Revision:

5a

 

Date: 04/20/2009

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON , D.C.

 

 

 

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

HAWKER BEECHCRAFT

 

 

 

 

 

BE-1900D

 

 

 

 

 

 

 

 

 

 

 

John 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

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO. 5a

DATE: 04/20/2009

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

--

Highlights of Change

VII

--

Definitions

VIII

--

Preamble

IX

--

Guidelines for (O) & (M) Procedures

X THRU XVI

21

Air Conditioning

21-1, 2, 3, 4, 5

22

Auto Flight

22-1

23

Communications

23-1, 2, 3, 4

24

Electrical Power

24-1, 2

25

Equipment/Furnishings

25-1, 2, 3, 4, 5

25

Equipment/Furnishings

25-6

26

Fire Protection

26-1, 2

27

Flight Controls

27-1, 2

28

Fuel

28-1, 2, 3, 4, 5

30

Ice and Rain Protection

30-1, 2, 3, 4

31

Indicating/Recording Systems

31-1, 2, 3, 4

32

Landing Gear

32-1, 2

33

Lights

33-1, 2, 3

34

Navigation

34-1, 2, 3, 4, 5

34

Navigation

34-6 THRU 10

35

Oxygen

35-1

37

Vacuum/Pressure

37-1, 2

38

Water/Waste

38-1

52

Doors

52-1

56

Windows

56-1

61

Propellers

61-1

73

Engine Fuel & Control

73-1

74

Ignition

74-1

77

Engine Indicating

77-1

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5

DATE: 02/07/2006

PAGE NO:

II

Log of Revisions

Rev No.

Date

Page Numbers

Initials

0a

02/14/1992

HIGHLIGHTS OF REV.

 

0a

02/14/1992

23-2

 

0b

04/30/1992

HIGHLIGHTS OF REV.,GUIDELINES

 

0b

04/30/1992

28-2

 

0c

07/23/1993

HIGHLIGHTS OF REV.,DEFINITIONS

 

0c

07/23/1993

GUIDELINES

 

0c

07/23/1993

21-1,21-2,21-3,22-1,23-1

 

0c

07/23/1993

23-2,24-1,24-2,25-1,25-2

 

0c

07/23/1993

26-1,27-1,27-2,28-1,28-2

 

0c

07/23/1993

30-1,30-2,30-3,30-4,31-1

 

0c

07/23/1993

32-1,33-1,33-2,33-3,34-1

 

0c

07/23/1993

34-2,34-3,34-4,35-1,37-1

 

0c

07/23/1993

52-1,61-1

 

0d

12/15/1993

HIGHLIGHTS OF REV.,GUIDELINES

 

0d

12/15/1993

21-1,21-2,21-3,23-1,23-2

 

0d

12/15/1993

24-1,28-1,31-1,33-1,33-2

 

0d

12/15/1993

33-3,34-4,52-1

 

0e

05/24/1994

HIGHLIGHTS OF REV.,GUIDELINES

 

0f

10/28/1994

HIGHLIGHTS OF REV.,GUIDELINES

 

0f

10/28/1994

30-1,30-2,30-3,30-4

 

0g

12/08/1995

HIGHLIGHTS OF REV.,DEFINITIONS

 

0g

12/08/1995

GUIDELINES

 

0g

12/08/1995

34-3,34-4,52-1

 

0h

02/15/1996

HIGHLIGHTS OF REV.,DEFINITIONS

 

0h

02/15/1996

GUIDELINES

 

0h

02/15/1996

23-2,23-3,30-1,30-2,30-3

 

0h

02/15/1996

30-4,77-1

 

0i

03/18/1997

HIGHLIGHTS OF REV.,DEFINITIONS

 

0i

03/18/1997

25-1,25-2,26-1,32-2,33-1

 

0i

03/18/1997

34-1,34-2,34-3,34-4

 

0j

06/09/1997

HIGHLIGHTS OF REV.,DEFINITIONS

 

0j

06/09/1997

23-1,28-2,33-2,33-3,34-2

 

1

11/03/1998

HIGHLIGHTS OF REV.,DEFINITIONS

 

1

11/03/1998

GUIDELINES

 

1

11/03/1998

21-1,21-2,21-3,22-1,23-1

 

1

11/03/1998

23-2,23-3,24-1,24-2,25-1

 

1

11/03/1998

25-2,25-3,26-1,27-1,27-2

 

1

11/03/1998

28-1,28-2,28-3,28-4,30-1

 

1

11/03/1998

30-2,30-3,31-1,31-2,32-1

 

1

11/03/1998

32-2,33-1,33-2,33-3,34-1

 

1

11/03/1998

34-2,34-3,34-4,34-5,35-1

 

1

11/03/1998

37-1,52-1,56-1,61-1,74-1

 

1

11/03/1998

77-1

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5

DATE: 02/07/2006

PAGE NO:

III

Log of Revisions

Rev No.

Date

Page Numbers

Initials

2

10/25/1999

HIGHLIGHTS OF REV.,DEFINITIONS

 

2

10/25/1999

GUIDELINES

 

2

10/25/1999

21-1,21-2,21-3,22-1,25-1

 

2

10/25/1999

25-2,25-3,25-4,27-1,28-3

 

2

10/25/1999

31-1,31-2,33-1,33-2,33-3

 

2

10/25/1999

34-1,34-2,34-3,34-4,34-5

 

2

10/25/1999

34-6,56-1,61-1,74-1

 

3

04/11/2000

HIGHLIGHTS OF REV.,DEFINITIONS

 

3

04/11/2000

PREAMBLE,GUIDELINES

 

3

04/11/2000

22-1,56-1

 

3a

09/18/2001

HIGHLIGHTS OF REV.,DEFINITIONS

 

3a

09/18/2001

GUIDELINES

 

3a

09/18/2001

21-1,21-2,21-3,21-4,21-5

 

3b

02/15/2002

HIGHLIGHTS OF REV.,DEFINITIONS

 

3b

02/15/2002

GUIDELINES

 

3b

02/15/2002

21-1,21-2,21-3,21-4,21-5

 

3b

02/15/2002

34-1,34-2,34-3,34-4,34-5

 

3b

02/15/2002

34-6,34-7

 

4

07/30/2002

HIGHLIGHTS OF REV.,DEFINITIONS

 

4

07/30/2002

GUIDELINES

 

4

07/30/2002

21-1,21-2,21-3,21-4,21-5

 

4

07/30/2002

22-1,23-1,23-2,23-3,23-4

 

4

07/30/2002

24-1,24-2,25-1,25-2,25-3

 

4

07/30/2002

25-4,25-5,25-6,26-1,26-2

 

4

07/30/2002

27-1,27-2,28-1,28-2,28-3

 

4

07/30/2002

28-4,28-5,30-1,30-2,30-3

 

4

07/30/2002

30-4,31-1,31-2,31-3,31-4

 

4

07/30/2002

32-1,32-2,33-1,33-2,33-3

 

4

07/30/2002

34-1,34-2,34-3,34-4,34-5

 

4

07/30/2002

34-6,34-7,34-8,34-9,34-10

 

4

07/30/2002

35-1,37-1,37-2,38-1,52-1

 

4

07/30/2002

56-1,61-1,73-1,74-1,77-1

 

4a

10/04/2004

HIGHLIGHTS OF REV.,DEFINITIONS

 

4a

10/04/2004

GUIDELINES

 

4a

10/04/2004

22-1,25-1,25-2,25-3,25-4

 

4a

10/04/2004

25-5,25-6,26-1,26-2,27-1

 

4a

10/04/2004

27-2,28-1,28-2,28-3,28-4

 

4a

10/04/2004

28-5,30-1,30-2,30-3,30-4

 

4a

10/04/2004

31-1,31-2,31-3,31-4,33-1

 

4a

10/04/2004

33-2,33-3,34-1,34-2,34-3

 

4a

10/04/2004

34-4,34-5,34-6,34-7,34-8

 

4a

10/04/2004

34-9,34-10,37-1,37-2,38-1

 

4a

10/04/2004

52-1,56-1,73-1,74-1

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5a

DATE: 04/20/2009

PAGE NO:

IV

Log of Revisions

Rev No.

Date

Page Numbers

Initials

4b

12/14/2004

HIGHLIGHTS OF REV.,DEFINITIONS

 

4b

12/14/2004

27-2

 

5

02/07/2006

Log of Revisions

 

5

02/07/2006

Control Page

 

5

02/07/2006

Highlights of Change

 

5

07/05/2005

Definitions

 

5

02/07/2006

Guidelines for (O) & (M) Procedures

 

5

02/07/2006

21-1, 21-2, 21-3, 21-4, 21-5, 22-1, 23-1, 23-2,

23-3, 23-4, 24-1, 24-2, 25-1, 25-2, 25-3, 25-4, 25-5, 25-6, 26-1, 26-2, 27-1, 27-2, 28-1, 28-2, 28-3, 28-4, 28-5, 30-1, 30-2, 30-3, 30-4, 31-1, 31-2, 31-3, 31-4, 32-1, 32-2, 33-1, 33-2, 33-3, 34-1, 34-2, 34-3, 34-4, 34-5, 34-6, 34-7, 34-8, 34-9, 34-10, 34-11, 34-12, 35-1, 37-1, 37-2,  38-1, 52-1, 59-1, 61-1, 73-1, 74-1, 77-1.

 

5a

04/20/2009

Log of Revisions, Control Page,

Highlights of Change, Definitions, Preamble, Guidelines for (O)&(M) Procedures, 28-1, 35-1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5a

DATE: 04/20/2009

PAGE NO:

V

Control Page

System

Page No.

Rev. No.

Current Date

Cover Page

-

5a

04/20/2009

Table of Contents

I

5a

04/20/2009

Log of Revisions

II

5

02/07/2006

 

III

5

02/07/2006

 

IV

5a

04/20/2009

Control Page

V

5a

04/20/2009

 

VI

5a

04/20/2009

Highlights of Change

VII

5a

04/20/2009

Definitions

VIII

5a

04/20/2009

Preamble

IX

5a

04/20/2009

Guidelines for (O) & (M) Procedures

X

5a

04/20/2009

 

XI

5

02/07/2006

 

XII

5

02/07/2006

 

XIII

5a

04/20/2009

 

XIV

5

02/07/2006

 

XV

5a

04/20/2009

 

XVI

5

02/07/2006

21

21-1

5

02/07/2006

 

21-2

5

02/07/2006

 

21-3

5

02/07/2006

 

21-4

5

02/07/2006

 

21-5

5

02/07/2006

22

22-1

5

02/07/2006

23

23-1

5

02/07/2006

 

23-2

5

02/07/2006

 

23-3

5

02/07/2006

 

23-4

5

02/07/2006

24

24-1

5

02/07/2006

 

24-2

5

02/07/2006

25

25-1

5

02/07/2006

 

25-2

5

02/07/2006

 

25-3

5

02/07/2006

 

25-4

5

02/07/2006

 

25-5

5

02/07/2006

 

25-6

5

02/07/2006

26

26-1

5

02/07/2006

 

26-2

5

02/07/2006

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5a

DATE: 04/20/2009

PAGE NO:

VI

Control Page

System

Page No.

Rev. No.

Current Date

 

 

 

 

27

27-1

5

02/07/2006

 

27-2

5

02/07/2006

28

28-1

5a

04/20/2009

 

28-2

5

02/07/2006

 

28-3

5

02/07/2006

 

28-4

5

02/07/2006

 

28-5

5

02/07/2006

30

30-1

5

02/07/2006

 

30-2

5

02/07/2006

 

30-3

5

02/07/2006

 

30-4

5

02/07/2006

31

31-1

5

02/07/2006

 

31-2

5

02/07/2006

 

31-3

5

02/07/2006

 

31-4

5

02/07/2006

32

32-1

5

02/07/2006

 

32-2

5

02/07/2006

33

33-1

5

02/07/2006

 

33-2

5

02/07/2006

 

33-3

5

02/07/2006

34

34-1

5

02/07/2006

 

34-2

5

02/07/2006

 

34-3

5

02/07/2006

 

34-4

5

02/07/2006

 

34-5

5

02/07/2006

 

34-6

5

02/07/2006

 

34-7

5

02/07/2006

 

34-8

5

02/07/2006

 

34-9

5

02/07/2006

 

34-10

5

02/07/2006

 

34-11

5

02/07/2006

 

34-12

5

02/07/2006

35

35-1

5a

04/20/2009

37

37-1

5

02/07/2006

38

38-1

5

02/07/2006

52

52-1

5

02/07/2006

56

56-1

5

02/07/2006

61

61-1

5

02/07/2006

73

73-1

5

02/07/2006

74

74-1

5

02/07/2006

77

77-1

5

02/07/2006

 

37-2

5

02/07/2006

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO. 5a

DATE: 04/20/2009

PAGE NO.

VII

HIGHLIGHTS OF CHANGE

 

 

Definitions

Change format of DEFINITIONS section to accommodate new FSIMS MMEL distribution format.

 

 

Preamble

Change format of PREAMBLE section to accommodate new FSIMS MMEL distribution format.

 

 

Guidelines (O)&(M)

Update introduction to Guidelines for (O) & (M) Procedures.

 

 

28-1

Change Remarks to require operative Standby Electric Boost Pump.

Add (O) procedure to configure and check Standby Electric Boost Pump.

Revise Guidelines for (O) & (M) procedure for Engine Driven Low Pressure Fuel Boost Pump failure.

 

 

35-1

Change Oxygen System description to Passenger Oxygen System and add NOTE to specify requirement for Cockpit Crew Oxygen.

 

 

35-2

Change External Oxygen Gauge Remarks to remove inappropriate identification of personnel and add (M).

 

 

35-4

Add relief for PBE IAW PL-43.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5a

DATE: 04/20/2009

PAGE:

VIII

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.

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5a

DATE: 04/20/2009

PAGE NO:

IX

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

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5a

DATE: 04/20/2009

PAGE NO:

X

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 some items. These procedures must be established by the operator and may be based on the aircraft manufacturer’s recommended procedures, Supplemental Type Certificate modifier’s recommended procedures, or equivalent operator procedures.  When recommended procedures are published the operator should comply with these procedures. If recommended procedures are not published, the following guidelines delineate the aspects to be considered by the operator in the development of required procedures.

 

21-3-1

(O) Procedure to verify environmental and instrument air valves are closed prior to each flight.

 

 

21-3-2

(O) Procedure to verify environmental and instrument air valves are closed prior to each flight and to either extinguish or mask illuminated annunciator.

 

 

21-4

(O) Procedure to verify appropriate environmental bleed air valve is closed prior to every flight and either extinguish or mask illuminated annunciator, if applicable.

 

 

21-5

(O) Procedure to extinguish or mask illuminated annunciator, if applicable.

 

 

21-8

(M) Procedure for removing or securing outflow/safety valve in the open position.

 

 

21-9

(M) Procedure for removing or securing outflow/safety valve in the open position.

 

 

21-9-1

(O) Procedure to ensure each crew (and dispatcher if applicable) is aware of pressurization capability and/or limitations.

 

 

21-9-2

(O) Procedure to ensure each crew (and dispatcher if applicable) is aware of pressurization capability and/or limitations.

 

 

21-9-3

(O) Procedure to ensure each crew (and dispatcher if applicable) is aware of pressurization capability and/or limitations.

 

 

21-9-4

(O) Procedure to ensure first flight is planned assuming aircraft will not pressurize. If aircraft pressurizes normally, appropriate adjustments can be made to the flight plan. Coordination with dispatch, if applicable, should be accomplished.

 

Procedure to ensure each crew (and dispatcher if applicable) is aware of pressurization capability and/or limitations.

 

 

21-14

(O)Procedure to verify affected environmental bleed air valve(s) is/are closed prior to each flight.

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5

DATE: 02/07/2006

PAGE NO:

XI

Guidelines for (O) & (M) Procedures

21-17

(O) Procedure to extinguish or mask illuminated annunciator, if applicable.

 

 

22-1

(M)Procedure to disable the autopilot and determine that the servos do not cause binding of the control cables.

 

 

22-2

(O)Procedure to disable Rudder Boost function.

 

(M)Procedure to disable the yaw damper and determine that the rudder servo does not cause binding of the control cables.

 

Acceptable procedure: Move rudder pedals through full travel to ensure no restrictions and pull and band "servo" circuit breaker.

 

 

22-2-1

(O)Procedure to disable the rudder boost function.

 

 

22-2-2

(M)Procedure to disable the yaw damper and determine that the rudder servo does not cause binding of the control cables. Acceptable procedure: Same as 22-2 above.

 

 

22-2-3

(M)Procedure to disable the yaw damper and determine that the rudder servo does not cause binding of the control cables. Acceptable procedure: Same as 22-2 above.

 

 

22-2-4

(M)Procedure to disable the yaw damper and determine that the rudder servo does not cause binding of the control cables. Acceptable procedure: Same as 22-2 above.

 

 

23-1

(O)Procedure to specify how passengers are to be briefed and to operate within the MMEL restrictions.

 

 

23-12

(O)Procedure to ensure remaining Long Range Communications System(s) operate normally.

 

 

24-3

(O)Procedure to ensure that the electrical load is less than 50% on the operative side generator prior to take-off and at all times during flight and that loads are not added if the generator on the operative side fails.

 

 

24-6

(M)Procedure to ensure ground power relay is open.

 

 

24-7

(O)Procedure to ensure connection and disconnection of power cart is verified.

 

 

24-9

(O)Procedure to verify generator bus tie relay is closed.

 

 

25-1-2

(O)Procedure to ensure crew awareness of inoperative restraining bar.

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION: 5

DATE: 02/07/2006

PAGE NO:

XII

Guidelines for (O) & (M) Procedures

 

 

25-2

(M)Procedure to secure the ELT to preclude false operation.

 

 

25-10

(M)Procedure to ensure seat is locked in the appropriate position.

 

 

25-13

(O)Procedure to ensure crew awareness of specific airspeed information.

 

 

25-14

(M)Procedure to lock the rudder pedals in a position that allows full rudder pedal movement.

 

 

25-17

(O)Procedure to ensure sufficient waste receptacles are available for the intended flight.

 

(M)Procedure to secure access to the affected waste receptacle.

 

 

25-20

(M)Procedure to secure the compartment/closet in closed position.

 

 

25-21

(M)Procedure to ensure that cargo is not secured by an inoperative cargo restraint system.

 

 

26-3

(O)Procedure to ensure waste receptacle is empty and lavatory is used by crewmembers only.

(M)Procedure to lock and placard Lavatory Door.

 

 

26-4

(O)Procedure to ensure waste receptacle is empty and Lavatory is used by crewmembers only.

(M)Procedure to lock and placard Lavatory Door.

 

 

27-2

(O)Procedure to verify the flaps are secure and in the UP position, the circuit breaker is pulled and a placard is installed which states the following:

"DO NOT SILENCE THE LANDING GEAR WARNING HORN". The placard should be installed near the landing gear warning horn silence button.

 

 

27-4

(O)Procedure to ensure there is no binding of the trim cables prior to each flight.

Acceptable procedure: Manually operate trim full travel and visually observe to verify full travel.

 

 

 

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PAGE NO:

XIII

Guidelines for (O) & (M) Procedures

28-1

(O) Operations procedure to ensure Standby Electric Boost Pump is operative and Fuel Low Pressure light is operative and extinguished

 

(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.

 

 

28-5-1

(O)Procedure to deactivate the pump and ensure no electrical power is supplied to it.

Procedure to ensure auxiliary fuel is balanced prior to each flight and is considered unusable for flight planning purposes.

 

 

28-7

(O)Procedure to ensure fuel balance is maintained within AFM limits.

 

Acceptable procedure: Fill fuel tanks and calculate fuel burn from full tanks.

 

 

28-7-1

(O)Procedure to ensure fuel balance is maintained within AFM limits.

 

Acceptable procedure: Fill fuel tanks and calculate fuel burn from full tanks.

 

 

28-7-2

(O)Procedure to ensure fuel balance is maintained within AFM limits.

 

 

30-2

(O)Procedure to determine inoperative motor does not affect other actuator motor.

 

(O)Procedure to ensure ice vanes are in the extended position.

 

(M)Procedure to secure vanes in the extended position.

 

 

30-4-1

(O)Procedure for flight crewmember to verify operation of Inertial Ice Vane prior to each departure.

 

(M)Procedure to secure vanes in the extended position.

 

 

30-4-2

(M)Procedure to secure vanes in the extended position

 

 

30-6

(M)Procedure to ensure affected windshield has an effective hydrophobic coating each flight day of operation without operative Windshield Wipers.

 

 

30-12

(M)Procedure to secure shutoff valves in the closed position and secure circuit breaker.

 

 

 

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DATE: 02/07/2006

PAGE NO:

XIV

Guidelines for (O) & (M) Procedures

31-2

(O)Procedure for recording aircraft time for maintenance purposes.

 

 

31-5

(O)Procedure to check operation of individual circuits.

 

 

31-11

(M)Procedure to pull and collar CB in the open position.

(O)Procedure to ensure that aircraft time entries are made in the aircraft flight log.

 

 

32-1

(O)Procedure to ensure crew and dispatcher awareness for compliance with MMEL restrictions and AFM procedures.

(M)Procedure to ensure nose wheel is in the free caster mode and secure circuit breaker.

 

 

32-1-1

(O)Procedure to ensure crew and dispatcher awareness for compliance with MMEL restrictions and AFM procedures

 

 

32-1-2

(O)Procedure to ensure crew awareness that nose steering is in the free caster mode and for compliance with MMEL restrictions and AFM procedures

(M)Procedure to ensure nose wheel is in the free caster mode and secure circuit breaker.

 

 

32-4

(O)Procedure to ensure crew awareness of change in nose wheel steering and for compliance with MMEL restrictions.

 

(M)Procedure to disconnect and secure actuator.

 

 

32-5

(M)Maintenance procedure to check hydraulic fluid level at the time of discovery and prior to the first flight of the day.

(O)Procedure to check for leaks prior to and after each flight.

 

 

32-7

(O)Procedures to secure aircraft during ground emergencies and prior to releasing toe brakes during normal operations.

 

 

32-8

(O)Procedure to ensure crew awareness of the requirement to manually move the down lock latch.

 

 

33-2-3

(O)Procedure to verify switch function is operative.

 

 

34-3

(O)Procedure to ensure crew awareness of the need to regularly check/reset directional gyro.

NOTE: Do NOT select the Heading input (with the HD Reversionary Switch) of the affected Flightdeck Heading Indicator to a single, common gyro heading source. This is NOT permitted because it reduces the heading source redundancy.

 

 

34-12-1

(O)Procedure to ensure crew awareness of inoperative G0-AROUND mode.

 

 

 

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PAGE NO:

XV

Guidelines for (O) & (M) Procedures

34-13

(O)Operations procedure to ensure autopilot hold is operative and enroute operations do not require its use.

 

 

34-15

(M)Procedure to deactivate and secure the system.

 

(O)Procedure to operate without TCAS I system.

 

 

34-16

(M)Procedure to deactivate and secure the system.

 

(O)Procedure to operate without TCAS II system.

 

 

34-16-2

(O)Procedure to ensure non-flying pilot monitors pilot display.

(O)Procedure to ensure TA ONLY mode is selected and all TA functions/elements are operative.

 

 

34-16-3

(O)Procedure to ensure all RA display/functions are operative.

 

 

34-19-1

(O)Procedure to ensure crew awareness of inoperative GPWS and alternate methods for ground proximity awareness.

 

 

34-19-1-a

(O)Procedure for crew awareness of inoperative mode(s) and alternate methods of operating without the inoperative mode(s).

 

 

34-19-1-d

(O)Procedure to establish alternate methods of operating without advisory callouts.

 

 

34-19-1-e

(O)Procedure to establish alternate method of operating without the windshear mode.

 

 

34-19-2

(O)Procedure for crew awareness of inoperative FLTA / PDA and alternate method for terrain awareness.

 

 

34-19

C

(O)Procedure to verify Test Mode is functional with crew awareness of which modes are operative / inoperative.  Establish alternate methods to operate without affected modes.(e.g., TAWS, GPWS modes, Windshear, FLTA/PDA, as applicable)

 

 

34-21

(O)Procedure to establish alternate method of operating without the Multifunction Display (MFD).

 

 

34-24-1&2

(O)Procedure to operate with expired Navigation Databases.

 

 

35-2

(M) Procedure to use the oxygen pressure gauge in the cockpit during servicing.

 

 

35-3

(M)Procedure to prohibit oxygen flow from affected outlet.

 

 

 

 

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DATE: 02/07/2006

PAGE NO:

XVI

Guidelines for (O) & (M) Procedures

 

 

37-1

(O)Procedure to insure Left and Right Instrument Air Sources are operative prior to each departure.

 

 

37-2

(O)Procedure to verify inoperative valve is in the closed position.

 

 

37-3

(O)Procedure to ensure L&R Instrument Air Sources are operative and all provisos are complies with prior to each flight.

 

(O)Procedure to ensure L&R Instrument Air Sources are operative and all provisos are complies with prior to each flight.

 

 

38-1

(M)Procedure to deactivate the affected components and ensure there are no leaks.

 

 

 

(M) Procedure to drain and ensure the system is not serviced.

 

 

38-2

(M)Procedure to deactivate the affected components and ensure there are no leaks.

 

(M) Procedure to deactivate the associated components to prevent leaks and to placard the Lavatory Door.

 

 

52-4

(O) Procedure to manually lower the Main Cabin Door in such a manner as to prevent personal injury and aircraft damage.

 

 

52-6

(M) Procedure to remove Cargo Door Snubber and Placard Cargo Door near the handle to warn ground personnel that the CDS is inoperative.

 

 

56-1

(O)Procedure to ensure that AFM Limitations are complied with.

 

 

56-2

(O)Procedure to ensure that AFM Limitations are complied with.

 

 

73-1

(O)Procedure to determine inoperative condition is not caused by

 

a leak or broken fuel line.

 

 

 

DEPARTMENT OF TRANSPORTATION

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AIRCRAFT: HAWKER BEECHCRAFT

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REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

21-1

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Air Cycle Air Conditioning System

C

1

0

May be inoperative for unpressurized flight provided the Environmental Bleed Air Valves are closed.

 

 

 

 

 

 

 

 

2.

Vapor Cycle Air Conditioning System

C

1

0

 

 

 

 

 

 

 

 

 

3.

L or R BL AIR FAIL Annunciator System

 

 

 

 

 

 

 

 

 

 

 

 

1)

Annunciator fails to illuminate

B

2

1

(O) One may be inoperative provided:

a)          Environmental and Instrument Bleed Air Valves on inoperative side are verified closed before each flight, and

b)          Aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

2)

Annunciator remains illuminated

B

2

1

(O) One may be illuminated provided:

a)          Environmental and Instrument Bleed Air Valves on inoperative side are verified closed before each flight, and

b)          Aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

4.

L or R ENVIR FAIL Annunciator Systems

C

2

1

(O) One may be inoperative provided Environmental Bleed Air Valve on inoperative side is closed.

 

 

 

 

 

 

 

 

 

 

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REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

21-2

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

5.

CABIN ALT HI Annunciator System

C

1

0

(O) May be inoperative for pressurized flight:

a)          At or below 10,000 feet MSL, and

b)          Above 10,000 feet MSL up to and including 12,000 feet MSL for not more than 30 minutes.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative for unpressurized flight in accordance with FAR.

 

 

 

 

 

 

 

 

6.

Cabin Rate of Climb Indicator

C

1

0

May be inoperative for pressurized flight provided Differential Pressure/Cabin Altitude Indicator is operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative for unpressurized flight provided the dump valve is in the open position.

 

 

 

 

 

 

 

 

7.

Differential Pressure/Cabin Altitude Indicator

C

1

0

May be inoperative for unpressurized flight provided the dump valve is in the open position.

 

 

 

 

 

 

 

 

8.

Outflow/Safety Valves

C

2

0

(M) May be inoperative for unpressurized flight provided one valve is removed or secured in the open position.

 

 

 

 

 

 

 

 

 

 

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REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

21-3

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

9.

Pressurization System

C

1

0

(M) May be inoperative provided one Outflow/Safety valve is removed or secured in the open position.

 

 

 

 

 

 

 

 

1)

Maximum Pressure Differential Function

C

1

0

(O) May be inoperative, resulting in failure to achieve maximum pressure differential, provided:

a)          Available stabilized maximum differential must be known and considered for dispatch flight planning, and

b)          Cabin Altitude does not exceed 9,500 feet.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided flight remains at or below 10,000 feet MSL.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any available pressurization capability may be used provided system limits are not exceeded.

 

 

 

 

 

 

 

 

2)

Cabin Pressure Control Function

C

1

0

(O) May be inoperative, resulting in failure to pressurize at selected altitude, provided system can maintain cabin altitude at or below 9,500 feet.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any available pressurization capability may be used provided system limits are not exceeded.

 

 

 

 

 

 

 

 

3)

Cabin Rate Control Function

C

1

0

(O) May be inoperative, resulting in disagreement between selected rate and actual rate, provided system can maintain cabin altitude at or below 9,500 feet.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any available pressurization capability may be used provided system limits are not exceeded.

 

 

(Continued)

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

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PAGE NO:

21-4

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

9.

Pressurization System (Continued)

 

 

 

 

 

 

 

 

 

 

 

 

3)

Cabin Rate Control Function

C

1

0

(O) May be inoperative, resulting in fluctuations of rate indicator, provided:

a)          System can maintain cabin altitude at or below 9,500 feet, and

b)          Fluctuation cannot cause cabin pressure to exceed maximum differential.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any available pressurization capability may be used provided system limits are not exceeded.

 

 

 

 

 

 

 

 

4)

Cabin Pressure TEST Function

C

1

0

(O) May be inoperative provided system can maintain cabin altitude at or below 9,500 feet.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any available pressurization capability may be used provided system limits are not exceeded.

 

 

 

 

 

 

 

 

10.

Environmental Temperature Control

C

1

0

May be inoperative for unpressurized flight provided the Environmental Bleed Air Valves are closed.

 

 

 

 

 

 

 

 

1)

Automatic Function

C

1

0

May be inoperative provided the Manual Function is operative.

 

 

 

 

 

 

 

 

2)

Manual Function

C

1

0

May be inoperative provided the Automatic Function is operative.

 

 

 

 

 

 

 

 

 

 

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DATE: 02/07/2006

PAGE NO:

21-5

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

11.

Manual Temperature Control

 

 

 

DELETED Combined with Item 21-10

 

 

 

 

 

 

 

 

12.

Vent Blowers

C

2

0

 

 

 

 

 

 

 

 

 

13.

Cabin Temperature Gauge

C

1

0

 

 

 

 

 

 

 

 

 

14.

Environmental Bleed Air Systems

C

2

1

(O) One may be inoperative provided:

a)          Environmental Bleed Air Valve on inoperative side is closed, and

b)          ENVIR FAIL Annunciator is operative on operative Environmental Bleed Air System.

 

 

 

 

 

 

 

 

 

 

C

2

0

(O) May be inoperative for unpressurized flight provided all Environmental Bleed Air Valves are closed.

 

 

 

 

 

 

 

 

15.

Precooler and Bypass Valve Systems

 

 

 

DELETED Revision 1. Combined with Item 21-14.

 

 

 

 

 

 

 

 

 

16.

L or R ENVIR OFF Annunciator Systems

C

2

1

One may be inoperative.

 

 

 

 

 

 

 

 

17.

CAB DIFF HI Annunciator System

C

1

0

(O)

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

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REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

22-1

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. 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.

 

 

 

 

 

 

 

 

 

1)

Autopilot Disconnect

C

2

0

May be inoperative provided the autopilot is no utilized at less than initial approach altitude.

 

 

 

 

 

 

 

 

 

 

2.

Yaw Damper/Rudder Boost System

C

1

0

(O)(M)

 

 

 

 

 

 

 

 

1)

Rudder Boost Function Only

C

1

0

(O)

 

 

 

 

 

 

 

 

2)

Yaw Damper Function Only

C

1

0

(M)

 

 

 

 

 

 

 

 

3)

LEFT/RIGHT YAW DAMP Computers

C

2

1

One may be inoperative provided the operative computer is selected.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)

 

 

 

 

 

 

 

 

4)

***

Single YAW DAMP Computer

C

1

0

(M)

 

 

 

 

 

 

 

 

3.

Rudder Boost

 

 

 

DELETED Revision 1. Combined with Yaw Damper System.

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

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AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

23-1

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

1.  ***

Passenger Address System

 

 

 

 

 

 

 

 

 

 

 

 

1)

Passenger Carrying Operations

C

1

-

(O) May be inoperative provided:

a)          PA not required by FAR, and

b)          Alternate, normal and emergency procedures, and/or operating restrictions are established and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any station that operates normally may be used.

 

 

 

 

 

 

 

 

2)

Other Operations

D

1

0

May be inoperative unless procedures require its use.

 

 

 

 

 

 

 

 

2.  ***

Recorded Passenger Briefing Unit

D

-

0

 

 

 

 

 

 

 

 

 

3.

Static Discharge Wicks

C

-

17

Any combination of wicks may be missing or broken except:

a)          4 on each wing (includes aileron and winglet),

b)          3 on each side of horizontal stabilizer (includes tailet),

c)          1 on horizontal stabilizer aft bullet, and

d)          1 on each ventral fin.

 

 

 

 

 

 

 

 

4.

Communications Equipment (VHF, UHF)

D

-

-

Any in excess of those required by FAR may be inoperative provided it is not powered by an Emergency Power Supply and is not required for Emergency Procedures.

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

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AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

23-2

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

5.

Flight Deck Speakers

C

2

1

One may be inoperative.

 

 

 

 

 

 

 

 

 

 

C

2

0

May be inoperative provided an operative headset is used by each flight crewmember.

 

 

 

 

 

 

 

 

6.  ***

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)

Installed for an operator other than a holder of an Air Carrier or Commercial Operator certificate

A

1

0

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

 

 

 

 

 

 

 

 

 

 

 

7.  ***

GND COMM PWR System

D

1

0

 

 

 

 

 

 

 

 

 

8.

Crew Intercom System

B

1

0

May be inoperative for operations not using or requiring a second-in-command.

 

 

 

 

 

 

 

 

9.  ***

SELCAL/CALSEL Systems

C

1

0

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

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BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

23-3

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

10.

Push to Talk Switch (Radio)

 

 

 

 

 

 

 

 

 

 

 

 

1)

Aircraft equipped with separate hand held microphone plug-in (Second-in-command required)

C

2

1

One may be inoperative provided hand microphone on affected side is operative.

 

 

 

 

 

 

 

 

2)

Aircraft equipped with separate hand held microphone plug-in (Second-in-command not required)

C

2

1

Right side may be inoperative.

 

 

 

 

 

 

 

 

3)

Aircraft without separate hand held microphone plug-in (Second in command not required.)

C

2

1

Right side may be inoperative.

 

 

 

 

 

 

 

 

11. ***

Observers Headset Audio Jack

C

-

0

May be inoperative provided an alternate audio source is available.

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

23-4

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

12. ***

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 system operates normally,

b)          Alternate procedures are established and used

c)          SATCOM coverage is available over the intended route of flight, and

d)          Prior coordination with the appropriate ATC facility is required when Inmarsat codes for SATCOM Voice are not available.

 

NOTE: SATCOM is to be used only as a backup to normal HF communications unless otherwise authorized by the appropriate ATC facilities.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

24-1

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

24

ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

 

1.

AC VOLT/FREQ. Meter

 

 

 

DELETED Revision 1.

 

 

 

 

 

 

 

 

2.

L or R DC GEN Annunciator System

B

2

1

One may be inoperative provided:

a)          Both DC LOAD meters are operative,

b)          Both Generator Bus Ties are operative, and

c)          Both L and R GEN TIE OPEN Annunciator Systems are operative.

 

 

 

 

 

 

 

 

3.

DC LOAD Meters

B

2

1

(O) One may be inoperative provided:

a)          Electrical load is maintained within the capacity of one generator at all times.

b)          Both L and R DC GEN Annunciator Systems are operative and

c)          Aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

4.

Inverters

B

2

1

One may be inoperative for day VFR provided:

a)          No passengers are carried, and

b)          Both L and R AC Bus Annunciator Systems are operative.

 

 

 

 

 

 

 

 

5.

L or R AC BUS Annunciator System

B

2

0

May be inoperative provided:

a)          Both Inverters are operative, and

b)          AC VOLT/FREQ Meter is operative.

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

24-2

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

24

ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

 

6.

External Power System

C

1

0

(M)

 

 

 

 

 

 

 

 

7.

EXTERNAL POWER Annunciator System

C

1

0

(O)

 

 

 

 

 

 

 

 

8.

Generator Bus Tie

B

2

1

One may be inoperative for day VMC provided both DC GEN Annunciators are operative.

 

 

 

 

 

 

 

 

9.

L or R GEN TIE OPEN Annunciator Systems

B

2

0

(O) May be inoperative provided:

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

b)          Both DC Gen Annunciators are operative.

 

 

 

 

 

 

 

 

 

10.

AC VOLT/FREQ Meter Frequency select button

C

1

0

May be missing or broken provided frequency information can be obtained from the Meter.

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

25-1

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

25

EQUIPMENT/ FURNISHING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Passenger Seat(s)

C

-

0

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) is blocked and placarded “DO NOT OCCUPY”.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: A seat with an inoperative seat belt is considered to be inoperative.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Affected seat(s) may include the seat(s) behind and/or adjacent to the outboard seats.

 

 

 

 

 

 

 

 

1)

Recline Mechanism

C

-

-

May be inoperative and seat occupied provided seat is secure in the upright position.

 

 

 

 

 

 

 

 

2)

Underseat Baggage Restraining Bars

C

-

-

(O) May be inoperative provided:

a)          Baggage is not stowed under seat with inoperative restraining bar,

b)          Associated seat is placarded “DO NOT STOW BAGGAGE UNDER THIS SEAT”, and

c)          Procedures are established to alert crew of inoperative restraining bar.

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

25-2

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

1.

Passenger Seat(s) (Continued)

 

 

 

 

 

3)

Armrest

C

-

-

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 upright position.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

4)

Forward Observer Seat

C

-

0

May be inoperative provided:

a)          Another forward passenger seat is made available to the Administrator for the performance of official duties, and

b)          An audio source is available.

 

 

 

 

 

 

 

 

2.  ***

Emergency Locator Transmitter (ELT) System

C

1

0

(M)As required by FAR.

 

 

 

 

C

1

0

(M)May be inoperative for published scheduled flights in scheduled air carrier service.

 

 

 

 

 

 

 

 

3.

ELT Remote Switch

 

 

 

DELETED Combined with ELT System, Revision 5

|

|

 

 

 

 

 

 

 

4.  ***

Passenger Convenience Items

(Expires December 31, 2007)

 

 

 

 

 

 

(Continued)

 

-

-

Passenger convenience items, as expressed in this MMEL, are those related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ashtrays, stereo equipment, overhead reading lamps, etc. Items addressed elsewhere in this document shall not be included. (M) and (O) procedures may be required and included in the air carrier’s appropriate document.

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

25-3

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

4.

Passenger Convenience Items           (Continued)

 

 

 

NOTE: Exterior lavatory door ash trays are not considered convenience items

 

 

 

 

 

 

 

 

 

4.

***

Non-Essential Equipment & Furnishings (NEF)

(Before or after December 31, 2007)

 

-

-

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.

 

 

 

 

 

 

 

 

 

5.

Emergency Medical Equipment

D

-

-

Any in excess of those required by FAR may be incomplete or missing provided required distribution is maintained.

 

 

 

 

 

 

 

 

6.

Flotation Devices

D

-

-

Any in excess of those required by FAR may be inoperative or missing provided required distribution is maintained.

 

 

 

 

 

 

 

 

7.  ***

Flashlight/Flashlight Assembly

D

-

-

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

 

 

 

 

 

 

 

 

8.

Cockpit Overhead Crew Assist Straps

D

-

-

May be inoperative or missing.

 

 

 

 

 

 

 

 

9.

Cockpit Sun Visors

C

2

0

May be inoperative or missing provided there are no visual restrictions to the flight crew.

 

 

 

 

 

 

 

 

10.

Crew Seat Adjustment

A

-

0

(M) May be inoperative provided:

a)          Seat(s) are locked in a position that permits normal pilot visibility,

b)          Full flight control movement is available,

c)          Position of seat is acceptable to the flight crew,

d)          Crew Rudder Pedal Adjustment is operative, and

e)          Repairs are made within one flight day.

 

 

 

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT: HAWKER BEECHCRAFT

BE-1900D

REVISION NO: 5

DATE: 02/07/2006

PAGE NO:

25-4

 

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

11.

Crew Arm Rests

C

-

0

May be inoperative provided arm rest is secured in the upright position.

 

 

 

 

 

 

 

 

12.

Flightdeck Doors /

Security Barrier

C

-

0

May be inoperative provided door is secured open or does not block nor impede egress to exit.