Revision:

14

 

Date: 09/16/2008

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON, D.C.

 

 

 

 

 

 

 

 

**************************************

For Part 91 Operations Only

**************************************

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

BEECHCRAFT MODEL 200 AND F-90

 

 

 

 

 

Applicable Models:

200 / 200C / 200CT / 200T / A100-1 / A200 / A200C / A200CT

B200 / B200C / B200CT / B200T / B200GT / B200CGT

and

F90

 

 

 

 

 

John A. Vetter

 

 

Chairman, Flight Operations Evaluation Board

(FOEB)

 

 

 

 

 

 

 

 

 

 

 

Federal Aviation Administration

 

 

Kansas City Aircraft Evaluation Group

 

 

DOT Building

 

 

901 Locust Street, Room 332

 

 

Kansas City, MO 64106-2641

 

 

 

 

 

 

 

 

Telephone:

(816)-329-3233

 

FAX:

(816)-329-3241

 

 

 

 

 

 


 

 

 

--

Table of Contents

I

--

Log of Revisions

II, III, IV

--

Control Page

V, VI, VII

--

Highlights of Change

VIII, IX, X

--

Definitions

XI THRU XVI

--

Preamble

XVII, XVIII

--

Guidelines for (O) & (M) Procedures

XIX THRU XXVI

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

 

 

 


 

 

 

 

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

 

 

 

 

 


 

 

 

 

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

 

 

 

 

 


 

 

 

 

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

 

 

 

 

 


 

 

 

 

Cover Page

-

14

09/16/2008

Table of Contents

I

14

09/16/2008

Log of Revisions

II

14

09/16/2008

 

III

14

09/16/2008

 

IV

14

09/16/2008

Control Page

V

14

09/16/2008

 

VI

14

09/16/2008

 

VII

14

09/16/2008

Highlights of Change

VIII

14

09/16/2008

 

IX

14

09/16/2008

 

X

14

09/16/2008

Definitions

XI

11

09/11/2006

 

XII

11

09/11/2006

 

XIII

11

09/11/2006

 

XIV

11

09/11/2006

 

XV

11

09/11/2006

 

XVI

11

09/11/2006

Preamble

XVII

1

07/05/1990

 

XVIII

1

07/05/1990

Guidelines for (O) & (M) Procedures

XIX

14

09/16/2008

 

XX

14

09/16/2008

 

XXI

14

09/16/2008

 

XXII

14

09/16/2008

 

XXIII

14

09/16/2008

 

XXIV

14

09/16/2008

 

XXV

14

09/16/2008

 

XXVI

14

09/16/2008

21

21-1

14

09/16/2008

 

21-2

14

09/16/2008

 

21-3

14

09/16/2008

22

22-1

14

09/16/2008

 

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

 

 

 

 


 

 

 

 

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

14

09/16/2008

 

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

 

 

 

 


 

 

 

 

35

35-1

14

09/16/2008

37

37-1

12

11/03/2003

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

 

 

 

 


 

 

Definitions

Updated in accordance with (IAW) Policy Letter 25 (PL-25).

Guidelines

[(O) & (M)]

Updated.

21-1,2,3,4,5 6,7,9,18,19

Add (O) procedure to configure and operate unpressurized.

21-4

Add “Cabin” to item description.

22-1

Note added for RVSM operations.

22-2

Change Yaw Damper relief format to comply with PL-31.

22-3

Autopilot Disconnect Switch relief revised to comply with PL-93 and address Emergency Procedures requirement for Trim Interrupt Switch.

22-4

Add (O) to develop alternate procedure.

22-5,6,7

Amend applicability for equipment versus serial number.

23-2

PA System relief category and wording revised IAW PL-09.

23-3&4

Combine relief to eliminate need for (M) procedure.

23-6

Change format of Boom Microphone relief to comply with PL-31 & PL-58.

23-7

CVR relief updated IAW PL-29 and format IAW PL-31

23-9

Add clarification to Item description and change to category D

23-10

HF relief changed to comply with PL-106.

23-15

Add “Push-to-Talk Switch” to Remarks.

23-16

SELCAL relief added per PL-117.

24-2,3,5

Revise applicability for GT serial numbers.

24-4

Delete relief for DC Load Meters because are need for Emergency and Abnormal Procedures IAW PL-63.

24-8

Add Remarks to EFIS Standby Power because it is essential to EFIS operation when it is installed.

24-11,12

Add “Caution Lights” to annunciator description in Remarks.

25-2

Passenger Seat relief  added IAW with PL-79.

25-4

Emergency Medical Equipment relief updated IAW PL-73.

25-5

Updated ELT relief IAW PL-120. Add relief for ELT Remote Switch.

25-6

PCI replaced with NEF relief IAW PL-116.

25-10

Removed “Galley” from Item Title to reflect aircraft configuration.

25-12

Cabin Storage Relief updated per PL-104.

25-13

Add “deactivated” to remarks IAW (M) procedure requirements.

25-15

Change Category for Pyrotechnic Signal & Number Required/Installed to “-“

25-16

Deleted PBE & relocate to Chapter 35 IAW PL-43.

25-18

Change Remarks wording to standard format and revise (M) procedure.

25-19

Change Number Required to “-“.

25-22

Moved Airspeed Bugs to Chapter 34 with Airspeed Indicators.

26-3

Deleted Lavatory Fire Extinguisher System. Not applicable to aircraft.

26-4

Deleted NOTE 2. Not applicable to aircraft.

27-1

Add (O) procedure for checking trim tab operation.

27-2

Add (O) procedure for checking Flap operation prior to each departure.

27-3

Change format IAW Pl-31 and MMEL consistency.

27-4

Change Remarks format and add deactivation of Electric Pitch Trim.

27-4-3

Add Remarks and (M) procedure to deactivate Electric Pitch Trim.


28-1

Add NOTE to see AFM Limitations, Revise Remarks to correlate to AFM Limitations and Procedures and add (M) to deactivate affected pump.

28-2 & 3

Deleted specific items and combined relief with Aux. Fuel Transfer System.

28-5

Add (M) procedure to ensure sending unit does not leak or obstruct flow.

28-6

Add requirement for operative Fuel Flow Indicators to Remarks.

28-7

Reformat Aux. Fuel Transfer Systems to combine relief in single item.

28-8

Move Fuel Flow Indicators to Chapter 73.

28-9

Add (M) procedure and change Remarks to account for next failure.

28-10

Delete Fuel Management Function due to lack of acceptable failure mode.

30-5-1

Add relief for Pitot Heat Annunciator

30-10-1-a

Correct format IAW PL-31 to remove NOTE and add applicability.

30-10-2-a

Correct format IAW PL-31 to remove NOTE and add applicability.

30-10-2-b

Remove model applicability because possible installation on all models

30-10-2-c

Add model applicability by serial number because of change in type design.

30-12

Add relief for Electric Inlet Boot Heaters.

31-3

Flight Data Recorder relief updated IAW PL-87.

31-4

Relocate Master Caution Annunciators from Chapter 33.

31-5

Relocate Master Warning Annunciators from Chapter 33.

31-6

Relocate Unassigned Annunciators from Chapter 33.

31-7

Add relief for Engine Trend Monitor systems.

32-3

Add number installed and number required to clarify applicability

32-5

Change Remarks to specify interval to check hydraulic oil level.

32-6

Change Remarks to include operative Down Lock Release Button.

33-1

Update Cabin Lighting System to establish minimum lighting.

33-9

Wing Ice Light(s) relief updated IAW PL-72 and AD for Wing Icing Lights.

33-12

Delete and relocate Master Caution Annunciators to Chapter 31.

33-14

Delete “NOTE: Refer to Item 33-3”.

33-15

Delete and relocate Master Warning Annunciators to Chapter 31.

33-16

Delete and relocate Unassigned Annunciators to Chapter 31.

34-1,2,3

Change applicability to specific configuration in Remarks and format Remarks to incorporate NOTE. Add RVSM NOTE to 34-1

34-4

Change applicability to equipment. Change Remarks and Add NOTE.

34-5

Change applicability to equipment. Remove relief for left side Heading Indicator to comply with PL-30.

34-6

Change Remarks for second relief to day VFR.

34-7

Update ATC Transponder relief IAW PL-76. Add RVSM NOTE.

34-8

Update Navigation descriptor to current available equipment.

34-10

Change applicability to equipment description.

34-10-1,2

Add (O) procedure for determining MPU is operative.

34-12

Change Flight Director Remarks to reference approach procedures.

34-13

Correct Radar Altimeter format and Remarks for affected systems. Add (M) and (O) Procedures.

34-16,17

Correct format IAW PL-31.

34-18

Add NOTE regarding RVSM.

 

 


 

 

34-19

Delete Speed Control Indicator due to lack of acceptable failure mode.

34-20-2

Corrected Remarks format IAW PL-31 and incorporate NOTE into Remarks

34-21

Add AHRS to Remarks.

34-22

TCAS II relief updated to comply with PL-32.

34-23

TCAS I relief updated to comply with PL-32.

34-24

Relief updated IAW PL-54 to incorporate TAWS.

34-27

Standby Attitude Indicator relief changed to comply with PL-111. Remove ***

34-29 & 30

Revise Navigation Database Remarks to account for RNAV terminal operations.

34-32

Change Moving Map Display relief to Independent Multi-Function Display to incorporate additional affected systems and functions.

34-33

Update Windshear IAW PL-67.

34-34

Update Windshear IAW PL-67.

34-36 & 37

Deleted due to variation in installation making applicability indefinable.

34-38

Deleted relief for PFD, aircraft limitations require both PFDs be operative.

35-1

Add NOTE to oxygen relief.

35-4

Protective Breathing Equipment relief added per PL-43.

46-1

Electronic Flight Bag and IFIS-5000 relief added.

52-1

Add passenger briefing to Remarks for Cabin Door Warning Light.

61-4

Correct applicability for autofeather and reformat remarks IAW PL-31

73-1

Add Chapter 73 with relief for Fuel Flow Indicators with (M) procedure.

77-1 & 2

Remove ***

79-1

Remove ***


 

1.  System Definitions.

 

System numbers are based on the Air Transport Association (ATA) Specification and items are numbered sequentially.

 

a.  "Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column.

 

b.  "Number Installed" (Column 2) is the number (quantity) of items normally installed in the aircraft.  This number represents the aircraft configuration considered in developing this MMEL.  Should the number be a variable (e.g., passenger cabin items) a number is not required.

 

c.  "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met.

 

NOTE:  Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator.

 

d.  "Remarks or Exceptions" (Column 4) in this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

 

e.  A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only.  The change bar is dropped at the next revision of that page.

 

2.  "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification Office.  The FAA approved AFM/RFM for the specific aircraft is listed on the applicable Type Certificate Data Sheet.

 

3.  "As required by FAR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules.  The number of items required by the FAR must be operative.  When the listed item is not required by FAR it may be inoperative for the time specified by repair category.  The term “14 CFR” may be substituted for “FAR” in MMELs or operator MELs.

 

4.  Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition.

 

NOTE:  To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be determined by the operator.


 

5.  "-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed.

 

6.  "Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft.

 

7.  "ER" refers to extended range operations of a two-engine airplane (ETOPS) which has a type design approval for ER operations (ETOPS) and complies with the provisions of Advisory Circular 120-42A.

 

8.  "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations.

 

9.  "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

 

10.  "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft (structural) or in the engine(s) (induction).

 

11.  Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for operation with the listed item inoperative.

 

12.  ”Inoperative" means a system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or tolerance(s).

 

13.  ”Notes:" in Column 4 provides additional information for crewmember or maintenance consideration.  Notes are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator of the responsibility for compliance with all applicable requirements.  Notes are not a part of the provisos.

 

14.  Inoperative components of an inoperative system:  Inoperative items which are components of a system which is inoperative are usually considered components directly associated with and having no other function than to support that system.  (Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MMEL).


 

15.  "(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative.  Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions.  Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel.  The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator.  Appropriate procedures are required to be published as part of the operator's manual or MEL.

 

16.  "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative.  Normally these procedures are accomplished by the flight crew however, other personnel may be qualified and authorized to perform certain functions.  The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the operator.  Appropriate procedures are required to be published as a part of the operator's manual or MEL.

 

NOTE:  The (M) and (O) symbols are required in the operator's MEL unless otherwise authorized by the Administrator.

 

17.  "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition for safe flight.  An acceptable method of securing or deactivating will be established by the operator.

 

18.  "Visual Flight Rules" (VFR) is as defined in FAR Part 91.  This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

 

19.  "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight.  This does not preclude operating under Instrument Flight Rules.

 

20.  "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

 

21.  "Passenger Convenience Items" means those items related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ash trays, stereo equipment, overhead reading lamps, etc.

 


 

22.  Repair Intervals:  All users of an MEL approved under FAR 121, 125, 129 and 135 must effect repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators:

 

Category A.  Items in this category shall be repaired within the time interval specified in the remarks column of the operator's approved MEL.

 

Category B.  Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook.  For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29th.

 

Category C.  Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook.  For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

 

Category D.  Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days (2880 hours), excluding the day the malfunction was recorded in the aircraft maintenance log and/or record.

 

The letter designators are inserted adjacent to Column 2.

 

23.  Electronic fault alerting system – General

 

New generation aircraft display system fault indications to the flight crew by use of computerized display systems.  Each aircraft manufacturer has incorporated individual design philosophies in determining the data that would be represented.  The following are customized definitions (specific to each manufacturer) to help determine the level of messages affecting the aircraft's dispatch status.  When preparing the MEL document, operators are to select the proper Definition No. 23 for their aircraft, if appropriate.

 

NO CUSTOMIZED DEFINITIONS OF FAULT ALERTING ARE APPLICABLE TO THE BEECH AIRCRAFT MODEL 200 / F90 AIRCRAFT.

 

24.  "Administrative control item" means an item listed by the operator in the MEL for tracking and informational purposes.  It may be added to an operator's MEL by approval of the Principal Operations Inspector provided no relief is granted, or provided conditions and limitations are contained in an approved document (i.e. Structural Repair Manual, airworthiness directive, etc.).  If relief other than that granted by an approved document is sought for an administrative control item, a request must be submitted to the Administrator.  If the request results in review and approval by the FOEB, the item becomes an MMEL item rather than an administrative control item.

 


 

25.  "***" symbol in Column 1 indicates an item which is not required by regulation but which may have been installed on some models of aircraft covered by this MMEL.  This item may be included on the operator's MEL after the approving office has determined that the item has been installed on one or more of the operator's aircraft.  The symbol, however, shall not be carried forward into the operator's MEL.  It should be noted that neither this policy nor the use of this symbol provide authority to install or remove an item from an aircraft.

 

26.  "Excess Items" means those items that have been installed that are redundant to the requirements of the FARs.

 

27.  "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance log and or record.  This day is excluded from the calendar days or flight days specified in the MMEL for the repair of an inoperative item of equipment.  This provision is applicable to all MMEL items, i.e., categories "A, B, C, and D."

 

28.  “Considered Inoperative”, as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative.  The item shall not be used or operated until the original deferred item is repaired.  Additional actions include:  documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repair category.

 

29.  “Is not used” in the provisos, remarks or exceptions for an MMEL item may specify that another item relieved in the MMEL “is not used”.  In such cases, crewmembers should not activate, actuate, or otherwise utilize that component or system under normal operations.  It is not necessary for the operators to accomplish the (M) procedures associated with the item.  However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crewmembers that a component or system is not to be used under normal operations.

 

 


 

30.  Nonessential equipment and furnishings (NEF) are those items installed on the aircraft as part of the original certification, supplemental type certificate, or engineering order that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules.  They are those items that if inoperative, damaged or missing have no effect on the aircraft’s ability to be operated safely under all operational conditions.  These nonessential items may be installed in areas including, but not limited to, the passenger compartment, flight deck area, service areas, cargo areas, crew rest areas, lavatories, and galley areas.  NEF items are not items already identified in the MEL or CDL of the applicable aircraft.  They do not include items that are functionally required to meet the certification rule or for compliance with any operational rule.  Operator’s NEF process shall not provide for deferral of items within serviceable limits identified in the manufacturer’s maintenance manual or operator’s approved maintenance program such as wear limits, fuel/hydraulic leak rates,

oil consumption, etc.  Cosmetic items that are fully serviceable but worn or soiled may be deferred under an operator’s NEF process.

 

 


 

This preamble is applicable to, and will be included in, master minimum equipment lists (MMEL) issued under the provisions of Section 91.30(a) [NEW Section 91.213(a)(2)].  It is not applicable to MMEL's issued under the provisions of Parts 121, 125, 129, and 135 of the FAR.

 

Except as provided in Section 91.30(d) [NEW Section 91.213(d)], or under the provisions of an approved MMEL, all equipment installed on an aircraft in compliance with the airworthiness standards or operating rules must be operative.  Experience has shown that with the various levels of redundancy designed into modern aircraft, operation of every system or component installed may not be necessary when the remaining equipment can provide an acceptable level of safety.

 

An MMEL is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public.  The FAA-approved MMEL includes only those items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations.  The MMEL and FAA-issued letter of authorization are used as an MEL by an operator and permit operation of the aircraft with inoperative equipment.

 

The MMEL includes all items of installed equipment that are permitted to be inoperative.  Equipment required by the FAR, and optional equipment in excess of FAR requirements, is included with appropriate conditions and limitations.  For each listed item, the installed equipment configuration considered to be normal for the aircraft is specified.  Items of equipment installed on aircraft (except for passenger convenience items such as galley equipment and passenger entertainment devices), such as "TCAS," windshear detection devices, and ground proximity warning systems (GPWS) that are in excess of what is required, and are not listed on the MMEL, must be operational for dispatch unless MMEL relief is sought through the FSDO having jurisdiction for the operator.  If MMEL relief is sought, the operator must notify the FSDO who will make a request of the FOEB to convene and consider adding the equipment to the MMEL.  The operator may then dispatch with the equipment disabled, or rendered inoperative, in accordance with all FAR.  It is incumbent on the operator to endeavor to determine if O and/or M procedures for that equipment must be developed.  If so, any procedures developed must comply with all FAR.  Procedures developed to use the MMEL must not conflict with either the aircraft flight manual limitations, emergency procedures, or with airworthiness directives (AD), all of which take precedence over the MMEL and those procedures.

 


 

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures, and other restrictions, as necessary, are required to be accomplished by the operator to ensure that an acceptable level of safety is maintained.  Those procedures should be developed from guidance provided in the manufacturer's aircraft flight and/or maintenance manuals, manufacturer's recommendations, engineering specifications, and other appropriate sources.  Procedures must not be contrary to any FAR.  Wherever the statement "as required by FAR" appears in the MMEL, the operator must either list the specific FAR by part and section and carry the FAR on board the aircraft or specify the requirements and/or limitations to conduct the flight in accordance with the appropriate FAR.

 

The MMEL is intended to permit operations with inoperative items of equipment for the minimum period of time necessary until repairs can be accomplished.  It is important that repairs be accomplished at the earliest opportunity in order to return the aircraft to its design level of safety and reliability.  Inoperative equipment in all cases must be repaired, or inspected and deferred, by qualified maintenance personnel at the next required inspection [Section 91.165(c), NEW Section 91.405(c)].  The repair intervals indicated by the Letters A, B, and C inserted adjacent to column 2 are NOT applicable to this MMEL.

 

The MMEL provides for release of the aircraft for flight with inoperative equipment.  When an item of equipment is discovered to be inoperative, it is reported by making an entry in the aircraft maintenance records.  The item is then either repaired or deferred per the MMEL or other approved means acceptable to the Administrator prior to further operation.  In addition to the specific MMEL conditions and limitations, determination by the operator that the aircraft is in condition for safe operations under anticipated flight conditions must be made for all items of inoperative equipment.  When these requirements are met, the aircraft may be considered airworthy and returned to service.  Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained.  When operating with multiple inoperative items, the interrelationship between those items, and the effect on aircraft operation and crew workload, must be considered.  Operators are expected to establish a controlled and sound repair program, including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

 

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.

 


 

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.

 

21-8

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

 

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.

 


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.


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.


 

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.


 

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.

 


 

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.

 


 

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.

 


 

35-3

 

(M) Maintenance procedure to block and placard affected Seat and to block flow of oxygen from the inoperative Mask.

 

37-2

(O) Operations procedure to verify inoperative Valve is 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.

 


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.

|

 

 

 

 

 

 

 


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)

C

2

1

(M) One may be inoperative in the INSTR AND ENVIR OFF position.

 

 

 

 

 

 

 

 

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

 

 

 

 

 

 

 

 

 


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

 

 

 

 

 

 

 

 

 


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

(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

 

 

|

|

|

|

 

 

 

 

 

 

 

 

 

B

-

0

May be inoperative provided:

a)      Autopilot is not used, and

b)      Second level switch trim interrupt function remains operative.

|

|

|

|

|

 

 

 

 

 

 

 

 

 

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.

|

|

|

|

|

|

|

 

 

 

 

 

 

 


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.

 

 

|

|

 

 

 

 

 

 

 


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