secured in a position
acceptable to affected
crewmember, and
b) Repairs are made within
2 flight-days.

21-02 Vertical Adjustment A 2 0 (M) May be inoperative provided:

a) Seat is secured in a position
acceptable to affected
crewmember, and
b) Repairs are made within
2 flight-days.

21-03 Armrests B 4 0 (M) May be inoperative in up position

or removed provided seat is
acceptable to affected crewmember.

21-04 Lumbar/Thigh Supports C 4 0 May be inoperative provided seat is

acceptable to affected crewmember.

21-05 Headrests C 2 0 May be inoperative or missing

*** provided seat is acceptable to
affected crewmember.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-22
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

22 Galley/Lavatory Waste
Receptacle Access
Doors/Covers

22-01 Galley Waste C - - (M)(O) May be inoperative provided:

Receptacle Access a) Associated container is empty,
Doors/Covers b) Container access is secured
to prevent waste introduction
into compartment, and
c) Procedures are established to
ensure that sufficient
galley/lavatory waste
receptacles are available to
accommodate all waste that
may be generated during
flight.

22-02 Lavatory Waste C - - (M)(O) May be inoperative provided:

Receptacle Access a) Associated container is empty,
Doors/Covers b) Container access is secured
to prevent waste introduction
into compartment,
c) Lavatory is used only by
crewmembers, and
d) Associated lavatory entrance
door is locked closed and
placarded “INOPERATIVE -
DO NOT ENTER”.

NOTE: These provisions are not

intended to prohibit lavatory
use or inspection by
crewmembers.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-23
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

23 Automatic Cargo D - 0 NOTE: Any portion of system(s) that

*** Loading Systems operates normally may be
used.

24 Storage Bins/Cabin,
*** Galley, and Lavatory
Storage
Compartments/Closets

24A C - - (M) May be inoperative provided:

a) Procedures are established to
secure the affected bin,
compartment, or closet in the
closed position,
b) Affected bin, compartment, or
closet is prominently
placarded “DO NOT USE”,
c) Any emergency equipment
located in affected bin,
compartment, or closet is
considered inoperative, and
d) Affected bin, compartment, or
closet is not used for storage
of any item(s) except for those
permanently affixed.

NOTE 1: For overhead bins, if no |

partitions are installed, the
entire overhead bin is
considered inoperative.

NOTE 2: Proviso is not intended to |

preclude crewmember |
inspections. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-24
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

24 Storage Bins/Cabin,
*** Galley, and Lavatory
Storage
Compartments/Closets
(Cont’d)

24B C - - (M)(O) May be inoperative provided:

a) For non-retractable doors,
affected door is removed,
b) For retractable doors, affected
door is removed or secured in
the retracted (fully open)
position,
c) Affected bin, compartment, or
closet is not used for storage
of any items except those
permanently affixed,
d) Affected bin, compartment, or
closet is prominently
placarded “DO NOT USE”,
e) Procedures are established
and used to alert
crewmembers and
passengers of inoperative
bins, compartments, or
closets, and
f) Passengers are briefed that
affected bin, compartment, or
closet is not used.

NOTE 1: For overhead bins if no

partitions are installed,
entire overhead bin is
considered inoperative.

NOTE 2: Any emergency equipment

located in the affected bin,
compartment or closet
(permanently affixed) is
available for use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-25
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

24 Storage Bins/Cabin,
*** Galley, and Lavatory
Storage
Compartments/Closets
(Cont’d)

24C C - - May be inoperative in closed position |

provided: |
a) Affected bin, compartment, or |
closet is prominently |
placarded “DO NOT USE”, |
b) Any emergency equipment |
located in affected bin, |
compartment, or closet is |
considered inoperative, and |
c) Location placarding for any |
emergency equipment stored |
in affected bin, compartment, |
or closet is removed or |
obscured. |

NOTE: Use of this proviso may be |

dependent upon an operator’s |
aircraft security program, as |
appropriate. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-26
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

24 Storage Bins/Cabin,
*** Galley, and Lavatory
Storage
Compartments/Closets
(Cont’d)

24-01 Multi Latch/ C - - One latch/lug per compartment may

*** Quarter-Turn Lug be inoperative provided:
Installations a) Remaining latch(es)/lug(s) on
affected compartments
operates normally, and
b) If affected compartment is
used for a galley cart, cart
remains empty.

24-02 Storage Compartment D - 0 (M) May be inoperative in the

*** Key Locks unlocked position provided doors can
be secured by other means.

25 Beds C - 0 May be inoperative provided manual

*** (Electrical Operation) override system operates normally.
(Jet Aviation Engineering
Services (JAES))

26 Tables
*** (Electrical Operation)
(Jet Aviation Engineering
Services (JAES))

26A C - 0 May be inoperative provided manual

override system operates normally.

26B C - 0 May be inoperative provided seats at

associated inoperative table are
not occupied.

27 Crash Pads C - 0 May be inoperative or missing

*** (Jet Aviation Engineering provided associated seat adjacent to
Services (JAES)) crash pad is not occupied.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 25-27
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
25. Equipment/Furnishings
Change
Sequence No. Item 1 2 3 4 Bar

28 Cockpit Smoke Vision D 2 0 May be inoperative or missing.

*** System (CSVS)
(-600/-700/-800/-900/
-900ER)
(STC ST00892LA)

29 Secondary Door Barrier

*** (Flight Deck Security)

29A C 1 0 (O) May be inoperative provided:

a) Barrier remains in retracted
position, and
b) Alternate procedures are
established and used.

29B C 1 0 (M)(O) May be inoperative provided:

a) Barrier is removed, and
b) Alternate procedures are
established and used.

29C D 1 0 May be inoperative provided

procedures do not require its use.

30 Security Kit and/or D - 0 May be inoperative, missing, or have

*** Associated Equipment missing equipment.

31 Supernumerary Seats D - 0 (M) May be inoperative provided:

*** (-800BCF and a) Seat is not occupied, and
ST02556SE) b) Seat is stowed or secured.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

01 Engine and APU Fire C 3 0

Extinguisher Discharge
Lights

02 Engine Overheat and

Fire Detection Systems

02-01 Basic Systems C 4 2 (M) One overheat detection system

(-100/-200) or one fire detection system per
engine may be inoperative provided
operative system is tested and
operates normally before each
departure.

02-02 Dual Loop C 4 2 (O) Except for ER operations beyond

120 minutes, one loop (A or B) per
engine may be inoperative provided |
remaining operative loops are verified |
to operate normally once each |
flight-day. |

03 Portable Fire D - - Any in excess of those required by |

Extinguishers 14 CFR may be inoperative or |
removed provided: |
a) Inoperative fire extinguisher |
remains in a certified location |
until removed from the aircraft |
at the next suitable |
maintenance facility, |
b) Location placarding is |
removed or obscured, and |
c) Required distribution is |
maintained. |

NOTE: Inoperative fire extinguishers, |

removed from a certified |
location or removed from the |
aircraft, are subject to 49 CFR |
dangerous goods regulations. |

03-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper installation |
and servicing is verified at each |
preflight. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

04 Wheel Well Fire

Detection System

04A C 1 0 (M) May be inoperative provided: |

a) Wheel Well fire detection |
system is deactivated, and |
b) Brake temperature monitoring |
system (BTMS) operates |
normally. |

04B C 1 0 (M)(O) May be inoperative provided: |

a) Wheel well fire detection |
system is deactivated, |
b) Landing gear remain |
extended for ten minutes after |
takeoff, and |
c) Appropriate performance |
adjustments are applied. |
|
NOTE: In case of engine failure after |
V1, landing gear should be
retracted until takeoff
obstacles are cleared.

05 APU Fire Extinguisher C 2 0 (M) Discs may be missing provided

Discharge Discs indicator reading is checked to verify
(-100/-200/-300/ proper charge.
-400/-500)

05-01 HTL Type C 2 0 (M) Discs may be missing provided

*** bottle integrity is verified by checking
APU fire extinguisher bottle discharge
light or weighing bottle once each
flight-day.

06 APU Fire Shutoff System C 1 0 (O) Except for ER operations, may be

inoperative provided APU is not used.

07 APU Fire Extinguisher C 1 0 (O) Except for ER operations, may be

System inoperative provided APU is not used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

08 APU Fire Detection

System

08-01 Single and Dual Loop C - 0 (O) Except for ER operations, may be
inoperative provided APU is not used.

08-02 APU DET INOP Light C 1 0 (O) May be inoperative extinguished

*** provided:
d) APU fire detection system
operates normally, and
e) A fire warning test is
performed before each APU
start.

08-03 Dual Loop C 2 1 (O) Except for ER operations beyond

*** 120 minutes, one loop (A or B) may |
be inoperative.

08-04 External Warning C 1 0 May be inoperative for ground

Horn/Warning Light operation provided flight deck APU
Overheat/Fire Protection Panel is
continuously monitored.

09 Engine/APU Fire C 3 0 (M) May be inoperative provided:

Extinguisher Test a) Failure is verified to be in
System squib test circuit.
(EXT TEST) b) Squib circuit is verified to
(Squib Test) operate normally once each
flight-day.

09-01 APU Fire Extinguisher C 2 1 (O) May be inoperative provided

Squib Test Circuits remaining APU Squib test circuit is
(EXT TEST) verified to operate normally once
(-300/-400/-500/-600/ each flight-day.
-700/-800/-900/-900ER)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

09 Engine/APU Fire
Extinguisher Test
System
(EXT TEST)
(Squib Test)
(Cont’d)

09-02 APU Squib Light C 1 0 (O) Except for ER operations, may be

inoperative provided APU is not used.

10 Fire Warning Bell

10-01 Bell Cutout Switch C 1 0 May be inoperative provided:

(Overheat/Fire a) Bell cutout function of both
Protection Panel) Master Fire Warning lights
operates normally, and
b) Fire Warning Bell operates
normally.

10-02 Bell Cutout Function of C 2 1 May be inoperative provided:

Master Fire Warning a) Bell cutout function switch
Light operates normally, and
b) Fire Warning Bell operates
normally.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

12 Wing-Body Overheat
Detector System
(Left)

12-01 -100/-200/-300/-400/ C 1 0 (O) Except for ER operations, may be

-500/-600/-700/-800 inoperative provided:
c) Right pack and right engine |
bleed is used for
pressurization only,
d) Use of APU is prohibited
except for engine start,
e) Isolation valve and left engine
bleed valve remain closed for
all operations except engine
start,
f) Airplane is not operated in
known or forecast icing
conditions, and
g) Flight altitude remains at or
below FL 250.

12-02 -900/-900ER C 1 0 (O) Except for ER operations, may be

inoperative provided:
a) Right pack and right engine |
bleed is used for
pressurization only,
b) Use of APU is prohibited
except for engine start,
c) Isolation valve and left engine
bleed valve remain closed for
all operations except engine
start,
d) Airplane is not operated in
known or forecast icing
conditions,
e) Flight altitude remains at or
below FL 250,
f) Forward cargo heat duct is
secured closed, and
g) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

13 Wing-Body Overheat
Detector System
(Right)

13-01 -100/-200/-300/-400/ C 1 0 (O) Except for ER operations, may be

-500/-600/-700/-800 inoperative provided:
a) Left pack and left engine or
APU bleed air is used for
pressurization only,
b) Isolation valve and right
engine bleed valve remain
closed for all operations
except engine start,
c) Airplane is not operated in
known or forecast icing
conditions, and
d) Flight altitude remains at or
below FL 250.

13-02 -900/-900ER C 1 0 (O) Except for ER operations, may be

inoperative provided:
a) Left pack and left engine or
APU bleed air is used for
pressurization only,
b) Isolation valve and right
engine bleed valve remain
closed for all operations
except engine start,
c) Airplane is not operated in
known or forecast icing
conditions,
d) Flight altitude remains at or
below FL 250,
e) Forward cargo heat duct is
secured closed, and
f) Airport ambient temperature
does not exceed 103 °F
(39 °C).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo C 2 0 (O) May be inoperative provided

*** Compartment Fire procedures are established and used
Detection/Suppression to ensure main deck cargo
Systems compartment remains empty or is
(737C/QC/-700C/-700 verified to contain only empty cargo
Combi/-800BCF, STCs handling equipment, ballast (ballast
ST01566LA, -400C may be loaded in ULDs), and/or Fly
ST00235BO, -400 Away Kits.
Combi ST00248BO,
SA2970SO, ST01827LA, NOTE: Operator MELs must define
ST00283AT, which items are approved for
ST01961SE, and inclusion in Fly Away Kits and
ST02556SE) which materials can be used
as ballast.

14-01 Fire Detection

(-700C, -700 Combi/
-800BCF,
STC ST01566LA)

14-01A C 2 1 (O) One loop (A or B) may be

inoperative in Combi or Cargo mode.

14-01B C 2 0 May be inoperative in Passenger

mode.

14-02 Fire Detection

(-400C ST000235BO,
-400 Combi
ST00248BO)

14-02-01 Cargo Fire Flight Deck C 1 0 May be inoperative provided Main

Unit (CFFU) Deck Cargo Compartment Fire
Detection System is considered
inoperative.

14-02-01-01 FAULT Legend C 1 0 (M) May be inoperative provided

system integrity is confirmed by
self-test at Cargo Fire Maintenance
Unit (CFMU).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-02 Fire Detection

(-400C ST000235BO,
-400 Combi
ST00248BO)
(Cont’d)

14-02-01 Cargo Fire Flight Deck

Unit (CFFU)
(Cont’d)

14-02-01-02 Legend Back-lighting C 2 0 (O) May be inoperative provided:

(CARGO FIRE MAIN a) CFFU test is acceptable,
DECK and TEST) b) Operations are not dependent
on its use, and
c) Sufficient cockpit lighting is
available for normal
operations.

14-02-01-03 FIRE Legend C 1 0 May be inoperative provided master

FIRE WARN lights and master fire
warning bell are checked to operate
normally before each departure.

14-02-01-04 System Self-Test C 1 0 May be inoperative provided master

FIRE WARN lights and master fire
warning bell are checked to operate
normally before each departure.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-02 Fire Detection

(-400C ST000235BO,
-400 Combi
ST00248BO)
(Cont’d)

14-02-02 Cargo Fire Maintenance C 1 0 May be inoperative provided Main

Unit (CFMU) Deck Cargo Compartment Fire
Detection System is considered
inoperative.

14-02-02-01 CFMU Indicator Lights C 20 0 (M) Individual lights may be

inoperative provided:
a) Each corresponding location
is independently verified by
CFFU, and
b) Self-test is accomplished.

NOTE: Dual loop coverage is

maintained with loss of one
CFMU loop “A” or “B”
subassembly failure.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-03 Fire Suppression System C 1 0 May be inoperative in Passenger

(-700C/-700 Combi/ mode.
-800BCF,
STC ST01566LA)

14-03-01 DEPR Light

14-03-01A C 1 0 May be inoperative in Passenger

mode.

14-03-01B C 1 0 May be inoperative in Combi or

Cargo mode provided MAIN SYS
light illuminates during system test.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-03 Fire Suppression System

(-700C/-700 Combi/
-800BCF,
STC ST01566LA)
(Cont’d)

14-03-02 MAIN SYS Light

14-03-02A C 1 0 May be inoperative in Passenger

mode.

14-03-02B C 1 0 (M) May be inoperative in Combi or

Cargo mode provided:
a) Failure is verified to be in light
circuit, and
b) System circuit is verified to
operate normally once each
flight-day.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors C - 0 May be inoperative provided Main

(737C/QC/-700C/-700 Deck Cargo Compartment Fire
Combi/-800BCF, STCs Detection System is considered
ST01566LA, inoperative.
ST00235BO,
SA2970SO, -400 Combi NOTE: Refer to MMEL Item 26-14-01 |
ST00248BO, (Fire Detection -700C, -700 |
ST01827LA, Combi/-800BCF, |
ST01961SE, and STC ST01566LA). |
ST02556SE)

14-04-01 (STC ST01566LA Only) C 12 6 May be inoperative provided all

detectors in opposite loop operate
normally.

14-04-02 System Test Feature C 1 0 (M) May be inoperative provided an

(737C/QC/-700 Combi/ acceptable method is used to verify
-800BCF, and detector system integrity.
STC ST01566LA)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-03 System Power (Blue) C 1 0 (M) May be inoperative provided

Light smoke detectors operate normally.
(PEMCO Aeroplex, Inc.)
(-300QC, -300F,
STC SA2970SO)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-04 (STC ST00235BO Only)

14-04-04-01 Smoke Detector Units C 10 - (O) Detector(s) may be inoperative

provided no cargo is carried in
affected zone.

14-04-04-02 Smoke Detector Loops C 20 10 One loop in any detector may be

inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-05 (STC ST00248BO Only)

14-04-05-01 Smoke Detector Units C 4 0 May be inoperative provided Main

Deck Cargo Compartment Fire
Detection System is considered
inoperative.

14-04-05-02 Smoke Detector Loops C 8 4 One loop in any detector may be

inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-06 (STC ST01827LA Only)

14-04-06-01 -300 C 12 10 Two detectors may be inoperative

provided:
a) Inoperative detectors are not
in adjacent locations, and
b) Detector #1, most forward
detector, operates normally.

14-04-06-02 -400 C 12 10 (M) Two detectors may be

inoperative provided they are not in
adjacent locations.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-07 (STC ST01961SE Only)

14-04-07-01 Smoke Detectors C 20 19 (O) One detector (bus A or B) may be

inoperative provided remaining
detectors are verified to operate
normally before each departure.

14-04-07-02 DET FAULT Light C 1 0 (M) May be inoperative provided:

a) All CCP smoke detector lights
operate normally, and
b) System integrity is verified to
operate normally before each
departure.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-07 (STC ST01961SE Only)

(Cont’d)

14-04-07-03 CCP Smoke Detector C 20 0 (M) May be inoperative provided:

Lights a) DET FAULT Light operates
normally, and
b) System integrity is verified to
operate normally before each
departure.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-07 (STC ST01961SE Only)

(Cont’d)

14-04-07-04 CARGO Light C 1 0 (M) May be inoperative provided:

a) DEPRESS Light operates
normally,
b) All Class E shutoff valves are
verified to be closed after
pressing the DEPRESS
switch, and
c) The forward outflow valve is
verified to be open after
pressing the DEPRESS
switch.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-20
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

14 Main Deck Cargo

*** Compartment Fire
Detection/Suppression
Systems
(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA, -400C
ST00235BO, -400
Combi ST00248BO,
SA2970SO, ST01827LA,
ST00283AT,
ST01961SE, and
ST02556SE)
(Cont'd)

14-04 Smoke Detectors

(737C/QC/-700C/-700
Combi/-800BCF, STCs
ST01566LA,
ST00235BO,
SA2970SO, -400 Combi
ST00248BO,
ST01827LA,
ST01961SE, and
ST02556SE)
(Cont’d)

14-04-07 (STC ST01961SE Only)

(Cont’d)

14-04-07-05 DEPRESS Light C 1 0 (M) May be inoperative provided:

a) All Class E shutoff valves are
verified to be closed after
pressing the DEPRESS
switch, and
b) The forward outflow valve is
verified to be open after
pressing the DEPRESS
switch.

14-04-08 Smoke Detectors C 20 10 (O) One or more detector of the same

(STC ST02556SE) loop (A or B) may be inoperative
provided all detectors of the opposite
loop are verified to operate normally
before each departure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-21
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

15 Lavatory Fire
Extinguisher Systems

15-01 Passenger Configuration

15-01A C - 0 For each lavatory, lavatory fire

extinguisher system may be
inoperative provided associated
lavatory smoke detection system
operates normally.

15-01B C - 0 (M)(O) For each lavatory, lavatory fire

extinguisher system may be
inoperative provided:
a) Lavatory waste receptacle is
empty,
b) Associated lavatory door is
locked closed and placarded:
“INOPERATIVE -
DO NOT ENTER”, and
c) Lavatory is used only by
crewmembers.

NOTE: These provisions are not

intended to prohibit lavatory
use or inspection by
crewmembers.

15-02 Cargo Configuration D - 0

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-22
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

16 Lavatory Smoke
Detection System

16-01 Passenger Configuration C - 0 (M)(O) For each lavatory, lavatory

smoke detection system may be
inoperative provided:
a) Lavatory waste receptacle is
empty,
b) Associated lavatory door is
locked closed and placarded:
“INOPERATIVE -
DO NOT ENTER”, and
c) Lavatory is used only by
crewmembers.

NOTE: These provisions are not

intended to prohibit lavatory
use or inspection by
crewmembers.

16-02 Cargo Configuration D - 0

16-03 Lavatory Smoke C - 0 (M) May be inoperative provided

*** Detector SELF TEST associated lavatory smoke detector is
Switch verified to operate normally.

16-04 Lavatory Smoke C - 0 (M) May be inoperative provided

*** Detector TEST Switch each lavatory smoke detector is
on Flight Attendant’s verified to operate normally.
Panel
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-23
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

17 Engine Fire Extinguisher

*** Thermal/Discharge Discs
(-100/-200)

17-01 Discharge (Yellow) Discs C 2 0 (M) May be missing provided

indicator readings or other acceptable
means are used to verify adequate
charge.

17-02 Thermal (Red) Discs C 2 0 (M) May be missing provided

indicator readings or other acceptable
means are used to verify adequate
charge.

18 Wing-Body Overheat
Test System

18-01 Flight Deck Test Feature C 1 0 (M) May be inoperative provided

system integrity is verified by an
acceptable procedure once each
flight-day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-24
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

19 Lower Cargo C - 0 (O) May be inoperative provided

*** Compartment Fire procedures are established and used
Detection/Suppression to ensure associated compartment
Systems remains empty or is verified to
(All models and STCs) contain only empty cargo handling
equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away
Kits.

NOTE 1: Operator MELs must define

which items are approved
for inclusion in Fly Away
Kits and which materials
can be used as ballast.

NOTE 2: Class E cargo

compartments require only
installation of smoke or fire
detection systems
(not suppression).

19-01 Fwd/Aft Detection Loops

19-01-01 Boeing installed system, C 4 2 (O) One loop (A or B) in each

*** STC ST00749LA-D, compartment may be inoperative
ST00763LA-D, provided opposite loop is checked to
ST01184LA, operate normally.
ST01674AT,
ST01424LA, ST10153T,
ST01804LA,
ST01114WI Only

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-25
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

19 Lower Cargo
*** Compartment Fire
Detection/Suppression
Systems
(All models and STCs)
(Cont’d)

19-01 Fwd/Aft Detection Loops

(Cont’d)

19-01-02 STC ST00405LA-D Only C - 2 (O) May be inoperative provided

*** one loop in each compartment is
checked to operate normally.

19-02 Extinguisher Bottles

***

19-02-01 No. 1 C 1 0 (O) May be inoperative provided

*** (STC ST01424LA, associated cargo compartment
ST01457LA, and remains empty.
ST01804LA Only)

19-02-02 No. 2 C 1 0 (M)(O) Except for ER operations,

*** (Boeing installed system may be inoperative with cargo carried
and STC ST01184LA in compartment.
Only)

19-02-03 No. 2 C 1 0 (M)(O) May be inoperative provided

*** (STC ST01424LA associated cargo compartment
ST01457LA, and remains empty.
ST01804LA Only)

19-02-04 No. LRD2 C 1 0 (O) Except for ER operations, may be

*** (STC ST00405LA-D inoperative with cargo carried in
Only) compartment.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-26
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

19 Lower Cargo
*** Compartment Fire
Detection/Suppression
Systems
(All models and STCs)
(Cont’d)

19-03 Squib Lights C 2 0 (O) May be inoperative provided

*** (STC ST01424LA, and associated cargo compartment
ST01457LA Only) remains empty.

19-04 DISCH Light(s)

***

19-04-01 Boeing installed system, C 1 0 (M) May be inoperative provided

*** STC ST01184LA and associated extinguisher bottle(s) is
ST00405LA-D Only verified to have an adequate charge
once each flight-day.

19-04-02 STC ST01424LA, C 2 0 May be inoperative provided

*** ST01457LA, and associated compartment remains
ST01804LA Only empty.

19-05 Extinguisher Bottle C - 0 (M) May be inoperative provided

*** Pressure Switch associated extinguisher bottle(s) is
(Boeing installed system verified to have an adequate charge
only) once each flight-day.

19-06 EXT Lights C 2 0 (M) May be inoperative provided:

*** (FWD and AFT) a) Failure is verified to be in
(Boeing installed system, squib light circuit, and
STC ST01184LA and b) Squib circuit is verified to
ST00405LA-D Only) operate normally once each
flight-day.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-27
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

19 Lower Cargo
*** Compartment Fire
Detection/Suppression
Systems
(All models and STCs)
(Cont’d)

19-07 Fault(s) Indicated by B - - Dispatch with MX indicator

*** Illumination of MX illuminated is permitted provided
Indicator green SYS OK indicator remains
(STC ST00511LA, illuminated.
ST00404LA-D,
ST00740LA-D, NOTE: This is a fault tolerant system
ST00745LA-D, and unit will continue to
ST00751LA-D, and perform its intended function
ST00990LA-D Only) as long as green SYS OK
indicator remains illuminated.

19-07-01 Display of FWD INOP B - - (O) May be displayed provided green

and/or AFT INOP SYS OK indicator remains illuminated
Message(s) and indicated cargo bay remains
empty.

19-07-02 Smoke Detector(s) C - - (O) One smoke detector may be

inoperative in each compartment
provided SYS OK indicator on CDU
remains illuminated.

NOTE: MX indicator on CDU will

remain illuminated.

19-08 Control Panel ALARM C 1 0 (O) May be inoperative provided Fire

*** OFF Switch Bell cutout switch silences Cargo Bay
(STC ST00749LA-D and Fire Protection Fire Warning Bell.
ST00763LA-D Only)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-28
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

19 Lower Cargo
*** Compartment Fire
Detection/Suppression
Systems
(All models and STCs)
(Cont’d)

19-09 DET Lights C 4 2 (O) One light in each compartment

*** (STC ST01674AT, and may be inoperative provided
ST01114WI Only) remaining loop in associated
compartment is checked to operate
normally before each departure.

19-10 FAIL Lights C 4 2 (O) One light in each compartment

*** (STC ST01674AT, and may be inoperative provided
ST01114WI Only) remaining loop in associated
compartment is checked to operate
normally before each departure.

19-11 Smoke Detectors

***

19-11-01 STC ST01674AT, and C - - (M) One detector in each detector

*** ST01114WI Only enclosure may be inoperative
provided remaining detector in
associated detector enclosure is
verified to operate normally before
each departure.

19-11-02 STC ST01424LA, and C 12 6 (M) May be inoperative provided

*** ST01804LA (-300) Only 2 FWD and 4 AFT in same loop are
functional.

19-11-03 STC ST01457LA, and C 14 7 (M) May be inoperative provided

*** ST01804LA (-400) Only 3 FWD and 4 AFT in same loop are
functional.

19-11-04 STC ST01804LA (-200) C 10 5 (M) May be inoperative provided

*** 2 FWD and 3 AFT in same loop are
functional.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-29
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

19 Lower Cargo
*** Compartment Fire
Detection/Suppression
Systems
(All models and STCs)
(Cont’d)

19-12 Fault Panel D 1 0

*** (E and E Compartment,
STCs ST01674AT, and
ST01114WI Only)

19-13 DETECTOR FAULT C 1 0 (O) May be inoperative provided the

*** Light cargo fire TEST switch is used to
(Boeing Installed System check for faults in the cargo fire
Only) detection and suppression system
before each flight.
|
21 Cabin Configuration Test C 2 0 (M) May be inoperative provided:
Panel CARGO/ a) EE Bay Mode Selector Switch
PASSENGER Lights is verified to be in appropriate
(-700C and -700 Combi) position for intended airplane
configuration before each
departure, and
b) Passenger Oxygen Shutoff
Valve is verified to be in
appropriate position for
intended airplane
configuration before each
departure.

22 Galley Fire Detection C 1 0 (M) May be inoperative provided

*** System procedures are established and used
(Jet Aviation Engineering to deactivate cooktop.
Services (JAES))
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-30
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

23 Galley Vent Fire C 1 0 (M) May be inoperative provided

*** Extinguisher System procedures are established and used
(STC ST09977) to deactivate cooktop and vent fan.

24 Smoke Detectors
*** (Jet Aviation Engineering
Services (JAES))

24-01 Equipment Cabinets C - 0 (M) May be inoperative provided all

equipment in cabinet is deactivated
off.

24-02 Cabin Compartments C - 0 (O) May be inoperative provided

associated cabin compartment
remains open and is continuously
monitored.

25 Engine Start Lever Fire A 2 0 (O) May be inoperative provided:

*** Indication Lights a) Engine No. 1 and Engine
No. 2 fire handle switch lights
function normally prior to
engine start for each flight,
and
b) Repairs are made within
3 flight-days.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 26-31
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
26. Fire Protection
Change
Sequence No. Item 1 2 3 4 Bar

26 Supernumerary and
*** Lavatory Compartment
Fire Detection/
Suppression Systems
(STC ST02556SE)

26A C 1 0 (O) May be inoperative provided the

supernumerary compartment is
occupied during all phases of the
flight.

26B C 1 0 (O) May be inoperative while the

supernumerary compartment is
not occupied provided the flight deck
door and the lavatory door remain
opened and secured during all
phases of the flight.

26-01 Supernumerary C 1 0 (O) May be inoperative while the

Compartment Smoke supernumerary compartment is
Detector not occupied provided the flight deck
door remains opened and secured
during all phases of the flight.

26-02 Lavatory Smoke C 1 0 (O) May be inoperative while the

Detector supernumerary compartment is
not occupied provided the flight deck
door and the lavatory door remain
opened and secured during all
phases of the flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

01 Stabilizer Main Electrical C 1 0

Trim Operating Light
(-100/-200)
|
03 Wing Trailing Edge Flap
Position Indication
System

03-01 Mechanical Asymmetry C 1 1 (O) Left Flap position indication may

Protection be inoperative provided proper flap
(-100/-200) operation is verified prior to each
takeoff.

04 Leading Edge Flap/Slat

Position Light Systems

04-01 (-300,-400,-500)

04-01A C 1 0 Aft overhead LE DEVICES

Annunciator panel may be
inoperative provided forward panel
lights operate normally.

04-01B C 1 0 (M) Forward panel lights may be

inoperative provided:
a) LE DEVICES Annunciator
panel operates normally and
is used to verify proper LE |
DEVICE position, |
b) Stall warning operation of
both systems is verified to
operate normally, and
c) A placard is installed to
indicate proper positions for
flap configuration in use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

04 Leading Edge Flap/Slat

Position Light Systems
(Cont’d)

04-01 (-300,-400,-500)
(Cont’d)

04-01-01 Leading Edge Slat C 6 5 (M)(O) Indication lights on forward

Indications panel, and in addition, indication
(-300/-500) lights for one leading edge slat on
overhead annunciator panel may be
inoperative provided:
a) Normal operation is verified
by flightcrew before each
takeoff and landing,
b) Maximum speed is limited to
300 KIAS at/below FL 200 or
.65 Mach above FL 200,
c) All remaining indications on
overhead annunciator panel
operate normally, and
d) Stall warning operation of
both systems is verified to
operate normally.

04-01-02 Leading Edge Slat C 6 5 (M)(O) Indication lights on forward

Indications panel, and in addition, indication
(-400) lights for one leading edge slat,
except for slats 3 and 4, on overhead
annunciator panel may be inoperative
provided:
a) Normal operation is verified
by flightcrew before each
takeoff and landing,
b) Maximum speed is limited to
300 KIAS at/below FL 200 or
.65 Mach above FL 200,
c) All remaining indications on
overhead annunciator panel
operate normally, and
d) Stall warning operation of
both systems is verified to
operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

04 Leading Edge Flap/Slat

Position Light Systems
(Cont’d)

04-02 (-100, -200, -600, -700,

-800, -900, -900ER)

04-02A C 1 0 Aft overhead LE DEVICES

Annunciator panel may be
inoperative provided forward panel
lights operate normally.

04-02B C 1 0 (M) Forward panel lights may be

inoperative provided:
a) Aft overhead LE DEVICES
Annunciator panel operates
normally and is used to verify
proper LE DEVICE position, |
and
b) A placard is installed to
indicate proper position for
flap configuration in use.

04-02-01 Leading Edge Slat C 6 5 (M)(O) Indication lights on forward

Indications panel, and in addition, indication
(-100/-200) lights for one leading edge slat on
overhead annunciator panel may be
inoperative provided:
a) Normal operation is verified
by flightcrew before each
takeoff and landing,
b) Maximum speed is limited to
300 KIAS at/below FL 200
or.65 Mach above FL 200,
and
c) All remaining indications on
overhead annunciator panel
operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

04 Leading Edge Flap/Slat

Position Light Systems
(Cont’d)

04-02 (-100, -200, -600, -700,

-800, -900, -900ER)
(Cont’d)

04-02-02 Leading Edge Slat C 8 7 (M)(O) Indication lights on forward

Indications panel, and in addition, indication
(-600/-700) lights for one leading edge slat,
except for slats 4 and 5, on overhead
annunciator panel may be inoperative
provided:
a) Normal operation is verified
by flightcrew before each
takeoff and landing,
b) Maximum speed is limited to
300 KIAS at/below FL 200 or
.65 Mach above FL 200,
c) All remaining indications on
overhead annunciator panel
operate normally, and
d) Stall warning operation of
both systems is verified to
operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

04 Leading Edge Flap/Slat

Position Light Systems
(Cont’d)

04-02 (-100, -200, -600, -700,

-800, -900, -900ER)
(Cont’d)

04-02-03 Leading Edge Slat C 8 7 (M)(O) Indication lights on forward

Indications panel, and in addition, indication
(-800) lights for one leading edge slat,
except for slats 3, 4, 5, and 6, on
overhead annunciator panel may be
inoperative provided:
a) Normal operation is verified
by flightcrew before each
takeoff and landing,
b) Maximum speed is limited to
300 KIAS at/below FL 200 or
.65 Mach above FL 200,
c) All remaining indications on
overhead annunciator panel
operate normally, and
d) Stall warning operation of
both systems is verified to
operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

04 Leading Edge Flap/Slat

Position Light Systems
(Cont’d)

04-02 (-100, -200, -600, -700,

-800, -900, -900ER)
(Cont’d)

04-02-04 Leading Edge Slat C 8 7 (M)(O) Indication lights on forward

Indications panel, and in addition, indication
(-900/-900ER) lights for one leading edge slat,
except for slats 2, 3, 4, 5, 6, and 7, on
overhead annunciator panel maybe
inoperative provided:
a) Normal operation is verified
by flightcrew before each
takeoff and landing,
b) Maximum speed is limited to
300 KIAS at/below FL 200 or
.65 Mach above FL 200,
c) All remaining indications on
overhead annunciator panel
operate normally, and
d) Stall warning operation of
both systems is verified to
operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

05 Flight Control Low C 2 0 May be inoperative provided warning

Pressure Lights lights, hydraulic pressure, and quality
(A and B) indicators operate normally.
Systems
(-100/-200)
|
07 Auto Speed Brake
*** System

07-01 All Models Except -800 C 1 0 (M)(O) May be inoperative provided:

with Short Field a) System is deactivated,
Performance (SFP) b) Operations are conducted in
Option and -900ER accordance with AFM, and
c) For models with Blended
Winglet or Split Scimitar
Winglet with Speed Brake
Load Alleviation System,
Speed Brake Load Alleviation
System is considered
inoperative.

NOTE: Refer to MMEL Item 27-20 |

(Speedbrake Load Alleviation |
System) |

07-02 -800SFP C 1 0 (M)(O) May be inoperative provided:

a) System is deactivated, and
b) Appropriate performance
adjustments are applied.

07-03 -900ER C 1 0 (M)(O) May be inoperative provided:

a) System is deactivated,
b) Appropriate performance
adjustments are applied, and
c) Load Alleviation System is
considered inoperative.

NOTE: Refer to MMEL Item 27-20 |

(Speedbrake Load Alleviation |
System) |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

08 Flap Load Limiter

System

08-01 -100/-200 C 1 0 (M) May be inoperative provided:

*** a) Flaps are verified to operate
normally throughout their full
range before each departure,
and
b) Flaps are not extended
beyond Flaps 30 at gross
weights above 98,000 lbs. |
(44,453 kg).

08-02 -300/-400/-500 C 1 0 May be inoperative provided flaps are

not extended beyond Flaps 30.

08-03 -600 C 1 0 May be inoperative provided:

a) Flaps are not extended
beyond Flaps 30 at gross
weights above 93,830 lbs. |
(42,560 kg), and
b) Flaps are not extended
beyond Flaps 15 at gross
weights above 105,040 lbs. |
(47,645 kg).

08-04 -700 C 1 0 May be inoperative provided:

a) Flaps are not extended
beyond Flaps 30 at gross
weights above 93,480 lbs. |
(42,401 kg), and
b) Flaps are not extended
beyond Flaps 15 at gross
weights above 104,403 lbs. |
(47,356 kg).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

08 Flap Load Limiter

System
(Cont’d)

08-05 -800 without Short Field C 1 0 May be inoperative provided:

Performance (SFP) a) Flaps are not extended
Option beyond Flaps 30 at gross
weights above 93,995 lbs. |
(42,635 kg), and
b) Flaps are not extended
beyond Flaps 15 at gross
weights above 104,875 lbs. |
(47,570 kg).

08-06 -800 with Short Field C 1 0 May be inoperative provided:

Performance (SFP) a) Flaps are not extended
Option beyond Flaps 30 at gross
weights above 95,800 lbs. |
(43,454 kg),
b) Flaps are not extended
beyond Flaps 15 at gross
weights above 105,000 lbs. |
(47,627 kg), and
c) Flaps are not extended
beyond Flaps 10 at gross
weights above 135,800 lbs. |
(61,597 kg).

08-07 -900 C 1 0 May be inoperative provided:

a) Flaps are not extended
beyond Flaps 30 at gross
weights above 94,760 lbs. |
(42,982 kg), and
b) Flaps are not extended
beyond Flaps 15 at gross
weights above 105,130 lbs. |
(47,686 kg).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

08 Flap Load Limiter

System
(Cont’d)

08-08 -900ER C 1 0 May be inoperative provided:

a) Flaps are not extended
beyond Flaps 30 at landing
gross weights above
105,800 lbs. (47,990 kg),
b) Flaps are not extended
beyond Flaps 15 at landing
gross weighs above
113,400 lbs. (51,437 kg), |
c) Flaps are not extended
beyond Flaps 10 at landing
gross weights above
135,600 lbs. (61,507 kg), |
d) Flaps are not extended
beyond Flaps 15 at takeoff
gross weights above
155,600 lbs. (70,578 kg), and |
e) Flaps are not extended
beyond Flaps 5 at takeoff
gross weights above
176,000 lbs. (79,832 kg). |
|
10 FEEL DIFF PRESS Light B 1 0 (M) May be inoperative provided
System Elevator feel system is verified to
operate normally once each
flight-day.

11 Auto Slat Fail Light C 1 0 (M) May be inoperative provided:

System a) Auto slat systems are verified
(-300/-400/-500/-600/ to operate normally, and
-700/-800/-900/-900ER) b) Verification is repeated every
2 flight-days.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

12 Auto Slat Systems C 2 1 (O) One system may be inoperative

(-300/-400/-500.-600/ provided:
-700/-800/-900/-900ER) a) Remaining auto slat system is
checked to operate normally,
and
b) Auto Slat fail light operates
normally.
|
14 Rudder Trim Indicator

14-01 (-600/-700/-800/-900/ C 1 0 (O) May be inoperative provided:

-900ER) a) Control Surface Position
Indication System is installed
and operates normally,
b) Rudder trim actuator is
checked to operate normally,
and
c) Rudder trim is checked to be
centered before each
departure.

14-02 (All Models, Upon C 1 0 (O) May be inoperative provided:

Incorporation of Boeing a) Rudder trim actuator is
Service Bulletin checked to operate normally,
737-27-1252, and
737-27-1253, or b) Rudder trim is checked
737-27-1255, or centered before each
Production Equivalent) departure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

15 Mechanical Flaps C 1 0
*** Position 30 Stop
(-100/-200 Modified by
STC ST00131SE)

16 SPEED BRAKE/
SPEEDBRAKES
EXTENDED Light

16-01 (-300/-400/-500) D 1 0
***

16-02 (-600/-700/-800/-900/ C 1 0 (M) May be inoperative provided

-900ER) speedbrakes are verified to operate
normally.

17 Wheel to Rudder C 1 0
Interconnect System
(WTRIS)
(-600/-700/-800/-900/
-900ER)

18 Control Surface Position C 1 0

*** Indicating System

19 Rudder Pressure C 1 0 (M)(O) May be inoperative provided:

Reducer (RPR) System a) RPR system is deactivated,
(-100/-200/-300/-400/ and
-500) b) RPR valve is verified to
provide high pressure output.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

20 Speedbrake Load
*** Alleviation System

20-01 -700/-800 with Blended

Winglet or Split Scimitar
Winglet
STC ST00830SE

20-01-01 -700

20-01-01A C 1 0 (M)(O) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to full
up position,
b) Airspeed does not exceed
265 KIAS when in-flight gross
weight is in excess of
143,000 lbs. (64,863 kg), |
c) Severe turbulent air
penetration speed is
265 KIAS or 0.76 Mach,
whichever is lower, when
in-flight gross weight is in
excess of 143,000 lbs. |
(64,863 kg), and
d) Automatic Speedbrake
System is considered
inoperative.

NOTE: Refer to MMEL Item 27-07 |

(Auto Speed Brake System) |

20-01-01B C 1 0 (M) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to full
up position, and
b) Takeoff weight does not
exceed 143,500 lbs. |
(65,090 kg).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

20 Speedbrake Load
*** Alleviation System
(Cont’d)

20-01 -700/-800 with Blended

Winglet or Split Scimitar
Winglet
STC ST00830SE
(Cont’d)

20-01-02 -800

20-01-02A C 1 0 (M)(O) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to full
up position,
b) Airspeed does not exceed
265 KIAS when in-flight gross
weight is in excess of
155,000 lbs. (70,306 kg), |
c) Severe turbulent air
penetration speed is
265 KIAS or 0.76 Mach,
whichever is lower, when
in-flight gross weight is in
excess of 155,000 lbs. |
(70,306 kg), and
d) Automatic Speedbrake
System is considered
inoperative.

NOTE: Refer to MMEL Item 27-07 |

(Auto Speed Brake System). |

20-01-02B C 1 0 (M) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to full
up position, and
b) Takeoff weight does not
exceed 155,500 lbs. |
(70,533 kg).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

20 Speedbrake Load
*** Alleviation System
(Cont’d)

20-02 -300/-500 with Blended

Winglet
STC ST01219SE

20-02A C 1 0 (M) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to the
full up position,
b) Airspeed does not exceed
265 KIAS when in-flight gross
weight is in excess of
125,000 lbs. (56,699 kg), and |
c) Severe turbulent air
penetration speed is
265 KIAS or 0.73 Mach,
whichever is lower, when
in-flight gross weight is in
excess of 125,000 lbs. |
(56,699 kg).

20-02B C 1 0 (M) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to full
up position, and
b) Takeoff weight does not
exceed 126,500 lbs. |
(57,380 kg).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

20 Speedbrake Load
*** Alleviation System
(Cont’d)

20-03 -900ER with Blended

Winglet or Split Scimitar
Winglet

20-03A C 1 0 (M)(O) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to full
up position,
b) Airspeed does not exceed
265 KIAS when in-flight gross
weight is in excess of
170,000 lbs. (77,110 kg), |
c) Severe turbulent air
penetration speed is
265 KIAS or 0.76 Mach,
whichever is lower, when
in-flight gross weight is in
excess of 170,000 lbs. |
(77,110 kg), and
d) Automatic Speedbrake
System is considered
inoperative.

NOTE: Refer to MMEL Item 27-07 |

(Auto Speed Brake System) |

20-03B C 1 0 (M) May be inoperative provided:

a) Speedbrake handle forces are
normal from full down to full
up position, and
b) Takeoff weight does not
exceed 170,500 lbs. |
(77,337 kg).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 27-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
27. Flight Controls
Change
Sequence No. Item 1 2 3 4 Bar

21 STBY RUD ON light C 1 0 (M)(O) May inoperative provided:

*** (Boeing Service Bulletin a) Rudder is verified to operate
737-27A-1279, normally on hydraulic systems
737-27-1252R3, A and B independently,
737-27-1253R3, b) Standby hydraulic pump is
737-27-1255R3, or verified to operate normally,
Production Equivalent and
Incorporated) c) Rudder force fight monitor is
deactivated.

22 Quiet Wing Flaps 1*

*** System
(STC ST01535SE Only)

22-01 -200 C 1 0 May be inoperative provided:

a) Flaps 1* control switch is
positioned in UP position,
b) System is deactivated by
pulling and collaring circuit
breaker MS3320-3,
c) Appendix QWS001 “Flaps 1*
High Altitude Kit” is not used,
and
d) All other aspects of QWS
supplement are followed.

NOTE: C/b MS3320-3 is located on

P6-2 panel.

23 Elevator Tab Control A 8 6 (M) One may be broken or missing |

Springs per elevator provided: |
(-600/-700/-800/ a) Broken spring is removed,
-900/-900ER) and
b) Repairs are made within
10 flight-days.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

01 Fuel Boost Pumps

(Main Tanks)

01-01 (-100/-200/-300/
-400/-500)
(All pumps except
Plessey 8240 MK I and
MK II)

01-01-01 Aft Pumps C 2 1 (M)(O) One may be inoperative

provided:
a) Both main tank forward
pumps operate normally,
b) At start of takeoff, fuel
quantity in associated tank is
not less than 7,500 lbs. |
(3,402 kg),
c) A minimum fuel quantity of
2,500 lbs. (1,134 kg) is |
maintained in associated tank,
and
d) Boost pump is deactivated.

01-01-02 Forward Pumps C 2 1 (M)(O) One may be inoperative

provided:
a) Both main tank aft pumps
operate normally,
b) At start of takeoff, fuel
quantity in associated tank is
not less than 4,800 lbs. |
(2,177 kg),
c) A minimum fuel quantity of
1,800 lbs. (817 kg), and |
d) Boost pump is deactivated.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

01 Fuel Boost Pumps

(Main Tanks)
(Cont’d)

01-02 (-100/-200/-300)
(Plessey 8240 MK I and
MK II)

01-02-01 Aft Pumps C 2 1 (M)(O) Except for ER operations, one

may be inoperative provided:
a) Both main tank forward
pumps operate normally,
b) At start of takeoff, fuel
quantity in associated tank is
not less than 7,500 lbs. |
(3,402 kg),
c) A minimum fuel quantity of
2,500 lbs. (1,134 kg) is |
maintained in associated tank,
and
d) Boost pump is deactivated.

01-02-02 Forward Pumps C 2 1 (M)(O) Except for ER operations, one

may be inoperative provided:
a) Both main tank aft pumps
operate normally,
b) At start of takeoff, fuel
quantity in associated tank is
not less than 4,800 lbs. |
(2,177 kg),
c) A minimum fuel quantity of
1,800 lbs. (817 kg) is |
maintained in associated tank,
and
d) Boost pump is deactivated.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

01 Fuel Boost Pumps

(Main Tanks)
(Cont’d)

01-03 (-600/-700/-800/
-900/-900ER)

01-03-01 Aft Pumps C 2 1 (M)(O) Except for ER operations

beyond 120 minutes, one may be
inoperative provided:
a) Both main tank forward
pumps operate normally,
b) At start of takeoff, fuel
quantity in associated tank is
not less than 7,500 lbs. |
(3,402 kg),
c) A minimum fuel quantity of
2,500 lbs. (1,134 kg) is |
maintained in associated tank,
and
d) Boost pump is deactivated.

01-03-02 Forward Pumps C 2 1 (M)(O) Except for ER operations

beyond 120 minutes, one may be
inoperative provided:
a) Both main tank aft pumps
operate normally,
b) At start of takeoff, fuel
quantity in associated tank is
not less than 4,800 lbs. |
(2,177 kg),
c) A minimum fuel quantity of
1,800 lbs. (817 kg) is |
maintained in associated tank,
and
d) Boost pump is deactivated.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

02 Fuel Boost Pumps

(Center Tank)

02A C 2 1 (M) May be inoperative provided:

a) Tank remains empty, and
b) Boost pump is deactivated.

02B C 2 1 (M)(O) May be inoperative with

center tank fueled provided:
a) Fuel quantity remaining in
main wing tanks is adequate
to reach a suitable airport if
remaining center pump fails at
any time,
b) Zero fuel weight calculations
are adjusted by weight of
center tank fuel,
c) Effect on airplane balance, in
event fuel cannot be used, is
accounted for,
d) LOW PRESSURE light of
operating center fuel tank
pump operates normally,
e) Center tank quantity indication
operates normally, and
f) Boost pump is deactivated.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

02 Fuel Boost Pumps

(Center Tank)
(Cont’d)

02C C 2 0 (M) May be inoperative provided:

a) Center tank quantity indication
operates normally,
b) Center tank remains empty or
zero fuel weight calculations
are adjusted by weight of
center tank fuel, and
c) Boost pump is deactivated.

NOTE: AFM fuel loading and usage |

limitations are for usable fuel. |

02-01 Universal Fault C 2 0 May be inoperative provided

Interrupter (UFI) associated center tank boost pump is
(STC ST01844LA, -300, considered inoperative.
ST02076LA,
-600/-700/-800/-900) NOTE: Refer to MMEL Item 28-02 |
(Fuel Boost Pumps (Center |
Tank)). |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

03 Fuel Boost Pump Low

Pressure Warning Light
Systems

03-01 Main Tank Pump Low C 4 3 (M)(O) May be inoperative provided:

Pressure Warning Light a) Associated fuel pump is not
Systems used, and
b) MASTER CAUTION lights
and FUEL system annunciator
light are verified to operate
normally.
03-01-01 Main Tank Pump Lights

03-01-01A C 4 3 May be inoperative provided:

a) Both pumps in associated
tank operate normally, and
b) Associated tank quantity
indicator operates normally.

03-01-01B C 4 3 May be inoperative for an associated

inoperative pump.

03-02 Center Tank Pump Low

Pressure Warning Light
Systems

03-02A C 2 1 (M)(O) May be inoperative provided:

a) Associated fuel pump is not
used, and
b) MASTER CAUTION lights
and FUEL system annunciator
light are verified to operate
normally.

03-02B C 2 0 May be inoperative provided:

a) Center tank fuel is not
required for flight,
b) Center tank fuel boost pumps
are turned off, and
c) Center tank remains empty or
zero fuel weight calculations
are adjusted by weight of
center tank fuel.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

03 Fuel Boost Pump Low

Pressure Warning Light
Systems
(Cont’d)

03-02 Center Tank Pump Low

Pressure Warning Light
Systems
(Cont’d)

03-02-01 Center Tank Pump C 2 0 (M)(O) May be inoperative provided:

Lights a) Center Tank Fuel Quantity
Indicator operates normally,
and
b) MASTER CAUTION lights
and FUEL system annunciator
light are verified to operate
normally.

04 APU Fuel Valve C 1 0 (M)(O) Except for ER operations,

may be inoperative provided:
a) APU is not used, and
b) Valve is deactivated closed.

05 Crossfeed VALVE OPEN C 1 0 (M) Except for ER operations, may be

Light inoperative provided:
a) Crossfeed valve is verified to
operate normally,
b) Fuel quantity indication for
both main tanks operates
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

06 Flight Deck Fuel C 2 1 (M)(O) Except for ER operations, one

Quantity Indicators may be inoperative provided:
(Main Tanks) a) All boost pumps in associated
tank operate normally,
b) Fuel flow meters operate
normally,
c) Center tank indicator operates
normally,
d) Flightcrew periodically
computes fuel remaining, or
checks fuel remaining against
a precomputed fuel burn
chart, and
e) Fuel quantity in associated
main tank is verified by an
acceptable procedure.
07 Flight Deck Fuel
Quantity Indicator
(Center Tank)

07-01 (-100 and -600/-700/ C 1 0 May be inoperative provided:

-800/-900/-900ER) a) One center tank boost pump
operates normally, and
b) Center tank remains empty.

07-02 (-200/-300/-400/-500) C 1 0 (M) May be inoperative provided:

a) One center tank boost pump
operates normally, and
b) Center tank remains empty

07-03 (-100/-200/-300/ C 1 0 (M) Except for ER operations, may be

-400/-500) inoperative provided:
a) Both center tank boost pumps
operate normally, and
b) Fuel quantity in center tank is
verified by an acceptable
procedure.

07-04 (-600/-700/-800/ C 1 0 (M) Except for ER operations, may be

-900/-900ER) inoperative provided:
(With Boeing Service a) Both center tank boost pumps
Bulletin 737-28A1206 or operate normally, and
Production Equivalent b) Fuel quantity in center tank is
Installed) verified by an acceptable
procedure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

08 Fuel Temperature C 1 0 May be inoperative provided Total Air

Indicator Temperature or Ram Air
Temperature is substituted as an
indication of fuel temperature.

09 Fuel Quantity Totalizer C 1 0

***

10 Pressure Fueling System C 1 0 (M) May be inoperative provided

alternate procedures are established
and used.

10-01 Fueling Manifold Check C - 0 (M) May be inoperative provided

Valves associated Fueling Shutoff Valve is
verified to operate normally.

10-02 Fueling Shutoff Valve C - 0 (M) May be inoperative closed

provided:
a) Verify the refuel valve is
closed by pressurizing the
fueling manifold and verify
that fuel does not flow to the
tank with the failed refuel
valve, and
b) After removal of the fueling
nozzle, check the fueling
receptacle for leakage.
Leakage is not allowed.

10-03 Refuel Panel Fueling C 1 0 May be inoperative off provided refuel

Power Control Switch panel indicator test switch operates
normally in AUX FUELING POWER
CONTROL position or FUEL DOOR
SWITCH BYPASS position as
applicable.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

11 Fueling Bay Fuel Cap D 1 0

***

12 Refueling Control Panel C - 0 (M) May be inoperative provided fuel

Quantity Indicators quantity is verified by an acceptable
procedure.
|
14 Aft Auxiliary Fuel Tank
*** Boost Pumps
(Boeing Aux Tank)

14A C 2 1 (O) One may be inoperative provided:

a) Fuel quantity in other tanks is
adequate to reach an
alternate destination if
remaining pump fails at any
time, and
b) Fuel in tank is included as
part of zero fuel weight.

14B C 2 0 May be inoperative provided tank

remains empty.

14C C 2 0 May be inoperative provided fuel in

tank is included as part of zero fuel
weight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

15 Flight Deck Fuel

*** Quantity Indicators
(Aft Auxiliary Tank)

15-01 Boeing Tank Indicator

(Boost Pump Transfer
System)

15-01A C 1 0 (M)(O) May be inoperative provided

both boost pumps operate normally
when tank is fueled.

15-01B C 1 0 May be inoperative provided tank

remains empty.

15-02 Rogerson/PATS Tank

Indicator
(Pressurized Transfer
System)

15-02A C 1 0 (M)(O) May be inoperative provided:

a) Both auxiliary fuel transfer
systems operate normally,
b) Flight deck center tank fuel
quantity indicator operates
normally,
c) Tank is emptied and serviced
with a known quantity of fuel,
and
d) AFM normal procedures are
used for in-flight fuel transfer.

15-02B C 1 0 May be inoperative provided tank

remains empty.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

16 Fuel Measuring C - 0 (M) May be inoperative or

Sticks/Dripsticks broken/missing provided fuel quantity
is determined by other acceptable
means.

17 Fuel Scavenge System

***

17A C 1 0 May be inoperative with fuel

scavenge shutoff valve closed.

17B C 1 0 (O) May be inoperative with fuel

scavenge shutoff valve open
provided No. 1 Main Fuel Tank
forward boost pump remains off.

17C C 1 0 May be inoperative with fuel

scavenge shutoff valve open
provided center tank remains empty.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

18 Aft Auxiliary Tank

*** Pressurized Transfer
System
(Rogerson/PATS Aux
Tank)

18A C 2 1 (O) One may be inoperative provided:

a) Remaining transfer system
operates normally,
b) Fuel quantity in other tanks is
adequate to reach an
alternate destination if
remaining valve fails at any
time, and
c) Fuel in tank is included as
part of zero fuel weight.

18B C 2 0 May be inoperative provided tank

remains empty.

18C C 2 0 (O) May be inoperative provided fuel

in tank is included as part of zero fuel
weight.

19 Aft Auxiliary Tank C 2 1 (O) One may be inoperative provided:

*** Refueling Valves a) Remaining refueling valve
(Rogerson Aux Tank) operates normally, and
b) Automatic refueling shutoff
system operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

20 Aft Auxiliary Tank LOW

*** PRESSURE TRANSFER
Lights
(Rogerson Aux Tank)

20A C 2 1 (O) One may be inoperative provided:

a) Auxiliary fuel tank indicator
operates normally, and
b) Automatic transfer system
operates normally.

20B C 2 0 (O) May be inoperative for an

associated inoperative fuel transfer
system.

21 Fuel Quality Test

Switches

21-01 Digital System C - 0

21-02 Analog System

(-100/-200/-300)

21-02-01 Flight Deck C 1 0 (M) May be inoperative provided

associated fuel quantity indicators are
verified to operate normally once
each flight-day.

21-02-02 Fueling Panel C - 0 (M) May be inoperative provided

associated fuel quantity is verified by
an acceptable procedure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

22 FUEL/SPAR VALVE
CLOSED Lights

22-01 FUEL VALVE CLOSED C 2 0 (M) May be inoperative provided:

Lights a) Associated valve is verified to
(-100/-200/-300/ operate normally, and
-400/-500) b) Crossfeed VALVE OPEN light
operates normally.

22-02 SPAR VALVE CLOSED C 2 0 (M) May be inoperative provided:

Lights a) Associated valve is verified to
(-600/-700/-800/ operate normally, and
-900/-900ER) b) Crossfeed VALVE OPEN light
operates normally.

23 Fuel Summation Unit

*** (FSU)
(-200/-300/-400/-500)

23-01 PDCS C 1 0 (M)(O) May be inoperative provided

PDCS functions requiring gross
weight are not used.

23-02 FMCS C 1 0 (M)(O) May be inoperative provided:

(Software Update 7.4 a) FMCS functions requiring
and prior) gross weight are not used,
and
b) AFDS VNAV mode is not
used.

23-03 FMCS C 1 0 (M)(O) May be inoperative provided

(Software Updates 7.5, alternate procedures are established
8.5, 10x, 11, and 12) and used.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

25 Center Tank Fuel Boost

*** Pump Automatic Shutoff
System
(Service Bulletin
737-28A1228,
737-28A1216,
737-28A1206, or
Equivalent Installed)

25-01 All Models

25-01A C 2 0 May be inoperative provided

associated center tank fuel boost
pump is considered inoperative.

NOTE: Refer to MMEL Item 28-02 |

(Fuel Boost Pumps |
(Center Tank)). |

25-01B C 2 0 May be inoperative provided center

tank remains empty.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

25 Center Tank Fuel Boost

*** Pump Automatic Shutoff
System
(Service Bulletin
737-28A1228,
737-28A1216,
737-28A1206, or
Equivalent Installed)
(Cont’d)

25-02 -100/-200-300/-400/-500 C 2 0 May be inoperative with center tank

fueled provided:
a) Both center tank fuel boost
pump Low Pressure Warning
Light Systems operate
normally,
b) Center tank fuel quantity
indication operates normally,
c) Center tank fuel boost pump
switches must not be ON
unless personnel are
available in the flight deck to
monitor low pressure lights,
d) For ground operations, center
tank fuel boost pump switches
must not be positioned to ON
unless the center tank fuel
quantity exceeds 1,000 lbs. |
(453 kg), except when
defueling or transferring fuel,
e) Both center tank fuel boost
pumps are positioned OFF at
first indication of fuel pump
low pressure, and
f) Center tank fuel boost pumps
may be positioned ON when
established in cruise flight if
the center tank contains fuel.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

25 Center Tank Fuel Boost

*** Pump Automatic Shutoff
System
(Service Bulletin
737-28A1228,
737-28A1216,
737-28A1206, or
Equivalent Installed)
(Cont’d)

25-03 -600/-700/-800/ C 2 0 May be inoperative with center tank

-900/-900ER fueled provided:
a) Both center tank fuel boost
pump Low Pressure Warning
Light Systems operate
normally,
b) Center tank fuel quantity
indication operates normally,
c) Center tank fuel boost pumps
must not be ON unless
personnel are available in the
flight deck to monitor low
pressure lights,
d) For ground operations, center
tank fuel boost pump switches
must not be positioned to ON
unless the center tank fuel
quantity exceeds 1,000 lbs. |
(453 kg), except when
defueling or transferring fuel,
e) Center tank fuel boost pumps
are OFF for takeoff if center
tank fuel is less than
5,000 lbs. (2,300 kg) with |
airplane readied for initial taxi,

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

25 Center Tank Fuel Boost

*** Pump Automatic Shutoff
System
(Service Bulletin
737-28A1228,
737-28A1216,
737-28A1206, or
Equivalent Installed)
(Cont’d)

25-03 -600/-700/-800/ C 2 0 f) Both center tank fuel boost

-900/-900ER pumps are selected OFF
(Cont’d) when center tank fuel quantity
reaches 1,000 lbs. (453 kg) of |
fuel during climb and cruise,
g) Both center tank fuel boost
pumps are selected OFF
when center tank fuel quantity
reaches 3,000 lbs. (1,400 kg) |
of fuel during descent and
landing,
h) Both center tank fuel boost
pumps are positioned OFF at
first indication of fuel pump
low pressure,
i) Center tank fuel boost pumps
may be positioned ON when
established in cruise flight if
the center tank contains more
than 1,000 lbs. (453 kg) of |
fuel,
j) If the main tanks are not full,
the zero fuel gross weight of
the airplane plus the weight of
center tank fuel may exceed
the maximum zero fuel weight
by up to 5,000 lbs. (2,300 kg) |
for takeoff, climb, and cruise
and up to 3,000 lbs. |
(1,400 kg) for descent and
landing provided that the
effects of balance (CG) have
been considered, and
k) Defueling with passengers
on board is prohibited.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-20
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

26 Fuel Shutoff Valve D 1 0 (M) May be inoperative provided |

Battery and Charger Fuel Shutoff Valve Battery and |
(-600/700/-800/ Charger is deactivated. |
-900/-900ER)

100 Forward Auxiliary Fuel

System Transfer Valves
(PATS, -700/-800/
-900ER)

100A B 2 1 (M)(O) One may be inoperative

provided:
a) Inoperative FWD Aux tank
transfer valve is verified
“closed” and remains closed,
b) Remaining Fwd Aux tank
transfer valve operates
normally,
c) Fuel quantity in main tanks is
adequate to reach an
alternate destination if
remaining transfer valve fails
at any time, and
d) Fuel in tank is included as
part of zero fuel weight.

100B C 2 0 May be inoperative provided Fwd Aux

tank remains empty.

100C C 2 0 May be inoperative provided fuel in

Fwd Aux tank is included as part of
zero fuel weight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-21
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

101 Forward Auxiliary Fuel

System Vent Valves
(PATS, -700/-800/
-900ER)

101A B 2 1 (M)(O) One may be inoperative

provided:
a) Remaining Fwd Aux Tank
vent valve operates normally,
b) Fuel quantity in main tanks is
adequate to reach an
alternate destination if
remaining vent valve fails at
any time, and
c) Fuel in tank is included as
part of zero fuel weight.

101B C 2 0 May be inoperative provided Fwd Aux

tank remains empty.

101C C 2 0 May be inoperative provided Fwd Aux

tank is included as part of zero fuel
weight.

102 Forward Auxiliary Fuel

System Bleed Air Valve
(PATS, -700/-800/
-900ER)

102A C 1 0 May be inoperative provided:

a) Both air conditioning packs
operate normally,
b) Cabin pressure control
system operates normally,
and
c) Fwd Aux fuel quantity
indicator operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-22
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

102 Forward Auxiliary Fuel

System Bleed Air Valve
(PATS, -700/-800/
-900ER)
(Cont’d)

102B C 1 0 May be inoperative provided Fwd Aux

tank remains empty.

102C C 1 0 May be inoperative provided fuel in

Fwd Aux tank is included as part of
zero fuel weight.

103 Aft Auxiliary Fuel System

Transfer Valves
(PATS, -700/-800/
-900ER)

103A B 2 1 (M)(O) One may be inoperative

provided:
a) Inoperative Aft Aux tank
transfer valve is verified
“closed” and remains closed,
b) Remaining Aft Aux tank
transfer valve operates
normally,
c) Fuel quantity in main tanks is
adequate to reach an
alternate destination if
remaining transfer valve fails
at any time, and
d) Fuel in Aft Aux tank is
included as part of zero fuel
weight.

103B C 2 0 May be inoperative provided Aft Aux

tank remains empty.

103C C 2 0 May be inoperative provided fuel in

Aft Aux tank is included as part of
zero fuel weight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-23
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

104 Aft Auxiliary Fuel System

Vent Valves
(PATS, -700/-800/
-900ER)

104A B 2 1 (M)(O) One may be inoperative

provided:
a) Remaining Aft Aux tank vent
valve operates normally,
b) Fuel quantity in main tanks is
adequate to reach an
alternate destination if
remaining vent valve fails at
any time, and
c) Fuel in Aft Aux tank is
included as part of zero fuel
weight.

104B C 2 0 May be inoperative provided Aft Aux

tank remains empty.

104C C 2 0 May be inoperative provided fuel in

Aft Aux tank is included as part of
zero fuel weight.

105 Aft Auxiliary Fuel System

Bleed Air Valve
(PATS, -700/-800/
-900ER)

105A C 1 0 May be inoperative provided:

a) Both air conditioning packs
operate normally,
b) Cabin pressure control
system operates normally,
and
c) Aft Aux fuel quantity indicator
operates normally.

105B C 1 0 May be inoperative provided Aft Aux

tank remains empty.

105C C 1 0 May be inoperative provided fuel in

Aft Aux tank is included as part of
zero fuel weight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-24
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

106 Auxiliary Fuel System C 1 0 (M) May be inoperative provided

Isolation Valve Open isolation valve is visually verified
Light open before each flight.
(PATS, -700/-800/
-900ER)

107 Auxiliary Fuel System C 1 0 (M) May be inoperative provided

Isolation Valve Closed isolation valve is visually verified
Light closed before each auxiliary
(PATS, -700/-800/ refueling.
-900ER)

108 Auxiliary Fuel System C 1 0 (M) May be inoperative provided:

Isolation Valve a) Isolation valve is safety wired
(PATS, -700/-800/ in open position, and
-900ER) b) Electrical connector is capped
for flight.

NOTE: Fuel remaining in auxiliary

tanks may be used for flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-25
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

109 Auxiliary Tank Fueling

Valves
(PATS, -700/-800/
-900ER)

109-01 Forward Auxiliary C 1 0 (M) May be inoperative provided

Refueling Valve forward refueling valve is verified
“closed”.

NOTE 1: Auxiliary Fuel Tank shall not

be fueled until refueling
valve has been verified to
operate normally.

NOTE 2: Fuel remaining in tank may

be used for flight.

109-02 Aft Auxiliary Refueling C 1 0 (M) May be inoperative provided aft

Valve refueling valve is verified “closed”.

NOTE 1: Auxiliary Fuel Tanks shall

not be fueled until refueling
valve has been verified to
operate normally.

NOTE 2: Fuel remaining in tank may

be used for flight.

110 Auxiliary Fuel System

Alert Message Display
(PATS, -700/-800/
-900ER)

110A C 2 1 (M) One may be inoperative provided

transfer system is verified to operate
normally.

110B C 2 0 May be inoperative provided auxiliary

tanks remain empty.

110C C 2 0 May be inoperative provided fuel

auxiliary tanks are included as part of
zero fuel weight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-26
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

111 Auxiliary fuel Control C 1 0 (O) May be inoperative provided

Unit auxiliary fuel tanks remain empty.
(PATS, -700/-800/
-900ER)

112 Auxiliary Fuel Low Level

Float Switches
(PATS, -700/-800/
-900ER)

112-01 Forward Tank System

112-01A C 2 1 (O) One low level switch may be

inoperative provided fuel quantity
indicators operate normally.

112-01B C 2 0 (O) May be inoperative provided tank

remains empty.

112-01C C 2 0 (O) May be inoperative provided fuel

in tank is included as part of zero fuel
weight.

112-02 Aft Tank System

112-02A C 2 1 (O) One low level switch may be

inoperative provided fuel quantity
indicators operate normally.

112-02B C 2 0 (O) May be inoperative provided tank

remains empty.

112-02C C 2 0 (O) May be inoperative provided fuel

in tank is included as part of zero fuel
weight.

113 Auxiliary Fuel Processor C 1 0 (O) May be inoperative provided

(PATS, -700/-800/ auxiliary fuel tank remains empty.
-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-27
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

114 Auxiliary Fuel Pressure

Switches
(PATS, -700/-800/
-900ER)

114-01 Forward Tank Pressure

Switches

114-01A C 2 1 (M) One may be inoperative

provided:
a) Failed pressure switch
indicates low pressure,
b) Pressurization system
operates normally, and
c) Air conditioning packs operate
normally.

114-01B C 2 0 May be inoperative provided tank

remains empty.

114-01C C 2 0 May be inoperative provided fuel in

tank is included as part of zero fuel
weight.

114-02 Aft Tank Pressure

Switches

114-02A C 2 1 (M) One may be inoperative

provided:
a) Failed pressure switch
indicates low pressure,
b) Pressurization system
operates normally, and
c) Air conditioning packs operate
normally.

114-02B C 2 0 May be inoperative provided tank

remains empty.

114-02C C 2 0 May be inoperative provided fuel in

tank is included as part of zero fuel
weight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-28
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

115 Auxiliary Fuel Center

Tank Float Switches
(PATS, -700/-800/
-900ER)

115A C 2 0 (O) May be inoperative provided

auxiliary fuel tanks remain empty.

115B C 2 0 (O) May be inoperative provided fuel

in tank is included as part of zero fuel
weight.

116 Auxiliary Fuel

Maintenance Switches
(PATS, -700/-800/
-900ER)

116A C 2 1 (M) One may be inoperative

provided:
a) Affected maintenance
switch/indicator is failed in an
open condition, and
b) Remaining maintenance
switch/indicator is verified to
operate normally.

116B C 2 0 May be inoperative provided auxiliary

fuel tanks remain empty.

116C C 2 0 May be inoperative provided fuel in

tank is included as part of zero fuel
weight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-29
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

117 Auxiliary Fuel Alert

Switches
(PATS, -700/-800/
-900ER)

117A C 2 1 (M) One may be inoperative

provided:
a) Affected alert switch/indicator
is failed in an open condition,
and
b) Remaining alert
switch/indicator is verified to
operate normally.

117B C 2 0 May be inoperative provided auxiliary

fuel tanks remain empty.

117C C 2 0 May be inoperative provided fuel in

tank is included as part of zero fuel
weight.

118 Auxiliary Fuel Test C 2 0 (M) May be open provided:

Switches a) Associated fuel quantity
(PATS, -700/-800/ indicator display is verified to
-900ER) operate normally before each
flight, and
b) Alert message displays are
verified to operate normally
before each flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 28-30
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
28. Fuel
Change
Sequence No. Item 1 2 3 4 Bar

119 Flight Deck Fuel

Quantity Indicators
(Auxiliary Tanks)
(PATS, -700/-800/
-900ER)

119-01 Aft Auxiliary Tank

System

119-01A C 2 1 (O) One may be inoperative provided

transfer system operates normally
and total fuel quantity on the FMC is
verified to be correct.

119-01B C 2 0 May be inoperative provided auxiliary

fuel tanks remain empty.

119-01C C 2 0 May be inoperative provided fuel in

tank is included as part of zero fuel
weight.

119-02 Forward Auxiliary Tank

System

119-02A C 2 1 (O) One may be inoperative provided

transfer system operates normally
and total fuel quantity on the FMC is
verified to be correct.

119-02B C 2 0 May be inoperative provided auxiliary

fuel tanks remain empty.

119-02C C 2 0 May be inoperative provided fuel in

tank is included as part of zero fuel
weight
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 29-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
29. Hydraulic Power
Change
Sequence No. Item 1 2 3 4 Bar

01 Ground Interconnect C 1 0 (M) May be inoperative provided

Valve valve remains closed.
(System A and B)
(-100/-200)

02 System B Pumps

02-01 (-100/-200) C 2 1 Except for ER operations, one may

be inoperative provided:
a) Pressure indicator operates
normally, and
b) Thrust reversers operate
normally.

02-02 Engine Driven Hydraulic C 1 0

Pump Depressurization
Function
(-300/-400/-500/-600/
-700/-800/-900/-900ER)

03 System Pressure
Indications
(A and B)

03-01 (-100/-200) C 2 0 (O) May be inoperative provided:

a) Associated system pressure |
is checked from brake
pressure indicator before
each departure, and
b) All hydraulic low pressure
lights operate normally.

03-02 (-300/-400/-500/-600/ C 2 1 (O) One may be inoperative provided:

-700/-800/-900/-900ER) a) Associated system pressure |
is checked before each
departure, and
b) All hydraulic low pressure
lights operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 29-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
29. Hydraulic Power
Change
Sequence No. Item 1 2 3 4 Bar

04 System A Pump Low C 2 1 (O) One may be inoperative provided

Pressure Indication output of associated pump is checked
Systems before each departure.

05 System B Pump Low C 2 1 (O) One may be inoperative provided

Pressure Indication output of associated pump is checked
Systems before each departure.
|
07 System A and B
Overheat Light System

07-01 System A Over-heat D 2 0

*** Lights
(-100/-200)

07-02 System B Over-heat C 2 0 May be inoperative provided

Lights associated system B Low Pressure
(-100/-200) light operates normally.

07-03 (-300/-400/-500/-600/ C 2 0 May be inoperative provided

-700/-800/-900/-900ER) associated Low Pressure light
operates normally.

08 Hydraulic Quantity Low C 1 0 (M) May be inoperative provided

Level Light System B quantity is verified adequate before
(-100/-200) each departure.

09 Hydraulic Quantity Low C 1 0 (M) May be inoperative provided

Level Light System quantity is verified adequate before
(Standby System) each departure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 29-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
29. Hydraulic Power
Change
Sequence No. Item 1 2 3 4 Bar

10 System A Pumps

10-01 Engine Driven Hydraulic C - 0

Pump Depressurization
Function

11 System A Quantity
Indication System
(Flight Deck)

11-01 -100/-200 C 1 0 (M) May be inoperative provided:

a) Associated quantity is verified |
adequate before each
departure,
b) Associated system A pressure |
indicator operates normally,
and
c) System B and Standby
systems low quantity lights
operate normally.

11-02 (-300/-400/-500/-600/ C 1 0 (M) May be inoperative provided:

-700/-800/-900/-900ER) a) Associated quantity is verified |
adequate before each
departure,
b) Associated system pressure |
indication operates normally,
and
c) Associated pump low pressure |
lights operate normally.

12 Standby System Low C 1 0 (M) May be inoperative provided:

Pressure Light a) Standby system low quantity
light operates normally,
b) Output of standby pump is
verified before each departure,
and
c) Both System B pumps
operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 29-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
29. Hydraulic Power
Change
Sequence No. Item 1 2 3 4 Bar

13 Hydraulic Reservoir C - 1 (M) May be inoperative provided

Pressurization System reservoir can be pressurized.
Sources
|
15 System B Quantity C 1 0 (M) May be inoperative provided:
Indication System a) Associated quantity is verified |
(Flight Deck) adequate before each
(-300/-400/-500/-600/ departure,
-700/-800/-900/-900ER) b) Associated system pressure |
indication operates normally,
and
c) Associated pump low pressure |
lights operate normally.

16 Hydraulic Reservoir Air C - 0

*** Pressure Indicator
(Wheel Well)

17 Hydraulic Reservoir C - 0
Quantity Indicator
(Wheel Well)

18 Hydraulic Reservoir Fill C 1 0

System
(Wheel Well)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

01 Wing Anti-Ice Valves C 2 0 (M)(O) Except for ER operations

beyond 120 minutes, may be
inoperative closed provided airplane
is not operated in known or forecast
icing conditions.

01-01 (-100/-200) C 2 0 (M)(O) May be inoperative open

provided:
a) Valve is manually closed for
engine start,
b) Associated manifold is
depressurized when outside
air temperature is above 50 °F
(10 °C),
c) Associated engine bleed
thrust limits are followed when
manifold is pressurized, and
d) Air conditioning and
pressurization requirements
are followed when one or both
manifolds are depressurized.

01-02 (-300/-400/-500/-600/ C 2 1 (M)(O) One may be inoperative open

-700/-800/-900/-900ER) provided:
a) Except for engine start,
associated manifold is
depressurized when outside
air temperature is above 50 °F
(10 °C),
b) Associated engine bleed
thrust limits are followed when
manifold is pressurized, and
c) Air conditioning and
pressurization requirements
are followed when one
manifold is depressurized.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

02 Wing Anti-Ice Valve C 2 0 (M) May be inoperative provided

Position Lights valve is verified to operate normally
before operating in known or forecast
icing conditions.

03 Engine and Nose Cowl

Anti-Ice Valves

03-01 (-100/-200)

03-01A C 6 5 (M)(O) One may be inoperative

closed provided:
a) All remaining anti-ice valves
operate normally, and
b) Airplane is not operated in
known or forecast icing
conditions.

03-01B C 6 5 (M)(O) One may be inoperative open

provided:
a) All remaining valves operate
normally,
b) Operating temperature for
cowl valves is limited to 50 °F
(10 °C) maximum (ambient or
total air temperature) unless
S/B 71-1045 or 71-1046
“Nose Cowl TAI Spray Ring
Modification” or production
equivalent has been
incorporated, and
c) Appropriate performance
adjustments are applied.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

03 Engine and Nose Cowl

Anti-Ice Valves
(Cont’d)

03-02 (-300/-400/-500)

03-02A C 2 1 (M) One may be inoperative closed

provided airplane is not operated in
known or forecast icing conditions.

03-02B C 2 1 (M)(O) One may be inoperative

locked open provided:
a) Associated High Stage Valve
is considered inoperative,
b) Ambient temperature is below
100 °F (38 °C),
c) A minimum of 60% N1 is
maintained on associated
engine during flight in icing
conditions, and
d) Appropriate performance
adjustments are applied.

NOTE: Refer to MMEL Item 36-09 |

(High Stage Valves) |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 5. REPAIR CATEGORY
6. NO. INSTALLED
Boeing B-737 7. NO. REQUIRED FOR DISPATCH
8. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

03 Engine and Nose Cowl

Anti-Ice Valves
(Cont’d)

03-03 (-600/-700/-800/-900/
-900ER)

03-03A C 2 1 (M) Except for ER operations beyond

120 minutes, one may be inoperative
closed provided airplane is not
operated in known or forecast icing
conditions.

03-03B C 2 1 (M)(O) One may be inoperative

locked open provided:
a) Associated High Stage Valve
is considered inoperative,
b) Ambient temperature is below
100 °F (38 °C),
c) A minimum of 60% N1 is
maintained on associated
engine during flight in icing
conditions, and
d) Appropriate performance
adjustments are applied.

NOTE: Refer to MMEL Item 36-09 |

(High Stage Valves) |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

04 Engine and Nose Cowl

Anti-Ice Valve Position
Lights or TAI Indications

04-01 (-100/-200) C - 0 (M) May be inoperative provided

valve is verified to operate normally
before each departure.

04-02 (-300/-400/-500/-600/ C - 0 (O) May be inoperative provided

-700/-800/-900) valve is verified to operate normally
before each departure.

04-03 (-600/-700/-800/ C 4 2 One valve position indication

-900/-900ER) (either COWL VALVE OPEN light or
TAI indication) for each engine may
be inoperative provided other valve
position indication for that engine
operates normally.

04-04 (All Models) C - - May be inoperative provided

associated valve is considered
inoperative.

NOTE: Refer to MMEL Item 30-03 |

(Engine and Nose Cowl |
Anti-Ice Valves) |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

05 Pitot/Static Probe
Heaters

05-01 (-100/-200/-300/
-400/-500)

05-01-01 No. 1 Aux Pitot/Static B 1 0 May be inoperative provided:

Heater a) No. 2 Aux Pitot Static heater
(Right Lower Probe) operates normally,
b) RVSM operations are not
conducted, and
c) Airplane is not operated in
known or forecast icing
conditions.

05-01-02 No. 2 Aux Pitot/Static

Heater
(Left Lower Probe)

05-01-02A B 1 0 May be inoperative provided:

a) No. 1 Aux Pitot Static heater
operates normally,
b) RVSM operations are not
conducted, and
c) Airplane is not operated in
known or forecast icing
conditions.

05-01-02B B 1 0 May be inoperative provided:

a) No.1 Aux Pitot Static heater
operates normally, and
b) Dispatch deviations for
associated equipment are
observed.

05-01-03 Pitot/Static Heaters B 2 1 Pilot’s or copilot’s may be inoperative

(Upper Probes) for day VMC provided airplane is not
operated in visible moisture or in
known or forecast icing conditions.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

05 Pitot/Static Probe
Heaters
(Cont’d)

05-02 (-600/-700/-800/
-900/-900ER)

05-02-01 Left/Right Pitot Heaters B 2 1 Except for ER operations beyond

120 minutes, one may be inoperative
for day VMC provided:
a) Aux Pitot heater operates
normally,
b) Airplane is not operated in
visible moisture, and
c) Airplane is not operated in
known or forecast icing
conditions.

05-02-02 Aux Pitot Heater B 1 0 Except for ER operations beyond

(Right Lower Probe) 120 minutes, may be inoperative
provided:
a) Both Left and Right Pitot
heaters operate normally, and
b) Airplane is not operated in
known or forecast icing
conditions.

06 Vertical Stabilizer Pitot B 2 1 Except for ER operations beyond

*** Heaters 120 minutes, one may be inoperative
(Elevator and Rudder provided airplane is not operated in
Feel Systems) known or forecast icing conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

07 Total Air Temperature

Probe Heater

07A C - 0 Except for ER operations beyond

120 minutes, may be inoperative
provided airplane is not operated in
known or forecast icing conditions.

07B C - 0 (O) May be inoperative provided an

alternate temperature indicator
system is installed and operating
normally (i.e., Ram Air or Static Air
Temperature).

08 Angle of Attack Sensor C - 0 Except for ER operations beyond

Heater(s)/Stall Warning 120 minutes, may be inoperative
System Sensor provided airplane is not operated in
Heater(s)/Alpha Vane known or forecast icing conditions.
Heater(s)

09 Pitot, Pitot/Static and

Temperature Probe
Heater Lights

09-01 Green (Heater On)

*** Lights
(-100/-200)

09-01-01 Pitot and Pitot/Static B - - (M) One may be inoperative provided:

a) Required heater function is
verified before each departure,
and
b) HEATER OFF light operates
normally.

09-01-02 Temperature

09-01-02A C 1 0 (M) May be inoperative provided

associated heater function is verified
to operate normally before each
departure.

09-01-02B C 1 0 May be inoperative provided

associated heater is inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

09 Pitot, Pitot/Static and

Temperature Probe
Heater Lights
(Cont’d)

09-02 Amber (Heater Off)

*** Lights

09-02-01 Pitot and Pitot/Static B - 0 (M) Except for ER operations beyond

120 minutes, may be inoperative
provided:
a) Associated heater function is
verified to operate normally,
and
b) Airplane is not operated in
known or forecast icing
conditions.

09-02-02 Temperature

09-02-02A C - 1

09-02-02B C - 0 (M) May be inoperative provided

associated heater function is verified
to operate normally before each
departure.

09-02-02C C - 0 May be inoperative provided

associated heater is inoperative.

10 Wing Anti-Ice Duct

Overheat System

10-01 Ground Test Feature C 1 0

*** (-300/-400/-500)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

11 Electrically Heated
Windshields

11-01 No.1 or No. 2 Window C 4 3 Except for ER operations beyond

(100/-200) 120 minutes, one No. 1 or No. 2
window heater may be inoperative
provided:
a) Airplane is not operated in
known or forecast icing
conditions,
b) Windshield defog system
operates normally, and
c) Airspeed is limited to
250 KIAS below 10,000 ft.
MSL.

11-02 No. 1 Window C 2 1 Except for ER operations beyond

(-300/-400/-500/-600/ 120 minutes, one may be inoperative
-700/-800/-900/-900ER) provided:
a) Airplane is not operated in
known or forecast icing
conditions,
b) Both No.2 window heaters
operate normally,
c) Windshield defog system
operates normally,
d) Airspeed is limited to
250 KIAS below 10,000 ft.
MSL, and
e) Associated switch remains |
OFF. |

11-03 No. 2 Window C 2 1 One may be inoperative provided:

(-300/-400/-500/-600/ a) Both No. 1 window heaters
-700/-800/-900/-900ER) operate normally,
b) Windshield defog system
operates normally,
c) Airspeed is limited to
250 KIAS below 10,000 ft.
MSL, and
d) Associated switch remains |
OFF. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

11 Electrically Heated
Windshields
(Cont’d)

11-04 No. 4 or No. 5 Window C 4 0 No. 4 and No. 5 window heat may be
*** inoperative provided airspeed is
limited to 250 KIAS below 10,000 ft.
MSL.

11-05 No. 3 Window Heat D 2 0

*** System(s)

12 Windshield Defog C 1 0 May be inoperative provided

System electrically heated windshields for
No. 1 and No. 2 windows operate
normally.

13 Windshield Wiper C 2 0 May be inoperative provided:

System(s) a) Airplane is not operated in
precipitation within 5 statute
miles of airport of takeoff or
intended landing, and
b) Approach minimums do not
require its use.

13-01 Park Function C 2 0 May be inoperative for all flight

conditions provided blade(s) can be
positioned in a location that will not
obstruct forward vision.

13-02 Intermittent Speed D 2 0

*** Function
(-300/-400/-500/-600/
-700/-800/-900/-900ER)

13-03 Low Speed Function C 2 0 May be inoperative provided

associated high speed function
operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

13 Windshield Wiper
System(s)
(Cont’d)

13-04 High Speed Function

13-04A C 2 1 One may be inoperative provided

associated low speed function
operates normally.

13-04B C 2 0 May be inoperative provided both low

speed functions operate normally and
rain intensity is less than moderate.

14 Rain Repellent System D 1 0

*** (Including RainBoe and
STC ST09864SC)
(-100/-200/-300/
-400/-500)

15 Windshield Perimeter C 2 0
*** Heater(s)

16 HEATER OFF Light B 1 0 (O) May be inoperative provided:

*** (-100/-200) a) Remaining components of
pitot heat system are verified
to operate normally, and
b) Airplane is not operated in
known or forecast icing
conditions.

17 COWL ANTI-ICE Lights

(-300/-400/-500/-600/
-700/-800/-900/-900ER)

17A C 2 1 Except for ER operations beyond

120 minutes, one may be inoperative
provided airplane is not operated in
known or forecast icing conditions.

17B C 2 1 (M)(O) One may be inoperative

provided associated cowl anti-ice
valve is locked open.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 30-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
30. Ice and Rain Protection
Change
Sequence No. Item 1 2 3 4 Bar

18 Alpha Vane Heater Light

*** Systems

18A C 2 0 (M) May be inoperative provided

associated heater function is verified
to operate normally before each
departure.

18B C 2 0 May be inoperative provided

associated heater is considered
inoperative.

NOTE: Refer to MMEL Item 30-08 |

(Angle of Attack Sensor |
Heater(s)/Stall Warning |
System Sensor Heater(s)/ |
Alpha Vane Heater(s)) |

19 Drain Mast Heaters C 2 0 (M) May be inoperative provided

*** water supply to associated
components is secured off.

20 Ice Detection System D 1 0

***

21 Control Stand Wing

*** Anti-Ice Switches

21A C 2 0 (O) May be inoperative closed.

21B C 2 0 (O) May be inoperative open.

22 Air Data Probe Heat |

Systems |

22-01 AUTO activation C 2 0 (O) May be inoperative provided |

(-100/-200/-300/-400/- probe heat lights are not illuminated |
500 upon incorporation when PITOT STATIC PROBE HEAT |
of Boeing Service A and B switches are in the ON |
Bulletin 737-30A1064) position. |

22-02 AUTO activation C 2 0 (O) May be inoperative provided |

(-700/-800/-900/-900ER probe heat lights are not illuminated |
Line Number 3424 and when PITOT STATIC PROBE HEAT |
on) A and B switches are in the ON |
position. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

01 Clocks C 2 1 One may be inoperative at either pilot

or copilot station.

01-01 Automatic UTC Update C 2 0 (O) May be inoperative provided

*** Function manual mode is set and operates
normally.

02 Flight Data Recorder

System (FDR)

02-01 For Air Carrier or Holder

of a Commercial
Operator Certificate

02-01A C - - Any in excess of those required by

14 CFR may be inoperative.

02-01B A - 0 May be inoperative provided:

a) Cockpit Voice Recorder
(CVR) operates normally,
b) Airplane is not dispatched
from a designated airport as
listed in operator’s MEL
unless:
1) FDR failure occurs after
pushback but prior to
takeoff, or
2) FDR repair was attempted
but was not successful.
c) In those cases where repair is
attempted but not successful,
aircraft may be dispatched on
a flight or series of flights until
next designated airport where
repair must be accomplished
prior to dispatch, and
d) Repairs are made within
3 flight-days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

02 Flight Data Recorder

System (FDR)
(Cont’d)

02-01 For Air Carrier or Holder

of a Commercial
Operator Certificate
(Cont’d)

02-01-01 FDR Recording A - - Up to three recording parameters

Parameters Required by may be inoperative provided:
14 CFR a) Cockpit Voice Recorder
(CVR) operates normally, and
b) Repairs are made within
20 calendar-days.

02-01-02 FDR Recording A - - May be inoperative provided repairs

Parameters Not are made prior to completion of next
Required by 14 CFR heavy maintenance visit.

02-02 For an Operator other

than a Holder of an Air
Carrier or Commercial
Operator Certificate

02-02A C - 1 Any in excess of those required by

14 CFR may be inoperative.

02-02B A - 0 May be inoperative provided repairs

are made in accordance with
applicable 14 CFR.
|
04 Reference Speed C 1 0
*** Computer
(Total Fuel and VRef
Indicator -100/-200)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

|
06 AIDS Maintenance D 1 0
*** Recorder

07 Aircraft Condition D 1 0
*** Monitoring System
(ACMS)

07-01 Quick Access Recorder D 1 0

(Includes Avionica
miniQAR)
(STCs ST02472AT or
ST03151AT)

08 Common Display
System (CDS)
(-600/-700/-800/
-900/-900ER)

08-01 Display Units (DU)

08-01-01 Lower DU C 1 0 (O) May be inoperative provided:

a) All remaining DUs operate
normally, and
b) It is checked that engine
display can be switched to an
alternate DU.

08-01-02 Inboard DU A 2 1 (O) For EFIS/MAP configuration, one

may be inoperative provided:
a) It is checked that engine
display can be switched to an
alternate DU,
b) All navigation must be based
on ILS/VOR/DME, and
c) Repairs are made within
1 flight-day.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

08 Common Display
System (CDS)
(-600/-700/-800/
-900/-900ER)
(Cont’d)

08-02 CDS MAINT

Annunciation

08-02-01 PFD/ND B - 0 May be dispatched with faults

indicated by CDS MAINT
annunciation provided CDS
Operational Program Software (OPS)
P/N 3111-HNP-01A-05 or later, is
installed.

08-02-02 EFIS/MAP A - 0 May be dispatched with faults

indicated by CDS MAINT
annunciation provided:
a) Captain’s Inboard DU
operates normally,
b) CDS Operational Program
Software (OPS)
P/N 3111-HNP-01A-05 or
later is installed, and
c) Repairs are made within
1 flight-day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

09 Remote Light Sensor C 1 0 May be inoperative provided all

System manual display brightness controls
(-300/-400/-500/-600/ operate normally.
-700/-800/-900/-900ER)

10 Speed Reference C 1 0 May be inoperative provided speeds

Selector can be set using CDU.
(-600/-700/-800/
-900/-900ER)

11 Mechanical Timer
***

11A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

11B D 1 0 May be inoperative provided

procedures do not require its use.

12 Deleted in Revision 62. |

12A Deleted in Revision 62. |

12B Deleted in Revision 62. |

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

13 Flat Panel Display

*** System
(Universal Avionics, Inc.
EFI-890)
(STC ST03355AT and
ST03362AT)

13-01 Inboard DU (ND) A 2 1 (O) For PFD/ND configuration, one

may be inoperative provided:
a) Reversionary Display on PFD
is checked prior to departure,
b) PFD Lateral Deviation Scale
operates normally, and
c) Repairs are made within
2 flight-days.

13-01-01 Display Control Panel A - 0 May be inoperative provided:

Switches/Control Knobs a) Inboard DU is considered
inoperative, and
b) Repairs are made within
2 flight-days.

13-01-01-01 TERR C 2 1

13-01-01-02 TFC C 2 1

13-01-01-03 WX C 2 1

13-02 Outboard DU (PFD)

13-02-01 Display Control Panel

Switches/Control Knobs

13-02-01-01 RA/DA Set C 2 0 May be inoperative provided

approach minimums do not require its
use.

13-02-01-02 RA/DA C 2 0 May be inoperative provided

approach minimums do not require its
use.

13-02-01-03 RA/Test C 2 0

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

13 Flat Panel Display

*** System
(Universal Avionics, Inc.
EFI-890)
(STC ST03355AT and
ST03362AT)
(Cont’d)

13-03 Forward Electronic Panel B 1 0

(ND)
(-200)

13-03-01 TERR B 1 0 May be inoperative provided Terrain

Awareness and Warning System
(TAWS) are considered inoperative.

13-03-02 TFC

13-03-02A D 1 0 May be inoperative provided TCAS

VSI operates normally.

13-03-02B C 1 0 May be inoperative provided TCAS is

considered inoperative.

13-03-03 WX C 1 0 May be inoperative provided Weather

Radar is considered inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 31-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
31. Indicating/Recording Systems
Change
Sequence No. Item 1 2 3 4 Bar

14 TAKEOFF CONFIG
*** Light
|
14-03 -600/-700/-800/ C 2 1 (O) May be inoperative provided the
-900/-900ER associated CABIN ALTITUDE
(Upon Incorporation of warning light operates normally and
Boeing Service Bulletin flightcrew performs a briefing on
737-31A1332, or cabin altitude warning indications and
Production Equivalent) procedures before engine start for the
STC ST03312NY first flight of the day or following any
change of either flightcrew member.

15 Flat Panel Display

*** System Innovative
Solutions and Support
(STC ST03125NY)
(-300/-400/-500)

15-01 Integrated Flat Panel C 4 3 One ND may be inoperative.

Display (IFPD)

15-02 Display Control Panel A 2 1 (O) One may be inoperative provided:

(DCP) a) All functions of operative DCP
are verified to operate
normally,
b) The appropriate ALTN DCP is
selected, and
c) Repairs are made within
2 flight-days.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-1
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

01 Gear Seal Warning C 1 0 (M) May be inoperative provided gear

*** System seal function is checked once each
(-100/-200) flight-day.

02 Antiskid System

02-01 (-100/-200/-300/ C 1 0 (O) May be inoperative provided

-400/-500) operations are conducted in
compliance with AFM.

02-02 (-600/-700/-800/ C 1 0 (M)(O) May be inoperative provided:

-900/-900ER) a) Associated Antiskid
channel(s) is deactivated, and
b) Operations are conducted in
compliance with AFM.

03 Parking Brake Valve C 1 0 (M)(O) May be inoperative provided:

(-300/-400/-500/-600/ a) Antiskid system is
-700/-800/-900/-900ER) deactivated, and
b) Operations are conducted in
compliance with AFM
inoperative decrements.

04 Parking Brake Light

04-01 Solenoid Parking Brake C 1 0 (O) May be inoperative provided

Valve Installed antiskid system is turned OFF when
(-100/-200) parking brake is used.

04-02 Motor Operated Parking C 1 0 (M) May be inoperative provided

Brake Valve Installed parking brake shutoff valve is verified
to operate normally.

04-03 External Parking Brake

*** Light

04-03A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

04-03B D 1 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-2
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

05 Main Wheel Well C 1 0 (M) May be inoperative provided

*** Inflatable Seal System system is deactivated and secured.
(-100/-200)

06 Landing Gear Warning C - 2 Either of two other indicating systems

and Indicating System may be inoperative provided center
(-100/-200/-300/ panel indications operate normally.
-400/-500)

06-01 Secondary Gear B 1 0 (O) May be inoperative provided Main

Warning System Gear and Nose Gear Viewer are
(Pemco F/QC and accessible during all phases of flight.
COMBI)

07 Automatic Brake System C 1 0 (M) May be inoperative provided

*** system is deactivated and secured.

08 Rudder Pedal Nose

Wheel Steering System

08-01 Rotary Actuator C 1 0 (M)(O) May be inoperative

(-300/-400/-500/-600/ deactivated in disengage position
-700/-800/-900/-900ER) provided:
a) Operation of associated
systems is not affected, and
b) All takeoffs and landings are
made by pilot with access to
an operating tiller.

09 Direct Reading Tire D - 0

*** Pressure Gauge

10 Alternate Antiskid Valves C 2 0 (M) May be inoperative provided

(-300/-400/-500/-600/ manual braking capability of alternate
-700/-800/-900/-900ER) brake system is verified on
associated wheels.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-3
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

11 Brake Temperature
*** Monitor System

11A C 1 0 (O) May be inoperative provided AFM

Maximum Quick Turnaround Weight
limitations are observed.

11B D 1 0 (O) May be inoperative provided:

a) AFM Maximum Quick
Turnaround Weight limitations
are observed, and
b) Procedures are not based on
its use.

12 Nose Wheel Steering C 1 0 (M) May be inoperative provided:

*** Switch a) Nose wheel steering is
(-300/-400/-500/-600/ powered by Hydraulic
-700/-800/-900/-900ER) System A, and
b) Landing gear transfer valve is
verified to operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-4
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

13 Hydraulic Brake
Pressure Indication
System

13-01 (-100/-200)

13-01-01 Wheel Well Brake C 2 0 May be inoperative provided

Accumulator Gauges associated flight deck brake pressure
indicator operates normally.

13-01-02 Flight Deck HYD BRAKE C 2 1 (M) One brake indication (A or B)

PRESS Indicator may be inoperative provided
Systems associated brake accumulator charge
is verified normal once each
flight-day.

13-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)

13-02-01 Wheel Well Brake C 1 0 May be inoperative provided flight

Accumulator Gauge deck brake pressure indicator
operates normally.

13-02-02 Flight Deck HYD BRAKE C 1 0 (M) May be inoperative provided

PRESS Indicator System brake accumulator charge is verified
normal once each flight-day.

14 Gear Retraction Braking C 1 0 (O) May be inoperative provided:

System a) After takeoff, landing gear
(-600/-700/-800/ remains extended for
-900/-900ER) 2 minutes before retraction,
and
b) Takeoff performance is based
on Landing Gear Extended.

15 Landing Gear Selector C 1 0 (M)(O) May be inoperative provided it

Valve Bypass Module is deactivated in normal position.
(-600/-700/-800/
-900/-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-5
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

16 Landing Gear Actuation B 1 0 (M)(O) May be inoperative provided:

System a) Inoperative components are
(-600/-700/-800/ secured by an accepted
-900/-900ER) procedure,
b) Landing gear is secured in
down position, and
c) Airplane is dispatched in
accordance with AFM Gear
Extended Appendix.

17 Proximity Switch
Electronics Unit (PSEU)
System and
Supplemental Proximity
Sensor Electronics Unit
(SPSEU)
(-600/-700/-800/
-900/-900ER)

17-01 PSEU Fault

17-01A C - 0 (M) May be dispatched with faults

indicated by PSEU light provided
PSEU is checked for faults before
each departure.

17-01B C - 0 May be dispatched with faults

indicated by PSEU light provided
PSEU light can be extinguished.

17-02 PSEU Light C 1 0 (M) May be inoperative provided

PSEU is checked for faults before
each departure.

17-03 Supplemental Proximity C 1 0 (M) May be inoperative provided

*** Sensor Electronics Unit SPSEU is checked for faults before
(SPSEU) Light each departure.
(-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-6
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

18 Landing Gear Alternate B 1 0 (M)(O) May be inoperative provided:

Extension System a) Inoperative Components are
(-600/-700/-800/ secured by an accepted
-900/-900ER) procedure,
b) Landing gear is secured in
down position, and
c) Airplane is dispatched in
accordance with AFM Gear
Extended Appendix.

19 Main Landing Gear B 4 3 (M)(O) One spring on one main gear

Uplock Springs uplock mechanism may be missing
provided landing gear lever remains
in UP position for duration of flight
until gear extension is required.

20 Landing Gear Frangible C 2 0 (M) May be broken or missing

Fitting provided fitting is replaced with a
(-600/-700/-800/ hydraulic cap assembly.
-900/-900ER)

21 Flap Landing Warning C 1 0 (M) Switch contacts normally in use

Switch, S138 may be inoperative provided:
(-600/-700/-800/ a) S138 switch is rewired using
-900/-900ER) an alternate set of contacts,
and
b) PSEU BITE is used to verify
normal operation of S138
switch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-7
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

22 Two-Position Tail Skid

22-01 (-800 with Short Field

*** Performance
(SPF Option)

22-01-01 Retraction Mechanism

22-01-01A C 1 0 (M)(O) May be inoperative provided:

a) Tail skid is secured in
retracted position, and
b) Appropriate performance
adjustments are applied.

22-01-01B C 1 0 (M)(O) May be inoperative provided:

a) Tail skid is secured in
extended position, and
b) Appropriate performance
adjustments are applied.

22-01-02 Cartridge Core Assembly B 1 0 (M)(O) May be inoperative provided:

a) Detailed AMM inspection
reveals no internal and
external structural damage,
b) Tail skid is secured in
retracted position, and
c) Appropriate performance
adjustments are applied.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 32-8
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
32. Landing Gear
Change
Sequence No. Item 1 2 3 4 Bar

22 Two-Position Tail Skid

(Cont’d)

22-02 (-900ER)

22-02-01 Retraction Mechanism

22-02-01A C 1 0 (M)(O) May be inoperative provided:

a) Tail skid is secured in
retracted position, and
b) Appropriate performance
adjustments are applied.

22-02-01B C 1 0 (M)(O) May be inoperative provided:

a) Tail skid is secured in
extended position, and
b) Appropriate performance
adjustments are applied.

22-02-02 Cartridge Core Assembly B 1 0 (M)(O) May be inoperative provided:

a) Detailed AMM inspection
reveals no internal and
external structural damage,
b) Tail skid is secured in
retracted position, and
c) Appropriate performance
adjustments are applied.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

01 Cockpit/Flight C - - Individual lights may be inoperative

Deck/Flight provided:
Compartment and a) Remaining Lighting System
Instrument Lighting lights are sufficient to clearly
System illuminate all required
instruments, controls, and
other devices for which they
are provided,
b) Remaining Lighting System
lights are positioned so that
direct rays are shielded from
flightcrew members’ eyes,
and
c) Lighting configuration and
intensity is acceptable to the
flightcrew.

NOTE 1: Individual button/switch

lights and/or
annunciation/indications are
excluded from this relief.

NOTE 2: Unaided operation (without

NVGs) may be permitted
with inoperative NVG
supplemental lights; cracked
or missing filters.

02 Cabin Interior
Illumination
(Includes Pemco
-300QC and
-400 COMBI)

02-01 Passenger and Combi C - - Individual lights may be inoperative

Configurations without provided sufficient lighting remains
Photoluminescent for cabin attendants/cargo couriers to
Emergency Escape Path perform their duties.
Marking Systems

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

02 Cabin Interior
Illumination
(Includes Pemco
-300QC and
-400 COMBI)
(Cont’d)

02-02 Passenger and Combi C - - Individual lights may be inoperative

Configurations with provided:
Photoluminescent a) Sufficient lighting remains for
Emergency Escape Path cabin attendants/cargo
Marking Systems couriers to perform their
duties, and
b) Remaining lighting is sufficient
to charge Photoluminescent
Emergency Escape Path
Marking System.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

03 Passenger Lighted
Information Signs and
Notice System

03-01 “NO SMOKING/

FASTEN SEAT BELT/
RETURN TO SEAT”
Signs

03-01A C - - (M) May be inoperative provided:

a) Associated passenger seat or
lavatory is not occupied from
which a passenger lighted
information sign is not readily
legible, and
b) Associated seat or lavatory is
blocked and placarded
“DO NOT OCCUPY”.

NOTE: These conditions are not

intended to prohibit lavatory
use or inspections by
crewmembers.

03-01B C - - (O) May be inoperative and

associated passenger seat or
lavatory may be occupied provided:
a) PA system operates normally,
and
b) PA system is used to notify
passengers and cabin crew
when associated sign(s) are
placed on or off.

03-02 All-Cargo, C - - (O) May be inoperative provided

Supernumerary/Courier alternate procedures are established
Area Lighted Information and used to notify
Signs couriers/supernumeraries when
associated sign(s) are placed on or
off.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

03 Passenger Lighted
Information Signs and
Notice System
(Cont’d)

03-03 Aural Tone System C 1 0

03-04 Flight Deck Automatic C 1 0 (O) May be inoperative provided:

Function a) Manual control function
operates normally, and
b) Alternate procedures are
established and used.

04 Lower Cargo C - 0 Light Lens excluded.

Compartment Light
Systems
(Fwd/Aft)

04-01 Light Lens C - 0 May be broken/missing provided

(-100/-200/-300/-400/ associated light bulb is removed. LED
-500/-900/-900ER) light, no associated LED Module
removal required.

04-02 Light Lens C - 0 May be broken/missing provided

(-600/-700/-800 Prior to associated light bulb is removed. LED
Incorporation of Boeing light, no associated LED Module
Service Bulletins removal required.
737-26-1121, and
737-1122, and either
737-21-1135 or
737-21-1163 or their
Production Equivalents)

04-03 Light Lens C - - Any number from aft lower cargo

(-600/-700/-800 Upon compartment and one from forward
Incorporation of Boeing lower cargo compartment may be
Service Bulletins broken/missing provided associated
737-26-1121, and light bulb is removed. LED light, no
737-1122, and either associated LED Module removal
737-21-1135 or required.
737-21-1163 or their
Production Equivalents)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

05 High Intensity or Strobe

Lights System

05-01 All Models C 1 0 May be inoperative provided

*** (Except Models with anti-collision beacons operate
STCs ST01821LA, normally.
ST01873LA, and
ST02015LA)

05-02 Models with STCs C 1 0 May be inoperative provided anti-

ST01821LA, collision beacons operates normally.
ST01873LA, and
ST02015LA

06 Anti-Collision Beacons
(Without Blended
Winglet or Split Scimitar
Winglet, -800/-900/
-900ER Blended Winglet
or Split Scimitar Winglet,
and -700 Blended
Winglet or Split Scimitar
Winglet with Dual Glass
Lens)
(Except STCs
ST01821LA and
ST01873LA)

06A C 2 0 May be inoperative provided wing

tip/winglet and tail strobe lights are |
installed and operate normally.

06B C 2 0 May be inoperative provided:

a) At least one tail or wing
tip/winglet strobe light |
operates normally, and
b) Operations are not conducted
at night.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

06 Anti-Collision Beacons
(Without Blended
Winglet or Split Scimitar
Winglet, -800/-900/
-900ER Blended Winglet
or Split Scimitar Winglet,
and -700 Blended
Winglet or Split Scimitar
Winglet with Dual Glass
Lens)
(Except STCs
ST01821LA and
ST01873LA)
(Cont’d)

06-01 Blended Winglet

06-01-01 (-700 with Single Plastic C 2 0 May be inoperative other than night
Lens) operations provided strobe lights
operate normally.
|
06-01-03 (-300/-500 with
STC ST01219SE and
Winglet Strobe Lights)

06-01-03A C 2 0 May be inoperative provided winglet

strobe lights operate normally.

NOTE: Tail strobe light may be

inoperative.

06-01-03B C 2 0 May be inoperative provided at least

one tail or winglet strobe light
operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

06 Anti-Collision Beacons
(Without Blended
Winglet or Split Scimitar
Winglet, -800/-900/
-900ER Blended Winglet
or Split Scimitar Winglet,
and -700 Blended
Winglet or Split Scimitar
Winglet with Dual Glass
Lens)
(Except STCs
ST01821LA and
ST01873LA)
(Cont’d)

06-01 Blended Winglet

(Cont’d)

06-01-04 (-700 with single Plastic C 3 0 May be inoperative for other than
Lens and night operations provided strobe
STC ST02015LA and 3rd lights operate normally.
anti-collision beacon)
NOTE: Three anti-collision beacons
must be operative from
sunset to sunrise operations.

06-02 (STCs ST01821LA and C 2 0 May be inoperative for other than

ST01873LA) night operations provided strobe
lights operate normally.

07 Wing Illumination Lights C 2 0 (O) May be inoperative provided

ground deicing procedures do not
require their use.

07-01 Overwing Ice Lights C 2 0

*** (Grimes Aerospace
STC ST500CH)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

08 Landing Lights

08-01 With Retractable

Landing Lights

08-01A C 4 2 One may be inoperative on each side

provided one of two operating lights
is in fixed position.

08-01B C 4 0 May be inoperative provided

operations are not conducted at
night.

08-01-01 Retractable Light

Extend/Retract Motors

08-01-01A C 2 0 (M)(O) May be inoperative provided:

a) Light is in extended position,
b) Light illuminates normally, and
c) Appropriate performance
adjustments are applied.

08-01-01B C 2 0 (O) May be inoperative provided:

a) Associated light is considered
inoperative, and
b) Appropriate performance
adjustments are applied when
associated light is not in the
fully retracted position.

08-01-02 Pulse Light System D 1 0

***

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

08 Landing Lights
(Cont’d)

08-02 LED Array

*** (Light Assembly)

08-02A C 4 2 One LED array (light assembly) may

be inoperative on each side.

NOTE: There is an inboard LED array

(light assembly) and an
outboard LED array (light
assembly) inside the strakelet
on each wing. These same
lights are also used for the taxi
lights. Taxi lights may also be
affected (see item 33-09).

08-02B C 4 2 Both LED arrays on one side may be

inoperative provided the Runway
Turn Off light on the same side
operates normally.

NOTE: There is an inboard LED array

(light assembly) and an
outboard LED array (light
assembly) inside the strakelet
on each wing. These same
lights are also used for the taxi
lights. Taxi lights may also be
affected (see item 33-09).

08-02C C 4 0 May be inoperative provided

operations are not conducted at
night.

NOTE: There is an inboard LED array

(light assembly) and an
outboard LED array (light
assembly) inside the strakelet
on each wing. These same
lights are also used for the taxi
lights. Taxi lights may also be
affected (see item 33-09).
08-02-01 Alternate Flash Function D - 0
***
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

09 Taxi Light

09-01 Nose Gear Taxi Light C 1 0

***

09-02 LED Array C 4 0 NOTE: There is an inboard LED array

*** (Light Assembly) (light assembly) and an
outboard LED array (light
assembly) inside the strakelet
on each wing. These same
lights are also used for the
landing lights. Landing lights
may also be affected
(see item 33-08).

10 Runway Turn Off Lights C 2 0

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

11 Wing Tip Position Lights C 4 0 May be inoperative provided

operations are not conducted from
sunset to sunrise.

11-01 Light Bulbs/Lamps/LED C - 4 Any except following minimum may

Modules be inoperative for operations from
(Without Blended sunset to sunrise:
Winglet or Split Scimitar a) One stationary red wing tip
Winglet, Blended bulb,
Winglet, or Split Scimitar b) One stationary green wing tip
Winglet with Dual Glass bulb, and
Lens, and -300/-500 with c) One stationary white tail light
Blended Winglet) bulb at each wing tip position.

11-02 Light Bulbs/Lamps

(-700/-800 Blended
Winglet with Single
Plastic Lens)

11-02A C - 5 Any except following minimum may

be inoperative for operations from
sunset to sunrise:
a) Both stationary red wing tip
bulbs,
b) One stationary green wing tip
bulb, and
c) One stationary white tail light
bulb at each wing tip position.

11-02B B - 4 Any except following minimum may

be inoperative for operations from
sunset to sunrise:
a) One stationary red wing tip
bulb,
b) One stationary green wing tip
bulb, and
c) One stationary white tail light
bulb at each wing tip position.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

12 Door Locked Light C 1 0 May be inoperative provided locking

*** (Flight Deck to Cabin) function operates normally.
(Not 14 CFR Part 25,
§ 25.795 Compliant)
|
14 Exterior Emergency
Lighting System

14A B 1 0 May be inoperative provided

operations are not conducted at
night.

14B B 1 0 May be inoperative for all-cargo night

operations provided forward entry
door escape slide lights operate
normally.

15 Interior Emergency Exit

Lighting System

15-01 Mixed or All-Cargo C 1 0 Lights may be inoperative in cargo

Configuration areas provided:
a) No persons occupy that area,
and
b) Forward entrance door light
operates normally at all times.

15-02 Emergency Aisle Lights C - - Light assemblies installed above aisle

*** (-600/-700/-800/ may be inoperative provided no two
-900/-900ER) adjacent (opposite side) light
assemblies are inoperative.

15-03 Advance Technology C - - Light assemblies installed above aisle

*** Interior (ATI) (curved edge of stowage bins) may
(Aisle Light Assemblies) be inoperative provided no two
(-200/-300/-400/-500) adjacent (opposite side) light
assemblies are inoperative.

15-04 Flight Deck Exit Light C 1 0 May be inoperative provided

*** operations are not conducted at
night.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

16 System Annunciator
Lights, Left and Right
(Pilot’s Light Shield)

16A C - - (O) One light may be inoperative for

an operating system.

16B C - - May be inoperative for an associated

inoperative system.

17 Flight Deck Master C - - (O) May be inoperative provided

Lights Test and intended function of associated
Individual Lights light(s) is verified once each
Press-to-Test Features flight-day.

18 Wheel Well Lights

18-01 Dome Lights C 3 0

18-02 Inspection Flood Lights

18-02-01 (-100/-200/-300/
-400/-500)

18-02-01A C 3 1 Main gear lights may be inoperative

provided operations are not
conducted at night.

18-02-01B D 3 0 Lights may be inoperative provided a

landing gear indicating system other
than viewer system and independent
of center panel is installed and
operates normally.

18-02-02 (-600/-700/-800/ D 2 0
-900/-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

19 Floor Proximity
Emergency Escape Path
Marking System
(All Models and STCs)

19-01 Incandescent Lighting C - - Individual lights may be inoperative

System provided minimum acceptable lighting
levels specified in one of the following
documents are complied with:
a) FAA engineering approval
letter,
b) FAA approved report of Type
Design holder,
c) Limitations and Conditions
section of the applicable
Supplemental Type Certificate
(STC), or
d) An FAA-approved report
incorporated in the Master
Drawing List for the applicable
STC.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

19 Floor Proximity
Emergency Escape Path
Marking System
(All Models and STCs)
(Cont’d)

19-02 Photoluminescent C - - Components may be inoperative

Lighting System provided minimum acceptable lighting
levels specified in one of the following
documents are complied with:
a) FAA engineering approval
letter,
b) FAA-approved report of Type
Design holder,
c) Limitations and Conditions
section of the applicable
Supplemental Type Certificate
(STC), or
d) An FAA-approved report
incorporated in the Master
Drawing List for the applicable
STC.

19-03 Seat Mounted LED and C - - Individual lights may be inoperative

Incandescent Lighting provided minimum acceptable lighting
Systems levels specified in one of the following
documents are complied with:
a) FAA engineering approval
letter,
b) FAA-approved report of Type
Design holder,
c) Limitations and Conditions
section of the applicable
Supplemental Type Certificate
(STC), and
d) An FAA-approved report
incorporated in the Master
Drawing List for the applicable
STC.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

20 LOGO Light System D 1 0

***

21 Main Deck Cargo

*** Compartment Lighting
(737C, 737-700C/
-800BCF, and STCs
ST01566LA, SA2969SO,
SA2970SO, ST00287AT,
ST00283AT,
ST01827LA,
ST01961SE, and
ST02556SE)

21-01 Cargo Door Floodlights

21-01A C - 0 (M) May be inoperative for night

operations provided alternate
procedures are established and used.

21-01B C - 0 May be inoperative provided

operations are not conducted at
night.

NOTE: Not required for all-passenger

operations.

21-02 Cargo Compartment

Lights
(-800BCF, STCs |
ST00283AT,
ST01827LA, and
ST02556SE)

21-02A C - 0 (M) May be inoperative for night

operations provided alternate
procedures are established and used.

21-02B C - 0 May be inoperative provided

operations are not conducted at
night.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

22 Main Deck Cargo Door

*** System Annunciator
Light
(737-300 QC, PEMCO
Aeroplex, Inc.
-300/-400, and STCs
ST01566LA,
ST01961SE, and
ST02556SE)

22-01 System Annunciator A 2 1 (M)(O) One warning light may be

Lights, Pilot’s Overhead illuminated provided:
Panel a) Alternate procedures are
(737-300QC, and STCs established and used to verify
ST01566LA, main cargo door is closed and
ST01961SE, and locked, and
ST02556SE) b) Repairs are made within
2 flight-days.

22-02 System Annunciator A - - (M)(O) One warning light may be

Lights, Operator Control inoperative provided:
Panel a) It is not a VENT DOOR OPEN
(737-300QC, PEMCO light,
Aeroplex, Inc. b) Vent door handle is locked,
-300/-400, and STCs c) Outside view port is verified
ST01566LA, green,
ST01961SE, and d) Individual lock is not loose,
ST02556SE) e) Main cargo door is verified
closed, latched, and locked,
and
f) Repairs are made within
2 flight-days.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

23 Master Dim System B 1 0 Dim function may be inoperative

provided:
a) TEST and BRT functions
operate normally,
b) Except during light test, switch
is placed in BRT, and
c) Light intensity is acceptable to
flightcrew.

24 Sterile Flight
*** Compartment Light
System

24A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

24B D 1 0 May be inoperative provided

procedures do not require its use.

25 Service Area Light

Systems
(Nose, Electrical
Equipment,
Air Conditioning,
Aft Accessory,
APU, Tailcone
Compartments, and
Fueling Panel)

25A C - 0

25B D - 0 May be inoperative provided

operations are not conducted at
night.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 33-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
33. Lights
Change
Sequence No. Item 1 2 3 4 Bar

26 Main Cargo C - 0 May be inoperative provided in-flight

Compartment In-Flight access to the main deck cargo
Access Alert System compartment is prohibited.
(-800BCF, |
STC ST01961SE and
ST02556SE)

26-01 Main Cargo C - 0 May be inoperative provided in-flight

Compartment Lights access to the main deck cargo
compartment is prohibited.

26-02 Main Cargo C 2 0 May be inoperative provided in-flight

Compartment Alert access to the main deck cargo
Horns compartment is prohibited.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

01 Mach/Airspeed
Indications

01-01 Mach Indications C 2 1 One may be inoperative provided

one Mach/Airspeed warning
and Mach trim system operate
normally.

01-01-01 (-100/-200/-300/ C 2 0 May be inoperative provided:

-400/-500) a) Airplane remains at or below
FL 230, and
b) Airspeed remains at or below
320 KIAS.

01-01-02 (-600/-700/-800/ C 2 0 May be inoperative provided:

-900/-900ER) a) Airplane remains at or below
FL 280, and
b) Airspeed remains at or below
320 KIAS.

01-02 Airspeed Indicators C 2 1 One may be inoperative provided:

*** (-300/-400/-500) a) EFIS Speed Tape displays
are installed and operate
normally, and
b) One Mach/Airspeed warning
operates normally.

01-03 EFIS Speed Tape C 2 0 May be inoperative provided airspeed

*** (-300/-400/-500) indicators are installed and operate
normally at each pilot’s station.

01-04 Airspeed Cursor A 2 1 (O) One may be inoperative provided:

*** (-100/-200/-300/ a) Alternate procedures are
-400/-500) established and used, and
b) Repairs are made within
3 flight-days.

01-05 External Airspeed C - 0 (O) May be inoperative or missing

*** Markers (Bugs) provided alternate procedures are
(-100/-200/-300/ established and used.
-400/-500)

01-06 Digital Airspeed Readout C - 0

*** (-100/-200/-300/
-400/-500)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

02 Mach/Airspeed Warning
Systems

02-01 Maximum Operating C 2 1 One may be inoperative provided

Speed Indication clacker warning system operates
normally and is independent from
Mach Indicator.

02-02 Clacker

02-02-01 (-100/-200)

02-02-01A C - 1

02-02-01B B - 0 Systems may be inoperative provided:

a) Both Mach indicators operate
normally,
b) 340 KIAS/.78 Mach airspeed
limitations are observed, and
c) If overspeed warning occurs
earlier than scheduled during
flight, speed must remain
below point at which the
warning occurs.

02-02-01C B - 0 Systems may be inoperative provided:

a) Both Mach indicators operate
normally,
b) 340 KIAS/.78 Mach airspeed
limitations are observed, and
c) If overspeed warning occurs
below .78 Mach, system must
be deactivated by pulling
associated circuit breaker and
observe speed limits.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

02 Mach/Airspeed Warning
Systems
(Cont’d)

02-02 Clacker
(Cont’d)

02-02-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)

02-02-02A C 2 1

02-02-02B B 2 0 Systems may be inoperative provided:

a) Both Mach indicators operate
normally,
b) 330 KIAS/.76 Mach airspeed
limitations are observed, and
c) If overspeed warning occurs
earlier than scheduled during
flight, speed must remain
below point at which the
warning occurs.

02-02-02C B 2 0 Systems may be inoperative provided:

a) Both Mach indicators operate
normally,
b) 330 KIAS/.76 Mach airspeed
limitations are observed, and
c) If overspeed warning occurs
below .76 Mach, system must
be deactivated by pulling
associated circuit breaker and
observe speed limits.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

03 Altimeter Vibrators

03-01 Servo-Pneumatic C 2 1 One may be inoperative provided

associated air data computer
operates normally.

03-02 Pneumatic C 2 1 One may be inoperative provided

VMC exist at departure and arrival
airports.

03-03 Pneumatic C 1 0 May be inoperative provided VMC

(With Electric/Electronic exist at departure and arrival airports.
Altimeter)

03-04 One Pneumatic and One

Servo-Pneumatic

03-04A C 2 1 Servo-Pneumatic may be inoperative

provided associated air data
computer operates normally.

03-04B C 2 1 Pneumatic may be inoperative

provided VMC exist at departure and
arrival airports.

03-05 Standby Altimeter C 1 0 May be inoperative provided VMC

Vibrator exist at departure and arrival airports.
(With Electric/Electronic
Altimeter)

04 Static Air Temperature D - 0

*** Indication

05 Total Air Temperature C - 0 May be inoperative provided an

Indication alternate air temperature indication
(e.g., PDCS, FMCS, RAT, SAT)
operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

|
07 Standby Horizon
Indicator

07-01 Standby Attitude B 1 0 May be inoperative provided:

Indicator a) Operations are conducted in
Day VMC only, and
b) Operations are not conducted
into known or forecast
over-the-top conditions.

07-02 ILS Indication D 1 0

***

08 Angle of Attack C - 0
*** Indications

09 Turn and Bank Indicators

09-01 Rate of Turn Indicators

*** (-100/-200/-300/
-400/-500)

09-01A C 2 1

09-01B C 2 0 May be inoperative provided Standby

Horizon Indicator operates normally.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

11 Standby Magnetic
Compass

11A B 1 0 May be inoperative provided any

combination of three gyro or INS
(IRU) stabilized compass systems
are operative.

11B B 1 0 May be inoperative provided:

a) Any combination of two gyro
or INS (IRU) stabilized
compass systems are
operative, and
b) Airplane is operated with dual
independent navigation
capability and under positive
radar control by ATC on
enroute portion of flight.

11C C 1 0 May be inoperative for flights that are

entirely within areas of magnetic
unreliability provided two stabilized
directional gyro systems are installed,
operative, and used in conjunction
with free gyro navigation techniques.

12 Flight Director Systems C 2 0 May be inoperative provided

approach minimums do not require its
use.

13 Distance Measuring D - - Any in excess of those required by

Equipment Systems 14 CFR may be inoperative.

14 Marker Beacon Receiver C - 0 May be inoperative provided

System approach minimums do not require its
use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

15 Weather Radar

15-01 Weather Radar with

Windshear Detection
and Avoidance System
(Predictive) Installed

15-01A B - 0 (O) May be inoperative provided:

a) Weather radar is not required
by 14 CFR, and
b) Alternate procedures are
established and used.

NOTE: Operator’s alternate

procedures should include
reviewing windshear
avoidance and windshear
recovery procedures.

15-01B C - 0 (O) May be inoperative provided:

a) Weather radar is not required
by 14 CFR,
b) Alternate procedures are
established and used, and
c) Windshear Warning and
Guidance System (Reactive)
operates normally.

15-01C D - 1 May be inoperative provided one

remaining weather radar operates
normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

15 Weather Radar
(Cont’d)

15-02 Weather Radar without

Windshear Detection
and Avoidance System
(Predictive) Installed

15-02A C - 0 May be inoperative provided weather

radar is not required by 14 CFR.

15-02B D - 1 May be inoperative provided one

remaining weather radar operates
normally.

15-03 Windshear Detection

*** and Avoidance System
(Predictive)

15-03A B - 0 (O) May be inoperative provided

alternative procedures are
established and used.

NOTE: Operator’s alternate

procedures should include
reviewing windshear
avoidance and windshear
recovery procedures.

15-03B C - 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Windshear Warning and
Guidance System (Reactive)
operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

15 Weather Radar
(Cont’d)

15-04 Autotilt/Multiscan C 1 0 May be inoperative provided manual

*** Function tilt function operates normally.
(Including STCs
ST01843AT,
ST01470LA-D)

15-05 Stabilization Function C 1 0 (M) May be inoperative provided:

*** a) Manual tilt control operates
normally, and
b) Antenna is verified to scan in
a horizontal plane with tilt at
zero degrees.

16 Radio Compass D - - Any in excess of those required by

Systems 14 CFR may be inoperative.
(ADF)

17 VHF Navigation Systems

(VOR/ILS)

17-01 (-100/-200/-300/ D - - Any in excess of those required by

-400/-500) 14 CFR, and not powered by a
Standby Bus, may be inoperative
provided approach minimums do not
require its use.

17-01-01 Auto Tune Function C - 0 (O) May be inoperative provided:

a) Enroute or approach
procedures do not require its
use, and
b) Manual tuning operates
normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

17 VHF Navigation Systems

(VOR/ILS)
(Cont’d)

17-02 (-300/-400/-500 D - - Any in excess of those required by

GNLU-920 MMR, 14 CFR, and not powered by a
STC ST00998LA-D) Standby Bus, may be inoperative
provided approach minimums do not
require its use.

17-02-01 Equipment Cooling Fan B 2 0

17-03 (-600/-700/-800/
-900/-900ER)

17-03-01 VOR Systems D 2 - Any in excess of those required by

14 CFR, and not powered by a
Standby Bus, may be inoperative.

17-03-02 ILS Systems D 2 - Any in excess of those required by

14 CFR, and not powered by a
Standby Bus, may be inoperative
provided approach minimums do not
require its use.
|

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

18 ATC Transponders and

Automatic Altitude
Reporting System

18A B 2 0 May be inoperative provided: |

a) Operations do not require its
use, and
b) Prior to flight, approval is
obtained from ATC facilities
having jurisdiction over
planned route of flight.

18B D 2 1 Any in excess of those required by |

14 CFR may be inoperative.

18-01 Elementary and A - 0 May be inoperative provided:

Enhanced Downlink a) Operations do not require its
Aircraft Reportable use, and
Parameters Not b) Repairs are made prior to
Required by 14 CFR completion of next heavy
maintenance visit.
18-02 ADS-B Out Extended
*** Squitter |

18-02A B - 0 (O) May be inoperative provided prior |

to flight, authorization is obtained |
from ATC facilities having jurisdiction |
over planned route of flight using an |
approved process. |

NOTE: Any ADS-B Out function that |

operates normally may be
used.

18-02B C - 1 One may be inoperative. |

18-02C D - 0 May be inoperative provided: |

a) Enroute operations do not |
require its use, and |
b) It is not required by 14 CFR. |

NOTE: Any ADS-B Out function that |

operates normally may be |
used. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

19 Instrument Comparator C - 0 May be inoperative provided

*** or Warning System approach minimums do not require its
(-200/-300/-400/-500, use.
Includes
STC ST03355AT)

20 Radio Altimeter Systems

20-01 Receiver/Transmitters

20-01-01 (-100/-200)

20-01-01A A - 0 (M)(O) May be inoperative

deactivated provided:
a) Approach minimums or
operating procedures do not
require its use,
b) Associated autopilot is not
used for approach and
landing,
c) Autothrottle is not used for
approach and landing, and
d) Repairs are made within
2 flight-days.

20-01-01B C - 0 (M)(O) May be inoperative

deactivated provided:
a) Approach minimums or
operating procedures do not
require its use,
b) Associated autopilot is not
used for approach and
landing,
c) Autothrottle is not used for
approach and landing, and
d) GPWS is not required by
14 CFR.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

20 Radio Altimeter Systems

(Cont’d)

20-01 Receiver/Transmitters
(Cont’d)

20-01-02 (-300/-400/-500)

20-01-02A C 2 1 (M)(O) May be inoperative

deactivated provided:
a) Approach minimums or
operating procedures do not
require its use,
b) Associated autopilot is not
used for approach and
landing,
c) Autothrottle is not used for
approach and landing,
d) Associated flight director is
not used for approach and
landing, and
e) GPWS operates normally.

20-01-02B A 2 1 (M)(O) May be inoperative

deactivated provided:
a) Approach minimums or
operating procedures do not
require its use,
b) Associated autopilot is not
used for approach and
landing,
c) Autothrottle is not used for
approach and landing,
d) Associated flight director is
not used for approach and
landing, and
e) Repairs are made within
2 flight-days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

20 Radio Altimeter Systems

(Cont’d)

20-01 Receiver/Transmitters
(Cont’d)

20-01-03 (-600/-700/-800/ C 2 1 (M)(O) May be inoperative

-900/-900ER) deactivated provided:
a) Approach minimums or
operating procedures do not
require its use,
b) Associated autopilot is not
used for approach and
landing,
c) Autothrottle is not used for
approach and landing, and
d) Associated flight director is
not used for approach and
landing.

NOTE: If arming LNAV on ground |

with one radio altimeter |
inoperative, the flight directors |
and autopilot should be |
controlled by the FCC on the |
same side as the valid radio |
altimeter (i.e., the first flight |
director and/or autopilot to be |
engaged must be receiving |
valid radio altitude data). |
20-02 Indications

20-02A C - 2 May be inoperative provided:

a) Independent radio altimeters
operate normally for both
flightcrew members, and
b) Approach minimums do not
require their use.

20-02B C - 0 (M)(O) May be inoperative provided:

a) Associated
receiver/transmitter is verified
to operate normally, and
b) Approach minimums or
operating procedures do not
require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

21 Air Data System A - 0 (O) May be inoperative provided:

*** (Non Electric Airspeed a) Dispatch deviations for
Indicators associated equipment are
(-200) observed,
b) All associated equipment is
listed in this column of each
operator’s MEL, and
c) Repairs are made within
3 flight-days.

22 Alternate Static System C 1 0 May be inoperative provided

(-100/-200) pneumatic airspeed and altimeters
are installed and operating at both
pilot stations.

23 True Airspeed Indication C - 0

***
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

25 Altitude Alerting System A 1 0 (O) May be inoperative provided:

a) Autopilot with altitude hold
and altitude capture operates
normally,
b) Enroute operations (i.e.,
RVSM) do not require its use,
c) Airplane does not depart from
a designated airport (as listed
in the operator’s MEL) where
repair or replacement can be
made, and
d) Repairs are made within
3 flight-days.

25-01 Aural Alert C - 0 May be inoperative provided:

a) Visual alert operates normally,
and
b) Autopilot with altitude hold
and altitude capture operates
normally.

25-02 Visual Alert C - 0 May be inoperative provided:

a) Aural alert operates normally,
and
b) Autopilot with altitude hold
and altitude capture operates
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

26 Terrain Awareness and

Warning System (TAWS)
(Includes
STC ST03355AT and
ST03362AT)

26-01 Ground Proximity A 1 0 (O) May be inoperative provided:

Warning System a) Alternate procedures are
(GPWS) established and used, and
b) Repairs and made within
2 flight-days.

26-01-01 Modes 1 thru 4 A 4 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Repairs are made within
2 flight-days.

26-01-02 Test Mode A 1 0 May be inoperative provided:

a) GPWS is considered
inoperative, and
b) Repairs are made within
2 flight-days.

26-01-03 Glideslope Deviation(s)

(Mode 5)

26-01-03A C 2 1

26-01-03B B 2 0

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

26 Terrain Awareness and

Warning System (TAWS)
(Includes
STC ST03355AT and
ST03362AT)
(Cont’d)

26-01 Ground Proximity

Warning System
(GPWS)
(Cont’d)

26-01-04 Advisory Callouts

26-01-04A B - 0 (O) May be inoperative provided

alternate procedures are established
and used.

26-01-04B C - 0 (O) May be inoperative provided:

a) Advisory callout not required
by 14 CFR, and
b) Alternate procedures are
established and used.
26-01-05 Windshear Warning and
*** Flight Guidance Mode
(Reactive)

26-01-05A B 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Operator’s alternate

procedures should include
reviewing windshear
avoidance and windshear
recovery procedures.

26-01-05B C 1 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Windshear Detection and
Avoidance System
(Predictive) operates
normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

26 Terrain Awareness and

Warning System (TAWS)
(Includes
STC ST03355AT and
ST03362AT)
(Cont’d)

26-02 Terrain System - B 1 0 (O) May be inoperative provided

Forward Looking Terrain alternate procedures are established
Avoidance (FLTA) and and used.
Premature Descent Alert
(PDA) Functions

26-03 Terrain Displays

26-03A C - 1

26-03B B - 0

26-03-01 Vision One D - 0

*** (STC ST03355AT)

26-04 Runway Awareness and C 1 0

*** Advisory System (RAAS)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-20
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

27 Long Range Navigation C - O As required by 14 CFR.

*** Systems
(INS, Loran, Omega)

28 Performance Data C 1 0
*** Computer System
(PDCS)

29 Speed Command C 2 0
*** (Fast-Slow) Indicators
(-100/-200/-300/
-400/-500)

30 ADI Test C 2 0
*** (-100/-200/-300/
-400/-500)

31 Speed Cursor Remote C 1 0

*** Drive (-100/-200/-300/ |
-400/-500) |

32 Instrument Transfer C 1 0 (O) May be inoperative provided:

Switching System a) Associated instruments
operate normally from isolated
sources, and
b) Inoperative switches are not
moved during flight.

33 Vertical Gyro System

(-100/-200)

33-01 Number 1 and 2 C 2 1 One may be inoperative provided:

a) Auxiliary vertical gyro
operates normally, and
b) Vertical gyro switch is
selected to auxiliary position.

33-02 Auxiliary Gyro C 1 0

***
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-21
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

35 Inertial Reference B 2 1 (O) Except for ER operations, one

Systems (IRS) may be inoperative provided:
(-300/-400/-500/-600/ a) Remaining IRS operates
-700/-800/-900/-900ER) normally and is used for both
Attitude Indications and both
HSIs,
b) Flight is restricted to day
VMC,
c) Standby Magnetic Compass
operates normally,
d) Standby Horizon Indicator or
ISFD attitude display operates
normally,
e) Both Vertical Speed
Indications are switched to
remaining IRS, if required,
and
f) Autopilots (any mode) are not
used unless SB-737-22-1140
or equivalent is incorporated.

35-01 IRS Data Display C 1 0 May be inoperative provided one

(Aft Overhead Panel) FMCS CDU operates normally.

35-02 HSI Ground Speed C 2 0 May be inoperative provided IRS

Display Data Display operates normally.
(Non-EFIS -300/
-400/-500)

35-03 IRS Ground Crew Call C 1 0

Horn

36 Flight Management
Computer System
(FMCS)

36-01 (-200 CMA-900 D 1 0 (M) May be inoperative provided FMS

*** FMS/GPS) is deactivated.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-22
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-01 (-200 CMA-900

*** FMS/GPS)
(Cont’d)

36-01-01 Annunciator C 9 0 (M) May be inoperative provided FMS

Lights/Switches is deactivated.
(STC ST6895-AT)

36-01-01-01 NAV/FMS

36-01-01-01A D 2 0 May be inoperative provided FMS is

considered inoperative.

36-01-01-01B A 2 1 May be inoperative on non-flying

pilot’s side provided:
a) Captain’s HDG/NAV light and
switch operate normally, and
b) Repairs are made within
3 flight-days.
36-01-01-02 WPT

36-01-01-02A C 2 0 May be inoperative provided

procedures do not require its use.

36-01-01-02B A 2 1 May be inoperative on non-flying

pilot’s side provided repairs are made
within 3 flight-days.
36-01-01-03 GPS APPR CAP

36-01-01-03A C 1 0 May be inoperative provided

procedures do not require its use.

36-01-01-03B C 1 0 May be inoperative provided:

a) FMS-DME is operational, and
b) Area of flight has adequate
DME coverage (minimum of
three DME stations in range
at all times).

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-23
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-01 (-200 CMA-900

*** FMS/GPS)
(Cont’d)

36-01-01 Annunciator
Lights/Switches
(STC ST6895-AT)
(Cont’d)

36-01-01-04 GPS INT

36-01-01-04A C 2 0 May be inoperative provided

procedures do not require its use.

36-01-01-04B A 2 1 May be inoperative on non-flying

pilot’s side provided repairs are made
within 3 flight-days.

36-01-01-05 OFFSET C 2 0 May be inoperative provided

procedures do not require its use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-24
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-01 (-200 CMA-900

*** FMS/GPS)
(Cont’d)

36-01-02 FMU C - 1 May be inoperative provided unit is

not required to meet 14 CFR
navigation requirements.

36-01-03 MCDU C 1 0 May be inoperative provided unit is

not required to meet 14 CFR
navigation requirements.

36-01-04 Navigation Databases A - 0 May be inoperative provided:

a) Operations do not require its
use,
b) It is not used in a primary
navigation system required by
14 CFR,
c) Alternate procedures are
developed and used,
d) The ICAO Flight Plan is
updated (as required) to notify
ATC of the navigation
equipment status of the
aircraft, and
e) It is repaired within
10 flight-days.

NOTE: An out-of-currency or
out-of-date navigation
database is not authorized
MMEL relief per 14 CFR.
36-01-05 DME

36-01-05A C 1 0 Any in excess of those required by

14 CFR may be inoperative.

36-01-05B C 1 0 May be inoperative provided GPS is

operational.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-25
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-01 (-200 CMA-900

*** FMS/GPS)
(Cont’d)

36-01-06 GPS

36-01-06A C 1 0 May be inoperative provided all

navigation is based on
ILS/VOR/DME.

36-01-06B C 1 0 May be inoperative provided:

a) FMS-DME is operational, and
b) Area of flight has adequate
DME coverage (minimum of
three DME stations in range
at all times).

36-01-07 HSI Switching Unit

(STC ST01676AT)

36-01-07A C 2 0 May be inoperative provided FMS is

considered inoperative.

36-01-07B C 2 1

36-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)

36-02-01 FMC Alert Lights

36-02-01A C 2 1 One may be inoperative provided

FMC is not used for autopilot
guidance during approach.

36-02-01B C 2 0 May be inoperative provided FMC is

not used for autopilot guidance.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-26
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Cont’d)

36-02-02 Computer C - 1 May be inoperative provided it is not

required to meet 14 CFR navigation
requirements.

36-02-02-01 -300/-400/-500 C - 0 Except for ER operations, may be

inoperative provided:
a) IRS display unit (on aft
overhead panel) operates
normally, and
b) EFIS speed tapes are not
used as primary airspeed
indication.

36-02-02-02 -600/-700/-800/-900/ C - 0 (M) Except for ER operations, may be |

-900ER inoperative provided:
a) IRS display unit (on aft
overhead panel) operates
normally, |
b) Speed Reference Selector
operates normally, and |
c) Autothrottle system is |
deactivated and considered |
inoperative. |

NOTE: Refer to MMEL Item 22-04 |

(Autothrottle System) |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-27
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Cont’d)

36-02-03 CDU/MCDU
***

36-02-03A C - 1 May be inoperative provided enroute

procedures do not require its use.

36-02-03B C - 0 Except for ER operations, may be

inoperative provided:
a) IRS display unit (on aft
overhead panel) operates
normally, and
b) Unit is not required to meet
14 CFR navigation
requirements.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-28
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Cont’d)

36-02-04 Alternate Navigation

*** Control Display Unit
(ANCDU)

36-02-04-01 CRT ANCDU C - 0 May be inoperative provided:

(-300/-400/-500) a) IRS data display (on aft
overhead panel) operates
normally, and
b) Unit is not required to meet
14 CFR navigation
requirements.

NOTE: Two independent navigation

systems are required for
operations beyond range of
radio navigation aids. Requires
dual ANCDU or ANCDU and
CDU/Computer or dual
CDU/Computers.

36-02-04-02 LCD ANCDU C - 0 May be inoperative provided it is not

(-700IGW) required to meet 14 CFR navigation
requirements.

NOTE: Two independent navigation

systems are required for
operations beyond range of
radio navigation aids. Requires
dual CDU/Computers, or one
GPS capable Multimode
Receiver with onside LCD
Alternate Nav CDU (ANCDU)
and Electronic Standby Attitude
Indicator (ESAI), in conjunction
with one Inertial Reference
System (IRS), and one
CDU/Computer.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-29
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Cont’d)

36-02-05 Navigation Databases A - 0 May be inoperative provided:

a) Operations do not require its
use,
b) It is not used in a primary
navigation system required by
14 CFR,
c) Alternate procedures are
developed and used,
d) The ICAO Flight Plan is
updated (as required) to notify
ATC of the navigation
equipment status of the
aircraft, and
e) It is repaired within
10 flight-days.

NOTE: An out-of-currency or
out-of-date navigation
database is not authorized
MMEL relief per 14 CFR.

36-02-06 HSI Miles to Waypoint C 2 0 May be inoperative provided

Display procedures do not require its use.
(Non-EFIS-300/-400/
-500)

36-03 Universal Avionics C 2 0 May be inoperative provided it is not

*** UNS-1F required to meet 14 CFR navigation
(STC ST03356AT and requirements.
ST03362AT)

36-03-01 Navigation Computer C 2 0 May be inoperative provided it is not

Unit (NCU) required to meet 14 CFR navigation
requirements.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-30
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-03 Universal Avionics

*** UNS-1F
(STC ST03356AT and
ST03362AT)
(Cont’d)

36-03-02 Control Display Unit C 2 0 Except for ER operations, may be

(CDU) inoperative provided:
(-300) a) IRS display unit (on aft
overhead panel) operates
normally, and
b) Unit is not required to meet
14 CFR navigation
requirements.

36-03-03 Global Navigation C 2 0 May be inoperative provided all

Satellite System (GNSS) navigation is based on
ILS/VOR/DME.

36-03-04 Navigation Display (ND) C 2 1 May be inoperative provided:

Caution Annunciator a) Data Block operates normally
Data Block on flying pilot’s ND, and
(FMS Alerts) b) FMC is not used for autopilot
(-300) guidance during approach.

NOTE: Requires installation of

Universal Avionics EFI-890
Display, STC ST03355AT.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-31
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-03 Universal Avionics

*** UNS-1F
(STC ST03356AT and
ST03362AT)
(Cont’d)

36-03-05 ND Flight Plan Status C 2 1 May be inoperative on non-flying

Block pilot’s ND.
(-300)
NOTE: Requires installation of
Universal Avionics EFI-890
Display, STC ST03355AT.

36-03-06 Navigation Databases A - 0 May be inoperative provided:

a) Operations do not require its
use,
b) It is not used in a primary
navigation system required by
14 CFR,
c) Alternate procedures are
developed and used,
d) The ICAO Flight Plan is
updated (as required) to notify
ATC of the navigation
equipment status of the
aircraft, and
e) It is repaired within
10 flight-days.

NOTE: An out-of-currency or
out-of-date navigation
database is not authorized
MMEL relief per 14 CFR.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-32
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

36 Flight Management
Computer System
(FMCS)
(Cont’d)

36-04 Innovative Solutions and

*** Support FMS
(STCST03272CH)
(-400)

36-04-01 Advanced Navigation - C 2 1 One may be inoperative provided

Multipurpose Control offside AN-MCDU is available for
Display Unit manual selection.
(AN-MCDU)

36-04-02 Global Positioning C 2 0 One or both may be inoperative

System (GPS) provided operations and procedures
do not require GPS use.

37 Windshear Warning and

*** Flight Guidance System
(Reactive)

37A B 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Operator’s alternate

procedures should include
reviewing windshear
avoidance and windshear
recovery procedures.

37B C - 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Windshear Detection and
Avoidance System
(Predictive) operates
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-33
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

38 Pitch Limit Indication C 2 0

*** (PLI)
|
40 Traffic Collision and
Avoidance System
(TCAS)
(Includes
STC ST03355AT and
ST03362AT)

40A B - 0 (M) May be inoperative provided:

a) System is deactivated and
secured, and
b) Enroute or approach
procedures do not require its
use.

40B C - 0 (M) May be inoperative provided:

a) Not required by 14 CFR,
b) System is deactivated and
secured, and
c) Enroute or approach
procedures do not require its
use.

40-01 Combined Traffic Alert C 2 1 May be inoperative on non-flying pilot

*** (TA) and Resolution side provided:
Advisory (RA) Dual a) TA and RA visual display is
Display operative on flying pilot side,
and
b) TA and RA audio function is
operative on flying pilot side.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-34
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

40 Traffic Collision and

Avoidance System
(TCAS)
(Includes
STC ST03355AT and
ST03362AT)
(Cont’d)

40-02 Resolution Advisory (RA)

Display System(s)

40-02A C 2 1 May be inoperative on non-flying pilot

side.

40-02B C - 0 (O) May be inoperative provided:

a) Traffic Alert (TA) visual
display and audio functions
are operative,
b) TA only mode is selected by
crew, and
c) Enroute or approach
procedures do not require its
use.

40-03 Traffic Alert (TA) Display C - 0 (O) May be inoperative provided:

System(s) a) RA visual display and audio
functions are operative, and
b) Enroute or approach
procedures do not require its
use.

40-04 Audio Functions B 1 0 May be inoperative provided enroute

or approach procedures do not
require use of TCAS.

40-05 Airspace Selection C - 0

*** Function

41 Engine Pressure Ratio C 1 0

*** Limit (EPRL) System
(-100/-200)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-35
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

42 Radio Magnetic
Indicators (RMI)

42-01 (-100/-200) C - 1 May be inoperative provided affected

RMI is not a source of heading data
for Horizontal Situation Indicator
(HSI).

42-02 (-300/-400/-500) C - 1

42-03 (-600/-700/-800/
-900/-900ER)

42-03-01 EFIS/Map C 3 1 Two may be inoperative provided

Captain’s RMI or Standby RMI
operates normally.

42-03-02 PFD/ND C 1 0 Standby RMI may be inoperative

*** provided Captain’s Inboard DU is
connected to Standby Power.

43 Radio Height Alert D 2 0

***

44 Head-Up Display D - 0 May be inoperative provided

*** System (HUD) procedures do not require its use.

NOTE: Any mode which operates

normally may be used.

45 Global Positioning
*** System (GPS)

45A C - 0 May be inoperative provided alternate

procedures are established and used.

45B D - 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-36
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

46 Microwave Landing D - 0 May be inoperative provided

*** System (MLS) approach procedures do not require
its use.

47 ILS Beam Deviation C 2 0 May be inoperative provided

*** Lights approach minimums do not require
their use.

48 EFIS Control Panel

48-01 Map Switches

*** (-300/-400/-500)

48-01-01 VOR/ADF C 2 1

48-01-02 NAV AID C 2 1

48-01-03 ARPT C 2 1

48-01-04 RTE DATA C 2 1

48-01-05 WPT C 2 1

48-02 Decision Height C 2 0 May be inoperative provided:

*** Reference (DH REF) a) Approach procedures do not
Indication require its use, and
(-300/-400/-500) b) Decision height is displayed
on both EADIs.

48-03 Decision Height/Mins C 2 0 May be inoperative provided

*** Selector approach procedures do not require
(-300/-400/-500/-600/ its use.
-700/-800/-900/-900ER)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-37
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

48 EFIS Control Panel

(Cont’d)

48-04 Map Switches

(-600/-700/-800/
-900/-900ER)

48-04-01 POS C 2 1

48-04-02 STA C 2 1

48-04-03 ARPT C 2 1

48-04-04 DATA C 2 1

48-04-05 WPT C 2 1

49 Right IRS DC Power B 1 0 (O) May be inoperative provided:

Supply System a) Remaining IRS Mode Selector
(-300/-400/-500/-600/ Unit lights are not illuminated,
-700/-800/-900/-900ER) and
b) Autopilot dual channel mode
is not used during approach.
|
51 Metric Altimeter D - 0 May be inoperative provided
*** operations do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-38
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

52 Performance C - 0 (O) May be inoperative provided:

*** Management System a) TAT Indicator operates
(PMS) with Windshear normally,
Detection/Alerting b) PMS remains uncoupled from
System autopilot,
(STC SA2018NM) c) Autothrottle system is
considered inoperative, and
d) Windshear Detection and
Guidance is considered
inoperative.

53 Automatic Dependent D - 0 May be inoperative provided it is not

*** Surveillance-Broadcast required by 14 CFR.
(ADS-B) System
NOTE: If ADS-B is installed in lieu of
or as a replacement for
14 CFR required equipment,
repair category in operator’s
MEL will be same as that of
14 CFR required equipment.

53-01 Cockpit Display and D - 0 NOTE: Cockpit Display Traffic

Traffic Information Information (CDTI) display of
(CDTI) data from other aircraft
systems may be used.

53-02 CDTI Control Panel D - 0 May be inoperative provided:

a) Flight ID can be set, and
b) Screen display is acceptable
to flightcrew.

53-03 Data Link Transmitter(s) D - 0 NOTE: In some aircraft, the Data Link
Transmission is an integral
part of the transponder, and
relief is provided in that
section.

53-04 Data Link Receivers D - 0

53-05 ADS-B Applications D - 0

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-39
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

54 Integrated Standby
*** Systems

54-01 Integrated Standby

Flight Display (ISFD)

54-01-01 Attitude Display B 1 0 May be inoperative provided:

a) Operations are conducted in
Day VMC only, and
b) Operations are not conducted
into known or forecast
over-the-top conditions.

54-01-02 ILS Indication D 1 0

54-01-03 Heading Display C 1 0

54-01-04 Metric Altimeter Display D 1 0 May be inoperative provided

operations do not require its use.

54-01-05 Dedicated Battery C 1 0

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-40
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

54 Integrated Standby
*** Systems
(Cont’d)

54-02 Integrated Standby

Instrument System (ISIS)
(Boeing
SB 737-31-1435)

54-02-01 Attitude Display B 1 0 May be inoperative provided:

a) Operations are conducted in
Day VMC only, and
b) Operations are not conducted
into known or forecast
over-the-top conditions.

54-02-02 ILS Indication D 1 0

54-02-03 Heading Display C 1 0

54-02-04 Metric Altimeter Display D 1 0 May be inoperative provided

operations do not require its use.

54-02-05 Dedicated Battery C 1 0

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-41
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

54 Integrated Standby
*** Systems
(Cont’d)

54-03 Electronic Standby

Instrument System
(ESIS)
(STC ST03125NY)
(-300/-400/-500 Series)

54-03-01 Attitude Display B 1 0 May be inoperative provided:

a) Operations are conducted in
Day VMC only, and
b) Operations are not conducted
into known or forecast
over-the-top conditions.

54-03-02 Heading Display C 1 0

54-03-03 VOR/ILS Indications C 1 0 May be inoperative provided

procedures do not require its use.

55 Vertical Situation Display

*** (VSD) System
(-600/-700/-800/
-900/-900ER)

55A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

55B D 1 0 May be inoperative provided

procedures do not require its use.

56 Global Navigation D 2 - May be inoperative provided

*** Satellite Landing System approach minimums do not require its
(GLS) use.
(-600/-700/-800/
-900/-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 34-42
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
34. Navigation
Change
Sequence No. Item 1 2 3 4 Bar

57 Enhanced Vision D - 0 (M) May be inoperative provided EVS

*** System (EVS) is deactivated.
STC ST00039MC
NOTE: For the EVS to be considered
operative, the EVS Yoke
Switch must be operative.

57-01 EVS Window Heat D - 0 (O) Avoid using EVS in known or

forecasted icing conditions.

57-02 Secondary (Non-HUD) D - 0 (M) May be inoperative provided

EVS Display System procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 35-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
35. Oxygen
Change
Sequence No. Item 1 2 3 4 Bar

|
02 Passenger Service Units B - - (M) May be inoperative provided:
(PSUs) a) Associated seats are blocked
and placarded to prevent
occupancy, and
b) Units operate normally for all
usable lavatory and flight
attendant locations.

02-01 Automatic Presentation C 1 0 (M)(O) May be inoperative provided:

a) Alternate deployment system
is verified to operate normally,
and
b) Airplane remains at or below
FL 300.

02-02 Door Latches B - - (M) Automatic opening feature of

door latch(es) may be inoperative
unlatched and taped closed provided:
a) PSU oxygen system operates
normally,
b) Flight remains at or below
FL 250, and
c) Passenger(s) occupying
seat(s) with inoperative door
latch(es) are briefed on
oxygen mask procedure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 35-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
35. Oxygen
Change
Sequence No. Item 1 2 3 4 Bar

03 Oxygen Pressure
Indicators

03-01 Flight Deck Crew C 1 0 (M) May be inoperative provided an

Oxygen Indicator alternate procedure is used to verify
that oxygen supply is above minimum
requirements for dispatch.

03-02 External Service Panel C 1 0 (M) May be inoperative provided an

*** Crew Oxygen Indicator alternate procedure is used to verify
that oxygen supply is above minimum
requirements for dispatch.

03-03 Flight Deck Passenger C 1 0 (M) May be inoperative provided an

Oxygen Indicator alternate procedure is used to verify
(-100/-200) that oxygen supply is above minimum
requirements for dispatch.

03-04 Flight Deck C 1 0 (M) May be inoperative provided an

Crew/Passenger Oxygen alternate procedure is used to verify
Indicator that oxygen supply is above minimum
(-600/-700/-800, requirements for dispatch.
-900/-900ER)

03-05 Overpressure Discharge C - 0 (O) May be damaged or missing. |

Indication Disk
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 35-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
35. Oxygen
Change
Sequence No. Item 1 2 3 4 Bar

04 Portable Oxygen Bottles D - - Any in excess of those required by |

or Units (Including 14 CFR may be inoperative or |
Masks and Hoses) removed provided: |
a) An inoperative or not properly |
serviced portable oxygen |
bottle/unit remains in a |
certified location until |
removed or serviced at the |
next suitable maintenance |
facility, |
b) Location placarding is |
removed or obscured, and |
c) Required distribution is |
maintained. |

NOTE 1: Inoperative portable oxygen |

bottles or units, removed |
from a certified location or |
removed from the aircraft, |
are subject to 49 CFR |
dangerous goods |
regulations. |

NOTE 2: Medical equipment installed |

in the aircraft as part of an |
EMS operation is not |
considered part of the |
normal complement of |
equipment. No MMEL relief |
applies to that equipment |
and 14 CFR maintenance |
and inspection |
requirements do not apply. |

04-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper installation |
and servicing is verified at each |
preflight. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 35-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
35. Oxygen
Change
Sequence No. Item 1 2 3 4 Bar

05 Passenger Oxygen
System

05A B 1 0 (M)(O) May be inoperative provided:

a) Flight is not conducted where
minimum enroute altitude is
above 14,000 ft. MSL,
b) Both air conditioning packs
operate normally,
c) Remaining components of
pressurization system operate
normally,
d) Airplane remains at or below
FL 250,
e) Portable oxygen units are
provided for 10% of
passengers, and
f) Passengers are appropriately
briefed.

05B C 1 0 May be inoperative for all-cargo

configuration.

05C B 1 0 May be inoperative provided flight is

conducted at or below 10,000 ft. MSL.

05D Supernumerary Oxygen C - 0 May be inoperative provided

Masks associated seat is not occupied.
(-800BCF and
ST02556SE)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 35-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
35. Oxygen
Change
Sequence No. Item 1 2 3 4 Bar

06 Portable Protective D - - Any in excess of those required by

Breathing Equipment 14 CFR may be inoperative or
(PBE) removed provided: |
a) Inoperative PBE remains in a |
certified location until |
removed from the aircraft at |
the next suitable maintenance |
facility, |
b) Location placarding is
removed or obscured, and
c) Required distribution is
maintained.

NOTE: Inoperative PBEs, removed

from a certified location, or
removed from the aircraft, are
subject to 49 CFR dangerous
goods regulations.

06-01 Tamper Seals or Tags C - - (O) May be inoperative, damaged, or |

*** missing provided proper installation |
and operation is verified at each |
preflight. |

07 External Service Panel, C 1 0 (M) May be inoperative provided

*** Oxygen Fill Station leak-tight integrity of oxygen supply
system is not affected.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 36-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
36. Pneumatic
Change
Sequence No. Item 1 2 3 4 Bar

01 Manifold Isolation
Shutoff Valve

01-01 (-100/-200) C 1 0 (M) May be inoperative provided:

a) Valve remains closed except
for engine start, and
b) Airplane is not operated in
known or forecast icing
conditions.

01-02 (-300/-400/-500) C 1 0 (M) May be inoperative provided:

a) Modified Main Engine controls
or production equivalent have
been installed,
b) Valve remains closed except
for engine start, and
c) Airplane is not operated in
known or forecast icing
conditions.

01-03 (-600/-700/-800/ C 1 0 (M) Except for ER operations beyond

-900/-900ER) 120 minutes, may be inoperative
provided:
a) Valve remains closed except
for engine start, and
b) Airplane is not operated in
known or forecast icing
conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 36-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
36. Pneumatic
Change
Sequence No. Item 1 2 3 4 Bar

02 Ground Pneumatic
Connector Check Valve

02A C 1 0 (M)(O) Except for ER operations

beyond 120 minutes, may be
inoperative open provided:
a) Right pneumatic manifold
remains depressurized after
starting right engine,
b) Airplane is not operated in
known or forecast icing
conditions, and
c) Altitude remains at or below
FL 250.

02B C 1 0 May be inoperative closed.

03 Precooler Control Valves

03-01 (-100/-200) C 2 0 (M)(O) May be inoperative provided:

a) Associated engine bleed
shutoff valve remains closed
after engine start, and
b) Airplane is not operated in
known or forecast icing
conditions.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 36-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
36. Pneumatic
Change
Sequence No. Item 1 2 3 4 Bar

03 Precooler Control Valves

(Cont’d)

03-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)

03-02A C 2 0 (O) Except for ER operations beyond

120 minutes, may be inoperative in
any position provided:
a) Associated engine bleed
shutoff valve remains closed,
and
b) Airplane is not operated in
known or forecast icing
conditions.

03-02B C 2 0 (M)(O) Except for ER operations

beyond 120 minutes, may be
inoperative full open provided:
a) Airplane is not operated in
known or forecast icing
conditions, and
b) Appropriate performance
adjustments are applied.

04 Pneumatic Pressure C 2 0 (O) May be inoperative provided

Indication Systems alternate procedures are established
and used.

05 Engine Bleed Air Shutoff

Valves (PRSOV)

05-01 (-100/-200) C 2 0 (M)(O) May be inoperative provided:

a) Valve is secured closed after
engine start, and
b) Airplane is not operated in
known or forecast icing
conditions.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 36-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
36. Pneumatic
Change
Sequence No. Item 1 2 3 4 Bar

05 Engine Bleed Air Shutoff

Valves (PRSOV)
(Cont’d)

05-02 (-300/-400/-500/-600/ |
-700/-800/-900/-900ER)

05-02A C 2 1 (M)(O) Except for ER operations |

beyond 120 minutes, may be |
inoperative provided: |
a) Valve is secured closed |
before engine start, |
b) Airplane is not operated in |
known or forecast icing |
conditions, and |
c) Flight altitude remains at or |
below FL 250. |

05-02B C 2 0 (M)(O) Except for ER operations |

beyond 120 minutes, may be |
inoperative provided: |
a) Valves are secured closed |
before engine start, |
b) Airplane is not operated in |
known or forecast icing |
conditions, |
c) APU bleed air system |
operates normally, and |
d) Flight altitude remains at or |
below 17,000ft. |

06 Dual Bleed Light System C 1 0 (O) May be inoperative provided:

a) APU bleed air is not used in
flight, and
b) APU bleed valve is verified
closed before each departure.

07 13th Stage Bleed Air C 2 0 (M) May be inoperative provided

Modulating and Shutoff airplane is not operated in known or
Valves forecast icing conditions.
(-100/-200)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 36-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
36. Pneumatic
Change
Sequence No. Item 1 2 3 4 Bar

08 Engine Bleed Trip Off C 2 0 (O) Except for ER operations beyond

Lights 120 minutes, may be inoperative
provided:
a) Associated engine bleed is
not used except for engine
start, and
b) Airplane is not operated in
known or forecast icing
conditions.

09 High Stage Valves C 2 1 (M) One may be inoperative locked

(-300/-400/-500/-600/ closed provided a minimum of 60%
-700/-800/-900/-900ER) N1 is maintained on associated
engine during flight in icing
conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 38-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
38. Water/Waste
Change
Sequence No. Item 1 2 3 4 Bar

01 Potable Water Systems

01A C - - (M) Individual components may be

inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system
components are verified not to
have leaks.

NOTE: Any portion of system which

operates normally may be
used.

01B C - - (M) May be inoperative provided:

a) System is drained, and
b) Procedures are established to
ensure that system is not
serviced.

02 Lavatory Waste Systems |

02A C - - (M) Individual components may be

inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system
components are verified not to
have leaks.

NOTE: Any portion of system which

operates normally may be
used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 38-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
38. Water/Waste
Change
Sequence No. Item 1 2 3 4 Bar

02 Lavatory Waste Systems

(Cont’d)

02B C - - (M) Associated lavatory system(s)

may be inoperative provided:
a) Associated components are
deactivated or isolated to
prevent leaks, and
b) Associated lavatory door is |
secured closed and placarded
“INOPERATIVE –
DO NOT ENTER”.

NOTE: These provisions are not

intended to prohibit
inspections by crewmembers.

02-01 Vacuum Blower C 1 0 (M)(O) May be inoperative provided:

(-600/-700/-800/ a) Vacuum blower is
-900/-900ER) deactivated, and
b) Lavatories are not used on
the ground or at flight altitudes
below 16,000 ft.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 46-1
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
46. Information Systems
Change
Sequence No. Item 1 2 3 4 Bar

01 Electronic Flight Bag

*** (EFB) System

01-01 Class 3 EFBs

(Including Boeing)

01-01A C - 1

01-01B C - - (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Any function, program, or

document which operates
normally may be used.

01-01C D - 0 May be inoperative provided

procedures do not require its use.

01-02 (STC ST03165AT Only)

01-02A D 2 0 (M) May be inoperative provided

procedures do not require its use.

01-02B C 2 0 (M)(O) May be inoperative provided

alternate procedures are established
and used.

01-02-01 Mounting Cradle C 2 1 (M)(O) May be inoperative provided

alternate procedures are established
and used.

01-02-02 Liquid Crystal Display C 2 1 One may be inoperative provided

alternate source for required
information is available and used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 46-2
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
46. Information Systems
Change
Sequence No. Item 1 2 3 4 Bar

01 Electronic Flight Bag

*** (EFB) System
(Cont’d)

01-02 (STC ST03165AT Only)

(Cont’d)

01-02-03 Control Panel Module/ C 2 1 One may be inoperative provided

Peripheral Connectivity alternate source for required
Unit information is available and used.

01-02-03-01 ON/OFF Switch C 2 1 One may be inoperative in ON

position provided:
a) EFB Battery charging system
operates normally, and
b) Normal power to unit is
available and operates
normally.

01-02-04 Computer Processing C 2 1 One may be inoperative provided

Unit (CPU) alternate source for required
information is available and used.

01-02-04-01 Backup Battery C 2 1 One may be inoperative provided

normal power is available and
operates normally.

01-02-05 Standby Button

01-02-05A C 2 0 May be inoperative in operational

mode.

01-02-05B C 2 0 May be inoperative in Standby mode

provided display is considered
inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 46-3
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
46. Information Systems
Change
Sequence No. Item 1 2 3 4 Bar

01 Electronic Flight Bag

*** (EFB) System
(Cont’d)

01-03 Stowage/Charger
Assembly
(STC ST01118CH Only)

01-03-01 Class 1 EFB with All D 1 0 May be inoperative provided

Battery Types procedures do not require its use.

01-03-02 Class 1 EFB with Lithium C 1 0 (M)(O) May be inoperative provided

Ion Battery alternate procedures are established
and used.

NOTE: If a Class 1 EFB is to be

used, alternate procedures
must ensure the battery is
charged to a “sufficiently
charged” state at appropriate
time intervals.

01-04 Data Connectivity

(Class 2)

01-04A C - - (O) May be inoperative provided

alternate procedures are established
and used.

01-04B D - 0 May be inoperative provided

procedures do not require its use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 46-4
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
46. Information Systems
Change
Sequence No. Item 1 2 3 4 Bar

01 Electronic Flight Bag

*** (EFB) System
(Cont’d)

01-05 Power Supply/Power |

Connection |

01-05A C - - (O) May be inoperative provided

alternate procedures are established
and used.

01-05B D - - May be inoperative provided

procedures do not require its use.

01-06 Mounting Device

(Class 2)

01-06A C - - (M)(O) May be inoperative provided:

a) Associated EFB and
hardware is stowed, secured |
by an alternate means, or |
removed from the aircraft, and
b) Alternate procedures are
established and used.

01-06B D - - (M)(O) May be inoperative provided:

a) Associated EFB and
hardware is stowed, secured |
by an alternate means, or |
removed from the aircraft, and
b) Procedures do not require its
use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 46-5
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
46. Information Systems
Change
Sequence No. Item 1 2 3 4 Bar

01 Electronic Flight Bag

*** (EFB) System
(Cont’d)

01-07 STC ST02949CH Only

01-07A C 2 1

01-07B C 2 0 (O) May be inoperative provided

alternate procedures are established
and used.

01-07C D 2 0 May be inoperative provided

procedures do not require its use.

NOTE: Any function, program, or

document which operates
normally may be used.

01-07-01 Interface Unit C 1 0 (O) May be inoperative provided an

alternate source for required
information is available and used.

02 Onboard Network
*** System (ONS)
(-700/-800/
-900/-900ER)

02A C 1 0 (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Any function that operates

normally may be used.

02B D 1 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 55a PAGE NO. 47-1
DATE: 02/13/2012
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
47. Inert Gas System
Change
Sequence No. Item 1 2 3 4 Bar

01 Nitrogen Generation
*** System (NGS)
(All Models)

01 All Models A 1 0 (M) May be inoperative provided:

(Upon Incorporation of a) NGS shutoff valve is
Boeing Service Bulletin deactivated closed, and
737-47-1002, b) Repairs are made within
737-47-1003, 10 flight-days.
737-47-1004,
737-47-1005,
737-47-1006
737-47-1007,
737-47-1008, or
Production Equivalent)

01-01 Nitrogen Generation C 1 0

Degraded
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 49-1
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
49. Airborne Auxiliary Power
Change
Sequence No. Item 1 2 3 4 Bar

01 Auxiliary Power Unit C 1 0 Except for ER operations, may be

(APU) inoperative provided:
a) Procedures do not require its
use, and
b) Perform a visual inspection of
the tail cone area and the
adjacent control surfaces to
confirm that there is no
evidence of heat damage or
delamination.

02 APU Annunciator LOW C 2 0 May be inoperative provided APU

OIL PRESSURE and Auto Shutdown System operates
OVER SPEED Lights normally.

03 APU Auto Shutdown C 1 0 (M) Except for ER operations, may be

System inoperative provided:
(-100/-200/-300/ a) APU is not used in flight,
-400/-500) b) APU annunciator lights
operate normally, and
c) APU is monitored
continuously.

04 APU Annunciator LOW C 1 0 (M) May be inoperative and APU

OIL QUANTITY/MAINT used provided oil quantity is checked
Light once each flight-day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 49-2
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
49. Airborne Auxiliary Power
Change
Sequence No. Item 1 2 3 4 Bar

05 APU EGT Indicator

05-01 Model GTCP85-129 C 1 0 (O) Except for ER operations, may be

inoperative provided:
a) All warning and caution lights
operate normally,
b) APU is used to supply
electrical power and for
starting one engine only, and
c) Passengers are not permitted
on board until APU has been
shut down.

05-02 Model GTCP36-280, C 1 0

APS-2000, and
AS 131-9B

06 APU Inlet Door

06A C 1 0 (O) May be inoperative open.

06B C 1 0 (O) Except for ER operations, may be

inoperative in any other position if
APU is not used.

07 APU Bleed Air Valve

07A C 1 0 (M) May be inoperative closed.

NOTE: APU may be used to provide

electrical power.

07B C 1 0 (O) Except for ER operations, may be

inoperative provided:
a) APU bleed air check valve
operates normally, and
b) APU is not operated.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 49-3
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
49. Airborne Auxiliary Power
Change
Sequence No. Item 1 2 3 4 Bar

08 APU DC Fuel Boost D 1 0

*** Pump

09 APU Surge Control

System

09-01 Surge Bleed Valve

*** (Models GTCP85-129
and APS-2000)
(-100/-200/-300/
-400/-500)

09-01A C 1 0 May be inoperative in open position

provided APU bleed air is not used
for engine start on ground.

NOTE: Relief also applies to

airplanes modified by STC
SA5730NM or ST00131SE
provided APU is not operating
during approach.

09-01B C 1 0 May be inoperative in closed position

provided APU operation is limited to
FL 250 or below.

NOTE: Relief also applies to

airplanes modified by STC
SA5730NM or ST00131SE.

09-02 Surge Control Valve

(Model AS 131-9B)
(-600/-700/-800/
-900/-900ER)

09-02A C 1 0 May be inoperative in open position

provided APU bleed air is not used.

NOTE: APU may be used to provide

electrical power.

09-02B C 1 0 (O) Except for ER operations, may be

inoperative in closed position
provided APU is not used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 49-4
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
49. Airborne Auxiliary Power
Change
Sequence No. Item 1 2 3 4 Bar

10 APU Cockpit Hourmeter D 1 0

*** (-100/-200/-300/
-400/-500)

11 APU Start Counter D 1 0

*** Meter
(-100/-200/-300/
-400/-500)

12 APU Annunciator HIGH C 1 0

OIL TEMP/FAULT Light

13 APU Fuel Heater C 1 0 (M) May be inoperative provided APU

*** (-100/-200/-300/ operates normally.
-400/-500)

14 APU Flap Indicator

*** Interlock System
(-100/-200 Modified by
STC SA5730NM or
ST00131SE)

14A C 1 0 (O) May be inoperative provided:

a) Remaining APU surge bleed
valve is operating, and
b) APU bleed air is used during
approach.

14B C 1 0 (O) May be inoperative provided APU

is not operating during approach.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 49-5
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
49. Airborne Auxiliary Power
Change
Sequence No. Item 1 2 3 4 Bar

15 Start Power Unit C 1 0 (M) Except for ER operations, may be

(-600/-700/-800/ inoperative provided procedures do
-900/-900ER) not require use of APU.

15-01 AC/DC Start Systems C 2 1

16 Start Converter Unit C 1 0 (M) Except for ER operations, may be

(-600/-700/-800/ inoperative provided procedures do
-900/-900ER) not require use of APU.

16-01 Voltage Regulator C 1 0 Except for ER operations, may be

Function inoperative provided APU generator
is not used for electrical power.

NOTE: APU may be used as a

pneumatic source.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

01 Forward Air Stair D 1 0 NOTE: Any mode that operates

*** normally may be used.

02 Aft Air Stair

*** (-100/-200)

02A C 1 1 Electrical mode may be inoperative

provided door operates normally as
an emergency exit in passenger
configuration.

02B D 1 0 May be inoperative in all-cargo

configuration only.

03 Door Warning Light

System

03-01 Entry/Service/Cargo/ C - 0 (M) May be inoperative provided

Equipment/Airstair associated door is verified closed and
locked before each departure.

NOTE: On -600/-700/-800/-900/
-900ER, if two or more
entry/service door warning
lights are inoperative due to
failed door sensors, overwing
exit flight lock system and mid
exit flight lock system
(-900ER) will not function
properly. Refer to item 52-15.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

03 Door Warning Light

System
(Cont’d)

03-02 Overwing C - 0 (M) May be inoperative provided:

(-600/-700/-800/ a) Associated door is verified
-900/-900ER) closed and latched before
each departure, and
b) Associated flight lock is
verified to operate normally.

03-03 Cabin Door Indication C 1 0 (O) May be inoperative provided

System associated doors are verified in
(-800EF accordance with following prior to
STC ST02000NY Only) taxi, takeoff, and landing:
a) Entry Area/Main Lounge is
Open,
b) Private Bedroom is Closed,
c) Guest Lavatory is Closed, and
d) Aft Lounge/Galley is Open.

03-04 Mid-Exit C 1 0 (M) May be inoperative provided

*** (-900ER) associated door is verified closed and
latched before each departure.

04 Tire Burst Screen C 1 0 (M) May be inoperative provided:

*** Warning Light System a) Main wheel well screens are
(-100/-200/-300) inspected for security and
damage before each
departure, and
b) For combined Equipment/Tire
Burst Screen Warning Light,
visually verify that electronics
compartment and lower nose
compartment are secured and
locked, and main wheel well
screen is secured and
undamaged before each
departure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

05 Left Main Cabin Door

Pressure Stop Fittings

05-01 Aft Airstair Door and

Forward Entry Door

05-01A B - - (M)(O) One per door may be broken

or missing provided:
a) There are no visible defects
on other fittings for associated
door,
b) Pressure differential does not
exceed 6.0 psi, and
c) Analog cabin pressure control
system standby control mode
operates normally and STBY
is used.

05-01B B - - (M)(O) One per door may be broken

or missing provided:
a) There are no visible defects
on other fittings for associated
door,
b) Pressure differential does not
exceed 6.0 psi,
c) Digital cabin pressure control
system AUTO or ALTN
control mode operates
normally, and
d) Alternate procedures are
established and used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-4
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

05 Left Main Cabin Door

Pressure Stop Fittings
(Cont’d)

05-02 Aft Door without Airstairs

05-02A B - - (M)(O) One per door may be broken

or missing provided:
a) There are no visible defects
on other fittings for associated
door,
b) Pressure differential does not
exceed 3.4 psi, and
c) Analog cabin pressure control
system standby control mode
operates normally and STBY
is used.

05-02B B - - (M)(O) One per door may be broken

or missing provided:
a) There are no visible defects
on other fittings for associated
door,
b) Pressure differential does not
exceed 3.4 psi,
c) Digital cabin pressure control
system AUTO or ALTN
control mode operates
normally, and
d) Alternate procedures are
established and used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-5
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

06 Lower Cargo Doors

Pressure Stop Fittings

06-01 (All Models) A 24 22 (M) Any one may be broken or

missing on each door or frame
provided:
a) No defects are visible on
other fittings for associated
door,
b) Cabin pressure controller
AUTO mode operates
normally,
c) Adjacent stop fittings are
inspected within 25 flights,
and
d) Not more than 50 flights are
made before completion of
repairs or replacements.

06-02 (-100/-200/-300/-400/ C 24 20 (M)(O) Two may be broken or

-500/-900/-900ER) missing on each door or frame
provided airplane is operated in an
unpressurized configuration only.

06-03 (-600/-700/-800 Prior to C 24 20 (M)(O) Two may be broken or

Incorporation of Boeing missing on each door or frame
Service Bulletins provided airplane is operated in an
737-26-1121 and unpressurized configuration only.
737-26-1122, and either
737-21-1135 or
737-21-1163 or their
Production Equivalents)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-6
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

06 Lower Cargo Doors

Pressure Stop Fittings
(Cont’d)

06-04 (-600/-700/-800 C 24 20 (M)(O) Two may be broken or

All-Passenger missing on each door or frame
Configuration Upon provided:
Incorporation of Boeing a) Flight is conducted in an
Service Bulletins unpressurized configuration,
737-26-1121 and and
737-26-1122, and either b) Procedures are established
737-21-1135 or and used to ensure lower
737-21-1163 or their forward cargo compartment
Production Equivalents) remains empty or is verified to
contain only empty cargo
handling equipment, ballast
(ballast may be loaded in
ULDs), and/or Fly Away Kits.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

07 Entry/Service Door Hold- C - 0 May be inoperative for all-cargo

Open Latch Assemblies operations.

07-01 Latch Release Lever C - 0

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-7
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

08 Flight Deck Door Lock

*** System
(Not 14 CFR Part 25,
§ 25.795 Compliant)

08A C 1 0 (M) May be inoperative provided:

a) Door lock solenoid is
deactivated in locked position,
and
b) Door is verified to lock and
unlock manually.

08B C 1 0 May be inoperative provided

supplemental flight deck door security
device is installed and operates
normally.

08C D 1 0 May be inoperative provided all-cargo

operations are being conducted.

09 Lower Cargo Doors Door C 2 0 (M) May be inoperative provided a

Balance Mechanism safety hold open device is used when
door is in open position.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-8
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

10 Main Cabin Cargo Door

(PEMCO Aeroplex, Inc.
STC SA2969SO)

10-01 Latch Pin, Latch Base, A 8 7 (M)(O) One may be broken or

and Lower Jamb Latch missing from main cargo door
Fitting provided:
a) A visual check is made before
departure to ensure no
defects are visible on other
latch bases, pins, or lower
jamb latch fittings,
b) Latch pin and latch base of
damaged latch does not
interfere with continuous safe
operation of remaining latches
and pins,
c) Flight is conducted in an
unpressurized configuration,
d) Procedures are established
and used to ensure main and
lower lobe cargo
compartments remain empty
or are verified to contain only
empty cargo handling
equipment, ballast (ballast
may be loaded in ULDs),
and/or Fly Away Kits, and
e) Repairs are made within
2 flight-days.

NOTE: Operator MELs must define

which items are approved for
inclusion in Fly Away Kits and
which materials can be used
as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-9
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

10 Main Cabin Cargo Door

(PEMCO Aeroplex, Inc.
STC SA2969SO)
(Cont’d)

10-02 Hydraulic Cylinder

Latching Mechanism

10-02A B 2 1 (M) One may be inoperative provided

remaining latch cylinder is operative
through gear box.

10-02B C 2 0 (M) May be inoperative provided door

may be latched and unlatched
manually.

10-03 Hydraulic System B 1 0 (M) May be inoperative provided door

Control Valve may be locked and unlocked
manually.

10-04 Lifting Actuator B 2 0 (M) May be inoperative provided door

Assembly is verified latched and locked.

10-05 Double Piloted Check B 1 0 (M) May be inoperative provided door

Valve may be locked and unlocked
manually.

10-06 Lock, Lock Mount, and A 2 1 (M)(O) One may be inoperative

Locking Fittings provided:
a) No defects are visible on
remaining lock or lock mount
of associated door, and
b) Repairs are made within
2 flight-days.

10-07 Sequence Valves B 2 0 (M) May be inoperative provided door

is verified latched and locked.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-10
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

10 Main Cabin Cargo Door

(PEMCO Aeroplex, Inc.
STC SA2969SO)
(Cont’d)

10-08 Priority Valve B 1 0 (M) May be inoperative provided door

is verified latched and locked.

10-09 Hydraulic Lock Actuators C 2 0 (M) May be inoperative provided door

can be unlocked and unlatched
manually.

11 Main Cargo Door C 1 0 (M) May be inoperative provided door

Electrically Powered is closed, latched, and locked before
Hydraulic Pump each departure.
(Standalone Hydraulic
System Only)
(PEMCO Aeroplex, Inc.
STC SA2969SO)

12 Main Cargo Door C 1 0 (M) May be inoperative.

Hydraulic Hand Pump
(PEMCO F, QC, and
COMBI Models Only)

13 Main Cargo Door

Lift/Operating Systems

13-01 Electric and/or Manual

Mode
(-200C and
STC SA2969SO)

13-01A C - 1 One may be inoperative provided

remaining mode operates normally.

13-01B C - 0 (M) May be inoperative provided door

is verified closed and locked before
each departure.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-11
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

13 Main Cargo Door

Lift/Operating Systems
(Cont’d)

13-02 Electric Mode C 1 0 (M) May be inoperative provided

(-700C/-800BCF) manual mode is verified to operate
normally.

13-03 Hydroelectric and/or C 2 1 One may be inoperative provided

Manual Mode remaining mode operates normally.
(STCs ST01566LA,
ST00287AT,
ST01827LA,
ST01961SE, and
ST02556SE)

13-03-01 (STCs ST01566LA, C 2 0 (M) May be inoperative provided door

ST01961SE, and is verified closed, latched, and locked
ST02556SE) before each departure.

14 Lower Cargo Doors Hold

*** Open
Mechanism/Device

14A C 2 0 May be inoperative provided Door

Balance Mechanism operates
normally.

14B C 2 0 May be inoperative provided cargo

compartment remains empty.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-12
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

15 Flight Lock System

15-01 Overwing Exit C - 0 (M)(O) May be inoperative provided:

(-600/-700/-800/ a) For inoperative flight lock(s), |
-900/-900ER) inputs to associated flight |
deck indications are |
deactivated, |
b) Each affected exit is verified |
to be capable of being
unlatched and opened before
each departure, and
c) A person employed by |
operator is designated to
remain seated in passenger
seat nearest affected exit
when cabin differential
pressure is less than 4.0 psi.

15-02 Mid Exit C - 0 (M)(O) May be inoperative provided:

*** (-900ER) a) For inoperative flight lock(s), |
inputs to associated flight |
deck indications are |
deactivated, |
b) Each affected exit is verified |
to be capable of being
unlatched and opened before
each departure, and
c) A person employed by |
operator is designated to
remain seated in passenger
seat nearest affected exit
when cabin differential
pressure is less than 4.0 psi.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-13
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

16 Main Cabin Exit/Slide

(All-Cargo Configuration)

16A C - 0 All doors/slides in cargo area except

L1/R1 may be inoperative or slide
missing without restriction.

16B B - 1 L1 may be inoperative or slide

missing provided R1 operates
normally.

16C B - 1 R1 may be inoperative or slide

missing provided L1 operates
normally.

16D B - 0 May be inoperative or slide missing

provided:
a) Only essential crewmembers,
including official observer(s) in
observer seat(s), are allowed
on the flight, and
b) An alternate means of egress
is available.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-14
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

17 Boeing/C&D Aerospace C 1 0 (M)(O) May be inoperative provided:

*** Enhanced Flight Deck a) Automatic locking system is
Security Door Automatic deactivated,
Locking System b) Door dead bolt operates
(14 CFR Part 25, normally and is used to lock
§ 25.795 Compliant) door, and
c) Alternate procedures are
established and used for
locking and unlocking door
using dead bolt.

17-01 Flight Deck Access C 1 0 (M)(O) May be inoperative provided:

Panel System a) Keypad is deactivated, and
(Keypad, Door Chime) b) Alternate procedures are
established and used.

17-01-01 LEDs C 3 0 (O) May be inoperative provided

alternate procedures are established
and used.

17-01-02 Door Bell Mode C 1 0 (O) May be inoperative provided

*** alternate procedures are established
and used.

17-01-03 Switch Guard C 1 0 May be inoperative or missing

provided flight deck door LOCK FAIL
light operates normally.

17-02 Flight Deck Door LOCK C 1 0 (M) May be inoperative provided

FAIL Light automatic lock controls are verified to
operate normally.

17-03 Flight Deck Door AUTO C 1 0 (M) May be inoperative provided:

UNLK Light a) Automatic lock controls are
verified to operate normally,
and
b) Door chime operates
normally.

17-04 Flight Deck Door Lock C 1 0 (M)(O) May be inoperative provided: |

Control Selector a) Keypad is deactivated,
b) Automatic lock is verified to
operate normally, and
c) Alternate procedures are
established and used.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-15
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

18 Boeing/C&D Aerospace C 1 0 May be inoperative provided

*** Enhanced Flight Deck automatic lock controls operate
Security Door Dead Bolt normally.
(14 CFR Part 25,
§ 25.795 Compliant)

19 JAMCO Flight Deck C 1 0 (M)(O) May be inoperative provided:

*** Security Door Automatic a) Automatic locking system is
Locking System deactivated,
(14 CFR Part 25, b) Mechanical Catch (Latch) Pin
§ 25.795 Compliant) operates normally and is used
to lock door, and
c) Alternate procedures are
established and used for
locking and unlocking flight
deck door using Mechanical
Catch (Latch) Pin.

19-01 Door Automatic Locking C 2 1 (M) One may be inoperative provided

Solenoid remaining locking solenoid operates
normally.

19-02 Door Warning System

19-02-01 Speakers C 2 1 (M)(O) One may be inoperative

*** provided remaining speaker is
verified to operate normally once
each flight-day.

19-02-02 LED C 2 0
*** (Green Indicator Light)

19-02-03 Aural Warning System C 1 0 (M)(O) May be inoperative provided:

*** a) AUTO UNLK Light is verified
to operate normally, and
b) Alternate procedures are
established and used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-16
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

19 JAMCO Flight Deck

*** Security Door Automatic
Locking System
(14 CFR Part 25,
§ 25.795 Compliant)
(Cont’d)

19-03 Door Control Panel

19-03-01 Door LOCK FAIL Light C 1 0 (M) May be inoperative OFF provided
*** automatic lock controls are verified to
operate normally.

19-03-02 Door AUTO UNLK Light C 1 0 (M)(O) May be inoperative OFF

*** provided:
a) Automatic lock controls are
verified to operate normally,
b) Aural Warning system
operates normally, and
c) Alternate procedures are
established and used.

19-03-03 Door HARD LOCK Light C 1 0 (M)(O) May be inoperative provided:

*** a) Automatic lock controls are
verified to operate normally,
and
b) Alternate procedures are
established and used.

19-03-04 Door UNLKD C 1 0 (M)(O) May be inoperative provided:

*** Switch/UNLK Switch a) Door can be opened manually
Position from flight deck,
b) Remaining automatic lock
controls are verified to
operate normally, and
c) Alternate procedures are
established and used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-17
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

19 JAMCO Flight Deck

*** Security Door Automatic
Locking System
(14 CFR Part 25,
§ 25.795 Compliant)
(Cont’d)

19-03 Door Control Panel

(Cont’d)

19-03-05 Door UNLKD Light C 1 0 (M)(O) May be inoperative provided:

*** a) Automatic lock controls are
verified to operate normally,
and
b) Aural warning system
operates normally.

19-03-06 Door EMRG ENTRY C 1 0 (M) May be inoperative provided door

ACTIVE Light aural warning system is verified to
operate normally.

19-03-07 Door OPEN Light C 1 0 (M)(O) May be inoperative provided

Automatic Lock controls are verified
to operate normally.

19-04 FLIGHT DECK DOOR C 1 0

Warning/Caution Light

19-05 Cabin Pushbutton Entry C 1 0 (O) May be inoperative provided

*** Pad/Keypad alternate procedures are established
and used.

19-05-01 Keypad Indicator Lights C 3 0 (M)(O) May be inoperative provided:

a) Keypad is verified to operate
normally, and
b) Alternate procedures are
established and used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-18
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

20 Flight Deck Door

Pressure Relief Panels

20-01 JAMCO Flight Deck A 3 0 May be inoperative in latched position

*** Security Door Pressure provided repairs are made within
Relief Latches 2 flight-days.
(14 CFR Part 25,
§ 25.795 Compliant)

20-02 Boeing/C&D Aerospace A 2 0 May be inoperative provided:

*** Enhanced Flight Deck a) Panels are in latched position,
Security Door and
(14 CFR Part 25, b) Repairs are made within
§ 25.795 Compliant) 2 flight-days.

21 JAMCO Flight Deck C 1 0 (M) May be inoperative provided

*** Security Door automatic lock system is verified to
Mechanical Catch Pin operate normally.
Lock
(14 CFR Part 25,
§ 25.795 Compliant)

22 Flight Deck Door Hold D 1 0

*** Open Device
(e.g., Door Stop,
Foot Plunger)

23 Flight Deck Door

*** Viewing Port

23A A 1 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Repairs are made within
3 flight-days.

23B C 1 0 (O) May be inoperative provided:

a) An electronic flight deck door
visual surveillance system is
installed and operates
normally, and
b) Alternate procedures are
established and used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 52-19
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
52. Doors
Change
Sequence No. Item 1 2 3 4 Bar

23 Flight Deck Door

*** Viewing Port
(Cont’d)

23-01 All-Cargo Configuration

23-01A C 1 0 May be inoperative provided

courier/supernumerary compartment
remains empty.

23-01B D 1 0 May be inoperative provided

procedures do not require its use.

24 Main Cabin Cargo Door

Vent Door

24-01 All-Cargo Configuration C 2 1 (M) Inoperative Vent Door must be

(STC ST01827LA) mechanically closed before dispatch.

25 Cargo Door Exterior C 2 0 (M) May be inoperative or missing

Handle Recess/Hinge provided the affected cargo door
Spring Assemblies exterior handle is secured in a
recessed position flush with the
fuselage.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 73-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
73. Engine Fuel and Control
Change
Sequence No. Item 1 2 3 4 Bar

01 Fuel Heater Timers C 2 1 (O) One may be inoperative provided

(-100/-200) associated fuel heater VALVE OPEN
light operates normally.

02 Fuel Heater Valves C 2 0 (M)(O) May be inoperative closed

(-100/-200) provided fuel temperature is
maintained at or above 32 °F (0 °C).

03 Fuel Heater VALVE

OPEN Lights
(-100/-200)

03A C 2 0 (M) May be inoperative provided

valve is verified to operate normally
before each departure.

03B C 2 0 (O) May be inoperative provided fuel

temperature is maintained at or
above 32 °F (0 °C).

04 Fuel Filter Differential

Pressure Warning
Systems

04-01 (-100/-200) C 2 1 (O) May be inoperative provided fuel

heater system is checked to operate
normally.

04-02 (-300/-400/-500/-600/ C 2 1 (M) May be inoperative provided

-700/-800/-900/-900ER) malfunction is verified to be in
warning system.

05 Fuel Flow Indication C 2 1 One may be inoperative provided:

Systems a) N1, N2 for associated engine
operate normally, and
b) Both main tank fuel quantity
indicators operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 73-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
73. Engine Fuel and Control
Change
Sequence No. Item 1 2 3 4 Bar

06 Fuel Used Indicators C 2 0

***

07 Power Management C 2 0 (O) May be inoperative provided:

Control (PMC) Systems a) Both PMCs remain OFF, and
(-300/-400/-500) b) AFM Appendix performance
adjustments are applied.

08 Power Management C 2 0 (O) May be inoperative provided:

Control (PMC) INOP a) Both PMCs remain OFF, and
Lights b) AFM Appendix performance
(-300/-400/-500) adjustments are applied.
|
10 Fuel Control ENG C 2 0 (M) May be inoperative provided
VALVE CLOSED associated valve is verified to operate
Indicating System normally.
(-600/-700/-800/
-900/-900ER)

11 Electronic Engine
Control (EEC)
(-600/-700/-800/
-900/-900ER)

11-01 Normal (ON) Mode C 2 0 (O) May be inoperative provided:

a) Both engines are operated in
ALTERNATE mode,
b) Strut/Wing leading edge
over-braided wire bundles are
installed per Boeing Service
Bulletin or production
equivalent, and
c) Applicable AFM performance
adjustments are applied.

12 Electronic Engine A 4 3 (M) May be inoperative deactivated

Control (EEC) Alternate provided repairs are made in
Power Supply System accordance with the times
(-600/-700/-800/ established in Boeing Maintenance
-900/-900ER) Planning Data document, D626A001,
Section 1, items 73-020-01 and
73-020-02.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 74-1
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
74. Ignition
Change
Sequence No. Item 1 2 3 4 Bar

01 Ignition Systems

01-01 (-100/-200)

01-01-01 High Energy System C 4 2 Except for ER operations, left igniter

(Twin 20 Joule) may be inoperative on each engine.

01-01-02 Low Energy System C 2 0 (O) May be inoperative provided

(4 Joule) switching is available to permit
selection of operative high energy
system for continuous ignition.

01-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)

01-02-01 Left Ignition Systems

01-02-01A B 2 1 One may be inoperative provided:

a) Ignition Select Switch remains
in BOTH position, and
b) Right ignition systems operate
normally.

01-02-01B C 2 0 (O) Except for ER operations, may be

inoperative provided:
a) Ignition Select Switch remains
in BOTH position, and
b) Associated engine right
ignition system operates
normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 74-2
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
74. Ignition
Change
Sequence No. Item 1 2 3 4 Bar

01 Ignition Systems
(Cont’d)

01-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Cont’d)

01-02-02 Right Ignition Systems

01-02-02A B 2 1 (M)(O) One may be inoperative

provided:
a) Ignition Select Switch remains
in BOTH position,
b) Left ignition systems operate
normally, and
c) Associated engine left igniter
is connected to AC Standby
Bus by an acceptable
configuration.

01-02-02B C 2 0 (M)(O) Except for ER operations,

may be inoperative provided:
a) Ignition Select Switch remains
in BOTH position,
b) Associated engine left ignition
systems operate normally,
and
c) Associated engine left igniter
is connected to AC Standby
Bus by an acceptable
configuration.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 52 PAGE NO. 75-1
DATE: 04/29/2008
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
75. Bleed Air
Change
Sequence No. Item 1 2 3 4 Bar

01 Gravel Protection D 1 0 (M) Valves may be inoperative closed

*** System provided operations do not require its
(-100/-200) use.

02 High Pressure Turbine C 2 0 (M) May be inoperative provided

*** Clearance Control system(s) are deactivated.
(HPTCC) Timer(s)
(-300/-400/-500)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 77-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
77. Engine Indicating
Change
Sequence No. Item 1 2 3 4 Bar

01 Engine Pressure Ratio

Systems
(-100/-200)

01-01 Digital Counters C 2 0

01-02 EPR Reference C 2 1

Selectors

02 N1 Tachometers

02-01 (-100/-200) B 2 1 (O) One may be inoperative provided

N2 and fuel flow indicator for
associated engine operate normally.

02-01-01 Digital Counters B 2 0 NOTE: An indicator with an operating

*** pointer is considered to
operate normally.

02-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)

02-02-01 Digital Counters B 2 0 (O) Except for EIS/CDS equipped

airplanes, may be inoperative
provided autothrottle is used for
takeoff thrust setting.

NOTE: An indicator with an operating

pointer is considered to
operate normally.

02-02-02 Reference N1 Bugs C 2 1

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 77-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
77. Engine Indicating
Change
Sequence No. Item 1 2 3 4 Bar

02 N1 Tachometers
(Cont’d)

02-02 (-300/-400/-500/-600/
-700/-800/-900/-900ER)
(Cont’d)

02-02-03 Manual Set Indication C 2 0

02-03 N1 Warning Lights B 2 0 May be inoperative provided

*** (-100/-200/-300/ associated N1 pointer operates
-400/-500) normally.

03 N2 Tachometers

03-01 (-100/-200) B 2 1 (O) One may be inoperative provided:

a) N1 and fuel flow indicators for
associated engine operate
normally, and
b) An alternate starting
procedure is established and
used.

03-02 (-300/-400/-500) B 2 1 (O) One may be inoperative provided:

a) N1 and fuel flow indicators for
associated engine operate
normally,
b) An alternate starting
procedure is established and
used, and
c) Engine #1 N2 tach generator
operates normally.

03-03 Digital Counters C 2 0 May be inoperative except for

*** EIS/CDS equipped airplanes.

NOTE: An indicator with an operating

pointer is considered to
operate normally.

03-04 N2 Warning Lights B 2 0 May be inoperative provided

*** (-100/-200/-300/ associated N2 pointer operates
-400/-500) normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 77-3
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
77. Engine Indicating
Change
Sequence No. Item 1 2 3 4 Bar

|
05 Vibration Indicating
Systems

05-01 (-100/-200) C 2 0
***

05-02 (-300/-400/-500/-600/ C 2 1
-700/-800/-900/-900ER)

06 EGT Indications

06-01 Digital Counters C 2 0 May be inoperative except for

*** EIS/CDS equipped airplanes.

06-02 EGT Warning Lights C 2 0 May be inoperative provided

*** (-100/-200/-300/ associated EGT pointer operates
-400/-500) normally.
|
09 Abnormal Start C 2 0
*** Indication Systems
(-300/-400/-500/-600/
-700/-800/-900/-900ER)

10 LOW IDLE Light B 1 0 (M) May be inoperative provided:

(-300/-400/-500) a) Engine idle control system is
verified to operate normally,
and
b) Both engines installed are
“modified” engines (Boeing
SB 737-77-1031 or production
equivalent).
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 78-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
78. Engine Exhaust
Change
Sequence No. Item 1 2 3 4 Bar

01 Thrust Reverser
Systems

01-01 (-100/-200)

01-01A C 2 1 (M)(O) One may be inoperative

provided thrust reverser is
deactivated and secured closed.

01-01B C 2 1 (M)(O) One may be inoperative

provided:
a) Thrust reverser guide carriage
is verified to be in over-center
(forward thrust) position, and
b) Override System is armed
only after landing.

NOTE: Relief also applies to

airplanes modified by
STC SA5730NM or
ST00131SE.

01-02 (-300/-400/-500) C 2 1 (M)(O) One may be inoperative

provided thrust reverser is locked in
forward thrust position.

01-03 (-600/-700/-800/ C 2 1 (M)(O) One may be inoperative

-900/-900ER) provided:
a) Thrust reverser is locked in
forward thrust position, and
b) Appropriate performance
adjustments are applied.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 78-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
78. Engine Exhaust
Change
Sequence No. Item 1 2 3 4 Bar

02 REVERSER C 2 1 (M) One may be inoperative provided

UNLOCKED Lights reverser is locked in closed
(-100/-200/-300/ (forward thrust) position.
-400/-500)
NOTE: Relief also applies to
airplanes modified by STC
SA5730NM or ST00131SE.
|
04 Thrust REVERSER C - 0 (M) May be inoperative provided
*** ARMED Light(s) lights are deactivated.
(-100/-200)
NOTE: Relief also applies to
airplanes modified by STC
SA5730NM or ST00131SE.

05 Thrust Reverser C 2 1 One may be inoperative for an

Override Switches associated inoperative thrust
(-100/-200) reverser.

NOTE: Relief also applies to

airplanes modified by STC
SA5730NM or ST00131SE.

06 Thrust Reverser LOW C 1 0 (M) May be inoperative provided

*** PRESSURE Light accumulators are charged before
(-100/-200) each departure.

NOTE 1: Reverse thrust may not be

available when System A
pressure is lost.

NOTE 2: Relief also applies to

airplanes modified by STC
SA5730NM or ST00131SE.

07 REVERSER Lights C 2 1 (M) One may be inoperative provided

(Aft Overhead Panel) associated reverser is locked in
(-300/-400/-500/-600/ closed (forward thrust) position.
-700/-800/-900/-900ER)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 79-1
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
79. Engine Oil
Change
Sequence No. Item 1 2 3 4 Bar

01 Oil Quantity Indication B 2 1 (M) Except for ER operations, one

Systems may be inoperative provided:
a) Oil tank is filled to maximum
recommended capacity at
each refueling,
b) There is no evidence of above
normal oil consumption or
leakage, and
c) Associated low oil pressure
warning system operates
normally.

01-01 Oil Quantity Indicator C 1 0 (M) May be inoperative provided:

*** Test Switch a) Oil tanks are filled to
(-100/-200/-300/ maximum recommended
-400/-500) capacity at each refueling,
b) There is no evidence of above
normal oil consumption or
leakage, and
c) Engine low oil pressure
warning systems operate
normally.

02 Oil Filter Bypass

Warning Systems

02-01 (-100/-200/-300/-400/ C 2 1 (M) One may be inoperative provided:

-500/-600/-700/-800/ a) Malfunction is in warning
-900/-900ER) system, and
b) Oil filter is inspected for
presence of contaminants
once each flight-day.

02-02 (-600/-700/-800/ C 2 1 (M) One may be inoperative provided:

-900/-900ER) a) Malfunction is in the warning
system,
b) All three Magnetic Chip
Detectors are inspected for
presence of contaminants
once each flight-day, and
c) Oil supply filter pop-out
indicator is confirmed not
extended once each
flight-day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 62 PAGE NO. 79-2
DATE: 11/28/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
79. Engine Oil
Change
Sequence No. Item 1 2 3 4 Bar

|
04 Oil Low Pressure B 2 0 May be inoperative provide
Warning Systems associated oil pressure, oil
temperature, and oil quantity
indicators operates normally.

04-01 (-100/-200/-300/-400/ B 2 0 May be inoperative provided: |

-500 upon incorporation a) Associated oil pressure, oil |
of Boeing Service temperature and oil quantity |
Bulletin 737-30A1064) indicators operates normally, |
and |
b) AUTO function of the Air Data |
Heat System is considered |
inoperative. |

NOTE: Refer to MMEL Item 30-22-01 |

(Air Data Probe Heat |
Systems, AUTO activation). |
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 80-1
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
80. Starting
Change
Sequence No. Item 1 2 3 4 Bar

01 Starter Valve Open

Indications

01-01 (-100/-200) C 2 0 May be inoperative provided Start

*** Valve Arming System is installed and
operating normally.

01-02 (-300/-400/-500/-600/ C 2 1 (O) One may be inoperative provided

-700/-800/-900/-900ER) it is checked after engine start that
associated valve is closed.

02 Engine Starter Auto

*** Cutout

02-01 (-100/-200) C 2 0 May be inoperative provided:

a) Flightcrew manually selects
Start Switch to OFF at 40%
N2, and
b) Takeoff in icing conditions is
not permitted with No. 1
Engine Starter Auto Cutout
inoperative.

02-02 (-300/-400/-500) C 2 0 May be inoperative provided

flightcrew manually selects Start
Switch OFF at 46% N2.

02-03 (-600/-700/-800/ C 2 0 May be inoperative provided

-900/-900ER) flightcrew manually selects Start
Switch OFF or AUTO at 55% N2.

03 Starter Valves

03-01 (-100/-200) C 2 0 (M)(O) May be inoperative provided

alternate starting procedures are
established and used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 58 PAGE NO. 80-2
DATE: 10/10/2015
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Boeing B-737 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
80. Starting
Change
Sequence No. Item 1 2 3 4 Bar

03 Starter Valves
(Cont’d)

03-02 (-300/-400/-500) C 2 1 (M)(O) One may be inoperative

provided:
a) Modified Main Engine
Controls or production
equivalent have been
incorporated,
b) Associated start valve light
operates normally, and
c) Manual override start
procedures are used.

03-03 (-600/-700/-800/ C 2 1 (M)(O) Except for ER operations, one

-900/-900ER) may be inoperative provided:
a) Associated start valve
indication operates normally,
and
b) Manual override start
procedures are used.

04 Starter Valve Arming C 1 0 May be inoperative provided Starter

*** System Valve Open Lights are installed and
(-100/-200) operating normally.