DEPARTMENT OF TRANSPORTATION     Revision: 5

Date: 12/27/95

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

Grumman G-159 Models

Federal Aviation Administration

Flight Standards Division

AIRCRAFT EVALUATION GROUP, LGB AEG

3960 PARAMOUNT BLVD.

LAKEWOOD, CA 90712-4137

TELEPHONE:  (310) 627-5272

FAX:  (310) 627-5281



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Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II

--     Control Page                            III, IV

--     Highlights of Change                    V

--     Definitions                             VI, VII, VIII, IX --     Definitions                             X, XI, XII, XIII --     Preamble                                XIV, XV

21     Air Conditioning                        21-1, 2, 3, 4, 5 21     Air Conditioning                        21-6, 7

22     Auto Flight                             22-1

23     Communications                          23-1, 2, 3, 4

24     Electrical Power                        24-1, 2, 3, 4

25     Equipment/Furnishings                   25-1, 2, 3, 4

26     Fire Protection                         26-1, 2, 3

27     Flight Controls                         27-1

28     Fuel                                    28-1, 2, 3

29     Hydraulic Power                         29-1

30     Ice and Rain Protection                 30-1, 2

31     Indicating/Recording Systems            31-1

32     Landing Gear                            32-1

33     Lights                                  33-1, 2, 3, 4

34     Navigation                              34-1, 2, 3, 4, 5 34     Navigation                              34-6, 7

35     Oxygen                                  35-1

49     Airborne Auxiliary Power                49-1, 2 52     Doors                                   52-1

61     Propellers                              61-1 73     Engine Fuel & Control                   73-1 77     Engine Indicating                       77-1 79     Engine Oil                              79-1 80     Starting                                80-1 82     Water Injection                         82-1



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Log of Revisions

| REV.NO.  |  DATE      | PAGE NUMBERS                   | INITIALS  |

| 5        | 12/27/95   | ALL PAGES                      |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |           |                                |           | |          |            |                                |           | Page 2

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|          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |           |                                |           | |          |            |                                |           | |          |            |                                |           | |         |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |           |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           |



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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       5        12/27/95 Table of Contents                        I       5        12/27/95 Log of Revisions                         II      5        12/27/95 Control Page                             III     5        12/27/95 IV      5        12/27/95 Highlights of Change                     V       5        12/27/95 Definitions                              VI      6        01/31/95 VII     6        01/31/95 VIII    6        01/31/95 IX      6        01/31/95 Page 3

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   X       6        01/31/95 XI      6        01/31/95 XII     6        01/31/95 XIII    6        01/31/95 Preamble                                 XIV     2        06/14/89 XV      2        06/14/89 21                                       21-1    5        12/27/95 21-2    5        12/27/95 21-3    5        12/27/95 21-4      5        12/27/95 21-5    5        12/27/95    21-6    5        12/27/95 21-7    5        12/27/95 22                                       22-1    5        12/27/95 23                                             23-1    5        12/27/95 23-2    5        12/27/95 23-3    5        12/27/95 23-4    5        12/27/95 24                                       24-1    5        12/27/95 24-2    5        12/27/95 24-3    5        12/27/95 24-4    5        12/27/95 25                                       25-1      5        12/27/95 25-2    5        12/27/95    25-3    5        12/27/95 25-4    5        12/27/95 26                                       26-1    5        12/27/95 26-2    5        12/27/95 26-3    5        12/27/95 27                                       27-1    5                                              12/27/95



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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

28                                       28-1    5        12/27/95 28-2    5        12/27/95 28-3    5        12/27/95 29                                       29-1    5        12/27/95 30                                       30-1    5        12/27/95 30-2    5        12/27/95 31                                       31-1    5        12/27/95 32                                       32-1    5        12/27/95 33                                       33-1    5        12/27/95 33-2    5        12/27/95 33-3    5        12/27/95 33-4    5        12/27/95 34                                       34-1      5        12/27/95 34-2    5        12/27/95    34-3    5        12/27/95 34-4    5             12/27/95 34-5    5        12/27/95 Page 4

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   34-6    5        12/27/95 34-7    5        12/27/95 35                                       35-1    5        12/27/95 49                                             49-1    5        12/27/95 49-2    5        12/27/95 52                                       52-1    5        12/27/95 61                                       61-1    5        12/27/95 73                                             73-1    5        12/27/95 77                                       77-1    5        12/27/95 79                                             79-1    5        12/27/95 80                                       80-1    5        12/27/95 82                                       82-1    5        12/27/95



FEDERAL AVIATION ADMINISTRATION   Page: V

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MASTER MINIMUM EQUIPMENT LIST    Date: 12/27/95

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Highlights of Change

EFFECTIVE ABOVE DATE, the Gulfstream G-159 Master Minimum Equipment List (MMEL) is revised. Revision 5 is a STANDARD revision which is the result of a public Flight Operations Evaluation Board (FOEB) meeting held on September 15, 1994 to consider approximately 400 proposals for MMEL relief. Many new items are given relief in this revision. Some relief that was granted in the past has been removed as a result of FAA policy changes since the last MMEL revision. FAA Policy Letters 1-78 and FAA Global Changes 2-26 have been reviewed and incorporated in this revision This revision also incorporates the four column MMEL format and Category A-D repair intervals.

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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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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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Definitions

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

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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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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

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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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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.                                            | |

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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)                                           |



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     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

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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



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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

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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.

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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.



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | Page 14

G159R5.txt

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G159R5.txt

| FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 21-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Cabin Blower          |    |    |                                       | |                           |    |    |                                       | |      1) Pressurized     C | 1  | 0  | (M)(O)May be inoperative provided:  | | |         Configuration     |    |    |     a) Blower Dump System is        | | |                           |    |    |        operative,                   | | |                           |    |    |     b) APU is operative, and        | | |                           |    |    |     c) APU Air Load System is       | | |                           |    |    |        operative.                   | | |                           |    |    |           OR                        | | |                         C |    |    |     d) Blower drive shaft is        | | |                           |    |    |        removed,                     | | |                           |    |    |     e) APU is operative, and        | | |                           |    |    |     f) APU Air Load System is       | | |                           |    |    |        operative.                   | | |                           |    |    |                                       | |      2) Unpressurized   C | 1  | 0  | (M)(O)May be inoperative provided:  | | |         Configuration     |    |    |     a) Blower Dump System is        | | |                           |    |    |        operative, and               | | |                           |    |    |     b) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |           OR                        | | |                         C |    |    |     c) Blower drive shaft is        | | |                           |    |    |        removed, and                 | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | Page 15

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|                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 21-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -2  Cabin Pressure      C | 1  | 0  | (M)(O)May be inoperative provided:  | | |     Warning System        |    |    |     a) Cabin Altitude Indicator is  | | |                           |    |    |        operative, and               | | |                           |    |    |     b) Manual Pressure Control      | | |                           |    |    |        System is operative.         | | |                           |    |    |          OR                         | | |                         C |    |    |     c) Aircraft is operated in      | | |                           |    |    |        unpressurized configuration, | | |                           |    |   |        and                          | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | |                         C | 1  | 0  | (M)(O)May be inoperative provided:  | | |                           |    |    |     a) Cabin Differential Pressure  | | |                           |    |    |        Indicator is operative, and  | | |                           |    |    |     b) Manual Pressure Control      | | |                           |    |    |        System is operative.         | | |                           |    |    |           OR                        | | |                         C |    |    |     c) Aircraft is operated in      | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |        and                          | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 21-3     | | --------------------------------------------------------------------------- | Page 16

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|                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |   -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -3  Cockpit Temperature C | 4  | 0  | (O)All may be inoperative provided: | | |     Control System &      |    |    |     a) Aircraft is operated in      | | |     Cabin Temperature     |    |    |        unpressurized configuration, | | |     Control Systems       |    |   |        and                          | | |                           |    |    |     b) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | |      1) Automatic       C | 2  | 0  | Both Systems may be inoperative     | | |         Systems           |    |    | provided:                           | | |                           |    |    |     a) Associated Manual Control    | | |                           |    |    |        System is operative, and     | | |                           |    |    |     b) Cabin Temperature Indicator  | | |                           |    |    |        is operative.                | | |                           |    |    |                                       | |      2) Manual Systems  C | 2  | 0  | Both Systems may be inoperative     | | |                           |    |    | provided:                           | | |                           |    |    |   a) Associated Automatic Control   | | |                           |    |    |      System is operative, and       | | |                           |    |    |   b) Cabin Temperature Indicator    | | |                           |    |    |        is operative.                | | |                           |    |    |                                       | | -4  Cabin Pressure      C | 1  | 0  | (O)May be inoperative provided:     | | |     Differential          |    |    |     a) Cabin Altitude Indicator is  | | |     Indicator             |    |    |        operative, and               | | |                           |    |    |     b) A chart is provided for the  | | |                           |    |    |        crew to convert Cabin        | | |                           |    |    |        Altitude to Differential     | | |                           |    |    |        Pressure.                    | | |                           |    |    |           OR                        | | |                         C |    |    |     c) Aircraft is operated in      | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |        and                          | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 21-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | Page 17

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| NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -5  Blower Dump System    |    |    |                                       | |                           |    |    |                                       | |     1) Pressurized      C | 1  | 0  | (M)May be inoperative provided:     | | |        Configuration      |    |    |     a) Spill valve is secured OPEN, | | |                           |    |    |     b) APU is operative, and        | | |                           |    |    |     c) APU Air Load System is       | | |                           |    |    |        operative.                   | | |                         C |    |    |           OR                        | | |                           |    |    |     d) Blower drive shaft is        | | |                           |    |    |        REMOVED,                     | | |                           |    |    |     e) APU is operative, and        | | |                           |    |    |     f) APU Air Load System is       | | |                           |    |    |        operative.                   | | |                           |    |    |                                       | |     1) Unpressurized    C | 1  | 0  | (M)(O)May be inoperative provided:  | | |        Configuration      |    |    |     a) Spill valve is secured OPEN, | | |                           |    |    |        and                          | | |                           |    |    |     b) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |           OR                        | | |                         C |    |    |     c) Blower Drive Shaft is        | | |                           |    |    |        removed, and                 | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | | -6  Cockpit Temperature C | 1  | 0  | May be inoperative provided:        | | | *** Indicator             |    |    |     a) Cockpit Automatic            | | |                           |    |    |        Temperature Control System   | | |                           |    |    |        is operative, and            | | |                           |    |    |     b) Cabin Temperature indicator  | | |                           |    |    |        is operative.                | | |                           |    |    |                                       | | -7  Ground Cooling Fan  C | 1  | 0  | (M)(O)May be inoperative provided:  | | |     System                |    |    |     a) Ram Air Limiter doors are    | | |                           |    |    |        secured in full OPEN         | | |                           |    |    |        position, and                | | |                           |    |    |     b) APU Air Load System is       | | |                           |    |    |        utilized inflight only.      | | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 21-5     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | Page 18

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|                           |    |    |                                       | |                           |    |    |                                       | | -8  Cabin Temperature   C | 1  | 0  | May be inoperative provided:        | | |     Indicator             |    |    |     a) Cabin Automatic Temperature  | | |                           |    |    |        Control System is operative, | | |                           |    |    |           OR                        | | |                         C |    |    |     b) Cabin Manual Temperature     | | |                           |    |    |        Control System is operative. | | |                           |    |    |                                       | | -9  Cooling Turbine     C | 1  | 0  | (0)May be inoperative provided:     | | |                           |    |    |     a) Aircraft is operated in an   | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |     b) Blower Dump System is        | | |                           |    |    |        operative, and               | | |                           |    |    |     c) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |           OR                        | | |                         C |    |    |     d) Aircraft is operated in an   | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |     e) Blower drive shaft is        | | |                           |    |    |        removed,                     | | |                           |    |    |     f) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | | -10 Outflow Valve       C | 1  | 0  | (M)(O)May be inoperative provided:  | | |     System                |    |    |     a) Valve is secured OPEN,       | | |                           |    |    |     b) Blower Dump System is        | | |                           |    |    |        operative,                   | | |                           |    |    |     c) Aircraft is operated in      | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |        and                          | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 21-6     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -11 Safety Valve        C | 1  | 0  | (M)(O)May be inoperative provided:  | | Page 19

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|                           |    |    |     a) Valve is secured OPEN,       | | |                           |    |    |     b) Blower Dump System is        | | |                           |    |    |        operative,                   | | |                           |    |    |     c) Aircraft is operated in      | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |        and                          | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | | -12 Cabin Altitude      C | 1  | 0  | (O)May be inoperative provided:     | | |     Indication System     |    |    |     a) Cabin Differential Pressure  | | |                           |    |    |        Indicator is operative, and  | | |                           |    |    |     b) A chart is provided for the  | | |                           |    |    |        crew to convert differential | | |                           |    |    |        pressure to cabin altitude.  | | |                           |    |    |           OR                        | | |                         C |    |    |     c) Aircraft is operated in      | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |        and                          | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | | -13 Cabin Rate of Climb C | 1  | 0  | May be inoperative provided:        | | |     Indication System     |    |    |     a) Cabin Altitude Indicator is  | | |                           |    |    |        operative, and               | | |                           |    |    |     b) Automatic Cabin Pressure     | | |                           |    |    |        Control System is operative. | | |                           |    |    |           OR                        | | |                         C |    |    |     c) Aircraft is operated in      | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |        and                          | | |                           |    |    |     d) Aircraft is operated at or   | | |                           |    |    |        below 10,000 feet.           | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 21-7     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -14 Automatic Cabin     C | 1  | 0  | (O)May be inoperative provided:     | | |     Pressure Control      |    |    |     a) Cabin Altitude Indicator is  | | |     System                |    |    |        operative,                   | | |                           |    |    |     b) Cabin Differential Pressure  | | Page 20

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|                           |    |    |        Indicator is operative,      | | |                           |    |    |     c) Cabin Rate of Climb          | | |                           |    |    |        Indicator is operative, and  | | |                           |    |    |     d) Cabin Pressure Warning       | | |                           |    |    |        System is operative.         | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 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    C | 1  | 0  | (M)(O)May be inoperative provided   | | | ***                       |    |    | approach procedures do not require  | | |                           |    |    | its use.                            | | |                           |    |    |                                       | | -2  Yaw Damper System   C | 1  | 0  | (M)                                 | | |                           |    |    |                                       | Page 21

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| -3  Yaw Damper Engage   C | 1  | 0  | (O)May be inoperative provided Yaw  | | | *** Indication System     |    |    | Damper is considered inoperative.   | | |                           |    |    |                                       | | -4  Electric Trim       C | -  | 0  | (M)May be inoperative provided:     | | | *** Systems               |    |    |     a) System(s) are mechanically   | | |                           |    |    |        and electrically locked out, | | |                           |    |    |        and                          | | |                           |    |    |     b) All Mechanical Trim Systems  | | |                           |    |    |        are operative.               | | |                           |    |    |                                       | | -5  Autopilot Engage    C | 1  | 0  | (O)May be inoperative provided      | | | *** Indication System     |    |    | autopilot system is also made       | | |                           |    |    | inoperative.                        | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 23-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Communication       C | -  | -  | As required by FAR and no relief    | | |     Systems (VHF, HF,     |    |    | may be provided to an inoperative   | | |     UHF)                  |    |    | system or component if powered by   | | |                           |    |    | an emergency bus or equivalent and  | | |                           |    |    | required to accomplish an emergency | | |                           |    |    | procedure.                          | | |                           |    |    |                                       | | -2  Cockpit to Cockpit    |    |    | DELETED, Rev. 5.                    | | Page 22

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|     Interphone System     |    |    |                                     | | |                           |    |    |                                       | | -3  Cockpit Cabin         |    |    |                                       | | *** Interphone Systems    |    |    |                                       | |                           |    |    |                                       | |      1) Passenger       C | -  | 0  | May be inoperative provided paging  | | |         Configuration     |    |    | (PA) system is operative on         | | |                           |    |    | passenger carrying flights.         | | |                           |    |    |                                       | |      2) Cargo           C | -  | 0  |                                     | | |         Configuration     |    |    |                                     | | |                           |    |    |                                       | | -4  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 Deck/Cabin Interphone | | |                           |    |    |        system operates normally.    | | |                           |    |    |                                       | | ***  2) Cargo           D | 1  | 0  |                                     | | |         Configuration     |    |    |                                     | | |                           |    |    |                                       | | -5  Cabin to Cabin      C | -  | 0  |                                     | | | *** Interphone System     |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 23-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -6  Prerecorded         C | -  | 0  | (O)May be inoperative provided      | | | *** Passenger             |    |    | alternate procedures are            | | |     Announcement          |    |    | established and used.               | | |     Systems               |    |    |                                     | | |                           |    |    |                                       | | -7  Hand Held           C | -  | 0  | May be inoperative provided:        | | |     Microphones           |    |    |     a) Each cockpit crewmember uses | | |                           |    |    |        a boom microphone, and       | | |                           |    |    |     b) Each (Control Wheel) Press-  | | |                           |    |    |        to-Talk Switch is operative. | | |                           |    |    |                                       | Page 23

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|                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 23-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -8  Boom Microphones      |    |    |                                     | | |                           |    |    |                                     | | | Cockpit Voice Recorder    |    |    |                                     | | | and Flight Data           |    |    |                                     | | | Recorder Installed        |    |    |                                     | | |                           |    |    |                                     | | |      1) Cockpit Voice   A | -  | 0  | May be inoperative provided:        | | |         Recorder          |    |    |     a) Flight Data Recorder         | | |         Equipped To       |    |    |        operates normally, and       | | |         Record Boom       |    |    |     b) Repairs are made within      | | |         Microphone per    |    |    |        three flight days.           | | |         FAR 121.139(e),   |    |    |                                     | | |         135.151(d) or     |    |    |                                     | | |         125.227(e)        |    |    |                                     | | Page 24

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|                           |    |    |                                     | | | ***  2) Cockpit Voice   D | -  | 0  |                                     | | |         Recorder Not      |    |    |                                     | | |         Equipped To       |    |    |                                     | | |         Record Boom       |    |    |                                     | | |         Microphone        |    |    |                                     | | |                           |    |    |                                     | | | Cockpit Voice Recorder    |    |    |                                     | | | and NO Flight Data        |    |    |                                     | | | Recorder Installed        |    |    |                                     | | |                           |    |    |                                     | | |      1) Cockpit Voice   A | -  | 0  | May be inoperative provided repairs | | |         Recorder          |    |    | are made within three flight days.  | | |         Equipped To       |    |    |                                     | | |         Record Boom       |    |    |                                     | | |         Microphone per    |    |    |                                     | | |         FAR 121.139(e),   |    |    |                                     | | |         135.151(d) or     |    |    |                                     | | |         125.227(e)        |    |    |                                     | | |                           |    |    |                                     | | | ***  2) Cockpit Voice   D | -  | 0  |                                     | | |         Recorder Not      |    |    |                                     | | |         Equipped To       |    |    |                                     | | |         Record Boom       |    |    |                                     | | |         Microphone        |    |    |                                     | | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 23-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -9  Selective Call      C | -  | 0  | May be inoperative provided         | | | *** Systems (SEL/CAL)     |    |    | procedures do not require its use.  | | |                           |    |    |                                       | | -10 Emergency Locator   C | -  | -  | As required by FAR.                 | | | *** Transmitters (ELT)    |    |    |                                     | | |                           |    |    |                                       | | -11 Flitephone System   C | 1  | 0  |                                     | | | ***                       |    |    |                                     | | |                           |    |    |                                       | | -12 Cockpit Speakers    C | 2  | 0  | May be inoperative provided:        | | |                           |    |    |     a) Affected speaker is not      | | |                           |    |    |        required for aural warnings, | | |                           |    |    |        and                          | | |                           |    |    |     b) An operative headset is      | | |                           |    |    |        provided for each person on  | | |                           |    |    |        cockpit duty.                | | |                           |    |    |                                       | Page 25

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| -13  Cockpit Voice        |    |    |                                     | | | ***  Recorder (CVR)       |    |    |                                     | | |                           |    |    |                                     | | |        Flight Data      A | 1  | 0  | (M)May be inoperative provided      | | |        Recorder (FDR)     |    |    | flight Data Recorder (FDR) is       | | |        installed          |    |    | operative.                          | | |                           |    |    |                                     | | |        NO Flight Data   A | 1  | 0  | (M)May be inoperative provided      | | |        Recorder (FDR)     |    |    | repairs are made within three       | | |        installed          |    |    | flight days.                        | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 24-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Batteries           B | 2  | 1  | (M)(O)One may be inoperative        | | |                           |    |    | provided:                           | | |                           |    |    |     a) Aircraft is operated during  | | |                           |    |    |        day VMC,                     | | |                           |    |    |     b) There are no other           | | |                           |    |    |        electrical power source      | | |                           |    |    |        failures,                    | | |                           |    |    |     c) Associated battery cables    | | |                           |    |    |        are disconnected and         | | |                           |    |    |        secured, and                 | | |                           |    |    |     d) Associated battery           | | |                           |    |    |        disconnect switch is pushed. | | |                           |    |    |                                       | | -2  DC Generators       B | 2  | 1  | (M)(O)One may be inoperative        | | |                           |    |    | provided:                           | | |                           |    |    |     a) Generator drive shaft is     | | |                           |    |    |        removed and generator is     | | |                           |    |    |        reinstalled,                 | | |                           |    |    |     b) Associated electrical cables | | Page 26

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|                           |    |    |        are secured, and             | | |                           |    |    |     c) APU Generator is operative.  | | |                           |    |    |                                       | | -3  Alternators         B | 2  | 1  | (M)(O)One may be inoperative        | | |                           |    |    | provided:                           | | |                           |    |    |     a) Aircraft is not operated in  | | |                           |    |    |        known of forecast icing      | | |                           |    |    |        conditions,                  | | |                           |    |    |     b) Alternator drive shaft is    | | |                           |    |    |        removed and alternator is    | | |                           |    |    |        reinstalled, and             | | |                           |    |    |     c) Associated electrical cables | | |                           |    |    |        are secured.                 | | |                           |    |    |                                       | | -4  Main Inverters      C | 2  | 1  | (M)(O)One may be inoperative        | | |                           |    |    | provided remaining inverter is      | | |                           |    |    | verified to power AC buses.         | | |                           |    |    |                                       | | -5  E Inverter            |    |    | DELETED, Rev. 5.                    | | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 24-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -6  AC Voltmeter          |    |    | DELETED, Rev. 5.                    | | |                           |    |    |                                       | | -7  Engine Generator      |    |    |                                     | | |     D.C. Volt/Amp meter   |    |    |                                     | | |                           |    |    |                                     | | |      1) Voltmeters      C | 2  | 0  | (O)Both may be inoperative          | | |                           |    |    | provided:                           | | |                           |    |    |     a) Associated Engine Generator  | | |                           |    |    |        DC Ammeter is operative,     | | |                           |    |    |     b) DC Bus Voltmeter is          | | |                           |    |    |        operative, and               | | |                           |    |    |     c) Associated Generator Off     | | |                           |    |    |        Warning Light is operative.  | | |                           |    |    |                                     | | |      2) Ammeters        C | 2  | 1  | One may be inoperative provided     | | |                           |    |    | associated Engine Generator DC      | | |                           |    |    | voltmeter is operative.             | | |                           |    |    |                                       | | -8  DC Bus Voltmeter      |    |    | DELETED, Rev. 5.                    | | |                           |    |    |                                       | | -9  APU Generator       C | 1  | 0  | (O)May be inoperative provided APU  | | |     Ammeter               |    |    | Generator is not used.              | | Page 27

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|                           |    |    |                                       | | -10 APU Generator       C | 1  | 0  | (M)(O)May be inoperative provided:  | | |                           |    |    |     a) Both DC Generators are       | | |                           |    |    |        operative,                   | | |                           |    |    |     b) APU generator belt is        | | |                           |    |    |        removed, and                 | | |                           |    |    |     c) Associated electrical cables | | |                           |    |    |        are secured.                 | | |                           |    |    |                                       | | -11 "C" Inverter        D | 1  | 0  | (M)                                 | | | ***                       |    |    |                                     | | |                           |    |    |                                       | | -12 Frequency Meter     C | 1  | 0  |                                     | | | *** System                |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 24-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -13 Alternator/Overheat C | 2  | 1  | (O)(M)One may be inoperative        | | |     Warning Systems       |    |    | provided:                           | | |                           |    |    |     a) Aircraft is not operated in  | | |                           |    |    |        known or forecast icing      | | |                           |    |    |        conditions,                  | | |                           |    |    |     b) Associated Alternator drive  | | |                           |    |    |        shaft is removed and         | | |                           |    |    |        alternator is reinstalled,   | | |                           |    |    |     c) Associated electrical cables | | |                           |    |    |        are secured, and             | | |                           |    |    |     d) Aircraft is operated in      | | |                           |    |    |        accordance with AFM          | | |                           |    |    |        Limitations.                 | | |                           |    |    |                                       | | -14 Battery Temperature   |    |    |                                     | | | *** Monitor Systems       |    |    |                                     | | |     (Indicator &          |    |    |                                     | | |     Caution Light)        |    |    |                                     | | |                           |    |    |                                     | | |     Nicad Batteries     C | -  | -  | (M)(O)One may be inoperative        | | |     Installed             |    |    | provided associated Battery is      | | |                           |    |    | electrically disconnected and       | | |                           |    |    | secured.                            | | |                           |    |    |                                       | | -15 DC Generator        C | 2  | 1  | (M)(O)One may be inoperative        | | Page 28

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|     Overheat Warning      |    |    | provided:                           | | |     Lights                |    |    |     a) Affected Generator drive     | | |                           |    |    |        shaft is removed and         | | |                           |    |    |        generator is reinstalled,    | | |                           |    |    |     b) Associated electrical cables | | |                           |    |    |        are secured, and             | | |                           |    |    |     c) APU Generator is operative.  | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 24-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -16 Battery Monitor       |    |    |                                     | | | *** System Ammeters       |    |    |                                     | | |                           |    |    |                                     | | |     Nicad Batteries     C | 2  | 0  | Both may be inoperative provided:   | | |     Installed             |    |    |     a) Essential D.C. Voltmeter is  | | |                           |    |    |        operative,                   | | |                           |    |    |     b) Associated Battery Fail      | | |                           |    |    |        Lights are operative, and    | | |                           |    |    |     c) Battery Disconnect Lights    | | |                           |    |    |        are operative.               | | |                           |    |    |                                       | | -17 Generator Off       C | 2  | 1  | (O)One may be inoperative provided: | | |     Lights                |    |    |     a) Associated Engine Generator  | | |                           |    |    |        D.C. Voltmeter is operative, | | |                           |    |    |        and                          | | |                           |    |    |     b) Associated Engine Generator  | | |                           |    |    |        D.C. Ammeter is operative.   | | |                           |    |    |                                       | | -18 Alternator Off      C | 2  | 1  | (O)One may be inoperative provided  | | |     Lights                |    |    | Engine Driven Alternator A.C.       | | |                           |    |    | Voltmeter is operative.             | | |                           |    |    |                                       | | -19 External Power      C | 1  | 0  | (M)                                 | | |     System                |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 29

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 25-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Crash Axe           B | -  | -  | As required by FAR.                 | | |                           |    |    |                                       | | -2  First Aid Kits      D | -  | -  | Any in excess or those required by  | | |                           |    |    | FAR may be incomplete or missing    | | |                           |    |    | provided required distribution is   | | |                           |    |    | maintained.                         | | |                           |    |    |                                       | | -3  Hand Fire             |    |    | Moved to Chapter 26, Rev. 5.        | | |     Extinguisher          |    |    |                                     | | |                           |    |    |                                       | | -4  Overwater Equipment C | -  | -  | As required by FARs.                | | |                           |    |    |                                       | | -5  Passenger Seats     C | -  | 0  | (M)May be inoperative provided the  | | |                           |    |    | following are accomplished using an | | |                           |    |    | approved maintenance procedure:     | | |                           |    |    |     a) Appropriately secure or stow | | |                           |    |    |        affected seat so that it     | | |                           |    |    |        does not block egress to an  | | |                           |    |    |        aisle or exit, and           | | |                           |    |    |     b) Ensure that affected Seat is | | |                           |    |    |        blocked and placarded "DO    | | |                           |    |    |        NOT OCCUPY".                 | | |                           |    |    |                                     | | |                           |    |    | NOTE 1:  A seat with an inoperative | | |                           |    |    |          seatbelt is considered to  | | |                           |    |    |          be inoperative.            | | |                           |    |    |                                     | | |                           |    |    | NOTE 2:  A seat with an inoperative | | |                           |    |    |          recline mechanism is       | | |                           |    |    |          considered inoperative if  | | Page 30

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|                           |    |    |          the seat cannot be secured | | |                           |    |    |          in the upright position.   | | |                           |    |    |                                       | | -6  Crewmember Shoulder B | -  | -  | Any in excess of those required for | | |     Harnesses             |    |    | flight deck crew members (including | | |                           |    |    | official observer in observer seat) | | |                           |    |    | may be inoperative.                 | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 25-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -7  Observer Seat(s)      |    |    |                                     | | |                           |    |    |                                     | | |        1) Primary       A | -  | -  | May be inoperative provided:        | | |           Observer Seat   |    |    |     a) A passenger seat in          | | |           (including      |    |    |        passenger cabin is available | | |           associated      |    |    |        to an FAA inspector for      | | |           equipment)      |    |    |        performance of official      | | |                           |    |    |        duties, and                  | | |                           |    |    |     b) Repairs are made within two  | | |                           |    |    |        flight days.                 | | |                           |    |    |          OR                         | | |                         A |    |    |     c) The secondary observer's     | | |                           |    |    |        seat is available to the FAA | | |                           |    |    |        inspector for the            | | |                           |    |    |        performance of official      | | |                           |    |    |        duties, and                  | | |                           |    |    |     d) Repairs are made within two  | | |                           |    |    |        flight days.                 | | |                           |    |    |          OR                         | | |                         A |    |    |     e) The primary observer's seat  | | |                           |    |    |        is available with the        | | |                           |    |    |        required minimum safety      | | |                           |    |    |        equipment (safety belt and   | | |                           |    |    |        oxygen) and acceptable to    | | |                           |    |    |        the FAA for the performance  | | |                           |    |    |        of official duties, and      | | |                           |    |    |     f) Repairs are made within two  | | |                           |    |    |        flight days.                 | | |                           |    |    |                                       | |                           |    |    |       (continued)                   | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 31

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 25-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -7  Observer Seat(s)      |    |    |                                     | | |     (cont'd)              |    |    |                                     | | |                           |    |    |                                     | | |        1) Primary         |    |    | NOTE 1:  These provisos are         | | |           Observer Seat   |    |    |          intended to provide for    | | |           (including      |    |    |          occupancy of the above     | | |           associated      |    |    |          seats by an FAA inspector  | | |           equipment)      |    |    |          when the minimum safety    | | |           (cont'd.)       |    |    |          equipment (oxygen and      | | |                           |    |    |          safety belt) is functional | | |                           |    |    |          and the inspector          | | |                           |    |    |          determines the conditions  | | |                           |    |    |          to be acceptable.          | | |                           |    |    |                                     | | |                           |    |    | NOTE 2:  The pilot-in-command will  | | |                           |    |    |          determine if the minimum   | | |                           |    |    |          safety equipment is        | | |                           |    |    |          functional for other       | | |                           |    |    |          persons authorized to      | | |                           |    |    |          occupy any observer        | | |                           |    |    |          seat(s).                   | | |                           |    |    |                                     | | |        2) Additional    D | -  | 0  | May be inoperative.                 | | | ***       Observer        |    |    |                                     | | |           Seat(s)         |    |    |                                     | | |                           |    |    |                                       | | -8  "Fasten Seat Belt   C | -  | -  | One or more signs or placards may   | | |     While Seated" sign    |    |    | be illegible or missing provided a  | | |     or placards           |    |    | legible sign or placard is readable | | |                           |    |    | from each occupied passenger seat.  | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 32

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 25-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -9  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          | | |                           |    |    | equipment, movie equipment, ash     | | |                           |    |    | trays, stereo equipment, overhead   | | |                           |    |    | reading lamps, etc.  Items          | | |                           |    |    | addressed elsewhere in this         | | |                           |    |    | document shall not be included. (M) | | |                           |    |    | and (O) procedures may be required  | | |                           |    |    | and included in the air carrier's   | | |                           |    |    | appropriate document.               | | |                           |    |    |                                     | | |                           |    |    | NOTE:  LAVATORY DOOR ASHTRAYS ARE   | | |                           |    |    | NOT CONSIDERED CONVENIENCE ITEMS.   | | |                           |    |    |                                       | | -10 Megaphones          B | -  | 0  | 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.                  | | |                           |    |    |                                     | | |                           |    |    | NOTE:  Not required for all-cargo   | | |                           |    |    |        operations.                  | | |                           |    |    |                                       | | -11 Flotation Devices   C | -  | -  | Any in excess of those required by  | | |                           |    |    | FAR may be inoperative.             | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 33

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 26-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  APU Fire Detection  C | 1  | 0  | (M)(O)May be inoperative provided   | | |     System                |    |    | APU is not used.                    | | |                           |    |    |                                       | | -2  Fire Extinguishing    |    |    | DELETED, Rev. 5.                    | | |     System Engines        |    |    |                                     | | |                           |    |    |                                       | | -3  APU Fire            C | -  | -  | (O)May be inoperative provided APU  | | |     Extinguishing         |    |    | is not used.                        | | |     System                |    |    |                                     | | |                           |    |    |                                       | | -4  Rear Baggage        C | -  | 0  | (O)May be inoperative provided      | | | *** Compartment Smoke     |    |    | cabin to baggage compartment door   | | |     Detector Systems      |    |    | remains OPEN.                       | | |                           |    |    |                                       | | -5  Passenger           C | -  | 0  | (O)May be inoperative provided door | | | *** Compartment Closet    |    |    | remains OPEN for visual check from  | | |     Smoke Detector        |    |    | crew stations.                      | | |                           |    |    |                                       | | -6  Entranceway Baggage C | -  | -  | (O)May be inoperative provided      | | | *** Compartment Smoke     |    |    | doors remain OPEN for visual check  | | |     Detector              |    |    | from crew stations.                 | | |                           |    |    |                                       | | -7  Portable Fire       D | -  | -  | Any in excess of those required by  | | |     Extinguishers         |    |    | 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    | | |                           |    |    |        can not be mistaken for a    | | |                           |    |    |        functional unit, and         | | |                           |    |    |     b) Required distribution is     | | |                           |    |    |        maintained.                  | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |

Page 34

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 26-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -8  Lavatory Fire         |    |    |                                     | | | *** Extinguisher          |    |    |                                     | | |     Systems               |    |    |                                     | | |                           |    |    |                                     | | |        1) Passenger     C |  - | -  | (M)(O)May be inoperative in each    | | |           Configuration   |    |    | lavatory provided:                  | | |                           |    |    |     a) Lavatory Smoke Detector      | | |                           |    |    |        System operates normally.    | | |                           |    |    |          OR                         | | |                           |    |    |     b) Lavatory waste receptacle is | | |                           |    |    |        empty,                       | | |                           |    |    |     c) Lavatory door is locked      | | |                           |    |    |        CLOSED and placarded,        | | |                           |    |    |        "INOPERATIVE-DO NOT ENTER",  | | |                           |    |    |        and                          | | |                           |    |    |     d) Lavatory is not used for any | | |                           |    |    |        purpose.                     | | |                           |    |    |                                     | | |                           |    |    | NOTE:  These provisos are not       | | |                           |    |    |        intended to prohibit         | | |                           |    |    |        lavatory inspections by      | | |                           |    |    |        crewmembers.                 | | |                           |    |    |                                     | | |        2) Cargo         D | -  | 0  |                                     | | |           Configuration   |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | Page 35

G159R5.txt

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G159R5.txt

|                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 26-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -9  Lavatory Smoke        |    |    |                                     | | | *** Detection Systems     |    |    |                                     | | |                           |    |    |                                     | | |      1) Passenger       C | -  | -  | (M)(O)May be inoperative in each    | | |         Configuration     |    |    | lavatory provided:                  | | |                           |    |    |     a) Lavatory Fire Extinguisher   | | |                           |    |    |        System operates normally.    | | |                           |    |    |          OR                         | | |                           |    |    |     b) Lavatory waste receptacle is | | |                           |    |    |        empty,                       | | |                           |    |    |     c) Lavatory door is locked      | | |                           |    |    |        CLOSED and placarded,        | | |                           |    |    |        "INOPERATIVE-DO NOT ENTER",  | | |                           |    |    |        and                          | | |                           |    |    |     d) Lavatory is not used for any | | |                           |    |    |        purpose.                     | | |                           |    |    |                                     | | |                           |    |    |     NOTE: These provisos are not    | | |                           |    |    |           intended to prohibit      | | |                           |    |    |           lavatory inspections by   | | |                           |    |    |           crewmembers.              | | |                           |    |    |                                     | | |     2) Cargo            D | -  | 0  |                                     | | |        Configuration      |    |    |                                     | | |                           |    |    |                                       | | -10 Galley Fire         C | -  | 0  |                                     | | | *** Extinguishing         |    |    |                                     | | |     Systems               |    |    |                                     | | |                           |    |    |                                       | | -11 Galley Smoke        C | -  | 0  |                                     | | | *** Detection Systems     |    |    |                                     | | |                           |    |    |                                       | | -12 Flame Detectors     C | -  | 0  |                                     | | | ***                       |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | Page 36

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G159R5.txt

| FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 27-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 27  FLIGHT CONTROLS       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Stall Warning         |    |    | DELETED, Rev. 5.                    | | |     System                |    |    |                                     | | |                           |    |    |                                       | | -2  Flap Position         |    |    | DELETED, Rev. 5.                    | | |     Indicator             |    |    |                                     | | |                           |    |    |                                       | | -3  Trim Tab Indicators C | -  | 0  | (O)May be inoperative provided      | | | *** (Electric)            |    |    | electric trim or electronic flight  | | |                           |    |    | control systems are considered      | | |                           |    |    | inoperative.                        | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | Page 37

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G159R5.txt

| AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 28-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Fuel Quantity       C | 2  | 1  | (M)(O)One may be inoperative        | | |     Indicators            |    |    | provided:                           | | |                           |    |    |     a) Both tanks are completely    | | |                           |    |    |        filled using overwing        | | |                           |    |    |        refueling,                   | | |                           |    |    |     b) Both fuel flow meters are    | | |                           |    |    |        operative,                   | | |                           |    |    |     c) Circuit breaker of the       | | |                           |    |    |        inoperative system is pulled | | |                           |    |    |        and collared,                | | |                           |    |    |     d) After takeoff, power is set  | | |                           |    |    |        by matching TGT indications  | | |                           |    |    |        on both engines, and         | | |                           |    |    |     e) Flight crew maintains a log  | | |                           |    |    |        of fuel burned.              | | |                           |    |    |         OR                          | | |                         C |    |    |     f) Affected tank is defueled    | | |                           |    |    |        before each refueling,       | | |                           |    |    |     g) Affected tank is fueled with | | |                           |    |    |        a known quantity of fuel,    | | |                           |    |    |     h) Both fuel flow meters are    | | |                           |    |    |        operative,                   | | |                           |    |    |     i) Circuit breaker of the       | | |                           |    |    |        inoperative system is pulled | | |                           |    |    |        and collared,                | | |                           |    |    |     j) After takeoff, power is set  | | |                           |    |    |        by matching TGT indications  | | |                           |    |    |        on both engines, and         | | |                           |    |    |     k) Flight crew maintains a log  | | |                           |    |    |        of fuel burned.              | | |                           |    |    |                                       | | -2  Fuel Crossfeed        |    |    | DELETED, Rev. 5.                    | | |     Valve                 |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 28-2     | Page 38

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G159R5.txt

| --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -3  Fuel Filter Heat    C | 2  | 0  | (M)(O)Both may be inoperative       | | |     Systems               |    |    | provided:                           | | |                           |    |    |     a) Anti-icing additives are     | | |                           |    |    |        added to fuel,               | | |                           |    |    |     b) Hot Air Gate Valve remains   | | |                           |    |    |        CLOSED, and                  | | |                           |    |    |     c) Aircraft is operated in      | | |                           |    |    |        accordance with AFM          | | |                           |    |    |        Limitations and Procedures.  | | |                           |    |    |           OR                        | | |                         C |    |    |     d) Aircraft is operated with    | | |                           |    |    |        fuel temperatures above +10  | | |                           |    |    |        degrees C.                   | | |                           |    |    |                                       | | -4  Fuel Boost Pumps    C | 4  | 3  | (O)One may be inoperative provided: | | |                           |    |    |     a) Fuel Intertank Valve is      | | |                           |    |    |        installed and operative, and | | |                           |    |    |     b) Aircraft is operated in      | | |                           |    |    |        accordance with AFM          | | |                           |    |    |        Procedures.                  | | |                           |    |    |                                       | | -5  Low Fuel Quantity   C | 2  | 1  | (M)(O)One may be inoperative        | | |     Warning Systems       |    |    | provided both Fuel Quantity         | | |                           |    |    | Indicators are operative.           | | |                           |    |    |                                     | | |                         C | 2  | 0  | (M)(O)Both may be inoperative       | | |                           |    |    | provided:                           | | |                           |    |    |     a) Both Fuel Quantity           | | |                           |    |    |        Indicators are operative,    | | |                           |    |    |     b) All Fuel Boost Pumps are     | | |                           |    |    |        operative, and               | | |                           |    |    |     c) Fuel Crossfeed Valve is      | | |                           |    |    |        OPENED when either wing tank | | |                           |    |    |        contains 2000 pounds or less | | |                           |    |    |        fuel.                        | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 28-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | Page 39

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G159R5.txt

| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -6  Fuel Intertank      C | 1  | 0  | (O)May be inoperative provided:     | | | *** Valve                 |    |    |     a) All Fuel Boost Pumps are     | | |                           |    |    |        operative, and               | | |                           |    |    |     b) All Fuel Quantity Indicators | | |                           |    |    |        are operative.               | | |                           |    |    |                                       | | -7  Single Point        C | 1  | 0  | (M)May be inoperative provided      | | | *** Refueling System      |    |    | procedures are established to       | | |                           |    |    | deactivate single point refueling   | | |                           |    |    | system.                             | | |                           |    |    |                                       | | -8  Fuel Temperature    C | 2  | 0  | (O)Both may be inoperative          | | | *** Indication Systems    |    |    | provided:                           | | |                           |    |    |     a) Fuel Filter Heat System is   | | |                           |    |    |        operative for affected       | | |                           |    |    |        engine.                      | | |                           |    |    |     b) OAT Indicator is operative,  | | |                           |    |    |        and                          | | |                           |    |    |     c) Aircraft is operated in      | | |                           |    |    |        accordance with AFM          | | |                           |    |    |        Limitations and Procedures.  | | |                           |    |    |           OR                        | | |                         C |    |    |     d) Aircraft is operated at      | | |                           |    |    |        outside air temperatures     | | |                           |    |    |        above +10 degrees C.         | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 29-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | Page 40

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G159R5.txt

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 29  HYDRAULIC POWER       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Hydraulic Pumps       |    |    | DELETED, Rev. 5.                    | | |     (engine driven)       |    |    |                                     | | |                           |    |    |                                       | | -2  Auxiliary Pump        |    |    | DELETED, Rev. 5.                    | | |                           |    |    |                                       | | -3  Normal Hydraulic      |    |    | DELETED, Rev. 5.                    | | |     Pressure Gauge        |    |    |                                     | | |                           |    |    |                                       | | -4  Auxiliary Hydraulic C | 1  | 0  |                                     | | |     Pressure Gauge        |    |    |                                     | | |                           |    |    |                                       | | -5  Brake Accumulator   C | 1  | 0  |                                     | | |     Pressure Gauge        |    |    |                                     | | |     (Nose Wheelwell)      |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 30-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 30  ICE AND RAIN          |    |    |                                       | Page 41

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|     PROTECTION            |    |    |                                       | |                           |    |    |                                       | | -1  Engine and          C | 2  | 0  | (M)(O)Both may be inoperative       | | |     Propeller Deicing     |    |    | provided aircraft is not operated   | | |     Systems               |    |    | into known or forecast icing        | | |                           |    |    | conditions.                         | | |                           |    |    |                                       | | -2  Pitot Heaters       B | 2  | 1  | (M)(O)One may be inoperative        | | |                           |    |    | provided aircraft is not operated   | | |                           |    |    | in visible moisture or known or     | | |                           |    |    | forecast icing conditions.          | | |                           |    |    |                                       | | -3  Windshield Wiper    C | 2  | 0  | (O)Both may be inoperative provided | | |     Systems               |    |    | aircraft is not operated in         | | |                           |    |    | precipitation within 5 NM of the    | | |                           |    |    | airport of takeoff or intended      | | |                           |    |    | landing.                            | | |                           |    |    |                                       | | -4  Airfoil Deicing     C | 1  | 0  | (M)(O)May be inoperative provided   | | |     System (Wing &        |    |    | aircraft is not operated into known | | |     Empennage)            |    |    | or forecast icing conditions.       | | |                           |    |    |                                       | | -5  Windshield Heat     B | 2  | 0  | (O)(M)Both may be inoperative       | | |     Systems               |    |    | provided:                           | | |                           |    |    |     a) Aircraft is not operated in  | | |                           |    |    |        known or forecast icing      | | |                           |    |    |        conditions, and              | | |                           |    |    |     b) Aircraft is operated in      | | |                           |    |    |        accordance with AFM          | | |                           |    |    |        Limitations.                 | | |                           |    |    |                                       | | -6  DV Window Heat      C | 2  | 0  | (M)(O)Both may be inoperative       | | |     Systems               |    |    | provided:                           | | |                           |    |    |     a) Aircraft is not operated in  | | |                           |    |    |        known or forecast icing      | | |                           |    |    |        conditions, and              | | |                           |    |    |     b) Aircraft is operated in      | | |                           |    |    |        accordance with AFM          | | |                           |    |    |        Limitations.                 | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 30-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 30  ICE AND RAIN          |    |    |                                       | |     PROTECTION            |    |    |                                       | |                           |    |    |                                       | | -7  Side Window Heat    C | 2  | 0  |                                     | | Page 42

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| *** Systems               |    |    |                                     | | |                           |    |    |                                       | | -8  Pneumatic Boots     C | 1  | 0  | (O)May be inoperative provided:     | | |     Pressure Gauge        |    |    |     a) Suction Gauge is operative,  | | |                           |    |    |        and                          | | |                           |    |    |     b) Suction Gauge is verified to | | |                           |    |    |        have normal indications      | | |                           |    |    |        before takeoff.              | | |                           |    |    |                                       | | -9  Pitot Heat Light    B | 2  | 0  | (M)(O)Both may be inoperative       | | |     Systems               |    |    | provided:                           | | |                           |    |    |     a) All other elements of the    | | |                           |    |    |        pitot heat system are        | | |                           |    |    |        checked and operate          | | |                           |    |    |        normally, and                | | |                           |    |    |     b) Aircraft is not operated in  | | |                           |    |    |        known or forecast icing      | | |                           |    |    |        conditions.                  | | |                           |    |    |                                       | | -10 Ice Detection       C | 1  | 0  |                                     | | | *** Systems               |    |    |                                     | | |                           |    |    |                                       | | -11 Pneumatic Boots     C | 1  | 0  | (O)May be inoperative provided:     | | |     Suction Gauge         |    |    |     a) Aircraft is not operated in  | | |                           |    |    |        known or forecast icing      | | |                           |    |    |        conditions,                  | | |                           |    |    |     b) Aircraft is operated in an   | | |                           |    |    |        unpressurized configuration, | | |                           |    |    |        and                          | | |                           |    |    |     c) Aircraft is operated at or   | | |                           |    |    |        below 10,000 ft.             | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 31-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 31  INDICATING/RECORDING  |    |    |                                       | |     SYSTEMS               |    |    |                                       | |                           |    |    |                                       | | -1  Clock               C | -  | 1  |                                     | | |                           |    |    |                                       | | -2  Flight Data         A | 1  | 0  | May be inoperative provided:        | | Page 43

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| *** Recorder (FDR)        |    |    |     a) Cockpit Voice Recorder (CVR) | | |     System                |    |    |        System is operative, and     | | |                           |    |    |     b) Repairs are made within      | | |                           |    |    |        three flight days.           | | |                           |    |    |                                       | | -3  Cockpit Voice         |    |    | Moved to Chapter 23, Rev. 5.        | | |     Recorder (CVR)        |    |    |                                     | | |     System                |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 32-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 32  LANDING GEAR          |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -1  Anti-Skid Systems     |    |    |                                     | | |                           |    |    |                                     | | |      1) Mechanical      C | 1  | 0  | (O)May be inoperative provided      | | |                           |    |    | aircraft is operated in accordance  | | |                           |    |    | with AFM Limitations.               | | Page 44

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|                           |    |    |                                     | | | ***  2) Electrical      C | 1  | 0  | (M)(O)May be inoperative provided   | | |                           |    |    | aircraft is operated in accordance  | | |                           |    |    | with AFM Limitations.               | | |                           |    |    |                                       | | -2  Landing Gear          |    |    | DELETED, Rev. 5.                    | | |     Position Indicator    |    |    |                                     | | |                           |    |    |                                       | | -3  Park Brake            |    |    | DELETED, Rev. 5.                    | | |                           |    |    |                                       | | -4  Anti-Skid           C | -  | 0  | (M)(O)May be inoperative provided:  | | | *** Indication Systems    |    |    |     a) Anti-skid System is          | | |     (Electronic Anti-     |    |    |        electrically disabled, and   | | |     Skid)                 |    |    |     b) Aircraft is operated in      | | |                           |    |    |        accordance with AFM          | | |                           |    |    |        Limitations.                 | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 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            | | |     Deck/Flight           |    |    | inoperative provided remaining      | | |     Compartment and       |    |    | lights are:                         | | |     Instrument Lighting   |    |    |     a) Sufficient to clearly        | | |     Systems (Excluding    |    |    |        illuminate all required      | | |     EFIS)                 |    |    |        instruments, controls and    | | |                           |    |    |        other devices for which it   | | Page 45

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|                           |    |    |        is provided,                 | | |                           |    |    |     b) Positioned so that direct    | | |                           |    |    |        rays are shielded from       | | |                           |    |    |        flight crewmembers' eyes,    | | |                           |    |    |        and                          | | |                           |    |    |     c) Lighting configuration and   | | |                           |    |    |        intensity is acceptable to   | | |                           |    |    |        the flight crew.             | | |                           |    |    |                                       | | -2  Passenger Cabin     C | -  | -  | (O)May be inoperative provided:     | | |     Interior              |    |    |     a) Sufficient lighting is       | | |     Illumination          |    |    |        operative for crew to        | | |     Systems               |    |    |        perform required duties, and | | |                           |    |    |     b) Lighting configuration at    | | |                           |    |    |        dispatch is acceptable to    | | |                           |    |    |        flight crew.                 | | |                           |    |    |                                       | | -3  Passenger Notice    B | 1  | 0  | (O)May be inoperative provided      | | |     System (No Smoking/   |    |    | procedures are established and used | | |     Fasten Seat Belts)    |    |    | for notifying the passengers when   | | |                           |    |    | seat belts should be fastened and   | | |                           |    |    | smoking is prohibited.              | | |                           |    |    |                                       | | -4  Exterior Emergency  B | -  | -  | As required by FAR.                 | | |     Lights                |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 5        | PAGE:    | |                                          |                       |          | |                  G-159                   | DATE: 12/27/95        | 33-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | -5  Landing Light       C | 2  | 1  | (M)(O)One may be inoperative        | | |     Systems               |    |    | provided Taxi Lights are operative. | | |                           |    |    |                                     | | |                         C | 2  | 0  | (M)(O)Both may be inoperative       | | |                           |    |    | provided airplane is not operated   | | |                           |    |    | at night.                           | | |                           |    |    |                                       | | -6  Taxi Lights         C | 2  | 0  | (M)                                 | | |                           |    |    |                                       | | -7  Position Light      C | -  | -  | (O)May be inoperative provided:     | | Page 46

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|     Bulbs                 |    |    |     a) One light bulb is operative  | | |                           |    |    |        at each position.            | | |                           |    |    |           OR                        | | |                           |    |    |     b) Aircraft is not operated at  | | |                           |    |    |        night.                       | | |                           |    |    |                                       | | -8  Beacons             C | 3  | 0  | (O)All may be inoperative provided  | | |                           |    |    | aircraft is not operated at night.  | | |                           |    |    |                                       | | -9  Strobe "Anti-       B | 3  | 0  | (O)All may be inoperative provided: | | | *** Collision) Lights     |    |    |     a) Aircraft is not operated at  | | |                           |    |    |        night.                       | | |                           |    |    |           OR                        | | |                           |    |    |     b) All Beacons are operative.   | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |