Date: 06/02/2004

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

M A S T E R   M I N I M U M   E Q U I P M E N T   L I S T

BRITISH AEROSPACE

BA-4100

/S/

       JAMES M. EITEL CHAIRMAN, FLIGHT OPERATIONS EVALUATION BOARD (FOEB)

Federal Aviation Administration

Flight Standards Division

SEATTLE AIRCRAFT EVALUATION GROUP

1601 Lind Ave. S.W.

RENTON, WASHINGTON  98055-4056

TELEPHONE: COMM: (425) 227-2280

FAX:  (425) 227-1270

DEPARTMENT OF TRANSPORTATION     Revision: 5

  Revision: 5

MASTER MINIMUM EQUIPMENT LIST      Date: 06/02/2004

BA-4100

Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II

--     Control Page                            III, IV, V

--     Highlights of Change                    VI, VII, VIII

--     Definitions                             IX, X, XI, XII

--     Definitions                             XIII, XIV, XV, XVI --     Preamble                                XVII, XVIII

21     Air Conditioning                        21-1, 2, 3, 4

22     Auto Flight                             22-1

23     Communications                          23-1, 2, 3, 4, 5 23     Communications                          23-6  THRU 10

23     Communications                          23-11  THRU 15 24     Electrical Power                        24-1, 2

25     Equipment/Furnishings                   25-1, 2, 3, 4, 5 25     Equipment/Furnishings                   25-6, 7, 8

26     Fire Protection                         26-1, 2, 3

27     Flight Controls                         27-1, 2

28     Fuel                                    28-1, 2

29     Hydraulic Power                         29-1

30     Ice and Rain Protection                 30-1, 2, 3, 4, 5 31     Indicating/Recording Systems            31-1, 2

32     Landing Gear                            32-1, 2

33     Lights                                  33-1, 2, 3, 4

34     Navigation                              34-1, 2, 3, 4, 5 34     Navigation                              34-6  THRU 10

35     Oxygen                                  35-1

38     Water/Waste                             38-1, 2 52     Doors                                   52-1, 2 61     Propellers                              61-1

73     Engine Fuel & Control                   73-1 74     Ignition                                74-1 76     Engine Controls                         76-1 77     Engine Indicating                       77-1 79     Engine Oil                              79-1 82     Water Injection                         82-1

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BA-4100

Log of Revisions

¦ REV.NO.  ¦  DATE      ¦ PAGE NUMBERS                   ¦ INITIALS  ¦

¦ 0a       ¦ 05/09/1994 ¦ HIGHLIGHTS OF REV.             ¦           ¦ ¦ 0a       ¦ 05/09/1994 ¦ 21-4                           ¦           ¦ ¦ 1        ¦ 07/08/1994 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 1        ¦ 07/08/1994 ¦ 21-4,23-2,24-1,24-2,25-1       ¦           ¦ ¦ 1        ¦ 07/08/1994 ¦ 25-2,25-3,33-3,34-2,34-7       ¦           ¦ ¦ 1        ¦ 07/08/1994 ¦ 52-1,79-1                      ¦           ¦ ¦ 2        ¦ 01/31/1995 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2        ¦ 01/31/1995 ¦ 21-1,21-4,22-1,23-2,25-4       ¦           ¦ ¦ 2        ¦ 01/31/1995 ¦ 29-1,30-2,31-1,32-1,34-1       ¦           ¦ ¦ 2        ¦ 01/31/1995 ¦ 52-1,61-1                      ¦           ¦ ¦ 3        ¦ 02/06/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 3        ¦ 02/06/1996 ¦ 21-4,23-3,25-4,25-5,26-2       ¦           ¦ ¦ 3        ¦ 02/06/1996 ¦ 28-2,29-1,30-1,30-2,33-1       ¦           ¦ ¦ 3        ¦ 02/06/1996 ¦ 34-2,52-1,77-1,82-1            ¦           ¦ ¦ 3a       ¦ 06/11/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 3a       ¦ 06/11/1996 ¦ 25-5,33-4                      ¦           ¦ ¦ 3b       ¦ 01/03/1997 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 3b       ¦ 01/03/1997 ¦ PREAMBLE                       ¦           ¦ ¦ 3b       ¦ 01/03/1997 ¦ 23-3,25-5                      ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ 21-3,21-4,22-1,23-1,23-2       ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ 23-3,23-4,23-5,23-6,25-1       ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ 25-2,25-3,25-4,25-5,25-6       ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ 25-7,25-8,26-1,26-2,26-3       ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ 31-1,31-2,34-1,34-2,34-3       ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ 34-4,34-5,34-6,34-7,34-8       ¦           ¦ ¦ 4        ¦ 01/22/2001 ¦ 34-9,35-1,38-1,38-2            ¦           ¦ ¦ 4a       ¦ 03/22/2001 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 4a       ¦ 03/22/2001 ¦ 23-6,25-2,26-1,26-3,34-10      ¦           ¦ ¦ 4a       ¦ 03/22/2001 ¦ 52-1,52-2                      ¦           ¦ ¦ 5        ¦            ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 5        ¦            ¦ 22-1,23-1,23-2,23-3,23-4       ¦           ¦ ¦ 5        ¦            ¦ 23-5,23-6,23-7,23-8,23-9       ¦           ¦ ¦ 5        ¦            ¦ 23-10,23-11,23-12,23-13,23-14  ¦           ¦ ¦ 5        ¦            ¦ 23-15,25-5,25-6,25-8,26-1      ¦           ¦ ¦ 5        ¦            ¦ 26-2,26-3,30-1,30-2,30-3       ¦           ¦ ¦ 5        ¦            ¦ 30-4,30-5,31-1,32-1,32-2       ¦           ¦ ¦ 5        ¦            ¦ 34-1,34-2,34-3,34-4,34-5       ¦           ¦ ¦ 5        ¦            ¦ 34-6,34-7,34-8,34-9,34-10      ¦           ¦ ¦ 5        ¦            ¦ 38-2                           ¦           ¦

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  FEDERAL AVIATION ADMINISTRATION     Page: III

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BA-4100

Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       5        06/02/2004 Table of Contents                        I       5        06/02/2004 Log of Revisions                         II      5        06/02/2004 Control Page                             III     5        06/02/2004 IV      5        06/02/2004 V       5        06/02/2004 Highlights of Change                     VI      5        06/02/2004 VII     5        06/02/2004 VIII    5        06/02/2004 Definitions                                    IX      6        01/31/1995 X       6         01/31/1995 XI      6        01/31/1995 XII     6        01/31/1995 XIII    6        01/31/1995 XIV     6        01/31/1995 XV      6        01/31/1995 XVI     6        01/31/1995 Preamble                                         XVII    2        06/14/1989 XVIII   2        06/14/1989 21                                       21-1    2         01/31/1995 21-2    ORIGINAL 05/27/1993 21-3    4        01/22/2001 21-4    4        01/22/2001 22                                       22-1    5        06/02/2004 23                                       23-1    5        06/02/2004 23-2    5        06/02/2004 23-3    5                06/02/2004 23-4    5        06/02/2004 23-5    5         06/02/2004 23-6    5        06/02/2004 23-7    5        06/02/2004 23-8    5        06/02/2004 23-9    5        06/02/2004 23-10   5                06/02/2004 23-11   5        06/02/2004 23-12   5         06/02/2004 23-13   5        06/02/2004 23-14   5        06/02/2004 23-15   5        06/02/2004 24                                                                                24-1    1        07/08/1994

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

                                         24-2    1        07/08/1994 25                                       25-1    4        01/22/2001 25-2    4 a      03/22/2001 25-3    4        01/22/2001 25-4    4        01/22/2001 25-5    5        06/02/2004 25-6    5        06/02/2004 25-7    4        01/22/2001 25-8    5        06/02/2004 26                                       26-1    5        06/02/2004 26-2    5        06/02/2004 26-3    5        06/02/2004 27                                       27-1    ORIGINAL 05/27/1993 27-2    ORIGINAL 05/27/1993 28                                       28-1    ORIGINAL 05/27/1993 28-2    3        02/06/1996 29                                       29-1    3        02/06/1996 30                                       30-1    5        06/02/2004 30-2    5        06/02/2004 30-3    5        06/02/2004 30-4    5        06/02/2004 30-5    5        06/02/2004 31                                       31-1    5        06/02/2004 31-2    4        01/22/2001 32                                       32-1    5        06/02/2004 32-2    5        06/02/2004 33                                       33-1    3        02/06/1996 33-2    ORIGINAL 05/27/1993 33-3    1        07/08/1994 33-4    3 a      06/11/1996 34                                       34-1    5        06/02/2004 34-2    5        06/02/2004 34-3    5        06/02/2004 34-4    5        06/02/2004 34-5    5        06/02/2004 34-6    5        06/02/2004 34-7    5        06/02/2004 34-8    5        06/02/2004 34-9    5        06/02/2004 34-10   5        06/02/2004

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

35                                       35-1    4        01/22/2001 38                                       38-1    4        01/22/2001 38-2    5        06/02/2004 52                                       52-1    4 a      03/22/2001 52-2    4 a      03/22/2001 61                                       61-1    2        01/31/1995 73                                       73-1    ORIGINAL 05/27/1993 74                                       74-1    ORIGINAL 05/27/1993 76                                       76-1    ORIGINAL 05/27/1993 77                                       77-1    3        02/06/1996 79                                       79-1    1        07/08/1994 82                                                    82-1    3        02/06/1996

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BA-4100

Highlights of Change

EFFECTIVE ABOVE DATE, the British Aerospace BA-4100 Master Minimum Equipment List has been revised.  Please replace pages of previous lists with Revision 5 for a complete up-to-date MMEL.  This revision updates the document to current policy letters that are applicable.  Retain

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

ATA 22  AUTOFLIGHT

Item 3,  Electric Elevator Trim:  Amended category from "C" to "B", reference Policy Letter (PL) 101.

Item 4,  Autopilot Disconnect: Amended number installed/required from

"1/0" to "2/1", additionally revised proviso to reflect number installed/required.

ATA 23  COMMUNICATIONS

Item 2,  Passenger Address System: Added second proviso to comply with PL 109.

Item 4,  Communication Systems (VHF, UHF): Deleted HF from title and deleted sub-item 2, complies with PL 95.

Item 5,  Ground Crew Interphone: Deleted, relief incorporated into item 23-11, complies with PL 9.

Item 8,  Boom Microphones: Title was amended from "FAR 121.359(e)" to "FAR 121.359(g)".  Added proviso to sub-item 2, PL 58.

Item 11, Crewmember Alerting System: Amended to comply with PL 9.

Item 15, Alerting System (Audio/Visual): Amended to comply with PL 9.

Item 16, High Frequency Communication System: Reformat to comply with PL 106.

Item 17, Automatic Flight Information System: New item.

Item 18, Handset Systems: New item, complies with PL 9.

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  FEDERAL AVIATION ADMINISTRATION   Page: VII

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Highlights of Change

ATA 25  EQUIPMENT/FURNISHINGS

Item 7,  Passenger Seat(s): Amended category to comply with PL 79.

Item 8,  Passenger Convenience Items: Amended number required for

dispatch

to comply with PL 33.

Item 16, "Fasten Seat Belt While Seated" Sign or Placard: Amended word "readable" to "visible", complies with PL 89.

Item 17, Galley Waste Receptacles Access Doors/Covers: Amended to comply with PL 96.

ATA 26  FIRE PROTECTION

Item 1,  Lavatory Smoke Detection System: Amended proviso "c" and Note 1 to comply with PL 24.

ATA 30  ICE AND RAIN PROTECTION

Item 4,  Pitot Heater Failure Lights: Added second proviso to comply with PL 90.

ATA 31  INDICATING/RECORDING SYSTEMS

Item 2,  Flight Data Recorder (FDR) System:  Added first proviso to comply with PL 87.

ATA 32  LANDING GEAR

Item 6,  Anti-Skid System:  Added sub-item 2 "Wet Runways" to comply with PL 113.

ATA 34  NAVIGATION

Item 4,  Standby Attitude Indicator: Amended to comply with PL 111.

Item 8,  Radio Altimeter: Amended to provide consistent relief with TCAS and GPWS relief.

Item 12, Altitude Alerting: Amended proviso "b" and added second proviso to comply with PL 39.

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MASTER MINIMUM EQUIPMENT LIST    Date: 06/02/2004

BA-4100

Highlights of Change

Item 13, ATC Transponder/Automatic Altitude Reporting Systems: Amended first proviso to comply with PL 76.

Item 24, Traffic Alert Collision Avoidance System: Amended first proviso category from "B" to "A" to comply with PL 32.

Item 25, Ground Proximity Warning System: Added two provisos to comply with PL 54.

Item 27, Flight Management Systems: Deleted first proviso to comply with PL 98.

ATA 38  WATER/WASTE

Item 2,  Lavatory Waste Systems: Amended second proviso to comply with PL 83.

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BA-4100

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.

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

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BA-4100

Definitions

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 time specified by repair category.

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

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

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

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

7.  "ER" refers to extended range operations of a two-engine

airplane 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

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Definitions

operation with the  listed item inoperative.

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

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

14.  Inoperative components of an inoperative system:

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

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

who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of the operator's manual or MEL.

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

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BA-4100

Definitions

required to be published as a part of the operator's manual or MEL.

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

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

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

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

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

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

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

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

     Category B.  Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the malfunction was recorded in the aircraft maintenance

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BA-4100

Definitions

record/logbook.  For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29th.

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

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

The letter designators are inserted adjacent to Column 2.

23. Electronic fault alerting system - General                  ¦

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

a.   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.   ¦

System conditions that result only in a maintenance level       ¦ message, i.e. no correlation with a higher level EICAS message, ¦

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BA-4100

Definitions

do not affect dispatch and do not require action other than as  ¦ addressed within an operators standard maintenance program.     ¦

b.   DOUGLAS  (MD-11)                                           ¦

Some Douglas 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-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-320/319/   ¦ 321, A-330, and A-340 also provide MAINTENANCE status messages. ¦

Any message that effects airplane dispatchability will normally ¦ be at the WARNING, CAUTION or STATUS level. MAINTENANCE         ¦ messages (A-320/319/321, 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-320/319/321) or CMS (A-330/A-340) interrogation. The systems ¦ are designed to be fault tolerant, however for any MAINTENANCE  ¦ status (Class II) message, the A-320/319/321 MEL must be        ¦ verified for dispatch capability. For the A-330 and A-340,      ¦ MAINTENANCE status messages do not affect dispatch.             ¦

d.   FOKKER  (FK-100)                                           ¦

  Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

BA-4100

Definitions

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.           ¦

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

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

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

27.  "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft

FEDERAL AVIATION ADMINISTRATION     Page: XV

  D."

FEDERAL AVIATION ADMINISTRATION     Page: XVI

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

BA-4100

Definitions

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

  FEDERAL AVIATION ADMINISTRATION   Page: XVII

Revision: 2

MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

BA-4100

Preamble

(Effective 6/14/89)

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.

 

FEDERAL AVIATION ADMINISTRATION   Page: XVIII Revision: 2 MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

BA-4100

Preamble

(Effective 6/14/89)

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.  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.

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/31/1995      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 1.  High Pressure Shut  C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦     Off Valves            ¦    ¦    ¦ failed valve(s) are isolated in the   ¦ ¦                           ¦    ¦    ¦ closed position.                      ¦

¦ 2.  Temperature           ¦    ¦    ¦                                       ¦ ¦     Controls              ¦    ¦    ¦                                       ¦

¦     1) Automatic        C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ associated manual temperature         ¦ ¦                           ¦    ¦    ¦ control operates normally.            ¦

¦     2) Manual           C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ associated automatic temperature      ¦ ¦                           ¦    ¦    ¦ control operates normally.            ¦

¦                           ¦    ¦    ¦ NOTE: One operative auto control      ¦ ¦                           ¦    ¦    ¦       and one operative manual        ¦ ¦                           ¦    ¦    ¦       control is acceptable.          ¦

¦ 3.  Cabin Temperature   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦

¦ 4.  Cabin Punkah        D ¦ -  ¦ 0  ¦                                       ¦ ¦     Louvers               ¦    ¦    ¦                                       ¦

¦ 5.  Cabin Distribution  C ¦ 2  ¦ 0  ¦                                       ¦ ¦     System Temperature    ¦    ¦    ¦                                       ¦ ¦     Changeover Valves     ¦    ¦    ¦                                       ¦

¦ 6.  Cabin Supplemental  D ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦ *** Heater System         ¦    ¦    ¦ cabin supplemental heater is          ¦ ¦                           ¦    ¦    ¦ deactivated.                          ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 05/27/1993      ¦ 21-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 7.  Cabin Pressurization  ¦    ¦    ¦                                       ¦

¦     1) Automatic Con-   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        trol Function      ¦    ¦    ¦     a) Manual control function        ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) All system indications and     ¦ ¦                           ¦    ¦    ¦        warnings operate normally.     ¦

¦     2) Manual Control   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Function           ¦    ¦    ¦     a) Automatic control function     ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) All system indications and     ¦ ¦                           ¦    ¦    ¦        warnings operate normally.     ¦

¦     3) Automatic and    C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦        Manual Control     ¦    ¦    ¦     a) Flight is conducted in an      ¦ ¦        Function           ¦    ¦    ¦        unpressurized configuration,   ¦ ¦                           ¦    ¦    ¦     b) Electro-pneumatic valve is     ¦ ¦                           ¦    ¦    ¦        secured open, and              ¦ ¦                           ¦    ¦    ¦     c) Overwater operations are not   ¦ ¦                           ¦    ¦    ¦        conducted.                     ¦

¦ 8.  Electro-Pneumatic   C ¦ 1  ¦ 0  ¦ (O)May be inoperative closed          ¦ ¦     Outflow Valve         ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Manual cabin pressurization    ¦ ¦                           ¦    ¦    ¦        system operates normally,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) All pressurization system      ¦ ¦                           ¦    ¦    ¦        indicators and warnings        ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦                         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative open         ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration,   ¦ ¦                           ¦    ¦    ¦     b) Valve is secured in the open   ¦ ¦                           ¦    ¦    ¦        position, and                  ¦ ¦                           ¦    ¦    ¦     c) Overwater operations are not   ¦ ¦                           ¦    ¦    ¦        conducted.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/22/2001      ¦ 21-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 9.  Pneumatic Outflow   C ¦ 1  ¦ 0  ¦ (O)May be inoperative closed          ¦ ¦     Valve                 ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Automatic cabin pressuziza-    ¦ ¦                           ¦    ¦    ¦        tion system operates           ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) All pressurization system      ¦ ¦                           ¦    ¦    ¦        indicators and warning         ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦                         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative open         ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration,   ¦ ¦                           ¦    ¦    ¦     b) Valve is secured in the open   ¦ ¦                           ¦    ¦    ¦        position, and                  ¦ ¦                           ¦    ¦    ¦     c) Overwater operations are not   ¦ ¦                           ¦    ¦    ¦        conducted.                     ¦

¦ 10. Cabin Altitude      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided all    ¦ ¦     Rate of Change        ¦    ¦    ¦ other system equipment, warnings      ¦ ¦     Indicator             ¦    ¦    ¦ and indicators operate normally.      ¦

¦ 11. Cabin Altitude      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Indicator             ¦    ¦    ¦     a) Cabin DIFF pressure indica-    ¦ ¦                           ¦    ¦    ¦        tor operates normally,         ¦ ¦                           ¦    ¦    ¦     b) Cabin altitude warning         ¦ ¦                           ¦    ¦    ¦        system operates normally,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) A chart is provided to         ¦ ¦                           ¦    ¦    ¦        convert cabin differential     ¦ ¦                           ¦    ¦    ¦        pressure to cabin altitude.    ¦

¦                         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ flight is conducted in an             ¦ ¦                           ¦    ¦    ¦ unpressurized configuration.          ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/22/2001      ¦ 21-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 12. Differential        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Pressure Indicator    ¦    ¦    ¦     a) Cabin altitude indicator       ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) A chart is provided to         ¦ ¦                           ¦    ¦    ¦        convert cabin altitude to      ¦ ¦                           ¦    ¦    ¦        cabin pressure.                ¦

¦                         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ flight is conducted in an             ¦ ¦                           ¦    ¦    ¦ unpressurized configuration.          ¦

¦ 13. CABIN PRESS Light   C ¦ 1  ¦ 0  ¦ May be inoperative for operations     ¦ ¦                           ¦    ¦    ¦ at or below 10,000 feet MSL.          ¦

¦ 14. Cockpit Air Demist/ D ¦ 2  ¦ 0  ¦ (O)Foot warmer selector may be        ¦ ¦     Foot Selector         ¦    ¦    ¦ inoperative provided windscreen       ¦ ¦                           ¦    ¦    ¦ demist operates normally.             ¦

¦ 15. Vapor Cycle         D ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦ ¦     Cooling System        ¦    ¦    ¦ system is deactivated.                ¦

¦ 16. Evaporator Fans     D ¦ 3  ¦ -  ¦ (M)May be inoperative provided the    ¦ ¦                           ¦    ¦    ¦ inoperative fan(s) is deactivated.    ¦

¦                           ¦    ¦    ¦ NOTE:  If ONE fan is inoperative      ¦ ¦                           ¦    ¦    ¦        the Vapor Cycle Cooling        ¦ ¦                           ¦    ¦    ¦        System may be used.  If MORE   ¦ ¦                           ¦    ¦    ¦        THAN ONE fan is inoperative    ¦ ¦                           ¦    ¦    ¦        the Vapor Cycle Cooling        ¦ ¦                           ¦    ¦    ¦        System must be deactivated.    ¦

¦ 17. Recirculation Fan   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦ ¦                           ¦    ¦    ¦ fan is deactivated.                   ¦

¦ 18. Environmental       B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Control System        ¦    ¦    ¦     a) Ram Air Ventilation System     ¦ ¦     (ECS) (Left or        ¦    ¦    ¦        operates normally, and         ¦ ¦     Right)                ¦    ¦    ¦     b) Failed ECS is verified OFF.    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 22-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 1.  Autopilot System    B ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦ ***                       ¦    ¦    ¦     a) Autopilot is deactivated,      ¦ ¦                           ¦    ¦    ¦     b) Approach minimums do not       ¦ ¦                           ¦    ¦    ¦        require its use, and           ¦ ¦                           ¦    ¦    ¦     c) Flight controls operate        ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ *** 1) Yaw Damper       C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦        Function           ¦    ¦    ¦ flight controls operate normally.     ¦

¦ 2.  Yaw Damper System   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦ ***                       ¦    ¦    ¦ flight controls operate normally.     ¦

¦ 3.  Electric Elevator   B ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦     Trim                  ¦    ¦    ¦     a) Manual elevator trim           ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     b) Electric elevator trim is      ¦ ¦                           ¦    ¦    ¦        deactivated,                   ¦ ¦                           ¦    ¦    ¦     c) Autopilot is deactivated,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     d) Approach minimums do not       ¦ ¦                           ¦    ¦    ¦        require use of autopilot.      ¦

¦ 4.  Autopilot           C ¦ 2  ¦ 1  ¦ One may be inoperative provided     | ¦ ¦ *** Disconnect            ¦    ¦    ¦ the autopilot is not utilized at      ¦ ¦                           ¦    ¦    ¦ less than initial approach            ¦ ¦                           ¦    ¦    ¦ altitude.                             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 1.  Cockpit Voice         ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Recorder (CVR)        ¦    ¦    ¦     a) Flight data recorder (FDR)     ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

¦ 2.  Passenger Address     ¦    ¦    ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦     1) Passenger        B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Configuration      ¦    ¦    ¦     a) Alternate, normal and          ¦ ¦                           ¦    ¦    ¦        emergency procedures, and/or   ¦ ¦                           ¦    ¦    ¦        operating restrictions are     ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Flight attendant alerting    | ¦ ¦                           ¦    ¦    ¦        system (audio and visual)    | ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦                           ¦    ¦    ¦ NOTE: Any station function(s) that  | ¦ ¦                           ¦    ¦    ¦       operate normally may be used.   ¦

¦                         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦    a) PA not required by FAR, and   | ¦ ¦                           ¦    ¦    ¦    b) Alternate, normal and         | ¦ ¦                           ¦    ¦    ¦       emergency procedures, and/or  | ¦ ¦                           ¦    ¦    ¦       operating restrictions are    | ¦ ¦                           ¦    ¦    ¦       established and used.         | ¦

¦                           ¦    ¦    ¦ NOTE: Any station function(s) that  | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

¦         a) Lavatory     C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦            Speakers       ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 2.  Passenger Address     ¦    ¦    ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦ ***  2) Cargo           C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦         Configuration     ¦    ¦    ¦ alternate, normal and emergency     | ¦ ¦         (Courier/         ¦    ¦    ¦ procedures, and/or operating        | ¦ ¦         Supernumerary     ¦    ¦    ¦ restrictions are established        | ¦ ¦         Address System)   ¦    ¦    ¦ and used.                           | ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦         a) Lavatory     C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦            Speakers       ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦ 3.  Flight Compartment  C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Speakers              ¦    ¦    ¦     a) They are not required for      ¦ ¦                           ¦    ¦    ¦        emergency procedures, and      ¦ ¦                           ¦    ¦    ¦     b) Headsets are installed and     ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 4.  Communication       D ¦ -  ¦ -  ¦ Any in access of those required by    ¦ ¦     Systems (VHF,         ¦    ¦    ¦ FAR may be inoperative provided       ¦ ¦     UHF)                  ¦    ¦    ¦ it is not powered by the Emergency  | ¦ ¦                           ¦    ¦    ¦ AC Bus, Emergency DC Bus, Battery     ¦ ¦                           ¦    ¦    ¦ Bus, Battery Direct Bus, or the DC    ¦ ¦                           ¦    ¦    ¦ Transfer Bus and not required for     ¦ ¦                           ¦    ¦    ¦ emergency procedures                  ¦

¦     1) VHF Comm           ¦    ¦    ¦                                       ¦

¦        a) Frequency     C ¦ -  ¦ 0  ¦                                       ¦ ¦           Transfer        ¦    ¦    ¦                                       ¦ ¦           Light           ¦    ¦    ¦                                       ¦

¦        b) Frequency     C ¦ -  ¦ 0  ¦                                       ¦ ¦           Transfer        ¦    ¦    ¦                                       ¦ ¦           Switch          ¦    ¦    ¦                                       ¦

¦        C) Frequency     C ¦ -  ¦ 2  ¦                                       ¦ ¦           Selector        ¦    ¦    ¦                                       ¦ ¦           Knob            ¦    ¦    ¦                                       ¦

¦        d) Frequency     C ¦ -  ¦ 2  ¦                                       ¦ ¦           Indication      ¦    ¦    ¦                                       ¦

¦ *** 2) High Frequency     ¦    ¦    ¦ Deleted, relief incorporated into   | ¦ ¦        (HF)Communi-       ¦    ¦    ¦ item 23-16, revision 5.             | ¦ ¦        cation System      ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 5. Ground Crew            ¦    ¦    ¦ Deleted, relief incorporated into   | ¦ ¦    Interphone             ¦    ¦    ¦ item 23-11, revision 5.             | ¦

¦ 6. Static Discharge     C ¦ -  ¦ 10 ¦ Any in excess of the required         ¦ ¦    Wicks                  ¦    ¦    ¦ number of discharge wick may be       ¦ ¦                           ¦    ¦    ¦ missing provided the minimum number   ¦ ¦                           ¦    ¦    ¦ on each control surface, as listed    ¦ ¦                           ¦    ¦    ¦ below remain:                         ¦ ¦                           ¦    ¦    ¦     a) Two wicks on each aileron,     ¦ ¦                           ¦    ¦    ¦     b) One wick on each elevator,     ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) One wick on the rudder.        ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 7.  Passenger Briefing  D ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     System                ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

¦ 8.  Boom Microphones      ¦    ¦    ¦                                       ¦

¦     1) Cockpit Voice    A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦        Recorder           ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦ ¦        Equipped to        ¦    ¦    ¦        operates normally, and         ¦ ¦        Record Boom        ¦    ¦    ¦     b) Repairs are made within        ¦ ¦        Microphone per     ¦    ¦    ¦        three flight days.             ¦ ¦        FAR 121.359(g),    ¦    ¦    ¦                                     | ¦ ¦        135.151(d) or      ¦    ¦    ¦                                       ¦ ¦        125.227(e)         ¦    ¦    ¦                                       ¦

¦ *** 2) Cockpit Voice    D ¦ -  ¦ 0  ¦ Any in excess of those required by  | ¦ ¦        Recorder Not       ¦    ¦    ¦ FAR may be inoperative.             | ¦ ¦        Equipped to        ¦    ¦    ¦                                       ¦ ¦        Record Boom        ¦    ¦    ¦                                       ¦ ¦        Microphone         ¦    ¦    ¦                                       ¦

¦ 9.  Hand-held Micro-    D ¦ 2  ¦ 0  ¦                                       ¦ ¦ *** phones                ¦    ¦    ¦                                       ¦

¦ 10. Selective Call      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦ *** System (SELCAL)       ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 11. Crewmember            ¦    ¦    ¦                                       ¦ ¦     Interphone System     ¦    ¦    ¦                                       ¦

¦     1) Passenger          ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   B ¦ -  ¦ -  ¦ (O)May be inoperative provided:     | ¦ ¦           to Cabin,       ¦    ¦    ¦     a) Flight deck to cabin and     | ¦ ¦           Cabin to        ¦    ¦    ¦        cabin to flight deck         | ¦ ¦           Flight Deck     ¦    ¦    ¦        interphone functions         | ¦ ¦           Functions       ¦    ¦    ¦        operate normally on          | ¦ ¦                           ¦    ¦    ¦        at least fifty percent       | ¦ ¦                           ¦    ¦    ¦        of the cabin handsets, and   | ¦ ¦                           ¦    ¦    ¦     b) Alternate communications       ¦ ¦                           ¦    ¦    ¦        procedures between the         ¦ ¦                           ¦    ¦    ¦        affected Flight Attendants     ¦ ¦                           ¦    ¦    ¦        station(s) are established   | ¦ ¦                           ¦    ¦    ¦        and used.                      ¦

¦                           ¦    ¦    ¦ NOTE: Any station function(s) that  | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

¦        b) Flight Deck   C ¦ 1  ¦ 0  ¦ (O)Flight interphone flight deck    | ¦ ¦           to Ground       ¦    ¦    ¦ to ground/ground to flight deck     | ¦ ¦           Function        ¦    ¦    ¦ function may be inoperative         | ¦ ¦                           ¦    ¦    ¦ provided:                           | ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used, and    | ¦ ¦                           ¦    ¦    ¦     b) Nose gear/forward fuselage   | ¦ ¦                           ¦    ¦    ¦        service interphone jack      | ¦ ¦                           ¦    ¦    ¦        operates normally.           | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 11. Crewmember            ¦    ¦    ¦                                       ¦ ¦     Interphone System     ¦    ¦    ¦                                       ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦     1) Passenger          ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        b) Flight Deck   C ¦ 1  ¦ 0  ¦ (O)Service interphone flight deck   | ¦ ¦           to Ground       ¦    ¦    ¦ to ground/ground to flight deck     | ¦ ¦           Function        ¦    ¦    ¦ function may be inoperative         | ¦ ¦                           ¦    ¦    ¦ provided:                           | ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used, and    | ¦ ¦                           ¦    ¦    ¦     b) Nose gear/forward fuselage   | ¦ ¦                           ¦    ¦    ¦        flight interphone jack       | ¦ ¦                           ¦    ¦    ¦        operates normally.           | ¦

¦                         B ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

¦ *** 2) Cargo              ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦           to Cabin,       ¦    ¦    ¦ alternate, normal and emergency     | ¦ ¦           Cabin to        ¦    ¦    ¦ procedures, and/or operating        | ¦ ¦           Flight Deck     ¦    ¦    ¦ restrictions are established        | ¦ ¦           Functions       ¦    ¦    ¦ and used.                           | ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 11. Crewmember            ¦    ¦    ¦                                       ¦ ¦     Interphone System     ¦    ¦    ¦                                       ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦ *** 2) Cargo              ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        b) Flight Deck   C ¦ 1  ¦ 0  ¦ (O)Flight interphone flight deck    | ¦ ¦           to Ground       ¦    ¦    ¦ to ground/ground to flight deck     | ¦ ¦           Function        ¦    ¦    ¦ function may be inoperative         | ¦ ¦                           ¦    ¦    ¦ provided:                           | ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used, and    | ¦ ¦                           ¦    ¦    ¦     b) Nose gear/forward fuselage   | ¦ ¦                           ¦    ¦    ¦        service interphone jack      | ¦ ¦                           ¦    ¦    ¦        operates normally.           | ¦

¦                         C ¦ 1  ¦ 0  ¦ (O)Service interphone flight deck   | ¦ ¦                           ¦    ¦    ¦ to ground/ground to flight deck     | ¦ ¦                           ¦    ¦    ¦ function may be inoperative         | ¦ ¦                           ¦    ¦    ¦ provided:                           | ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used, and    | ¦ ¦                           ¦    ¦    ¦     b) Nose gear/forward fuselage   | ¦ ¦                           ¦    ¦    ¦        flight interphone jack       | ¦ ¦                           ¦    ¦    ¦        operates normally.           | ¦

¦                         B ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 12. Forward Flight      C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** Attendant Handset     ¦    ¦    ¦                                       ¦

¦ 13. ARINC Communica-    C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦ *** tions Addressing      ¦    ¦    ¦ alternate procedures are              ¦ ¦     and Reporting         ¦    ¦    ¦ established and used.                 ¦ ¦     System (ACARS)        ¦    ¦    ¦                                       ¦ ¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

¦     1) ACARS Printer    D ¦ 1  ¦ 0  ¦                                       ¦

¦ 14. Emergency Locator   C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦ ¦     Transmitter (ELT)     ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-10    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 15. Alerting System       ¦    ¦    ¦                                       ¦ ¦     (Audio/Visual)        ¦    ¦    ¦                                     | ¦

¦     1) Passenger          ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   B ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦           Call Visual     ¦    ¦    ¦ flight deck audio alerting system   | ¦ ¦           Alerting        ¦    ¦    ¦ operates normally.                  | ¦ ¦           System          ¦    ¦    ¦                                       ¦ ¦                           ¦    ¦    ¦ NOTE: The flight deck audio         | ¦ ¦                           ¦    ¦    ¦       alerting must always          | ¦ ¦                           ¦    ¦    ¦       be operative.                 | ¦

¦        b) Flight        B ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦           Attendant       ¦    ¦    ¦     a) PA system operates normally, | ¦ ¦           Visual          ¦    ¦    ¦     b) If affected visual alerting  | ¦ ¦           Alerting        ¦    ¦    ¦        system is used for lavatory  | ¦ ¦           System          ¦    ¦    ¦        smoke detector alerting, an  | ¦ ¦                           ¦    ¦    ¦        alternate lavatory smoke     | ¦ ¦                           ¦    ¦    ¦        detector alert (audio or     | ¦ ¦                           ¦    ¦    ¦        visual) is installed and     | ¦ ¦                           ¦    ¦    ¦        operates normally, and       | ¦ ¦                           ¦    ¦    ¦     c) Alternate procedures for     | ¦ ¦                           ¦    ¦    ¦        contacting flight attendants | ¦ ¦                           ¦    ¦    ¦        are established and used.    | ¦

¦                           ¦    ¦    ¦ NOTE 1: Passenger to Attendant      | ¦ ¦                           ¦    ¦    ¦         Call System is considered   | ¦ ¦                           ¦    ¦    ¦         a passenger convience item. | ¦

¦                           ¦    ¦    ¦ NOTE 2: Any audio alerting system   | ¦ ¦                           ¦    ¦    ¦         function(s) that operates   | ¦ ¦                           ¦    ¦    ¦         normally may be used.       | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-11    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 15. Alerting System       ¦    ¦    ¦                                     | ¦ ¦     (Audio/Visual)        ¦    ¦    ¦                                     | ¦ ¦     (Cont'd)              ¦    ¦    ¦                                     | ¦

¦     1) Passenger          ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        c) Flight        B ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦           Attendant       ¦    ¦    ¦     a) PA system operates normally, | ¦ ¦           Audio           ¦    ¦    ¦     b) If affected audio alerting   | ¦ ¦           Alerting        ¦    ¦    ¦        system is used for lavatory  | ¦ ¦           System          ¦    ¦    ¦        smoke detector alerting, an  | ¦ ¦                           ¦    ¦    ¦        alternate lavatory smoke     | ¦ ¦                           ¦    ¦    ¦        detector alert (visual or    | ¦ ¦                           ¦    ¦    ¦        audio) is installed and      | ¦ ¦                           ¦    ¦    ¦        operates normally, and       | ¦ ¦                           ¦    ¦    ¦     c) Alternate procedures for     | ¦ ¦                           ¦    ¦    ¦        contacting flight attendants | ¦ ¦                           ¦    ¦    ¦        are established and used.    | ¦

¦                           ¦    ¦    ¦ NOTE 1: Passenger to Attendant      | ¦ ¦                           ¦    ¦    ¦         Call System is considered   | ¦ ¦                           ¦    ¦    ¦         a passenger convience item. | ¦

¦                           ¦    ¦    ¦ Note 2: Any audio alerting system   | ¦ ¦                           ¦    ¦    ¦         function(s) that operates   | ¦ ¦                           ¦    ¦    ¦         normally may be used.       | ¦

¦ *** 2) Cargo              ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   B ¦ 1  ¦ 0  ¦ May be inoperative provided the     | ¦ ¦           Call Visual     ¦    ¦    ¦ flight deck audio alerting          | ¦ ¦           Alerting        ¦    ¦    ¦ system operates normally.           | ¦ ¦           System          ¦    ¦    ¦                                     | ¦

¦        b) Flight Deck   D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦           Call System     ¦    ¦    ¦ courier/supernumerary compartment   | ¦ ¦                           ¦    ¦    ¦ remains unoccupied.                 | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-12    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 15. Alerting System       ¦    ¦    ¦                                     | ¦ ¦     (Audio/Visual)        ¦    ¦    ¦                                     | ¦ ¦     (Cont'd)              ¦    ¦    ¦                                     | ¦

¦ *** 2) Cargo              ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        c) Courier/      B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦           Supernumerary   ¦    ¦    ¦     a) Courier/supernumerary        | ¦ ¦           Visual          ¦    ¦    ¦        address system operates      | ¦ ¦           Alerting        ¦    ¦    ¦        normally, and                | ¦ ¦           System          ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and use.         | ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ courier/supernumerary compartment   | ¦ ¦                           ¦    ¦    ¦ remains unoccupied.                 | ¦

¦                           ¦    ¦    ¦ NOTE: Any visual alerting system    | ¦ ¦                           ¦    ¦    ¦       function(s) that operate      | ¦ ¦                           ¦    ¦    ¦       normally may be used.         | ¦

¦        d) Courier/      B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦           Supernumerary   ¦    ¦    ¦     a) Courier/supernumerary        | ¦ ¦           Audio           ¦    ¦    ¦        address system operates      | ¦ ¦           Alerting        ¦    ¦    ¦        normally, and                | ¦ ¦           System          ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and use.         | ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ courier/supernumerary compartment   | ¦ ¦                           ¦    ¦    ¦ remains unoccupied.                 | ¦

¦                           ¦    ¦    ¦ NOTE: Any audio alerting system     | ¦ ¦                           ¦    ¦    ¦       function(s) that operate      | ¦ ¦                           ¦    ¦    ¦       normally may be used.         | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-13    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 16. High Frequency (HF) D ¦ -  ¦ -  ¦ Any in excess of those required     | ¦ ¦     Communication         ¦    ¦    ¦ by FAR may be inoperative.          | ¦ ¦     System                ¦    ¦    ¦                                       ¦ ¦                         C ¦ -  ¦ 1  ¦ (O)May be inoperative while         | ¦ ¦                           ¦    ¦    ¦ conducting operations that          | ¦ ¦                           ¦    ¦    ¦ require two LRCS provided:          | ¦ ¦                           ¦    ¦    ¦     a) SATCOM (High or Low Gain)    | ¦ ¦                           ¦    ¦    ¦        Data Link system operates    | ¦ ¦                           ¦    ¦    ¦        normally, and                | ¦ ¦                           ¦    ¦    ¦     b) SATCOM Data Link             | ¦ ¦                           ¦    ¦    ¦        communication operates       | ¦ ¦                           ¦    ¦    ¦        normally over the intended   | ¦ ¦                           ¦    ¦    ¦        route of flight.             | ¦

¦ 17. Automatic Flight    C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦ *** Information System    ¦    ¦    ¦ alternate procedures are            | ¦ ¦     (AFIS)                ¦    ¦    ¦ established and used.               | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-14    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 18. Handset Systems       ¦    ¦    ¦                                     | ¦

¦     1) Passenger          ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) Flight deck to cabin         | ¦ ¦                           ¦    ¦    ¦        communication operates       | ¦ ¦                           ¦    ¦    ¦        normally, and                | ¦ ¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used.        | ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦        b) Cabin         B ¦ -  ¦ -  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) Fifty percent of cabin       | ¦ ¦                           ¦    ¦    ¦        handsets operate normally,   | ¦ ¦                           ¦    ¦    ¦        and                          | ¦ ¦                           ¦    ¦    ¦     b) Alternate communication      | ¦ ¦                           ¦    ¦    ¦        procedures between the       | ¦ ¦                           ¦    ¦    ¦        affected Flight Attendants   | ¦ ¦                           ¦    ¦    ¦        station(s) are established   | ¦ ¦                           ¦    ¦    ¦        and used.                    | ¦

¦                           ¦    ¦    ¦ NOTE 1: An operative handset at     | ¦ ¦                           ¦    ¦    ¦         an inoperative flight       | ¦ ¦                           ¦    ¦    ¦         attendant seat shall not    | ¦ ¦                           ¦    ¦    ¦         be counted to satisfy the   | ¦ ¦                           ¦    ¦    ¦         fifty percent requirement.  | ¦

¦                           ¦    ¦    ¦ NOTE 2: Any handset(s) function(s)  | ¦ ¦                           ¦    ¦    ¦         that operate normally may   | ¦ ¦                           ¦    ¦    ¦         be used.                    | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 23-15    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 18. Handset Systems       ¦    ¦    ¦                                     | ¦

¦ *** 2) Cargo              ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   C ¦ -  ¦ 0  ¦ May be inoperative provided flight  | ¦ ¦                           ¦    ¦    ¦ deck to courier/supernumerary       | ¦ ¦                           ¦    ¦    ¦ communication operates normally.    | ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦        b) Courier/      D ¦ -  ¦ 1  ¦                                     | ¦ ¦           Supernumerary   ¦    ¦    ¦                                     | ¦ ¦                         D ¦ -  ¦ 0  ¦ May beinoperative provided          | ¦ ¦                           ¦    ¦    ¦ courier/supernumerary compartment   | ¦ ¦                           ¦    ¦    ¦ remains unoccupied.                 | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/08/1994      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 1.  Ammeters            B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦                           ¦    ¦    ¦ corresponding voltmeter function      ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦ 2.  Voltmeters          C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦                           ¦    ¦    ¦ associated ammeter function           ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦ 3.  External Power      C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     System                ¦    ¦    ¦ procedures do not require its use.    ¦

¦ 4.  Battery  HI TEMP    B ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦     Indications (NiCad    ¦    ¦    ¦ provided:                             ¦ ¦     Batteries Only)       ¦    ¦    ¦     a) BATT indicator operates        ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Battery indication function    ¦ ¦                           ¦    ¦    ¦        of ammeter operates            ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     c) Battery contactor operates     ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     d) Amber ELECT Caption on CAP     ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 5.  U/VOLT Indications  C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦                           ¦    ¦    ¦     a) Associated voltmeter           ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) Associated generator voltage   ¦ ¦                           ¦    ¦    ¦        is 28.5V (+0.3V, -0.7V)        ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/08/1994      ¦ 24-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 6.  EMERG BUS           C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Indication            ¦    ¦    ¦     a) Both emergency bus remote      ¦ ¦                           ¦    ¦    ¦        controlled circuit breakers    ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     b) Amber ELECT caption on CAP     ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 7.  BUS TIE CLOSED      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     Indication            ¦    ¦    ¦ left and right bus tie contactors     ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

¦ 8.  ESS BUS             C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Indications           ¦    ¦    ¦     a) Associated essential busbar    ¦ ¦                           ¦    ¦    ¦        contactor operates normally,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Amber ELECT caption on CAP     ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 9.  NON ESS BUS         C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Indication            ¦    ¦    ¦     a) Non essential busbar           ¦ ¦                           ¦    ¦    ¦        contactor operates normally,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Amber ELECT caption on CAP     ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 10. GEN Indications     B ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided:   ¦ ¦                           ¦    ¦    ¦     a) Associated starter/generator   ¦ ¦                           ¦    ¦    ¦        contactor operates normally,   ¦ ¦                           ¦    ¦    ¦     b) Ammeter operates normally,     ¦ ¦                           ¦    ¦    ¦     c) BUS TIE CLOSED caption         ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     d) Amber ELECT caption on CAP     ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 11. Inverter L FAIL     B ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     and R FAIL            ¦    ¦    ¦     a) Both inverters operate         ¦ ¦     Indications           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Amber ELECT caption on CAP     ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/22/2001      ¦ 25-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 1.  Pilot's Seat          ¦    ¦    ¦                                       ¦ ¦     Adjustment            ¦    ¦    ¦                                       ¦

¦     1) Vertical Mode    C ¦ 2  ¦ 0  ¦ (M)Adjustment in a vertical mode      ¦ ¦                           ¦    ¦    ¦ may be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Seat is secured at the         ¦ ¦                           ¦    ¦    ¦        individual crewmember's        ¦ ¦                           ¦    ¦    ¦        requirements, and              ¦ ¦                           ¦    ¦    ¦     b) Fore-aft adjustment operates   ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦     2) Armrests         C ¦ 4  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ associated armrest is removed or      ¦ ¦                           ¦    ¦    ¦ secured in a stowed position.         ¦

¦     3) Lumbar and       C ¦ 6  ¦ 0  ¦                                       ¦ ¦        Thigh Supports     ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4 a      ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/22/2001      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 2.  Forward Observer    A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Seat (Including       ¦    ¦    ¦     a) A passenger seat in the        ¦ ¦     All Associated        ¦    ¦    ¦        passenger cabin is made        ¦ ¦     Equipment)            ¦    ¦    ¦        available to an FAA inspec-    ¦ ¦                           ¦    ¦    ¦        tor for the performance of     ¦ ¦                           ¦    ¦    ¦        official duties, and           ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two (2) flight days.           ¦

¦                         A ¦ 1  ¦ 0  ¦ May be in operative provided:         ¦ ¦                           ¦    ¦    ¦     a) Required minimum safety        ¦ ¦                           ¦    ¦    ¦        equipment (safety belt,        ¦ ¦                           ¦    ¦    ¦        and oxygen) is available,      ¦ ¦                           ¦    ¦    ¦     b) Seat is acceptable to          ¦ ¦                           ¦    ¦    ¦        the FAA inspector for          ¦ ¦                           ¦    ¦    ¦        performance of official        ¦ ¦                           ¦    ¦    ¦        duties, and                    ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two (2) flight days.           ¦

¦                           ¦    ¦    ¦ NOTE 1: These provisos are intended   ¦ ¦                           ¦    ¦    ¦         to provide for occupancy of   ¦ ¦                           ¦    ¦    ¦         the above seat by an FAA      ¦ ¦                           ¦    ¦    ¦         inspector when the minimum    ¦ ¦                           ¦    ¦    ¦         safety equipment (oxygen      ¦ ¦                           ¦    ¦    ¦         and safety belt) is func-     ¦ ¦                           ¦    ¦    ¦         tional and the inspector      ¦ ¦                           ¦    ¦    ¦         determines the conditions     ¦ ¦                           ¦    ¦    ¦         to be acceptable.             ¦

¦                           ¦    ¦    ¦ NOTE 2: The pilot-in-command will     ¦ ¦                           ¦    ¦    ¦         determine if the minimum      ¦ ¦                           ¦    ¦    ¦         safety equipment is func-     ¦ ¦                           ¦    ¦    ¦         tional for other persons      ¦ ¦                           ¦    ¦    ¦         authorized to occupy the      ¦ ¦                           ¦    ¦    ¦         observer seat.                ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/22/2001      ¦ 25-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 3.  Flight Attendant    A ¦ 1  ¦ 0  ¦ (M)(O)Flight Attendant seat may       ¦ ¦     Seat Assembly         ¦    ¦    ¦ be inoperative provided:              ¦ ¦                           ¦    ¦    ¦     a) Affected seat or seat          ¦ ¦                           ¦    ¦    ¦        assembly is not occupied,      ¦ ¦                           ¦    ¦    ¦     b) Flight attendant displaced     ¦ ¦                           ¦    ¦    ¦        by inoperative seat occupies   ¦ ¦                           ¦    ¦    ¦        the passenger seat most        ¦ ¦                           ¦    ¦    ¦        accessible to the              ¦ ¦                           ¦    ¦    ¦        inoperative seat,              ¦ ¦                           ¦    ¦    ¦     c) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used as        ¦ ¦                           ¦    ¦    ¦        published in crew member       ¦ ¦                           ¦    ¦    ¦        manuals,                       ¦ ¦                           ¦    ¦    ¦     d) Folding type seat is stowed    ¦ ¦                           ¦    ¦    ¦        or secured in the retracted    ¦ ¦                           ¦    ¦    ¦        position,                      ¦ ¦                           ¦    ¦    ¦     e) Passenger seat assigned to     ¦ ¦                           ¦    ¦    ¦        flight attendant is            ¦ ¦                           ¦    ¦    ¦        placarded "FOR FLIGHT          ¦ ¦                           ¦    ¦    ¦        ATTENDANT ONLY", and           ¦ ¦                           ¦    ¦    ¦     f) Repairs are made within two    ¦ ¦                           ¦    ¦    ¦        (2) flight days.               ¦

¦                           ¦    ¦    ¦ NOTE 1: A folding seat that will      ¦ ¦                           ¦    ¦    ¦         not stow is considered        ¦ ¦                           ¦    ¦    ¦         inoperative.                  ¦

¦                           ¦    ¦    ¦ NOTE 2: A seat position with an       ¦ ¦                           ¦    ¦    ¦         inoperative or missing        ¦ ¦                           ¦    ¦    ¦         lap belt is considered        ¦ ¦                           ¦    ¦    ¦         inoperative.                  ¦

¦ 4.  Megaphones          D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦                           ¦    ¦    ¦ FAR may be inoperative or missing     ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Inoperative megaphone is       ¦ ¦                           ¦    ¦    ¦        removed from passenger         ¦ ¦                           ¦    ¦    ¦        cabin, and                     ¦ ¦                           ¦    ¦    ¦     b) Required distribution is       ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/22/2001      ¦ 25-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 5.  First Aid Kits      D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦                           ¦    ¦    ¦ FAR may be incomplete or missing      ¦ ¦                           ¦    ¦    ¦ provided required distribution is     ¦ ¦                           ¦    ¦    ¦ maintained.                           ¦

¦ 6.  Emergency Flash-      ¦    ¦    ¦                                       ¦ ¦     light/Holders         ¦    ¦    ¦                                       ¦

¦     1) Flight Compart-  C ¦ 2  ¦ 0  ¦ May be inoperative or missing         ¦ ¦        ment               ¦    ¦    ¦ provided the crewmember assigned      ¦ ¦                           ¦    ¦    ¦ to the affected position has a        ¦ ¦                           ¦    ¦    ¦ normally operating flashlight         ¦ ¦                           ¦    ¦    ¦ readily available.                    ¦

¦     2) Passenger        C ¦ 1  ¦ 0  ¦ May be inoperative or missing         ¦ ¦        Cabin              ¦    ¦    ¦ provided the crewmember assigned      ¦ ¦                           ¦    ¦    ¦ to the affected position has a        ¦ ¦                           ¦    ¦    ¦ normally operating flashlight         ¦ ¦                           ¦    ¦    ¦ readily available.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 25-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 7.  Passenger Seat(s)   C ¦ -  ¦ -  ¦ May be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a) Does not block an Emergency    ¦ ¦                           ¦    ¦    ¦        Exit,                          ¦ ¦                           ¦    ¦    ¦     b) Seat does not restrict any     ¦ ¦                           ¦    ¦    ¦        passenger from access to the   ¦ ¦                           ¦    ¦    ¦        main aircraft aisle, and       ¦ ¦                           ¦    ¦    ¦     c) The affected seat(s) is        ¦ ¦                           ¦    ¦    ¦        blocked and placarded "DO      ¦ ¦                           ¦    ¦    ¦        NOT OCCUPY"                    ¦

¦                           ¦    ¦    ¦ NOTE 1: A seat with an inoperative    ¦ ¦                           ¦    ¦    ¦         seat belt is considered       ¦ ¦                           ¦    ¦    ¦         inoperative.                  ¦

¦                           ¦    ¦    ¦ NOTE 2: Inoperative seats do not      ¦ ¦                           ¦    ¦    ¦         affect the required number    ¦ ¦                           ¦    ¦    ¦         of Flight Attendants.         ¦

¦                           ¦    ¦    ¦ NOTE 3: Affected seat(s) may          ¦ ¦                           ¦    ¦    ¦         include the seat(s) behind    ¦ ¦                           ¦    ¦    ¦         and/or adjacent outboard      ¦ ¦                           ¦    ¦    ¦         seats.                        ¦

¦     1) Recline          C ¦ -  ¦ -  ¦ (M)May be inoperative and seat        ¦ ¦        Mechanism          ¦    ¦    ¦ occupied provided seat is secured     ¦ ¦                           ¦    ¦    ¦ in the up-right position.             ¦

¦     2) Underseat        C ¦ -  ¦ -  ¦ (M)(O)May be inoperative provided     ¦ ¦        Baggage            ¦    ¦    ¦     a) Baggage is not stowed under    ¦ ¦        Restraining        ¦    ¦    ¦        seat with inoperative          ¦ ¦        Bars               ¦    ¦    ¦        restraining bar,               ¦ ¦                           ¦    ¦    ¦     b) Associated seat is placarded   ¦ ¦                           ¦    ¦    ¦        "DO NOT STOW BAGGAGE UNDER     ¦ ¦                           ¦    ¦    ¦        THIS SEAT", and                ¦ ¦                           ¦    ¦    ¦     c) Procedures are established     ¦ ¦                           ¦    ¦    ¦        to alert Cabin Crew of         ¦ ¦                           ¦    ¦    ¦        inoperative restraining bar.   ¦

¦     3) Electrical/      C ¦ -  ¦ -  ¦ (M)May be inoperative and seat        ¦ ¦        Electronic/Sys-    ¦    ¦    ¦ occupied provided associated          ¦ ¦        tems/Components    ¦    ¦    ¦ component(s)is deactivated.           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 25-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 8.  Passenger             ¦ -  ¦ 0  ¦ Passenger convenience items, as     | ¦ ¦ *** Convenience Items     ¦    ¦    ¦ expressed in this MMEL, are those     ¦ ¦                           ¦    ¦    ¦ related to passenger convenience,     ¦ ¦                           ¦    ¦    ¦ comfort or entertainment such as      ¦ ¦                           ¦    ¦    ¦ but not limited to, galley equip-     ¦ ¦                           ¦    ¦    ¦ ment, movie equipment, ash trays,     ¦ ¦                           ¦    ¦    ¦ stereo equipment, overhead reading    ¦ ¦                           ¦    ¦    ¦ lamps, etc.  Items addressed else-    ¦ ¦                           ¦    ¦    ¦ where in this document shall not      ¦ ¦                           ¦    ¦    ¦ be included.  (M) and (O) proce-      ¦ ¦                           ¦    ¦    ¦ dures may be required and included    ¦ ¦                           ¦    ¦    ¦ in the air carrier's appropriate      ¦ ¦                           ¦    ¦    ¦ document.                             ¦

¦                           ¦    ¦    ¦ NOTE: Lavatory door ash tray is not   ¦ ¦                           ¦    ¦    ¦       considered a passenger          ¦ ¦                           ¦    ¦    ¦       convenience item.               ¦

¦ 9.  Sun Visors          C ¦ 2  ¦ 0  ¦                                       ¦

¦ 10. Flotation           D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     Equipment             ¦    ¦    ¦ FAR may be inoperative or missing     ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Inoperative flotation equip-   ¦ ¦                           ¦    ¦    ¦        ment is tagged inoperative,    ¦ ¦                           ¦    ¦    ¦        removed from the installed     ¦ ¦                           ¦    ¦    ¦        location, and placed out of    ¦ ¦                           ¦    ¦    ¦        sight so it can not be         ¦ ¦                           ¦    ¦    ¦        mistaken for a functional      ¦ ¦                           ¦    ¦    ¦        unit, and                      ¦ ¦                           ¦    ¦    ¦     b) Required distribution is       ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/22/2001      ¦ 25-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 11. Underseat Baggage     ¦    ¦    ¦ Moved to Item 25-7 in Revision 4.     ¦ ¦     Restraining Bars      ¦    ¦    ¦                                       ¦

¦ 12. Flight Crew         D ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Baggage Net           ¦    ¦    ¦     a) Baggage is not stowed in       ¦ ¦     Retention System      ¦    ¦    ¦        the compartment, and           ¦ ¦                           ¦    ¦    ¦     b) Retention net and anchoring    ¦ ¦                           ¦    ¦    ¦        bar are secured.               ¦

¦ 13. Lavatory Door       B ¦ 1  ¦ 0  ¦ May be inoperative provided door      ¦ ¦                           ¦    ¦    ¦ is secured closed and placarded,      ¦ ¦                           ¦    ¦    ¦ "INOPERATIVE - DO NOT ENTER".         ¦

¦ 14. Lavatory Flapper    B ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Valve                 ¦    ¦    ¦     a) Valve is secured closed, and   ¦ ¦                           ¦    ¦    ¦     b) Lavatory door is secured       ¦ ¦                           ¦    ¦    ¦        closed and placarded,          ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE - DO NO ENTER".   ¦

¦ 15. Exterior Lavatory     ¦    ¦    ¦                                       ¦ ¦     Door Ashtrays         ¦    ¦    ¦                                       ¦

¦     1) Airplanes with   A ¦ -  ¦ -  ¦ One may be missing provided it is     ¦ ¦        more than one      ¦    ¦    ¦ replaced within 10 calendar days.     ¦ ¦        exterior lava-     ¦    ¦    ¦                                       ¦ ¦        tory door ash-     ¦    ¦    ¦                                       ¦ ¦        tray installed     ¦    ¦    ¦                                       ¦

¦     2) Airplanes with   A ¦ 1  ¦ 0  ¦ May be missing provided it is         ¦ ¦        only one           ¦    ¦    ¦ replaced within 3 calendar days.      ¦ ¦        exterior lava-     ¦    ¦    ¦                                       ¦ ¦        tory door ash-     ¦    ¦    ¦                                       ¦ ¦        tray installed     ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 25-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 16. "Fasten Seat Belt   C ¦ -  ¦ -  ¦ One or more signs or placards may     ¦ ¦     While Seated" Sign    ¦    ¦    ¦ be illegible or missing provided      ¦ ¦     or Placard            ¦    ¦    ¦ a legible sign or placard is          ¦ ¦                           ¦    ¦    ¦ visible from each occupied          | ¦ ¦                           ¦    ¦    ¦ passenger seat.                       ¦

¦ 17. Galley Waste        C ¦ -  ¦ -  ¦ (M)(O)May be inoperative provided   | ¦ ¦     Receptacles Access    ¦    ¦    ¦     a)The container is empty and    | ¦ ¦     Doors/Covers          ¦    ¦    ¦       the access is secured to      | ¦ ¦                           ¦    ¦    ¦       prevent waste introduction    | ¦ ¦                           ¦    ¦    ¦       into the compartment, and     | ¦ ¦                           ¦    ¦    ¦     b)Procedures are established    | ¦ ¦                           ¦    ¦    ¦       to ensure that sufficient     | ¦ ¦                           ¦    ¦    ¦       galley waste receptacles      | ¦ ¦                           ¦    ¦    ¦       are available to accommodate  | ¦ ¦                           ¦    ¦    ¦       all waste that may be         | ¦ ¦                           ¦    ¦    ¦       generated on a flight.        | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 26-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 1.  Lavatory Smoke      C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the          ¦ ¦     Detection System      ¦    ¦    ¦ lavatory smoke detection system may   ¦ ¦                           ¦    ¦    ¦ be inoperative provided:              ¦ ¦                           ¦    ¦    ¦     a) Lavatory waste receptacle is   ¦ ¦                           ¦    ¦    ¦        empty,                         ¦ ¦                           ¦    ¦    ¦     b) Lavatory door is secured       ¦ ¦                           ¦    ¦    ¦        closed and placarded,          ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT          ¦ ¦                           ¦    ¦    ¦        ENTER", and                    ¦ ¦                           ¦    ¦    ¦     c) Lavatory is used only by     | ¦ ¦                           ¦    ¦    ¦        crewmembers.                 | ¦

¦                           ¦    ¦    ¦ NOTE 1: These provisos are not        ¦ ¦                           ¦    ¦    ¦         intended to prohibit          ¦ ¦                           ¦    ¦    ¦         lavatory use or inspection  | ¦ ¦                           ¦    ¦    ¦         by crewmembers.             | ¦

¦                           ¦    ¦    ¦ NOTE 2: A lavatory smoke detection    ¦ ¦                           ¦    ¦    ¦         system is not required for    ¦ ¦                           ¦    ¦    ¦         all-cargo operations.         ¦

¦ 2.  Fire Bottle         C ¦ 3  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦     Discharge             ¦    ¦    ¦ bottle pressure is verified before    ¦ ¦     Indicators            ¦    ¦    ¦ the first flight of the day.          ¦

¦ 3.  Ventral-Pod         C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦ *** Baggage               ¦    ¦    ¦ Ventral-Pod Baggage Compartment       ¦ ¦     Compartment Bay       ¦    ¦    ¦ Bay remains empty.                    ¦ ¦     Smoke Detection       ¦    ¦    ¦                                       ¦ ¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided only      ¦ ¦                           ¦    ¦    ¦ non-combustible materials are         ¦ ¦                           ¦    ¦    ¦ carried.                              ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 26-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 4.  Lavatory Fire       C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the          ¦ ¦     Extinguisher          ¦    ¦    ¦ lavatory fire extinguisher system     ¦ ¦     Systems               ¦    ¦    ¦ may be inoperative provided           ¦ ¦                           ¦    ¦    ¦ Lavatory Smoke Detector system        ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦                         C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the          ¦ ¦                           ¦    ¦    ¦ lavatory fire extinguisher system     ¦ ¦                           ¦    ¦    ¦ may be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Lavatory waste receptacle      ¦ ¦                           ¦    ¦    ¦        is empty,                      ¦ ¦                           ¦    ¦    ¦     b) Lavatory door is locked        ¦ ¦                           ¦    ¦    ¦        closed and placarded,          ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT          ¦ ¦                           ¦    ¦    ¦        ENTER", and                    ¦ ¦                           ¦    ¦    ¦     d) Lavatory is not used for any   ¦ ¦                           ¦    ¦    ¦        purpose.                       ¦

¦                           ¦    ¦    ¦ NOTE 1: These provisions are not      ¦ ¦                           ¦    ¦    ¦         intended to prohibit          ¦ ¦                           ¦    ¦    ¦         lavatory inspections by       ¦ ¦                           ¦    ¦    ¦         crewmembers.                  ¦

¦                           ¦    ¦    ¦ NOTE 2: A lavatory fire extinguish-   ¦ ¦                           ¦    ¦    ¦         er system is not required     ¦ ¦                           ¦    ¦    ¦         for all-cargo operations.     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 26-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 5.  Portable Fire       D ¦ -  ¦ -  ¦ Any in excess of those required       ¦ ¦     Extinguishers         ¦    ¦    ¦ by FAR may be inoperative or          ¦ ¦                           ¦    ¦    ¦ missing provided:                     ¦ ¦                           ¦    ¦    ¦     a) The inoperative fire           ¦ ¦                           ¦    ¦    ¦        extinguisher is tagged         ¦ ¦                           ¦    ¦    ¦        inoperative, removed from      ¦ ¦                           ¦    ¦    ¦        the installed location, and    ¦ ¦                           ¦    ¦    ¦        placed out of sight so it      ¦ ¦                           ¦    ¦    ¦        cannot be mistaken for a       ¦ ¦                           ¦    ¦    ¦        functional unit, and           ¦ ¦                           ¦    ¦    ¦     b) Required distribution is       ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

¦ 6.  Cargo Compartment   C ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Fire Detection/       ¦    ¦    ¦ associated cargo compartment          ¦ ¦     Suppression Systems   ¦    ¦    ¦ remains empty.                        ¦

¦                           ¦    ¦    ¦ NOTE 1: Does not preclude the         ¦ ¦                           ¦    ¦    ¦         carriage of empty cargo       ¦ ¦                           ¦    ¦    ¦         containers, pallets,          ¦ ¦                           ¦    ¦    ¦         ballast or cargo restraint    ¦ ¦                           ¦    ¦    ¦         components.                   ¦

¦                           ¦    ¦    ¦ NOTE 2: Class E cargo components      ¦ ¦                           ¦    ¦    ¦         require only the              ¦ ¦                           ¦    ¦    ¦         installation of smoke or      ¦ ¦                           ¦    ¦    ¦         fire detection systems        ¦ ¦                           ¦    ¦    ¦         (not suppression).            ¦

¦     1) Ventral-Pod      C ¦ 4  ¦ 2  ¦ (O)One loop/detector (A or B) in      ¦ ¦        Baggage            ¦    ¦    ¦ each compartment may be               ¦ ¦        Compartment Bay/   ¦    ¦    ¦ inoperative.                          ¦ ¦        Aft Baggage Bay    ¦    ¦    ¦                                       ¦ ¦        Detection Loops/   ¦    ¦    ¦                                       ¦ ¦        Detectors          ¦    ¦    ¦                                       ¦

¦     2) Control Panel    C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦        Aural Warning      ¦    ¦    ¦ master warning CAP light and          ¦ ¦        Chime OFF          ¦    ¦    ¦ master warning operates normally.     ¦ ¦        (STC ST01086LA)    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 05/27/1993      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 1.  Control (Gust)      C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Lock System           ¦    ¦    ¦     a) System is secured and          ¦ ¦                           ¦    ¦    ¦        and verified unlocked,         ¦ ¦                           ¦    ¦    ¦     b) Full and free movement of      ¦ ¦                           ¦    ¦    ¦        flight controls is verified    ¦ ¦                           ¦    ¦    ¦        before each departure, and     ¦ ¦                           ¦    ¦    ¦     c) Airplane is not taxied with    ¦ ¦                           ¦    ¦    ¦        tailwind component greater     ¦ ¦                           ¦    ¦    ¦        than 20 knots.                 ¦

¦ 2.  CONT DISC (Control  C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦     Disconnect) Warning   ¦    ¦    ¦ control disconnect handles are        ¦ ¦     System                ¦    ¦    ¦ verified to be fully engaged before   ¦ ¦                           ¦    ¦    ¦ each departure.                       ¦

¦ 3.  Ground Spoiler      C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     System                ¦    ¦    ¦     a) System is deactivated,         ¦ ¦                           ¦    ¦    ¦     b) Reverse thrust, normal         ¦ ¦                           ¦    ¦    ¦        braking and anti-skid          ¦ ¦                           ¦    ¦    ¦        systems operate normally,      ¦ ¦                           ¦    ¦    ¦     c) Spoiler switch is set to       ¦ ¦                           ¦    ¦    ¦        ARM, and                       ¦ ¦                           ¦    ¦    ¦     d) Operations are conducted in    ¦ ¦                           ¦    ¦    ¦        accordance with the AFM.       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 05/27/1993      ¦ 27-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 4.  Ground (SPOILER)    C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Extend Caption        ¦    ¦    ¦     a) Spoiler operation is veri-     ¦ ¦                           ¦    ¦    ¦        fied to operate normally       ¦ ¦                           ¦    ¦    ¦        before departure, and          ¦ ¦                           ¦    ¦    ¦     b) Spoiler extend warnings        ¦ ¦                           ¦    ¦    ¦        L SPLR and R SPLR captions     ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦ 5.  Rudder Pedal        C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦     Adjustment System     ¦    ¦    ¦ rudder pedals can be secured in a     ¦ ¦                           ¦    ¦    ¦ position which meets individual       ¦ ¦                           ¦    ¦    ¦ pilot requirements.                   ¦

¦ 6.  Trim Tab Position   C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Indicators            ¦    ¦    ¦     a) Associated trim tab is         ¦ ¦     (Aileron & Rudder)    ¦    ¦    ¦        verified to operate            ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Trim tab is verified to be     ¦ ¦                           ¦    ¦    ¦        in the neutral position        ¦ ¦                           ¦    ¦    ¦        before each departure.         ¦

¦ 7.  Flap Position       A ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Indicator             ¦    ¦    ¦     a) Flaps are verified to          ¦ ¦                           ¦    ¦    ¦        operate normally before        ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 05/27/1993      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 1.  Fuel Quantity       B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Gages                 ¦    ¦    ¦     a) Fuel quantity is verified      ¦ ¦                           ¦    ¦    ¦        by other acceptable means      ¦ ¦                           ¦    ¦    ¦        after each refueling, and      ¦ ¦                           ¦    ¦    ¦     b) Both fuel flow meters/fuel     ¦ ¦                           ¦    ¦    ¦        used indicators and asso-      ¦ ¦                           ¦    ¦    ¦        ciated low fuel level warn-    ¦ ¦                           ¦    ¦    ¦        ing lights operate normally.   ¦

¦ 2.  Low Level Fuel      C ¦ 2  ¦ 0  ¦ May be inoperative provided fuel      ¦ ¦     Warning Lights        ¦    ¦    ¦ quantity gages operate normally.      ¦

¦ 3.  Fuel Crossfeed      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Light                 ¦    ¦    ¦     a) Crossfeed operation is         ¦ ¦                           ¦    ¦    ¦        verified to operate normally   ¦ ¦                           ¦    ¦    ¦        before each departure, and     ¦ ¦                           ¦    ¦    ¦     b) Both fuel pressure annuncia-   ¦ ¦                           ¦    ¦    ¦        tor lights, pressure gages     ¦ ¦                           ¦    ¦    ¦        and fuel quantity gages        ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦ 4.  Fuel Pressure       C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦     Gages                 ¦    ¦    ¦ both fuel flow gages and fuel low     ¦ ¦                           ¦    ¦    ¦ pressure warning lights operate       ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦ 5.  Fuel Low Pressure   C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     Lights                ¦    ¦    ¦ associated fuel pressure gages        ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/06/1996      ¦ 28-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 6.  Refuel Warning      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Light                 ¦    ¦    ¦     a) Refuel/Defuel Control Panel    ¦ ¦                           ¦    ¦    ¦        switches are verified OFF,     ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Refuel door is verified        ¦ ¦                           ¦    ¦    ¦        closed before each             ¦ ¦                           ¦    ¦    ¦        departure.                     ¦

¦ 7.  Refuel Valves       C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ refuel valves are verified closed.    ¦

¦ 8.  Refuel Control      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Panel                 ¦    ¦    ¦     a) Refuel valves are verified     ¦ ¦                           ¦    ¦    ¦        closed, and                    ¦ ¦                           ¦    ¦    ¦     b) Refuel/Defuel Control Panel    ¦ ¦                           ¦    ¦    ¦        switches are verified OFF.     ¦

¦ 9.  Refuel Valve Cap    D ¦ 1  ¦ 0  ¦ May be inoperative or missing         ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Receptacle is free of          ¦ ¦                           ¦    ¦    ¦        contamination before each      ¦ ¦                           ¦    ¦    ¦        refueling, and                 ¦ ¦                           ¦    ¦    ¦     b) No leakage exists after        ¦ ¦                           ¦    ¦    ¦        refueling.                     ¦

¦ 10. Fuel Tank           C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Temperature           ¦    ¦    ¦     a) Total Air Temperature or       ¦ ¦     Indicator             ¦    ¦    ¦        Static Air Temperature is      ¦ ¦                           ¦    ¦    ¦        substituted for indication     ¦ ¦                           ¦    ¦    ¦        of fuel temperature, and       ¦ ¦                           ¦    ¦    ¦     b) AFM limitations are            ¦ ¦                           ¦    ¦    ¦        observed.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/06/1996      ¦ 29-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 1.  Hydraulic Reser-    C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     voir Contents         ¦    ¦    ¦     a) All other hydraulic system     ¦ ¦     Gage                  ¦    ¦    ¦        indications and captions       ¦ ¦                           ¦    ¦    ¦        operate normally,              ¦ ¦                           ¦    ¦    ¦     b) No hydraulic leaks are         ¦ ¦                           ¦    ¦    ¦        evident,                       ¦ ¦                           ¦    ¦    ¦     c) Reservoir is fully serviced    ¦ ¦                           ¦    ¦    ¦        before first departure each    ¦ ¦                           ¦    ¦    ¦        flight day, and                ¦ ¦                           ¦    ¦    ¦     d) Hydraulic quantity sight       ¦ ¦                           ¦    ¦    ¦        gage is verified adequate      ¦ ¦                           ¦    ¦    ¦        before each departure.         ¦

¦ 2.  Hydraulic HIGH      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided all    ¦ ¦     Temperature           ¦    ¦    ¦ other hydraulic system indications    ¦ ¦     Warning Caption       ¦    ¦    ¦ and captions operate normally.        ¦

¦ 3.  Hydraulic Reser-    C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     voir LOW Emergency    ¦    ¦    ¦     a) All other hydraulic system     ¦ ¦     Contents Light        ¦    ¦    ¦        indications and captions       ¦ ¦                           ¦    ¦    ¦        operate normally,              ¦ ¦                           ¦    ¦    ¦     b) Reservoir is fully serviced    ¦ ¦                           ¦    ¦    ¦        before first departure, and    ¦ ¦                           ¦    ¦    ¦     c) No hydraulic leaks are         ¦ ¦                           ¦    ¦    ¦        evident.                       ¦

¦ 4.  Hydraulic Pump      C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     LO PRES Lights        ¦    ¦    ¦ the main hydraulic pressure           ¦ ¦                           ¦    ¦    ¦ indicator operates normally.          ¦

¦ 5.  Hydraulic Main      C ¦ 1  ¦ 0  ¦ May be inoperative provided both      ¦ ¦     System Pressure       ¦    ¦    ¦ hydraulic pump LO PRES lights and     ¦ ¦     Gage                  ¦    ¦    ¦ the hydraulic reservoir HI TEMP       ¦ ¦                           ¦    ¦    ¦ light operate normally.               ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 30-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 1.  Windshield Heating  C ¦ 4  ¦ 3  ¦ One may be inoperative provided       ¦ ¦     Systems               ¦    ¦    ¦ left outboard system operates         ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦                         C ¦ 4  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Aircraft is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) Windscreen demist system       ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 2.  Propeller De-ice    C ¦ 2  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     System                ¦    ¦    ¦ airplane is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 3.  Pitot Heaters       B ¦ 2  ¦ 1  ¦ One may be inoperative for day        ¦ ¦     (No.1 and 2)          ¦    ¦    ¦ VMC conditions only.                  ¦

¦ 4.  Pitot Heater        B ¦ 3  ¦ 2  ¦ (M)One may be inoperative provided:   ¦ ¦     Failure Lights        ¦    ¦    ¦     a) Associated pitot heater is     ¦ ¦                           ¦    ¦    ¦        verified to operate            ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) CAP collector caption          ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦                         B ¦ 3  ¦ 0  ¦ (M)May be inoperative privided:     | ¦ ¦                           ¦    ¦    ¦     a) All other elements of the    | ¦ ¦                           ¦    ¦    ¦        pitot heat system operate    | ¦ ¦                           ¦    ¦    ¦        normally, and                | ¦ ¦                           ¦    ¦    ¦     b) The airplane is not operated | ¦ ¦                           ¦    ¦    ¦        in known or forecast icing   | ¦ ¦                           ¦    ¦    ¦        conditions.                  | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 30-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 5.  TAT Probe Heater    C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦                           ¦    ¦    ¦ airplane is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forcast icing conditions.          ¦

¦ 6.  Ice Detector        C ¦ 1  ¦ 0  ¦                                       ¦

¦ 7.  Static Plate        B ¦ 2  ¦ 1  ¦ One may be inoperative for day VMC    ¦ ¦     Heater                ¦    ¦    ¦ conditions only.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 30-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 8.  Windshield Wipers   C ¦ 2  ¦ 0  ¦ May be inoperative provided the       ¦ ¦                           ¦    ¦    ¦ airplane is not operated in           ¦ ¦                           ¦    ¦    ¦ precipitation within five nautical    ¦ ¦                           ¦    ¦    ¦ miles of the airport of takeoff or    ¦ ¦                           ¦    ¦    ¦ intended landing.                     ¦

¦     1) Fast Speed       C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦        Function           ¦    ¦    ¦     a) Associated slow speed func-    ¦ ¦                           ¦    ¦    ¦        tion operates normally, and    ¦ ¦                           ¦    ¦    ¦     b) Approach minimums do not       ¦ ¦                           ¦    ¦    ¦        require their use.             ¦

¦     2) Slow Speed       C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦        Function           ¦    ¦    ¦ associated fast speed function        ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦ 9.  Windshield Washers  D ¦ 2  ¦ 0  ¦                                       ¦

¦ 10. Airframe De-ice     B ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     (Wing, Vertical       ¦    ¦    ¦ airplane is not operated in known     ¦ ¦     and Horizontal        ¦    ¦    ¦ or forecast icing conditions.         ¦ ¦     Stabilizers)          ¦    ¦    ¦                                       ¦

¦ 11. Airframe De-ice       ¦    ¦    ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦     1) Automatic        B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Control Function   ¦    ¦    ¦     a) Manual control is verified     ¦ ¦                           ¦    ¦    ¦        to operate normally, and       ¦ ¦                           ¦    ¦    ¦     b) CCTs, ICE and FAULT indica-    ¦ ¦                           ¦    ¦    ¦        tions operate normally.        ¦

¦     2) Manual Control   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Function           ¦    ¦    ¦     a) Automatic control is veri-     ¦ ¦                           ¦    ¦    ¦        fied to operate normally,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) CCTs, ICE and FAULT indica-    ¦ ¦                           ¦    ¦    ¦        tions operate normally.        ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 30-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 12. Airframe De-ice     B ¦ 3  ¦ 2  ¦ (M)(O)One may be inoperative          ¦ ¦     Circuit Lights        ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Airframe De-ice system is      ¦ ¦                           ¦    ¦    ¦        verified to operate            ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Airframe De-ice FAULT and      ¦ ¦                           ¦    ¦    ¦        LO PRESS captions operate      ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 13. Windshield Heating  C ¦ 4  ¦ 3  ¦ (O)One may be inoperative provided:   ¦ ¦     Lights                ¦    ¦    ¦     a) Amber ICE CAP caption          ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) All other ice protection       ¦ ¦                           ¦    ¦    ¦        warnings operate normally.     ¦

¦                         C ¦ 4  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Airplane is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) Windscreen demist system       ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 14. Engine Anti-ice     C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Failure Lights        ¦    ¦    ¦     a) Amber ICE CAP caption          ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) All other ice protection       ¦ ¦                           ¦    ¦    ¦        warnings operate normally.     ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided the       ¦ ¦                           ¦    ¦    ¦ airplane is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 30-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 15. Propeller De-ice    C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Failure Lights        ¦    ¦    ¦     a) Amber ICE CAP caption          ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) All other ice protection       ¦ ¦                           ¦    ¦    ¦        warnings operate normally.     ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided the       ¦ ¦                           ¦    ¦    ¦ airplane is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 16. Elevator Anti-ice   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Failure Lights        ¦    ¦    ¦     a) Amber ICE CAP caption          ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) All other ice protection       ¦ ¦                           ¦    ¦    ¦        warnings operate normally.     ¦

¦ 17. Static Plate        B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Heater Failure        ¦    ¦    ¦     a) Amber ICE CAP caption          ¦ ¦     Lights                ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     b) All other ice protection       ¦ ¦                           ¦    ¦    ¦        warnings operate normally,     ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Associated heater plate is     ¦ ¦                           ¦    ¦    ¦        verified to operate            ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 18. Elevator Horn       B ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Anti-Ice System       ¦    ¦    ¦ airplane is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 31-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 1.  Clocks              C ¦ 2  ¦ 1  ¦ One may be inoperative at either      ¦ ¦                           ¦    ¦    ¦ the pilot or copilot station.         ¦

¦ 2.  Flight Data         C ¦ -  ¦ 1  ¦ Any in excess of those required     | ¦ ¦     Recorder (FDR)        ¦    ¦    ¦ by FAR may be inoperative.          | ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦     1) Flight Data      A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦        Recorder (FDR)     ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR)   ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     b) Airplane is not dispatched     ¦ ¦                           ¦    ¦    ¦        from a designated airport      ¦ ¦                           ¦    ¦    ¦        where repairs or replace-      ¦ ¦                           ¦    ¦    ¦        ments can be made, and         ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

¦     2) FDR Recording    A ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦        Parameters         ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR)   ¦ ¦        required by FAR    ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        20 claendar days.              ¦

¦     3) FDR Recording    A ¦ -  ¦ -  ¦ May be inoperative provided repairs   ¦ ¦        Parameters         ¦    ¦    ¦ are made prior to the completion      ¦ ¦        not required       ¦    ¦    ¦ of the next heavy maintenance         ¦ ¦        by FAR             ¦    ¦    ¦ visit.                                ¦

¦ 3.  Crew Checklist      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦ *** System                ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 4        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 01/22/2001      ¦ 31-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 4.  CAP Dim Facility    C ¦ 1  ¦ 0  ¦ May be inoperative provided bright    ¦ ¦                           ¦    ¦    ¦ mode is available for day             ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦ 5.  CAP MUTE Facility   D ¦ 1  ¦ 0  ¦ May be inoperative provided it has    ¦ ¦                           ¦    ¦    ¦ failed in the unmute position.        ¦

¦ 6.  Master WARNING      C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦     Lights                ¦    ¦    ¦ master warning aural alert and all    ¦ ¦                           ¦    ¦    ¦ discrete warning lights operate       ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦ 7.  Master CAUTION      C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦     Lights                ¦    ¦    ¦ master caution aural alert and all    ¦ ¦                           ¦    ¦    ¦ discrete caution lights operate       ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 32-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦ 1.  Normal Brake        C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Pressure Gage         ¦    ¦    ¦     a) Normal brake pressure warn-    ¦ ¦                           ¦    ¦    ¦        ing light operates normally,   ¦ ¦                           ¦    ¦    ¦     b) Emergency brakes are veri-     ¦ ¦                           ¦    ¦    ¦        fied to operate normally,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Symmetric braking is veri-     ¦ ¦                           ¦    ¦    ¦        fied before departure.         ¦

¦ 2.  Normal Brake Pres-  C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     sure Warning Light    ¦    ¦    ¦ both normal brake pressure gauges     ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

¦ 3.  Emergency Brake     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Pressure Gage         ¦    ¦    ¦     a) Emergency brake pressure       ¦ ¦                           ¦    ¦    ¦        warning light operates         ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Normal brakes operate          ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 4.  Emergency Brake     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Pressure Warning      ¦    ¦    ¦ emergency brake pressure gauge        ¦ ¦     Light                 ¦    ¦    ¦ operates normally.                    ¦

¦ 5.  Landing Gear Posi-    ¦    ¦    ¦                                       ¦ ¦     tion Indicators       ¦    ¦    ¦                                       ¦

¦     1) Normal Downlock  B ¦ 1  ¦ 0  ¦ Down and locked (green) lights may    ¦ ¦        Indicators         ¦    ¦    ¦ be inoperative provided all Standby   ¦ ¦                           ¦    ¦    ¦ lights (green) operate normally.      ¦

¦     2) Standby Down-    B ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦        lock Indicators    ¦    ¦    ¦ normal lights operate normally.       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/02/2004      ¦ 32-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦ 6. Anti-Skid System       ¦    ¦    ¦                                     | ¦ ¦    (Includes              ¦    ¦    ¦                                     | ¦ ¦    Annunciator Lights)    ¦    ¦    ¦                                     | ¦

¦    1) Dry Runways       B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ operations are conducted in         | ¦ ¦                           ¦    ¦    ¦ compliance with AFM.                | ¦

¦    2) Wet Runways       B ¦ 1  ¦ 0  ¦ (O)May be inoperative privided      | ¦ ¦       (No standing water  ¦    ¦    ¦    a)Operations are limited to      | ¦ ¦       in area of takeoff  ¦    ¦    ¦      utilization of PFCO or         | ¦ ¦       ground roll, no     ¦    ¦    ¦      grooved runways,               | ¦ ¦       snow, no icy        ¦    ¦    ¦    b)Thrust Reversers operate       | ¦ ¦       runway conditions.) ¦    ¦    ¦      normally,                      | ¦ ¦                           ¦    ¦    ¦    c)Acceptable Performance Data    | ¦ ¦                           ¦    ¦    ¦      from an Analysis of the        | ¦ ¦                           ¦    ¦    ¦      Accelerate Stop Capability     | ¦ ¦                           ¦    ¦    ¦      on wet Runway Surfaces is      | ¦ ¦                           ¦    ¦    ¦      developed amd used,            | ¦ ¦                           ¦    ¦    ¦    d)The cross wind component for   | ¦ ¦                           ¦    ¦    ¦      both departure and arrival     | ¦ ¦                           ¦    ¦    ¦      runways is forecast to be 15   | ¦ ¦                           ¦    ¦    ¦      knots or less,                 | ¦ ¦                           ¦    ¦    ¦    e)Acceptable Performance Data    | ¦ ¦                           ¦    ¦    ¦      Report is referenced in the    | ¦ ¦                           ¦    ¦    ¦      Operator's  Minimum Equipment  | ¦ ¦                           ¦    ¦    ¦      List (MEL) by Report Name,     | ¦ ¦                           ¦    ¦    ¦      Number, Revision Number, and   | ¦ ¦                           ¦    ¦    ¦      Acceptance Date,               | ¦ ¦                           ¦    ¦    ¦    f)Performance Data Report        | ¦ ¦                           ¦    ¦    ¦      assumes that reverse thrust    | ¦ ¦                           ¦    ¦    ¦      action is terminated at        | ¦ ¦                           ¦    ¦    ¦      60 knots, and                  | ¦ ¦                           ¦    ¦    ¦    g)Wet runway landing operations  | ¦ ¦                           ¦    ¦    ¦      are conducted in accordance    | ¦ ¦                           ¦    ¦    ¦      with available landing         | ¦ ¦                           ¦    ¦    ¦      performance data in the AFM.   | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/06/1996      ¦ 33-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 1.  Cockpit/Flight      C ¦ -  ¦ -  ¦ Individual lights may be inopera-     ¦ ¦     Deck/Flight Compart-  ¦    ¦    ¦ tive provided remaining lights are:   ¦ ¦     ment and Instrument   ¦    ¦    ¦     a) Sufficient to clearly          ¦ ¦     Lighting System       ¦    ¦    ¦        illuminate all required        ¦ ¦                           ¦    ¦    ¦        instruments, controls, and     ¦ ¦                           ¦    ¦    ¦        other devices for which it     ¦ ¦                           ¦    ¦    ¦        is provided,                   ¦ ¦                           ¦    ¦    ¦     b) Positioned so that direct      ¦ ¦                           ¦    ¦    ¦        rays are shielded from         ¦ ¦                           ¦    ¦    ¦        flight crewmember's eyes,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Lighting configuration and     ¦ ¦                           ¦    ¦    ¦        intensity is acceptable to     ¦ ¦                           ¦    ¦    ¦        the flight crew.               ¦

¦ 2.  Position Lights     C ¦ -  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦                         C ¦ -  ¦ 3  ¦ For night operations, all except      ¦ ¦                           ¦    ¦    ¦ the following minimum may be          ¦ ¦                           ¦    ¦    ¦ inoperative:                          ¦ ¦                           ¦    ¦    ¦     a) One stationary red wing tip    ¦ ¦                           ¦    ¦    ¦        light,                         ¦ ¦                           ¦    ¦    ¦     b) One stationary green wing      ¦ ¦                           ¦    ¦    ¦        tip light, and                 ¦ ¦                           ¦    ¦    ¦     c) One stationary white light     ¦ ¦                           ¦    ¦    ¦        at base of tail.               ¦

¦ 3.  Landing Lights      C ¦ 2  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦                         C ¦ 2  ¦ 1  ¦ One may be inoperative for night      ¦ ¦                           ¦    ¦    ¦ operations provided taxi light        ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦ 4.  Conspicuity Lights  C ¦ 2  ¦ 0  ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 05/27/1993      ¦ 33-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 5.  Taxi Light          C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦                           ¦    ¦    ¦ operations provided both landing      ¦ ¦                           ¦    ¦    ¦ lights operate normally.              ¦

¦ 6.  Baggage Compart-    C ¦ 2  ¦ 0  ¦                                       ¦ ¦     ment Lights (Main     ¦    ¦    ¦                                       ¦ ¦     and Ventral)          ¦    ¦    ¦                                       ¦

¦ 7.  Cabin Interior      C ¦ -  ¦ -  ¦ Individual lights may be inopera-     ¦ ¦     Normal Lighting       ¦    ¦    ¦ tive provided remaining lighting      ¦ ¦     System                ¦    ¦    ¦ is sufficient for cabin attendants    ¦ ¦                           ¦    ¦    ¦ to perform their duties.              ¦

¦ 8.  Beacon              B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     (Red Strobe)          ¦    ¦    ¦ adequate precautions are taken to     ¦ ¦                           ¦    ¦    ¦ clear the area before engine start,   ¦ ¦                           ¦    ¦    ¦ and while engines are running.        ¦

¦ 9.  Anti-collision      C ¦ 2  ¦ 0  ¦ May be inoperative for day            ¦ ¦     Lights (White)        ¦    ¦    ¦ operations.                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/08/1994      ¦ 33-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 10. Passenger Notice    C ¦ -  ¦ -  ¦ (M)No passenger seat or cabin         ¦ ¦     System ("No           ¦    ¦    ¦ attendant seat may be occupied from   ¦ ¦     Smoking/Fasten        ¦    ¦    ¦ which a "No Smoking/Fasten Seat       ¦ ¦     Belt" Sign)           ¦    ¦    ¦ Belt" sign is not readily legible,    ¦ ¦                           ¦    ¦    ¦ or that seat must be blocked and      ¦ ¦                           ¦    ¦    ¦ placarded - "DO NOT OCCUPY".          ¦

¦                         C ¦ -  ¦ -  ¦ (O)If one or more "No Smoking/        ¦ ¦                           ¦    ¦    ¦ Fasten Seat Belt" signs are           ¦ ¦                           ¦    ¦    ¦ inoperative, the affected passenger   ¦ ¦                           ¦    ¦    ¦ seat(s) or cabin attendant seat(s)    ¦ ¦                           ¦    ¦    ¦ may be occupied provided:             ¦ ¦                           ¦    ¦    ¦     a) Passenger Address System is    ¦ ¦                           ¦    ¦    ¦        operating normally and can     ¦ ¦                           ¦    ¦    ¦        be clearly heard throughout    ¦ ¦                           ¦    ¦    ¦        the cabin during flight, and   ¦ ¦                           ¦    ¦    ¦     b) An acceptable procedure is     ¦ ¦                           ¦    ¦    ¦        used to notify passengers      ¦ ¦                           ¦    ¦    ¦        when seat belts must be        ¦ ¦                           ¦    ¦    ¦        fastened and smoking is        ¦ ¦                           ¦    ¦    ¦        prohibited.                    ¦

¦                           ¦    ¦    ¦ NOTE: Not required for all-cargo      ¦ ¦                           ¦    ¦    ¦       operations unless cargo         ¦ ¦                           ¦    ¦    ¦       carriage requires persons       ¦ ¦                           ¦    ¦    ¦       to be in attendance in main     ¦ ¦                           ¦    ¦    ¦       cargo compartment.              ¦

¦ 11. Logo Lights         D ¦ -  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3 a      ¦ PAGE:    ¦ ¦                 BA-4100                  ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/11/1996      ¦ 33-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 12. Ice Observation     C ¦ 2  ¦ 0  ¦ May be inoperative for night          ¦ ¦     Lights                ¦    ¦    ¦ operations provided airplane is       ¦ ¦                           ¦    ¦    ¦ not operated in known or forecast     ¦ ¦                           ¦    ¦    ¦ icing conditions.                     ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦ 13. External Emergency  B ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     Lighting System       ¦    ¦    ¦ operations.                           ¦

¦ 14. Floor Proximity     C ¦ 1  ¦ 1  ¦ Individual lights may be nopera-      ¦ ¦     Emergency Escape      ¦    ¦    ¦ tive provided FAA approved minimum    ¦ ¦     Path Marking System   ¦    ¦    ¦ acceptable lighting levels specif-    ¦ ¦                           ¦    ¦    ¦ ied in one of the following           ¦ ¦                           ¦    ¦    ¦ documents are complied with:          ¦ ¦                           ¦    ¦    ¦     a) FAA engineering approval       ¦ ¦                           ¦    ¦    ¦        letter.                        ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     b) FAA approved report of the     ¦ ¦                           ¦    ¦    ¦        Type Design holder.            ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     c) Limitations and Conditions     ¦ ¦                           ¦    ¦    ¦        section of the applicable      ¦ ¦                           ¦    ¦    ¦        Supplemental Type              ¦ ¦                           ¦    ¦    ¦        Certificate (STC).             ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     d) An FAA approved report         ¦ ¦                           ¦    ¦    ¦        incorporated in the Master     ¦ ¦                           ¦    ¦    ¦        Drawing List for the           ¦ ¦                           ¦    ¦    ¦        applicable STC.                ¦

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