U.S.

Department of Transportation Federal Aviation Administration

Master Minimum Equipment List

BOEING

B-767 200/300/300F/300BCF/400ER

Michael F. Garrett Flight Operations Evaluation Board (FOEB)

Federal Aviation Administration Seattle Aircraft Evaluation Group 1601 Lind Ave SW Renton, WA 98057

Telephone: FAX:

(425) 917-6600 (425) 917-6638

FEDERAL AVIATION ADMINISTRATION

Page I Revision 33c Date: 08/20/2010

MASTER MINIMUM EQUIPMENT LIST B-767 Contents

SYSTEM Contents Highlights of Change Definitions (Operator Responsibiity) Preamble (Operator Responsibility) 21 - Air Conditioning 22 - Auto Flight 23 - Communications 24 - Electrical Power 25 - Equipment/Furnishings 26 - Fire Protection 27 - Flight Controls 28 - Fuel 29 - Hydraulic Power 30 - Ice and Rain Protection 31 - Indicating/Recording Systems 32 - Landing Gear 33 - Lights 34 - Navigation 35 - Oxygen 36 - Pneumatic 38 - Water/Waste 46 - Information Systems 47 Inert Gas System 49 - Airborne Auxiliary Power 52 - Doors 56 - Windows 73 - Engine Fuel & Control 74 - Ignition 75 - Bleed Air 77 - Engine Indicating 78 - Engine Exhaust 79 - Engine Oil 80 - Engine Starting

PAGE(S) I II, III IV V 21-1 Thru 21-24 22-1 Thru 22-7 23-1 Thru 23-17 24-1 Thru 24-8 25-1 Thru 25-12 26-1Thru 26-9 27-1 Thru 27-4 28-1 Thru 28-10 29-1 Thru 29-4 30-1 Thru 30-9 31-1 Thru 31-5 32-1 Thru 32-7 33-1 Thru 33-9 34-1 Thru 34-16 35-1 Thru 35-4 36-1 Thru 36-13 38-1 46-1 47-1 49-1 Thru 49-2 52-1 Thru 52-13 56-1 73-1 Thru 73-6 74-1 75-1 Thru 75-3 77-1 Thru 77-3 78-1, 78-2 79-1 Thru 79-2 80-1

REVISION 33c 33c 33c 33c 33b 33b 33c 33c 33c 33c 33b 33c 33a 33c 33 33b 33c 33b 33b 33c 33b 33 33c 32b 33c 33 33c 32b 32b 32b 33b 33a 32b

DATE 08/20/2010 08/20/2010 08/20/2010 08/20/2010 05/01/2010 05/01/2010 08/20/2010 08/20/2010 08/20/2010 08/20/2010 05/01/2010 08/20/2010 06/18/2009 08/20/2010 05/05/2009 05/01/2010 08/20/2010 05/01/2010 05/01/2010 08/20/2010 05/01/2010 05/05/2009 08/20/2010 04/29/2008 08/20/2010 05/05/2009 08/20/2010 04/29/2008 04/29/2008 04/29/2008 05/01/2010 06/18/2009 04/29/2008

FEDERAL AVIATION ADMINISTRATION

Page II Revision 33c Date: 08/20/2010

MASTER MINIMUM EQUIPMENT LIST B-767

Highlights of Change EFFECTIVE ABOVE DATE, the Boeing 767 Master Minimum Equipment List has been revised. Please replace ALL pages within the affected ATA chapter for a complete up-to-date MMEL. SEE NOTE BELOW FOR IMPORTANT INFORMATION ABOUT REVISIONS. Retain this sheet with your MMEL until the next revision is issued. NOTE: The Definitions pages and Preamble pages are not contained in this revision. Operators must insert the applicable DEFINITIONS from current Policy Letter 25 and the applicable PREAMBLE from current Policy Letter 34 (Air Carriers) or Policy Letter 36 (Part 91 Operators) into their MEL. ATA System/Sequence Number COMMUNICATIONS 25-1 SAT Communication Systems (Includes Wingspeed SCS STC ST02534CH) ELECTRICAL POWER 00-1 Engine Generator Systems (IDG, GCB) Minor edit to sub-item 1)c. Added at least one to the proviso. No change to relief. Minor edit to proviso in sub-ite 6). No change to relief. Remarks

23 ***

24

25

EQUIPMENT/ FURNISHINGS 25-7 Lower Lobe Crew Rest Module (STC ST01994SE) Storage Bin(s)/ Cabin and Galley Storage Compartments/ Closets Minor edit to NOTE.

***

28-1

Revised in accordance with MMEL Policy Letter 104, Revision 4, dated June 18, 2010.

50-1 Lower Cargo Compartment Lining Panels, Floor Panels, and Walkways 1) Lining Panels Removed Sidewalls from title and made applicable to all paneling within the cargo compartment. The subitems, 1) and 2) were broken out for the 2007 B-767 FOEB, and this sub-item was mis-named: the word "sidewall" has been misinterpreted to mean ONLY the sidewall panels, which excluds endwalls, ceiling and slopers. Revised in accordance with MMEL Policy Letter 100, Revision 2, dated January 20, 2009.

54-1 Cargo Restraint Systems/Devices

FEDERAL AVIATION ADMINISTRATION

Page III Revision 33c Date: 08/20/2010

MASTER MINIMUM EQUIPMENT LIST B-767 ATA System/Sequence Number (Including Main Deck 9 "g" Barrier Net) 26 FIRE PROTECTION 26-2 Lavatory Fire Extinguisher System 26-3 Lavatory Smoke Detection System Remarks

Revised relief in accordance with MMEL Policy Letter 24, Rev 4, dated 11/02/2010. Revised relief in accordance with MMEL Policy Letter 24, Rev 4, dated 11/02/2010.

21

AIR CONDITIONING 52-1 Pack RESET Switches Removed the word One from second proviso.

28

FUEL 41-1 Fuel Tank Quantity Indications Systems (Flight Deck) Revised MMEL subitem 1) proviso i) to delete reference to Service Bulletin 767-28-0052. Revise subitem 2) title to delete references in parentheses. Delete subitem 3) title and move subitems 3)a) and 3)b) under subitem 2); revise new subitem 2)a) title to include SB for 767400ER; revise new subitem 2)b) title to be specific to airplanes subject to AD. Proposals for subitem 2) change only the configuration applicability; there are no changes to associated Remarks Or Exceptions. Re-number remaining subitem.

30

ICE AND RAIN PROTECTION 21-1 Engine Anti-Ice Valves Minor edit to Sub-item 4) Cowl Valves, c) RB211-254, proviso paragraph b). No change to relief.

33-1 Temperature (TAT) Probe Heater Systems 33 LIGHTS 43-1 Position Lights (Bulbs) 2) -300/-300F With Blended Winglets STC ST01920SE (LED Lights)

Spelling correction in proviso paragraph a).

Added Light Emitting Diode (LED) Module Position Light installed with Blended Winglets under STC ST01920SE. Renumbered the -400ER to sub-item 3).

36

PNEUMATICS 22-4 L and R Bleed ISLN VALVE Lights Revised Number Installed and Number Required for Dispatch in sub-item 1) -200/-300. No change to proviso relief.

FEDERAL AVIATION ADMINISTRATION

Page IV Revision 33c Date: 08/20/2010

MASTER MINIMUM EQUIPMENT LIST B-767 ATA System/Sequence Number Remarks

47 ***

INERT GAS SYSTEM 11-1 Nitrogen Generation System (NGS) 1) Nitrogen Generation Performance

Added new ATA Chapter Added new Item.

Added new sub-item.

52

DOORS 11-4 Main Entry Doors/Slides/ Emergency Exits Revised relief for All Cargo and Combination Passenger/Cargo in accordance with Policy Letter 1, Revision 4 dated February 27, 2010 and Policy Letter 99, Revision 2 dated February 26, 2010.

73

ENGINE FUEL & CONTROL 21-1 Electronic Engine Control (EEC) Systems 5) EEC C1 Faults (CF6 FADEC) Revised proviso to reflect the current location of Time Limited Dispatch information, relocated at FAA request.

FEDERAL AVIATION ADMINISTRATION

Page V Revision 33c Date: 08/20/2010

MASTER MINIMUM EQUIPMENT LIST B-767 Definitions

Insert current Policy Letter 25 DEFINITIONS here.

FEDERAL AVIATION ADMINISTRATION

Page VI Revision 33c Date: 08/20/2010

MASTER MINIMUM EQUIPMENT LIST B-767 Preamble

Insert current Policy Letter 34 or 36, as applicable, PREAMBLE here.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 20-1 A/C Ozone Converters Flight Deck Supply Boost Fan Gasper Fan Recirculation Fans 1) -200/-300 C C 2 2 1 0 May be inoperative provided both packs operate normally. C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-1

As required by FAR.

22-1 *** 24-1 *** 25-1

(M) May be inoperative deactivated.

2)

-400ER

C C

2 2

1 0 (O) May be inoperative provided: a) Both packs operate normally, and b) Appropriate performance adjustments are applied. (M) May be inoperative provided associated EICAS message is verified to operate normally.

25-2

Recirculation Fan INOP Lights Forward Cargo Air Conditioning System Crew Rest Area Air Distribution System (STC ST00973WI-D) 1) Air Supply Shutoff Valves

28-1 *** 29-1 ***

(M) May be inoperative closed provided associated crew rest area is locked closed and placarded DO NOT USE. NOTE: These provisos are not intended to prohibit crew rest area inspections.

2)

Boost Fans

(M) May be inoperative deactivated provided associated heater is deactivated.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 29-2 *** Lower Lobe Crew Rest Air Distribution System (STC ST01994SE) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-2

(M) May be inoperative provided: a) Lower lobe crew rest module is not used and personal items are removed, and b) Lower lobe crew rest door is closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest inspections by crew members.

31-1

Auto Cabin Pressure Control Systems

C C

2 2

1 0

One may be inoperative provided manual mode and one autopilot operate normally. (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Manual cabin pressure control system operates normally, c) For cargo compartments with Class C fire suppression, procedures are established 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, d) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, e) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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 f) For -400ER, appropriate performance adjustments are applied. 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 FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 31-1 Auto Cabin Pressure Control Systems (Contd) C 2 0 (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Extended overwater flight is prohibited, c) For cargo compartments with Class C fire suppression, procedures are established 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, d) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, e) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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 f) For -400ER, appropriate performance adjustments are applied. NOTE: Operator MELs must define which items are approved for inclusion in Fly Away Kits and which materials can be used as ballast. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-3

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 31-2 Manual Cabin Pressure Control System C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-4

(M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Extended overwater flight is prohibited, c) For cargo compartments with Class C fire suppression, procedures are established 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, d) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, e) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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 f) For -400ER, appropriate performance adjustments are applied. 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 FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 31-3 Outflow Valve C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-5

(M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Extended overwater flight is prohibited, c) For cargo compartments with Class C fire suppression, procedures are established 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, d) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, e) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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 f) For -400ER, appropriate performance adjustments are applied. 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 FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 32-1 Positive Pressure Relief Valves C C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-6

(M) One may be inoperative closed. (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Manual cabin pressure control system operates normally, c) For cargo compartments with Class C fire suppression, procedures are established 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, d) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, e) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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 f) For -400ER, appropriate performance adjustments are applied. 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 FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 32-1 Positive Pressure Relief Valves (Contd) C 0 (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Extended overwater flight is prohibited, c) For cargo compartments with Class C fire suppression, procedures are established 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, d) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, e) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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 f) For -400ER, appropriate performance adjustments are applied. NOTE: Operator MELs must define which items are approved for inclusion in Fly Away Kits and which materials can be used as ballast. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-7

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 33-1 CABIN RATE of Climb Indicator C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-8

May be inoperative provided both automatic pressure control systems operate normally. (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) For cargo compartments with Class C fire suppression, procedures are established 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, c) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, d) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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) For -400ER, appropriate performance adjustments are applied. 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 FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 33-2 CABIN DIFF Pressure Indicator C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-9

(O) May be inoperative provided: a) CABIN ALT indicator operates normally, and b) A chart is provided to convert cabin altitude to cabin differential pressure. (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) For cargo compartments with Class C fire suppression, procedures are established 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, c) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, d) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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) For -400ER, appropriate performance adjustments are applied.

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 FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 33-3 CABIN ALT Indicator C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-10

(O) May be inoperative provided: a) CABIN DIFF pressure indicator operates normally, and b) A chart is provided to convert cabin differential pressure to cabin altitude. (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) For cargo compartments with Class C fire suppression, procedures are established 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, c) For forward lower lobe cargo compartments with Class E fire suppression, procedures are established 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, d) For ATC A1NM -200 SF and -300BCF with Class E fire suppression, procedures are established and used to ensure all 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) For -400ER, appropriate performance adjustments are applied. NOTE: Operator MELs must define which items are approved for inclusion in Fly Away Kits and which materials can be used as ballast.

33-4

Outflow VALVE Position Indicator AUTO INOP Light (Cabin Altitude Control)

33-5

(O) May be inoperative provided: a) Both automatic pressure control systems operate normally, and b) CABIN ALT or CABIN RATE of climb indicator operates normally. May be inoperative provided flight remains at or below 10,000 feet MSL.

33-6

Cabin Altitude Warning System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 40-1 Cargo Heating Systems 1) *** 2) Fwd and Aft Bulk a) Bulk Cargo Vent Fan 40-2 Cargo Heat Indicating Systems (OVHT and/or ON Light) 1) Fwd and Aft a) -200/-300 C 0 (M) May be inoperative provided overheat protective system(s) is verified to operate normally. (M) May be inoperative provided associated cargo heat system is selected OFF. C C C 2 1 1 0 0 0 (M) May be inoperative deactivated. (M) May be inoperative deactivated. (O) May be inoperative provided Bulk Cargo Heat Selector remains in NORM position. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-11

b) -400ER *** 2) Bulk a) -200/-300

(M) May be inoperative provided overheat protective system(s) is verified to operate normally. May be inoperative provided bulk cargo heat system is selected OFF.

b) -400ER 45-1 Flight Crew Auxiliary Heat Systems

C C C

1 4 4

0 0 0 May be inoperative OFF. (M) May be inoperative provided associated system is deactivated. NOTE: Any portion which operates normally may be used.

45-2

Forward Door Area Heater System (ATC A1NM -200 SF, -300BCF, -300F, -300BDSF)

(M) May be inoperative deactivated.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 45-3 Door Heater Systems (Type A, I, III Doors) Air Conditioning Packs 1) -200/-300 C 2 1 (O) One may be inoperative provided: a) Airplane remains at or below FL 350, and b) Flight remains within 60 minutes of landing at a suitable airport. (O) One may be inoperative provided: a) Airplane remains at or below FL 350, b) Flight remains within 60 minutes of landing at a suitable airport, and c) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) Flight is conducted in an unpressurized configuration, b) Both recirculation fans operate normally, and c) 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 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: Classic Interior is on most -200/-300 passenger airplanes. All 767 passenger airplanes built prior to March 2000 and some built since then have classic interior. NOTE 3: 767 New Look Interior (NLI) looks similar to 777 interior. NLI, also referred to as Signature Series Interior, was first installed in 767 in March 2000. C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-12

(M) May be inoperative deactivated.

51-1

2)

-400ER

3)

-200/-300 Passenger Airplanes with Classic Interior

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 51-2 Pack Flow Control/Shutoff Valves 1) Hi Flow Mode (-200/-300 Passenger) 2) Hi Flow Mode (All Cargo Configuration) 51-3 Pack Temperature Control Systems (-200/-300) 1) Auto Mode C 2 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-13

(M)(O) May be inoperative closed for an associated inoperative pack.

Except for ER operations, one may be inoperative provided remaining (opposite) pack operates normally.

May be inoperative OFF for an associated inoperative pack.

May be inoperative provided associated Standby Mode operates normally. May be inoperative provided associated Auto Mode operates normally. (M)(O) One valve may be inoperative deactivated in mid position provided: a) Associated pack is operated in STBY, and b) Remaining (opposite) pack operates normally in AUTO. (M) One may be inoperative closed in STBY provided remaining (opposite) pack operates normally in AUTO. May be inoperative for an associated inoperative pack.

2) Standby Mode

51-4

Pack Temperature Control Valves (-200/-300)

51-5

Pack Altitude Switch (-200/-300)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 51-6 Main Cargo Air Distribution Riser Shutoff Valves 1) -300F C 1 (M) May be inoperative closed provided: a) Corresponding zone trim air modulating valve is deactivated closed, and b) Operation is limited to one pack. NOTE: In event of operating pack failure, turn on remaining pack. 2) -200PC, -200SF, ATC A1NM -200 SF, -300BCF and -300BDSF C 1 (M) May be inoperative closed provided: a) Corresponding zone trim air modulating valve is deactivated closed, b) Operation is limited to one pack, and c) Operations are limited to FL 350 and below. NOTE: In event of operating pack failure, turn on remaining pack. 51-7 Air Cycle Machine 1) -200/-300 C 2 1 (M)(O) Except for ER operations, one may be inoperative provided: a) Associated pack is operated in STBY WARM, b) Flow control valve in associated pack is verified to operate normally, c) Remaining (opposite) pack operates normally, and d) Associated pack is turned OFF at TAT above 0 degrees C. (M)(O)One may be inoperative with associated pack selected on provided: a) Remaining (opposite) pack operates normally, b) Remaining (opposite) engine bleed system operates normally, c) Associated Turbine Bypass valve is secured open, and d) Appropriate performance adjustments are applied. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-14

2) -400ER

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 52-1 Pack RESET Switches C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-15

One may be inoperative provided both packs operate normally. May be inoperative for an associated inoperative pack(s). |

52-2 52-3

Pack INOP Lights Air Conditioning Pack OFF Lights

C C

2 2

1 1 (M) One may be inoperative OFF provided associated EICAS message and all other pack indications operate normally. May be inoperative provided: a) Associated condenser low limit control system operates normally, and b) Associated ram air inlet door operates normally. One may be inoperative for an associated inoperative pack. (M) May be inoperative provided: a) CTC sensor for associated pack is verified to operate normally, b) Associated CTC operates normally, and c) Associated secondary heat exchanger outlet temperature sensor system operates normally. One may be inoperative for an associated inoperative pack. May be inoperative provided at least one sensor per pack operates normally.

52-5

Secondary Heat Exchanger Outlet Temperature Sensor Systems (-400ER)

52-6

ASCTU Pack Outlet Temperature Sensors (-400ER)

52-7

Compressor Discharge Temperature Sensors (-400ER)

(M) May be inoperative for an associated inoperative pack provided at least two sensors are verified to operate normally on remaining (opposite) pack.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 52-8 Condenser Low Limit Control Systems (-400ER) C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-16

(M)(O) One may be inoperative provided: a) Associated condenser low limit valve is secured open, b) Remaining (opposite) pack operates normally, c) Remaining (opposite) engine bleed system operates normally, and d) Appropriate performance adjustments are applied. One may be inoperative for an associated inoperative pack. (M)(O) May be inoperative provided doors are secured open with pack(s) operating.

53-1

Ram Air Inlet/Exhaust Door Systems

(M)(O) May be inoperative in any position provided associated pack is considered inoperative.

58-1

Forward Equipment Cooling AUTO System 1) -200/-300 C 1 0 May be inoperative provided STBY control system is used. May be inoperative provided: a) STBY control system is used, and b) Both packs operate normally. (M) May be inoperative provided: a) STBY control system is used, and b) Heat exchanger bypass valve is deactivated CLOSED.

2) -400ER

58-2

Forward Equipment Cooling Temperature Control System (Two Supply Fan Installation)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 58-3 Forward Equipment Cooling Supply Fans 1) Two Supply Fan Installation C 2 1 One may be inoperative provided: a) Forward equipment cooling exhaust fan operates normally, and b) Automatic control system operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-17

2) One Supply Fan Installation a) -200/-300 C 1 0 May be inoperative provided: a) Forward equipment cooling exhaust fan operates normally, b) STBY control system is used, and c) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air. (O) May be inoperative provided: a) Forward equipment cooling exhaust fan operates normally, b) STBY control system is used, c) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air, d) Both packs operate normally, and e) SMOKE/OVRD valve is verified to operate normally.

b) -400ER

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 58-4 Forward Equipment Cooling Exhaust Fan 1) Two Supply Fan Installation 2) One Supply Fan Installation a) -200/-300 C 1 0 May be inoperative provided: a) Forward equipment cooling supply fan operates normally, b) STBY control system is used, and c) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air. (O) May be inoperative provided: a) Forward equipment cooling supply fan operates normally, b) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air, c) Both packs operate normally, and d) SMOKE/OVRD valve is verified to operate normally. C 1 0 May be inoperative provided both forward equipment cooling supply fans operate normally, NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-18

b) -400ER

58-5

Aft Equipment/ Lav/Galley Exhaust (Vent) Fans Forward Equipment Cooling Ground Supply Valve

58-6 ***

(M) May be inoperative secured closed.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 58-7 Forward Equipment Cooling Overboard Exhaust Valve 1) Two Supply Fan Installation 2) One Supply Fan Installation a) -200/-300 C 1 0 (M)(O) May be inoperative secured closed provided: a) STBY control system is used, and b) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air. (M)(O) May be inoperative secured closed provided: a) STBY control system is used, b) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air, and c) Both packs operate normally. C 1 0 (M)(O) May be inoperative secured closed. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-19

b) -400ER

58-8

Forward Equipment Cooling Inboard Supply Valve 1) One Supply Fan Installation a) -200/-300 C 1 0 (M) May be inoperative secured closed provided: a) STBY control system is used, and b) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air. (M) May be inoperative secured closed provided: a) STBY control system is used, b) For ground operation above 29 degrees C OAT, main cabin is supplied with conditioned air, and c) Both packs operate normally.

b) -400ER

58-9 ***

Avionics Cooling Refrigeration Unit (ACRU) ACRU Supply Valve

58-10 ***

(M) May be inoperative secured closed.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 58-11 *** 58-12 *** ACRU Isolation Valve Instrument Cooling Monitor System D 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-20

(M) May be inoperative secured open.

(M) For ER operations, may be inoperative provided availability of adequate air flow is verified before each departure. Except for ER operations, may be inoperative. (M) May be inoperative provided associated IFE system is deactivated.

D 58-13 *** In-Flight Entertainment (IFE) Cooling Systems AVS/Forward IFE Cooling Overboard Ground Exhaust Valves 1) Alternate Ventilation System (AVS) Overboard Valve (-400ER) *** 2) Forward IFE Cooling Overboard Ground Exhaust Valves C D

1 -

0 0

58-14

(M) May be inoperative secured closed provided both packs operate normally.

(M) One may be inoperative secured open.

(M) May be inoperative provided: a) One valve is secured closed, and b) Both packs operate normally. (M) May be inoperative deactivated provided associated chiller is deactivated.

58-16 ***

F1 Forward Galley Chiller Smoke Detector Flight Deck Panel Cooling Shutoff Valve

58-17 ***

(M) May be inoperative deactivated open.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 61-1 Cabin COMPT TEMP Control Systems 1) Passenger a) -200/-300/ -400ER C 0 (M) May be inoperative provided associated zone trim air modulating valve(s) or trim air regulating/shutoff valve(s) remains closed. (M) May be inoperative for unannunciated faults that do not affect zone temperature control availability. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-21

b) -400ER Control Panel Functions 2) All Cargo Configuration

(M) May be inoperative provided associated zone trim air modulating valve remains closed.

61-2

Flight Deck COMPT TEMP Control System 1) Passenger C 1 0 (M) Both auto and manual mode may be inoperative provided associated zone trim air modulating valve or trim air regulating/shutoff valve remains closed. (M) May be inoperative for unannunciated faults that do not affect zone temperature control availability. May be inoperative provided MAN mode operates normally. May be inoperative provided AUTO mode operates normally. (M) May be inoperative provided associated trim air regulating/shutoff valve is secured closed.

2) -400ER Control Panel Functions 3) AUTO Mode

4) MAN Mode

61-3

Trim Air Regulating/Shutoff Valve System(s) (Passenger Airplanes)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 61-4 Zone Trim Air Modulating Valves 1) Passenger C 0 (M) May be inoperative provided associated valve is closed. May be inoperative in any position provided trim air switch remains OFF. Main cargo compartment valves may be inoperative closed. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-22

2)

All Cargo Configuration

61-5 61-6

Trim Air OFF Light(s) COMPT TEMP INOP Lights 1) Passenger a) -200/-300

(M) May be inoperative provided associated trim air modulating valve remains closed. (M) May be inoperative provided associated trim air regulating/shutoff valve remains closed. (O) May be inoperative. (M) FWD and/or AFT light(s) may be inoperative provided associated trim air modulation valve(s) remains closed.

b) -400ER 2) All Cargo Configuration

C C

4 3

0 1

61-7

Trim Air Check Valves (-200/-300) 1) Passenger C 2 0 (M) May be inoperative provided one failed check valve is secured closed. (M)(O) May be inoperative provided: a) Failed check valve is secured closed, and b) Trim air is available from side opposite to valve which is secured closed.

2)

All Cargo Configuration

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 61-8 Cabin Temperature Controllers (CTC) (-400ER) C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-23

(M)(O) One may be inoperative provided: a) Associated pack flow control valve is secured closed, b) Remaining (opposite) pack operates normally, c) Remaining (opposite) engine bleed system operates normally, and d) Appropriate performance adjustments are applied. One may be inoperative for associated inoperative pack.

64-1

Trim Air Valve Position Indicator Forward Overboard Valve (-300/-400ER) COMPT TEMP Indications Crew Rest Area Temperature Control System (STC ST00973WI-D) 1) Pre-Heater System 2) Heaters 3) Heat Select Switches

64-2 ***

(M) May be inoperative provided valve is deactivated closed.

65-1

66-1 ***

(M) May be inoperative deactivated.

C C

2 2

0 0

(M) May be inoperative deactivated. (M) May be inoperative deactivated provided associated heater and boost fan are deactivated. (M) May be inoperative provided: a) Heater System is deactivated b) Lower lobe crew rest module is not used and personal items are removed, and c) Lower lobe crew rest door is closed and placarded INOPERATIVE-DO NOT ENTER

66-2 ***

Lower Lobe Crew Rest Bunk Heater System (ST01994SE)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 21 - AIR CONDITIONING 71-1 *** CTT Systems Zonal Comfort System 1) Zonal Humidifier System a) Humidifiers 2) Zonal Drying System D 1 0 (M) May be inoperative provided humidifier system is deactivated. (M) May be inoperative deactivated. (M) May be inoperative provided: a) Zonal drying system is deactivated, and b) Humidifier system is deactivated. (M) May be inoperative provided: a) Affected zonal dryer is deactivated, and b) Associated humidifier is deactivated. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 21-24

D D

7 1

0 0

a) Zonal Dryers

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 22 - AUTO FLIGHT 10-1 Autopilot Systems C 3 2 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 22-1

(M) One may be inoperative provided: a) Associated FCC SERVO circuit breaker is pulled and collared, b) If FCC Single Source option is installed, Autopilot Flight Director System is verified not in a single source configuration prior to each departure, and c) Approach minimums do not require its use. (M) Two may be inoperative provided: a) At least two FCC power circuit breakers remain in, b) Associated FCC SERVO circuit breakers are pulled and collared, c) If FCC Single Source option is installed, Autopilot Flight Director System is verified not in a single source configuration prior to each departure, and d) Approach minimums do not require their use. (M) Except for ER operations, all may be inoperative provided: a) At least one FCC power circuit breaker remains in, b) All three FCC SERVO circuit breakers are pulled and collared, c) Enroute operations and approach minimums do not require their use, and d) Number of flight segments and segment duration is acceptable to flight crew. One may be inoperative provided: a) Autopilots are not used below 1,500 feet AGL, and b) Approach minimums do not require use of autopilot. May be inoperative provided: a) Autopilots are not used below 1,500 feet AGL, and b) All other A/P disengagement alerts operate normally.

11-1

Control Wheel Disengage Switches

11-2

A/P DISC Light (-200/-300)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 22 - AUTO FLIGHT 11-3 Mode Control Panel Selectors 1) VERT SPD Selector (DN & UP) 2) BANK LIMIT Selector 3) Selector Push Functions a) IAS/MACH b) ALT c) HDG SEL C C B 1 1 1 0 0 0 (O) May be inoperative. (O) May be inoperative. (O) May be inoperative. NOTE: Rotational function of these selectors must operate normally. 11-4 Mode Control Panel Switches 1) A/P Engage Switches/ Paddles (L CMD, C CMD, R CMD) C 3 1 (O) May be inoperative. NOTE: All operative autopilots may be used during autoland operations. C 1 0 (O) May be inoperative provided FL CH mode operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 22-2

(O) May be inoperative.

Except for ER operations, may be inoperative provided: a) Enroute operations and approach minimums do not require their use, and b) Number of flight segments and segment duration is acceptable to flight crew.

***

2) A/P CWS Engage Switches 3) A/T ARM Switch

May be inoperative OFF provided approach minimums do not require use of autothrottle system. (O) May be inoperative provided procedures and approach minimums do not require its use. (Continued)

4) A/T SPD Mode Engage Switch

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 22 - AUTO FLIGHT 11-4 Mode Control Panel Switches (Contd) 5) F/D Switches C 2 0 May be inoperative OFF provided approach minimums do not require use of flight director displays. May be inoperative provided IAS is displayed in associated window. May be inoperative provided approach minimums do not require use of autopilot or flight director. (O) May be inoperative. (O) May be inoperative. (O) One may be inoperative provided procedures or enroute operations do not require its use. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 22-3

6) IAS/MACH SEL Switch 7) APP Switch

8) ***

LOC Switch

C C C

1 1 4

0 0 3

9) B/CRS Switch 10) V NAV, FL CH, V/S, ALT HOLD Switches 11) L NAV, HDG HOLD Switches

(O) One may be inoperative provided: a) HDG SEL operates normally, and b) Procedures or enroute operations do not require its use. May be inoperative provided both thrust levers are operated manually for takeoff.

12) EPR/N1/THR Switch 11-5 Mode Control Panel Windows 1) Airspeed (IAS/MACH) a) -200/-300

(O) May be inoperative provided command airspeed bug on airspeed indicator (and ADI speed tape, if installed) operates normally on both sides. (O) May be inoperative provided selected airspeed indications on both PFDs operate normally. (O) May be inoperative provided selected airspeed indications on both PFDs operate normally. (Continued)

b) -400ER

c) -200/-300 (STC ST02165NY)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 22 - AUTO FLIGHT 11-5 Mode Control Panel Windows (Contd) 2) Heading (HDG) a) -200/-300 C 1 0 (O) May be inoperative provided selected heading indications on both HSIs operate normally. (O) May be inoperative provided selected heading indications on both PFDs operate normally. (O) May be inoperative provided selected heading indications on both PFDs operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 22-4

b) -400ER

c) -200/-300 (STC ST02165NY) 3) Vertical Speed (VERT SPD) a) -400ER

(O) May be inoperative provided Vertical Speed mode is not selected. (O) May be inoperative provided selected vertical speed indications on both PFDs operate normally. (O) May be inoperative provided selected vertical speed indications on both PFDs operate normally.

b) -200/-300 (STC ST02165NY) 4) Altiitude (ALT) (-400ER) 11-6 Mode Control Panel Switch Lights 1) Autopilot Engage Switch Lights (CMD) 2) Mode Selector Switch Lights

(O) May be inoperative provided selected altitude indications on both PFDs operate normally.

Lights for any two switches may be inoperative. NOTE: A switch with one lamp operational is considered to be operating normally.

B 14-1 Autoland Status Annunciators (-200/-300) C

0 0 May be inoperative provided approach minimums do not require their use.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 22 - AUTO FLIGHT 14-2 Automatic Landing System (AUTOLAND) 1) Triple Channel Autoland (LAND 3) 21-1 Yaw Dampers C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 22-5

May be inoperative provided approach minimums do not require its use.

May be inoperative provided approach minimums do not require its use.

(M) One may be inoperative provided remaining yaw damper is verified to operate normally. NOTE: Airplanes without SB 767-22-7 or production equivalent installed, see AFM Limitations.

21-2

Modal Suppression Systems Thrust Management System (Including Autothrottle System) 1) Autothrottle Servo C 1 0

Deleted, MMEL Rev. 23a.

30-1

(M) May be inoperative provided approach minimums do not require its use.

(M) May be inoperative provided: a) Autothrottles are deactivated, and b) Approach minimums do not require use of autothrottle.

2) Autothrottle Disconnect Switches

(M) May be inoperative provided: a) Autothrottles are deactivated, and b) Approach minimums do not require use of autothrottle. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 22 - AUTO FLIGHT 30-1 Thrust Management System (Including Autothrottle System) (Contd) 3) Thrust Mode Select Panel (-200/-300) a) Derate Switches b) TEMP SEL Selector c) TO/GA Switch d) CLB Switch C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 22-6

C C

1 1

0 0 (O) May be inoperative provided Automatic Climb Thrust Select option is installed and operates normally. (O) May be inoperative provided Max Continuous Thrust is set manually if required.

e) CON Switch

f) CRZ Switch 30-2 Go-Around and Takeoff/Go-Around Switches 1) Go-Around Switches (-200/-300)

(M) One may be inoperative provided: a) Approach minimums do not require its use, and b) Remaining Go-Around switch is verified to operate normally. May be inoperative provided: a) Both thrust levers are operated manually for go-around, and b) Autopilot and Flight Director are not used below 500 feet AGL or applicable approach minimum, whichever is higher. NOTE: Flight Director Go-Around and Windshear guidance are not available with both goaround switches inoperative. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 22 - AUTO FLIGHT 30-2 Go-Around and Takeoff/Go-Around Switches (Contd) 2) Takeoff/GoAround (TO/GA) Switches (-400ER) C 2 1 (M) One may be inoperative provided: a) Approach minimums do not require its use, and b) Remaining TO/GA switch is verified to operate normally. May be inoperative provided: a) Both thrust levers are operated manually for takeoff and go-around, and b) Autopilot and Flight Director are not used below 500 feet AGL or applicable approach minimum, whichever is higher. NOTE: Flight Director Go-Around and Windshear guidance are not available with both goaround switches inoperative. 34-1 Autothrottle Disconnect (A/T DISC) Light C 1 0 May be inoperative provided: a) Associated EICAS annunciation operates normally, and b) Associated aural alert operates normally. May be inoperative provided: a) A/T ARM switch remains OFF, and b) Approach minimums do not require its use. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 22-7

41-1

Maintenance Control Display Panel (MCDP)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 00-1 10-1 *** 11-1 Boom Microphones Radio Tuning Panels (Digital RTP) Communications Systems (VHF, HF, UHF) 1) VHF Comm a) Frequency In Use Light b) Frequency Transfer Switch C 0 C 3 2 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-1

Moved to 23-51-5, MMEL Rev. 29. One may be inoperative provided left Radio Tuning Panel operates normally. Any in excess of those required by FAR, and not powered by a Standby Bus, may be inoperative.

May be inoperative provided associated VHF active frequency can be selected.

Any in excess of those required by FAR, and not powered by a Standby Bus, may be inoperative.

c) Frequency Selector Knob d) Frequency Indication 2) High Frequency (HF) Communication System

Any in excess of those required by FAR may be inoperative.

(O) May be inoperative while conducting operations that require two LRCS provided: a) SATCOM Voice or Data Link operates normally, b) Alternate procedures are established and used, c) SATCOM coverage is available over intended route of flight, and d) If Inmarsat codes are not available while using SATCOM voice, prior coordination with appropriate ATS facility is required. NOTE: SATCOM is to be used only as a backup to normal HF communication unless otherwise authorized by appropriate ATS facilities.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 11-2 *** Flight Deck Communications Systems (Datalink) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-2

(O) May be inoperative provided alternate procedures are established and used.

May be inoperative provided procedures do not require its use. Moved to 23-11-1, MMEL Rev. 7.

12-1

VHF Communications Transmitters & Receivers Emergency Locator Transmitter (ELT) Selective Call System (SELCAL) C 1 0

12-2

Moved to 25-63-10, MMEL Rev. 32.

21-1 ***

(O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. NOTE: Any mode which operates normally may be used.

1) Channels

22-1 ***

ACARS System

***

1) ACARS Printer

(O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used for subsystems.

22-2 ***

Multipurpose Interactive Display Unit

May be inoperative provided procedures do not require its use.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 25-1 *** SAT Communication Systems (Includes (Wingspeed SCS STC ST02534CH) C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-3

(O) May be inoperative provided alternate procedures are established and used.

May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (M)(O) May be inoperative provided alternate procedures are established and used. (M) May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O) May be inoperative provided all messaging data transfers are via SCS Voice (handset).

1) SATCOM Voice

***

2) HF/SAT XFER Switches (P5 Panel)

***

3) SATCOM Lights

4) SCS Aircraft Communication Unit Wingspeed SCS (STC ST02534CH) 5) Cockpit Display Device (CDD) Wingspeed SCS (STC ST02534CH)

(M) May be inoperative provided Master position operates normally.

(O) May be inoperative provided SCS Voice (handset) operates normally. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 25-1 *** SAT Communication Systems (Includes Wingspeed SCS STC ST02534CH) (Contd) 6) Remote Processor Unit (RPU) Wingspeed SCS (STC ST02534CH) C 2 1 (M) May be inoperative provided Master position operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-4

(O) May be inoperative provided SCS Voice (handset) operates normally. NOTE: Any function of system that operates normally may be used.

7) SCS Printer Wingspeed SCS (STC ST02534CH) 25-2 *** Automated Flight Information Reporting System (AFIRS) (STC ST02523NY)

(O) May be inoperative provided alternate procedures are established and used.

May be inoperative provided procedures do not require its use. NOTE: Any portion of system that operates normally may be used.

1) Global Voice SATCOM

(O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. (Continued)

a) Cockpit Dialer Pad

b) Handset

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 25-2 *** Automated Flight Information Reporting System (AFIRS) (STC ST02523NY) (Contd) 1) Global Voice SATCOM (Contd) b) Handset (Contd) 2) Global Messaging D 1 0 May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. NOTE: Any portion of system that operates normally may be used. 31-1 Passenger Address System (PA) 1) Passenger Configuration 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 and visual) operates normally. NOTE: Any station function(s) that operate normally may be used. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-5

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 31-1 Passenger Address System (PA) (Contd) 1) Passenger Configuration (Contd) C 1 0 (O) May be inoperative provided: a) PA not required by FAR, and b) Alternate, normal and emergency procedures, and/or operating restrictions are established and used. NOTE: Any station function(s) that operate normally may be used. a) Lavatory Speakers b) Cabin Speakers C 0 (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided inoperative speakers are not adjacent to each other. (M) No passenger seat, cabin attendant seat or crew rest area bunk may be occupied from which Passenger Address System is not audible and intelligible; seat must be blocked and placarded DO NOT OCCUPY. May be inoperative provided: a) Procedures do not require their use, and b) ALL position operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-6

***

c) Zone Selection Rotary Switch Positions, FWD Attendant Panel 2) All Cargo Configuration (Courier/ Supernumerary Address System)

(O) May be inoperative provided alternate, normal and emergency procedures and/or operating restrictions are established and used.

May be inoperative provided procedures do not require its use. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use.

a) Lavatory Speakers

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 31-2 *** Pre-recorded Passenger Announcement System C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-7

(O) May be inoperative provided alternate procedures are established and used.

May be inoperative provided procedures do not require its use. Moved to 23-51-5, MMEL Rev. 29.

31-3

Headsets/ Microphones (Or Equivalent) Crewmember Interphone Systems 1) Passenger Configuration a) Flight Deck to Cabin, Cabin to Flight Deck Functions B -

40-1

(O) May be inoperative provided: a) Flight deck to cabin and cabin to flight deck interphone functions operate normally on at least fifty percent of cabin handsets, and b) Alternate communication procedures between affected flight attendant stations are established and used. NOTE: Any station function(s) that operate normally may be used.

b) Cabin to Cabin Function

(O) May be inoperative provided: a) Cabin to cabin interphone functions operate normally on at least fifty percent of cabin handsets, and b) Alternate communications procedures between affected flight attendant stations are established and used. NOTE: Any station function(s) that operate normally may be used. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 40-1 Crewmember Interphone Systems (Contd) 1) Passenger Configuration (Contd) c) Flight Deck to Ground Function 1) Large Turbojet Powered Airplanes Operating Under FAR Part 121 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 service interphone jack operates normally. (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 flight interphone jack operates normally. (O) May be inoperative provided alternate procedures are established and used. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-8

2) All Other Aircraft/ Operations

2) All Cargo Configuration a) Flight Deck to Cabin, Cabin to Flight Deck Functions C 1 0 (O) May be inoperative provided alternate, normal and emergency procedures, and/or operating restrictions are established and used,

May be inoperative provided procedures do not require its use. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 40-1 Crewmember Interphone Systems (Contd) 2) All Cargo Configuration (Contd) b) Cabin to Cabin Function c) Flight Deck to Ground Function 1) Large Turbojet Powered Airplanes Operating Under FAR Part 121 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 service interphone jack operates normally. D 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-9

(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 flight interphone jack operates normally. (O) May be inoperative provided alternate procedures are established and used. (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use.

2) All Other Aircraft/ Operations

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 40-2 *** Crew Rest Interphone System and PA Announcement (STCs ST00973WID, ST01994SE) D 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-10

(M) May be inoperative provided: a) Associated crew rest is not used by personnel, and b) Associated crew rest door is locked closed and placarded DO NOT USE - COMM INOP. NOTE: These provisos are not intended to prohibit crew rest inspections by crew members.

1) Pilot Crew Rest (ST00973WI-D)

(O) Either PA or Interphone may be inoperative provided remaining system is verified to operate normally. (O) Either PA or Interphone may be inoperative provided remaining system is verified to operate normally. (M) May be inoperative provided: a) Lower lobe crew rest module is not used and personal items are removed, and b) Lower lobe crew rest door is closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest inspections by crew members.

2) Attendant Crew Rest (ST00973WI-D) 40-3 *** Lower Lobe Crew Rest Interphone System (STC ST01994SE)

41-1

Alerting System (Audio/Visual) 1) Passenger Configuration a) Flight Deck Call Visual Alerting System B 1 0 May be inoperative provided flight deck audio alerting system operates normally. NOTE: Flight deck audio alerting system must always be operative. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 41-1 Alerting System (Audio/Visual) (Contd) 1) Passenger Configuration (Contd) b) Flight Attendant Visual Alerting System 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 (audio or visual) 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 an NEF item. NOTE 2: Any visual alerting system function(s) that operates normally may be used. c) Flight Attendant Audio Alerting System 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 (audio or visual) 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 an NEF item. NOTE 2: Any audio alerting system function(s) that operates normally may be used. 2) All Cargo Configuration a) Flight Deck Call Visual Alerting System B 1 0 May be inoperative provided flight deck audio alerting system operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-11

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 41-1 Alerting System (Audio/Visual) (Contd) 2) All Cargo Configuration (Contd) b) Flight Deck Call System c) Courier/ Supernumerary Visual Alerting System D 1 0 May be inoperative provided courier/supernumerary compartment remains unoccupied. (O) May be inoperative provided: a) Courier/supernumerary address system operates normally, and b) Alternate procedures are established and used. May be inoperative provided courier/supernumerary compartment remains unoccupied. NOTE: Any visual alerting system function(s) that operates normally may be used. d) Courier/ Supernumerary Audio Alerting System B 1 0 (O) May be inoperative provided: a) Courier/supernumerary address system operates normally, and b) Alternate procedures are established and used. May be inoperative provided courier/ supernumerary compartment remains unoccupied. NOTE: Any audio alerting system function(s) that operates normally may be used. e) Main Cargo Deck Crew Aural Warning System B 1 0 May be inoperative provided access to main cargo compartment is prohibited in flight. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-12

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 41-2 Crew Rest Module Call System (STC ST02372AT) 1) Flight Deck to Crew Rest Module/Crew Rest Module to Flight Deck Call Functions C 2 0 (M) May be inoperative provided: a) Crew rest module is not used, and b) Crew rest door is closed and placarded INOPERATIVE DO NOT ENTER. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-13

NOTE: These provisos are not intended to prohibit crew rest area inspections by crewmembers. 2) Flight Deck Visual Alert B 1 0 May be inoperative provided flight deck audio alerting system operates normally.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 42-1 Handset Systems 1) Passenger Configuration *** a) Flight Deck C 1 0 (O) May be inoperative provided: a) Flight deck to cabin communication operates normally, and b) Alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O) May be inoperative provided: a) Fifty percent of cabin handsets operate normally, b) One handset must operate normally at each pair of exit doors, and c) Alternate communication procedures between affected flight attendant stations are established and used. NOTE 1: An operative handset at an inoperative flight attendant seat shall not be counted to satisfy fifty percent requirement. Any handset function that operates normally may be used. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-14

b) Cabin

NOTE 2:

2) All Cargo Configuration *** a) Flight Deck C 1 0 May be inoperative provided flight deck to courier/ supernumerary communication operates normally. May be inoperative provided procedures do not require its use.

***

b) Courier/ Supernumerary

May be inoperative provided courier/supernumerary compartment remains unoccupied.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 43-1 Ground Crew Call System 1) Ground Crew Call Horn 51-1 Flight Deck Interphone System Audio Select Panels Flight Deck Speakers C 2 0 C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-15

(O) May be inoperative provided alternate procedures are established and used. (O) May be inoperative provided alternate procedures are established and used. Moved to 23-40-1, MMEL Rev. 30.

51-2 51-3

Deleted, MMEL Rev. 18. May be inoperative provided: a) Procedures do not require their use, and b) TSO headset earphones/headphones (or equivalent) are installed and operate normally.

51-4

Push-To-Talk (PTT) Switches 1) Control Wheel PTT Switches C 2 1 (M) One may be inoperative provided: a) Associated audio selector panel or glareshield PTT switch operates normally, and b) Affected switch is deactivated. (M) One may be inoperative provided: a) Associated control wheel or glareshield PTT switch operates normally, and b) Affected switch is verified failed open. (M) One may be inoperative provided: a) Associated audio selector panel or control wheel PTT switch operates normally, and b) Affected switch is deactivated. Any Boom and/or Hand Microphones in excess of those required by FAR for flight deck crewmembers may be inoperative or missing. May be inoperative or missing provided: a) Associated hand microphone is installed and operates normally, b) Flight Data Recorder (FDR) operates normally, and c) Repairs are made within three flight days. May be inoperative or missing provided associated boom microphone operates normally. (Continued)

2) Flightcrew Audio Selector Panel PTT Switches *** 3) Glareshield PTT Switches

51-5

Flight Crew Communication Equipment 1) Boom Microphones

2)

Hand Microphones

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 51-5 Flight Crew Communication Equipment (Contd) 2) Hand Microphones (Contd) a) Dual Tone MultiFrequency (DTMF) (Telephone Dialing Feature) D 0 May be inoperative or missing provided procedures do not require its use. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-16

***

(O) May be inoperative provided: a) Voice mode operates normally, and b) Alternate procedures are established and used.

May be inoperative provided procedures do not require its use. Either captains or first officers earphone/ headphone may be inoperative or missing provided associated flight deck speaker operates normally.

3) TSO Headset Earphones/ Headphones 70-1 *** Surveillance Systems (Flight Deck Door, Cabin, Cargo) 1) Flight Deck Door

(M)(O) May be inoperative and components may be missing provided alternate procedures are established and used. NOTE: Any part of system that operates normally may be used.

May be inoperative provided procedures do not require its use. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 23 - COMMUNICATIONS 70-1 *** Surveillance Systems (Flight Deck Door, Cabin, Cargo) (Contd) 2) Cabin/Cargo C 1 0 (M)(O) May be inoperative and components may be missing provided alternate procedures are established and used. NOTE: Any part of system that operates normally may be used. D 1 0 May be inoperative provided procedures do not require its use. May be inoperative provided: a) Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 23-17

71-1

Cockpit Voice Recorder (CVR) System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 00-1 Engine Generator Systems (IDG, GCB) 1) GE and RB211 B 2 1 (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) APU generator operates normally and is used to supply busses of inoperative channel throughout flight, b) All generator control units, including APU, operate normally, c) For ER operations, at least one Hydraulic Motor Generator (HMG) is verified to operate normally, and d) If APU has been operating for an extended period of time in heavy falling or blowing snow, inspect inlet plenum before departure to verify that accumulations of snow or ice are not present. (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) APU generator operates normally and is used to supply busses of inoperative channel throughout flight, b) All generator control units, including APU, operate normally, c) For ER operations, at least one Hydraulic Motor Generator (HMG) is verified to operate normally, d) If APU has been operating for an extended period of time in heavy falling or blowing snow, inspect inlet plenum before departure to verify that accumulations of snow or ice are not present, e) FUEL TEMP indicating system operates normally, f) For engine air oil cooler operating normally, fuel tank temperature remains at or above -37 degrees C, g) For engine air oil cooler open, fuel tank temperature remains at or above -30 degrees C, and h) For either f) or g) configuration, fuel tank temperature must remain above specified minimum throughout entire flight. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-1

2) PW4000

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 00-1 Engine Generator Systems (IDG, GCB) (Contd) 3) JT9D B 2 1 (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) APU generator operates normally and is used to supply busses of inoperative channel throughout flight, b) All generator control units, including APU, operate normally, c) For ER operations, at least one Hydraulic Motor Generator (HMG) is verified to operate normally, d) If APU has been operating for an extended period of time in heavy falling or blowing snow, inspect inlet plenum before departure to verify that accumulations of snow or ice are not present, and e) If IDG is disconnected, manual fuel heat cycle must be completed before takeoff when fuel temperature is below 0 degrees C. Except for ER operations, may be inoperative provided both engine generators operate normally. (M) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Both engine generators operate normally, and b) At least one Hydraulic Motor Generator (HMG) is verified to operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-2

00-2

APU Generator

11-1

Generator DRIVE Lights 1) -200/-300 B 2 1 (M) One may be inoperative off provided associated EICAS message is verified to operate normally. (M) One may be inoperative off provided associated IDG is disconnected.

B 1) -400ER C

2 2

1 0

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 25-1 *** Hydraulic Motor Generators (HMG) 1) Air Data Computer (ADC) Equipped Airplanes C 0 (O) Except for ER operations, may be inoperative provided: a) Center IRS operates normally, and b) First officer's IRS instrument source select switch operates normally. Except for ER operations, may be inoperative for Day VMC flight. (M)(O) For ER operations up to 120 minutes, may be inoperative provided: a) Both engine generators and APU generator operate normally, b) Center IRS operates normally, and c) First officer's IRS instrument source select switch operates normally. (M)(O) For ER operations beyond 120 minutes, may be inoperative provided: a) Both engine generators and APU generator operate normally, b) APU is started before reaching ETOPS segment, then operated continuously until within 60 minutes of a suitable airport, c) Center IRS operates normally, d) First officer's IRS instrument source select switch operates normally, and e) Operations are limited to not more than three flight days before repair is made. (M) Except for ER operations beyond 120 minutes, may be inoperative provided: a) At least one Hydraulic Motor Generator (HMG) is verified to operate normally, and b) Operations are limited to not more than three flight days before repair is made. (M) May be inoperative provided: a) Both engine generators and APU generator operate normally, and b) At least one Hydraulic Motor Generator (HMG) is verified to operate normally. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-3

C C

0 0

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 25-1 *** Hydraulic Motor Generators (HMG) (Contd) 2) Air Data Inertial Reference System (ADIRS) Equipped Airplanes C 1 0 Except for ER operations, may be inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-4

(M) For ER operations up to 120 minutes, may be inoperative provided both engine generators and APU generator operate normally. (M)(O) For ER operations beyond 120 minutes, may be inoperative provided: a) Both engine generators and APU generator operate normally, b) APU is started before reaching ETOPS segment, then operated continuously until within 60 minutes of a suitable airport, and c) Operations are limited to not more than three flight days before repair is made.

25-2 ***

Hydraulic Motor Generator Valves 1) Air Data Computer (ADC) Equipped Airplanes C 0 (M)(O) Except for ER operations, may be inoperative closed provided: a) Center IRS operates normally, and b) First officer's IRS instrument source select switch operates normally. (M) Except for ER operations, may be inoperative closed for Day VMC flight. (M)(O) For ER operations up to 120 minutes, may be inoperative closed provided: a) Both engine generators and APU generator operate normally, b) Center IRS operates normally, and c) First officer's IRS instrument source select switch operates normally. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 25-2 *** Hydraulic Motor Generator Valves (Contd) A 0 (M)(O) For ER operations beyond 120 minutes, may be inoperative closed provided: a) Both engine generators and APU generator operate normally, b) APU is started before reaching ETOPS segment, then operated continuously until within 60 minutes of a suitable airport, c) Center IRS operates normally, d) First officer's IRS instrument source select switch operates normally, and e) Operations are limited to not more than three flight days before repair is made. (M) Except for ER operations beyond 120 minutes, may be inoperative closed provided: a) At least one Hydraulic Motor Generator (HMG) is verified to operate normally, and b) Operations are limited to not more than three flight days before repair is made. (M) May be inoperative closed provided: a) Both engine generators and APU generator operate normally, and b) At least one Hydraulic Motor Generator (HMG) is verified to operate normally. (M) Except for ER operations, may be inoperative closed. . NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-5

2)

Air Data Inertial Reference System (ADIRS) Equipped Airplanes

(M) For ER operations up to 120 minutes, may be inoperative closed provided both engine generators and APU generator operate normally. (M)(O) For ER operations beyond 120 minutes, may be inoperative closed provided: a) Both engine generators and APU generator operate normally, b) APU is started before reaching ETOPS segment, then operated continuously until within 60 minutes of a suitable airport, and c) Operations are limited to not more than three flight days before repair is made.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 27-1 BUS OFF Lights C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-6

(O) One may be inoperative provided Bus Tie ISLN lights and associated GEN CONT OFF light operate normally. (M)(O) One may be inoperative provided associated EICAS message L(R) GEN OFF is verified to operate normally. One may be inoperative for an associated inoperative generator. (O) May be inoperative. (M) May be inoperative provided EICAS message APU GEN OFF is verified to operate normally. May be inoperative provided APU generator is not required for flight. May be inoperative provided associated BUS OFF light operates normally.

27-2

GEN CONT OFF Lights

1) -400ER 27-3 APU GEN OFF Light

C C

2 1

0 0

27-4

BUS TIE ISLN Lights UTILITY BUS OFF Lights Generator FIELD OFF Lights Standby Power Bus OFF Light 1) -200/-300

27-5

27-6 *** 30-1

(M)(O) May be inoperative provided: a) Both EICAS systems operate normally, and b) All other Standby Bus indications are verified to operate normally. (O) May be inoperative.

2) -400ER

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 31-1 APU Battery 1) Airplanes without Main/ APU Battery Tie System Airplanes with Main/ APU Battery Tie System C 1 0 (M)(O) May be inoperative provided: a) APU battery is deactivated or removed, and b) APU is considered inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-7

2)

(M)(O) May be inoperative provided: a) APU battery is deactivated or removed, b) APU is considered inoperative, and c) Operations do not require paralleling of Main and APU batteries.

31-2

APU Battery Charger 1) Airplanes without Main/ APU Battery Tie System Airplanes with Main/ APU Battery Tie System C 1 0 (M) May be inoperative provided: a) APU battery charger is deactivated or removed, and b) APU is not required. (M) May be inoperative provided: a) APU battery charger is deactivated or removed, b) APU is not required, and c) Operations do not require paralleling of Main and APU batteries. May be inoperative provided: a) Operations do not require paralleling of Main and APU batteries, b) Both engine generators operate normally, and c) APU generator operates normally. May be inoperative provided APU is considered inoperative. (M) May be inoperative provided APU TRU is deactivated. (O) May be inoperative provided alternate procedures are established and used.

2)

31-3 ***

Standby Power Main/APU Battery Tie System

32-1 ***

APU Start Transformer Rectifier Unit

32-2 ***

First Officers Display Transformer Rectifier Unit (-400ER)

May be inoperative provided procedures do not require its use.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 24 - ELECTRICAL POWER 41-1 External Power System(s) 1) EXT PWR AVAIL Light (Flight Deck) 2) EXT PWR ON Light (Flight Deck) 3) EXTERNAL POWER CONNECTED Light (External Power Panel) 4) EXTERNAL POWER NOT IN USE Light (External Power Panel) 51-1 Utility Bus Systems (All Cargo Configuration) Voltage Harmonic Filters C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 24-8

(O) May be inoperative provided alternate procedures are established and used.

(O) May be inoperative provided alternate procedures are established and used.

(O) May be inoperative provided alternate procedures are established and used.

(O) May be inoperative provided alternate procedures are established and used.

(M)(O) May be inoperative provided bus is deactivated.

51-2

(M) May be inoperative provided associated individual video system (IVS) zone is deactivated. May be inoperative provided associated video system remains off.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 00-1 Crewmember Shoulder Harness (Flight Deck) Flight Crew Seat 1) Power Adjustment System Manual Adjustment System a) Recline A 2 0 (M) May be inoperative provided: a) Seat is secured in upright position and is acceptable to affected crewmember, b) Fwd/aft and vertical manual adjustment modes operate normally, and c) Repairs are made within two flight days May be inoperative provided: a) Affected armrest is in up position or removed, and b) Seat is acceptable to affected crewmember. May be inoperative provided seat is acceptable to affected crewmember. D 2 0 May be inoperative provided fwd/aft and vertical manual adjustment modes operate normally. D NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-1

Any in excess of those required for flight deck crew members (including official observer in observer's seat) may be inoperative.

11-1 ***

2)

b) Armrest

c) Lumbar, Thigh Supports and Headrest 11-2 Observer Seat(s) 1) Primary Observer Seat (Including Associated Equipment)

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 two flight days. May be inoperative provided: a) Secondary observers seat is available to an FAA inspector for performance of official duties, and b) Repairs are made within two flight days. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 11-2 Observer Seat(s) (Contd) 1) Primary Observer Seat (Including Associated Equipment) (Contd) A 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 two flight days. NOTE 1: These provisos are intended to provide for occupancy of above seats by an FAA inspector when minimum safety equipment (oxygen and safety belt) 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 observer seat(s). *** 2) Additional Observer Seat (Including Associated Equipment) Non-Essential Equipment & Furnishings (NEF) D 0 NOTE: Pilot-in-Command will determine if minimum safety equipment is functional for other persons authorized to occupy additional observer seat(s). NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-2

20-1 ***

May be inoperative, damaged, or missing provided that item(s) is deferred in accordance with operators NEF deferral program. NEF program, procedures, and processes are outlined in operators (insert name) Manual. (M) and (O) procedures, if required, must be available to flight crew and included in operators appropriate document. NOTE: Exterior lavatory door ash trays are not considered NEF items.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 25-1 Flight Attendant Seat Assembly (Single or Dual Position) 1) Required Flight Attendant Seats B (M)(O) One seat position or assembly (dual position) may be inoperative provided: a) Affected seat position 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 assigned duties, c) Alternate procedures are established and used as published in crewmember 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 ONLY. 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. 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 FAR 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) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-3

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 25-1 Flight Attendant Seat Assembly (Single or Dual Position) (Contd) 2) Excess Flight Attendant Seat C (M) May be inoperative provided: 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. 3) All Cargo Configuration D May be inoperative provided affected seat or seat assembly is not occupied. (M) May be inoperative provided: a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to main aircraft aisle, and c) Affected seat(s) is blocked and placarded DO NOT OCCUPY. NOTE 1: A seat with an inoperative seat belt is considered inoperative. NOTE 2: Inoperative seat(s) does not affect required number of Flight Attendants. NOTE 3: Affected seat(s) may include seat(s) behind and/or adjacent outboard seats. 1) Recline Mechanism D (M) May be inoperative and seat occupied provided seat is secured in full upright position. May be inoperative and seat occupied provided seat is immovable in full upright position. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-4

25-2

Passenger Seats

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 25-2 Passenger Seats (Contd) 2) Underseat Baggage Restraining Bars C (M)(O) May be inoperative provided: a) Baggage is not stowed under seat with inoperative restraining bar, b) Associated seat is placarded DO NOT STOW BAGGAGE UNDER THIS SEAT, and c) Procedures are established to alert Cabin Crew of inoperative restraining bar. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-5

3) Armrest a) Armrest with Recline Mechanism D (M) May be inoperative or missing and seat occupied provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to main aircraft aisle, and c) If armrest is missing, seat is secured in upright position. May be inoperative or missing and seat occupied provided: a) Armrest does not block an Emergency Exit, and b) Armrest does not restrict any passenger from access to main aircraft aisle. (M) May be inoperative provided: a) Seat is not occupied, and b) Seat is stowed or secured. (M) May be inoperative provided armrest is stowed in retracted position or removed. (M) May be inoperative and seat occupied provided seat is secured in upright position. Moved to 25-25-2, MMEL Rev. 24.

b) Armrest without Recline Mechanism

25-3 ***

Supernumerary Seats (All Cargo Configuration) 1) Armrests

2)

Recline Mechanism

25-4

Underseat Baggage Restraining Bars Crew Rest Bunk Restraints C 0

25-5

(M) May be inoperative provided associated bunk is blocked and placarded INOPERATIVE DO NOT USE.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 25-6 Crew Rest Module (STC ST02372AT) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-6

(M) May be inoperative provided: a) Crew rest module is not used and personal items are removed, and b) Crew rest door is closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest area inspections by crewmembers.

25-7 ***

Lower Lobe Crew Rest Module (STC ST01994SE)

(M) May be inoperative provided: a) Lower lobe crew rest module is not used and personal items are removed, and b) Lower lobe crew rest door is closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest area inspections by crew members.

1) Crew Rest Seat

(M) May be inoperative provided seat is placarded INOPERATIVE - DO NOT USE. (M) May be inoperative provided: a) Procedures are established to secure compartment CLOSED, b) Associated bin or compartment is prominently placarded DO NOT USE, c) Any emergency equipment located in affected compartment is considered inoperative, and d) Affected compartment is not used for storage of any item(s) except for those permanently affixed. NOTE: For overhead storage compartments, if no partitions are installed, the entire overhead storage compartment is considered one compartment. (Continued) | | | | |

28-1

Storage Bin(s)/ Cabin and Galley Storage Compartments/ Closets

| | | |

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 28-1 Storage Bin(s)/Cabin and Galley Storage Compartment/ Closets (Contd) C (M) May be inoperative provided: a) Affected door(s) is removed, or, for retractable doors, secured in the retracted (fully open) position, b) Associated bin or compartment is not used for storage of any item(s) except for those permanently affixed, c) Associated bin or compartment is prominently placarded DO NOT USE, d) Procedures are established and used to alert crew members and passengers of inoperative bins, and e) Passengers are briefed that associated bin or compartment is not used. NOTE 1: For overhead storage compartments, if no partitions are installed, the entire overhead storage compartment is considered one compartment. NOTE 2: Any emergency equipment located in the associated compartment (permanently affixed) is available for use. 1) Multi Latch/ Quarter Turn Lug Installations C One latch/lug per compartment may be inoperative provided: a) Remaining latch(es)/lug(s) on affected compartments operate normally, and b) If affected compartment is used for a galley cart, cart remains empty. (M) May be inoperative in unlocked position provided doors can be secured by other means. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-7

| | |

| | | |

***

2) Storage Compartment Key Locks

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 38-1 Exterior Lavatory Door Ashtrays 1) Airplanes with More Than One Exterior Lavatory Door Ashtray Installed 2) Airplanes with Only One Exterior Lavatory Door Ashtray Installed 38-2 Galley Waste Receptacle Access Doors/ Covers A One may be missing provided it is replaced within ten calendar days. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-8

May be missing provided it is replaced within three calendar days.

(M)(O) May be inoperative provided: a) Container is empty and access is secured to prevent waste introduction into compartment, and b) Procedures are established to ensure that sufficient galley waste receptacles are available to accommodate all waste that may be generated on flight. (M) May be inoperative provided: a) Associated lavatory waste container is empty and access is secured to prevent waste introduction into waste container, b) Lavatory is only used by crewmembers, and c) Associated lavatory entrance door is locked closed and placarded INOPERATIVE DO NOT USE. NOTE: These provisos are not intended to prohibit lavatory use or inspections by crewmembers.

41-1

Lavatory Waste Container Flapper/Access Doors

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 50-1 Lower Cargo Compartment Lining Panels, Floor Panels, and Walkways 1) Lining Panels C (O) May be damaged or missing provided procedures are established 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. 2) Floor Panels and Walkways a) Airplanes with Full Floors C (O) May be damaged or missing provided procedures are established 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. b) Airplanes with Partial Floors 53-1 *** 54-1 Cargo Loading Systems Cargo Restraint Systems/Devices (Including Main Deck 9 "g" Barrier Net) C May be damaged or missing. | NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-9

NOTE: Any portion of system(s) that operates normally may be used. (M) May be inoperative, or missing provided: a) Acceptable cargo loading limits from an approved source, i.e. an approved Cargo Loading Manual, Cargo Handling Manual, or Weight and Balance Document are observed, and b) Repairs are made prior to the completion of the next heavy maintenance visit. May be inoperative or missing provided associated cargo compartment remains empty. | | | | | | | |

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 55-1 Main Deck 9 "g" Barrier Net System Flight Crew/ Supernumerary Escape Devices (All Cargo Configuration) 1) Inertial Escape Reels C (M) May be inoperative provided: a) Occupants are limited to number of operative escape reels, and b) Inoperative escape reel(s) is removed from installed location. (M) May be inoperative provided: a) Occupants are limited to number of operative escape harness(es), and b) Inoperative escape harness(es) is removed from installed location. (M) May be inoperative provided: a) Lower lobe crew rest module is not used and personal items are removed, and b) Lower lobe crew rest door is closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest area inspections by crew members. 62-1 Flotation Equipment (Crew and Passengers) Megaphones 1) Passenger Configuration D Any in excess of those required by FAR may be inoperative or missing provided: a) Inoperative megaphone is removed from passenger cabin, and b) Required distribution is maintained. D Any in excess of those required by FAR may be inoperative or missing provided required distribution is maintained. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-10

Moved to 25-54-1, MMEL Rev. 31.

61-1

2)

Escape Harnesses

61-2 ***

Lower Lobe Crew Rest Escape Harness (STC ST01994SE)

63-1

2) All Cargo Configuration

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 63-2 ***. Emergency Evacuation Signal System C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-11

(O) May be inoperative provided alternate procedures for initiating an emergency evacuation are established and used. May be inoperative provided procedures do not require its use. One or more signs or placards may be illegible or missing provided a legible sign or placard is visible from each occupied passenger seat. May be inoperative or missing provided crewmember assigned to associated seat has a flashlight of equivalent characteristics readily available. (O) May be inoperative provided alternate procedures are established and used.

63-3

Fasten Seat Belt While Seated Signs or Placards Flight Attendant Flashlight/Holder Assemblies Onboard Weight and Balance System (All Cargo Configuration) Emergency Assurance Vision System (EVAS) (STC ST00731LA) Emergency Locator Transmitter (ELT) 1) Survival Type ELTs 2) Fixed ELTs

63-4

63-5 ***

63-6 ***

May be inoperative or removed provided procedures do not require its use.

63-10

Any in excess of those required by FAR may be inoperative or missing. (M) May be inoperative provided: a) System is deactivated, and b) Repairs are made within 90 days. May be missing provided repairs are made within 90 days. (M) Any in excess of those required by FAR may be inoperative provided system is deactivated. Any in excess of those required by FAR may be missing.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 25 - EQUIPMENT AND FURNISHINGS 64-1 Emergency Medical Equipment 1) First Aid Kit (FAK) and/or Associated Equipment A (O) If more than one is required by FAR, only one of required first aid kits may be incomplete, missing or inoperative provided: a) FAK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within three flight cycles. Any in excess of those required by FAR may be incomplete, missing or inoperative. (O) May be incomplete, missing or inoperative provided: a) EMK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within three flight cycles. Any in excess of those required by FAR may be incomplete, missing or inoperative. (O) May be incomplete, missing or inoperative provided: a) AED is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within three flight cycles. Any in excess of those required by FAR may be incomplete, missing or inoperative. (M) May be inoperative provided: a) Overwing escape system is verified to operate normally, and b) Operations are limited to not more than 50 flight hours before repairs are made. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 25-12

2) Emergency Medical Kit (EMK) and/or Associated Equipment

3) Automated External Defibrillators (AED) and/or Associated Equipment

66-3

Overwing Escape Squib Test System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 10-1 Crew Rest Smoke Detection Systems (STC ST00973WID) C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-1

(M) May be inoperative provided: a) Associated crew rest area is not used and personal items are removed, and b) Associated crew rest door is locked closed and placarded INOPERATIVE - DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest area inspections by crewmembers.

10-2

Crew Rest Module Smoke Detection Systems (STC ST02372AT)

(M) May be inoperative provided: a) Crew rest module is not used and personal items are removed, and b) Crew rest door is closed and placarded INOPERATIVE - DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest area inspections by crewmembers.

10-3 ***

Lower Lobe Crew Rest Smoke Detection Systems (STC ST01994SE)

(M) May be inoperative provided: a) Heater system is deactivated. b) Crew rest module is not used and personal items are removed, and c) Crew rest door is closed and placarded INOPERATIVE - DO NOT ENTER NOTE: These provisos are not intended to prohibit crew rest area inspections by crewmembers.

11-1

Engine Fire Detection Systems 1) Detection Loops C 4 2 Except for ER operations beyond 120 minutes, one loop per engine may be inoperative.

11-2

Engine Overheat Detection Systems 1) Detection Loops C 4 2 Except for ER operations beyond 120 minutes, one loop per engine may be inoperative.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 12-1 Engine Strut Overheat Detection Systems (RB211) 1) Detection Loops C 4 2 Except for ER operations beyond 120 minutes, one loop per engine may be inoperative. (M) Indication may be inoperative provided smoke sampling system integrity is verified before each departure. May be inoperative provided APU is considered inoperative. (M)(O) May be inoperative provided: a) Other procedures do not require use of APU, b) APU is used for ground operations only, c) APU is continuously monitored by ground personnel when operating, d) APU external control system operates normally, and e) APU is not used during taxi. Except for ER operations beyond 120 minutes, one loop per engine may be inoperative. (O) May be inoperative provided procedures are established 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. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-2

14-1

CARGO DET AIR Indicating System

15-1

APU Fire Detection System

1) Detection Loops

16-1

Lower Cargo Compartment Fire Detection Systems (Fwd and Aft)

1)

Detectors a) -200/-300 C 4 2 (O) One in each compartment may be inoperative provided remaining detector is verified to operate normally before each departure. One in each compartment zone may be inoperative. (Continued)

b) -400ER

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 16-1 Lower Cargo Compartment Fire Detection Systems (Fwd and Aft) (Contd) 2) Detector Loops (ATC A1NM -200 SF, -300BCF) 3) Detector Fans a) -200/-300 b) -400ER 16-2 Main Deck Cargo Compartment Fire Detection System (All Cargo Configuration) C C C 4 8 1 2 4 0 One in each compartment may be inoperative. One in each compartment zone may be inoperative. (O) May be inoperative provided procedures are established 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. C 4 2 (O) One in each compartment may be inoperative provided remaining detector loop is verified to operate normally before each departure. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-3

1)

Loops

(M) One detector loop may be inoperative provided remaining detector loop is verified to operate normally before each departure. (O) One detector in each zone may be inoperative provided the remaining detector in that zone is verified to operate normally before each departure. May be inoperative provided BTMS operates normally. NOTE: Avoid possibility of retracting an overheated wheel by monitoring brake temperature indications.

2)

Detectors (-300BDSF)

16

17-1

Wheel Well Fire Detection System

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 17-1 Wheel Well Fire Detection System (Contd) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-4

(M) May be inoperative provided an accepted procedure is used to ensure brakes are cool before engine start. NOTE 1: Avoid possibility of retracting an overheated wheel by leaving landing gear extended for ten minutes after takeoff. Pilots must consider possibility of ice accumulation with landing gear extended during winter operations. NOTE 2: In case of engine failure after V1, landing gear should be retracted until takeoff obstacles are cleared.

18-1

DUCT LEAK Detection Systems 1) L and R Loops C A 4 2 1 One loop in each system may be inoperative. (M)(O) May be inoperative provided: a) Associated ENG BLEED switch remains OFF, b) Associated bleed ISLN valve remains closed except for engine start, c) Airplane is not operated in known or forecast icing conditions, d) Airplane remains at or below FL 270, e) APU is used as an air source during takeoff and landing, f) One body loop operates normally, g) For GE and PW engines, associated fan air modulation valve is secured in intermediate position, h) For GE and PW engines, appropriate performance adjustments are applied, and i) Operation is limited to one flight day before repairs are made. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 18-1 DUCT LEAK Detection Systems (Contd) 1) L and R Loops (Contd) A 1 (M)(O) May be inoperative provided: a) Associated ENG BLEED switch remains OFF, b) Associated bleed ISLN valve remains closed except for engine start, c) Airplane is not operated in known or forecast icing conditions, d) Airplane remains at or below FL 270, e) ADP inoperative penalties are applied, f) Center Hydraulic Motor Generator (HMG) is considered inoperative, g) One body loop operates normally, h) For GE and PW engines, associated fan air modulation valve is secured in intermediate position, i) For GE and PW engines, appropriate performance adjustments are applied, and j) Operation is limited to one flight day before repairs are made. (O) May be inoperative provided: a) Associated ENG BLEED switch remains OFF, b) Associated bleed ISLN valve remains closed except for engine start, c) Airplane is not operated in known or forecast icing conditions, d) Airplane remains at or below FL 270, e) APU is used as an air source during takeoff and landing, f) One body loop operates normally, g) For GE and PW engines, appropriate performance adjustments are applied for an open fan air modulation valve, and h) Operation is limited to one flight day before repairs are made. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-5

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 18-1 DUCT LEAK Detection Systems (Contd) 1) L and R Loops (Contd) A 1 (O) May be inoperative provided: a) Associated ENG BLEED switch remains OFF, b) Associated bleed ISLN valve remains closed except for engine start, c) Airplane is not operated in known or forecast icing conditions, d) Airplane remains at or below FL 270, e) ADP inoperative penalties are applied, f) Center Hydraulic Motor Generator (HMG) is considered inoperative, g) One body loop operates normally, h) For GE and PW engines, appropriate performance adjustments are applied for an open fan air modulation valve, and i) Operation is limited to one flight day before repairs are made. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-6

2) Body Loop

C C

2 -

1 0 (O) May be inoperative provided: a) APU is not used as a pneumatic source except as required for engine start, b) APU bleed air switch remains off except as required for engine start, c) Center bleed ISLN valve remains closed except as required for engine start, d) ADP inoperative performance penalties are applied, e) Both center electric pumps operate normally, f) Airplane remains at or below FL 270, g) Center Hydraulic Motor Generator (HMG) is considered inoperative, and h) One L and one R loop operate normally. (M) May be inoperative provided detection system is verified to operate normally once each flight day. (O) May be inoperative.

3) Test Function

4) DUCT LEAK Lights (-400ER)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 20-1 Engine Fire Extinguisher Bottle Pressure Indicating System 1) Lower Cargo Compartment 2) APU 20-2 Fire Extinguisher SQUIB TEST System C 1 0 C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-7

(M) May be inoperative provided an acceptable test procedure is used once each flight day to verify that associated bottle is properly charged.

Moved to 26-23-1, MMEL Rev. 32.

Moved to 26-22-1, MMEL Rev. 32. (M) May be inoperative or individual test functions may be inoperative provided each squib circuit associated with an inoperative test function is verified to operate normally once each flight day. May be inoperative provided APU is considered inoperative. May be inoperative provided extinguisher system is inoperative. (O) May be inoperative provided procedures are established 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.

1) APU Squib Test Functions 2) Cargo Squib Test Functions

22-1

APU Fire Extinguisher System

Except for ER operations, may be inoperative provided APU is considered inoperative. Except for ER operations beyond 120 minutes, may be inoperative provided APU is considered inoperative.

***

1) Fire Extinguisher Bottle (Two Bottle System) 2) Fire Extinguisher Bottle Pressure Indicating System

(M) May be inoperative provided an acceptable test procedure is used once each flight day to verify that associated bottle(s) is properly charged.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 23-1 Lower Cargo Compartment Fire Extinguisher System (Metered or NonMetered) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-8

(O) May be inoperative provided 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.

1) Fire Extinguisher Bottles (Two and Three Bottle Systems) (-200/ -300) 2) Fire Extinguisher Bottles (Four Bottle System) (-400ER)

(O) Extinguisher bottle No. 2 or 2A may be inoperative with cargo carried in compartments provided: a) Airplane is operated pressurized, and b) A chart is provided to determine time airplane must remain in proximity to a suitable airport. (M)(O) Extinguisher bottle No. 2, 2A or 2B may be inoperative deactivated with cargo carried in compartments provided: a) Airplane is operated pressurized, and b) A chart is provided to determine time airplane must remain in proximity to a suitable airport. (M) May be inoperative provided an acceptable test procedure is used once each flight day to verify that associated bottle(s) is properly charged. May be inoperative provided associated fire bottle(s) is considered inoperative. (M) May be inoperative provided: a) Associated bottle is verified full, and b) Associated bottle squib is verified to operate normally before each departure. (M)(O) May be inoperative deactivated provided procedures are established 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.

3) Fire Extinguisher Bottle Pressure Indicating System

4) Bottle Pressure Switches (-400ER)

23-2

Lower Cargo Compartment Fire Extinguisher Flow Valves (Forward or Aft) (-400ER)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 26 - FIRE PROTECTION 26-1 Portable Fire Extinguishers D NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 26-9

Any in excess of those required by FAR may be inoperative or missing provided: a) Inoperative fire extinguisher is tagged inoperative, removed from installed location, and placed out of sight so it can not be mistaken for a functional unit, and b) Required distribution is maintained.

26-2

Lavatory Fire Extinguisher Systems 1) Passenger Configuration C 0 For each lavatory, lavatory fire extinguisher system may be inoperative provided associated Lavatory Smoke Detector System operates normally. (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 provisos are not intended to prohibit lavatory use or inspections by crewmembers. 2) All Cargo Configuration D 0 | | | |

26-3

Lavatory Smoke Detection Systems 1) Passenger Configuration C (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 provisos are not intended to prohibit lavatory use or inspections by crewmembers. | | | |

2)

All Cargo Configuration

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 27 FLIGHT CONTROLS 03-1 FLT CONTROL SHUTOFF Valves FLT CONTROL SHUTOFF OFF Lights Control Surface Position Indicating System Flap Position Indicator System 1) Position Needles (-200/-300) C 2 1 C 6 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 27-1

(M) May be inoperative open.

03-2

(M) May be inoperative provided associated valve is verified open before each departure.

08-1

(M) May be inoperative provided a visual flight control check is accomplished before each departure.

08-2

2) Position Sensors (-400ER) 09-1 Yaw Damper Stabilizer Trim Module (YSM)

(M)(O) One may be inoperative. NOTE: Associated autopilot will not engage until Approach Mode engages.

11-1

Aileron Trim System

(M) May be inoperative provided: a) One autopilot operates normally, and b) Aileron trim system is verified centered. (M)(O) May be inoperative unlocked provided maximum airspeed is limited to 270 KIAS or 0.73 Mach, whichever is less. (M)(O) May be inoperative provided aileron lockout system is verified to operate normally before each departure.

11-2

Outboard Aileron Lockout System

1) Indication System

21-1

Rudder Ratio Light

(M) May be inoperative off provided: a) RUDDER RATIO message on EICAS is verified to operate normally, and b) Both control channels operate normally.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 27 FLIGHT CONTROLS 21-3 Rudder Trim Indication System C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 27-2

(M) May be inoperative provided: a) Rudder trim actuator operates normally, b) Rudder control surface position indicating system operates normally, and c) Rudder trim is verified to be centered before each departure. (O) May be inoperative provided: a) Appropriate takeoff center of gravity restrictions are observed, and b) Improved Climb takeoffs are not conducted. (M) May be inoperative provided operation of associated system is verified once each flight day. (M) One may be inoperative provided: a) Remaining system is verified to operate normally before each departure, and b) Operations are limited to not more than three flight days before repair is made. (M) One may be inoperative on non-flying pilot's side provided stabilizer trim system is verified to operate normally. (M)(O) One may be inoperative provided: a) Horizontal stabilizer trim operates normally using stabilizer trim levers (Alternate Stabilizer Trim Switches), b) Approach minimums do not require use of three autopilots, and c) No arm or control valves are failed in energized position. One may be inoperative provided faulty indicator is not visible.

31-1

Elevator Feel Pressure Takeoff Limit Function (-400ER) Stall Warning Test Systems Stall Warning Systems (-400ER)

32-1

32-2

41-1

Control Wheel Trim Switch Systems

41-2

Horizontal Stabilizer Primary Trim Channels

48-1

STAB TRIM Indicators

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 27 FLIGHT CONTROLS 51-1 Automatic Flap Load Relief Retraction System (Trailing Edge) 1) -200/-300 (Actuator Rod End Down) C 1 0 (M) May be inoperative in normal (actuator extended) position provided flaps 30 are not used. NOTE: Flaps 25 may be used to AFM limit maximum landing weight. 2) -300 (Actuator Rod End Up) C 1 0 (M)(O) May be inoperative in normal (actuator retracted) position provided flaps 25 and flaps 30 adjusted maximum landing weights are observed. (M)(O) May be inoperative in normal (actuator retracted) position provided flaps 20, flaps 25 and flaps 30 adjusted maximum landing weights are observed. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 27-3

3) -400ER (Actuator Rod End Up)

61-1

Spoiler Systems 1) Speed Brake Load Alleviation System (-300/ -300F with Blended Winglets) STC ST01920SE C 1 0 (M)(O) May be inoperative provided: a) Speedbrake handle forces are verified normal from full down to full up position, and b) Airspeed does not exceed 290 KIAS, or .84 Mach, whichever is lower, when inflight gross weight is in excess of 340,000 pounds (154,545kg).

62-1

Auto Speed Brake System 1) Airplanes without Speed Brake Load Alleviation System C 1 0 (M)(O) May be inoperative provided: a) System is deactivated, and b) AFM decrements are applied if landing performance requires use of auto speed brakes. (M)(O) May be inoperative provided: a) System is deactivated, b) AFM decrements are applied if landing performance requires use of auto speed brakes, and c) Airspeed does not exceed 290 KIAS, or .84 Mach, whichever is lower, when inflight gross weight is in excess of 340,000 pounds (154,545kg).

2) Airplanes with Speed Brake Load Alleviation System (-300/ -300F with Blended Winglets) STC ST01920SE

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 27 FLIGHT CONTROLS 62-2 Speedbrake Caution Indication System C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 27-4

(O) May be inoperative provided speedbrake lever is not positioned beyond ARMED position inflight below 800 feet radio altitude or when landing flaps are extended. (M) May be inoperative provided associated EICAS message is verified to operate once each flight day.

63-1

AUTO SPDBRK, SPOILERS, and STAB TRIM Lights Leading Edge Slat Skew/Loss Detection System

81-1 ***

(M) May be inoperative deactivated provided leading edge slat system is verified to operate normally.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 11-1 21-1 Sump Drain Valves Pressure Fueling System 1) Fuel Shutoff Valves C C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-1

(M) One may be inoperative closed. (M) May be inoperative provided alternate procedures are established and used. (M) May be inoperative closed. (M) May be inoperative open if fuel jettison system is deactivated or not installed. May be inoperative or missing provided no leakage can be detected after refueling is complete. (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) Inoperative pump is deactivated, b) Both main tank quantity indications operate normally, and c) Following minimum fuel quantities are retained in affected tank for flight condition shown: With fuel tank dams installed (SB 767-28-11 or production equivalent): TAKEOFF - 10,000 lb. (4,540 kg) LANDING - 5,000 lb. (2,270 kg) Without fuel tank dams: TAKEOFF - 25,000 lb. (11,340 kg) LANDING - 7,000 lb. (3,175 kg)

C C

6 6

0 0

21-2 *** 22-1

Fueling Receptacle Cap Main Tank Fuel Pumps

1) Automatic Function of Left FWD Pump

(O) May be inoperative provided alternate procedures are established and used.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 22-2 Center Tank Fuel Pumps C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-2

(M)(O) One may be inoperative with center tank fueled provided: a) Fuel quantity in main tanks is adequate to reach a suitable airport if remaining 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) For -200/-300, low PRESS light operates normally on remaining pump, e) Center tank quantity indication operates normally, f) One crossfeed valve is open prior to takeoff and remains open until center tank pump is selected OFF, and g) Affected pump is deactivated. (M) May be inoperative provided: a) Center tank remains empty, b) Center tank is verified to be empty before each refueling, and c) Affected pumps are deactivated. (M) May be inoperative provided: a) Center tank remains empty, b) Center tank scavenge system is installed and operates normally, and c) Center tank fuel pumps are deactivated.

1) Airplanes with Service Bulletins 767-28-0052 or 767-28-0062 or Production Equivalent Installed 2) Airplanes Subject to Airworthiness Directive 200115-08 a) Airplanes without Automatic Shut Off System

(M) May be inoperative provided: a) Boeing Alternative Method of Compliance to Airworthiness Directive 2001-15-08 (Operations Manual Bulletin Center Tank Fuel Pumps) is in effect, b) Center tank is verified to contain less than 5,000 pounds (2,300 kg) of fuel, c) Center tank fuel is not used, and d) Affected pumps are deactivated.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 22-3 *** Dual Fuel Crossfeed Valves C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-3

(M)(O) One may be inoperative provided: a) Affected valve is secured closed, b) Remaining valve operates normally, and c) For ER operations, remaining valve is exercised during last hour of flight. May be inoperative provided center tank remains empty.

22-4

Center Tank Float Operated Shutoff Valves Automatic Shut Off System (Service Bulletins 76728A0083, 76728A0084, or Production Equivalent Installed)

22-5

May be inoperative provided associated center tank fuel pump is considered inoperative.

May be inoperative provided center tank remains empty. May be inoperative.

1) Airplanes Not Subject to Airworthiness Directive 2001-15-08

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 22-5 Automatic Shut Off System (Service Bulletins 76728A0083, 76728A0084, or Production Equivalent Installed) (Contd) 2) Airplanes Subject to Airworthiness Directive 2001-15-08 C 2 0 (O) May be inoperative with center tank fueled provided: a) Center tank fuel pump low PRESS lights operate normally, b) Center tank quantity indication operates normally, c) Center tank pumps are OFF for takeoff if center tank fuel is less than 5,000 pounds (2,300 kg) with airplane readied for initial taxi, d) Center tank fuel pumps are repositioned ON above 10,000 feet or after pitch attitude has been reduced to begin acceleration to climb speed, if more than 1,000 pounds (500 kg) remain in center tank, e) Both center tank fuel pumps are positioned OFF at first indication of fuel pump low pressure, f) Both center tank pumps are selected OFF when center tank fuel quantity reaches 1,000 pounds (500 kg) of fuel during climb, cruise or descent, g) In cruise and only when required to extinguish the FUEL CONFIG light and EICAS FUEL CONFIG message, both center tank pumps are selected OFF when center tank fuel quantity reaches 800 pounds (400 kg) of fuel, and h) For airplanes not equipped with a scavenge system, 1,000 pounds (500 kg) of center tank fuel is considered unusable. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-4

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 22-6 Universal Fault Interrupter (UFI) (STC ST TBD) APU (DC) Fuel Pump C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-5

May be inoperative provided associated Center Tank Boost Pump is considered inoperative.

25-1

(M) May be inoperative deactivated provided both left fuel tank boost pumps operate normally when APU is required for dispatch. (M) May be inoperative provided: a) APU is considered inoperative, and b) Valve is secured closed. (M) May be inoperative provided valve is secured closed. (M) May be inoperative closed. (M)(O) May be inoperative provided a) Jettison nozzle valves are secured closed, and b) Jettison transfer valves are secured closed. (M)(O)May be inoperative provided both center tank fuel pumps operate normally if center tank is used.

25-2

APU Fuel Shutoff Valve

25-3 *** 26-1 31-3 ***

APU Fuel Isolation Valve Defuel Valves Fuel Jettison System

C C

0 0

1) Center Tank Jettison Pumps 40-1 Crossfeed VALVE Light(s) 1) Single VALVE Installation

(M) Except for ER operations, may be inoperative provided: a) Crossfeed valve is verified to operate normally, and b) Both main fuel quantity indications operate normally. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 40-1 Crossfeed VALVE Light(s)(Contd) 2) Dual VALVE Installation a) -200/-300 C 2 1 (M) May be inoperative provided: a) One crossfeed valve is verified to operate normally, and b) Both main fuel quantity indications operate normally. (M) Except for ER operations, may be inoperative provided: a) Both crossfeed valves are verified to operate normally, and b) Both main fuel quantity indications operate normally. May be inoperative provided: a) One crossfeed valve operates normally, and b) Both main fuel quantity indications operate normally. Except for ER operations, may be inoperative provided: a) Both crossfeed valves operate normally, and b) Both main fuel quantity indications operate normally. (M) May be inoperative provided spar valve is verified to operate normally once each flight day. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-6

b) -400ER

40-2

SPAR VALVE Lights (-200/-300)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 41-1 Fuel Tank Quantity Indication Systems (Flight Deck) 1) Main Tank Indicators C 2 1 (M)(O) Except for ER operations, one may be inoperative provided: a) Fuel quantity in associated tank is verified by an alternate procedure, b) For non-PIP and non-Pegasus FMCs, both EICAS computers operate normally, c) Fuel flow indications operate normally, d) FMC FUEL is initialized with known total fuel quantity, e) Procedures to identify and contain an inflight engine fuel leak are used, f) All main tank boost pumps operate normally, g) For -200/-300, fuel pump low PRESS lights for associated tank operate normally, h) For Pegasus FMCs with Operational Program Software part number 3418-HNP-02C-08 or earlier, Thrust Management System operates normally, and i) For airplanes with Service Bulletin 767-080062, or production equivalent, center tank remains empty. NOTE: FUEL CONFIG advisory message for lateral imbalance may be inhibited. 2) Center Tank Indicator C 1 0 (M) May be inoperative provided: a) Center tank remains empty, b) Center tank scavenge system is installed and operates normally, and c) Center tank fuel pumps are deactivated. (Continued) | NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-7

| |

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 41-1 Fuel Tank Quantity Indication Systems (Flight Deck) (Contd) 2) Center Tank Indicator (Contd) a) Airplanes with Automatic Shut Off System (Service Bulletin 76728A0083, 767-28A0084, or Production Equivalent Installed) C 1 0 (M)(O) Except for ER operations, may be inoperative provided: a) Fuel quantity in associated tank is verified by an alternate procedure, b) Fuel flow indications operate normally, c) FMC FUEL is initialized with known total fuel quantity, d) Both main tank indicators operate normally, e) Procedures to identify and contain an inflight engine fuel leak are used, f) Both center tank boost pumps operate normally, and g) Center tank fuel pump low PRESS lights operate normally. (M) May be inoperative provided: a) Boeing Alternative Method of Compliance to Airworthiness Directives 2001-15-08 (Operations Manual Bulletin Center Tank Fuel Pumps) is in effect, b) Center tank is verified to contain less than 5,000 pounds (2,300 kg) of fuel, and c) Center tank fuel is not used. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-8

| |

b) Airplanes Subject to AD 2001-15-08 and without Automatic Shut 0ff System

| | |

3) Fuel Quantity Densitometers a) Honeywell C 3 0 (M) May be inoperative provided associated densitometer(s) is deactivated.

b) B.F. Goodrich (Simmonds)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 41-2 Fuel Quantity Processor Channels 1) Honeywell FQIS B 2 1 (M)(O) Except for ER operations, one channel may be inoperative provided: a) Total fuel quantity is determined by measuring sticks or other acceptable means after each refueling, and agrees with fuel quantity indications, b) Inoperative channel is deactivated by an acceptable procedure, c) All flight deck fuel indications operate normally, d) For non-PIP and non-Pegasus FMCs, both EICAS computers operate normally, e) Fuel flow indications operate normally, f) FMC TOTALIZER FUEL quantity agrees with fuel quantity indications, and g) For Pegasus FMCs with Operational Program Software part number 3418-HNP-02C-08 or earlier, Thrust Management System operates normally. (O) Except for ER operations, one channel may be inoperative provided: a) All flight deck fuel indications operate normally, b) For non-PIP and non-Pegasus FMCs, both EICAS computers operate normally, c) Fuel flow indications operate normally, d) FMC TOTALIZER FUEL quantity agrees with fuel quantity indications, and e) For Pegasus FMCs with Operational Program Software part number 3418-HNP-02C-08 or earlier, Thrust Management System operates normally. (M) May be inoperative provided alternate fueling procedures are established and used. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-9

2) B.F. Goodrich (Simmonds) FQIS

41-6

Fuel Quantity Indications (Fueling Panel)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 28 - FUEL 41-7 Total Fuel Quantity Indication C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 28-10

(O) May be inoperative provided: a) FMC is initialized with known total fuel quantity, b) For non-PIP and non-Pegasus FMCs, both EICAS computers operate normally, c) Fuel flow indications operate normally, d) Both FMCs operate normally, and e) For Pegasus FMCs with Operational Program Software part number 3418-HNP-02C-08 or earlier, Thrust Management System operates normally. (O) May be inoperative provided: a) Main tank fuel quantity indicators operate normally, and b) Center tank fuel quantity indicator is considered inoperative. May be inoperative for an associated inoperative pump. (M) May be inoperative provided associated EICAS message is verified to operate normally once each flight day.

42-1

Fuel Pump Low PRESS Lights 1) -200/-300

2) -400ER 43-1 FUEL TEMP Indicating System

C C

6 1

0 0 (O) May be inoperative provided Total Air Temperature (TAT) is used as an indication of fuel temperature. NOTE: Static Air Temperature may be used provided appropriate ram rise factor is applied.

44-1

Measuring Sticks

16

May be inoperative provided fuel quantity is determined by other approved means.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 29 - HYDRAULICS 11-1 Engine Driven Hydraulic Pumps 1) Depressurization Function 11-2 Center System (Electric) Hydraulic Pumps Air Driven Pump (ADP) C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 06/18/2009 MASTER MINIMUM EQUIPMENT LIST 33a PAGE: 29-1

Only pump No. 2 may be inoperative provided Air Driven Pump operates normally.

11-3

(M)(O) May be inoperative provided: a) Center Hydraulic Motor Generator (HMG) is not required, b) Both center system electric pumps operate normally, and c) Appropriate performance adjustments are applied.

11-4

ADP Controller 1) AUTO Function C 1 0 (O) May be inoperative provided: a) Control is ON for takeoff and landing, b) Center Hydraulic Motor Generator (HMG) is not required, or control is ON continuously when HMG is required, c) OFF position operates normally, and d) Appropriate performance adjustments are applied. May be inoperative provided: a) AUTO and OFF functions of ADP operate normally, and b) Center HMG is not required.

2) ON Function

11-5

Electric Demand Pump (ACMP) 1) AUTO Function B 2 1 One may be inoperative provided: a) Pump operates normally, and b) Associated pump is selected ON and remains on.

18-1

Remote Quantity Indicator Power Transfer Unit (PTU)

24-1

Deleted, MMEL Rev. 9.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 29 - HYDRAULICS 31-1 Hydraulic Low SYS PRESS Lights 1) Non-PTU Equipped Airplanes C 3 0 (M) May be inoperative provided: a) Associated pump low PRESS lights operate normally, and b) Associated HYD SYS PRESS EICAS indication is verified to operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 06/18/2009 MASTER MINIMUM EQUIPMENT LIST 33a PAGE: 29-2

2) PTU Equipped Airplanes a) Left Low SYS PRESS Light C 1 0 (M) May be inoperative provided: a) Associated pump low PRESS lights operate normally, b) Associated HYD SYS PRESS EICAS indication is verified to operate normally, and c) Left low pressure signal wire of PTU system is capped and stowed. (M) May be inoperative provided: a) Associated pump low PRESS lights operate normally, and b) Associated HYD SYS PRESS EICAS indication is verified to operate normally.

b) Right Low SYS PRESS Light

31-2

Pump Low PRESS Indication Systems 1) Left, Center, Right, and Air Driven Pump PRESS Lights C 7 4 (O) One in each hydraulic system may be inoperative provided: a) Associated low SYS PRESS light operates normally, and b) Associated pump is verified to operate normally before each departure. (O) One may be inoperative provided: a) Associated demand pump AUTO function is considered inoperative, b) Associated low SYS PRESS light operates normally, and c) Associated pump is verified to operate normally before each departure. (Continued)

2) Engine Driven Pump Indication Systems

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 29 - HYDRAULICS 31-2 Pump Low PRESS Indication Systems (Contd) 3) Center System No. 2 Electric Pump Indication System 4) Air Driven Pump (ADP) Indication System C 1 0 May be inoperative provided: a) Air Driven Pump operates normally, and b) Associated pump is selected OFF. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 06/18/2009 MASTER MINIMUM EQUIPMENT LIST 33a PAGE: 29-3

(O) May be inoperative provided: a) Both center system Electric Pumps operate normally, b) ADP is selected OFF, c) Center Hydraulic Motor Generator (HMG) is not required, and d) Appropriate performance adjustments are applied.

31-3 *** 32-1

HYD PRESS Indications (EICAS) Pump OVHT Indication Systems 1) Left, Center, Right, and Air Driven Pump OVHT Lights

(O) One in each hydraulic system may be inoperative provided: a) Associated low SYS PRESS light or pump low PRESS light operates normally, and b) Associated pump is verified to operate normally before each departure. May be inoperative provided: a) Air Driven Pump operates normally, and b) Associated pump is selected OFF.

2) Center System No. 2 Electric Pump Indication System 3) Air Driven Pump (ADP) Indication System

(O) May be inoperative provided: a) Both center system Electric Pumps operate normally, b) ADP is selected OFF, c) Center Hydraulic Motor Generator (HMG) is not required, and d) Appropriate performance adjustments are applied.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 29 - HYDRAULICS 33-1 Hydraulic System Low QTY or RSVR Lights C 3 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 06/18/2009 MASTER MINIMUM EQUIPMENT LIST 33a PAGE: 29-4

(M) May be inoperative provided associated HYD QTY indication(s) operates normally. (M) May be inoperative provided: a) Associated reservoir level(s) is verified normal before each departure, b) Associated SYS PRESS lights operate normally, and c) On PTU equipped airplanes, with left hydraulic system low QTY or RSVR lights inoperative, left low quantity signal wire of PTU system is capped and stowed. (M) May be inoperative provided: a) Associated reservoir level(s) is verified normal before each departure, b) Associated SYS PRESS lights operate normally, and c) On PTU equipped airplanes, with left hydraulic system low QTY or RSVR light inoperative, left low quantity signal wire of PTU system is capped and stowed.

33-2

HYD QTY Indications

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 11-1 Wing Anti-Ice Valves C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-1

(M) Except for ER operations beyond 120 minutes, may be inoperative closed provided airplane is not operated in known or forecast icing conditions. (O) May be inoperative provided associated valve operates normally. May be inoperative provided associated valve is inoperative. May be inoperative provided associated EICAS Advisory message L/R WING ANTI-ICE operates normally.

11-2

Wing Anti-Ice VALVE Lights

11-3

Wing Anti-Ice Ground Test Engine Anti-Ice Valves 1) Cowl Valves

21-1

(M) Except for ER operations beyond 120 minutes, one may be inoperative closed provided airplane is not operated in known or forecast icing conditions. (M)(O) One may be inoperative locked open provided: a) Fan air modulation valve is locked in intermediate position, b) High stage bleed valve is locked closed, c) Remaining (opposite) engine bleed system operates normally, d) Ambient temperature is below 38 degrees C, e) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained in icing conditions, f) Center Hydraulic Motor Generator (HMG) is considered inoperative, and g) Appropriate EPR limit and performance adjustments are applied. (M)(O) One may be inoperative open provided appropriate EPR limit and performance adjustments are applied. (M) May be inoperative closed. (Continued)

2) Cowl Valves (JT9D-7R4)

3) Stator Vane Valves (JT9D7R4)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 21-1 Engine Anti-Ice Valves (Contd) 4) Cowl Valves a) PW4000 C 2 1 (M)(O) One may be inoperative open provided: a) High pressure shutoff valve is secured closed, b) Bleed air switch for associated engine remains OFF except when TAT is 10 degrees C or below, c) For operations with associated bleed air switch OFF, 1) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, 2) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, 3) Airplane is not operated in known or forecast icing conditions, and 4) Airplane remains at or below FL 350, d) For operations with associated bleed air switch ON, a minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, e) Remaining (opposite) engine bleed system operates normally, f) Associated PRV operates normally, g) Center Hydraulic Motor Generator (HMG) is considered inoperative, and h) Appropriate performance adjustments are applied. NOTE: Bleed air switch for associated engine may be selected ON when TAT is 10 degrees C or below. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-2

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 21-1 Engine Anti-Ice Valves (Contd) 4) Cowl Valves (Contd) b) CF6-80C2 C 2 1 (M)(O) One may be inoperative open provided: a) High pressure shutoff valve is secured closed, b) Bleed air switch for associated engine remains OFF except when TAT is 10 degrees C or below, c) For operations with associated bleed air switch OFF, 1) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, 2) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, 3) Airplane is not operated in known or forecast icing conditions, and 4) Airplane remains at or below FL 350, d) For operations with associated bleed air switch ON, a minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, e) Remaining (opposite) engine bleed system operates normally, f) Associated PRV operates normally, g) Center Hydraulic Motor Generator (HMG) is considered inoperative, h) Associated thrust reverser is secured in forward thrust position, and i) Appropriate performance adjustments are applied. NOTE: Bleed air switch for associated engine may be selected ON when TAT is 10 degrees C or below. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-3

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 21-1 Engine Anti-Ice Valves (Contd) 4) Cowl Valves (Contd) c) RB211-524 C 2 1 (M)(O) One may be inoperative open provided: a) High pressure shutoff valve is secured closed, b) Bleed air switch for associated engine remains OFF except for engine start or when TAT is 10 degrees C or below, c) For operations with associated bleed air switch OFF, 1) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, 2) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, 3) Airplane is not operated in known or forecast icing conditions, and 4) Airplane remains at or below FL 350, d) For operations with associated bleed air switch ON, a minimum of 70% N1 (55% below 10,000 feet MSL) is maintained on associated engine in icing conditions, e) Remaining (opposite) engine bleed system operates normally, f) Associated FWSOV operates normally, g) Center Hydraulic Motor Generator (HMG) is considered inoperative, and h) Appropriate performance adjustments are applied. NOTE: Bleed air switch for associated engine may be selected ON when TAT is 10 degrees C or below. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-4

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 21-2 Engine Anti-Ice VALVE Lights 1) -200/-300 C 2 1 (M) One may be inoperative provided associated valve is verified to operate normally before operating in known or forecast icing conditions. One may be inoperative provided associated valve is inoperative. One may be inoperative provided associated EICAS Advisory message L/R ENG ANTI-ICE operates normally. One may be inoperative provided associated EICAS Advisory message L/R ENG ANTI-ICE operates normally. One may be inoperative provided associated EICAS Advisory message L/R ENG ANTI-ICE operates normally. (O) One may be inoperative provided associated EICAS Advisory message L/R ENG ANTI-ICE operates normally. (O) One may be inoperative provided associated EICAS Advisory message L/R ENG ANTI-ICE operates normally. (O) May be inoperative. (M)(O)One may be inoperative provided: a) Associated HPSOV is secured in closed position, b) Associated nacelle anti-ice valve operates normally, c) A minimum of 70% N1 (55% below 10,000 feet MSL) is maintained on associated engine in icing conditions, d) Remaining (opposite) engine bleed system operates normally, and e) Associated ENG COWL OVHT card is deactivated (removed) from fire detection card file. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-5

a) JT9D

b) CF6-80A/A2

c) RB211

d) CF6-80C2

e) PW4000

2) -400ER 21-3 Engine Cowl Overheat Indications (RB211)

C C

2 2

0 1

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 31-1 Pitot-Static Probe Heater Systems B 4 3 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-6

Except for ER operations beyond 120 minutes, one probe heater may be inoperative provided airplane is not operated in visible moisture, or in known or forecast icing conditions. (M) May be inoperative provided: a) Associated EICAS Advisory message is verified to operate normally, and b) Probe heater systems operate normally. May be inoperative provided associated probe heater is considered inoperative. May be inoperative provided associated probe heater is considered inoperative.

31-2

Probe Heat Lights (Except CAPT and F/O PITOT)

1) Pitot Probe Heat Lights 2) Angle of Attack (AOA) and Temperature (TAT) Probe Heat Lights 31-3 ENG EEC PROBE Light (JT9D)

(M) May be inoperative provided both probe heater functions are verified to operate normally before operating in known or forecast icing conditions. (O) May be inoperative provided a minimum of 50% N1 above 10,000 feet MSL, or 45% N1 at or below 10,000 feet MSL is maintained while in icing conditions. Except for ER operations beyond 120 minutes, may be inoperative provided: a) Pitot heater systems operate normally, b) Remaining probe heater indicating systems for operative probe heaters operate normally, and c) Airplane is not operated in known or forecast icing conditions. (M) May be inoperative provided: a) Associated AOA vane is verified intact, b) Remaining probe heater indicating systems for operative probe heaters operate normally, and c) Airplane is not operated in known or forecast icing conditions.

31-4

MACH PROBES Light (JT9D)

31-5

CAPT PITOT and F/O PITOT Heat Indicating Systems (Heater OFF Monitor)

32-1

Angle of Attack Sensor Heater Systems

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 33-1 Temperature (TAT) Probe Heater Systems C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-7

(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Remaining probe heater indicating systems for operative probe heaters operate normally, and b) Airplane is not operated in known or forecast icing conditions. (M)(O) May be inoperative provided: a) Associated Air Data System is considered inoperative, and b) Remaining probe heater indicating systems for operative probe heaters operate normally.

1) -400ER

34-1

Engine PT2/TT2 Probe Heater Systems 1) JT9D C 2 1 One may be inoperative provided associated engine EPR indication is considered inoperative. (O) One may be inoperative provided: a) Both EECs are switched to ALTN mode, b) N1, N2, and Fuel Flow systems on associated engine operate normally, and c) Appropriate procedures, AFM limitations and performance decrements are applied. One per engine may be inoperative. (O) May be inoperative provided at least 50% N1 above 10,000 feet MSL, or 45% N1 at or below 10,000 feet MSL is maintained while in icing conditions.

2) PW4000

34-2

Engine Mach Probe Heaters (JT9D)

C C

4 4

2 0

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 41-1 Flight Deck Window Heat Systems 1) No. 1 (fwd) Windows C 2 1 (M) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) Airplane is not operated in known or forecast icing conditions, b) Both No. 2 (side) window heaters operate normally, c) Associated windshield pneumatic anti-fog system operates normally, and d) Associated window heat is deactivated. (M) One may be inoperative provided: a) Both No. 1 (fwd) window heaters operate normally, and b) Associated window heat is deactivated. (M) May be inoperative provided associated window heat is deactivated. (M) May be inoperative provided associated window heat system is verified to operate normally before each departure. May be inoperative provided associated window heat system is inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-8

2) No. 2 (side) Windows

3) No. 3 (side) Windows 41-2 Window Heat INOP Lights

C 41-3 Window/Probe Heat Ground Test System Windshield Wipers C

4 1

1 0

42-1

May be inoperative provided airplane is not operated in precipitation within five statute miles of airport of takeoff or intended landing. May be inoperative provided associated low speed operates normally. May be inoperative provided associated high speed operates normally.

1) High Speed

2) Low Speed

*** 43-1 ***

3) Intermittent Rain Repellent System

C D

2 1

0 0

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 30 - ICE AND RAIN PROTECTION 71-1 Drain Mast Heaters C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 30-9

(M) May be inoperative provided water supply to associated galley, lavatory sink and drinking fountain is secured OFF.

72-1

Waste System Heaters 1) Drain Cap Gasket Heater 2) Rinse Hose Heater Boot C 1 0

80-1

Ice Detection System 1) Advisory D 1 0

***

***

2) Primary

(O) May be inoperative provided alternate procedures are established and used.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 31 - INDICATING / RECORDING SYSTEMS 25-1 31-1 Clocks Flight Data Recorder (FDR) System (Includes Digital Flight Data Acquisition Unit (DFDAU)) C C 2 1 1 Any in excess of those required by FAR may be inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/05/2009 MASTER MINIMUM EQUIPMENT LIST 33 PAGE: 31-1

May be inoperative provided: a) Cockpit Voice Recorder (CVR) operates normally, b) Airplane is not dispatched from a designated airport as listed in operators 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 three flight days. May be inoperative provided: a) Cockpit Voice Recorder (CVR) operates normally, and b) Repairs are made within twenty calendar days. May be inoperative provided repairs are made prior to completion of next heavy maintenance visit.

1) DFDR Recording Parameters required by FAR

2) DFDR Recording Parameters not required by FAR *** 3) Quick Access Recorder (QAR) Performance and Maintenance Recorder (PMR) Airplane Integrated Data System (AIDS) Aircraft Condition Monitoring System (ACMS)

35-1 ***

35-2 *** 35-3 ***

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 31 - INDICATING / RECORDING SYSTEMS 41-1 Engine Indication and Crew Alerting Systems (EICAS) (-200/-300) 1) Display Unit (DU) A 2 1 (M)(O) Except for ER operations, one may be inoperative provided: a) Standby Engine Instruments operate normally and are turned ON, b) Cargo FIRE/OVHT test is performed before each departure, c) Electronic Engine Control or autothrottle system operates normally, d) At least one autopilot operates normally, e) All EICAS computers operate normally, and f) Repairs or replacements are made within one flight day. NOTE: In event of an additional DU failure enroute, flight crew should consider landing as soon as practical. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/05/2009 MASTER MINIMUM EQUIPMENT LIST 33 PAGE: 31-2

2) Computer

(M)(O) Except for ER operations, one may be inoperative provided: a) Standby Engine Instruments operate normally and are turned ON, b) Electronic Engine Control or autothrottle system operates normally, c) At least one autopilot operates normally, d) SB 767-79-2 or equivalent (dual oil temperature sensors), is installed, e) Both Display Units operate normally, and f) Repairs or replacements are made within one flight day. NOTE: In event of an additional computer failure enroute, flight crew should consider landing as soon as practical.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 31 - INDICATING / RECORDING SYSTEMS 51-1 Master Caution/ Warning Systems 1) Master Warning Lights (Pilot's Glare Shield) a) -200/-300 C 2 1 One may be inoperative provided master warning aural system and all discrete warning lights operate normally. One may be inoperative provided master warning aural system operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/05/2009 MASTER MINIMUM EQUIPMENT LIST 33 PAGE: 31-3

b) -400ER

2) Master Caution Lights (Pilot's Glare Shield) a) -200/-300 C 2 1 One may be inoperative provided master caution aural system and all discrete warning lights operate normally. One may be inoperative provided master caution aural system operates normally.

b) -400ER

51-2 ***

Takeoff Configuration Check (T/O CHK) Switch

May be inoperative provided procedures do not require its use. Deleted, MMEL Rev. 31.

61-1

Cockpit Door Surveillance System (CDSS) EICAS Status Messages C 0

61-4

(M)(O) May be inoperative provided associated equipment is verified to operate normally before each departure. (M)(O) May be inoperative provided dispatch deviations for associated equipment are observed. (M) May be inoperative provided: a) Fuel quantity indication is verified to operate normally before each flight, and b) Dispatch deviations for associated equipment are observed.

61-5

EICAS Signal Consolidation Card (SCC)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 31 - INDICATING / RECORDING SYSTEMS 63-1 Display Units (DU) 1) -400ER 2) Flat Panel Display (STC ST02165NY) C C 6 4 5 3 One may be inoperative in lower center DU position. Except for ER operations, one may be inoperative in Navigation Display (ND) position. For ER operations, one may be inoperative in Navigation Display (ND) position. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/05/2009 MASTER MINIMUM EQUIPMENT LIST 33 PAGE: 31-4

63-2

Control Panels 1) EFIS Control Panels (-400ER) 2) Flat Panel Display Control Panel (DCP) (STC ST02165NY) C 2 1 (O) One may be inoperative provided associated CDU EFIS control functions are verified to operate normally. (O) One may be inoperative provided all functions of operative DCP are verified to operate normally.

63-3

Display Select Panel Indicator Lights (-400ER)

(O) May be inoperative provided: a) Display Select Panel switches are verified to operate normally, and b) Display Units operate normally. 2 Left or right may be inoperative.

63-4

Display Processing Computers (DPC) (-400ER) Display Control Unit Selector (DCU CTRL) (-400ER)

63-6

(M) May be inoperative provided: a) Selector is in AUTO position and not moved in flight, and b) Automatic source selection function is verified to operate normally. May be inoperative provided all manual display brightness functions operate normally.

63-7

Remote Light Sensor (RLS) System (-400ER)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 31 - INDICATING / RECORDING SYSTEMS 63-10 Data Concentrator Units 1) Panel Data Concentrator Unit (PDCU) (-400ER) 2) Flat Panel Display Data Concentrator Unit (DCU) (STC ST02165NY) C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/05/2009 MASTER MINIMUM EQUIPMENT LIST 33 PAGE: 31-5

(M) Except for ER operations, L, C, or R DCU may be inoperative provided DCU isolation is verified once each flight day.

(M) For ER operations, L or R DCU may be inoperative provided DCU isolation is verified once each flight day. May be dispatched with faults indicated by DISPLAY RESOURCES status message provided all Display Processing Computers operate normally.

63-11

Display Resource Faults (-400ER)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 32 - LANDING GEAR 30-1 Landing Gear Retracting System C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 32-1

(M)(O) May be inoperative provided: a) Inoperative components are properly secured by an accepted procedure, and b) Airplane is dispatched in accordance with appropriate AFM Landing Gear Extended Appendix. (M)(O) May be inoperative in latched position provided override mechanism is verified to operate normally. (M) One UP/DOWN electrical control circuit may be inoperative provided remaining UP/DOWN circuit is verified to operate normally once each flight day.

31-1

Landing Gear Lever Lock Solenoid Landing Gear Selector Valve Electrical Control Circuits (-400ER) Main Gear Door Uplock Springs

31-2

32-1

(M)(O) One spring on one door uplock mechanism may be missing provided speed does not exceed 270 KIAS/0.82 Mach. (M)(O) May be inoperative provided: a) Landing gear are secured in down position, b) Alternate extend system is deactivated, and c) Airplane is dispatched in accordance with appropriate AFM Landing Gear Extended Appendix. (M)(O) May be inoperative open provided: a) Landing gear doors are verified to open using alternate extend system, and b) Alternate procedures are established and used. (M) May be inoperative provided: a) Both door open control switches are verified to be open, b) Landing gear doors are verified to open using alternate extend system, and c) Landing gear doors are closed before each departure. (M)(O) May be inoperative closed provided: a) Landing gear are secured in down position, b) Alternate extend system is deactivated, and c) Airplane is dispatched in accordance with appropriate AFM Landing Gear Extended Appendix.

35-1

Landing Gear Alternate Extend System (-400ER)

1) Alternate Extend Hydraulic Pressure Switch

35-2

Ground Door Release Control System (-400ER)

1) Door Open Control Switches

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 32 - LANDING GEAR 41-1 Wheel Brakes C 8 7 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 32-2

(M)(O) One brake may be deactivated with a deactivation tool provided: a) Performance complies with AFM for one brake deactivated, and b) Antiskid operates normally on remaining wheels. (M)(O) One brake may be deactivated by capping off brake line provided: a) Takeoff performance is based on Landing Gear Extended, b) Takeoff and landing performance complies with AFM for one brake inoperative, c) After takeoff, gear remains extended for two minutes prior to retraction, and d) Antiskid operates normally on remaining wheels. (M)(O) May be inoperative provided associated EICAS Advisory message is verified to operate normally. (M) May be inoperative provided: a) C and R hydraulic low SYS PRESS lights operate normally, and b) Normal and alternate brake systems and brake accumulator are verified to operate normally. (O) May be inoperative provided: a) After takeoff, gear remains down for two minutes before retraction, and b) Takeoff performance is based on Landing Gear Extended. (O) May be inoperative provided: a) AFM decrements are applied for antiskid inoperative operations, and b) Approach minimums do not require its use. (M)(O) One channel and associated brake may be inoperative (brake deactivated or line capped) provided: a) Brake is deactivated by an acceptable procedure, and b) AFM decrements are applied for selected procedure.

41-2

BRAKE SOURCE Indication System

41-3

Gear Retraction Braking System

42-1

Antiskid System

1) Channels

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 32 - LANDING GEAR 42-2 Alternate Antiskid Valves C 4 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 32-3

(M)(O) May be inoperative provided: a) Manual braking capability on alternate brake system is verified on associated wheels, and b) Normal antiskid system operates normally. (M)(O) May be inoperative provided: a) Manual braking capability on alternate brake system is verified on associated wheels, and b) AFM decrements are applied for antiskid inoperative operations. (M) May be inoperative provided antiskid system is verified to operate normally. (O) May be inoperative provided AFM decrements are applied for antiskid inoperative operations.

42-3

ANTISKID Light

42-4

Autobrake System 1) -200/-300 C 1 0 May be inoperative provided: a) AUTO BRAKES light is not illuminated with autobrake switch OFF, and b) Approach minimums do not require its use. (M) May be inoperative with AUTO BRAKES light illuminated and autobrake switch OFF provided: a) Autobrake solenoid valve is verified closed, and b) Approach minimums do not require its use. (M) May be inoperative with AUTO BRAKES light illuminated and autobrake switch OFF provided: a) Module is deactivated, and b) Approach minimums do not require its use. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 32 - LANDING GEAR 42-4 Autobrake System (Contd) 2) -400ER C 1 0 May be inoperative provided: a) AUTOBRAKES EICAS message is not annunciated with autobrake switch OFF, and b) Approach minimums do not require its use. (M) May be inoperative with AUTOBRAKES EICAS message annunciated and autobrake switch OFF provided: a) Autobrake solenoid valve is verified closed, and b) Approach minimums do not require its use. (M) May be inoperative with AUTOBRAKES EICAS message annunciated and autobrake switch OFF provided: a) Module is deactivated, and b) Approach minimums do not require its use. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 32-4

42-5 *** 44-2

Taxi Speed Indication Parking Brake Valve

(M)(O) May be inoperative closed provided AFM performance decrements are applied for antiskid inoperative operations.

44-3

Parking Brake Lights 1) PARK BRAKE Light (-200/-300) C 1 0 (M) May be inoperative provided: a) Parking brake valve operates normally, and b) Antiskid light is verified to operate normally once each flight day. (O) May be inoperative provided AFM performance decrements are applied for antiskid inoperative operations. (O) May be inoperative provided EICAS Advisory message PARKING BRAKE is verified to operate normally. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 32 - LANDING GEAR 44-3 Parking Brake Lights (Contd) 2) Nose Gear Parking Brake Status Indicator Lights (PARKING BRAKE SET, BRAKE ON, BRAKE OFF) C 0 (M)(O) May be inoperative provided alternate procedures are established and used. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 32-5

***

May be inoperative provided procedures do not require its use. May be inoperative provided associated flight deck indication operates normally.

44-4

Brake Accumulator Pressure Gauge (Wheel Well) BRAKE PRESS Gauge (Flight Deck)

44-5

(M) May be inoperative provided: a) Brake accumulator charge is verified normal once each flight day, and b) Right low SYS PRESS light operates normally.

45-1 *** 45-2

Integral Tire Pressure Indicators Nose Wheel Spin Brakes (Snubbers) Tire Pressure Indicating System (TPIS) Brake Temperature Monitoring System (BTMS) Brake Cooling Fans 1) -200/-300

(M) May be damaged or missing.

45-3 ***

46-1 ***

NOTE: Brake cooling fans will be inoperative when all eight brake temperature readings are inoperative.

46-2 ***

(O) May be inoperative provided AFM Maximum Quick Turnaround Weight Penalty is observed. (M) May be inoperative provided associated fan shrouds are removed.

2) -400ER

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 32 - LANDING GEAR 51-1 Rudder Pedal Nose Wheel Steering B 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 32-6

(M)(O) May be inoperative provided: a) Approach minimums do not require its use, and b) All takeoffs and landings are made by a pilot with access to an operating tiller. (M) May be inoperative provided EICAS Advisory message GEAR DOORS is verified to operate normally.

61-1

Landing Gear DOORS Light System (-200/-300) Landing Gear Door Latch Proximity Sensor 1) System One

61-2

(M)(O) One may be inoperative provided: a) Appropriate performance adjustments are applied, and b) Remaining System One and all System Two sensors are verified to operate normally before each departure. (M)(O) One may be inoperative provided: a) Manual function of Passenger Notice System operates normally and procedures for its use are established and used, and b) All System One and remaining System Two sensors are verified to operate normally before each departure. NOTE: An inoperative System Two sensor will render Flight Deck Automatic Function of Passenger Notice System inoperative.

2) System Two (Passenger, 200PC, -200SF and -300BDSF)

3) System Two (ATC A1NM -200 SF, -300BCF, -300F) 71-1 Tail Skid (-300/ -400ER)

(M) One may be inoperative provided all System One and remaining System Two sensors are verified to operate normally before each departure.

(M)(O) May be inoperative provided: a) Tail skid is secured in extended position, b) Water supplies associated with aft drain mast are secured OFF, and c) Appropriate performance adjustments are applied.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 32 - LANDING GEAR 71-2 Tail Skid Indication System (-300/ -400ER) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 32-7

May be inoperative provided tail skid retraction mechanism is inoperative.

(M) May be inoperative provided tail skid extend/retract function is verified to operate normally once each flight day. (M)(O) May be inoperative provided: a) Tail skid is secured in extended position, b) Water supplies associated with aft drain mast are secured OFF, and c) Appropriate performance adjustments are applied. May be inoperative provided alternate indication operates normally. (M) May be inoperative provided tail skid extend/retract function is verified to operate normally once each flight day.

1) TAIL SKID Light (-300) 2) Proximity Switch System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 11-1 Flight Compartment and Instrument Lighting System C NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-1

Individual lights may be inoperative provided remaining lights are: a) Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided, b) Positioned so direct rays are shielded from flight crewmembers' eyes, and c) Lighting configuration and intensity is acceptable to flight crew.

1) Crew Entry Light (ATC A1NM 200SF, -300BCF, -300F) 14-1 Supernumerary Reading Lights Master Dim and Test System 1) Test Function

16-1

(M) May be inoperative provided intended function of associated light(s) is verified. May be inoperative provided: a) BRT functions operate normally, and b) Light intensity is acceptable to flight crew for type and duration of operations. May be inoperative provided remaining operative lighting is considered adequate by pilot in command.

2) Dim Function

20-1

Crew Rest Area Illumination System (STCs ST00973WID and ST02372AT) 1) Flashlight/ Holder Assemblies

May be inoperative or missing provided crewmember in associated bunk has a flashlight of equivalent characteristics readily available.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 20-2 *** Lower Lobe Crew Rest Illumination System (STC ST01994SE) 1) Main Light C 1 0 May be inoperative provided seat reading light operates normally. May be inoperative provided main light operates normally. May be inoperative provided associated bunk reading light operates normally. May be inoperative or missing provided crewmember in associated bunk has a flashlight of equivalent characteristics readily available. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-2

2) Vestibule Light

3) Bunk Lights

4) Flashlight/ Holder Assembly

21-1

Cabin Interior Illumination System 1) Passenger Configurations with Incandescent Emergency Escape Path Marking System 2) Passenger Configurations with Photoluminescent Emergency Escape Path Marking System C Individual lights may be inoperative provided: a) Remaining lighting is sufficient for cabin attendants to perform their duties, and b) For night ER operations, at least 75% of Night Lights must operate.

Individual lights may be inoperative provided: a) Remaining lighting is sufficient for cabin attendants to perform their duties, b) Minimum acceptable light levels specified in one of the following documents are maintained: 1) FAA engineering approval letter, 2) FAA approved report of Type Design holder, 3) Limitations and Conditions section of applicable Supplemental Type Certificate (STC), or 4) An FAA approved report incorporated in Master Drawing List for applicable STC, c) For night ER operations, at least 75% of Night Lights must operate.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 24-1 Passenger Lighted Information Signs System (NO SMOKING/FASTEN SEAT BELT/ RETURN TO SEAT) C NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-3

(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 must be blocked and placarded DO NOT OCCUPY. NOTE: These provisos are not intended to prohibit lavatory use or inspections by crewmembers.

(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. (O) May be inoperative provided alternate procedures are established and used to notify couriers/ supernumeraries when associated sign(s) are placed on or off.

1) All Cargo, Supernumerary/ Courier Area Lighted Information Signs 2) Aural Tone System 3) Flight Deck Automatic Function

(O) May be inoperative provided: a) Manual control function operates normally, and b) Alternate procedures are established and used. May be inoperative provided affected seat or bunk is placarded INOPERATIVE - DO NOT USE.

24-2 ***

Lower Lobe Crew Rest No Smoking/Fasten Seat Belt Signs (STC ST01994SE) Sterile Flight Compartment Light System

25-1 ***

(O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use.

31-1

Wheel Well Lights

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 31-2 *** 31-3 31-4 Exterior Cargo Loading Area Lights Service Lights Electrical Equipment Center Lights Cargo Compartment Lights 1) Cockpit Entry Light (-200PC) 2) Cabin Entry Light (-200PC, -200SF) 3) Main Deck Cargo Lights C 1 0 D 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-4

C C

8 9

0 0

37-1

May be inoperative provided access to main cargo deck is prohibited in flight. NOTE: Main Cargo Deck is defined as area aft of rigid barrier or 9g net, as installed.

(O) May be inoperative provided: a) No two adjacent lights are inoperative, and b) Remaining illumination is adequate to perform required crew duties. May be inoperative for hazardous materials designated CARGO AIRCRAFT ONLY provided Main Deck Cargo Compartment lights one position aft of hazardous material pallet/container position and forward to flight deck operate normally.

4) Sill Lights 5) Lower Cargo Compartments 6) Light Lens

C C

0 0 (O) May be inoperative provided procedures do not require their use. (M) May be broken/missing provided associated light is deactivated.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 37-2 Main Cargo Deck Crew Alerting System C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-5

May be inoperative provided access to main cargo compartment is prohibited in flight. (O) May be inoperative provided alternate procedures are established and used. (O) May be inoperative provided ground de-icing procedures do not require their use. One nose gear and/or one wing mounted light may be inoperative. May be inoperative for day operations.

41-1

Wing Illumination Lights Landing Lights

42-1

C 42-2 Taxi Lights C

4 -

0 0

42-3

Runway Turnoff Lights Position Lights (Bulbs) 1) -200/-300

43-1

One stationary light on forward and aft tip of each wing may be inoperative. May be inoperative for day operations. | | | | |

C 2) -300/300F With Blended Winglets STC ST01920SE (LED Lights) a) Forward Position Lights Module C

One stationary forward position light LED module on leading edge of each winglet may be inoperative.

| |

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 43-1 Position Lights (Bulbs) (Contd) 2) -300/300F With Blended Winglets STC ST01920SE (LED Lights) (Contd) a) Forward Position Lights Module (Contd) b) Aft Position Lights Module 3) -400ER C 4 0 May be inoperative for day operations. | NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-6

May be inoperative for day operations.

| | |

May be inoperative for day operations provided wing tip and tail cone white strobe lights operate normally. The following may be inoperative provided all strobe lights operate normally: a) One stationary light on forward tip of each wing, and b) One stationary white bulb on tail cone.

43-2

Door Threshold Light (ATC A1NM -200 SF, -300BCF, -300F) Anti-Collision Lights (Red Strobes/White Strobes) 1) -200/-300

44-1

C C

4 4

0 2

May be inoperative for day operations. Upper and lower red fuselage strobe lights may be inoperative provided wing tip white strobe lights operate normally. Wing tip white strobe lights may be inoperative provided upper and lower red fuselage strobe lights operate normally. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 44-1 Anti-Collision Lights (Red Strobes/White Strobes) (Contd) 2) -400ER B 5 0 May be inoperative for day operations provided all position lights operate normally. Upper and lower red fuselage strobe lights may be inoperative provided wing tip and tail cone white strobe lights, and all position lights (bulbs) operate normally. Wing tip and tail cone white strobe lights may be inoperative provided upper and lower red fuselage lights, and all position lights (bulbs) operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-7

45-1 *** 51-1

Logo Lights

Interior Emergency Lighting System (Battery Powered)

Light assemblies installed in ceiling above each main aisle may be inoperative provided no two adjacent (same aisle) light assemblies are inoperative. Lights/signs exclusively associated with one door, slide or emergency exit may be inoperative provided: a) Associated door, slide or emergency exit is considered inoperative, and b) Repairs are made within one flight day. (M) May be inoperative provided: a) Lower lobe crew rest module is not used and personal items are removed, and b) Lower lobe crew rest door is closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest inspections by crew members.

***

1) Lower Lobe Crew Rest Emergency Lights (STC ST01994SE)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 33 - LIGHTS 51-2 Exterior Emergency Lighting System (Battery Powered) Emergency Escape Path Marking System B 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 33-8

May be inoperative for day operations.

51-3

Lights/signs exclusively associated with one door, slide or emergency exit may be inoperative provided: a) Associated door, slide or emergency exit is considered inoperative, and b) Repairs are made within one flight day. Individual lights may be inoperative provided minimum acceptable lighting levels specified in one of the following documents are maintained: a) FAA engineering approval letter, b) FAA approved report of Type Design holder, c) Limitations and Conditions section of applicable Supplemental Type Certificate (STC), or d) An FAA approved report incorporated in Master Drawing List for applicable STC. Components may be inoperative provided minimum acceptable lighting levels specified in one of the following documents are maintained: a) FAA engineering approval letter, b) FAA approved report of Type Design holder, c) Limitations and Conditions section of applicable Supplemental Type Certificate (STC), or d) An FAA approved report incorporated in Master Drawing List for applicable STC. (O) May be inoperative provided: a) Alternate procedures are established and used to ensure 10 minutes of ON time does not occur, b) Affected emergency lights are verified to operate normally prior to first flight of each day, and c) Repairs are made within 10 flight days.

1) Incandescent Lighting System

2) Photoluminescent Lighting System

51-4

PowerSmart Wireless Emergency Primary Power System (WEPPS) Diagnostic Panel (STC ST03629AT)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 00-1 Instrument Source Select Switches 1) -200/-300 C (O) May be inoperative provided: a) Associated instruments operate from isolated sources, b) Inoperative switches are not moved in flight, and c) For ER operations, at least one FMC, EFI, and IRS switch must operate normally. (O) May be inoperative provided: a) Associated instruments operate from isolated sources, b) Inoperative switches are not moved in flight, and c) For ER operations, at least one FMC and IRS switch must operate normally. (O) May be inoperative provided: a) Associated instruments operate from isolated sources, b) Inoperative switches are not moved in flight, and c) For ER operations, at least one FMC, EFI, IRS and DCP switch must operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-1

2) -400ER

3) Flat Panel Display STC ST02165NY

13-1 ***

MACH/Airspeed Indicators 1) Mach Indicators C C 2 2 1 0 May be inoperative provided EFIS Mach indications are installed and operating normally at respective pilot's station.

May be inoperative provided: a) Airplane remains at or below FL 300, and b) A placard with this limitation is affixed to instrument panel.

2) Command Airspeed Cursors

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 13-1 *** MACH/Airspeed Indicators (Contd) 3) Airspeed Indicators C 2 0 May be inoperative provided EFIS airspeed indications are installed and operating normally at respective pilot's station. (O) May be inoperative or missing provided alternate procedures are established and used. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-2

4) External Airspeed Markers (Bugs) 13-2 Mach/Airspeed Warning Systems (Visual and Aural) Standby Altimeter Vibrator Total Air Temperature (TAT) Indication Static Air Temperature (SAT) Indicator (Center Panel) True Airspeed (TAS) Indicator (Center Panel) Speed Command (Fast-Slow) Indicators Altitude Alerting System

13-6

May be inoperative provided VMC exists at departure and arrival airports. (O) May be inoperative provided one other temperature indication (RAT or SAT) is available.

13-7

13-8 ***

13-9 ***

13-10 ***

16-1

(O) May be inoperative provided: a) Autopilot with altitude hold operates normally, b) Enroute operations do not require its use, c) Repairs are made within three flight cycles, and d) Airplane does not depart from an airport where repair or replacement can be made. May be inoperative provided it is not required by 14 CFR.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 21-1 Inertial Reference Systems (IRS) 1) IRU (-200/-300) a) Airplanes Without Hydraulic Motor (HMG) Installed C 3 2 (M) Left or center may be inoperative provided: a) Approach minimums do not require its use, and b) If left is inoperative, center is selected and isolation is verified once each flight day. (M) Right may be inoperative for Day VMC flight provided center is selected and isolation is verified once each flight day. (M)(O) Left or right may be inoperative provided: a) Approach minimums do not require its use, b) Center is selected and isolation is verified once each flight day, c) First officer's IRS instrument source select switch operates normally, and d) For ER operations, left and center must operate normally. Center may be inoperative for Day VMC flight. (M) One may be inoperative provided: a) Approach minimums do not require its use, and b) If left or right is inoperative, center is selected and isolation is verified once each flight day. For ER operations, may be inoperative provided both FMCS CDUs operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-3

b) Airplanes with HMG Installed

C 2) ADIRU Inertial Reference Function (-400ER) C

3 3

2 2

***

3) IRS Mode Selector Panel Display and Keyboard Functions

For non-ER operations, may be inoperative provided one FMCS CDU operates normally. Deleted, MMEL Rev. 7. Deleted, MMEL Rev. 7.

22-1 22-2

ADI HSI

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 22-3 Radio Distance Magnetic Indicators (RDMI) (-200/-300) C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-4

Right may be inoperative.

Left may be inoperative provided flight is restricted to Day VMC. Right and left may be inoperative provided standby power system powers the Captains instrument bus. May be inoperative provided associated EHSI ADF bearing pointer operates normally.

***

1) Airplanes with Independent ADF Radio Magnetic Indicators (RMI) (-200/-300)

May be inoperative provided associated radio compass ADF system is considered inoperative. May be inoperative provided approach minimums do not require their use. May be inoperative provided approach minimums do not require their use. NOTE: Windshear guidance may be unavailable.

22-4

Flight Director Systems 1) Displays

22-5

Electronic Flight Instrument (EFIS) Symbol Generators (-200/ -300)

(M) Except for ER operations, one may be inoperative provided symbol generator isolation is verified once each flight day. (M) For ER operations, L or R may be inoperative provided symbol generator isolation is verified once each flight day.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 22-6 *** EFIS Controls 1) Switches (NAV AID/ARPT/ RTE DATA/WPT/ WXR/TERR) (-200/-300) 2) Switches (WXR/STA/ WPT/ARPT/ DATA/POS/ TERR) (-400ER) 3) Switches (NAV AID/ARPT/RTE DATA/ WPT/WXR/TER) (Flat Panel Display STC ST02165NY) 4) Decision Height Indication (DH REF) (Airplanes without PFD) C One switch for each function may be inoperative provided procedures do not require its use. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-5

14

10

One switch for each function may be inoperative provided procedures do not require its use.

May be inoperative provided approach procedures do not require its use.

NOTE: Flight crew use EADI DH indication. a) Airplanes without Radio Altitude Indicators (Tape) *** b) Airplanes with Radio Altitude Indicators (Tape) C 2 0 May be inoperative. NOTE: Flight crew use EADI DH indication.

May be inoperative provided Radio Altitude Indicators (Tape) are installed and operate normally. NOTE: Flight crew use EADI DH indication. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 22-6 EFIS Controls (Contd) 5) HSI Selector a) MAP Position B 2 1 (O) May be inoperative provided: a) Both FMCs operate normally, and b) Alternate procedures are established and used. (O) May be inoperative provided: a) Both FMCs operate normally, and b) Alternate procedures are established and used. May be inoperative provided both FMCs operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-6

b) PLAN Position

6) HSI Range Selector 22-7 *** EFIS Speed Tape (-200/-300) 1) Mach Indications

C C

2 2

1 0 May be inoperative provided MACH indicators are installed and operating normally at respective pilot's station. May be inoperative provided: a) Airplane remains at or below FL 300, and b) A placard with this limitation is affixed to instrument panel. May be inoperative provided airspeed indicators are installed and operating normally at respective pilot's station.

2) Airspeed Indications

22-8

Pitch Limit Indicators Magnetic Compass (Standby)

23-1

(O) May be inoperative provided any combination of three gyro or INS (IRS) stabilized compass systems operate normally. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 23-1 Magnetic Compass (Standby) (Contd) B 1 0 (O) May be inoperative provided: a) Any combination of two gyro or INS (IRS) stabilized compass systems operate normally, and b) Airplane is operated with dual independent navigation capability and under positive radar control by ATC on enroute portion of flight. (O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two stabilized directional gyro systems are installed, operative, and used in conjunction with approved free gyro navigation techniques. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-7

24-1

Standby Attitude/ILS Indicator 1) 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.

2) Approach Mode 24-2 *** Integrated Standby Flight Display (ISFD) System 1) Attitude Display

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.

2) Approach Mode 3) Heading Display 4) Metric Altimeter Display

C C C

1 1 1

0 0 0 (O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 24-2 *** Integrated Standby Flight Display (ISFD) System (Contd) 5) Dedicated Battery/ Charger System 24-3 *** Electronic/ Integrated Standby Instrument System (ESIS/ ISIS) (STC ST02165NY) 1) 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. C 1 0 May be inoperative except for ER operations beyond 120 minutes. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-8

***

2) Approach Mode 3) Heading Display

C C D

1 1 1

0 0 0

25-1 *** 26-1

Instrument Comparator Unit Air Data Systems (-400ER) 1) Left and Right Air Data System

(M)(O) One may be inoperative provided: a) Center Air Data is selected and operates normally, b) Center ADIRU Inertial Reference Function is not selected OFF, and c) Air data isolation is verified.

2) Center Air Data System 30-1 Taxi Speed Indication ILS Systems

Moved to 32-42-5, MMEL Rev. 9.

31-1

Any in excess of those required by FAR, and not powered by a Standby Bus, may be inoperative.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 32-1 Marker Beacon System Radio Altimeter (RA) Systems (EADI) 1) Single Source Datalink to GPWS a) Left RA A 1 0 (O) May be inoperative provided: a) Approach minimums or operating procedures do not require its use, and b) Repairs are made within two flight days. (O) May be inoperative provided approach minimums or operating procedures do not require its use. (O) May be inoperative provided: a) GPWS is supplied with altitude data, and b) Approach minimums or operating procedures do not require its use. (O) May be inoperative provided: a) Approach minimums or operating procedures do not require its use, and b) Repairs are made within two flight days. (O) May be inoperative provided approach minimums or operating procedures do not require their use. C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-9

May be inoperative provided approach minimums do not require its use.

33-1

b) Center/Right RA 2) Multi-source Datalink to GPWS

33-2 ***

Radio Altitude Indicators (Altitude Tape) Metric Altimeter (Includes IS&S 9D80110-24 Metric/English Altimeter)

40-1 ***

May be inoperative provided operations do not require its use.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 43-1 Weather Radar Systems C NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-10

May be inoperative provided weather radar is not required by FAR.

D *** 1) Indicators D

1 Any in excess of those required by FAR may be inoperative. May be inoperative provided manual tilt function operates normally.

***

2) Autotilt/ Multiscan Function 3) WXR ON Light

***

(O) May be inoperative provided alternate procedures are established and used.

***

4) GAIN UCAL Light

***

5) Windshear Alert Mode (Predictive)

(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.

(O) May be inoperative provided: a) Alternate procedures are established and used, and b) Windshear Warning and Guidance System (Reactive) operates normally. (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within two flight days. (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within two flight days. May be inoperative provided: a) GPWS is considered inoperative, and b) Repairs are made within two flight days.

46-1

Ground Proximity Warning System (GPWS)

1) Modes 1 thru 4

2) Test Mode

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 46-1 Ground Proximity Warning System (GPWS) (Contd) 3) Glideslope Deviation (Mode 5) 4) Advisory Callouts (Mode 6) B 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-11

(O) May be inoperative provided alternate procedures are established and used. (O) May be inoperative provided: a) Advisory callout not required by FAR, and b) Alternate procedures are established and used. (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.

***

5) Windshear Alert Mode (Reactive) (Mode 7)

(O) May be inoperative provided: a) Alternate procedures are established and used, and b) Windshear Detection and Avoidance System (Predictive) operates normally. (O) May be inoperative provided alternate procedures are established and used.

***

6) Terrain Awareness Function 7) Terrain Displays

C B

1 0 0

***

8) Runway Awareness & Advisory System (RAAS) Windshear Warning and Flight Guidance System VOR Navigation Systems

46-2

Moved to 34-46-1, MMEL Rev. 25.

51-1

Any in excess of those required by FAR, and not powered by a Standby Bus, may be inoperative.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 53-1 ATC Transponders and Automatic Altitude Reporting Systems B 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-12

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. Any in excess of those required by FAR may be inoperative. May be inoperative provided: a) Operations do not require its use, and b) Repairs are made prior to completion of next heavy maintenance visit.

1) Elementary and Enhanced Downlink Aircraft Reportable Parameters not Required by FAR *** 2) ADS-B Extended Squitter Transmissions

May be inoperative provided: a) Operations do not require its use, and b) Repairs are made prior to completion of next heavy maintenance visit. Any in excess of those required by FAR may be inoperative. Any in excess of those required by FAR may be inoperative. May be inoperative provided it is not required by 14 CFR. NOTE: If ADS-B is installed in lieu of or as a replacement for 14 CFR required equipment, repair category in operators MEL will be the same as that of 14 CFR required equipment.

55-1

Distance Measuring Equipment Systems Radio Compass (ADF) Systems Automatic Dependent SurveillanceBroadcast (ADS-B) System

57-1

58-1 ***

1) Link and Display Processor Unit (LDPU) 2) Cockpit Display and Traffic Information (CDTI) 3) CDTI Control Panel

NOTE: Cockpit Display Traffic Information (CDTI) display of data from other aircraft systems may be used.

May be inoperative provided: a) Flight ID can be set, and b) Screen display is acceptable to flight crew. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 58-1 *** Automatic Dependent SurveillanceBroadcast (ADS-B) System (Contd) 4) 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. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-13

5) Data Link Receiver(s) 6) ADS-BApplications 58-2 *** ACSS Surveillance Processor (STC ST02126LA)

(M) May be inoperative provided: a) Automatic Dependent Surveillance-Broadcast (ADS-B) is considered inoperative, and b) TCAS is considered inoperative. May be inoperative provided: a) It is not required by FAR, b) Procedures do not require its use, and c) Merging & Spacing and CAVS operations are prohibited. NOTE: If ADS-B is installed in lieu of or as a replacement for FAR required equipment, repair category in operators MEL will be the same as that of FAR required equipment.

***

1) Automatic Dependent SurveillanceBroadcast (ADSB) Functionality

a) Cockpit Display of Traffic Information (CDTI) Functionality b) ADS-B Guidance Display (AGD)

May be inoperative provided: a) Procedures do not require its use, and b) Merging & Spacing and CAVS operations are prohibited. NOTE: ADS-B data transmissions may continue.

May be inoperative provided: a) Procedures do not require its use, and b) Merging & Spacing and CAVS operations are prohibited.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 60-3 *** Global Positioning Systems (GPS) C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-14

(O) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. May be inoperative provided: a) Procedures do not require its use, and b) Merging & Spacing and CAVS operations are prohibited.

1) ACSS Surveillance Processor (STC ST02126LA) 61-1 Flight Management Computer Systems (FMCS) 1) FMC (Including CDU/HMCDU/ MCDU) (-200/-300)

(M)(O) Except for ER operations, one may be inoperative provided enroute operations do not require its use. (M)(O) Except for ER operations, may be inoperative provided: a) Both Fuel Quantity Indicating System (FQIS) processor channels are verified to operate normally, b) All flight deck fuel quantity indications operate normally, and c) Enroute operations do not require its use. (M)(O) For long-range navigation operation, one FMC may be inoperative provided other approved means of navigation is available. NOTE: An associated HMCDU or MCDU, if operative, may be used to meet navigation requirements.

2) FMC (-400ER)

(M)(O) One may be inoperative provided enroute operations do not require its use.

3) Center MCDU (-400ER)

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 61-1 Flight Management Computer Systems (FMCS) (Contd) 4) Navigation Databases C (O) May be out of currency provided: a) Current aeronautical charts are used to verify navigation fixes prior to dispatch, b) Procedures are established and used to verify status and suitability of navigation facilities used to define route of flight, and c) Approach navigation radios are manually tuned and identified. (M) May be inoperative provided CDU MSG light and EICAS Advisory message FMC MESSAGE are verified to operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-15

5) FMC Annunciator Light (-200/-300) 61-2 Traffic Alert Collision Avoidance System (TCAS II)

(M) May be inoperative provided: a) System is deactivated and secured, and b) Enroute or approach procedures do not require its use. (M)(O) May be inoperative provided: a) Not required by FAR, b) System is deactivated and secured, and c) Enroute or approach procedures do not require its use. May be inoperative on non-flying pilot side provided: a) TA and RA visual display operates normally on flying pilot side, and b) TA and RA audio function operates normally on flying pilot side.

***

1) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System(s) 2) Resolution Advisory (RA) Display System(s)

May be inoperative on non-flying pilot side.

(O) May be inoperative provided: a) Traffic Alert (TA) visual display and audio functions operate normally, b) TA only mode is selected by crew, and c) Enroute or approach procedures do not require its use. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 34 - NAVIGATION 61-2 Traffic Alert Collision Avoidance System (TCAS II) (Contd) 3) Traffic Alert (TA) Display System(s) C 0 (O) May be inoperative provided: a) RA visual display and audio functions operate normally, and b) Enroute or approach procedures do not require its use. May be inoperative provided enroute or approach procedures do not require use of TCAS. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 34-16

4) Audio Functions

***

5) Airspace Selection Function ACSS Surveillance Processor TCAS II Functionality (STC ST02126LA)

61-3 ***

(O) May be inoperative provided: a) Function is secured according to an approved procedure, and b) Enroute or approach procedures do not require its use. (O) May be inoperative provided: a) Not required by FAR, b) Function is secured according to an approved procedure, and c) Enroute or approach procedures do not require its use. May be inoperative on non-flying pilot side.

1) Resolution Advisory (RA) Display System(s)

(O) May be inoperative provided: a) Traffic Alert (TA) visual display and audio functions operate normally, b) TA only mode is selected by crew, and c) Enroute or approach procedures do not require its use. (O) May be inoperative provided: a) RA visual display and audio functions operate normally, and b) Enroute or approach procedures do not require its use.

2) Traffic Alert (TA) Display System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION LIST AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 35 - OXYGEN 11-2 Crew Oxygen System 1) Pressure Indication (EICAS) 2) Bottle Gage (One Bottle System) 3) Bottle Gage (Two Bottle System) 4) Supernumerary Oxygen Masks B 1 0 (M) May be inoperative provided oxygen supply is verified to be above minimum required before each departure. May be inoperative provided pressure indication (EICAS) operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT 33b PAGE: 35-1

(M) May be inoperative provided pressure indication (EICAS) operates normally.

May be inoperative provided associated seat is not occupied. May be inoperative provided flight is not conducted above 10,000 feet MSL. (M) One may be inoperative provided: a) Line to inoperative pressure regulator is disconnected and plugged, b) Bottle gage on remaining bottle operates normally, and c) Oxygen supply is verified to be above minimum required before each departure. (O) May be damaged or missing.

5) Pressure Regulator (Two Bottle Systems)

6) Oxygen Thermal Relief Indicator 7) Crew Bottle Pressure Regulator (-200SF and -300BDSF)

(M) May be inoperative provided: a) One way interconnect line from supernumerary system is installed and operates normally, b) Pressure regulator on supernumerary bottle operates normally. c) Line to inoperative pressure regulator is disconnected and plugged, d) Bottle gage on supernumerary bottle operates normally, e) Oxygen supply is verified to be above minimum required before each departure, and f) All supernumerary area seats are not occupied.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION LIST AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 35 - OXYGEN 11-3 Supernumerary Oxygen System (-200SF and -300BDSF) 1) Pressure Indication a) EICAS B 1 0 (M) May be inoperative provided oxygen supply is verified to be above minimum required before each departure. May be inoperative provided EICAS pressure indication operates normally. May be inoperative provided associated seat is not occupied. May be inoperative provided flight is not conducted above 10,000 feet MSL. May be inoperative provided supernumerary seats are not occupied. Any in excess of those required by FAR may be inoperative or missing. (O) May be inoperative provided: a) Flight is not conducted where minimum enroute altitude is above 14,000 feet MSL, b) Both air conditioning packs operate normally, c) All other 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. May be inoperative provided flight is conducted at or below 10,000 feet MSL. (Continued) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT 33b PAGE: 35-2

May be inoperative provided supernumerary seats are not occupied.

b) Bottle Gage

2) Oxygen Masks

3) Pressure Regulator 20-1 PBE Smoke Hoods

21-1

Passenger Oxygen System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION LIST AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 35 - OXYGEN 21-1 Passenger Oxygen System (Contd) 1) Passenger Service Units (PSUs) B (M) May be inoperative with no flight altitude restriction provided: a) Affected seats are blocked and placarded to prevent occupancy, and b) Units operate normally for all usable lavatory and flight attendant locations. (M) May be inoperative provided: a) Manual deployment system operates normally, and b) Airplane remains at or below FL 300. (M) May be inoperative with no flight altitude restriction provided affected bunks are blocked and placarded INOPERATIVE - DO NOT USE. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT 33b PAGE: 35-3

2) Automatic Presentation System

3) Crew Rest Oxygen Modules (STC ST00973WI-D)

(M) May be inoperative provided: a) Portable oxygen bottle and mask are available for associated bunk occupant, b) Crew rest oxygen warning horn system is verified to operate normally, and c) Airplane remains at or below FL 300. (M) May be inoperative with no flight altitude restriction provided: a) Associated crew rest is not used and personal items are removed, and b) Associated crew rest door is locked and placarded INOPERATIVE - DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest inspections by crewmembers.

4) Crew Rest Oxygen Warning Horn Systems (STC ST00973WI-D)

5) Lower Lobe Crew Rest Passenger Service Units (STC ST01994SE)

(M) May be inoperative with no flight altitude restriction provided affected bunks are blocked and placarded INOPERATIVE - DO NOT USE.

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION LIST AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 35 - OXYGEN 21-1 Passenger Oxygen System (Contd) 6) Lower Lobe Crew Rest Altitude Alert Horn (STC ST01994SE) B 1 0 (M) May be inoperative with no flight altitude restriction provided: a) Lower lobe crew rest module is not used and personal items are removed, and b) Lower lobe crew rest door is locked and placarded INOPERATIVE - DO NOT ENTER. NOTE: These provisos are not intended to prohibit crew rest inspections by crewmembers. 31-1 Portable Oxygen Dispensing Units (Bottle and Mask) D (M) Any in excess of those required by FAR may be unserviceable or missing provided: a) Required distribution of serviceable bottles is maintained throughout aircraft, and b) Bottles not properly serviced are replaced, serviced, or removed at next available maintenance facility. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT 33b PAGE: 35-4

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 00-1 Air Supply Control and Test Unit (ASCTU) (-400ER) 1) Primary (Digital) Control Channels C 2 1 (M)(O) One may be inoperative deactivated provided: a) Associated ASCTU backup (analog) channel is verified to operate normally, b) Both associated Cabin Temperature Controller channels are verified to operate normally once each flight day, c) Both packs operate normally, d) Remaining (opposite) engine bleed system operates normally, e) Associated HPSOV is verified closed, f) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, g) Hydraulic Motor Generator (HMG) is not required, h) For CF6-80C2 engines, associated thrust reverser is secured in forward thrust position, i) Associated fan air modulation valve is secured in intermediate position, and j) Appropriate performance adjustments are applied. (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative deactivated provided: a) Associated ASCTU backup (analog) channel is verified to operate normally, b) Both associated Cabin Temperature Controller channels are verified to operate normally once each flight day, c) Both packs operate normally, d) Remaining (opposite) engine bleed system operates normally, e) Associated HPSOV is verified closed, f) Airplane is not operated in known or forecast icing conditions, g) Hydraulic Motor Generator (HMG) is not required, h) For CF6-80C2 engines, associated thrust reverser is secured in forward thrust position, and i) Appropriate performance adjustments are applied. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-1

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 00-1 Air Supply Control and Test Unit (ASCTU) (-400ER) (Contd) 2) Backup (Analog) Channels C 2 1 (M)(O) One may be inoperative deactivated provided: a) Associated ASCTU primary (digital) channel is verified to operate normally, b) Associated CTC operates normally, c) Both packs operate normally, and d) Remaining (opposite) engine bleed system operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-2

11-1

ENG BLEED Pressure Regulating and Shutoff Valves (PRSOV) 1) JT9D, CF6 & PW4000 C 2 1 (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) PRSOV is secured closed, b) Associated engine BLEED switch remains OFF, c) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, d) Airplane is not operated in known or forecast icing conditions, e) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, f) Remaining (opposite) engine bleed system operates normally, g) Airplane remains at or below FL 350, h) Center Hydraulic Motor Generator (HMG) is not required, and i) For CF6-80C2 and PW4000 engines, appropriate performance adjustments are applied for either of the following conditions: 1) Associated fan air modulation valve secured in intermediate position, or 2) Associated fan air modulation valve open. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 11-1 ENG BLEED Pressure Regulating and Shutoff Valves (PRSOV) (Contd) 2) RB211 C 2 1 (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) PRSOV is secured closed, except for engine start, b) Associated engine BLEED switch remains OFF, c) Start valve on remaining (opposite) engine operates normally, d) Airplane is not operated in known or forecast icing conditions, e) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, f) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, g) Remaining (opposite) engine bleed system operates normally, h) Flight remains at or below FL 350, and i) Center Hydraulic Motor Generator (HMG) is not required. (M)(O) One may be inoperative provided: a) Valve is secured closed, b) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, c) Remaining (opposite) engine bleed system operates normally, d) Center Hydraulic Motor Generator (HMG) is not required, and e) For CF6-80C2 engines, 1) Associated thrust reverser is secured in forward thrust position, and 2) Appropriate performance adjustments are applied. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-3

11-2

ENGINE HIGH STAGE Bleed Valve Systems (JT9D)/High Pressure Shutoff Valve (HPSOV) Systems (PW4000, CF6, RB211)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 11-3 Intermediate Pressure Check Valves (Low Pressure) C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-4

(M)(O) One may be inoperative open provided: a) Associated high stage bleed valve/HPSOV is secured closed, b) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, c) Remaining (opposite) engine bleed system operates normally, d) Center Hydraulic Motor Generator (HMG) is not required, and e) For CF6-80C2 engines, 1) Associated thrust reverser is secured in forward thrust position, and 2) Appropriate performance adjustments are applied. (M) May be inoperative provided: a) Valve is closed, and b) Bleed switch remains OFF. NOTE: APU may be used for electrical power.

11-4

APU BLEED Valve

11-5

APU BLEED Check Valve L and R Bleed ISLN Valves

May be inoperative provided APU bleed valve remains closed, except for engine start. (M) Except for ER operations beyond 120 minutes, one may be inoperative provided: a) Valve is closed except for engine start, b) Airplane is not operated in known or forecast icing conditions, and c) Both engine bleed valves operate normally. (O) May be inoperative provided: a) Valve remains closed except for engine start, b) APU is used as an air source during takeoff and landing or ADP inoperative penalties are applied, c) Both center electrical hydraulic pumps operate normally, d) Airplane remains at or below FL 270, and e) Center Hydraulic Motor Generator (HMG) is not required.

11-6

11-7

Center Bleed Isolation Valve

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 11-8 Engine Pressure Regulating Valve (PRV) Systems 1) CF6-80C2 & PW4000 C 2 1 (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative secured closed provided: a) Associated bleed valve switch remains closed, b) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, c) Airplane is not operated in known or forecast icing conditions, d) APU is used as air source for takeoff or ADP inoperative penalties are applied, e) Remaining (opposite) engine bleed system operates normally, f) Airplane remains at or below FL 350, g) Center Hydraulic Motor Generator (HMG) is not required, h) For CF6-80C2 engines, associated thrust reverser is secured in forward thrust position, and i) Appropriate performance adjustments are applied for either of the following conditions: 1) Associated fan air modulation valve secured in intermediate position, or 2) Associated fan air modulation valve open. (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative open provided: a) Associated HPSOV is secured closed, b) Associated pressure regulating valve will open fully pneumatically, c) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, d) Remaining (opposite) engine bleed system operates normally, and e) Center Hydraulic Motor Generator (HMG) is not required. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-5

2) PW4000

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 11-8 Engine Pressure Regulating Valve (PRV) Systems (Contd) 3) CF6-80C2 a) -200/-300 C 2 1 (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative open provided: a) Associated HPSOV is secured closed, b) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, c) Associated pressure regulating valve will open fully pneumatically, d) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, e) Associated engine BLEED switch is selected OFF, except when alternate procedures require its use, f) Airplane remains at or below FL 350, g) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, h) Center Hydraulic Motor Generator (HMG) is not required, i) Associated thrust reverser is secured in forward thrust position, j) Bleed system on remaining (opposite) engine operates normally, and k) Appropriate performance adjustments are applied for either of the following conditions: 1) Associated fan air modulation valve secured in intermediate position, or 2) Associated fan air modulation valve open. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-6

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 11-8 Engine Pressure Regulating Valve (PRV) Systems (Contd) 3) CF6-80C2 (Contd) b) -400ER C 2 1 (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative open provided: a) Associated HPSOV is secured closed, b) Associated bleed isolation valve is opened after takeoff, and closed before approach and landing, c) Associated pressure regulating valve is verified open, d) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, e) Associated engine BLEED switch is selected OFF, except when alternate procedures require its use, f) Airplane remains at or below FL 350, g) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, h) Center Hydraulic Motor Generator (HMG) is not required, i) Associated thrust reverser is secured in forward thrust position, j) Bleed system on remaining (opposite) engine operates normally, and k) Appropriate performance adjustments are applied. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-7

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 11-9 Engine Firewall Shutoff Valves (FWSOV) (RB211) C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-8

(M)(O) Except for ER operations beyond 120 minutes, one may be inoperative secured closed provided: a) Associated engine BLEED switch remains OFF, b) Associated engine bleed isolation valve is opened after takeoff, and closed before approach and landing, c) Airplane is not operated in known or forecast icing conditions, d) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, e) Remaining (opposite) engine bleed system operates normally, f) Airplane remains at or below FL 350, and g) Center Hydraulic Motor Generator (HMG) is not required. (M)(O) Except for ER operations beyond 120 minutes, one may be inoperative open provided: a) FWSOV opens fully pneumatically, b) Associated HPSOV is secured closed, c) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, d) Remaining (opposite) engine bleed system operates normally, and e) Center Hydraulic Motor Generator (HMG) is not required. May be inoperative open.

11-10

High Stage (HP) Check Valves (RB211)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 12-1 Precoolers 1) JT9D & CF680A/A2 C 2 1 (M)(O) Except for ER operations beyond 120 minutes, airplane may be dispatched with damage to one precooler and associated ducting between high stage bleed valve/HPSOV and low pressure shutoff valve provided: a) Associated high stage bleed valve/HPSOV is secured closed, b) Associated pressure regulating and shutoff valve is secured closed, c) Associated low pressure bleed duct is blocked by an approved tool, d) Airplane is not operated in known or forecast icing conditions, e) Center Hydraulic Motor Generator (HMG) is not required, f) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, g) Remaining (opposite) engine bleed system operates normally, h) Airplane remains at or below FL 350, i) APU is used as air source for ADP for takeoff or ADP inoperative penalties are applied, and j) Appropriate performance adjustments are applied for either of the following conditions: 1) Associated fan air modulation valve secured in intermediate position, or 2) Associated fan air modulation valve open. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-9

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 12-1 Precoolers (Contd) 2) PW4000 & CF680C2 C 2 1 (M)(O) Except for ER operations beyond 120 minutes, airplane may be dispatched with damage to one precooler and associated ducting between Pressure Regulating Valve (PRV) and Pressure Regulating and Shutoff Valve (PRSOV) provided: a) Associated PRV is secured closed, b) Associated PRSOV is secured closed, c) Airplane is not operated in known or forecast icing conditions, d) Associated bleed isolation valve is opened after takeoff and closed before approach and landing, e) Remaining (opposite) engine bleed system operates normally, f) Airplane remains at or below FL 350, g) APU is used as air source for takeoff or ADP inoperative penalties are applied, h) Center Hydraulic Motor Generator (HMG) is not required, i) For CF6-80C2 engines, associated thrust reverser is secured in forward thrust position, and j) Appropriate performance adjustments are applied for either of the following conditions: 1) Associated fan air modulation valve secured in intermediate position, or 2) Associated fan air modulation valve open. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-10

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 12-2 Fan Air (Precooler) Control Systems 1) JT9D, CF6 & PW4000 C 2 0 (M)(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Associated fan air modulation valve is secured in an intermediate position, and b) Appropriate performance adjustments are applied. (M)(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Associated fan air modulation valve is secured full open, b) Appropriate performance adjustments are applied, and c) Airplane is not operated in known or forecast icing conditions. (M)(O) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Associated fan air modulation valve is secured full open, and b) Airplane is not operated in known or forecast icing conditions. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-11

a) -200/-300

b) RB211

21-1

Bleed Air DUCT PRESS Indicating System 1) DUCT PRESS Indicators (P5 Panel) 2) Manifold Pressure Sensing Systems (-400ER) C 2 1

(M) One may be inoperative provided associated pack flow control valve inlet pressure sensor is verified to operate normally.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 21-2 Engine Bleed Air OFF Lights Intermediate Pressure Sensing Systems (-400ER) C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-12

21-3

(M)(O) One may be inoperative provided: a) Associated PRV operates normally, b) Associated HPSOV is verified closed, c) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, d) Remaining (opposite) engine bleed system operates normally, e) Hydraulic Motor Generator (HMG) is not required, and f) For CF6-80C2 engines, 1) Associated thrust reverser is secured in forward thrust position, and 2) Appropriate performance adjustments are applied. (M)(O) One may be inoperative provided: a) Associated high stage bleed valve/HPSOV is secured closed, b) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, c) Remaining (opposite) engine bleed system operates normally, d) Center Hydraulic Motor Generator (HMG) is not required, and e) For CF6-80C2 engines, 1) Associated thrust reverser is secured in forward thrust position, and 2) Appropriate performance adjustments are applied. (M)(O) One may be inoperative provided: a) Associated high stage bleed valve/HPSOV is secured closed, b) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, c) Remaining (opposite) engine bleed system operates normally, and d) Center Hydraulic Motor Generator (HMG) is not required.

22-1

BLEED Lights (-200/-300)

22-2

HI STAGE Lights (JT9D & CF680A/A2)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 36 - PNEUMATICS 22-3 OVHT Lights (CF680C2, PW4000 & RB211) 1) -200/-300 C 2 1 (M)(O) One may be inoperative provided: a) Associated HPSOV is secured closed, b) A minimum of 70% (55% below 10,000 feet MSL) N1 is maintained on associated engine in icing conditions, c) Remaining (opposite) engine bleed system operates normally, d) Center Hydraulic Motor Generator (HMG) is not required, and e) For CF6-80C2 engines, 1) Associated thrust reverser is secured in forward thrust position, and 2) Appropriate performance adjustments are applied. (O) May be inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 36-13

2) -400ER 22-4 L and R Bleed ISLN VALVE Lights 1) -200/-300

(O) One may be inoperative provided associated duct pressure indicator operates normally.

2) -400ER 22-5 C Bleed ISLN VALVE Light APU Bleed VALVE Light Manifold Temperature Sensing Systems (-400ER)

C C

2 1

0 0

22-6

22-7

(M) May be inoperative provided associated pack inlet temperature sensor is verified to operate normally.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 38 - WATER / WASTE 10-1 Potable Water Systems C NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 38-1

(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.

(M) May be inoperative provided: a) System is drained, and b) Procedures are established to ensure that system is not serviced. (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.

30-1

Lavatory Waste Systems (Including Wheelchair Accessible Lavatories)

(M) Associated lavatory system(s) may be inoperative provided: a) Associated components are deactivated or isolated to prevent leaks, b) Pilot-in-Command will determine if flight duration is acceptable with a FWD lavatory unusable, and c) Associated lavatory door(s) is secured closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit inspections by crewmembers.

32-1 ***

Tank Precharge Control Systems

(M) May be inoperative provided applicable precharge control valve is secured in open position.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 46 INFORMATION SYSTEMS 20-1 *** Electronic Flight Bag (EFB) System 1) Class 3 EFB (Boeing) C C 2 2 1 0 (O) May be inoperative provided alternate procedures are established and used. NOTE: Any function, program or document which operates normally may be used. D *** 2) Airport Moving Map Database a) STC ST02126LA *** 3) Navigation Database a) STC ST02126LA D 1 0 May be out of date provided Merging & Spacing operations are prohibited. (O) May be out of date provided merge waypoint is not inserted for Merging & Spacing function. D 2 0 (O) May be out of date provided alternate procedures are established and used. 2 0 May be inoperative provided procedures do not require its use. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/05/2009 MASTER MINIMUM EQUIPMENT LIST 33 PAGE: 46-1

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 47 INERT GAS SYSTEM *** 11-1 Nitrogen Gas Generation (NGS) A 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS | | | | | | | 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 47-1

(M) May be inoperative off provided: a) NGS Shutoff valve is deactivated closed, and b) Repairs are made within ten flight days.

1) Nitrogen Generation Performance

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 49 - AIRBORNE AUXILIARY POWER 11-1 Auxiliary Power Unit (APU) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 49-1

Except for ER operations, may be inoperative provided both engine generators operate normally. (M) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Both engine generators operate normally, and b) Hydraulic Motor Generator (HMG) is verified to operate normally. May be inoperative provided procedures do not require its use.

1) Pneumatic Function 15-1 APU Air Intake Door Actuation System 1) Door Closed

(M) May be inoperative secured closed provided APU is considered inoperative. (M)(O) May be inoperative fully open provided AFM performance decrements are applied.

2) Door Fully Open (-200/-300) 3) Door Partially Open a) -200/-300

(O) May be inoperative partially open provided: a) AFM performance decrements are applied, and b) APU is considered inoperative. (O) May be inoperative partially open provided: a) APU is considered inoperative, and b) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided door is secured in flight position.

b) -400ER

4) Door in Flight Position (-400ER) 61-1 APU External Control System

May be inoperative and APU used, provided a qualified operator remains in vicinity of flight deck APU control. (M) May be inoperative and APU used, provided an APU automatic fire extinguishing system is installed and verified to operate normally.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 49 - AIRBORNE AUXILIARY POWER 61-2 APU Controller Faults (-400ER) APU FAULT Light APU RUN Light C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 49-2

May be dispatched with faults annunciated by APU CONTROL status message.

70-1 70-2

C C

1 1

0 0 (O) May be inoperative provided another acceptable means to verify APU condition is available and used.

71-1

APU EGT Indication

72-1 ***

APU Hourmeter System

(M) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (M) May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use.

72-2 ***

APU Cyclemeter System

D 73-1 *** 94-1 APU RPM Indication APU OIL QTY Indication D

1 1

0 0

May be inoperative provided APU is considered inoperative. (M) May be inoperative provided oil quantity is verified by alternate means.

94-2

APU OIL TEMP Indication System (-400ER)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 11-1 Main Entry/Service Door Armed Indicators C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-1

(M) May be inoperative provided a procedure is used to verify that mode select mechanism is in slide armed mode before departure and in slide disarm mode before a non-emergency opening. May be damaged or missing.

11-2 ***

Main Entry/ Service Door Arming Lever Hinged Covers Entry Door Power Opening Assist Main Entry Doors/Slides/ Emergency Exits 1) Passenger Configuration

11-3

11-4

(M)(O) One may be inoperative or slide missing provided: a) All other main entry doors/exits are fully operational, b) Affected door is not used for passenger loading, c) A conspicuous barrier strap or rope and a placard stating that door is inoperative shall be placed across inoperative door, d) Emergency exit sign and floor proximity lights associated with inoperative exit must be covered to obscure signs and lights, e) Passengers must be briefed not to use affected door, f) All passenger seats halfway to next exit in each direction from inoperative door, across entire width of airplane, shall be blocked off with conspicuous tapes or ropes that contrast with interior prior to loading passengers. Only seats in these areas shall be blocked: main passenger aisles, cross aisles, and exit areas must not be blocked. (For an inoperative forward door/slide, blocked seating area shall extend from forward cabin end, rearward to a line halfway between inoperative forward door and next set of doors aft of inoperative one. For an inoperative rear door/slide, blocked seating area shall extend forward from aft cabin end to a line halfway between inoperative door and next set of doors forward of inoperative one), (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 11-4 Main Entry Doors/Slides/ Emergency Exits (Contd) 1) Passenger Configuration (Contd) g) Conspicuous signs and placards shall be placed in appropriate locations indicating these seats are not to be occupied by passengers, h) Seated capacity must not exceed rated capacity of remaining pairs of exits, i) For extended range/overwater operations, occupancy shall not exceed normal rated capacity of slide/rafts, or remaining slide/rafts or rated overload capacity of slide/rafts remaining after loss of one additional slide/raft of greatest capacity, whichever is least, j) Blocked seating layouts and evacuation procedures must be developed and approved by FAA certificate holding office for inclusion in operator's manual, and k) Repairs are made within one flight day. NOTE 1: Weight and balance manifest must be revised as necessary to ensure proper loading limits are observed. NOTE 2: Cabin attendants may be stationed in vicinity of each door within blocked area. 2) All Cargo Configuration a) All Doors Except L1/R1 b) Doors L1/R1 3) Combination Passenger/ Cargo Configurations C 0 All doors/slides may be inoperative or slides missing. | | | | | | | | | NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-2

C C

2 -

1 -

One door/slide may be inoperative or slide missing. All doors/slides in the cargo area may be inoperative or slide missing.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 30-1 Lower Cargo Doors 1) Cargo Door Lift/Latch Mechanisms (Std. DoorPassenger/ -200PC/-200SF/ ATC A1NM -200 SF/ -300BCF/ -300BDSF) C Either manual or electrical mode on each door may be inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-3

(M) Manual and electric modes may be inoperative provided associated door is verified closed and locked before each departure. Either manual or electrical mode on each door may be inoperative.

2) Cargo Door Hinge Power Units and Manual Hinge Drive Systems (Std. DoorPassenger/ -200PC/-200SF /ATC A1NM -200 SF/ -300BCF/ -300BDSF)

(M) Manual and electric modes may be inoperative provided associated door is verified closed and locked before each departure. (M) May be inoperative provided: a) Manual function operates normally, b) There is no damage to hook/latch mechanism, c) There is no damage to latch lock mechanism, d) Door is closed and locked using an accepted maintenance manual procedure, and e) All latch cams are visually confirmed to be in closed position before each departure.

3) Cargo Door Hook/Latch System Electrical Function (Large DoorPassenger/ -200PC/-200SF/ -300BCF/ -300BDSF) (Lower Doors -300F)

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 30-1 Lower Cargo Doors (Contd) 4) Cargo Door Lift System (Large DoorPassenger, -200PC/ -200SF/ -300BCF/ -300BDSF) (Lower Doors 300F) C Either manual or electric mode on each door may be inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-4

(M) Manual and electric modes may be inoperative provided associated door is verified closed and locked before each departure. Moved to 52-30-1-2, MMEL Rev. 19.

30-2

Cargo Door Hinge Power Units and Manual Hinge Drive Systems Cargo Door Control Panel Indicating Systems 1) DOOR OPEN Light (Std. Door Passenger/ -200PC/-200SF/ -300BDSF/ATC A1NM -200 SF/ -300BCF) 2) DOOR CLOSE Light (Std. Door Passenger/ -200PC/-200SF/ -300BDSF/ATC A1NM -200 SF/ -300BCF) C 0

30-3

May be inoperative provided DOOR CLOSE light operates normally.

(M) May be inoperative provided: a) Door Indication System for associated door is verified to operate normally, and b) Door is visually verified closed, latched, and locked before each departure.

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 30-3 Cargo Door Control Panel Indicating Systems (Contd) 3) DOOR OPEN and DOOR CLOSE Lights (Large Door Passenger/ -200PC/-200SF/ -300BDSF/ -300BCF) (Lower Doors -300F) 4) Main Deck Cargo Door Lights 32-1 Main Deck Cargo Door 1) Cargo Door Hook/Latch System (Electric) C 1 0 (M) May be inoperative provided: a) Manual function operates normally, b) There is no damage to hook/latch mechanism, c) There is no damage to lock mechanism, d) Door is closed and locked using an accepted maintenance manual procedure, and e) All latch cams are visually confirmed in closed position before each departure. C 0 (M) May be inoperative provided door is visually verified closed, latched, and locked before each departure. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-5

(M) May be inoperative provided door is visually verified closed, latched, and locked before each departure.

32-1

Main Deck Cargo Door (Contd) 2) Cargo Door Lift System (Manual and Electric) 3) Cargo Door Lock System (Electric) C 1 0 (M) May be inoperative provided door is verified closed, latched and locked before each departure.

(M) May be inoperative provided: a) Manual function operates normally, b) There is no damage to hook/latch mechanism, c) There is no damage to lock mechanism, d) Door is closed and locked using an accepted maintenance manual procedure, and e) All latch cams are visually confirmed in closed position before each departure.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 34-1 Cargo Door Stop Fitting Bearing Plates (Std. Doors Only) Bulk Cargo Door Balance Mechanism Crew Rest Doors (STC ST00973WI-D) C NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-6

One on forward and aft side of each cargo door frame may be missing.

35-1

(M) May be inoperative provided a safety hold open device is used when door is in open position. May be inoperative provided: a) Associated Crew Rest Area is not used and personal items are removed, and b) Associated Crew Rest Area door is locked closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit Crew Rest Area inspections by crew members.

50-1

1) Flight Crew Rest Door

(M) May be inoperative provided: a) Door is removed, and b) Crew rest area is not used for required crew member rest. (M) May be inoperative provided: a) Both attendant crew rest area doors are removed, and b) Crew rest area is not used for required crew member rest.

2) Attendant Crew Rest Doors

50-2 ***

Lower Lobe Crew Rest Doors (STC ST01994SE) 1) Main Entry C 2 0 Either or both the Main Entry Door and Main Entry Hatch may be inoperative provided: a) Associated Crew Rest Area is not used and personal items are removed, and b) Crew Rest Area Main Entry Door is locked closed and placarded INOPERATIVE DO NOT ENTER. NOTE: These provisos are not intended to prohibit Crew Rest Area inspections by crew members. (Continued)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 50-2 *** Lower Lobe Crew Rest Doors (STC ST01994SE) 2) Emergency Escape Hatch C 1 0 (M) May be inoperative provided: a) Associated Crew Rest Area is not used and personal items are removed, b) Associated Crew Rest Area main entry door is locked closed and placarded INOPERATIVE DO NOT ENTER, and c) Emergency Escape hatch is verified secured closed. (M) May be inoperative provided: a) Door can be locked and unlocked manually, and b) Door lock solenoid is deactivated in extended position. May be inoperative provided supplemental flight deck door security device is installed and operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-7

51-1 ***

Flight Deck Door Lock System (Not FAR 25.795 Compliant)

51-2

Rigid Barrier Access Door Latch System(s) (ATC A1NM -200SF/ -300BCF/ -300F/ -300BDSF) 1) Primary C 1 0 (M) May be inoperative provided: a) Door can be locked and unlocked manually with Secondary latch system, and b) Access to main cargo deck is prohibited in flight. May be inoperative provided Primary latch system operates normally.

2) Secondary

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 51-3 *** Boeing Enhanced Flight Deck Security Door Automatic Locking System (FAR 25.795 Compliant) A 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-8

(M)(O) May be inoperative provided: a) Automatic locking system is deactivated, b) Door dead bolt operates normally and is used to lock door, c) Alternate procedures are established and used for locking and unlocking door using dead bolt, and d) Repairs are made within two flight days. (M)(O) May be inoperative provided: a) Keypad is deactivated, and b) Alternate procedures are established and used. (O) May be inoperative provided alternate procedures are established and used. (O) May be inoperative provided alternate procedures are established and used. May be inoperative or missing provided alternate procedures are established and used. (M) May be inoperative provided automatic lock controls are verified to operate normally. (M) May be inoperative provided: a) Automatic lock controls are verified to operate normally, and b) Door chime operates normally. (M)(O) May be inoperative provided: a) Keypad is deactivated, b) Automatic lock is verified to operate normally, and c) Alternate procedures are established and used. (M) May be inoperative provided: a) Pressure sensing module is deactivated, and b) Repairs are made within two flight days. May be inoperative provided automatic lock controls operate normally.

1) Flight Deck Access Panel System (Keypad, Door Chime) a) LEDs

***

b) Door Bell Mode c) Switch Guard

2) Flight Deck Door LOCK FAIL Light 3) Flight Deck Door AUTO UNLK Light

4) Fight Deck Door Lock Control Selector

5) Pressure Rateof-Change Sensing Module 51-4 *** Boeing Enhanced Flight Deck Security Door Dead Bolt (FAR 25.795 Compliant)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 51-5 *** JAMCO Flight Deck Security Door Automatic Locking System (FAR 25.795 Compliant) C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-9

(M)(O) May be inoperative provided: a) Automatic locking system is deactivated, b) Mechanical Catch (Latch) Pin Lock 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 Lock. (M) One may be inoperative provided remaining locking solenoid is verified to operate normally.

1) Door Automatic Locking Solenoids 2) Door Warning System *** a) Speakers

(M)(O) One may be inoperative provided remaining speaker is verified to operate normally once each flight day.

***

b) LED (Green Indicator Lights) c) Aural Warning System

***

(M)(O) May be inoperative provided: a) Door AUTO UNLK light is verified to operate normally, and b) Alternate procedures are established and used.

3) Door Control Panel *** a) Door LOCK FAIL Light b) Door AUTO UNLK Light C 1 0 (M) May be inoperative OFF provided automatic lock controls are verified to operate normally. (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. (Continued)

***

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 51-5 *** JAMCO Flight Deck Security Door Automatic Locking System (FAR 25.795 Compliant) (Contd) 3) Door Control Panel (Contd) *** c) 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. (M)(O) May be inoperative provided: a) Door can be opened manually from flight deck, b) Remaining automatic lock controls are verified to operate normally, and c) Alternate procedures are established and used. (M)(O) May be inoperative provided: a) Automatic lock controls are verified to operate normally, and b) Aural warning system operates normally. (M) May be inoperative provided door aural warning system is verified to operate normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-10

***

d) Door UNLKD Switch/ UNLK Switch Position

***

e) Door UNLKD Light

***

f) Door EMRG ENTRY ACTIVE Light g) Door OPEN Light 4) FLIGHT DECK DOOR Warning/ Caution Light 5) Cabin Pushbutton Entry Pad/ Keypad

***

(M)(O) May be inoperative provided automatic lock controls are verified to operate normally.

***

(O) May be inoperative provided alternate procedures are established and used.

***

a) Keypad Indicator Lights

(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 FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 52 - DOORS 51-6 *** JAMCO Flight Deck Security Door Mechanical Catch (Latch) Pin Lock (FAR 25.795 Compliant) Smoke Barrier Access Door Latch System(s) (-200SF) 1) Primary C 1 0 May be inoperative provided door can be locked and unlocked with secondary latch system. May be inoperative provided primary latch system operates normally. C 1 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 08/20/2010 MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 52-11

(M) May be inoperative provided automatic lock system is verified to operate normally.

51-7

2) Secondary

71-1

Door Indication Systems 1) All Doors Except Main Deck Cargo Door 2) Main Deck Cargo Door (All Except ATC A1NM -200SF and -300BCF) C 0 (M) May be inoperative provided associated door(s) is verified closed, latched, and locked before each departure. (M) May be inoperative provided associated door(s) is verified closed, latched, and locked before each departure.

73-1 ***

Entry/Service Door Slide Armed Indicating Light System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 56 - WINDOWS 11-1 Flight Compartment Windows Entry/Service Door Viewport Heated Pane(s) B 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/05/2009 MASTER MINIMUM EQUIPMENT LIST 33 PAGE: 56-1

DELETED REVISION 33.

31-1 ***

(M) May be inoperative provided heated panes are deactivated.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 73 - ENGINE FUEL & CONTROL 14-1 Fuel Filter Heater Systems (JT9D) C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 73-1

08/20/2010

(M)(O) May be inoperative provided: a) Heater valve is verified closed or a blanking plate is installed, b) Fuel temperature indication operates normally, and c) Airplane is not operated with fuel temperature at or below -20 degrees C with IDG(s) on associated engine(s) operating normally. (M)(O) May be inoperative provided: a) Heater valve is verified closed or a blanking plate is installed, b) Fuel temperature indication operates normally, and c) Airplane is not operated with fuel temperature at or below +5 degrees C with IDG(s) on associated engine(s) operating inoperative. (O)May be inoperative.

1) Automatic Function 14-2 Fuel Heater VALVE Lights (JT9D) Fuel FILTER Bypass Lights (JT9D)

14-3

(M)(O) May be inoperative provided: a) Associated fuel filter heater system operates normally, and switch remains in AUTO, b) Associated fuel filter pressure switch operates normally, and c) Associated fuel filter is checked for presence of contaminants before each departure.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 73 - ENGINE FUEL & CONTROL 21-1 Electronic Engine Control (EEC) Systems 1) JT9D & CF6 Supervisory A 2 0 (O) For ER operations, may be inoperative provided: a) Both EECs are OFF, and b) Repairs are made within three flight days. (O) Except for ER operations, may be inoperative provided both EECs are OFF. (O) One may be inoperative provided: a) Both engines are operated in alternate (ALTN) mode, and b) Appropriate procedures, AFM limitations and performance decrements are applied. (O) One may be inoperative provided both engines are operated in alternate (ALTN) mode. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 73-2

08/20/2010

2) EEC NORM Mode (PW4000 & RB211)

3) EEC NORM Mode (CF6 FADEC) 4) EEC C1 Faults (PW4000)

May be dispatched with C1 faults provided repairs are made in accordance with times established by PW engine Type Certificate Data Sheet number E24NE, note 19. May be dispatched with C1 faults provided repairs are made in accordance with times established by CF680C2 Engine Manual GEK 92451, Task 05-51-73-200801. May be dispatched with C1 faults provided repairs are made in accordance with times established by RR engine Type Certificate Data Sheet number E30NE, note 17.

5) EEC C1 Faults (CF6 FADEC)

| | |

6) EEC C1 Faults (RB211)

May be dispatched with C1 faults provided repairs are made in accordance with times established by

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 73 - ENGINE FUEL & CONTROL 21-2 Electronic Engine Control (EEC) INOP/NORM/ ALTN Lights 1) EEC INOP (JT9D & CF6 Supervisory) C 2 0 (O) Except for ER operations, may be inoperative provided both EECs are OFF. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 73-3

08/20/2010

(O) May be inoperative provided: a) Both EECs are OFF, and b) Repairs are made within three flight days. (O) May be inoperative provided: a) Both EECs are operated in alternate (ALTN) mode, and b) Appropriate procedures, AFM limitations and performance decrements are applied.

2) EEC NORM/ALTN Lights (PW4000 & RB211)

3) EEC NORM/ALTN Lights (CF6 FADEC) a) -200/-300 C 2 0 (O) May be inoperative provided both EECs are operated in alternate (ALTN) mode.

b) -400ER 21-3 Fuel Control ENG VALVE Indication System 1) Fuel Control ENG VALVE Lights (-200/ -300) 2) Fuel Control ENG FUEL VAL Indication System (GE FADEC & PW4000) 21-4 Flight Idle/Ground Idle Systems

(M) May be inoperative provided associated engine fuel valve is verified to operate normally.

(M)(O) One may be inoperative provided: a) Associated engine fuel valve is verified to operate normally, and b) Associated EICAS message is deactivated.

Moved to 73-21-8, MMEL Rev. 19.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 73 - ENGINE FUEL & CONTROL 21-5 EEC Rating Data Entry Plug (PW4000) Turbine Overspeed Systems (RB211) Hydromechanical N2 Speed Governors (CF6 FADEC) Approach Idle/Minimum Idle Systems 1) Minimum Ground Idle (RB211, JT9D, & CF6 Supervisory) 2) Minimum Ground Idle (PW4000 & CF6 FADEC) C 2 0 (O) May be inoperative provided: a) Flight idle operates normally, and b) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) Flap actuated approach idle is verified to operate normally, and b) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided flap actuated approach idle is verified to operate normally. C 2 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 73-4

08/20/2010

Deleted, MMEL Rev. 17.

21-6

21-7

21-8

***

3) Continuous Ignition Actuated Approach Idle (PW4000 & CF6 FADEC) Engine Supplemental Control Unit (PW4000)

21-9 ***

(M) May be inoperative provided associated unit(s) is deactivated.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 73 - ENGINE FUEL & CONTROL 31-1 Fuel Flow Indications 1) JT9D C 2 1 (M) One may be inoperative provided: a) Associated N1, N2, and EPR indications operate normally, b) Main tank fuel quantity indicators operate normally, c) On airplanes with Simmonds FQIS PN S345N001-032, right and left main tank densitometers are disconnected for ER operations, and d) Autothrottle is not used. (M) One may be inoperative provided: a) Associated N1 and N2 indications operate normally, b) Main tank fuel quantity indicators operate normally, and c) On airplanes with Simmonds FQIS PN S345N001-032, right and left main tank densitometers are disconnected for ER operations. (M) One may be inoperative provided: a) Associated N1, N2, and EPR indications operate normally, b) Main tank fuel quantity indicators operate normally, and c) On airplanes with Simmonds FQIS PN S345N001-032, right and left main tank densitometers are disconnected for ER operations. (Continued) NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 73-5

08/20/2010

2) CF6

3) PW4000

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 73 - ENGINE FUEL & CONTROL 31-1 Fuel Flow Indications (Contd) 4) RB211 C 2 1 (M) One may be inoperative provided: a) Associated N1, N2, N3 and EPR indications operate normally, b) Main tank fuel quantity indicators operate normally, and c) On airplanes with Simmonds FQIS PN S345N001-032, right and left main tank densitometers are disconnected for ER operations. Moved to 28-43-1, MMEL Rev. 8. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS MASTER MINIMUM EQUIPMENT LIST 33c PAGE: 73-6

08/20/2010

32-1

Fuel Temperature Indicating System

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM REVISION NO : DATE: 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 74-1

2.

NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS

74 - ENGINE IGNITION 00-1 Ignition Systems A 4 3

(O) One may be inoperative provided: a) Ignition selector remains in BOTH position, b) Engine anti-ice system operates normally on associated engine, and c) Repair is made within one flight day. (O) Except for ER operations, one per engine may be inoperative provided: a) Ignition selector remains in BOTH position, and b) Engine anti-ice systems operate normally on associated engine(s). (O) May be inoperative provided start selector switch(es) AUTO position is placarded INOP, and that position is not used.

00-2

Auto Ignition (RB211)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 75 BLEED AIR 21-1 IDG Air/Oil Cooler Valves 1) JT9D & CF680A/A2 2) CF6-80C2 C 2 0 (M) May be inoperative open. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 75-1

(M)(O) May be inoperative provided: a) Valve(s) is deactivated open, and b) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) If engine AOC operates normally and IDG is connected, fuel tank temperature remains above -42 degrees C throughout flight, b) Valve(s) is deactivated open, and c) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) If engine AOC operates normally and IDG is disconnected, fuel tank temperature remains above -36 degrees C throughout flight, b) Valve(s) is deactivated open, and c) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) If engine AOC is inoperative open and IDG is connected, fuel tank temperature remains above -34 degrees C throughout flight, b) Valve(s) is deactivated open, and c) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) If engine AOC is inoperative open and IDG is disconnected, fuel tank temperature remains above -30 degrees C throughout flight, b) Valve(s) is deactivated open, and c) Appropriate performance adjustments are applied. (Continued)

3) PW4000

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 75 BLEED AIR 21-1 IDG Air/Oil Cooler Valves (Contd) 4) RB211 21-2 Engine Air /Oil Cooler Valves (PW4000) C C 2 2 0 0 (M) May be inoperative deactivated open. (M)(O) May be inoperative provided: a) If IDG is connected, fuel tank temperature remains above -34 degrees C throughout flight, b) Valve(s) is deactivated open, and c) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) If IDG is disconnected, fuel tank temperature remains above -30 degrees C throughout flight, b) Valve(s) is deactivated open, and c) Appropriate performance adjustments are applied. (M)(O) May be inoperative provided: a) Associated valve remains open, and b) For PW4000, appropriate performance adjustments are applied. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 75-2

23-1

Nacelle Zone Ventilation Valves (PW) and Core Compartment Cooling Valves (GE) Bore Cooling System (CF6FADEC) Turbine Case Cooling Systems (JT9D, CF6-80A/A2, PW4000 & CF6 FADEC)

23-2

Deleted, MMEL Rev. 8.

24-1

(M) May be inoperative provided associated turbine case cooling valve remains closed.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 75 BLEED AIR 24-2 *** Turbine Cooling Air Systems 1) Turbine Vane and Blade Cooling (TVBC) Systems (PW4000) 2) Eleventh Stage Cooling Valve (ESCV) Systems (CF6 FADEC) C 2 0 (M) May be inoperative provided associated turbine cooling valves are deactivated open. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 75-3

(M) May be inoperative provided associated turbine cooling valves are deactivated open.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 77 - ENGINE INDICATING 00-1 Target Parameter Indications Engine Pressure Ratio (EPR) Systems 1) JT9D C 2 1 (O) EICAS and/or STANDBY indications for one engine may be inoperative provided: a) Appropriate procedures, AFM limitations, and performance decrements are applied, b) N1 and N2 EICAS indications for associated engine operate normally, c) N1 STANDBY indications for associated engine operate normally, d) Fuel flow systems for associated engine operate normally, and e) Approach minimums do not require its use. (O) EICAS and/or STANDBY indications for one engine may be inoperative provided: a) Both EECs are switched to ALTN mode, b) Appropriate procedures, AFM limitations, and performance decrements are applied, c) N2 EICAS indications for both engines operate normally, d) For RB211, N3 EICAS indications for both engines operate normally, e) Fuel flow indications for associated engine operate normally, and f) Approach minimums do not require its use. (O) EICAS and/or STANDBY indications for one engine may be inoperative provided: a) EPR (EICAS and STANDBY) indications for both engines operate normally, b) N2 EICAS indications for associated engine operate normally, and c) Fuel flow indications for associated engine operate normally. (M) One N2 indication may be inoperative provided only indication function is inoperative. C 0 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 77-1

(O) May be inoperative provided an alternate means of achieving desired values is available and used.

11-1

2) PW4000 & RB211

12-1

N1 Tachometer Systems (JT9D)

12-2

N2 Tachometer Systems (EICAS) (-200/-300)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 77 - ENGINE INDICATING 12-3 N2 Tachometer Systems (Standby Engine Indicator (RB211)) N3 Tachometer Systems (EICAS) (RB211) EGT Indications (Standby Engine Indicator) (-200/-300) 1) JT9D C 2 1 One may be inoperative provided: a) EGT EICAS indication operates normally, b) N1 EICAS and Standby indications for both engines operate normally, c) N2 EICAS indications for both engines operate normally, and d) EPR EICAS indications for both engines operate normally. One may be inoperative provided: a) EGT EICAS indication operates normally, and b) N2 EICAS indications for both engines operate normally. B 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 77-2

Deleted, MMEL Rev. 25.

12-4

(O) One N3 indication may be inoperative provided only indication function is inoperative.

21-1

2) CF6

3) PW4000

One may be inoperative provided: a) EGT EICAS indication operates normally, b) N2 EICAS indications for both engines operate normally, and c) EPR EICAS indications for both engines operate normally. One may be inoperative provided: a) EGT EICAS indication operates normally, b) N2 EICAS indications for both engines operate normally, c) N3 EICAS indications for both engines operate normally, and d) EPR EICAS indications for both engines operate normally.

4) RB211

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 77 - ENGINE INDICATING 22-1 Engine Turbine Overheat Detection Systems (RB211) 1) Loops 31-1 Vibration Indicating Systems C C 4 2 2 1 One Loop per engine may be inoperative. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 77-3

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 78 - ENGINE EXHAUST 31-1 Thrust Reversers C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 78-1

(M)(O) One may be inoperative provided: a) Inoperative reverser is secured in forward thrust position, and b) Appropriate performance adjustments are applied. NOTE: During landing roll-out, differential braking may be required to maintain directional control.

34-1

REV ISLN Valve Light (-200/-300)

(M)(O) May be inoperative provided reverser isolation valve and reverser unlock indications operate normally. (O) One may be inoperative extended or retracted provided appropriate performance adjustments are applied. NOTE: Associated reverser thrust is limited to reverse idle when inoperative retracted.

34-2

Engine Reverse Lever Interlocks (RB211, PW4000 and CF6 FADEC)

34-3

Thrust Reverser Air System (RB211 & CF6-80C2) 1) Thrust Reverser PRSOV (CF680C2) C 2 1 (M)(O) One may be inoperative provided: a) Associated thrust reverser is secured in forward thrust position, and b) Appropriate performance adjustments are applied. (M)(O) One may be inoperative provided: a) Associated thrust reverser is secured in forward thrust position, and b) Appropriate performance adjustments are applied. (M)(O) One may be inoperative provided: a) No thrust reverser damage exists which would adversely affect airplane operation, b) Thrust reverser for associated engine is deactivated and locked in stowed (forward thrust) position, and c) Appropriate performance adjustments are applied. May be inoperative provided associated reverser unlock indication operates normally.

2) Thrust Reverser Air Motor Shutoff Valves (RB211)

36-1

REV Unlock Indications

36-2

Full REV Position Indications

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 78 - ENGINE EXHAUST 36-3 Reverser Position Sensing Systems (RB211, PW4000 & CF6 FADEC) C 2 1 NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 05/01/2010 MASTER MINIMUM EQUIPMENT LIST 33b PAGE: 78-2

(M)(O) One may be inoperative provided: a) Associated thrust reverser is secured in forward thrust position, and b) Appropriate performance adjustments are applied.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 79 - ENGINE OIL 31-1 OIL QTY Indications 1) -200/-300 B 2 1 (M) One may be inoperative provided: a) Oil tank is filled to recommended capacity before each departure, b) There is no evidence of above normal oil consumption or leakage, c) Associated ENG OIL PRESS and OIL TEMP indications operate normally, and d) Associated low ENG OIL PRESS light operates normally. (M) One may be inoperative provided: a) Oil tank is filled to recommended capacity before each departure, b) There is no evidence of above normal oil consumption or leakage, and c) Associated ENG OIL PRESS and OIL TEMP indications operate normally. (M)(O) May be inoperative provided oil pressure indication operates normally. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 06/18/2009 MASTER MINIMUM EQUIPMENT LIST 33a PAGE: 79-1

2) -400ER

32-1

L/R Oil Press Sensor Select Module (OPSSM) (RB211) Low ENG OIL PRESS Indication System (-200/ -300) 1) All except JT9D without SB76778-8 Installed, and CF6-80A/A2 without SB76778-8 Installed 2) JT9D without SB767-78-8 Installed, CF680A/A2 without SB767-78-8 Installed

33-1

May be inoperative provided associated OIL PRESS, TEMP and QTY indications operate normally.

(M) May be inoperative provided: a) Associated OIL PRESS, TEMP and QTY indications operate normally, and b) Thrust reverser is verified to operate normally.

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 79 - ENGINE OIL 34-1 Engine Bearing No. 3 Scavenge Oil Temperature Indications (PW4000) 1) L/R SCAV TEMP1 2) L/R SCAV TEMP2 34-2 ENG OIL TEMP Sensing Elements (JT9D, CF6-80A/A2, CF6-80C2 (PMC)) Engine Oil Filter Bypass Warning Systems (PW & GE) A 2 1 (M) May be dispatched with one message displayed provided repairs are made within three flight days. (M) May be dispatched with one message displayed provided repairs are made within ten flight days. (O) One sensing element on each engine may be inoperative provided both engine oil temperature indications are available from one EICAS computer. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 06/18/2009 MASTER MINIMUM EQUIPMENT LIST 33a PAGE: 79-2

35-1

(M) May be inoperative provided: a) It is verified that malfunction is in alerting system, and b) Main oil screen is checked for contaminants before each departure. (M) One may be inoperative provided: a) It is verified that malfunction is in alerting system, b) Pressure filter is replaced, and c) Magnetic Chip Detector is checked for contaminants before each departure. (M) One may be inoperative provided: a) It is verified that malfunction is in alerting system, b) Fine scavenge oil filter is replaced, and c) Magnetic Chip Detector is checked for contaminants before each departure.

35-2

Engine High Pressure Oil Filter Warning Indication (Approaching Blockage) (RB211)

35-3

Engine Fine Scavenge Oil Filter Warning Indications (Impending Bypass) (RB211)

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT: B-767 SYSTEM & SEQUENCE NUMBER 1. ITEM 2. REVISION NO : DATE: NUMBER INSTALLED 3. 80 - STARTING 00-1 Engine Start VALVE Lights 1) -200/-300 C 2 1 (O) One may be inoperative provided associated valve is verified closed after engine start. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 04/29/2008 MASTER MINIMUM EQUIPMENT LIST 32b PAGE: 80-1

2) -400ER 00-2 Engine Start Valves 1) -200/-300

(M)(O) One may be inoperative provided: a) Associated start VALVE light operates normally, and b) Manual override start procedures are used. (M)(O) One may be inoperative provided manual override start procedures are used. (O) May be inoperative provided alternate procedures are established and used.

2) -400ER

11-2

Starter Switch Holding/Cutout Systems