U.S. Department of Transportation

Federal Aviation Administration

Washington , D.C.

 

Master Minimum Equipment List

 

 

 

Revision: 14a

Date:  06/14/2010

 

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:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

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

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 34-16

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:

Beechcraft Model 200 and F-90

REVISION NO: 10

DATE: 04/08/2002

PAGE NO:

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:

Beechcraft Model 200 and F-90

REVISION NO: 13

DATE: 8/17/2004

PAGE NO:

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:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO:

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

06/14/2010

Highlights of Change, Definitions, Preamble

 

14a

06/14/2010

Guidelines for (O) & (M), 21-2, 22-1, 34-5, 37-1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO:

V

Control Page

System

Page No.

Rev. No.

Current Date

 

 

 

 

Cover Page

-

14a

06/14/2010

Table of Contents

I

14a

06/14/2010

Log of Revisions

II

10

04/08/2002

 

III

13

08/17/2004

 

IV

14a

06/14/2010

Control Page

V

14a

06/14/2010

 

VI

14a

06/14/2010

 

VII

14a

06/14/2010

Highlights of Change

VIII

14a

06/14/2010

Definitions

IX

14a

06/14/2010

Preamble

X

14a

06/14/2010

Guidelines for (O) & (M) Procedures

XI

14a

06/14/2010

 

XII

14a

06/14/2010

 

XIII

14a

06/14/2010

 

XIV

14a

06/14/2010

 

XV

14a

06/14/2010

 

XVI

14a

06/14/2010

 

XVII

14a

06/14/2010

 

XVIII

14a

06/14/2010

21

21-1

14

09/16/2008

 

21-2

14a

06/14/2010

 

21-3

14

09/16/2008

22

22-1

14a

06/14/2010

 

22-2

14

09/16/2008

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:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO:

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

14

09/16/2008

28

28-1

14

09/16/2008

 

28-2

14

09/16/2008

30

30-1

13

08/17/2004

 

30-2

14

09/16/2008

 

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

14

09/16/2008

 

34-2

14

09/16/2008

 

34-3

14

09/16/2008

 

34-4

14

09/16/2008

 

34-5

14a

06/14/2010

 

34-6

14

09/16/2008

 

34-7

14

09/16/2008

 

34-8

14

09/16/2008

 

34-9

14

09/16/2008

 

34-10

14

09/16/2008

 

34-11

14

09/16/2008

 

34-12

14

09/16/2008

 

34-13

14

09/16/2008

 

34-14

14

09/16/2008

 

34-15

13

08/14/2004

 

34-16

14

09/16/2008

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO:

VII

Control Page

System

Page No.

Rev. No.

Current Date

 

 

 

 

35

35-1

14

09/16/2008

37

37-1

14a

06/14/2010

46

46-1

14

09/16/2008

 

46-2

14

09/16/2008

52

52-1

14

09/16/2008

61

61-1

14

09/16/2008

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:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE:

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:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

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:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

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 secure Air Conditioner to ensure it will not affect any other System.

 

21-16-1

(O) Procedure to verify affected Environmental and Instrument Bleed Air Valves are CLOSED prior to each flight.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

XII

Guidelines for (O) & (M) Procedures

21-16-2

(O) Procedure to verify affected Environmental and Instrument Bleed Air Valves are 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 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

(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.

 

24-8

(M) Maintenance procedure to disconnect and remove the Standby Battery.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

XIII

Guidelines for (O) & (M) Procedures

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 and LOCK 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

(O) Operations procedure to ensure a sufficient number of Receptacles are available for the flight.

 

(M) Maintenance procedure to ensure the affected Receptacle is EMPTY and secured to prevent use.

 

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:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

XIV

Guidelines for (O) & (M) Procedures

 

25-14

 

(M) Maintenance procedure to secure the System inoperative.

 

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 used by crewmembers only.

 

(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

27-4-3

(M) Maintenance procedure to deactivate the Electric Trim and ensure 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 ensure proper operation of the Anti-Ice Vanes prior to each departure.

(M) Maintenance procedure to ensure the Anti-Ice Vanes are secured in the full EXTENDED position.

(O) Operations procedure to ensure that Surface Temperatures and Performance Charts are considered when applicable.

(M) Maintenance procedure to ensure the Anti-Ice Vanes are secured in the full EXTENDED position.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

XV

Guidelines for (O) & (M) Procedures

 

30-5-1

 

(O) Procedure to verify the operation of each pitot mast heat 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 Engine Anti-Ice On 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-

a & -b

(M) Maintenance procedure to ensure the Anti-Ice Vanes are secured in the fully EXTENDED position.

 

(O) Procedure to ensure that Surface Temperatures and Performance Charts are considered when applicable.

 

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 determine cause of malfunction and take appropriate action and determine Rudder Boost is not affected.

 

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.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

XVI

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.

 

34-10-1&2

(O) Procedure to determine the Multi-Function Processing Unit is operative.

 

34-13

(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.

 

34-18

(O) Operations procedure to verify Autopilot and Altitude Hold is operative and enroute operations do not Altitude Alerter.

 

34-20

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

 

34-21

(O) Operations procedure to ensure required number of sources of magnetic heading information are available and operative.

 

34-22

(M) Maintenance procedure to deactivate and SECURE the System.

 

34-22-2

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

 

34-22-3

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

 

34-23

(M) Maintenance procedure to deactivate and SECURE the TCAS System.

 

34-24

(O) Procedure to ensure pilot planning and awareness of terrain clearance.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

XVII

Guidelines for (O) & (M) Procedures

 

34-24-1

 

(O) Procedure to ensure alternate means of terrain awareness with inoperative GPWS.

 

34-24-1-a

O) Procedure to ensure alternate means of crew awareness with inoperative Mode(s).

34-24-1-b

(O) Procedure to ensure alternate means of terrain awareness with inoperative GPWS.

 

34-24-1-d

(O) Procedure to ensure alternate means of crew awareness with inoperative advisory callout(s).

 

34-24-1-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.

 

34-24-2

(O) Procedure to ensure alternate means of terrain awareness with inoperative FLTA/PDA Modes.

 

34-29-1

(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.

 

34-30-1

 

(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 NMS guidance in the terminal area.

 

34-32

(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.

 

34-33

(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.

 

34-34

(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.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO.

XVIII

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

(M) Maintenance procedure to determine Bleed Air Shutoff Valve(s) are secure in the CLOSED position

 

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

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

21-1

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Pressurization Controller

C

1

0

(O) May be inoperative for 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

(ALT WARN)

C

1

0

May be inoperative for pressurized flight at or below 10,000 feet MSL.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

 

5.

Cabin Rate of Climb Indicator

C

1

0

May be inoperative for pressurized flight provided CABIN ALTITUDE/ DIFFERENTIAL PRESSURE Indicator is operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

 

6.

Cabin Altitude/ Differential Pressure Indicator

C

1

0

(O) May be inoperative for unpressurized flight provided Safety Valve (Dump) is OPEN.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO:

21-2

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

7.

Bleed Air Shutoff Valves (Environmental) (3 Position Switch)

C

2

1

(M) One may be inoperative in the ENVIR OFF Position for pressurized flight.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O) May be inoperative in the ENVIR OFF position for unpressurized flight.

 

 

 

 

 

 

 

 

8.

Bleed Air Shutoff Valves (Pneumatic Instrument Air)

(3 Position Switch)

 

 

 

DELETED; Revision 14a,

See Chapter 37

|

|

 

 

 

 

 

 

 

9.

Bleed Air Shutoff Valves

(2 Position switch)

C

2

1

(M) One may be inoperative in the closed position for pressurized flight.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O) May be inoperative in closed position for unpressurized flight.

 

 

 

 

 

 

 

 

10.

AUTOMATIC Temperature Controller

C

1

0

May be inoperative provided MANUAL Temperature Controller is operative.

 

 

 

 

 

 

 

 

11.

MANUAL Temperature Controller

C

1

0

May be inoperative provided 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

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

21-3

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

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 Illuminate

C

2

1

(O) One may be inoperative provided:

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 Illuminated

C

2

1

(O) One may be inoperative provided:

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 System

C

1

0

 

 

 

 

 

 

 

 

 

18.

Bleed Air OFF Annunciator System

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

 

19.

Cabin Door Seal System

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

 

20.

Cabin Temperature Indicator System

C

1

0

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14a

DATE: 06/14/2010

PAGE NO:

22-1

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

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

(200 Series except 200T with Tip Tanks or STC SA3519NM & F90 except STC SA4130NM)

C

1

0

(M) May be inoperative provided aircraft is operated at or below 17,000 ft Pressure Altitude.

 

 

 

 

 

 

 

 

 

(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 SA3519NM)

C

1

0

(M)

 

 

 

 

 

 

 

 

 

(F-90 with STC SA4130NM)

C

1

0

(M)

|

 

 

 

 

 

 

 

3.

Autopilot Control Wheel Disconnect Switches

(AP/YD/TRIM DISC)

C

2

1

One may be inoperative on the non-flying pilot side provided:

a)          Autopilot is not used below 1,500 feet AGL, and

b)          Approach minimums do not require the use of the autopilot

 

 

 

 

 

 

 

 

 

(Except Garmin

GFC-700 AFCS equipped)

B

-

0

May be inoperative provided:

a)          Autopilot is not used, and

b)          Second level switch trim interrupt function remains operative.

|

|

 

 

 

 

 

 

 

 

(Except Garmin

GFC-700 AFCS equipped)

B

-

0

(M) May be inoperative provided:

a)          Autopilot is considered inoperative,

b)          Electric Elevator Trim is considered inoperative, and

c)          Yaw Damper is considered inoperative.

|

|

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

22-2

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

22

AUTO PILOT

 

 

 

 

 

 

 

 

 

 

 

 

4.

Autopilot Go-Around Switch

C

1

0

(O) May be inoperative provided:

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 Selector/Annunciator (Except Collins Proline 21 equipped)

C

1

0

(O) May be inoperative provided the affected Mode(s) is/are selected momentarily prior to departure to verify that proper Mode Annunciation is displayed on the pilot’s EFIS Display or Remote Annunciator Panel.

 

 

 

 

 

 

 

 

6.

Flight Director Mode Selector Panel Annunciator Lamps (Except Collins Proline 21 equipped)

C

1

0

(O) May be inoperative provided the affected Mode(s) is/are selected momentarily prior to departure to verify that proper Mode Annunciator is displayed on the Pilot’s EFIS Display or Remote Annunciator Panel.

 

 

 

 

 

 

 

 

7.

Autopilot/Flight Guidance Panel Lamps (Except Collins Proline 21 equipped)

C

1

0

(O) May be inoperative provided the affected Mode(s) is/are selected momentarily prior to departure to verify that proper Mode Annunciator is displayed on pilot’s EFIS Display or Remote Annunciator Panel.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

23-1

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Communications System (VHF, UHF)

D

-

-

Any in excess of those required by FAR 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 Configuration

C

1

0

(O) May be inoperative provided 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 System

(Including Audio Amp.)

C

2

0

(O) May be inoperative provided:

a)          Two operative Headsets are 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

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

23-2

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

6.

Boom Microphones

(includes headset mic)

 

 

 

 

 

 

 

 

 

 

 

 

1)

With FDR and Cockpit Voice Recorder Equipped To Record Boom Microphone

A

-

0

May be inoperative provided:

a)          Flight Data Recorder (FDR) operates normally, and

b)          Repairs are made within three flight days.

 

 

 

 

 

 

 

 

2)

With Only Cockpit Voice Recorder Equipped To Record Boom Microphone

A

-

0

May be inoperative provided repairs are made within three flight days.

 

 

 

 

 

 

 

 

3)

***

Without Cockpit Voice Recorder Equipped To Record Boom Microphone

D

-

0

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

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

23-3

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

7.

Cockpit Voice Recorder (CVR)

 

 

 

 

 

 

 

 

 

 

 

 

1)

With Flight Data Recorder (FDR) Installed

A

1

0

May be inoperative provided:

a)          Flight Data Recorder (FDR) operates normally, and

b)          Repairs are made within three flight days.

 

 

 

 

 

 

 

 

2)

Without Flight Data Recorder (FDR) Installed

A

1

0

May be inoperative provided repairs are made within three flight days.

 

 

 

 

 

 

 

 

3)

For Operators Other Than Air Carriers and Commercial Operators

A

1

0

May be inoperative provided repairs are made in accordance with applicable FARs.

 

 

 

 

 

 

 

 

8. ***

Passenger Call System

C

1

0

 

 

 

 

 

 

 

 

 

9. ***

Voice Activated Interphone System

(cockpit to cabin)

D

1

0

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

23-4

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

10.

High Frequency  (HF)

Communication System

D

-

-

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

 

 

 

 

 

 

 

 

 

 

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 Briefing System

D

1

0

(O) May be inoperative provided passengers are appropriately briefed prior to each departure.

 

 

 

 

 

 

 

 

12. ***

Flight Phone System

D

1

0

 

 

 

 

 

 

 

 

 

13. ***

Ground Communications Power System

D

1

0

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

23-5

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

14.

Push-to-Talk Switches

 

 

 

 

 

 

 

 

 

 

 

 

1)

Aircraft Equipped With Separate Hand Microphone Plug-In (Second-in-command Required)

C

2

1

One may be inoperative provided Hand Held Microphone on affected side is operative.

 

 

 

 

 

 

 

 

2)

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

C

2

1

Right side may be inoperative.

 

 

 

 

 

 

 

 

3)

Aircraft Without Separate Hand Microphone Plug-In. (Second-In-Command Not Required)

C

2

1

Right side may be inoperative.

 

 

 

 

 

 

 

 

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

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

23-6

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

16.

Selective Call Systems (SELCAL)

C

-

0

(O) May be inoperative provided 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

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

24-1

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

24

ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

 

1.

DC Generator Caution Lights

B

2

1

One may be inoperative provided corresponding Load Meter is monitored.

 

 

 

 

 

 

 

 

2.

Inverters

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

B

2

1

One may be inoperative for day VFR.

 

 

 

 

 

 

 

 

3.

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

B

2

1

One may be inoperative provided both Inverters are operative.

 

 

 

 

 

 

 

 

4.

DC Load Meter

 

 

 

DELETED, Revision 14

 

 

 

 

 

 

 

 

5.

AC Volt/Frequency Meter

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

B

1

0

May be inoperative provided Inverter Warning Light is operative.

 

 

 

 

 

 

 

 

6. ***

Battery Temperature Indicating System

C

1

0

May be inoperative provided the Standard Battery Charge Annunciator System is operative.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

24-2

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

24

ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

 

7. ***

Cabin AC Power System

C

-

0

(M)

 

 

 

 

 

 

 

 

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 Annunciator

C

1

0

(O)

 

 

 

 

 

 

 

 

11.

L or R GEN BUS TIE Relay

(Model F90 Only)

B

2

1

One may be inoperative for day VMC operations provided both DC GEN Annunciators/Caution Lights are operative.

 

 

 

 

 

 

 

 

12.

L or GEN BUS TIE Annunciator

(Model F90 Only)

B

2

0

(O) May be inoperative provided:

a)          Generator Bus Tie Relay is verified closed prior to each departure, and

b)          Both DC GEN Annunciators/ Caution Lights are operative.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 12

DATE: 11/03/2003

PAGE NO:

25-1

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

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

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

25-2

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

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:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

25-3

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

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 Defibrillator (AED) and/or Associated Equipment

D

-

-

May be incomplete, missing, or inoperative.

 

 

 

 

 

 

 

 

2) ***

Emergency Medical Kit (EMK) and/or Associated Equipment

D

-

-

May be incomplete, missing or inoperative.

 

 

 

 

 

 

 

 

3)

First Aid Kit (FAK) and/or Associated Equipment

D

-

-

Any in excess of those required by FAR may be incomplete, missing or 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:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

25-4

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

6.

Non-Essential Equipment & Furnishings (NEF)

 

-

0

May be inoperative, damaged, or missing provided that the item(s) is 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 While Seated” Sign or Placard

C

-

-

One or more Signs or Placards may be illegible or missing provided a legible Sign or Placard is visible from each occupied Passenger Seat.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

25-5

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

9. ***

Exterior Lavatory Door Ashtrays

 

 

 

 

 

 

 

 

 

 

 

 

1)

Airplanes With More Than One Exterior Lavatory Door Ashtray Installed

A

-

-

One may be missing provided it is replaced within 10 calendar days.

 

 

 

 

 

 

 

 

2)

Airplanes With Only One Exterior Lavatory Door Ashtray Installed

A

1

0

May be missing provided it is replaced within 3 calendar days.

 

 

 

 

 

 

 

 

10. ***

Waste Receptacle Access Doors/Covers

C

-

-

(M)(O) May be inoperative provided:

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 Systems

C

-

-

(M) May be inoperative or missing 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:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

25-6

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

12.

Cabin Storage Compartments / Closets

C

-

-

(M) May be inoperative provided:

a)          Procedures are established to 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 Key Locks

D

-

-

(M) May be inoperative in the unlocked position provided door latch remains operative.

 

 

 

 

 

 

 

 

13. ***

EMS Equipment

C

-

0

(O)(M) 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:

Beechcraft Model 200 and F-90

REVISION NO: 14

DATE: 09/16/2008

PAGE NO:

25-7

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

2. NUMBER INSTALLED

 

3. NUMBER REQUIRED FOR DISPATCH

 

4. REMARKS AND EXCEPTIONS

25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

14. ***

Smartstart Security System

C

1

0

(M)

 

 

 

 

 

 

 

 

15. ***

Pyrotechnic Signal

D

-

-

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

 

 

 

 

 

 

 

 

16.

Protective Breathing Device

 

 

 

DELETED REV.14, See Chapter 35.

 

 

 

 

 

 

 

 

17. ***

Sound Management System (Active Noise Canceling System)

D

-

0