Revision: 32

Date: 10/12/1990

DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

BAC 1-11

All Models

Federal Aviation Administration Flight Standards Division Seattle       Aircraft Evaluation Group                     SEA-AEG

1601 Lind Ave. S.W.

Renton, Washington 98057-4056

Telephone

FAX

(425) 917-6625

(425) 917-6638

  --

--

--

--

--

21

22-1

24

25

26

27

28

28-6

29

30

31-1

32

33

34

36-1

38-1

49

49-1

52-1

73

73-1

74-1

77-1

78-1

79-1

80-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 32

DATE:10/12/1990

PAGE NO.

I

TABLE OF CONTENTS

SYSTEM

SYSTEM NO.

PAGE NO.

Table of Contents

Log of Revisions

I

II

Control Page

Highlights of Change

III, IV

V

Definitions

-- Definitions

VI, VII, VIII

IX, X

-- Preamble

XI, XII

21-1, 2, 3, 4

Air Conditioning

22 Auto Flight

23 Communications

23-1, 2

24-1, 2, 3

Electrical Power

Equipment/Furnishings

25-1, 2, 3

26-1, 2, 3

Fire Protection

Flight Controls

27-1, 2, 3

28-1, 2, 3, 4, 5

Fuel

28 Fuel

Hydraulic Power

Ice and Rain Protection

29-1, 2

30-1, 2, 3

31 Indicating/Recording Systems

Landing Gear

32-1, 2

33-1, 2, 3, 4, 5

Lights

Navigation

34-1, 2, 3, 4

35-1, 2

35 Oxygen

36 Pneumatic

38 Water/Waste

Airborne Auxiliary Power

52 Doors

Engine Fuel & Control

74 Ignition

77 Engine Indicating 78 Engine Exhaust 79 Engine Oil

80 Starting

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION: 32

DATE:10/12/1990

PAGE NO:

II

Log of Revisions

Rev No.

Date

Page Numbers

Initials

32 10/12/1990 ALL PAGES

U.S. DEPARTMENT OF TRANSPORTATION

  -

32

32

32

32

32

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11

REVISION: 32

DATE:10/12/1990

PAGE NO:

III

Control Page

System

Page No.

Rev. No.

Current Date

Cover Page

Table of Contents

10/12/1990

10/12/1990

I

II

Log of Revisions

Control Page

10/12/1990

10/12/1990

III

IV 32 10/12/1990

Highlights of Change

Definitions VI 3 10/02/1989

V

10/12/1990

VII 3 10/02/1989

VIII 3 10/02/1989

IX

X

3 10/02/1989

3 10/02/1989

Preamble XI 2 06/14/1989 XII 2 06/14/1989 21 21-1 32 10/12/1990 21-2 32 10/12/1990 21-3 32           10/12/1990 21-4 32 10/12/1990 22 22-1 32 10/12/1990 23 23-1 32           10/12/1990 23-2 32 10/12/1990 24 24-1 32           10/12/1990 24-2 32           10/12/1990 24-3 32 10/12/1990 25 25-1 32           10/12/1990 25-2 32           10/12/1990 25-3 32 10/12/1990 26 26-1 32           10/12/1990 26-2 32           10/12/1990 26-3 32 10/12/1990 27 27-1 32           10/12/1990 27-2 32           10/12/1990 27-3 32 10/12/1990 28 28-1 32           10/12/1990 28-2 32           10/12/1990 28-3 32           10/12/1990 28-4 32           10/12/1990 28-5 32           10/12/1990 28-6 32 10/12/1990 29 29-1 32                                                                                               10/12/1990

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11

REVISION: 32

DATE:10/12/1990

PAGE NO:

IV

Control Page

System

Page No.

Rev. No.

Current Date

29-2 32 10/12/1990

30 30-1 32 10/12/1990

30-2 32 10/12/1990

30-3 32 10/12/1990

31 31-1 32 10/12/1990

32 32-1 32 10/12/1990

32-2 32 10/12/1990

33 33-1 32 10/12/1990

33-2 32 10/12/1990

33-3 32 10/12/1990

33-4 32 10/12/1990

33-5 32 10/12/1990

34 34-1 32 10/12/1990

34-2 32 10/12/1990

34-3 32 10/12/1990

34-4 32 10/12/1990

35 35-1 32 10/12/1990

35-2 32 10/12/1990

36 36-1 32 10/12/1990

38 38-1 32 10/12/1990

49 49-1 32 10/12/1990

52 52-1 32 10/12/1990

73 73-1 32 10/12/1990

74 74-1 32 10/12/1990

77 77-1 32 10/12/1990

78 78-1 32 10/12/1990

79 79-1 32 10/12/1990

80 80-1 32 10/12/1990

U.S. DEPARTMENT OF TRANSPORTATION

  25-7

28-8

28-9

28-12

28-14

28-17

28-18

28-19

28-20

35-2

35-3

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 32

DATE:10/12/1990

PAGE NO.

V

HIGHLIGHTS OF CHANGE

EFFECTIVE ABOVE DATE, The BAC-1-11 Master Minimum Equipment List has been revised. Please replace all pages of previous lists with Revision 32 for a complete up-to- date MMEL.

Retain this sheet with your MMEL until the next revision is issued.

24-4 Wording change

Added Passenger Convenience items.

28-4 Deleted

28-5 Deleted

Removed "If Installed"

Removed "If Installed"

28-10 Deleted

Added d) & e) Provisos

Added f), g) & h) Provisos

28-15 Deleted

Changed number required for dispatch Added STC 40, SA2971WE Proviso Added STC 40, SA2971WE Proviso Added STC 40, SA2971WE Proviso

30-3 Word correction

Removed "If Installed"

Word correction and removed "If Installed"

78-1 Word correction

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 3

DATE:10/02/1989

PAGE NO.

VI

DEFINITIONS

(Effective 10/02/1989)

1. System Definitions.

System numbers are based on the Air Transport Association (ATA) Specification Number 100 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.

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

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. Items installed that are in excess of the FAR requirements may be permitted by the operator's MEL to be inoperative if not otherwise required by the MMEL.

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 3

DATE:10/02/1989

PAGE NO.

VII

DEFINITIONS

(Effective 10/02/1989)

4."*" symbol in Column 4 indicates the listed item if inoperative, 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.

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

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 which has a type design approval for ER operations 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 or in the engine(s).

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.

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 3

DATE:10/02/1989

PAGE NO.

VIII

DEFINITIONS

(Effective 10/02/1989)

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.

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 3

DATE:10/02/1989

PAGE NO.

IX

DEFINITIONS

(Effective 10/02/1989)

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.

The letter designators are inserted adjacent to Column 2.

23. Engine Indicating Crew Alerting System (EICAS), Electronic Centralized Aircraft Monitoring System (ECAM) or similar systems that provide electronic messages refer to a system capable of providing different priority levels of systems information messages (e.g., Warning, Caution, Advisory Status and Maintenance).Any airplane discrepancy message that affects dispatchability will normally be at status message level (e.g., Advisory Status) or higher.

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.

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 3

DATE:10/02/1989

PAGE NO.

X

DEFINITIONS

(Effective 10/02/1989)

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 is 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 definition nor the use of this symbol provide authority to install or remove an item from an aircraft.

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 2

DATE:06/14/1989

PAGE NO.

XI

PREAMBLE

(Effective 06/14/1989)

The following is applicable for authorized certificate holders operating under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The FAR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety .A Master Minimum Equipment List (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 those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which take into consideration the operator's particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment.

Equipment not required by the operation being conducted and equipment in excess of FAR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained.

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment.

U.S. DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO. 2

DATE:06/14/1989

PAGE NO.

XII

PREAMBLE

(Effective 06/14/1989)

The MEL 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 Record/Logbook as prescribed by FAR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative.

When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by FAR. Such documentation is required prior to operation with any item of equipment inoperative.

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 interrelationships between those items and the effect on aircraft operation and crew workload will be considered.

Operators are 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

U.S. DEPARTMENT OF TRANSPORTATION

  21-1

1.

2

1

a)

b)

2

0

a)

b)

2.

2

0

3.

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

21 AIR CONDITIONING

Air Conditioning System

C

One may be inoperative provided:

The airplane remains at or below FL 250, and

|

Sufficient fuel is carried to permit continuation of flight from the most critical point to destination and alternate, or to a suitable airport at 10,000 feet MSL flight altitude.

C

(O) Both may be inoperative for unpressurized flight provided:

Ram air valve and Discharge (outflow) valve remains open, and The airplane remains at or below 10,000 feet MSL.

|

Flow Control and Shutoff

Valve (Master Valve)

C

(M) May be inoperative secured closed

provided the ram air valve operates

|

normally.

NOTE: A failed MAC valve must be closed.

Ram Air Valve

C

May be inoperative open provided the flight is conducted in an unpressurized

|

|

configuration.

|

C

May be inoperative closed provided both air conditioning and pneumatic systems

|

operate normally.

U.S. DEPARTMENT OF TRANSPORTATION

  21-2

4.

1

0

a)

b)

1

0

7.

1

0

.

8.

1

0

9.

1

0

a)

b)

c)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

21 AIR CONDITIONING

Radio Rack Cooling Fan

C 1 0

|

5. Discharge (Outflow)

Valve

C

May be inoperative open provided:

Flight is conducted in an unpressurized configuration, and Extended overwater flight is

|

|

|

prohibited.

|

6. Automatic Pressure

Control

C

May be inoperative provided the flight is conducted in an unpressurized

|

|

configuration.

|

Dump Valve Control

C

May be inoperative provided the airplane  | remains at or below 10,000 feet MSL

Discharge Valve Position

Indicator

C

May be inoperative provided the differential pressure gauge operates normally.

|

Suction Pump

C

(O) May be inoperative provided:

Discharge (outflow) valve remains fully open by manual control until after takeoff,

Cabin is depressurized, and Discharge valve is fully open by manual control before landing.

|

U.S. DEPARTMENT OF TRANSPORTATION

  21-3

1

0

1

0

1

0

a)

b)

1

0

a)

b)

c)

2

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

21 AIR CONDITIONING

10.  Safety Valve

C

May be inoperative provided the flight is conducted in an unpressurized

|

|

configuration.

|

11.  Cabin Altitude Warning

C

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

|

12. Cabin Differential

Pressure Indicator

C

C

May be inoperative provided:

The cabin altitude indicator

operates normally,

OR

The flight is conducted in an unpressurized configuration.

(O) May be inoperative provided:

|

|

|

|

|

13.  Cabin Altitude Indicator

C

C

Cabin differential pressure indicator operates normally, and A conversion chart is readily available to the flight crew,

OR

The flight is conducted in an unpressurized configuration.

|

|

|

|

|

|

|

14.  Cabin Rate of Climb Indicator

C 1 0

|

15.  Air Inlet Temperature

Indicators

C

May be inoperative provided temperature

control system operates normally in the

|

automatic mode.

U.S. DEPARTMENT OF TRANSPORTATION

  21-4

1

0

a)

b)

c)

d)

2

0

2

0

1

0

1

0

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

21 AIR CONDITIONING

16.  Heat Exchange Cooling

Fan

C

(O) May be inoperative provided:

Air conditioning system is not

used on the ground,

Both MAC valves are in the APU position,

The air delivery valve is turned off for takeoff, and

The air delivery valve is turned off for all flights at less than 165 KIAS.

|

|

|

|

17. Automatic Temperature

Control

C

(O) May be inoperative provided one manual control or one automatic control operates normally for each operating pack.

|

18. Manual Temperature

Control

C

(O) May be inoperative provided one manual control or one automatic control operates normally for each operating pack.

|

19. Temperature Valve

Position Indicator

1)  Cabin

C

May be inoperative provided cabin

temperature gauge operates normally.

|

|

2)  Flight Deck

C 1 0

|

20. Cabin Temperature

Indicator

C

May be inoperative provided:

Air inlet temperature gauge

operates normally, and

Cabin automatic temperature

control operates normally.

|

|

|

|

|

U.S. DEPARTMENT OF TRANSPORTATION

  22-1

1

0

3.

2

1

4.

1

0

5.

1

0

7.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

22 AUTO FLIGHT

1. Autopilot

C

|

NOTE: Any mode which functions

normally may be used.

2. Autopilot Disconnect

Light

C 2 1

|

|

Control Wheel Disengage

Switch

C

(O) One may be inoperative provided autopilot is not used at less than 1,500

|

feet AGL.

Glide Slope Annunciator

C

May be inoperative provided approach

minimums do not require autopilot use.

|

Torque Limiter Adapter (Autopilot Pitch Monitor System Installed)

C

May be inoperative provided autopilot is not used.

|

6. Yaw Damper

C 1 0

|

Air Data Sensor

C 1 0

|

U.S. DEPARTMENT OF TRANSPORTATION

  23-1

1

0

a)

b)

1

0

a)

b)

c)

d)

4.

12

5

-

-

6.

1

0

7.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

23 COMMUNICATIONS

1. Cockpit Interphone

System

Deleted, Rev. 32

|

2. Service Interphone System (Cockpit to Cabin) (Cabin to Cockpit) (Cockpit to Ground)

C

(O) May be inoperative provided:

Alternate, normal and emergency

procedures are established and

|

used, and

PA system operates normally.

3. Passenger Address

System

A

C

(O) May be inoperative provided: Alternate, normal, and emergency procedures are established and used,

Flight Deck/Cabin Interphone system operates normally, and Repair is made within 15 flight hours (domestic) or 25 flight

|

|

|

hours (international),

OR

All-cargo operations are being

conducted.

|

|

|

|

Static Discharge Wicks

C

May be damaged or missing provided a minimum of one on the outermost

|

extremity of each wing tip and tail plane tip remains.

5. Communications

Systems (VHF, HF, UHF)

C

As required by FAR.

|

Cockpit Voice Recorder

System (CVR)

B

May be inoperative provided Flight Data Recorder (FDR) operates normally.

|

Moved to 23-5

|

U.S. DEPARTMENT OF TRANSPORTATION

  23-2

8.

1

0

a)

b)

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

23 COMMUNICATIONS

Selective Call System

(SELCAL)

C 1 0

|

9. Flight Deck Speaker

System

C

Communications functions may be

inoperative provided:

Procedures do not require their

use, and

Headsets are installed and

operating normally.

|

10. Prerecorded Passenger

Announcement System

C

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

|

11.  ARINC Communications

***

Addressing and Reporting System (ACARS)

C 1 0

|

U.S. DEPARTMENT OF TRANSPORTATION

  24-1

2

1

a)

b)

c)

d)

e)

2.

1

0

3.

3

1

4.

1

1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

24 ELECTICAL POWER

1. Engine Driven

Generators (Including

CSD)

B

O) One may be inoperative provided:

The faulty generator CSDS is

|

disconnected following engine

start,

APU generator operates

normally, and is supplying power

to the bus,

A drain check of the left wing tank for freedom from water is made before dispatch,

Total planned flight time,

including diversion, does not

exceed 3.5 hours, and

The airplane remains at or below  | FL 300.

|

NOTE: The generator frequency meter

should remain selected to APU

position.

APU Generator

C

May be inoperative provided both engine  | generators are

operative.

|

KVA Meter (Engine and

APU)

C

One (of the two required generators) may be inoperative provided AC Voltmeter and

|

frequency meter indications for the

associated generator operate normally.

AC Voltmeter

C

Indication for one of the two required generators may be inoperative provided

|

KVA meter and frequency meter indications for the remaining generator operate normally.

U.S. DEPARTMENT OF TRANSPORTATION

  24-2

5.

1

1

6.

7.

2

1

a)

b)

9.

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

24 ELECTRICAL POWER

Frequency Meter

C

Indication for one of the two required generators may be inoperative provided KVA voltmeter and AC voltmeter indications for the remaining generator operate normally.

Static Inverter

Deleted, Rev. 32

|

Batteries

Deleted, Rev. 32

|

8. Transformer Rectifier

Ammeter

C

(M) One may be inoperative provided:              The associated TRU operates

|

|

normally, and

All other channel indicators

operate normally.

|

|

|

Battery Ammeter

C

May be inoperative provided the battery magnetic indicator operates properly.

10.  DC Voltmeter

Deleted, Rev. 32

|

11. Battery Magnetic

Indicator

C

May be inoperative provided the battery ammeter operates properly.

12. Transformer Rectifier

Unit

Deleted, Rev. 32

|

|

13.  AC Bus Fail Warning Light

Deleted, Rev. 32

|

|

14.  DC Bus Fail Warning Light

Deleted, Rev. 32

|

|

U.S. DEPARTMENT OF TRANSPORTATION

  24-3

2

1

a)

b)

c)

2

1

(M)

2

0

3

2

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

24 ELECTRICAL POWER

15. CSDS Low Pressure

Warning Lights

1)  Plessy Drive

C

(M) One may be inoperative provided:

At each Termination Check it is

|

verified that CSDS oil level is adequate, and that no evidence of oil leakage exists,

After starting the associated engine it is verified that generator frequency is within the allowable range of 392-408 Hz at idle RPM, and

Voltage frequency selector remains on the associated system, except for periodic checks of the remaining generator output.

2)  Airesearch Drive

C

|

C

(M) May be inoperative for inoperative generator(s).

|

|

16.  Generator Overheat

***

Warning Lights

C

May be inoperative for an associated inoperative generator.

|

|

U.S. DEPARTMENT OF TRANSPORTATION

  25-1

-

-

2.

-

-

3.

-

-

a)

b)

c)

d)

e)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

25 EQUIPMENT/

FURNISHINGS

1. Crewmember Shoulder

Harness (Flight Deck)

B

Any in excess of those required for flight deck crew members (including official

|

|

observer in forward observer seat) may be inoperative.

|

|

Megaphones

B

As required by FAR.

|

Flight Attendant Seat Assembly (Single or Dual Position)

C

(M) (O) One single or one dual position seat may be inoperative provided:

|

|

Affected seat position(s) is not

occupied,

|

|

Flight attendant(s) displaced by

inoperative seat position(s)

|

|

occupy the passenger seat(s)

most accessible to their assigned

|

|

exit,

Alternate procedures are established for displaced flight attendant(s),

|

|

|

Folding type seat is stowed or secured in the retracted position,

|

|

and

Passenger seat(s) assigned to flight attendant(s) is placarded: “FOR FLIGHT ATTENDANT USE

|

|

|

ONLY”.

|

|

|

NOTE 1: A folding seat that will not stow automatically is considered

|

|

inoperative.

NOTE 2: A seat position with an

inoperative or missing lap belt is considered inoperative.

|

|

|

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION

  25-2

3.

4.

-

-

-

-

-

-

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

25 EQUIPMENT/

FURNISHINGS

Flight Attendant Seat Assembly (Single or Dual Position) (Cont’d)

C

NOTE 3: The above provisos apply only to required flight attendant

|

|

seats. Seat positions in excess

of those required may be

|

|

inoperative provided they are

properly stowed or secured in

|

|

the retracted position. Individual

operators, when operating with

|

|

inoperative seats, will consider

the locations and combinations

|

|

of seats to ensure that the proximity to exits and distribution requirements of the applicable FAR are met.

|

|

|

|

“Fasted Seat Belt While Seated” Signs or Placards

C

One or more signs or placards may be illegible or missing provided a legible sign

|

|

or placard is readable from each occupied passenger seat.

|

|

5. Cabin Emergency Flashlight Holder/Flashlights

C

May be inoperative or missing provided the crewmember assigned to the affected

|

|

position has a normally operating

flashlight readily available.

|

|

6. Emergency Locator

Transmitter (ELT)

C

As required by FAR.

|

U.S. DEPARTMENT OF TRANSPORTATION

  25-3

-

0

8.

1

1

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

25 EQUIPMENT/

FURNISHINGS

7. Passenger Convenience

Item(s)

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, ash trays, 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.

NOTE: Lavatory door ash tray is not to be considered passenger

|

|

convenience items.

|

Forward observer seat

A

May be inoperative provided:

A passenger seat in the passenger cabin is made available to an FAA inspector for the performance of official duties, and

|

|

|

Operators are limited to not more than two flight days before repairs

|

|

are made.

|

|

|

|

U.S. DEPARTMENT OF TRANSPORTATION

  26-1

2.

3.

4.

1

0

6.

1

0

a)

b)

c)

d)

e)

8.

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

26 FIRE PROTECTION

1. Engine Overheat

Warning Lights (Zone 2)

(L.P. Cooling)

Deleted, Rev. 32.

|

Fire Extinguishers (Hand)

Deleted, Rev. 32.

|

Engine Firewall Shutoff

System

Deleted, Rev. 32.

|

APU Firewall Shutoff

System

C

May be inoperative provided APU is not used.

|

|

5. Engine Fire Extinguishing

System

Deleted, Rev. 32.

|

APU Fire Extinguishing

System

C

C

(O) May be inoperative provided:

APU is used for engine start only, It is continuously monitored by

|

the ground crew during operation, It is shut down immediately after engine start, and

No passengers are permitted in the aircraft during APU operation. OR

APU is not used.

7. Engine Fire Warning

System (Zone 1)

Deleted, Rev. 32.

|

APU Fire Warning

System

C

May be inoperative provided APU is not used.

|

U.S. DEPARTMENT OF TRANSPORTATION

  26-2

-

-

a)

b)

c)

d)

-

0

-

-

a)

b)

c)

d)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

26 FIRE PROTECTION

9. Lavatory Smoke

Detection Systems

C

(M) (O) for each lavatory, the lavatory smoke detection systems may be

|

inoperative provided:

Lavatory fire extinguisher system

operates normally.

OR

Lavatory waste receptacle is

C

empty,

Lavatory door is locked closed and placarded, “INOPERATIVE- DO NOT ENTER”, and

|

|

|

Lavatory is not used for any purpose.

|

|

|

|

C

May be inoperative for all cargo operations.

|

|

10. Lavatory Fire

Extinguisher System

C

M) (O) For each lavatory, the lavatory fire extinguisher may be inoperative provided:

|

Lavatory smoke detector system

operates normally.

OR

Lavatory waste receptacle is

C

empty,

Lavatory door is locked closed and placarded, “INOPERATIVE- DO NOT ENTER”, and

Lavatory is not used for any purpose.

NOTE 1: These provisos are not intended to prohibit lavatory inspection by crewmembers.

(Continued)

U.S. DEPARTMENT OF TRANSPORTATION

  26-3

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

26 FIRE PROTECTION

10. Lavatory Fire

Extinguisher System

(Cont’d)

NOTE 2: A lavatory fire extinguisher

system is not required for all- cargo operations.

|

|

|

U.S. DEPARTMENT OF TRANSPORTATION

  27-1

1.

2.

1

0

3.

2

1

a)

b)

4.

5.

6.

2

0

8.

9.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

27 FLIGHT CONTROLS

Feel Unit (Rudder and

Elevator)

Deleted, Rev. 32.

|

Tail Plane Indicator (TPI)

C

(M) May be inoperative provided a visual check is made to verify that the trim wheel

|

index correctly indicates horizontal

stabilizer position before each departure.

Flap Position Indicator

Pointers

C

(M) One pointer may be inoperative provided:

It is verified that the flaps operate normally throughout their full range, and

A visual inspection is made before each departure to verify that flaps are in the takeoff position, and that no asymmetry exists.

|

Flap Primary Shaft Fail

Caution Light

Deleted, Rev. 32

|

|

Flying Control Fail

Warning Lights

Deleted, Rev. 32

|

|

Lift Dumpers (400 series)

C

May be inoperative provided entire

system is deactivated.

|

NOTE: See AFM for related performance limitations.

7. Yaw Damper

C 1 0

Stall Warning Sensing

System

Deleted, Rev. 32.

|

Stick Shaker Motors

C 2 1

|

U.S. DEPARTMENT OF TRANSPORTATION

  27-2

1

0

1

0

2

1

a)

b)

2

1

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

27  FLIGHT CONTROLS

10. Stall Identification

Sensing (Stick Pusher)

C 2 1

|

11. Takeoff Configuration

Warning Horn

Deleted, Rev. 32

|

12.  H.P. Pressure Gauge

C

May be inoperative provided bottle pressure is verified adequate before each departure.

|

13.  L. P. Pressure Gauge

C

May be inoperative provided associated

low pressure warning light operates

|

normally.

14.  Stall WARNING Sensor

Heater Fail Lights

C

(M) One may be inoperative provided:

Sensor (vane) heaters operate

|

normally, and

The airplane is not operated in known or forecast icing conditions.

|

15.  Stall IDENT (Stick

Pusher) Heater Fail

Lights

C

(M) One may be inoperative provided:

Sensor (vane) heaters operate

|

normally, and

The airplane is not operated in known or forecast icing conditions.

16.  Stall WARNING & IDENT        Sensor (Vane) Lights

Deleted, Rev. 32

|

17. Klaxon

C 2 1

|

18.  Low Pressure Light

Emergency Elevator

System.

Deleted, Rev. 32

|

U.S. DEPARTMENT OF TRANSPORTATION

  27-3

1

0

1

0

a)

b)

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

27. FLIGHT CONTROLS

19.  Failure Light Emergency

Elevator System

Deleted, Rev. 32

|

20.  Electric Trim System

Deleted, Rev. 32

|

21.  Electric Trim System

Indicator

C

(M) May be inoperative provided trim tab is checked visually before each departure

|

to verify that it is in the faired position.

22. Elevator Damper

Engaged Light

C

(O) May be inoperative provided:

Before each departure, flight crew

shall perform a feel check of No.

|

1 elevator system to verify it is in the normal power mode, and

If gusty weather conditions exist, it is verified on the ground that the elevator gust damper is engaged.

23.  Mach Trim

C

May be inoperative provided AFM

Limitations are complied with.

|

U.S. DEPARTMENT OF TRANSPORTATION

  28-1

4

2

2.

2

0

3.

2

-

4.

5.

6.

2

-

a)

b)

7.

1

0

8.

1

0

9.

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

28 FUEL

1. Wing Tanks Booster

Pumps

C

(O) One boost pump per tank may be inoperative provided fuel dumping system

|

is not required.

Center Tank Booster

Pumps

C

May be inoperative provided use of center tank fuel is not required.

|

Transfer Valve

C

May be inoperative provided use of center tank fuel is not required.

|

Engine Low Pressure Warning Lights (Backing Pump)

Deleted, Rev. 32

|

Fuel Tank Boost Pump Low Pressure Warning Lights

Deleted, Rev. 32

|

Transfer Valve Magnetic

Indicator

C

C

May be inoperative provided:

If a wing tank quantity gauge is inoperative, the associated

|

transfer valve position indicator

operates normally,

OR

If use of center tank fuel is required, the transfer valve is secured OPEN.

|

|

|

Transfer Low Pressure

Light

C

(O) May be inoperative provided the center tank quantity gauge is monitored closely during flight.

|

Fuel Dumping System

C

(M) May be inoperative if deactivated in accordance with AFM Limitations.

|

Fuel Dump Valve and

Magnetic Indicators

C

(M) May be inoperative if deactivated in accordance with AFM Limitations.

|

U.S. DEPARTMENT OF TRANSPORTATION

  28-2

1

0

2

1

a)

b)

c)

d)

e)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

28 FUEL

10.  Fuel Crossfeed Valve

Deleted, Rev. 32

|

11.  Fuel Crossfeed Valve

Magnetic Indicator

C

May be inoperative provided fuel

crossfeed valve operates normally.

|

12.  Wing Tank Fuel Quantity Gauges

C

(M) (O) One may be inoperative provided: Fuel quantity is determined by

|

magnetic level indicator or other approved means before departure,

Fuel flow readings are logged, Procedures are established to assure that fuel flow is maintained essentially equal between engines,

With totalizers, a 5% excess reserve fuel quantity (over that otherwise required for the associated tank) is carried, and With no totalizers, a 10% excess reserve fuel quantity (over that

|

|

otherwise required for the

associated tank) is carried.

|

|

NOTE: Excess reserve fuel may be

distributed evenly between all

tanks in use.

13. Fuel Totalizer

C 1 0

|

U.S. DEPARTMENT OF TRANSPORTATION

  28-3

1

0

a)

b)

c)

d)

e)

f)

g)

h)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAC 1-11 All Models

REVISION NO: 32

DATE:  10/12/1990

PAGE NO:

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

1. SYSTEM,

SEQUENCE NUMBERS &

ITEM

28 FUEL

14.  Center Tank Fuel

Quantity Gauge

C

May be inoperative provided:

Fuel quantity is checked before

each flight by use of dripless

|

|

sticks,

All wing tank fuel quantity gauges operate normally,

Both fuel used counters operate

normally,

Both fuel flow gauges operate

normally, and

Airplane performance does not require fuel dumping for the en route engine out procedure. OR

Procedures are established to

C

C

assure that fuel in the affected tank will not be dumped below

|

the critical level for that flight.

OR

The tank remains empty (as verified by approved procedures). OR

A known quantity of fuel (as

|

C

verified by approved procedures)

is considered unusable, and is

|

computed as part of zero fuel weight.

15.  L/P Fuel Valve Magnetic Indicators

Deleted, Rev 32.

|

16. Fuel Temperature<