15

Revision:

Date: 03/01/2007

DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

BRITISH AEROSPACE JETSTREAM 3101

BRITISH AEROSPACE JETSTREAM 3201

Doug Edwards

Chairman, Flight Operations Evaluation Board

(FOEB)

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

Telephone:

FAX:

(816)-329-3233

(816)-329-3241

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

I

TABLE OF CONTENTS

SYSTEM

SYSTEM NO.

PAGE NO.

Table of Contents

Log of Revisions

I

II, III

Control Page

Highlights of Change

IV, V,VI

VII, VIII, IX, X

Definitions

-- Definitions

XI, XII, XIII, XIV

XV, XVI, XVII

-- Definitions

-- Preamble

XVIII, XIX

XX, XXI

Guidelines for (O) & (M) Procedures Guidelines for (O) & (M) Procedures

XXII, XXIII, XXIV

XXV, XXVI, XXVII

Guidelines for (O) & (M) Procedures Air Conditioning

XXVIII

1, 2, 3, 4

Auto Flight

Communications

1 THRU 6

24 Electrical Power

Equipment/Furnishings

Fire Protection

1 THRU 12

, 2, 3

Flight Controls

Fuel

1, 2

, 2

Hydraulic Power

Ice and Rain Protection

1, 2, 3

1, 2

Indicating/Recording Systems

Landing Gear

Lights

Navigation

, 2, 3, 4

1 THRU 15

Oxygen

Water/Waste

1, 2

Doors

Wings

Propellers

Engine/Fuel Controls

Ignition

Engine Controls

1, 2

Engine Oil

Water Injection

DEPARTMENT OF TRANSPORTATION

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

II

Log of Revisions

Rev No.

Date

Page Numbers

Initials

ORIGINAL 06/27/1983

1 03/23/1984 COMPLETE REVISION

ALL

2 06/06/1985 21-5 AND 82-1

3 02/18/1986 76-1

03/16/1987

5 07/20/1988 23-1, 33-2

2, 33-1, 33-2, 23-1, 33-2

6 11/10/1988 COMPLETE REVISION

02/19/1989

COMPLETE REVISION to add ABC repair interval.

06/22/1989

8 06/22/1989

HIGHLIGHTS OF REV., DEFINITIONS

PREAMBLE

05/01/1991

05/01/1991

HIGHLIGHTS OF REV., DEFINITIONS

1, 24-1, 24-2

9a

9a 08/07/1991 52-1, 76-1

08/07/1991

HIGHLIGHTS OF REV.

9b

9b 02/06/1992 33-2

02/06/1992

HIGHLIGHTS OF REV.

06/02/1992

06/02/1992

HIGHLIGHTS OF REV., GUIDELINES

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

06/02/1992

06/02/1992

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

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

06/02/1992

06/02/1992

5, 26-1, 27-1, 27-2, 28-1

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

06/02/1992

06/02/1992

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

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

06/02/1992

06/02/1992

1, 52-1, 61-1, 73-1, 74-1

2, 76-1, 79-1, 82-1

12/14/1992

12/14/1992

HIGHLIGHTS OF REV., GUIDELINES

1, 27-2, 52-1, 52-2

a

a 01/21/1994 34-3, 34-5

01/21/1994

HIGHLIGHTS OF REV., DEFINITIONS

b

b 01/28/1994 34-3, 34-5

01/28/1994

HIGHLIGHTS OF REV.

03/13/1995

12 03/13/1995

HIGHLIGHTS OF REV., DEFINITIONS

GUIDELINES

03/13/1995

03/13/1995

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

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

03/13/1995

03/13/1995

1, 25-2, 25-3, 25-4, 25-5

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

03/13/1995

03/13/1995

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

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

03/13/1995

03/13/1995

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

6, 35-1, 52-1, 52-2, 57-1

DEPARTMENT OF TRANSPORTATION

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

III

Log of Revisions

Rev No.

Date

Page Numbers

Initials

03/13/1995

03/13/1995

1, 73-1, 74-1, 74-2, 76-1

1, 82-1,

07/24/1995

07/24/1995

HIGHLIGHTS OF REV., DEFINITIONS

2, 33-3, 33-4, 34-1, 57-1

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a 12/14/1995

12/14/1995

HIGHLIGHTS OF REV., DEFINITIONS

GUIDELINES

a 12/14/1995

b

05/22/1998

HIGHLIGHTS OF REV., DEFINITIONS

GUIDELINES

b 05/22/1998

b

05/22/1998

1, 34-4, 34-5, 35-1

HIGHLIGHTS OF REV., DEFINITIONS

09/27/2000

14 09/27/2000

GUIDELINES

09/27/2000

09/27/2000

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

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

09/27/2000

09/27/2000

1, 25-2, 25-3, 25-4, 25-5

1, 27-2, 31-1, 33-1, 33-2

09/27/2000

09/27/2000

3, 33-4, 34-1, 34-2, 34-3

4, 34-5, 34-6, 35-1, 52-1

03/01/2007

15 03/01/2007

HIGHLIGHTS OF REV., DEFINITIONS

PREAMBLE, GUIDELINES

03/01/2007

03/01/2007

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

5, 23-6, 25-1, 25-2, 25-3

03/01/2007

03/01/2007

4, 25-5, 25-6, 25-7, 25-8

9, 25-10, 25-11, 25-12

03/01/2007

03/01/2007

1, 26-2, 26-3, 31-1, 31-2

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

03/01/2007

03/01/2007

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

, 34-11, 34-12, 34-13

03/01/2007

15 03/01/2007

, 34-15, 35-1, 38-1

DEPARTMENT OF TRANSPORTATION

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

IV

Control Page

System

Page No.

Rev. No.

Current Date

Cover Page

Table of Contents

/01/2007

/01/2007

I

II

Log of Revisions

/01/2007

III 15 03/01/2007

Control Page

IV

V 15

/01/2007

/01/2007

VI 15

VII

/01/2007

/01/2007

Highlights of Change

VIII

IX

/01/2007

/01/2007

X

Definitions XI

/01/2007

/12/2006

XII 10

XIII 10 05/12/2006

/12/2006

XIV 10

XV 10

/12/2006

/12/2006

XVI 10

XVII

/12/2006

/12/2006

XVIII

XIX

/12/2006

/12/2006

Preamble XX 2 06/14/1989

XXI 2 06/14/1989

Guidelines for (O) & (M) Procedures

XXII

XXIII

/01/2007

/01/2007

XXIV

XXV 15 03/01/2007

/01/2007

XXVI

XXVII 15 03/01/2007

15 03/01/2007

XXVIII 15 03/01/2007

/27/2000

21 21-1

/27/2000

/27/2000

/27/2000

/01/2007

22 22-1

23 23-1

/01/2007

/01/2007

/01/2007

/01/2007

/01/2007

/01/2007

24 24-1

/13/1995

DEPARTMENT OF TRANSPORTATION

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

V

Control Page

System

Page No.

Rev. No.

Current Date

Control Page (continued)

25 25-1 15 03/01/2007             5 03/01/2007 5 03/01/2007 5 03/01/2007             5 03/01/2007 5 03/01/2007 5 03/01/2007             5 03/01/2007 5         03/01/2007 10 15         03/01/2007 11 15         03/01/2007 12 15 03/01/2007 26 26-1 15 03/01/2007 5 03/01/2007 5 03/01/2007 27 27-1           14 09/27/2000 4 09/27/2000 28 28-1 12 03/13/1995 2 03/13/1995 29 29-1 12 03/13/1995 30 30-1 12 03/13/1995             2 03/13/1995 2 03/13/1995 31 31-1 15 03/01/2007 5 03/01/2007 32 32-1 12 03/15/1995 33 33-1 15 03/01/2007             4 09/27/2000 4 09/27/2000 4 09/27/2000 34 34-1 15 03/01/2007             4 09/27/2000 5 03/01/2007 5 03/01/2007             5 03/01/2007 5                                                                                   03/01/2007

DEPARTMENT OF TRANSPORTATION

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 AND 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

VI

Control Page

System

Page No.

Rev. No.

Current Date

Control Page (Continued)

(continued)

/01/2007

/01/2007

/01/2007

/01/2007

0 15

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/01/2007

/01/2007

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/01/2007

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/01/2007

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/27/2000

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/13/1995

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/13/1995

DEPARTMENT OF TRANSPORTATION

  23-14

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

VII

HIGHLIGHTS OF CHANGE

Definitions

Updated in accordance with Policy Letter 25, Global Change 142.

Guidelines

[(O) &(M)]

Updated IAW applicable Policy Letter Provisos and/or Industry requests.

ATA 22-1-1,

1-2 & 1-3

Autopilot relief updated to conform to PL-101 (GC-103).

ATA 22-4

Auto Pilot Disconnect relief added per PL-93.

ATA 23-1

HF removed from this item IAW PL-95 (GC-111) and put in ATA .  [Separate HF item required for HF relief to comply with

PL-106 (GC-135)].

ATA 23-1-1

Item changed to comply with PL 95 R1 (GC-111).

ATA 23-2-1

Changed to comply with PL-09 (GC-119).

ATA 23-2-2

Changed to comply with PL-09 (GC-119).

ATA 23-7 &

7-1, -2, & -3

Cockpit Voice Recorder relief updated to comply with PL-29 (GC-128).

ATA 23-8

(All)

Boom Microphone relief updated to comply with PL-58 (GC-100).

ATA 23-9

& 9-1

Selective Call Systems relief updated to comply with PL-117 (GC-137).

ATA 23-13

Electronic Checklist relief added.

ATA 23-14

HF relief updated to comply with PL-106 (GC-135).

ATA 23-15

ELT relief relocated to Item 23-15 and updated to comply with PL- 120 (GC-147).

ATA 25-2 &

2-1 & -2

Repair category changed to comply with PL-79 (GC-134).

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

VIII

HIGHLIGHTS OF CHANGE

ATA 25-2-3

Armrest relief added IAW PL-79 (GC-134).

ATA 25-5 &

5-1 & -2

Passenger Convenience Items and Non-Essential Equipment & Furnishings (NEF) updated to comply with PL-116 (GC-138).

ATA 25-6

ELT relief relocated to Item 23-15 to comply with PL-120 (GC-147).

ATA 25-7-1

Observer Seat relief updated IAW PL-56 (GC-127).

ATA 25-8-1

Flight Attendant Seat(s) relief updated IAW PL-97 (GC-124).

ATA 25-8-2

Flight Attendant Seat(s) relief updated IAW PL-97 (GC-124).

ATA 25-8-3

Flight Attendant Seat(s) relief updated IAW PL-97 (GC-124).

ATA 25-10

Lavatory relief moved to ATA 38-2.

ATA 25-15

-1, -2 & -3

Emergency Medical Equipment updated IAW PL-73 (GC-144).

ATA 25-17

& 17-1 & -2

Exterior Lavatory Door Ashtray relief updated IAW PL-85 (GC-80).

ATA 25-18

Galley Waste Receptacles Access Doors/Covers relief added to comply with PL-96 (GC-98).

ATA 25-19

Cabin and Galley Storage Compartments and Closets relief added to comply with PL-104 (GC-129).

ATA 25-20

Seat Belt Sign relief added to comply with PL-89.

ATA 25-21

Cargo Restraint Systems relief added to comply with PL-100 (GC-114).

ATA 26-4

Cargo Compartment Fire Detection/Suppression System(s) relief added IAW PL-102 (GC-77).

ATA 26-5

Lavatory Fire Extinguisher System relief added IAW PL-24 (GC-106).

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

IX

HIGHLIGHTS OF CHANGE

ATA-26-6

Lavatory Smoke Detection System added to comply with PL-24 (GC-106).

ATA 31-3

3-1, -2 & -3

Flight Data Recorder relief updated to comply with PL-87 (GC-136).

ATA 33-1

Title changed to comply with PL-77 (GC-63).

ATA 33-3

Wing Illumination Light relief updated to comply with PL-72 (GC-54).

ATA 34-3

& 3-1

Transponder relief updated IAW PL-76 (GC-133).

ATA 34-13

Distance Measuring Equipment (DME) relief updated IAW PL-03.

ATA 34-14

Standby Attitude Indicator relief updated IAW PL-111.

ATA 34-17

Altitude Alerting System relief updated to comply with PL-39.

ATA 34-20

“O” (Operations procedure required) added to the provisos to comply with PL-10.

ATA 34-21

Relief updated to comply with PL-32 (GC-145) for TCAS I.

ATA 34-22 &

22-1 through -5

Relief updated to comply with PL-32 (GC-145) for TCAS II.

ATA 34-23

(All)

GPWS/TAWS relief updated IAW PL-54 (GC-139).

ATA 34-25

Windshear Warning and Flight Guidance System (required by FAR) relief added to comply with PL-67 (GC-140).

ATA 34-26

Windshear Detection and Avoidance System (required by FAR) relief added to comply with PL-67 (GC-140).

ATA 34-27

Windshear Warning and Flight Guidance System (not required by FAR) relief added IAW PL-67 (GC-140).

DEPARTMENT OF TRANSPORTATION

  30-1

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

X

HIGHLIGHTS OF CHANGE

ATA 34-28

Windshear Detection and Avoidance System (not required by FAR) relief added IAW PL-67 (GC-140).

ATA 34-29 &

29-1 PL-98 (GC-71).

Flight Management System Navigation Databases updated IAW

ATA 34-30 &

Navigation Management System Navigation Databases updated IAW PL-98 (GC-71).

ATA 34-31 &

31-1 through -5

Automatic Dependent Surveillance-Broadcast (ADS-B) System

relief added to comply with PL-67 (GC-140).

ATA 34-32

Relief added for Multifunction Display (MFD).

ATA 34-33

Relief added for Multifunction Display Cooling Fan.

ATA 34-34

Relief added for GPS Switching Unit Base (both provisos).

ATA 35-6

Protective Breathing Equipment relief added to comply with PL-

ATA 38-1

Relief added for Potable Water System in accordance with PL-83 (GC-108).

ATA 38-2

Relief added for Lavatory Waste System in accordance with PL-83 (GC-108).

DEPARTMENT OF TRANSPORTATION

  c.

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.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 11

DATE: 09/11/2006

PAGE NO:

XI

DEFINITIONS

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.

   "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.

    "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.

DEPARTMENT OF TRANSPORTATION

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 11

DATE: 09/11/2006

PAGE NO:

XII

DEFINITIONS

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.

"Federal Aviation Regulations" (FAR) means the applicable portions of the Federal

Aviation Act and Federal Aviation Regulations.

    "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.

0. "Icing Conditions" means an atmospheric environment that may cause ice to form on

the aircraft (structural) or in the engine(s) (induction).

1. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that

must be complied with for operation with the listed item inoperative.

  2. ”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).

  3. ”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.

  4. 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).

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DEFINITIONS

  5. "(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.

. "(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.

  7. "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.

8. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from

filing an Instrument Flight Rules (IFR) flight plan.

    . "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.

  0. "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.

  1. "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.

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DEFINITIONS

  2. 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

6th, the three day interval would begin at midnight the 26th and end at midnight the

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

6th, 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.

. 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.

BOEING (B-757/767, B-747-400, B-777)

Boeing airplanes equipped with Engine Indicating and Crew Alerting Systems (EICAS) provide different priority levels of system messages (WARNING, CAUTION, ADVISORY, STATUS and MAINTENANCE).  Any messages that affects airplane dispatch status will be displayed at a STATUS message level or higher. The absence of an EICAS STATUS or higher level (WARNING, CAUTION, ADVISORY) indicates that the system/component is operating within its approved operating limits or tolerances.

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DEFINITIONS

System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program.

b. Boeing (B-717, MD-10, MD-11)

These aircraft are equipped with an alerting function which is a subsystem within the Electronic Instrument System (EIS). The alerting function provides various levels of system condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and STATUS)

Alerts that affect aircraft dispatch will include WARNING, CAUTION, STATUS or MAINTENANCE level. MAINTENANCE alerts are displayed on the status page of the EIS display panel under the maintenance heading.

A MAINTENANCE alert on the EIS indicates the presence of a system fault which can be identified by the Central Fault Display System (CFDS) interrogation. The systems are designed to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be verified for dispatch purposes.

c. AIRBUS (A-300-600, A-310, A-318/320/319/321, A-330, A-340)

Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system condition messages (WARNING, CAUTION, STATUS, and ADVISORY). A-318/320/319/ 321, A-330, and A-340 also provide MAINTENANCE status messages.

Any message that affects airplane dispatchability will normally be at the WARNING, CAUTION or STATUS level. MAINTENANCE messages (A-318/319/320/321, A-330, and A-340 only) are also indicated on ECAM Status Page below the white Maintenance label.

A MAINTENANCE status (Class II) message on ECAM indicates the presence of a system fault which can be identified by CFDS (A-318/319/320/321) or CMS (A-330/A- interrogation. The systems are designed to be fault tolerant. For A- 18/319/320/321, MAINTENANCE STATUS (Class II) do not affect dispatch but are

listed in the MMEL. Dispatch is allowed without specific conditions except for:

-  BLUE RSVR MAINTENANCE status:  If applicable, and

-  AIR BLEED MAINTENANCE status: As applicable.

For the A-330 and A-340, MAINTENANCE status messages do not affect dispatch.

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;

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MAINTENANCE status (Class II)

however for any

message, the A-320/319/321 MEL must be verified for dispatch capability.

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d. FOKKER(FK-100) ¶

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DEFINITIONS

d.  FOKKER (FK-100)

Fokker aircraft are equipped with Multi Function Display System (MFDS) which provides electronic message referring to the different priority levels of system information (WARNING (red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any messages that affects aircraft dispatch will be at the WARNING, CAUTION or AWARENESS level. In these cases the MEL must be verified for dispatch capability and maintenance may be required.

System conditions that only require maintenance are not ¦presented on the flight deck. These maintenance indications/messages may be presented on the Maintenance & Test Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by dedicated Built in Test Evaluation (BITE) of systems.

CANADAIR (CL-65, CL-604)

Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAAS) provide four classes of messages (WARNING, CAUTION, ADVISORY, and STATUS). Any message that affects aircraft dispatch will be at the WARNING, CAUTION, or STATUS level.

System conditions that only require maintenance are not visible to the flight crew.  These maintenance indications/messages are only activated by maintenance personnel using the Maintenance Diagnostics Computer.

EMBRAER (EMB-135/145, ERJ-170/190 Series)

The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew Alerting System (EICAS) that provides three different message levels:  WARNING, CAUTION, and ADVISORY.  The ERJ-170/190 Series add STATUS messages.

Failures that effect dispatchability are presented to the flight crew at one of these levels. Other failures may be presented only to the maintenance personnel on the Multi Function Display (MFD) maintenance pages or through the download of the Central Maintenance Computer (CMC). System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program.

Deleted:

equipped with Multi Function Display

Fokker aircraft are

System (MFDS) which provides electronic message referring to the different priority levels of system information (WARNING (red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white).Any messages that affects aircraft dispatch will be at the WARNING, CAUTION or AWARENESS level. In these cases the MEL must be verified for dispatch capability and maintenance may be required.¶ Section Break (Next Page)

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DEPARTMENT OF TRANSPORTATION

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DEFINITIONS

GULFSTREAM (G-IV, G-V, GV-SP, and GIV-X)

Gulfstream airplanes equipped with EICAS provide different priority levels of system messages:  WARNING (red), CAUTION (amber), ADVISORY, STATUS and MAINTENANCE (cyan or blue).  Any WARNING or CAUTION message affects airplane dispatch status and requires that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  STATUS messages which indicate a system failure (e.g., FMS-1 fail) require that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  Maintenance messages do not affect airplane dispatch status. They indicate the presence of a system fault which can be identified by Maintenance Data Acquisition Unit (MDAU on the G-V) interrogation, Central Maintenance Computer (CMC on the GV-SP/GIV-X) interrogation or by reference to the Airplane Flight Manual.

h.  De-  HAVILLAND (DASH 8 SERIES 400)

Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all cautions and warnings.  Advisory messages are displayed by the Electronic Indication System (EIS) or individual advisory lights supplied in the cockpit.

“Class 1 failures” are failures that prevent continued operation of a specific Line Replacement Unit or channel and are annunciated via advisory messages:  caution, warning or advisory lights in the flight compartment. Dispatch with such posted failures are to be in accordance with the MMEL.

“Class 2 failures” are failures which do not prevent continued system function.  These faults will not be annunciated to the flight crew and the absence of the higher level alert (warning, caution, advisory) indicates that the system/component is operating within its approved operating limits or tolerances.  Such faults would be evident during maintenance interrogation performed during maintenance activities.  Class 2 faults do not affect dispatch and will be listed in the Fault Isolation Manual (FIM).  Class 2 faults will be left to the discretion of the operators when these faults are to be rectified.

  4. "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.

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DEPARTMENT OF TRANSPORTATION

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DEFINITIONS

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.

6. "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

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.

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DEFINITIONS

  0. 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.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 2

DATE: 06/14/1989

PAGE NO:

XX

PREAMBLE

(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.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

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AIRCRAFT:

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REVISION: 2

DATE: 06/14/1989

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PREAMBLE

(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

DEPARTMENT OF TRANSPORTATION

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(M)

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(M)

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Guidelines for (O) & (M) Procedures

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

Maintenance procedure to ensure that no electrical or mechanical fault exists which would have an adverse effect on any other System.

Maintenance procedure to ensure the failed Valve is in the CLOSED/OFF position.

Maintenance procedure to ensure the Discharge Valve or Safety Valve is secured OPEN.

Maintenance procedure to ensure no electrical or mechanical fault exists.

Maintenance procedure to ensure the Discharge Valve or Safety Valve is secured OPEN.

Maintenance procedure to ensure the Discharge Valve or Safety Valve is secured OPEN.

Maintenance procedure to inspect Ground Heater to ensure no electrical or mechanical fault exists which would have an adverse effect on any other System.

Maintenance procedure to inspect Main Wheel Bay to ensure Air Conditioning Duct System integrity.

Maintenance procedure to ensure no electrical or mechanical fault exists which could have an adverse effect on any Flight Control function.

Maintenance procedure to ensure no electrical or mechanical fault exists which could have an adverse effect on any Flight Control function.

Maintenance procedure to ensure no electrical or mechanical fault exists which could have an adverse effect on any Flight Control function.

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(O)

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(O)

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Guidelines for (O) & (M) Procedures

Maintenance procedure to ensure no electrical or mechanical fault exists which could have an adverse effect on any Flight Control function.

Operations procedure to ensure appropriate briefings are provided to the passengers.  (Applies to both provisos.)

Operations procedure to ensure appropriate briefings are provided to the passengers.

Operations procedure to ensure procedures do not require SELCAL and alternate procedures are established and used when the SELCAL System is inoperative.

Operations procedure to ensure procedures do not require SELCAL and alternate procedures are established and used when the SELCAL System is inoperative.

Operations procedure to obtain information normally provided through the ACARS Printer.

Operations procedure to obtain information normally provided through the ACARS Printer.

Operations procedure to ensure SATCOM or Data Link operates normally, alternate procedures are established and used, SATCOM coverage is available over the intended route of flight and prior coordination with the appropriate ATS facility is conducted if Inmarsat codes are not available while using SATCOM Voice.

Operations procedure to ensure both Inverters are operative.

Operations procedure to alert Cabin Crew of inoperative Restraining Bar.

Maintenance procedure to ensure folding type Seat is stowed or secured in the RETRACTED position.

Operations procedure to ensure Flight Attendant occupies the most appropriate Seat to fulfill his/her duties.

DEPARTMENT OF TRANSPORTATION

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Guidelines for (O) & (M) Procedures

Maintenance procedure to ensure a folding type Seat is stowed or secured in the RETRACTED position.

Operations procedure to isolate Lavatory Electrical System from Aircraft Electrical System (pulling Circuit Breaker is acceptable and secure Lavatory Door Latch (taping the Door Latch is acceptable).

Operations procedure to ensure Automatic External Defibrillator (AED) is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit.

Operations procedure to ensure Emergency Medical Kit (EMK) is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit.

Operations procedure to ensure First Aid Kit (FAK) is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit.

Maintenance procedure to ensure Seat is locked in the appropriate position.

Maintenance procedure to ensure Container is EMPTY and Access  Door is SECURED to prevent waste introduction into the Compartment.

Operations procedure to ensure procedures are established to ensure sufficient Galley Waste Receptacles are available to accommodate all waste that may be generated on a flight.

Maintenance procedure to ensure Galley Storage Compartments and Closets are secured CLOSED.

Maintenance procedure to ensure cargo loading limits from an approved source are observed.

Maintenance procedure to ensure Lavatory Door is locked CLOSED and placarded “INOPERATIVE – DO NOT ENTER”.

Operations procedure to ensure Lavatory Waste Receptacle is EMPTY and Lavatory is used only by crewmembers.

DEPARTMENT OF TRANSPORTATION

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(O)

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(O)

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(M)

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(M)

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(O)

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Guidelines for (O) & (M) Procedures

Maintenance procedure to ensure Lavatory Door is locked CLOSED and placarded “INOPERATIVE – DO NOT ENTER”.

Operations procedure to ensure Lavatory Waste Receptacle is empty and the Lavatory is used only by crewmembers.

Maintenance procedure to ensure Flight Control functions are not adversely affected.

Maintenance procedure to isolate Electric Trim Servo and ensure Flight Controls are not adversely affected.

Operations procedure to determine fuel on board meets regulatory requirements for the intended flight.

Operations procedure to ensure a satisfactory field of vision is available to the crew.

Operations procedure to verify the Engine Anti-Ice System is operative.

Operations procedure to record elapsed flight time.

Maintenance procedure to verify the Normal Brake Accumulator is checked.

Maintenance procedure to deactivate the Fluorescent Lighting System and ensure specific follow-up action is performed in accordance with the applicable AD.

Operations procedure to ensure ground deicing procedures do not require the use of Wing Illumination Lights.

Operations procedure to ensure Autopilot with Altitude Hold is operative and enroute operations do not require use of the Altitude Alerting System.

Operations procedures to determine, prior to departure, items required in the provisos operate normally and Positive Radar Control can be maintained by ATC on the enroute portion of the flight.  (Applies to all provisos.)

DEPARTMENT OF TRANSPORTATION

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(M)

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(O)

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(O)

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(O)

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A-

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A-

(O)

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A-

(O)

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(O)

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B-

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(O)

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Guidelines for (O) & (M) Procedures

Maintenance procedure to ensure TCAS Unit is deactivated and secured.  (Applies to both provisos.)

Maintenance procedure to ensure TCAS Unit is deactivated and secured.  (Applies to both provisos.)

Operations procedures established to ensure the non-flying pilot monitors the pilot’s display, TA ONLY mode on the Resolution Advisory (RA) Display System is selected and all TA functions/elements are operative.

Operations procedure to ensure all RA display and audio functions are operative.

Operations procedure to establish and ensure use of alternate procedures.

1(a)

Operations procedure to establish and ensure use of alternate procedures.

1(d)

Operations procedure to establish and ensure use of alternate procedures.  (Applies to both provisos.)

1(e)

Operations procedure to establish and ensure use of alternate procedures.  (Applies to both provisos.)

Operations procedure to establish and use alternate procedures.

Operations procedure to establish and use alternate procedures.

1(a)

Operations procedure to establish and use alternate procedures.

1(d)

Operations procedure to establish and use alternate procedures. (Applies to both provisos.)

1(e)

Operations procedure to establish and use alternate procedures.

Operations procedure to establish and use alternate procedures.

Operations procedure to establish and use alternate procedures. (Applies to both provisos.)

Operations procedure to establish and use alternate procedures. (Applies to both provisos.)

DEPARTMENT OF TRANSPORTATION

  34-

27

(O)

34-

28

(O)

34-

29

-1

(O)

34-

30

-1

(O)

34-

32

(O)

34-

33

(O)

34-

34

(O)

(O)

35-

3

(M)

38-

1

(M)

(M)

38-

2

(M)

(M)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

XXVII

Guidelines for (O) & (M) Procedures

Operations procedure to establish and use alternate procedures.

Operations procedure to establish and use alternate procedures.

Operations procedure established to ensure use of current aeronautical charts, status of facilities used to define route of flight verified suitable and Radios are manually tuned and identified.

Operations procedure established to ensure use of current aeronautical charts, status of facilities used to define route of flight verified suitable and Radios are manually tuned and identified.

Operations procedure to ensure alternate procedures are used and the MFD Circuit Breaker is pulled and collared.

Operations procedure to ensure the MFD is considered inoperative and the MFD Fan Circuit Breaker is pulled and collared.

Operations procedure to ensure GPS is not used for navigation and the Captain’s Switching Unit Circuit Breaker is pulled and collared.

Operations procedure to ensure Captain’s GPS Switching Unit is operational and the First Officer’s Switching Unit Circuit Breaker is pulled and collared.

Maintenance procedure to ensure Flight Deck Gauge is operative. This procedure should also ensure the person charging the Oxygen  System is continuously aware of the pressure reading of the Flight Deck Gauge.

Maintenance procedure to ensure components are deactivated or isolated and System has no leaks.

Maintenance procedure to ensure System is drained and not serviced.

Maintenance procedure to ensure components are deactivated or isolated and System has no leaks.

Maintenance procedure to ensure components are deactivated or isolated, the Pilot-In-Command determines the flight duration is acceptable with Lavatory unusable and the Door is secured CLOSED and placarded.

DEPARTMENT OF TRANSPORTATION

  52-

1

(O)

52-

4

(M)

52-

6

(O)

74-

2

(O)

79-

1

(O)

79-

3

(M)

(O)

(M)

(O)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION: 15

DATE: 03/01/2007

PAGE NO:

XXVIII

Guidelines for (O) & (M) Procedures

Operations procedure for flight crew members to confirm by visual inspection that the Door is latched prior to departure.

Maintenance procedure to secure Cargo Bay Door.

Operations procedure to ensure the Door is supported externally and only one passenger is on the Door at a time.

Operations procedure to ensure Continuous Ignition is operative.

Operations procedure to verify proper Oil Cooler Flap operation prior to departure.

Maintenance procedure to deactivate the System.

Operations procedure to ensure AFM limitations and performance are complied with.

Maintenance procedure to deactivate the System.

Operations procedure to ensure AFM limitations are complied with.

DEPARTMENT OF TRANSPORTATION

  21

-1

1.

2

1

2.

2

1

a)

b)

c)

3.

4

2

4.

1

0

5.

1

0

1

0

a)

c)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION NO: 14

DATE:  09/27/2000

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

Air Conditioning Group

C

(M) One may be inoperative provided the opposite side System provides adequate heating and cooling.

Flow Control Valves

C

(M) One may be inoperative provided:

Components of the opposite side System provide adequate heating, cooling and pressurization,

Failed Valve is in CLOSED/OFF

position and

Cabin Altitude Warning Caption

is operative.

Temperature Controllers

(Automatic and Manual)

C

May be inoperative provided one Temperature Controller (Automatic or Manual) is operative on each side.

Recirculation Fan

C

Cabin Differential

Pressure Indicator

C

May be inoperative for unpressurized

flight.

C

May be inoperative for pressurized flight provided:

Cabin Altitude Indicator is

operative,

b) Cabin Altitude Warning System

is operative and

A Cabin Altitude Conversion Chart is available to the Cockpit Crew in flight.

DEPARTMENT OF TRANSPORTATION

  21

-2

6.

1

0

1

0

a)

c)

7.

1

0

1

0

b)

c)

8.

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION NO: 14

DATE: 09/27/2000

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

Cabin Altitude Indicator

C

May be inoperative for unpressurized

flight.

C

May be inoperative for pressurized flight provided:

Cabin Differential Pressure

Indicator is operative,

b) Cabin Altitude Warning System

is operative and

A Cabin Altitude Conversion Chart is available to the Cockpit Crew in flight.

Cabin Altitude Warning

Caption

C

May be inoperative for unpressurized

flight.

C

May be inoperative for pressurized flight provided:

a)  Aircraft is operated at or below 10,000 feet MSL,

Cabin Differential Pressure Indicator is operative and Cabin Altitude Indicator is operative.

Cabin Pressure/Rate of

Change Indicator

C

May be inoperative for unpressurized

flight.

C

May be inoperative for pressurized flight provided all other Pressurization Indicating and Warning Systems are operative.

DEPARTMENT OF TRANSPORTATION

  21

-3

9.

1

0

1

0

a)

b)

1

0

1

0

1

0

a)

11

1

0

1

0

13

.

***

14

.

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION NO: 14

DATE: 09/27/2000

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

Pressurization Controller

(Automatic Function)

C

May be inoperative for unpressurized flight provided the Discharge Valve or Safety Valve is OPEN.

C

May be inoperative for pressurized flight provided:

Pressurization can be adjusted using the Manual System and All other Pressurization Indicating and Warning Systems are operative.

. Manual Pressurization

Control (Rotating Knob)

C

May be inoperative for unpressurized

flight.

C

May be inoperative for pressurized flight provided:

Automatic function of the Pressurization Controller is operative and

b)  All other Pressurization

Indicating and Warning Systems

are operative.

. Pressurization Dump

Control (Toggle Switch)

C

(M) May be inoperative for unpressurized flight provided the Discharge Valve or Safety Valve is secured OPEN.

12.  Absolute Air Pressure

Regulator

C

May be inoperative for unpressurized

flight.

Freon Air Conditioner

System

D

1 0 (M)

Discharge Valve

C

(M) May be inoperative for unpressurized flight provided the Discharge Valve or Safety Valve is secured OPEN.

DEPARTMENT OF TRANSPORTATION

  21

-4

21

15

.

1

0

16

.

17

18

***

1

0

(M)

19

. O

2

1

20

.

2

1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION NO: 14

DATE: 09/27/2000

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

AIR CONDITIONING

Safety Valve

C

(M) May be inoperative for unpressurized flight provided the Discharge Valve or Safety Valve is secured OPEN.

Cabin Punka Louvres

DELETED REVISION 12.

NOTE:  These are considered Passenger Convenience Items.

. Cabin Temperature

Indicator

C

1 0

Cabin Ground Heater

D

  ver Temperature Caption (Main Wheel Bay)

C

(M) One may be inoperative provided:

a) Associated Air Conditioning

Group is selected OFF and

b)  Opposite side provides adequate heating and cooling.

Duct Over Temp Caption

C

(M) One may be inoperative provided:

a) Associated Air Conditioning

Group is selected OFF and

b)  Opposite side provides adequate heating and cooling.

DEPARTMENT OF TRANSPORTATION

  22

-1

1.

1

1

0

2

-

-

1

0

3)

-

0

2.

***

1

0

3.

***

4.

2

1

a)

2

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

BAE 3101 and 3201

REVISION NO: 15

DATE: 03/01/2007

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

22 AUTO FLIGHT

Autopilot

|

) Transport Category

Aircraft With Only One

Autopilot Installed

B

(M) As required by FAR.

|

|

|

) Transport Category

Aircraft With Two or More

Autopilots Installed

C

B

(M) As required by FAR.

|

|

|

|

Non Transport Category

Aircraft

C

May be inoperative provided operations

do not require its use.

|

|

Yaw Damper (As a

Component of Autopilot)

C

(M) May be inoperative provided Autopilot is OFF.

Yaw Damper (Not a

Component of Autopilot)

C

1 0 (M)

Autopilot Disconnect Functions (Quick Release Controls)

C

One may be inoperative provided:

Autopilot is not used below

1,500 feet AGL and

b)  Approach minimums do not

require the use of the Autopilot.

|

|

|

|

|

B

May be inoperative provided Autopilot is not used.

|

|

DEPARTMENT OF TRANSPORTATION

  23

-1

2

3

1.

-

-

-

0

c)

-

2

-

2

2.