U.S.

Department of Transportation
Federal Aviation Administration
Washington, D.C.

Master Minimum Equipment List

Revision: 14b
Date: 08/27/2010

Hawker Beechcraft Corporation

Beechcraft Model 200 and F90

Applicable Models:
200 / 200C / 200CT / 200T / A100-1 / A200 / A200C / A200CT
B200 / B200C / B200CT / B200T / B200GT / B200CGT
and
F90

Johnathon A Vetter, Chairman

Flight Operations Evaluation Board (FOEB)

Federal Aviation Administration

Aircraft Evaluation Group
DOT Building, Room 332
901 Locust Street
Kansas City, MO 64106-2641

Telephone: (816) 329-3233

FAX: (816) 329-3241
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 I
TABLE OF CONTENTS
SYSTEM NO. SYSTEM PAGE NO.

-- Table of Contents I
-- Log of Revisions II, III, IV
-- Control Page V, VI, VII
-- Highlights of Change VIII
-- Definitions IX
-- Preamble X
-- Guidelines for (O) & (M) Procedures XI THRU XVIII
21 Air Conditioning 21-1, 2, 3
22 Auto Flight 22-1, 2, 3
23 Communications 23-1 THRU 23-6
24 Electrical Power 24-1, 2
25 Equipment/Furnishings 25-1 THRU 25-7
26 Fire Protection 26-1, 2
27 Flight Controls 27-1
28 Fuel 28-1, 2
30 Ice and Rain Protection 30-1, 2, 3, 4, 5
31 Indicating/Recording Systems 31-1, 2
32 Landing Gear 32-1
33 Lights 33-1, 2, 3
34 Navigation 34-1 THRU 34-15
35 Oxygen 35-1
37 Vacuum/Pressure 37-1
46 Information Systems 46-1, 2
52 Doors 52-1
61 Propellers 61-1
73 Engine Fuel & Control 73-1
77 Engine Indicating 77-1
79 Engine Oil 79-1
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 10 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 04/08/2002 II
Log of Revisions
Rev No. Date Page Numbers Initials

0 02/27/1980
1 11/04/1981 Pen & Ink change to add Beech
B200C after the 200CT
2 02/01/1982 Pen & Ink change to include
Beech F-90
3 11/10/1983 All pages
4 07/30/1984 28-1
5 03/09/1988 All pages
6 07/07/1988 Page 21-2
7 03/16/1989 All pages
8 06/19/1989 DEFINITIONS, PREAMBLE
8a 04/16/1991 HIGHLIGHTS OF REV., DEFINITIONS
8a 04/16/1991 23-1
8b 01/13/1992 HIGHLIGHTS OF REV., GUIDELINES
8b 01/13/1992 22-1
9 07/08/1994 HIGHLIGHTS OF REV., DEFINITIONS
9 07/08/1994 GUIDELINES
9 07/08/1994 21-1, 21-2, 22-1, 23-1, 23-2
9 07/08/1994 24-1, 25-1, 25-2, 26-1, 27-1
9 07/08/1994 28-1, 28-2, 30-1, 30-2, 31-1
9 07/08/1994 32-1, 33-1, 33-2, 34-1, 34-2
9 07/08/1994 34-3, 34-4, 34-5, 34-6, 35-1
9 07/08/1994 52-1, 61-1
9a 08/17/1994 HIGHLIGHTS OF REV.
9a 08/17/1994 23-2
9b 10/20/1994 HIGHLIGHTS OF REV.
9b 10/20/1994 35-1
9c 03/17/1999 HIGHLIGHTS OF REV., DEFINITIONS
9c 03/17/1999 GUIDELINES
9c 03/17/1999 23-1, 25-1, 25-2, 26-1, 33-1
9c 03/17/1999 33-2, 34-1, 34-2, 34-3, 34-4
9c 03/17/1999 34-5, 34-6, 34-7, 61-1
9d 10/12/1999 HIGHLIGHTS OF REV., DEFINITIONS
9d 10/12/1999 PREAMBLE, GUIDELINES
9d 10/12/1999 34-7, 61-1
9e 09/27/2000 HIGHLIGHTS OF REV., DEFINITIONS
9e 09/27/2000 GUIDELINES
9e 09/27/2000 33-2, 34-1, 34-2, 34-3, 34-4
9e 09/27/2000 34-5, 34-6, 34-7, 34-8, 34-9
10 04/08/2002 HIGHLIGHTS OF REV., DEFINITIONS
10 04/08/2002 GUIDELINES
10 04/08/2002 21-1, 21-2, 22-1, 23-1, 23-2
10 04/08/2002 23-3, 24-1, 25-1, 25-2, 25-3
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 13 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 8/17/2004 III
Log of Revisions
Rev No. Date Page Numbers Initials

10 04/08/2002 26-1, 26-2, 27-1, 28-1, 28-2

10 04/08/2002 30-1, 30-2, 31-1, 32-1, 33-1
10 04/08/2002 33-2, 34-1, 34-2, 34-3, 34-4
10 04/08/2002 34-5, 34-6, 34-7, 34-8, 34-9
10 04/08/2002 34-10, 34-11, 35-1, 52-1, 61-1
11 03/31/2003 HIGHLIGHTS OF REV., DEFINITIONS
11 03/31/2003 GUIDELINES
11 03/31/2003 21-1, 21-2, 21-3, 22-1, 22-2
11 03/31/2003 23-1, 23-2, 23-3, 23-4, 24-1
11 03/31/2003 24-2, 25-1, 25-2, 25-3, 25-4
11 03/31/2003 25-5, 26-1, 26-2, 26-3, 27-1
11 03/31/2003 27-2, 28-1, 28-2, 30-1, 30-2
11 03/31/2003 30-3, 31-1, 32-1, 33-1, 33-2
11 03/31/2003 33-3, 34-1, 34-2, 34-3, 34-4
11 03/31/2003 34-5, 34-6, 34-7, 34-8, 34-9
11 03/31/2003 34-10, 34-11, 34-12, 34-13, 34-14
11 03/31/2003 34-15, 34-16, 35-1, 37-1, 52-1
11 03/31/2003 61-1, 77-1, 79-1
12 11/03/2003 HIGHLIGHTS OF REV., DEFINITIONS
12 11/03/2003 GUIDELINES
12 11/03/2003 21-1, 21-2, 21-3, 22-1, 22-2
12 11/03/2003 23-1, 23-2, 23-3, 23-4, 23-5
12 11/03/2003 23-6, 24-1, 24-2, 25-1, 25-2
12 11/03/2003 25-3, 25-4, 25-5, 26-1, 26-2
12 11/03/2003 26-3, 27-1, 27-2, 28-1, 28-2
12 11/03/2003 30-1, 30-2, 30-3, 30-4, 32-1
12 11/03/2003 33-1, 33-2, 33-3, 34-1, 34-2
12 11/03/2003 34-3, 34-4, 34-5, 34-6, 34-7
12 11/03/2003 34-8, 34-9, 34-10, 34-11
12 11/03/2003 34-12, 34-13, 34-14, 34-15
12 11/03/2003 34-16, 35-1, 37-1, 52-1
12 11/03/2003 61-1, 77-1, 79-1
12a 02/25/2004 HIGHLIGHTS OF REV., DEFINITIONS
12a 02/25/2004 GUIDELINES
12a 02/25/2004 27-1, 79-1
13 08/17/2004 HIGHLIGHTS OF REV., DEFINITIONS
13 08/17/2004 GUIDELINES
13 08/17/2004 21-3, 22-1, 22-2, 23-2, 24-1
13 08/17/2004 24-2, 25-3, 25-4, 26-3, 27-1
13 08/17/2004 28-2, 30-1, 30-2, 30-3, 30-4
13 08/17/2004 30-5, 34-1, 34-2, 34-3, 34-4
13 08/17/2004 34-5, 34-6, 34-7, 34-8, 34-9
13 08/17/2004 34-10, 34-11, 34-12, 34-13
13 08/17/2004 34-14, 34-15, 34-16, 34-17
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 IV
Log of Revisions
Rev No. Date Page Numbers Initials

14 09/16/2008 HIGHLIGHTS OF REV., DEFINITIONS

14 09/16/2008 GUIDELINES
14 09/16/2008 21-1, 21-2, 21-3, 22-1, 22-2, 23-1, 23-2, 23-3,
14 09/16/2008 23-4, 23-5, 23-6, 24-1, 24-2, 25-2, 25-3, 25-4,
14 09/16/2008 25-5, 25-6, 25-7, 26-2, 27-1, 28-1, 28-2, 30-2,
14 09/16/2008 30-3, 30-4, 30-5, 31-1, 31-2,32-1, 33-1, 33-2,
14 09/16/2008 33-3, 34-1, 34-2, 34-3, 34-4, 34-5, 34-6, 34-7,
14 09/16/2008 34-8, 34-9, 34-10, 34-11, 34-12, 34-13, 34-14,
14 09/16/2008 34-16, 35-1, 46-1, 46-2, 52-1, 61-1, 73-1, 77-1
14 09/16/2008 79-1
14a 06/04/2010 Highlights of Change, Definitions, Preamble
14a 06/04/2010 Guidelines for (O) & (M), 21-2, 22-1, 34-5, 37-1
14b 08/27/2010 Highlights of Change, 22-1, 22-2, 22-3, 27-1,
14b 08/27/2010 28-1, 30-1, 30-2, 34-1, 34-2, 34-4, 34-5, 34-6,
14b 08/27/2010 34-7, 34-8, 34-9, 34-10, 34-11, 34-12, 34-13,
14b 08/27/2010 34-14, 34-15, 37-1, 46-2, 52-1, 61-1
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 V
Control Page
System Page No. Rev. No. Current Date

Cover Page - 14b 08/27/2010

Table of Contents I 14b 08/27/2010
Log of Revisions II 10 04/08/2002
III 13 08/17/2004
IV 14b 08/27/2010
Control Page V 14b 08/27/2010
VI 14b 08/27/2010
VII 14b 08/27/2010
Highlights of Change VIII 14b 08/27/2010
VIIIa 14b 08/27/2010
Definitions IX 14a 06/04/2010
Preamble X 14a 06/04/2010
Guidelines for (O) & (M) Procedures XI 14b 08/27/2010
XII 14b 08/27/2010
XIII 14b 08/27/2010
XIV 14b 08/27/2010
XV 14b 08/27/2010
XVI 14b 08/27/2010
XVII 14b 08/27/2010
XVIII 14b 08/27/2010
21 21-1 14 09/16/2008
21-2 14a 06/04/2010
21-3 14 09/16/2008
22 22-1 14b 08/27/2010
22-2 14b 08/27/2010
22-3 14b 08/27/2010
23 23-1 14 09/16/2008
23-2 14 09/16/2008
23-3 14 09/16/2008
23-4 14 09/16/2008
23-5 14 09/16/2008
23-6 14 09/16/2008
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 VI
Control Page
System Page No. Rev. No. Current Date

24 24-1 14 09/16/2008
24-2 14 09/16/2008
25 25-1 12 11/03/2003
25-2 14 09/16/2008
25-3 14 09/16/2008
25-4 14 09/16/2008
25-5 14 09/16/2008
25-6 14 09/16/2008
25-7 14 09/16/2008
26 26-1 12 11/03/2003
26-2 14 09/16/2008
27 27-1 14b 08/27/2010
28 28-1 14b 08/27/2010
28-2 14 09/16/2008
30 30-1 14b 08/27/2010
30-2 14b 08/27/2010
30-3 14 09/16/2008
30-4 14 09/16/2008
30-5 14 09/16/2008
31 31-1 14 09/16/2008
31-2 14 09/16/2008
32 32-1 14 09/16/2008
33 33-1 14 09/16/2008
33-2 14 09/16/2008
33-3 14 09/16/2008
34 34-1 14b 08/27/2010
34-2 14b 08/27/2010
34-3 14 09/16/2008
34-4 14b 08/27/2010
34-5 14b 08/27/2010
34-6 14b 08/27/2010
34-7 14b 08/27/2010
34-8 14b 08/27/2010
34-9 14b 08/27/2010
34-10 14b 08/27/2010
34-11 14b 08/27/2010
34-12 14b 08/27/2010
34-13 14b 08/27/2010
34-14 14b 08/27/2010
34-15 14b 08/27/2010
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 VII
Control Page
System Page No. Rev. No. Current Date

35 35-1 14 09/16/2008
37 37-1 14b 08/27/2010
46 46-1 14 09/16/2008
46-2 14b 08/27/2010
52 52-1 14b 08/27/2010
61 61-1 14b 08/27/2010
73 73-1 14 09/16/2008
77 77-1 14 09/16/2008
79 79-1 14 09/16/2008
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 VIII
HIGHLIGHTS OF CHANGE

The following changes are the Highlights of Changes for Revision 14a.

Definitions Revised to reference the source document for definitions to avoid

duplication of changes published to definitions policy letter.

Preamble Revised to reference the source document for Preambles, both certificated
operators and Part 91 operators, to discontinue publication of duplicate
MMELs for differences in the Preambles.

21-8 Delete duplicate relief for Instrument Air Bleed Shutoff Valves and add
cross-reference to Chapter 37.

22-2 Yaw Damper (F-90 with STC SA4130NM) correct error for Number
Required to “0”

22-3 Add applicability for Garmin GFC-700 AFCS to maintain at least 1 Control
Wheel Disconnect Button for Garmin autopilot system.

34-13 Specify applicability of Remarks to Class A TAWS and TCAS II only.

37-2 Instrument Air Valves Remarks changed to add an (M) procedure per
duplicate 21-8 relief to secure valve because a malfunctioning valve is
unreliable to simply switch OFF.

The following changes are the Highlights of Changes for Revision 14b.

Revision 14b incorporates Model 200 HDC MMEL Revision 2.

22-2 Yaw Damper (200 HDC) Added model.

22-6 Flight Director relief relocated to chapter 22

22-6-a Flight Director Mode Selection Panel Annunciator Lamps become Sub-Item

27-4 Add RVSM NOTE

28-1 Add applicability for 200HDC to Standby Boost Pump

30-2 Revise Ice Vane Annunciator Remarks to verify operative.

30-5 Revise Pitot Heat Remarks to correct format and separate relief criteria.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 VIIIa
HIGHLIGHTS OF CHANGE

34-1 & 2 Revised Remarks to stipulate Electronic Air Data System instead of EFIS
to correct unnecessary exclusion of Proline 2 equipped aircraft.

34-4 Revised Turn/Slip Remarks to remove EFIS restriction because not

applicable for right side instruments and Day VFR is mitigation for left side.

34-8 Navigation Equipment reformatted into sub items and Remarks revised to
address operational considerations:
VOR/ILS TACAN Systems, Glide Slope, Marker Beacon System, DME,
RNAV, ADF, RMI and FMS are Navigation Equipment sub items.

34-9-1 Add relief for Radar Stabilization to WX Radar.

34-11 Radar Altimeter relief renumbered and Remarks changed to accommodate

variable installations.

34-12 Altitude Alerting System relief renumbered

34-13 Gyro-magnetic Compass System relief renumbered
34-14 Non-Stabilized Magnetic Compass relief renumbered
34-15 & 16 Traffic Alert Collision Avoidance System relief renumbered
34-17 TAWS/GPWS relief renumbered
34-18 Traffic Awareness System (TCAD/TAS relief renumbered
34-19 Ground Proximity Altitude Advisory System (GPAAS) relief renumbered

34-20 Standby Attitude Indicator relief renumbered and Remarks revised to

account for Standby Attitude Indicator required by Type Design Approvals.

34-21 Flight Profile Advisory System relief renumbered

34-22 Independent Multi-Function Display relief renumbered
34-23 & 24 Windshear relief renumbered

34-25 ADS-B relief renumbered and undated per PL-105

37-2 Instrument Air Valves Remarks changed to (O) procedure because no

mechanical means to secure valve closed. Valve must be powered closed.

46-3 XM Weather System is renumbered to 3. to allow relief to be used for non-

IFIS-5000 independent systems and changed to Category D.

52-6 Added 200 HDC Baggage Pod Door Warning Light

61-1 Add applicability to Reverse not Ready to exclude A200CT.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14a PAGE:
Beechcraft Model 200 and F-90 DATE: 06/04/2010 IX
DEFINITIONS

The Definitions must be inserted here in each Minimum Equipment List (MEL) from
current FAA MMEL Policy Letter PL-25, MMEL DEFINITIONS in accordance with current
FAA MMEL Policy Letter PL-70, DEFINITIONS REQUIRED IN MELs.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14a PAGE NO.
Beechcraft Model 200 and F-90 DATE: 06/04/2010 X
PREAMBLE

The applicable Preamble must be inserted here in each Minimum Equipment List (MEL)
from current FAA MMEL Policy Letter PL-34, MMEL AND MEL PREAMBLE or PL-36,
FAR PART 91MEL APPROVAL AND PREAMBLE.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 XI
Guidelines for (O) & (M) Procedures

The FOEB has identified a need for certain procedures to provide an adequate level of
safety while providing relief for the following items. These procedures must be
established by the operator. The following guidelines are to help establish these required
procedures:

21-1 (O) Procedure to ensure compliance with regulations, operational

requirements and passenger briefing information for unpressurized flight.

21-2 (M) Maintenance procedure to ensure the Safety Valve (Dump) is secured in
the open position.

(O) Procedure to ensure compliance with regulations, operational

requirements and passenger briefing information for unpressurized flight.

21-3 (M) Maintenance procedure to ensure the Safety Valve (Dump) is secured in
the open position.

(O) Procedure to ensure compliance with regulations, operational

requirements and passenger briefing information for unpressurized flight

21-4,5,6 (O) Procedure to ensure compliance with regulations, operational

requirements and passenger briefing information for unpressurized flight.

21-7 (M) Maintenance procedure to determine Bleed Air Shutoff Valve(s) are
secure in the closed position.

(O) Procedure to ensure compliance with regulations, operational

requirements and passenger briefing information for unpressurized flight.

21-9 (M) Maintenance procedure to determine Bleed Air Shutoff Valve(s) are
secure in the closed position.

(O) Procedure to ensure compliance with regulations, operational

requirements and passenger briefing information for unpressurized flight.

21-14 (M) Maintenance procedure to deactivate and secure Air Conditioner.

21-16-1 (O) Procedure to verify affected Environmental and Instrument Bleed Air
Valves are selected OFF and verified closed prior to each flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 XII
Guidelines for (O) & (M) Procedures
21-16-2 (O) Procedure to verify affected Environmental and Instrument Bleed Air
Valves are selected OFF and verified closed prior to each flight.

21-18 & 19 (O) Procedure to ensure compliance with regulations, operational

requirements and passenger briefing information for unpressurized flight.

22-1 (M) Maintenance procedure to deactivate the autopilot and ensure no

electrical or mechanical fault exists that will have an adverse affect on any
Flight Control function.

22-2 (M) Maintenance procedure to deactivate the Yaw Damper and ensure no
electrical or mechanical fault exists that will have an adverse affect on any
Flight Control function.

22-3 (M) Maintenance procedure to deactivate & secure autopilot and electric trim.

22-4 (O) Procedure to establish alternate method to accomplish a go-around.

22-5 (O) Operations procedure to verify prior to departure, the proper Autopilot
Mode Annunciation is displayed on the pilot's panels(s).

22-6-a (O) Operations procedure to verify, prior to departure, the proper Autopilot
Mode Annunciation is displayed on the pilot's panels(s).

22-7 (O) Operations procedure to verify, prior to departure, the proper Autopilot
Mode Annunciation is displayed on the pilot's panel(s).

23-2-1 (O) Operations procedure to specify how passengers will be briefed for
normal and emergency operation.

23-3 (O) Operations procedure to ensure aural warnings are available. NOTE:
An acceptable test would be to activate the Stall Warning System.

23-10 (O) Operations procedure to ensure SATCOM Data Link System operates
normally.

23-11 (O) Operations procedure to ensure passengers are briefed prior to

departure.

23-16 (O) Procedure to provide alternate means to maintain contact with aircraft.

23-16-1 (O) Procedure to provide alternate means to maintain contact with aircraft.

24-7 (M) Maintenance procedure to deactivate and secure the Cabin AC Power
System.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 XIII
Guidelines for (O) & (M) Procedures
24-8 (M) Maintenance procedure to disconnect and remove the Standby Battery.

24-9 (M) Maintenance procedure to placard and secure access to the aircraft
External Power Receptacle.

24-10 (O) Operations procedure to verify connection and disconnection of External

Power Supply.

24-12 (O) Operations procedure to verify Generator Bus Tie Relay is CLOSED and
both DC GEN Annunciators are operative prior to departure.

25-1-1 (M) Maintenance procedure to secure the affected Arm Rest(s) in the full up
or full down position.

25-1-4 (M) Maintenance procedure to secure the affected Seat in a position

acceptable to the flight crew allowing for full Flight Control movement and
normal pilot visibility.

25-2-1 (M) Maintenance procedure to secure Seat in the full upright position.

25-5-2-a (M) Maintenance procedure to disconnect Remote Switch and verify ELT is
armed.

25-10 (M) Maintenance procedure to ensure the affected Receptacle is empty and
secured to prevent use.

(O) Operations procedure to ensure a sufficient number of Receptacles are

available for the flight.

25-11 (M) Maintenance procedure to ensure inoperative Cargo Restraints are

isolated from use and Cargo Loading Limits are observed for remaining
restraints.

25-12 (M) Maintenance procedure to secure the affected compartment closed.

(M) Maintenance procedure to remove the affected compartment door(s)

(O) Operations procedure to ensure crew awareness and passenger briefing

regarding use of affected storage compartment.

25-12-1 (M) Maintenance procedure to ensure door latch is operable.

25-13 (M) Maintenance procedure to remove or deactivate/secure inoperative

System or equipment.

(O) Operations procedure to ensure crew awareness of inoperative

equipment.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 XIV
Guidelines for (O) & (M) Procedures
25-14 (M) Maintenance procedure to deactivate and secure the inoperative System.

25-18 (M) Maintenance procedure to secure the Cockpit and/or Cabin Partition
Doors / Curtains in the full open position or to remove Doors / Curtains.

26-4 (O) Operations procedure to ensure Lavatory is locked closed and accessed
only by crewmembers.

(M) Maintenance Procedure to ensure Lavatory Waste Receptacle is empty

and Door is placarded.

27-1 (O) Procedure to provide method to check trim tab for full range of motion
and ensure there is no restriction to movement.

27-2 (O) Procedure to provide method to verify full flap travel and correct
intermediate flap settings.

27-4 (M) Maintenance procedure to deactivate the Electric Trim and ensure
27-4-3 Manual Trim is operative.

28-1 (M) Procedure to deactivated and secure affected Standby Fuel Boost Pump.

28-5 (M) Maintenance procedure to ensure there are no fuel leaks or restrictions
to fuel flow associated with the Fuel Counter / Totalizer malfunction.

28-6 (O) Operations procedure to ensure the quantity and balance of fuel on
board meets the regulatory requirements for the intended flight and fuel
balance is maintained throughout flight.

28-9 (O) Operations procedure to ensure Standby Electric Boost Pump is turned
on and verified operative.

(M) Procedure to determine there is no fuel leak, the Low Pressure Pump has
disconnected (shaft has sheared), pump failure did not introduce debris into
the fuel system, and the Fuel Pressure Low annunciator is extinguished by
use of the Standby Electric Fuel Pump with the engine operating at takeoff
power.

30-2 (O) Operations procedure to verify operation of the Anti-Ice Vanes prior to
each departure.
(M) Maintenance procedure to secure Anti-Ice Vanes in the full extended
position.
(O) Operations procedure to ensure that Surface Temperatures and Ice Vane
Extended Performance Charts are considered.
(M) Maintenance procedure to secure the Anti-Ice Vanes in the full extended
position.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO.
Beechcraft Model 200 and F-90 DATE: 08/27/2010 XV
Guidelines for (O) & (M) Procedures
30-5-1 (O) Procedure to verify each pitot mast heat is operative prior to each flight.

30-10-1-a (O) Operations procedure to ensure aircraft is not operated in visible

moisture 5 degrees Celsius or below.

(M) Maintenance procedure to manually extend and secure the Anti-Ice

Vanes in the fully extended position.

(O) Operations procedure to ensure Ice Vanes Extended performance data

is used.

30-10-1-b (O) Operations procedure to ensure that is not operated in visible moisture 5
degrees Celsius or below.

30-10- 2- (M) Maintenance procedure to ensure the Anti-Ice Vanes are secured in the
a & -b fully extended position.

(O) Procedure to ensure that Surface Temperatures and Performance Charts

with Ice Vanes Extended are considered.

30-10-2-c (M) Maintenance procedure to manually extend and secure the Anti-Ice
Vanes in the fully extended position.

31-2 (O) Operations procedure to record flight time.

31-7 (O) Establish alternate procedure to collect engine trend monitoring data.

32-1 (O) Operations procedure to prevent movement of aircraft when stopped or

parked.

32-2 (M) Maintenance procedure to deactivate Brake Deice and ensure Rudder
Boost remains operative.

32-5 (M) Maintenance procedure to verify proper hydraulic fluid level prior to first
flight of each day.

32-6 (O) Operations procedure to ensure flight crew awareness of the requirement
to manually release the Down Lock Latch.

33-1 (O) Operations procedure to identify minimum sufficient operative lighting for
the crew to perform required duties and for passengers to locate items and
move safely about the cabin during night operations.
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Guidelines for (O) & (M) Procedures
33-4 (O) Operations procedure to appropriately brief the passengers.

34-2-1 (O) Operations procedure to ensure crew awareness of specific airspeed

information.

34-8-3-a (O) Procedure to ensure current navigation charts are available and used,
status of applicable Navigation Facilities are verified, Navigation Radios are
tuned manually, and flight planning is not predicated on use FMS guidance in
the terminal area.

34-10-1&2 (O) Procedure to determine the Multi-Function Processing Unit is operative.

34-11 (M) Procedure to deactivate and secure the Radar Altimeter System.

(O) Alternate procedure for terrain clearance awareness and approach

minimums awareness with the radar altimeter inoperative.

34-12 (O) Operations procedure to verify Autopilot with Altitude Hold is operative.

34-13 (O) Operations procedure to ensure equipment configuration and flight crew
awareness of the need to manually slave Directional Gyro.

34-14 (O) Operations procedure that identifies the required sources of magnetic
heading information needed to be available and operative.

34-15 (M) Maintenance procedure to deactivate and secure the TCAS II System.

34-15-2 (O) Operations procedure to ensure TA ONLY Mode is selected by the crew
and TA visual display and audio functions are operative.

34-15-3 (O) Operations procedure to ensure RA visual display and audio functions
are operative.

34-16 (M) Maintenance procedure to deactivate and secure the TCAS I System.

34-17 (O) Procedure to ensure pilot planning and awareness of terrain clearance.
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Guidelines for (O) & (M) Procedures
34-17-1 (O) Procedure to ensure alternate means of terrain awareness with
inoperative GPWS.

34-17-1-a O) Procedure to ensure alternate means of crew awareness with inoperative

Mode(s).

34-17-1-b (O) Procedure to ensure alternate means of terrain awareness with

inoperative GPWS.

34-17-1-d (O) Procedure to ensure alternate means of crew awareness with inoperative
advisory callout(s).

34-17-1-e (O) Procedures for windshear avoidance when Windshear Warning and
Flight Guidance System is inoperative. Procedure should include a review of
windshear avoidance and windshear recovery procedures.

34-17-2 (O) Procedure to ensure alternate means of terrain awareness with

inoperative FLTA/PDA Modes.

34-22 (O) Operations procedure must identify all systems and functions affected by
the inoperative MFD specific to each installation and provide for MEL deferral
of those affected systems.

34-23 (O) Establish alternate procedures for use when Windshear Warning and
Flight Guidance System is inoperative. Procedure should include a review of
windshear avoidance and windshear recovery procedures.

34-24 (O) Establish alternate procedures for use when Windshear Detection and
Avoidance System is inoperative. Procedure should include a review of
windshear avoidance and windshear recovery procedures.

35-2 (M) Maintenance procedure to ensure a qualified crew member is stationed

inside the aircraft to monitor the Internal Oxygen Gauge during servicing.
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Guidelines for (O) & (M) Procedures
35-3 (M) Maintenance procedure to block and placard affected Seat and to block
flow of oxygen from the inoperative Mask.

37-2 (O) Operations procedure to determine Bleed Air Shutoff Valve is in the
closed position prior to each departure.

46-1 (O) Procedure to ensure all the aeronautical information required for the flight
is available in paper form or dual redundant electronic form.

46-1-1 (O) Procedure to ensure adequate battery power supply for the EFB is
available for the duration of the flight plus one hour or all the aeronautical
information required for the flight is available in paper form.

46-1-2 (M) Procedure to secure the EFB in a useable position by other means and if
unable to secure the EFB, then remove the EFB from the aircraft.

(O) Procedure to ensure all the aeronautical information required for the flight
is available in paper form or dual redundant electronic form if the EFB is
removed.

46-1-3 (O) Procedure to provide alternate source of information normally provided

through EFB data connection.

46-2-1 & 2 (O) Procedure to ensure all the aeronautical information required for the flight
is available in paper form or dual redundant electronic form.

46-2-3 & 4 (O) Procedure to provide any required information normally provided through
the CMU or Third VHF Radio.

52-2 (O) Operations procedure to inspect the Cargo Door Latching Mechanism to
ensure the Door is latched prior to each departure.

52-3 (O) Operations procedure to inspect, using adequate Light, the Cabin Door
Latching Mechanism to ensure the Door is latched prior to each departure.

52-4 (O) Operations procedure to ensure crew awareness that the Cabin Door
must be lowered manually to prevent damage to personnel or the aircraft.

73-1 (M) Procedure to ensure there are no fuel leaks associated with the Fuel
Flow Indicator malfunction.

79-1 (O) Operations procedure to monitor corresponding Oil Pressure Gauge.

U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 14 PAGE NO:
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

1. Pressurization C 1 0 (O) May be inoperative for

Controller unpressurized flight.

2. Safety Valve (Dump) C 1 0 (M)(O) May be inoperative provided:

a) Airplane remains
unpressurized, and
b) Safety Valve (Dump) is blocked
open.

3. Outflow Valve C 1 0 (M)(O) May be inoperative provided:

a) Airplane remains
unpressurized, and
b) Safety Valve (Dump) is blocked
open.

4. Cabin Altitude Warning C 1 0 May be inoperative for pressurized

(ALT WARN) flight at or below 10,000 feet MSL.

C 1 0 (O) May be inoperative for

unpressurized flight.

5. Cabin Rate of Climb C 1 0 May be inoperative for pressurized

Indicator flight provided CABIN ALTITUDE/
DIFFERENTIAL PRESSURE Indicator
is operative.

C 1 0 (O) May be inoperative for

unpressurized flight.

6. Cabin Altitude/ C 1 0 (O) May be inoperative for

Differential Pressure unpressurized flight provided Safety
Indicator Valve (Dump) is OPEN.
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

7. Bleed Air Shutoff C 2 1 (M) One may be inoperative in the

Valves (Environmental) ENVIR OFF Position for pressurized
(3 Position Switch) flight.

C 2 0 (M)(O) May be inoperative in the

ENVIR OFF position for unpressurized
flight.

8. Bleed Air Shutoff DELETED; Revision 14a,

Valves (Pneumatic See Chapter 37
Instrument Air)
(3 Position Switch)

9. Bleed Air Shutoff C 2 1 (M) One may be inoperative in the

Valves closed position for pressurized flight.
(2 Position switch)

C 2 0 (M)(O) May be inoperative in closed

position for unpressurized flight.

10. AUTOMATIC C 1 0 May be inoperative provided MANUAL

Temperature Controller Temperature Controller is operative.

11. MANUAL Temperature C 1 0 May be inoperative provided

Controller AUTOMATIC Controller is operative.

12. Electric Heat C 1 0

13. Ventilation Blower DELETED REVISION 9.

14. Air Conditioner C 1 0 (M)

15. Aft Blower C 1 0

***
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

16. L or R BL AIR FAIL

Annunciator System

1) Annunciator Fails to C 2 1 (O) One may be inoperative provided:

Illuminate a) Environmental and Instrument
Bleed Air Valves on the
inoperative side are verified
closed before each flight, and
b) Aircraft is not operative into
known or forecast icing
conditions.

NOTE: Rudder Boost will be

inoperative.

2) Annunciator Remains C 2 1 (O) One may be inoperative provided:

Illuminated a) Environmental and instrument
Bleed Air Valves on the
inoperative side are verified
closed before each flight, and
b) Aircraft is not operated into
known or forecast icing
conditions.

NOTE: Rudder Boost will be

inoperative.

17. Ground Air Cooling C 1 0

*** System

18. Bleed Air OFF C 1 0 (O) May be inoperative for

Annunciator System unpressurized flight.

19. Cabin Door Seal C 1 0 (O) May be inoperative for

System unpressurized flight.

20. Cabin Temperature C 1 0

Indicator System
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

1. Autopilot System C - 0 (M) May be inoperative provided

operations do not require its use.

NOTE: RVSM is not authorized.

2. Yaw Damper C 1 0 (M) May be inoperative provided aircraft

(200 Series except is operated at or below 17,000 ft
200HDC, 200T with Tip Pressure Altitude. |
Tanks or STC
SA3519NM & F90
except STC SA4130NM)

(200T with Tip Tanks) C 1 0 (M) May be inoperative provided aircraft

is operated at or below 7,000 ft MSL.

(200 Series with STC C 1 0 (M)

SA3519NM)

(F-90 with STC C 1 0 (M)

SA4130NM)

(200 HDC Only) C 1 0 (M) May be inoperative provided aircraft |

is operated at or below 25,000 ft |
Pressure Altitude. |

3. Autopilot Control C 2 1 One may be inoperative on the non-

Wheel Disconnect flying pilot side provided:
Switches a) Autopilot is not used below
(AP/YD/TRIM DISC) 1,500 feet AGL, and
b) Approach minimums do not
require the use of the autopilot

(Except Garmin B - 0 May be inoperative provided: |

GFC-700 AFCS a) Autopilot is not used, and |
equipped) b) Second level switch trim
interrupt function remains
operative.
(Continued) |
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AIRCRAFT: REVISION NO: 14b PAGE NO:
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

3. Autopilot Control |
Wheel Disconnect |
Switches |
(Continued) |

(Except Garmin B - 0 (M) May be inoperative provided: |

GFC-700 AFCS a) Autopilot is considered |
equipped) inoperative,
b) Electric Elevator Trim is
considered inoperative, and
c) Yaw Damper is considered
inoperative.

4. Autopilot Go-Around C 1 0 (O) May be inoperative provided:

Switch a) Approach minimums do not
require its use, and
b) Alternate procedures are
established and used to
disconnect Autopilot and
establish initial pitch and wings
level attitude.

5. Autopilot Mode C 1 0 (O) May be inoperative provided the

Selector/Annunciator affected Mode(s) is/are selected
(Except Collins Proline momentarily prior to departure to verify
21 equipped) that proper Mode Annunciation is
displayed on the pilot’s EFIS Display or
Remote Annunciator Panel.

6. Flight Director System C 1 0 May be inoperative provided approach |

procedures do not require its use. |

NOTE: Any operative Mode may be |

used. |

a) Flight Director Mode C 1 0 (O) May be inoperative provided the |

Selector Panel affected Mode(s) is/are selected
Annunciator Lamps momentarily prior to departure to verify
(Except Collins Proline that proper Mode Annunciator is
21 equipped) displayed on the Pilot’s EFIS Display or
Remote Annunciator Panel.
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 14b PAGE NO:
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

7. Autopilot/Flight C 1 0 (O) May be inoperative provided the

Guidance Panel Lamps affected Mode(s) is/are selected
(Except Collins Proline momentarily prior to departure to verify
21 equipped) that proper Mode Annunciator is
displayed on pilot’s EFIS Display or
Remote Annunciator Panel.
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 23-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

1. Communications D - - Any in excess of those required by FAR

System (VHF, UHF) may be inoperative provided it is not
powered by Emergency Power Source
and not required for Emergency
Procedures.

2. Passenger Address
System (PA)

1) Passenger C 1 0 (O) May be inoperative provided

Configuration alternate normal and emergency
procedures and/or operating
restrictions are established and used..

2) Cargo Configuration D 1 0 May be inoperative provided

procedures do not require its use.

3. Cockpit Speakers C 2 0 (O) May be inoperative provided:

System a) Two operative Headsets are
(Including Audio Amp.) available to the flight crew, and
b) Aural warnings are available.

4. Audio Amplifiers DELETED Rev.14, Combine with

Cockpit Speakers.

5. Static Discharge Wicks C - - One Wick may be missing or broken

from:
1) Each Wing (includes Aileron),
2) Each side of Horizontal
Stabilizer, and
3) Vertical Stabilizer

NOTE: A Maximum of three (3) Static

Wicks may be broken or
missing.
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

6. Boom Microphones
(includes headset mic)

1) With FDR and Cockpit A - 0 May be inoperative provided:

Voice Recorder a) Flight Data Recorder (FDR)
Equipped To Record operates normally, and
Boom Microphone b) Repairs are made within three
flight days.

2) With Only Cockpit A - 0 May be inoperative provided repairs

Voice Recorder are made within three flight days.
Equipped To Record
Boom Microphone

3) Without Cockpit Voice D - 0 Any in excess of those required by FAR

*** Recorder Equipped To may be inoperative.
Record Boom
Microphone
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

7. Cockpit Voice
Recorder (CVR)

1) With Flight Data A 1 0 May be inoperative provided:

Recorder (FDR) a) Flight Data Recorder (FDR)
Installed operates normally, and
b) Repairs are made within three
flight days.

2) Without Flight Data A 1 0 May be inoperative provided repairs

Recorder (FDR) are made within three flight days.
Installed

3) For Operators Other A 1 0 May be inoperative provided repairs

Than Air Carriers and are made in accordance with
Commercial Operators applicable FARs.

8. Passenger Call System C 1 0

***

9. Voice Activated D 1 0
*** Interphone System
(cockpit to cabin)
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

10. High Frequency (HF) D - - Any in excess of those required by

Communication FAR may be inoperative.
System

C - 1 (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 the intended route of flight,
and
d) If INMARSAT Codes are not
available while using SATCOM
Voice prior coordination with
the appropriate ATS facility is
required.

NOTE: SATCOM is to be used only as

a backup to normal HF
communications unless
otherwise authorized by the
appropriate ATS facilities.

11. Recorded Passenger D 1 0 (O) May be inoperative provided

*** Briefing System passengers are appropriately briefed
prior to each departure.

12. Flight Phone System D 1 0

***

13. Ground D 1 0
*** Communications
Power System
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 23-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

14. Push-to-Talk Switches

1) Aircraft Equipped With C 2 1 One may be inoperative provided Hand

Separate Hand Held Microphone on affected side is
Microphone Plug-In operative.
(Second-in-command
Required)

2) Aircraft Equipped With C 2 1 Right side may be inoperative.

Separate Hand
Microphone Plug-In
(Second-In-Command
Not Required)

3) Aircraft Without C 2 1 Right side may be inoperative.

Separate Hand
Microphone Plug-In.
(Second-In-Command
Not Required)

15. Hand Held Microphone C 2 1 Right side may be inoperative.

C 2 1 One may be inoperative provided

Boom Microphone and Push-to-Talk
Switch are operative on side with
inoperative Microphone.
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

16. Selective Call Systems C - 0 (O) May be inoperative provided

(SELCAL) alternate procedures are established
and used.

D - 0 May be inoperative provided

procedures do not require its use.

1) Channels C - 0 (O) May be inoperative provided

alternate procedures are established
and use.

D - 0 May be inoperative provided

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 24-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER

1. DC Generator Caution B 2 1 One may be inoperative provided

Lights corresponding Load Meter is
monitored.

2. Inverters B 2 1 One may be inoperative for day VFR.

(Except SN BB-1769,
BB-1834, BB-1843,
BL-148 and After, BY-1
and after, and BZ-1
and after)

3. Inverters Warning Light B 2 1 One may be inoperative provided both

(Except SN BB-1769, Inverters are operative.
BB-1834, BB-1843,
BL-148 and After, BY-1
and after, and BZ-1
and after)

4. DC Load Meter DELETED, Revision 14

5. AC Volt/Frequency B 1 0 May be inoperative provided Inverter

Meter Warning Light is operative.
(Except SN BB-1769,
BB-1834, BB-1843,
BL-148 and After, BY-1
and after, and BZ-1
and after)

6. Battery Temperature C 1 0 May be inoperative provided the

*** Indicating System Standard Battery Charge Annunciator
System is operative.
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 14 PAGE NO:
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER

7. Cabin AC Power C - 0 (M)

*** System

8. EFIS Standby Power B 1 0 (M) May be inoperative provided:

a) Airplane is operated in day
VMC only, and
b) Standby Battery is
disconnected and removed.

9. External Power System C 1 0 (M)

10. External Power C 1 0 (O)

Annunciator

11. L or R GEN BUS TIE B 2 1 One may be inoperative for day VMC
Relay operations provided both DC GEN
(Model F90 Only) Annunciators/Caution Lights are
operative.

12. L or GEN BUS TIE B 2 0 (O) May be inoperative provided:

Annunciator a) Generator Bus Tie Relay is
(Model F90 Only) verified closed prior to each
departure, and
b) Both DC GEN Annunciators/
Caution Lights are operative.
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 12 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 11/03/2003 25-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

1. Crew Seats

1) Arm Rests C - 0 (M) May be inoperative provided the

affected Arm Rest(s) is/are stowed and
secured in the full up or full down
position and is/are acceptable to the
flight crew.

2) Lumbar Support C - 0 May be inoperative provided the Seat

configuration is acceptable to the flight
crew.

3) Shoulder Harness B 2 1 Right side may be inoperative provided

Seat is not occupied.

4) Seat Adjustment A - 0 (M) May be inoperative provided:

a) Seat(s) is/are locked in a
position that permits normal
pilot visibility,
b) Full Flight Control movement is
available,
c) Position of the affected Seat(s)
is/are acceptable to the flight
crew, and
d) Repairs are made within one
flight day.
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 25-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

2. Passenger Seat(s) D - - May be inoperative provided:

a) Seat does not block an
Emergency Exit,
b) Seat does not restrict any
passenger from access to the
main aircraft aisle, and
c) Affected seat(s) are blocked
and placarded “DO NOT
OCCUPY”.

NOTE 1: A seat with an inoperative

seat belt is considered
inoperative.

NOTE 2: Affected seat(s) may include

the seat(s) behind.

1) Recline Mechanism D - - (M) May be inoperative and seat

occupied provided seat is secured in
the full upright position.

D - - May be inoperative and seat occupied

provided seat is immovable in the full
upright position

2) Armrest D - - 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 the
main aircraft aisle, and
c) For an Armrest with a recline
mechanism, seat is secure in
the full upright position.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 25-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

3. Floatation Equipment D - - Any in excess of those required by

*** FAR may be inoperative or missing.

4. Emergency Medical
Equipment

1) Automatic External D - - May be incomplete, missing, or

*** Defibrillator (AED) inoperative.
and/or Associated
Equipment

2) Emergency Medical Kit D - - May be incomplete, missing or

*** (EMK) and/or inoperative.
Associated Equipment

3) First Aid Kit (FAK) D - - Any in excess of those required by

and/or Associated FAR may be incomplete, missing or
Equipment inoperative.

5. Emergency Locator
Transmitter (ELT)

1) Survival Type ELTs D - - Any in excess of those required by

FAR may be inoperative or missing.

2) Fixed ELTs A - 0 May be inoperative or missing provided

repairs are made within 90 days.

D - - Any in excess of those required by

FAR may be inoperative or missing.

a) Remote Switch D 1 0 (M) May be inoperative provided:

*** a) Remote switch is disconnected
from the ELT, and
b) ELT switch is placed in the
ARM position.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 25-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

6. Non-Essential - 0 May be inoperative, damaged, or

Equipment & missing provided that the item(s) is
Furnishings (NEF) deferred in accordance with the
operator’s NEF deferral program. The
NEF program, procedures, and
processes are outlined in the operators
(insert name) Manual. (M) and (O)
procedures, if required, must be
available to the flight crew and included
in the operator’s appropriate document.

NOTE: Exterior Lavatory Door Ash

Trays are not considered NEF
Items.

7. Electric Toilet C 1 0
***

8. “Fasten Seat Belt C - - One or more Signs or Placards may be

While Seated” Sign or illegible or missing provided a legible
Placard Sign or Placard is visible from each
occupied Passenger Seat.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 25-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

9. Exterior Lavatory Door

*** Ashtrays

1) Airplanes With More A - - One may be missing provided it is

Than One Exterior replaced within 10 calendar days.
Lavatory Door Ashtray
Installed

2) Airplanes With Only A 1 0 May be missing provided it is replaced

One Exterior Lavatory within 3 calendar days.
Door Ashtray Installed

10. Waste Receptacle C - - (M)(O) May be inoperative provided:

*** Access Doors/Covers a) The container is empty and the
access is secured to prevent
waste introduction into the
compartment, and
b) Procedures are established to
ensure that sufficient Waste
Receptacles are available to
accommodate all waste that
may be generated on a flight.

11. Cargo Restraint C - - (M) May be inoperative or missing

*** Systems provided 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.

C - - May be inoperative or missing provided

Cargo Compartment remains empty.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 25-6
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

12. Cabin Storage C - - (M) May be inoperative provided:

Compartments / a) Procedures are established to
Closets secure compartment closed,
b) Associated compartment is
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

C - - (M)(O) May be inoperative provided:

a) Affected door is removed,
b) Associated compartment is not
used for storage of any items,
except those permanently
affixed,
c) Associated compartment is
placarded “DO NOT USE”,
d) Passengers are briefed that
associated compartment is not
used.

NOTE: Any permanently affixed

Emergency Equipment located in
the associated storage
compartment is available for use.

1) Storage Compartments D - - (M) May be inoperative in the unlocked

Key Locks position provided door latch remains
operative.

13. EMS Equipment C - 0 (M)(O) May be inoperative provided the

*** inoperative system/component is
deactivated and secured.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 25-7
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

14. Smartstart Security C 1 0 (M)

*** System

15. Pyrotechnic Signal D - - Any in excess of those required by

*** FAR may be inoperative or missing.

16. Protective Breathing DELETED REV.14, See Chapter 35.

Device

17. Sound Management D - 0

*** System (Active Noise
Canceling System)

18. Cockpit and Cabin D - 0 May be inoperative provided

*** Partition door/curtain is secure in the full stowed
Doors/Curtains open position.

D - 0 (M) Curtains may be removed or

secured open by an alternate means.

19. Flashlight/ Flashlight D - - Any in excess of those required by

Holder FAR may be inoperative or missing.

20. Cockpit Overhead D - 0

Crew Assist Straps

21. Cockpit Sun Visors C 2 0 May be inoperative or missing provided

there are no visual restrictions to the
flight crew.

22. External Airspeed DELETED Rev.14, See Chapter 34.

Indicator Bug(s)

23. Emergency Vision C 2 0

*** Assurance System
(STC SA 1050WI)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 12 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 11/03/2003 26-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION

1. Portable Fire D - - Any in excess of those required by FAR

Extinguisher may be inoperative or missing
provided:
a) The inoperative Fire
Extinguisher is tagged
inoperative, removed from the
installed location and placed out
of sight so it cannot be mistaken
for a functional unit, and
b) Required distribution is
maintained.

2. Engine Fire C 2 0
*** Extinguisher Systems

1) “Push To Extinguish” A - - May be broken, missing or lacking

Guard Safety Wire provided:
a) Broken Guard shall not interfere
with the proper indication or
activation of System, and
b) Repairs are made within one
flight day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 26-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION

3. Lavatory Fire DELETED, Revision 14

*** Extinguisher System

4. Lavatory Smoke C - - (M)(O) Lavatory Smoke Detection

*** Detection System System may be inoperative provided:
a) Lavatory Waste Receptacle is
empty,
b) 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.

5. Cargo Compartment C - 0 May be inoperative provided Cargo

*** Fire Detection Compartment remains EMPTY.
Suppression Systems

NOTE: Does not preclude the carriage

of empty cargo containers,
pallets, ballast, etc.

6. Fire Extinguisher “Push DELETED REVISION 12. MOVED TO

To Extinguish” Guard ATA 26-2-1.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 27-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS

1. Trim Tab Position C 3 0 (O) May be inoperative provided:

Indicators (Rudder, a) Tab is visually checked for full
Aileron, and Elevator) range of operation,
b) Tab operation is not restricted,
and
c) Tab is positioned to neutral
prior to each departure and
neutral is verified by visual
inspection

2. Flap Position Indicator C 1 0 (O) May be inoperative provided:

a) Flaps are visually checked for
full travel and Flap operation is
not restricted, and
b) Flaps are visually checked for
proper setting prior to each
departure.

3. Rudder Boost C 1 0 May be inoperative provided aircraft is

(Except 200T) not modified with STC SA2307CE.

4. Electric Elevator Trim C 1 0 (M) May be inoperative provided:

System a) Electric Pitch Trim is
deactivated, and
b) Autopilot is not used.

NOTE: RVSM is not authorized. |

1) Trim Switches C - 0 NOTE: Any operative Trim Switch may

be used.

2) PITCH TRIM OFF C 1 0

Annunciation System

3) PITCH TRIM ON-OFF C 1 0 (M) May be inoperative provided:

Switch a) Electric Pitch Trim is
deactivated, and
b) Autopilot is not used.

5. Flap System DELETED REVISION 12

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 28-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

1. Standby Fuel Boost C 2 1 (M) One may be inoperative provided:

Pumps a) Emergency Engine Fuels are
(Except 200 HDC) not used, |
b) Both Engine Driven Low
Pressure Fuel Boost Pumps are
operative, and
c) Aircraft is not operated more
than 1 hour, at one-engine-
inoperative cruise, from a
suitable airport.

NOTE: See AFM Emergency Engine

Fuels Limitations.

(200 Series Only C 2 1 (M) One may be inoperative provided: |

Except 200HDC) a) Aircraft remains at or below |
20,000 feet Pressure Altitude,
b) Both Engine Driven Low
Pressure Fuel Boost Pumps are
operative, and
c) Aircraft is not operated more
than 1 hour, at one-engine-
inoperative cruise, from a
suitable airport.

(F90 Only) C 2 1 (M) One may be inoperative provided:

a) Aircraft remains at or below
17,000 feet Pressure Altitude,
b) Both Engine Driven Low
Pressure Fuel Boost Pumps are
operative, and
c) Aircraft is not operated more
than 1 hour, at one-engine-
inoperative cruise, from a
suitable airport.

2. Motive Flow Valves DELETED, Revision 14, See Auxiliary

Fuel Transfer System

3. Jet Transfer Pumps DELETED, Revision 14, See Auxiliary

Fuel Transfer System
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 28-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

4. Crossfeed Light C 1 0 May be inoperative provided proper

operation of Crossfeed System is
checked prior to departure.

5. Fuel Counter/ Fuel C 1 0 (M)

*** Totalizer

6. Fuel Quantity C 2 1 (O) One may be inoperative provided:

Indicators a) A reliable means is established
to determine that fuel quantity
on board meets regulatory
requirements for flight,
b) Both Fuel Flow Indicators are
operative, and
c) Procedures are established to
ensure fuel balance.

NOTE: Tip Tank Fuel Gauge must be

operative if installed.

7. Auxiliary Fuel Transfer

Systems

1) Automatic System C 2 0 May be inoperative provided Auxiliary

Tanks do not contain fuel.

2) Override System C 2 0 May be inoperative provided Auxiliary

Tanks do not contain fuel.

8. Fuel Flow Indicators DELETED Revision 14, See Chapter 73

9. Engine Driven Low B 2 1 (M)(O) One may be inoperative

Pressure Fuel Boost provided:
Pumps a) Both Standby Electric Boost
Pumps are operative,
b) Associated Standby Electric
Boost Pump is turned ON, and
c) Aviation gasoline is not used.

10. Fuel Management DELETED, Revision 14

Function
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 30-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION

1. Surface Deice System C 1 0 May be inoperative provided aircraft is

(Wing and Horizontal not operated in known or forecast icing
Stabilizer) conditions.

2. Green L & R Ice Vane C 4 2 (O) One may be inoperative on one or

Ext and Amber L & R both sides provided the Inertial Ice |
ICE VANE (or L & R Vanes are verified operative prior to |
ENG ICE FAIL) each departure. |
Annunciators
(200 Series Only)

C 4 0 (M)(O) Both may be inoperative on one

or both sides provided:
a) Inertial Ice Vanes are secured
in the extended position,
b) Where applicable, Performance
Data with Ice Vanes Extended
is used, and
c) Ambient surface temperature is
15 degrees Celsius or below for
takeoff and flight operations.

L & R ENG ANTI-ICE C 2 0 (M) May be inoperative on one or both

Annunciators sides provided affected Inertial Ice
(F90 Only) Vanes are secured in the extended
positions.

3. Windshield Heat C 2 0 May be inoperative provided aircraft Is

not operated in known or forecast icing
conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 30-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION

4. Windshield Wipers C 2 0 May be inoperative provided flight is

not conducted in precipitation within 5
nautical miles of the airport of takeoff
or intended landing.

5. Pitot Heaters B 2 1 Right side may be inoperative |

provided: |
a) SIC is not required, and |
b) Aircraft is not operated in |
known or forecast icing |
conditions. |
NOTE: RVSM is not authorized. |

C 2 0 May be inoperative provided: |

a) Aircraft is operated VFR only, |
and |
b) Aircraft is not operated in |
known or forecast icing |
conditions. |

1) Pitot Heat Annunciator C 2 0 (O) May be inoperative provided:

*** a) Both pitot heaters are
operative, and
b) Aircraft is not operated in
known or forecast icing
conditions.

6. Propeller Deice C 1 0 May be inoperative provided Manual

Systems (Automatic) Propeller Deice System is operative.

C 1 0 May be inoperative provided aircraft is

not operated in known or forecast icing
conditions.

7. Propeller Deice C 1 0 May be inoperative provided Automatic

System (Manual) Propeller Deice System is operative.

C 1 0 May be inoperative provided aircraft is

not operated in known or forecast icing
conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 30-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION

8. Heated Fuel Vents C 2 0 May be inoperative provided aircraft is

not operated in known or forecast icing
conditions.

9. Stall Warning Heater C 1 0 May be inoperative provided aircraft is

not operated in known or forecast icing
conditions.
10. Engine Inertial Ice
Vanes

1) Engine Inertial Ice

Vane Motors

a) Dual Motors System C 4 2 (O) One Actuator Motor on each Intake

(200 series & F90) System may be inoperative provided
aircraft is not operated in visible
moisture at 5 degrees Celsius or
below.

(200 series only) C 4 0 (M)(O) Both Actuator Motors on each

Intake System may be inoperative on
one or both sides provided:
a) Inertial Ice Vanes are secured
in the extended position,
b) Performance Data with Ice
Vanes Extended is used, and
c) Ambient surface temperature is
15 degrees Celsius or below for
takeoff and flight operations.

(F90 LA-202, LA-205 C 4 0 (M) Both Actuator Motors on each

and after) Intake System may be inoperative on
one or both sides provided Inertial Ice
Vanes are secured in the extended
position.

b) Single Motor System C 2 0 (O) The Actuator Motor on each Intake

with Manual Backup System may be inoperative provided
the aircraft is not operated in visible
moisture at 5 degree Celsius or below.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 30-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION

10. Engine Inertial Ice

Vanes (Continued)

2) Engine Inertial Ice

Vane Actuators

a) Dual Motor System C 2 0 (M)(O) The Actuator on the Intake

(200 series only) System may be inoperative provided:
a) Inertial Ice Vanes are secured
in the extended position,
b) Performance Data with Ice
Vanes Extended is used, and
c) Ambient surface temperature is
15 degrees Celsius or below for
takeoff and flight operations.

(F90 LA-202, LA-205 C 2 0 (M) The Actuator on the Intake System

and after) may be inoperative provided Inertial Ice
Vanes are secured in the extended
position.

b) Single Motor System C 2 0 (M)(O) The Manual Extend Backup

with Manual Extended Actuator on the Intake System may be
Backup inoperative provided:
a) Inertial Ice Vanes are secured
in the extended position,
b) Performance Data with Ice
Vanes Extended is used, and
c) Ambient surface temperature is
15 degrees Celsius or below for
takeoff and flight operations.

c) Manual Extend C 2 0 (M) The Manual Extend Actuator on

System/No Motors each Intake System may be
(F90 LA-2 thru LA-204 inoperative provided the Inertial Ice
except LA-202) Vanes are secured in the extended
position.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 30-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION

11. Propeller Deice C 1 0 May be inoperative provided aircraft is

Ammeter not operated in known or forecast icing
conditions.

12. Electric Engine Air Inlet C 2 1 May be inoperative provided the aircraft
Lip Boot Heat is not operated in areas of visible
moisture at temperatures less than 5
degrees Centigrade.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 31-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
31 INDICATING/
RECORDING
SYSTEMS

1. Clock With Sweep C 1 0 May be inoperative for VFR.

Second Hand Or
Electric Digital Clock

2. Flight Hour Recorder C 1 0 (O)

3. Flight Data Recorder C - - Any in excess of those required by

(FDR) System FAR may be inoperative.

A - 0 May be inoperative provided:

a) Cockpit Voice Recorder (CVR)
operates normally,
b) Airplane is not dispatched from
a designated airport as listed in
the operator’s MEL unless:
1. The FDR failure occurs after
pushback but prior to
takeoff or
2. The FDR repair was
attempted but was not
successful.
c) In those cases where repair is
attempted but not successful,
the aircraft may be dispatched
on a flight or series of flights
until the next designated airport
where repair must be
accomplished prior to dispatch,
and
d) Repairs are made within three
flight days.

(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 31-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
31 INDICATING/
RECORDING
SYSTEMS

3. Flight Data Recorder

(FDR) System
(Continued)

1) FDR Recording A - - May be inoperative provided:

Parameters Required a) Cockpit Voice Recorder (CVR)
by FAR operates normally, and
b) Repairs are made within 20
calendar days.

2) FDR Recording A - - May be inoperative provided repairs

Parameters Not are made prior to completion of the
Required by FAR next heavy maintenance check.

3) Operators Other Than C - 1 Any in excess of those required by

Holders of Air Carrier FAR may be inoperative.
or Commercial
Operator Certificates

A - 0 May be inoperative provided repairs

are made in accordance with
applicable FARs.

4. Master Caution B 2 1 One may be inoperative.

Annunciators

5. Master Warning A 2 1 One may be inoperative provided:

Annunciators a) Left side is operational for
single pilot operations, and
b) Repairs are made within one
flight day.

6. Unassigned (---) D - 0
Annunciators

7. Engine Trend D 1 0 (O) May be inoperative provided

*** Monitoring System alternate procedures are established
and used for engine trend monitoring.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 32-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR

1. Parking Brake C 1 0 (O)

2. Brake Deice System C 1 0 (M) May be inoperative provided

Rudder Boost is not affected.

NOTE: See AFM for Limitations.

3. Landing Gear Position A 6 3 One Lamp in each Indicator may be

Indicator Lamps inoperative provided:
a) One Lamp in each Indicator is
operative and provides
sufficient illumination for
positive Down and Locked
Indication, and
b) Repairs are made within one
flight day.

4. Landing Gear Handle C 2 1 One Bulb may be inoperative provided

Lights all Gear Positive Lights are operative.

5. Hydraulic Fluid Low C 1 0 (M) May be inoperative provided

Annunciator hydraulic fluid level is verified full each
flight day.

6. Landing Gear Handle C 1 0 (O) May be inoperative provided:

Solenoid a) Down Lock Latch is operative,
and
b) Down Lock Release Button is
operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 33-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

1. Cabin Lights Systems C - - (O) Individual lights may be inoperative

provided:
a) Cabin Emergency Lighting is
operative,
b) Sufficient Lighting is available
for crew to perform required
duties and
c) Sufficient Lighting is operative
for passenger carrying
operations at night.

2. Cockpit/ Flight Deck/ C - - Individual Lights may be inoperative

Flight Compartment provided remaining Lights are:
and Instrument Lighting a) Sufficient to clearly illuminate all
System required instruments, controls,
and other devices for which it is
provided,
b) Positioned so that direct rays
are shielded from flight
crewmembers eyes, and
c) Lighting configuration and
intensity is acceptable to the
flight crew.

3. Landing Lights C 2 0 May be inoperative for day operations.

C 2 1 One may be inoperative for night

operations provided Taxi Light is
operative.

4. Passenger Notice C 1 0 (O) May be inoperative provided

System (Fasten Seat appropriate verbal briefings are given
Belt-No Smoking) to the passengers.

5. Navigation Light C 1 0 May be inoperative for day operations.

System

6. Anti-Collision Beacon B 1 0 May be inoperative for day operations.

Light System

7. Strobe Light System C 1 0

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 33-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

8. Taxi Light C 1 0 May be inoperative for day operations.

C 1 0 May be inoperative for night operations

provided both Landing Lights are
operative

9. Wing Ice Lights C - 0 May be inoperative for day operations.

C - 0 May be inoperative provided:

a) Aircraft is not operated in
known or forecast icing
conditions at night, and
b) Ground deicing procedures do
not require the use of Wing Ice
Lights.

*** C 2 1 One may be inoperative provided:

a) The left light is operative for
single pilot operations, and
b) Ground deicing procedures do
not require the use of Wing Ice
Lights.

10. Recognition Lights C 2 0

***

11. Logo Light System C 1 0

***

12. Master Caution DELETED, Rev.14, Moved Chapter 31

13. Baggage Compartment C - 0

Lights

14. Pulselight System C 1 0

***
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

15. Master Warning DELETED, Rev.14, Moved Chapter 31

Annunciator

16. Unassigned (---) DELETED, Rev.14, Moved Chapter 31

Annunciators

17. Cabin Boarding C 1 0 Any operable Light may be used.

Lighting System

18. Emergency Instrument C 1 0 May be inoperative for day VFR

Lights operations.
U.S. DEPARTMENT OF TRANSPORTATION
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ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

1. Altimeters, Adjustable B 2 1 May be inoperative on right side

For Barometric provided:
Pressure a) Second In Command is not
(Mechanical Altimeters required, and
Only) b) Aircraft is not equipped with
Electronic Air Data System |
(ADC), Air Data Display Unit(s) |
or Servoed Electric Altimeter(s).

NOTE: RVSM is not authorized.

2. Airspeed Indicators B 2 1 May be inoperative on right side

(Mechanical Airspeed provided:
Indicators Only) a) Second In Command is not
required, and
b) Aircraft is not equipped with
Electronic Air Data System |
(ADC), or Servoed Electric |
Airspeed Indicator(s).

1) External Airspeed C - 0 (O) May be inoperative, missing, or

*** Indicator Bug(s) broken provided alternate procedures
are established and used for specific
airspeed awareness.

3. Gyroscopic Pitch And B 2 1 May be inoperative on right side

Bank Indicator provided:
Systems a) Second in command is not
(Mechanical Attitude required, and
Indicators Only) b) Aircraft is not equipped with
EFIS or Servoed Electric
Gyroscopic Pitch and Bank
Indicator.
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

4. Gyroscopic Rate of B 2 1 May be inoperative on right side

Turn/Slip Skid Indictors provided Second in Command is not |
(Mechanical Turn required |
Indicators Only)

B 2 1 May be inoperative provided aircraft is |

operated Day VFR. |
|
NOTE: Yaw Damper may be
inoperative on some aircraft.

5. Gyroscopic Directional B 2 1 May be inoperative on right side

Indictor System provided:
(Mechanical Heading a) Second in command is not
Indicators Only) required, and
b) Aircraft is not equipped with
EFIS.

6. Vertical Speed B 2 1 May be inoperative on right side.

Indicators (VSI)
(Mechanical VSI Only)

B 2 1 May be inoperative on left side

provided the aircraft is operated day
VFR.
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

7. ATC Transponders and B - 0 May be inoperative provided:

Automatic Altitude a) Operations do not require its
Reporting Systems use, and
b) Prior to flight, approval is
obtained from ATC facilities
having jurisdiction over the
planned route of flight.

NOTE: RVSM is not authorized.

D - 1 Any in excess of those required by

FAR may be inoperative.

1) Elementary And A - 0 May be inoperative provided:

*** Enhanced Downlink a) Operations do not require its
Aircraft Reportable use, and
Parameters Not b) Repairs are made prior to
Required By FAR completion of next heavy
maintenance visit.

2) ADS-B Squitter A - 0 May be inoperative provided:

*** Transmissions a) Operations do not require its
use, and
b) Repairs are made prior to
completion of next heavy
maintenance visit.

3) Control Wheel C 2 0 May be inoperative provided

Transponder Ident Transponder Ident Switch is operative.
Switch
U.S. DEPARTMENT OF TRANSPORTATION
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ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

8. Navigation Equipment |

1) VOR/ILS Systems C - - May be inoperative provided: |

a) Not required by FAR, and |
b) Operations do not require its |
use. |

TACAN Systems D - 0 May be inoperative provided |

operations do not require its use. |

a) Glide Slope C - - May be inoperative provided: |

a) Not required by FAR, and |
b) Operations do not require its |
use. |

b) Marker Beacon System C - 0 May be inoperative provided: |

a) Not required by FAR, and |
b) Operations do not require its |
use. |

2) Distance Measuring C - 0 May be inoperative provided a suitable |

Equipment (DME) operative RNAV system is available for |
Systems DME substitution. |

C - 0 May be inoperative provided |

operations do not require its use. |
D 2 1 |

3) Area Navigation C - - May be inoperative provided: |

(RNAV) a) Not required by FAR, and |
(Multi-Sensor, LORAN, b) Operations do not require its |
and/or GPS) use. |

D - 1 Any in excess of those required by |

FAR or operations may be inoperative. |

NOTE: RNAV Systems identified as |

FMS must only defer FMS |
functions limited to navigation |
and not affecting operation of |
other aircraft systems. |
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

8. Navigation Equipment |
3) Area Navigation |
(Continued) |
a) Navigation Databases C - - (O) May be out of currency provided: |
a) Current aeronautical charts are
used to verify navigation fixes
prior to each departure,
b) Procedures are established and
used to verify status and
suitability of navigation facilities
used to define route of flight,
c) Approach navigation radios are
manually tuned and identified,and
d) RNAV Departures, RNAV |
Arrivals, Instrument Approaches |
and published RNAV Routes |
based on RNAV guidance are |
not used. |

4) Automatic Direction C - - May be inoperative provided |

Finder (ADF) operations do not require its use. |

5) Radio Magnetic C - 0 May be inoperative provided: |

Indicator (RMI) a) Magnetic Compass is operative, |
b) Any navigation source not |
displayed on another indicator is |
considered inoperative. |

6) Flight Management NOTE: Systems identified as FMS that |

System (Aircraft provide only navigation |
Integrated Systems) functions are deferred with Area |
Navigation. |
C - 1 May be inoperative provided operations |
do not require its use. |

A - 0 May be inoperative provided: |

a) Operations do not require its |
use, |
b) Affected systems are identified |
and considered inoperative, and |
c) Repairs are made within two |
flight cycles. |
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

9. Weather Radar/ C 1 0 As required by FAR.

Thunderstorm
Detection Equipment

1) Radar Antenna C 1 0 May be inoperative provided: |

Stabilization a) Antenna sweep is parallel with |
lateral axis, and |
b) Antenna tilt control is operative. |

10. Electronic Flight

Instrument System
(EFIS) Multifunction
Display Unit (MFD)
(Collins EFIS-84 &
EFIS-85 equipped Only)

1) 3 Tube System C 1 0 (O) May be inoperative provided the

Multi-Function Processing Unit (MPU)
is operative.

2) 5 Tube System C 1 0 (O) May be inoperative provided Multi-

Function Processing Unit (MPU) is
operative.

11. Radar Altimeter C - 0 (M)(O) May be inoperative provided: |

a) Approach procedures do not |
require its use, and
b) Alternate procedures are
established and used.

NOTE: TAWS, GPWS and/or TCAS |

may be inoperative |
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIAGTION

12. Altitude Alerting A - 0 (O) May be inoperative provided: |

System a) Autopilot with Altitude Hold is
operative,
b) Enroute operations do not
require its use, and
c) Repairs are made within three
flight days.

C - 0 May be inoperative provided it is not

required by FAR.

NOTE: RVSM is not authorized

13. Gyro-magnetic C 2 1 (O) One Slaved Mode may be |

Compass System inoperative provided:
a) DG Mode is operative, and
b) Non-Stabilized Magnetic
Compass is operative.

1) Compass System #1 C 1 0 May be inoperative provided:

a) A Compass Switching System
is installed and operative,
b) Left side Heading Indicator is
operative, and
c) Magnetic heading information is
available and provided to the #1
Directional Indicator.

2) Compass System #2 C 1 0 May be inoperative provided Second-

In-Command is not required.

C 1 0 May be inoperative provided:

a) A Compass Switching System
is installed and operative,
b) Right side Heading Indicator is
operative, and
c) Magnetic heading information is
available and provided to the #2
Heading Indicator.
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

14. Non-Stabilized B 1 0 (O) May be inoperative provided any |

Magnetic Compass combination of three Gyro or
IRU/AHRS stabilized compass systems
are operative.

B 1 0 (O) May be inoperative provided:

a) Any combination of two Gyro or
IRU/AHRS Stabilized Compass
Systems are operative, and
b) Aircraft is operated with dual
independent navigation
capability and under Positive
Radar Control by ATC on the
enroute portion of the flight.

B 1 0 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.

15. Traffic Alert Collision B - 0 (M) May be inoperative provided: |

*** Avoidance System a) System is deactivated and
(TCAS II) secured, and
b) Enroute or approach
procedures do not require its
use.

C - 0 (M) May be inoperative provided:

a) System is not required by FAR,
b) System is deactivated and
secured, and
c) Enroute or approach
procedures do not require its
use.

(continued)
U.S. DEPARTMENT OF TRANSPORTATION
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FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 34-9
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

15. Traffic Alert Collision |

*** Avoidance System
(TCAS II) (Cont’d)

1) Combined Traffic Alert C 2 1 One may be inoperative on the non-

(TA) and Resolution flying pilot side provided:
Advisory (RA) Dual a) TA and RA visual display is
Display operative on flying pilot side,
and
b) TA and RA audio function is
operative on flying pilot side.

2) Resolution Advisory C 2 1 May be inoperative on non-flying pilot

(RA) Display System(s) side.

C - 0 (O) May be inoperative provided:

a) Traffic Alert (TA) visual display
and audio functions are
operative,
b) TA only mode is selected by the
crew, and
c) Enroute or approach
procedures do not require its
use.

3) Traffic Alert Display C - 0 (O) May be inoperative provided:

System(s) a) RA visual display and audio
functions are operative, and
b) Enroute or approach
procedures do not require its
use.

4) Audio Functions B 1 0 May be inoperative provided enroute or

approach procedures do not require
use of TCAS.

5) Airspace Selection C - 0
*** Function
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

16. Traffic Alert Collision B - 0 (M) May be inoperative provided: |

*** Avoidance System a) System is deactivated and
(TCAS I) secured, and
b) Enroute or approach
procedures do not require its
use.

C - 0 (M) May be inoperative provided:

a) System is not required by FAR,
b) System is deactivated and
secured, and
c) Enroute or approach
procedures do not require its
use.
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

17. Terrain Awareness A - 0 (O) May be inoperative provided: |

Warning System a) Alternate procedures are
(TAWS)/Ground established and used.
Proximity Warning b) Repairs are made within two (2)
System (GPWS) flight days.
(Class A or B
Required)

(Class C TAWS Or C - 0 (O) May be inoperative provided

GPWS Not required By alternate procedures are established
FAR) and used.

NOTE: Any mode that operates

normally may be used.

1) GPWS (Class A or B A - 0 (O) May be inoperative provided:

Required) a) Alternate procedures are
established and used.
b) Repairs are made within two (2)
flight days.

a) Modes 1-4 (Class A A 4 0 (O) May be inoperative provided:

TAWS Required) a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.

Modes 1 & 3 (Class B A 2 0 (O) May be inoperative provided:

TAWS Required) a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.

b) Test Mode (Class A or A 1 0 (O) May be inoperative provided:

B Required) a) GPWS is considered
inoperative, and
b) Repairs are made within two (2)
flight days.

(continued)
U.S. DEPARTMENT OF TRANSPORTATION
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1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

17. TAWS / GPWS |

1) GPWS (Continued)

c) Glideslope (Mod C - 1
Deviation(Mode 5)
(Class A TAWS
Required) B - 0

Modes 2, 4, & 5 (Class C 3 0

*** B TAWS Required)

d) Advisory Callouts B - 0 (O) May be inoperative provided

(Class A or B alternate procedures are established
Required) and used.

C - 0 (O) May be inoperative provided:

a) Advisory callout not required by
FAR, and
b) Alternate procedures are
established and used.

e) Windshear Mode B 1 0 (O) May be inoperative provided

*** (Reactive) (Class A alternate procedures are established
TAWS Required) and used.

NOTE: Alternate procedures should

include reviewing windshear
avoidance and windshear
recovery procedures.

C 1 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Windshear Detection and
Avoidance System (Predictive)
operates normally.

Windshear Mode C 1 0 (O) May be inoperative provided

*** (Reactive) (Class B alternate procedures are established
TAWS Required) and used.
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

17. TAWS / GPWS |

(Continued)

2) Terrain System B 1 0 (O) May be inoperative provided

Forward Looking alternate procedures are established
Terrain Avoidance and used.
(FLTA) And Premature
Descent Alert (PDA)
Functions (Class A Or
B Required)

3) Terrain Display (Class C - 1

A TAWS Required)

Terrain Display (Class C - 0

*** B TAWS Required)

4) Runway Awareness & C 1 0

*** Advisory System
(Class A Or B
Required)

18. Traffic Awareness D 1 0 |

*** System (TCAD/TAS) |
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

19. Ground Proximity C 1 0 |

*** Altitude Advisory
System (GPAAS)

20. Standby Attitude C - 0 May be inoperative provided not |

Indicator required by Type Design Approval (TC, |
STC, ATC) or 14 CFR instrument and |
equipment requirements. |

B - 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.

21. Flight Profile Advisory D - - |

*** System

22. Independent Multi- C 1 0 (O) May be inoperative provided: |

Function Display a) MFD system does not provide
(Excludes EFIS any primary flight or engine
Equipped Aircraft) instrument display, and
b) MFD integrated systems are
considered inoperative.
• Weather Radar
• TCAS Display
• Navigation Map Display
• TAWS Display
• Thunderstorm Detection

23. Windshear Warning C - 0 (O) May be inoperative provided |

*** and Flight Guidance alternate procedures are established
System (Reactive) and used.

24. Windshear Detection C - 0 (O) May be inoperative provided |

*** and Avoidance System alternate procedures are established
(Predictive) and used.
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

25. Automatic Dependent D - 0 May be inoperative provided it is not |

*** Surveillance Broadcast required by 14 CFR.
(ADS-B) System

NOTE: If ADS-B is installed in lieu of

or as replacement for 14 CFR
required equipment, the repair
category in the operator’s MEL
will be the same as that of the
14 CFR required equipment.

1) Cockpit Display and D - 0 NOTE: Cockpit Display Traffic |

Traffic Information Information (CDTI) display of
(CDTI) data from other aircraft
systems may be used

2) CDTI Control Panel D - 0 May be inoperative provided: |

a) Flight ID can be set, and
b) Screen display is acceptable to
the flight crew.

3) Data Link D - 0 NOTE: In some aircraft the Data Link |

Transmitter(s) Transmission is an integral |
part of the transponder and |
relief is provided in that |
section. |

4) Data Link Receiver(s) D - 0

5) ADS-B Applications D - 0 |
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN

1. Passenger Oxygen C 1 0 As required by FAR.

System

NOTE: Cockpit Crew Oxygen System

must be operative.

2. External Oxygen C 1 0 (M) May be inoperative provided the

Gauge Internal Oxygen Gauge (Cockpit) is
monitored while the Oxygen System is
serviced.

3. Passenger Oxygen C - 0 (M) May be inoperative provided:

Mask a) Corresponding Passenger Seat
is blocked and placarded “DO
NOT OCCUPY”, and
b) Affected Mask does not permit
flow when Cabin Oxygen
System is activated.

4. Protective Breathing D - 0
*** Equipment (PBE)
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
37 VACUUM/ PRESSURE

1. Suction Gauge C 1 0 May be inoperative provided aircraft is

not operated in known or forecast icing
conditions.

2. Instrument Air Valves C 2 1 (O) One may be inoperative provided: |

a) Affected Valve remains |
selected INSTR & ENVIR OFF, |
b) Affected Valve is verified closed |
prior to each Takeoff, and |
c) Aircraft is not operated in
known or forecast icing
conditions.
U.S. DEPARTMENT OF TRANSPORTATION
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Beechcraft Model 200 and F-90 DATE: 09/16/2008 46-1
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SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
46 INFORMATION
SYSTEMS

1. Electronic Flight Bag C - 0 (O) May be inoperative provided

*** System (EFB) alternate procedures are established
and used to ensure all information
associated with the flight is available at
the pilot station in current and
appropriate form.

NOTE 1: If alternate source is

electronic, dual redundancy is
required for operation.

NOTE 2: Any function, program or

document which operates
normally may be used.

1) Power Connection C - 0 (O) May be inoperative provided

*** (Class 1 & 2) alternate procedures are established
and used.

2) Mounting Device C - 0 (M)(O) May be inoperative provided:

*** (Class 2) a) The associated EFB and
hardware is secured by an
alternate means or removed
from the aircraft and
b) Alternate procedures are
established and used.

3) Data Connectivity C - 0 (O) May be inoperative provided

*** (Class 2) alternate procedures are established
and used.

4) EFB Printer C - 0 May be inoperative provided all

*** affected pertinent flight information is
printed and available prior to departure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 46-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
46 INFORMATION
SYSTEMS

2. Integrated Flight
Information System
(Pro Line 21 IFIS-
5000)

1) File Server Unit (FSU) C 1 0 (O)

(FSU INOP message)

*** C 2 0 (O) One or both may be inoperative

provided alternate procedures are
established and used to ensure all
information associated with the flight is
available at the pilot station in current
and appropriate form.

NOTE: If alternate source is electronic,

dual redundancy is required for
operation.

2) Cursor Control Panel C 2 0 (O) One or both may be inoperative

(CCP) provided alternate procedures are
established and used to ensure all
information associated with the flight is
available at the pilot station in current
and appropriate form.

3) Communications C 1 0 (O) May be inoperative provided

*** Management Unit alternate procedures are established
(CMU) and used for ACARS and Universal
WX inoperative.

4) Third VHF Comm C 1 0 (O) May be inoperative provided

*** Radio alternate procedures are established
and used for ACARS and Universal
WX inoperative.

3. XM Satellite Weather D 1 0 |
*** System
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 52-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS

1. Cabin Door Warning C 1 0 May be inoperative provided:

Light a) A flight crewmember confirms
by visual inspection that all
doors are latched prior to each
departure, and
b) “Fasten Seat Belt” Sign remains
ON and/or passengers are
orally briefed to remain seated
with their seat belts fastened for
the entire flight.

2. Cargo Door C 1 0 (O) May be inoperative provided a

Annunciator System crewmember confirms, by visual
inspection, the door is closed and
latched prior to each departure.

3. Cabin Door Lock and C 1 0 (O) May be inoperative provided the

Upper Door Latch Latching Mechanism is inspected using
Observation Light adequate Light by a crewmember prior
System(s) to each departure.

4. Entrance Door C 1 0 (O)

Snubber System

5. Airstair Door Cable D 1 0 May be missing.

Cover(s)

6. (200HDC) Baggage C 1 0 May be inoperative provided: |

Pod Door Warning a) All door latches are operative, |
Light and |
b) A flight crewmember confirms |
by visual inspection that door is |
latched prior to each departure. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14b PAGE NO:
Beechcraft Model 200 and F-90 DATE: 08/27/2010 61-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
61 PROPELLERS

1. Reverse Not Ready C 1 0 May be inoperative provided Propeller

Light Control Levers are in high RPM
(Except A200CT) position for reversing. |

2. Propeller C 1 0
Synchrophase System

3. Propeller C 1 0
Synchroscope

4. Autofeathering System C 1 0 May be inoperative provided:

(200, 200C and F90 a) Aircraft is not modified with
Only) STC SA2307CE, and
b) Aircraft is not equipped with
Four Bladed Propellers.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 73-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
73 ENGINE FUEL &
CONTROL

1. Fuel Flow Indicators B 2 1 (M) May be inoperative provided both

Fuel Quantity Indicating Systems are
operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 77-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
77 ENGINE INDICATING

1. Digital Percent Torque C 2 1 Digital portion only of the display may

Indicators be inoperative.

2. Digital N1 Indicators C 2 1 Digital portion only of the display may

be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 14 PAGE NO:
Beechcraft Model 200 and F-90 DATE: 09/16/2008 79-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
79 ENGINE OIL

1. Oil Pressure C 2 1 (O) One may be inoperative provided

Annunciators corresponding Oil Pressure Gauge is
monitored.