DEPARTMENT OF TRANSPORTATION     Revision: 2

Date: 01/30/97

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

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FEDERAL AVIATION ADMINISTRATION

AIRCRAFT EVALUATION GROUP, MKC-AEG

1201 WALNUT ST., SUITE 900

KANSAS CITY, MO  64106________________-

TELEPHONE:  (816) 426-3946

FAX:        (816) 426-3084



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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

--     Guidelines for (O) & (M) Procedures     XVI, XVII

21     Air Conditioning                        21-1, 2, 3

22     Auto Flight                             22-1

23     Communications                          23-1, 2

24     Electrical Power                        24-1

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

26     Fire Protection                         26-1, 2

27     Flight Controls                         27-1

28     Fuel                                    28-1

30     Ice and Rain Protection                 30-1

31     Indicating/Recording Systems            31-1

32     Landing Gear                            32-1

33     Lights                                  33-1, 2, 3

34     Navigation                              34-1, 2, 3, 4, 5 35     Oxygen                                  35-1

49     Airborne Auxiliary Power                49-1 77     Engine Indicating                       77-1 78     Engine Exhaust                          78-1



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Log of Revisions

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

| 1        | 04/07/92   | ALL PAGES                      |           | | 2        | 01/30/97   | HIGHLIGHTS OF REV.,DEFINITIONS |           | | 2        | 01/30/97   | GUIDELINES                     |           | | 2        | 01/30/97   | 21-1,21-2,21-3,22-1,23-1       |           | | 2        | 01/30/97   | 23-2,24-1,25-1,25-2,25-3       |           | | 2        | 01/30/97   | 25-4,26-1,26-2,27-1,28-1       |           | | 2        | 01/30/97   | 28-2,28-3,30-1,31-1,32-1       |           | | 2        | 01/30/97   | 33-1,33-2,33-3,33-4,34-1       |           | | 2        | 01/30/97   | 34-2,34-3,34-4,34-5,35-1       |           | | 2        | 01/30/97   | 49-1,77-1,78-1                 |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | Page 2

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



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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       2        01/30/97 Table of Contents                        I       2        01/30/97 Log of Revisions                         II      2        01/30/97 Control Page                             III     2        01/30/97 IV      2        01/30/97 Highlights of Change                     V       2        01/30/97 Definitions                              VI      6        01/31/95 VII     6        01/31/95 VIII    6       01/31/95 IX      6        01/31/95 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

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Guidelines for (O) & (M) Procedures      XVI     2        01/30/97 XVII    2        01/30/97 21                                       21-1    2        01/30/97 21-2    2        01/30/97 21-3    2       01/30/97 22                                       22-1    2        01/30/97 23                                       23-1    2        01/30/97 23-2    2        01/30/97 24                                       24-1    2        01/30/97 25                                       25-1    2        01/30/97 25-2    2        01/30/97 25-3    2        01/30/97 25-4    2        01/30/97 26                                              26-1    2        01/30/97 26-2    2        01/30/97 27                                       27-1    2        01/30/97 28                                       28-1    2        01/30/97 30                                       30-1    2        01/30/97 31                                       31-1    2        01/30/97 32                                       32-1    2        01/30/97 33                                       33-1    2        01/30/97 33-2    2        01/30/97 33-3    2        01/30/97 34                                               34-1    2        01/30/97



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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

34-2    2        01/30/97 34-3    2        01/30/97 34-4    2       01/30/97 34-5    2        01/30/97 35                                       35-1    2        01/30/97 49                                       49-1    2        01/30/97 77                                       77-1    2        01/30/97 78                                                                           78-1    2        01/30/97



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Highlights of Change

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This revision is a complete revision.  All pages of the MMEL should be replaced with this revision.

All asterisks representing placard requirements have been deleted in accordance with Policy Letter 61 desigated as Global Change 8.   Other changes were made in accordance with Policy Letters designated as Global Changes or to clarify the provisos.

All deletions were made in accordance with the proceedings of the Flight Operations Evaluation Board or to comply with the provisions of an Emergency Procedure.



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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.

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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 Page 6

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will be determined by the operator.

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

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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 Page 7

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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.

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.

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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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Definitions

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

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

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

The letter designators are inserted adjacent to Column 2.

23. Electronic fault alerting system - General                  | | New generation aircraft display system fault indications to the | flight crew by use of computerized display systems.  Each       | aircraft manufacturer has incorporated individual design        | philosophies in determining the data that would be              | represented.  The following are customized definitions (specific| to each manufacturer) to help determine the level of messages   | affecting the aircraft's dispatch status.  When preparing the   | MEL document, operators are to select the proper Definition No. | 23 for their aircraft, if appropriate.                          | | a.   BOEING  (B-757/767, B-747-400, B-777)                      | | Boeing airplanes equipped with Engine Indicating and Crew       | Alerting  Systems (EICAS), provide different priority levels of | system messages (WARNING,  CAUTION, ADVISORY, STATUS and        | MAINTENANCE).  Any messages that affects airplane dispatch      | status will be displayed at a STATUS message level or  higher.  | Page 9

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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.                                            | | 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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Definitions

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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 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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  D."

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

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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

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

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

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered.

Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

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



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Guidelines for (O) & (M) Procedures

The Flight Operations Evaluation Board (FOEB) has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items.  These procedures must be established by the operator.  The following guidelines are to help maintain these required procedures.

ATA 21-1   (M)Maintenance procedure to ensure valve is secured closed.

(M)Maintenance procedure to ensure all valves are secured closed.

ATA 21-2   (M)Maintenance procedure to ensure inoperative valve is secured closed and Outflow valves are operative.

ATA 21-3   (M)Maintenance procedure to ensure outflow valve is secured closed and both safety valves are operative.

ATA 22-1   (M)Maintenance procedure to determine that servos do not interfere with the flight controls.

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ATA 23-3   (O)Operations procedure to ensure passengers are properly briefed.

ATA 24-5   (M)Maintenance procedure to ensure inoperative inverter does not interfere with operation of other inverters.

ATA 25-3.1 (M)Maintenance procedure to secure or stow folding type seat in the retracted position.

(O)Operations procedure to establish alternate procedures for displaced flight attendant.

ATA 25-3.2 (M)Maintenance procedure to secure or stow folding type seat in the retracted position.

ATA 27-5   (M)Maintenance procedure to ensure gust lock is in the unlock position.

ATA 28-9   (M)Maintenance procedure to secure valve in the open position.



FEDERAL AVIATION ADMINISTRATION   Page XVII

Revision: 2

MASTER MINIMUM EQUIPMENT LIST    Date: 01/30/97

LOCKHEED 1329-25 JETSTAR II

Guidelines for (O) & (M) Procedures

ATA 28-10   (M)Maintenance procedure to secure valve in the closed position.

ATA 33-3    (O)Operations procedure to ensure passengers are briefed.

ATA 33-15   (M)Maintenance procedure to ensure minimum acceptable

lighting level(s) is maintained by remaining operative lights.

ATA 34-16   (O)Operations procedure to ensure pilot awareness of altitude assignments.

ATA 34-21.1 (M)Maintenance procedure to ensure system is deactivated and secured.

.2 (O)Operations procedure to ensure TA and RA elements and

audio functions are operative on flying pilot side and TA and RA display indications are visible to the non- flying pilot.

.3 (O)Operations procedure to ensure RA display is operative on flying pilot side.

(O)Operations procedure to ensure all TA display elements and voice command audio functions are operative and TA only mode is selected by the crew.

Page 15

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.4 (O)Operations procedure to ensure all RA display and audio functions are operative.

ATA 24-22   (M)Maintenance procedure to secure and deactivate system.

ATA 34-23.1 (O)Operations procedure to ensure pilot's altitude awareness.

.4 (O)Operations procedure to ensure pilot's altitude awareness.

.5 (O)Operations procedure to ensure pilot's altitude awareness.

ATA 78-2    (M)Maintenance procedure to ensure no external leakage exists.



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 21-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | | 1.  Bleed Air Pressure  C | 4  | 3  | (M)One may be inoperative provided  | | |     Shut off Valves       |    |    | valve is secured closed.            | | |                           |    |    |                                       | |                           |    |    |          OR                           | |                           |    |    |                                       | |                         C | 4  | 0  | (M)May be inoperative provided:     | | |                           |    |    |     a) Valves are secured closed    | | |                           |    |    |        and                          | | |                           |    |    |     b) Flight is conducted          | | |                           |    |    |        unpressurized.                 | |                           |    |    |                                       | | 2.  Safety Valves       C | 2  | 1  | (M)One may be inoperative           | | |                           |    |    | provided:                           | | |                           |    |    |     a) Inoperative safety valve is  | | |                           |    |    |        secured closed and           | | |                           |    |    |     b) Outflow Valves are             | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 3.  Outflow Valves      C | 2  | 1  | (M)One may be inoperative           | | |                           |    |    | provided:                             | |                           |    |    |     a) Inoperative outflow valve is | | |                           |    |    |        secured closed and           | | |                           |    |    |     b) Safety Valves are operative.   | |                           |    |    |                                       | | 4.  Cabin Altitude      C | 2  | 0  | May be inoperative for              | | |     Pressure Warning      |    |    | unpressurized flight.                 | |     Lights                |    |    |                                       | |                           |    |    |          OR                         | | Page 16

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|                           |    |    |                                       | |                         C | 2  | 0  | May be inoperative for pressurized    | |                           |    |    | flight at or below 10,000 ft. MSL.    | |                           |    |    |                                       | | 5.  Cabin Altitude      C | 1  | 0  | May be inoperative for              | | |     Low Pressure Warning  |    |    | unpressurized flight.                 | |     Horn (Oxygen Buzzer)  |    |    |                                       | |                           |    |    |          OR                           | |                           |    |    |                                       | |                         C | 1  | 0  | May be inoperative for pressurized    | |                           |    |    | flight at or below 10,000 ft. MSL.    | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 21-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | | 6.  Cabin Altimeter     C | 1  | 0  | May be inoperative provided Cabin   | | |                           |    |    | Differential Pressure Gauge is        | |                           |    |    | operative.                            | |                           |    |    |                                       | | 7.  Cabin               C | 1  | 0  | May be inoperative provided Cabin   | | |     Differential          |    |    | Altimeter is operative.               | |     Pressure Gauge        |    |    |                                       | |                           |    |    |                                       | | 8.  Manual Cabin        C | 1  | 0  | May be inoperative for              | | | *** Pressure Controller   |    |    | unpressurized flight.                 | |                           |    |    |                                       | | 9.  Automatic Cabin     C | 1  | 0  | May be inoperative for pressurized  | | | *** Pressure Controller   |    |    | flight provided Manual Cabin          | |                           |    |    | Pressure Controller is operative.     | |                           |    |    |                                       | | 10. Manifold            C | 1  | 0  | May be inoperative provided valve   | | |     Crossbleed Valve      |    |    | remains in closed position.           | |                           |    |    |                                       | | 11. Cabin Rate of         |    |    | DELETED REVISION 2.                 | | |     Climb Selector        |    |    |                                       | |                           |    |    |                                       | | 12. Automatic           C | 2  | 0  | May be inoperative provided Manual  | | |     Temperature Control   |    |    | Temperature Control System is       | | |     Systems               |    |    | operative.                          | | |                           |    |    |                                       | | 13. Manual Temperature  C | 2  | 0  | May be inoperative provided         | | |     Control Systems       |    |    | Automatic Temperature Control         | |                           |    |    | and temperature gauge are             | |                           |    |    | operative.                            | |                           |    |    |                                       | | 14. Electronic Cooling  C | 1  | 0  |                                     | | Page 17

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|     Fan                   |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 21-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | | 15. Refrigeration       C | 2  | 1  | One may be inoperative provided     | | |     Units                 |    |    | flight is maintained at or below    | | |                           |    |    | 15,000 ft MSL.                      | | |                           |    |    |                                       | |                           |    |    |          OR                         | | |                           |    |    |                                       | |                         C | 2  | 0  | May be inoperative provided ram air | | |                           |    |    | ventilation is used for all         | | |                           |    |    | flights.                            | | |                           |    |    |                                       | | 16. Air Conditioning    C | 2  | 1  | One may be inoperative provided     | | |     Shut Off Switches     |    |    | associated side Bleed Air Shut Off  | | |                           |    |    | Valves and Manifold Crossbleed      | | |                           |    |    | Valve are operative.                | | |                           |    |    |                                       | |                           |    |    |          OR                         | | |                           |    |    |                                       | |                         C | 2  | 0  | May be inoperative for              | | |                           |    |    | unpressurized flight using ram air  | | |                           |    |    | ventilation.                        | | |                           |    |    |                                       | | 17. Aux Vent Switch     C | 1  | 0  | May be inoperative provided Air     | | |                           |    |    | Conditioning Shut Off Switches        | |                           |    |    | are operative.                        | |                           |    |    |                                       | | 18. Pneumatic Relay     C | 1  | 0  | May be inoperative for              | | |                           |    |    | unpressurized flight.                 | |                           |    |    |                                       | | 19. Ram Air Valve         |    |    | DELETED REVISION 2.                 | | |                           |    |    |                                       | | 20. Pressure Regulator  C | 2  | 0  | May be inoperative for              | | |     and Shutoff Valves    |    |    | unpressurized flight.                 | |                           |    |    |                                       | |                           |    |    |                                       | Page 18

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



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 22-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 22  AUTO FLIGHT           |    |    |                                       | |                           |    |    |                                       | | 1.  Autopilot           C | -  | 0  | (M)As required by FAR.              | | |     ***                   |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 19

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



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 23-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | | 1.  Communications      C | -  | -  | As required by FAR.                 | | |     System                |    |    |                                       | |     (VHF, HF, UHF)        |    |    |                                       | |                           |    |    |                                       | | 2.  Cockpit Interphone  B | 1  | 0  | May be inoperative provided:        | | |     System                |    |    |     a) No emergency procedures are    | |                           |    |    |        predicated on its use, and     | |                           |    |    |     b) Aircraft remains at or         | |                           |    |    |        below FL410.                   | |                           |    |    |                                       | | 3.  Passenger Address     |    |    |                                     | | |     System                |    |    |                                     | | |                           |    |    |                                       | |     1) Passenger        B | 1  | 0  | (O)May be inoperative provided      | | |        Configuration      |    |    | alternate normal and emergency      | | |                           |    |    | procedures and/or operating         | | |                           |    |    | restrictions are established and    | | |                           |    |    | used.                               | | |                           |    |    |                                     | | |     2) Cargo            D | 1  | 0  |                                       | |        Configuration      |    |    |                                       | |                           |    |    |                                       | | 4.  Cockpit Voice       A | 1  | 0  | May be inoperative provided:        | | |     Recorder (CVR)        |    |    |     a) Flight Data Recorder is      | | |     (If FDR Required by   |    |    |        operating normally and       | | |     FAR)                  |    |    |     b) Repairs are made within      | | |                           |    |    |        three flight days.           | | |                           |    |    |                                       | |     Cockpit Voice       A | 1  | 0  | May be inoperative provided         | | |     Recorder (CVR)        |    |    | repairs are made within three         | |     (If No FDR Required   |    |    | flight days.                          | |     by FAR)               |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 20

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 23-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | | 5.  Boom Microphones      |    |    |                                       | |     (CVR and FDR          |    |    |                                       | |     Installations)        |    |    |                                       | |                           |    |    |                                       | |     1) Cockpit Voice    A | -  | 0  | May be inoperative provided:        | | |        Recorder Equipped  |    |    |     a) Flight Data Recorder (FDR)   | | |        to Record Boom     |    |    |        operates normally and        | | |        Microphone per     |    |    |     b) Repairs are made within      | | |        FAR 121.139(e) or  |    |    |        three flight days.           | | |        FAR 135.151(d)     |    |    |                                     | | |                           |    |    |                                       | |     2) Cockpit Voice    D | -  | 0  |                                     | | |        Recorder Not       |    |    |                                     | | |        Equipped to Record |    |    |                                     | | |        Boom Microphone    |    |    |                                     | | |                           |    |    |                                       | |     Boom Microphones      |    |    |                                     | | |     (CVR Installations)   |    |    |                                     | | |                           |    |    |                                       | |     1) Cockpit Voice    A | -  | 0  | May be inoperative provided         | | |        Recorder Equipped  |    |    | repairs are made within three       | | |        to Record Boom     |    |    | flight days.                        | | |        Microphone per     |    |    |                                     | | |        FAR 135.151(d)     |    |    |                                     | | |                           |    |    |                                       | |     2) Cockpit Voice    D | -  | 0  |                                     | | |        Recorder Not       |    |    |                                     | | |        Equipped to Record |    |    |                                     | | |        Boom Microphone    |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 21

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 24-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | | 1.  DC Starter          B | 4  | 3  | One generator and/or its            | | |     Generators            |    |    | associated control panel may be       | |                           |    |    | inoperative provided:                 | |                           |    |    |     a) Field is tripped and           | |                           |    |    |     B) Overheat light is operative.   | |                           |    |    |                                       | | 2.  DC Generator Out    B | 4  | 3  | One may be inoperative provided:    | | |     Lights                |    |    |     a) DC Voltmeter is operative,     | |                           |    |    |     b) DC Generator Loadmeters are    | |                           |    |    |        operative and                  | |                           |    |    |     c) Annunciator lights are         | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 3.  DC Generator        B | 4  | 2  | Two may be inoperative provided     | | |     Loadmeters            |    |    | Voltmeter, Overheat, and Generator    | |                           |    |    | Lights are operative.                 | |                           |    |    |                                       | | 4.  DC Voltmeter        B | 1  | 0  | May be inoperative provided:        | | |                           |    |    |     a) Bus Tie Open Light is          | |                           |    |    |        operative and                  | |                           |    |    |     b) Loadmeter, Overheat and        | |                           |    |    |        Generator Out Lights are       | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 5.  AC Inverters        B | 3  | 2  | (M)One may be inoperative.          | | |                           |    |    |                                       | | 6.  AC Voltmeter        B | 1  | 0  | May be inoperative provided:        | | |                           |    |    |     a) Frequency Meter is operative   | |                           |    |    |        and                            | |                           |    |    |     b) AC Bus Out Lights are          | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 7.  AC Bus Out Lights   B | 5  | 0  | May be inoperative provided AC      | | |                           |    |    | Voltmeter is operative.               | |                           |    |    |                                       | | 8.  Annunciator         B | 1  | 0  | May be inoperative provided AC      | | |     Inverter Out Light    |    |    | Voltmeter is operative.               | |                           |    |    |                                       | | 9.  AC Rotary Inverter  B | 1  | 0  |                                     | | | ***                       |    |    |                                       | |                           |    |    |                                       |

Page 22

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 25-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | | 1. Crash Ax             C | 1  | 0  |                                     | | | ***                       |    |    |                                       | |                           |    |    |                                       | | 2. First Aid Kits       D | -  | -  | Any in excess of those required by  | | |                           |    |    | FAR may be incomplete or missing    | | |                           |    |    | provided required distribution is   | | |                           |    |    | maintained.                         | | |                           |    |    |                                       | | 3. Flight Attendant       |    |    |                                       | | ***Seats (Single or       |    |    |                                       | |    Dual position)         |    |    |                                       | |                           |    |    |                                       | |    1) Seats required    B | -  | -  | (M)One single or dual position seat | | |       by FAR              |    |    | may be inoperative provided:          | |                           |    |    |     a) Affected seat position(s)      | |                           |    |    |        is not occupied,               | |                           |    |    |     b) Flight attendant(s)            | |                           |    |    |        displaced by inoperative       | |                           |    |    |        seat position(s) occupies      | |                           |    |    |        the passenger seat(s) most     | |                           |    |    |        accessible to their            | |                           |    |    |        assigned exit,                 | |                           |    |    |     c) Alternate operations           | |                           |    |    |        procedures are established     | |                           |    |    |        for displaced flight           | |                           |    |    |        attendant(s),                  | |                           |    |    |     d) Folding type seat that will    | |                           |    |    |        not stow automatically is      | |                           |    |    |        stowed or secured in the       | |                           |    |    |        RETRACTED position,            | |                           |    |    |     e) Passenger seat(s) assigned     | |                           |    |    |        to flight attendant(s) is      | |                           |    |    |        placarded "FOR FLIGHT          | |                           |    |    |        ATTENDANT USE ONLY", and       | |                           |    |    |                                       | |                           |    |    | NOTE:  A folding type seat that       | |                           |    |    |        will not stow automatically    | |                           |    |    |        is considered inoperative.     | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | Page 23

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|                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 25-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | | 3. Flight Attendant       |    |    |                                       | |    Seats (Single or Dual  |    |    |                                       | |    position               |    |    |                                       | |    (Continued)            |    |    |                                       | |                           |    |    |                                       | |    2) Seats in excess   B | -  | 0  | (M)May be inoperative provided:       | |       of the number       |    |    |     a) Affected seat position(s)      | |       required by FAR     |    |    |        is not occupied and            | |                           |    |    |     b) Folding type seat that will    | |                           |    |    |        not stow automatically is      | |                           |    |    |        stowed or secured in the       | |                           |    |    |        retracted position.            | |                           |    |    |                                       | |                           |    |    | NOTE 1: A Folding type seat that      | |                           |    |    |         will not stow                 | |                           |    |    |         automatically is              | |                           |    |    |         considered inoperative.       | |                           |    |    |                                       | |                           |    |    | NOTE 2: Individual operator MELs      | |                           |    |    |         will be specific as to the    | |                           |    |    |         numbers and locations of      | |                           |    |    |         inoperative seats and         | |                           |    |    |         combinations of seats to      | |                           |    |    |         ensure the proximity to       | |                           |    |    |         exits and distribution        | |                           |    |    |         requirements of the           | |                           |    |    |         applicable FAR are met.       | |                           |    |    |                                       | | 4. Flight Attendant     B | -  | -  | One may be inoperative provided     | | |    Seat Lap Belt          |    |    | associated Flight Attendant seat      | |                           |    |    | position is considered inoperative.   | |                           |    |    |                                       | |                           |    |    |                                       | | 5. ELT                  C | 1  | 0  | As required by FAR.                 | | |                           |    |    |                                       | |                           |    |    |          OR                         | | |                           |    |    |                                       | |                         C | 1  | 0  | May be inoperative for published    | | |                           |    |    | scheduled flights in scheduled air  | | |                           |    |    | carrier service.                      | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | Page 24

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| --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 25-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | | 6.  Passenger Convenience | -  | -  | Passenger convenience items, as     | | |     Item(s)               |    |    | 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.       | |                           |    |    | (O) and (M) procedures may be         | |                           |    |    | required and included in the air      | |                           |    |    | carrier's appropriate document.       | |                           |    |    |                                       | | 7.  Lavatory Door       A | 1  | 0  | May be missing provided it is       | | | *** Ashtray               |    |    | replaced within 3 calendar days.    | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | Page 25

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|                                          | DATE: 01/30/97        | 25-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | | 8.  Passenger Seats     C | -  | 0  | May be inoperative provided:        | | |                           |    |    |     a) Affected seat does not block | | |                           |    |    |        emergency egress to an aisle | | |                           |    |    |        or exit and                  | | |                           |    |    |     b) Affected seat is blocked and | | |                           |    |    |        placarded "Do Not Occupy".   | | |                           |    |    |                                       | |                           |    |    | NOTE 1: A seat with an inoperative  | | |                           |    |    |         seatbelt or shoulder        | | |                           |    |    |         harness is considered to    | | |                           |    |    |         be inoperative.             | | |                           |    |    |                                       | |                           |    |    | NOTE 2: A seat with an inoperative  | | |                           |    |    |         recline mechanism is        | | |                           |    |    |         considered inoperative if   | | |                           |    |    |         the seat back cannot be     | | |                           |    |    |         secured in the upright      | | |                           |    |    |         position.                   | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 26-1     | | --------------------------------------------------------------------------- | Page 26

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|                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | | 1.  Thermal Discharge   C | 2  | 0  | May be inoperative provided visual  | | |     Indicator             |    |    | indication of pressure gauges are   | | |                           |    |    | made prior to flight.               | | |                           |    |    |                                       | | 2.  Lavatory Smoke      C | -  | -  | For each lavatory, the lavatory     | | |     Detection Systems     |    |    | smoke detection system may be       | | |                           |    |    | inoperative provided:               | | |                           |    |    |     a) Lavatory Fire Extinguisher   | | |                           |    |    |        system operates normally.    | | |                           |    |    |                                       | |                           |    |    |           OR                        | | |                           |    |    |                                       | |                         C | -  | -  |     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 1:  These provisos are not       | |                           |    |    |          intended to prohibit         | |                           |    |    |          lavatory inspections by      | |                           |    |    |          crewmembers.                 | |                           |    |    |                                       | |                           |    |    | NOTE 2:  A lavatory smoke detection   | |                           |    |    |          system is not required for   | |                           |    |    |          all-cargo operations.        | |                           |    |    |                                       | | 3.  Engine Audible      C | 1  | 0  | May be inoperative provided engine  | | | *** Warning System        |    |    | overheat and engine fire detection  | | |                           |    |    | systems are operative.              | | |                           |    |    |                                       | | 4.  Forward Baggage     C | 1  | 0  | May be inoperative provided baggage | | | *** Compartment Smoke     |    |    | compartment remains empty.          | | |     Detection System      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 26-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | Page 27

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| NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | | 5.  Lavatory Fire       C | -  | -  | For each lavatory, the lavatory     | | |     Extinguisher Systems  |    |    | Fire Extinguisher system may be     | | |                           |    |    | inoperative provided:               | | |                           |    |    |     a) Lavatory Smoke Detection     | | |                           |    |    |        system operates normally.    | | |                           |    |    |                                       | |                           |    |    |           OR                        | | |                           |    |    |                                       | |                         C | -  | -  |     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 1:  These provisos are not       | |                           |    |    |          intended to prohibit         | |                           |    |    |          lavatory inspections by      | |                           |    |    |          crewmembers.                 | |                           |    |    |                                       | |                           |    |    | NOTE 2:  A lavatory fire              | |                           |    |    |          extinguisher system is not   | |                           |    |    |          required for all-cargo       | |                           |    |    |          operations.                  | |                           |    |    |                                       | | 6. Portable Fire        D | -  | -  | Any in excess of those required by  | | |    Extinguisher           |    |    | FAR may be inoperative or missing   | | |                           |    |    | provided:                           | | |                           |    |    |     a) The inoperative fire         | | |                           |    |    |        extinguisher is tagged       | | |                           |    |    |        inoperative, removed from    | | |                           |    |    |        the installed location, and  | | |                           |    |    |        placed out of sight so it    | | |                           |    |    |        cannot be mistaken for a     | | |                           |    |    |        functional unit and          | | |                           |    |    |     b) Required distribution is     | | |                           |    |    |        maintained.                  | | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 27-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | Page 28

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| 27  FLIGHT CONTROLS       |    |    |                                       | |                           |    |    |                                       | | 1.  Leading Edge Flap   C | 1  | 0  | May be inoperative provided visual  | | |     Position Indicator    |    |    | reference to position of flaps is   | | |                           |    |    | determined from pilot seat.         | | |                           |    |    |                                       | |                           |    |    | NOTE:  Wing illumination lights     | | |                           |    |    |        must be operative during     | | |                           |    |    |        night operations.            | | |                           |    |    |                                       | | 2.  Speed Brake         C | 1  | 0  | May be inoperative provided steady  | | |     Warning Light Flasher |    |    | warning light is operative.           | |                           |    |    |                                       | | 3.  Trim Tab Position   C | 1  | 0  | May be inoperative provided:        | | |     Indicators (Aileron,  |    |    |     a) Tab is visually checked for    | |     Rudder)               |    |    |        full range of operation and  | | |                           |    |    |     b) Tab is positioned to         | | |                           |    |    |        neutral prior to each        | | |                           |    |    |        departure and neutral        | | |                           |    |    |        position is verified by      | | |                           |    |    |        visual inspection.           | | |                           |    |    |                                       | | 4.  Speed Brake           |    |    | DELETED REVISION 2                    | |                           |    |    |                                       | | 5.  Rudder Gust Lock    C | 1  | 0  | (M)May be inoperative provided:     | | |                           |    |    |      a) Gust lock is verified in    | | |                           |    |    |         the unlock position and     | | |                           |    |    |      b) Rudder and throttle move-   | | |                           |    |    |         ment is unrestricted.       | | |                           |    |    |                                       | | 6.  Mach Trim System    B | 1  | 0  | May be inoperative provided:        | | |                           |    |    |      a) Speed is limited to         | | |                           |    |    |         .72 Mach and                  | |                           |    |    |      b) Normal pitch trim system is | | |                           |    |    |         not affected.               | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 28-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | Page 29

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| 1.  Main Tank Boost       |    |    |      Deleted Revision 2             | | |     Pumps                 |    |    |                                     | | |                           |    |    |                                       | | 2.  External Tank         |    |    |      Deleted Revision 2             | | |     Boost Pumps           |    |    |                                     | | |                           |    |    |                                       | | 3.  Emergency AC Boost    |    |    |      Deleted Revision 2             | | |     Pumps                 |    |    |                                     | | |                           |    |    |                                       | | 4.  Main Tanks Low        |    |    |      Deleted Revision 2             | | |     Fuel Pressure Warning |    |    |                                     | | |     Lights                |    |    |                                     | | |                           |    |    |                                       | | 5.  External Tanks Low  B | 2  | 1  |      Deleted Revision 2             | | |     Fuel Pressure         |    |    |                                     | | |     Warning Lights        |    |    |                                     | | |                           |    |    |                                       | | 6.  Fuel Quantity         |    |    |      Deleted Revision 2             | | |     Gauges Main Tanks     |    |    |                                     | | |                           |    |    |                                       | | 7.  Fuel Quantity         |    |    |      Deleted Revision 2             | | |     Gauges External Tanks |    |    |                                     | | |                           |    |    |                                       | | 8.  Main Tanks Low        |    |    |      Deleted Revision 2             | | |     Sump Level Warning    |    |    |                                     | | |     Lights                |    |    |                                     | | |                           |    |    |                                       | | 9.  Tank Shutoff        C | 4  | 2  | (M)One may be inoperative on each   | | |     Valves                |    |    | side of the aircraft. Valve should  | | |                           |    |    | be secured in the open position.    | | |                           |    |    |                                       | | 10. Jettison Valve      C | 2  | 0  | (M)May be inoperative provided:     | | |                           |    |    |      a) Takeoff weight is equal to  | | |                           |    |    |         or less than the maximum    | | |                           |    |    |         landing weight, and         | | |                           |    |    |      b) Valve is secured in the     | | |                           |    |    |         closed position.            | | |                           |    |    |                                       | | 11. Pressure Fueling    C | 1  | 0  |                                     | | |     System                |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 30-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 30  ICE AND RAIN          |    |    |                                       | |     PROTECTION            |    |    |                                       | |                           |    |    |                                       | | 1.  Wing De-icing       C | 1  | 0  | May be inoperative provided:        | | Page 30

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|     System                |    |    |     a) Aircraft is not operated     | | |                           |    |    |        in known or forecast icing   | | |                           |    |    |        conditions and               | | |                           |    |    |     b) Suction system is operative. | | |                           |    |    |                                       | | 2.  Windshield          C | 1  | 0  | May be inoperative provided:        | | |     Anti-Icing System     |    |    |     a) Aircraft is not operated in    | |                           |    |    |        known or forecast icing        | |                           |    |    |        conditions and                 | |                           |    |    |     b) Speed and altitude             | |                           |    |    |        restrictions per AFM are       | |                           |    |    |        complied with.                 | |                           |    |    |                                       | | 3.  Windshield Wiper    C | 2  | 0  | May be inoperative provided         | | |     Systems               |    |    | aircraft is not operated in           | |                           |    |    | precipitation within 5 nautical       | |                           |    |    | miles of the airport of takeoff       | |                           |    |    | or intended landing.                  | |                           |    |    |                                       | | 4.  Pitot Static and    B | 3  | 2  | Pilot or copilot system may be      | | |     Utility Heater        |    |    | inoperative provided:               | | |     Systems               |    |    |     a) Flight is conducted in VMC   | | |                           |    |    |        conditions only,             | | |                           |    |    |     b) Aircraft is not operated in  | | |                           |    |    |        known or forecast icing      | | |                           |    |    |        conditions,                  | | |                           |    |    |     c) Aircraft is not operated in  | | |                           |    |    |        visible moisture and         | | |                           |    |    |     d) Utility system is operative  | | |                           |    |    |        under all conditions.        | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 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 with sweep    C | 2  | 1  | One may be inoperative.             | | |     second hand or        |    |    |                                       | |     electric digital      |    |    |          OR                           | Page 31

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|                           |    |    |                                       | |                         C | 2  | 0  | May be inoperative for VFR            | |                           |    |    | operations.                           | |                           |    |    |                                       | | 2.  Flight Recorder     A | 1  | 0  | May be inoperative provided:        | | | *** (FDR)                 |    |    |     a) Cockpit Voice Recorder (CVR)   | |                           |    |    |        operates normally.             | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days.             | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 32-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 32  LANDING GEAR          |    |    |                                       | |                           |    |    |                                       | | 1.  Parking Brake         |    |    |      Deleted Rev. 1                   | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 32

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



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 33-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | | 1.  Cockpit/            C | -  | -  | Individual lights may be            | | |     Flight Deck/          |    |    | inoperative provided remaining      | | |     Flight Compartment    |    |    | lights are:                         | | |     and Instrument        |    |    |     a) Sufficient to clearly        | | |     Lighting System       |    |    |        illuminate all required        | |                           |    |    |        instruments, controls,       | | |                           |    |    |        and other devices for which  | | |                           |    |    |        it is provided,              | | Page 33

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|                           |    |    |     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.  Cabin Interior      C | -  | -  | May be inoperative provided         | | |     Illumination          |    |    | lighting configuration is             | |                           |    |    | acceptable to the flight crew.        | |                           |    |    |                                       | | 3.  Ordinance Lights    C | 1  | 0  | (O)May be inoperative provided      | | |                           |    |    | appropriate verbal briefings are    | | |                           |    |    | given.                              | | |                           |    |    |                                       | | 4.  Navigation Lights   C | 3  | 0  | May be inoperative for day          | | |                           |    |    | operations.                           | |                           |    |    |                                       | | 5.  Anti-Collision      B | 2  | 0  | May be inoperative for day          | | |     Lights                |    |    | operations.                           | |                           |    |    |                                       | | 6.  Wing Inspection     C | 1  | 0  | May be inoperative provided a       | | |     Light                 |    |    | portable lamp/light of adequate       | |                           |    |    | capacity for wing and/or control      | |                           |    |    | surface inspection is available for   | |                           |    |    | night operations in icing             | |                           |    |    | conditions.                           | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 33-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 7.  Landing Lights      C | 2  | 0  | May be inoperative for day          | | |                           |    |    | operations.                         | | |                           |    |    |                                       | |                           |    |    |       OR                            | | |                           |    |    |                                       | |                         C | 2  | 1  | One may be inoperative for night    | | |                           |    |    | operations provided the auxiliary   | | |                           |    |    | landing light is operative.         | | |                           |    |    |                                       | | 8.  Auxiliary Landing   C | 1  | 0  | May be inoperative for day          | | Page 34

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|     Light                 |    |    | operations.                         | | |                           |    |    |                                       | |                           |    |    |           OR                          | |                           |    |    |                                       | |                         C | 1  | 0  | May be inoperative for night        | | |                           |    |    | operations provided both landing    | | |                           |    |    | lights are operative.               | | |                           |    |    |                                       | | 9.  Vestibule Light     C | 1  | 0  | May be inoperative for day          | | |                           |    |    | operations.                           | |                           |    |    |                                       | | 10. Annunciator Master    |    |    |      Deleted Revision 7             | | |     Warning Light         |    |    |                                       | |                           |    |    |                                       | | 11. Aft Compartment     C | -  | 0  |                                     | | |     Light                 |    |    |                                       | |                           |    |    |                                       | | 12. Taxi Lights         C | 2  | 0  | May be inoperative for day          | | |                           |    |    | operations.                         | | |                           |    |    |                                       | |                           |    |    |       OR                            | | |                           |    |    |                                       | |                         C | 2  | 1  | One may be inoperative for night    | | |                           |    |    | operations provided Auxiliary       | | |                           |    |    | Landing Light is operative.         | | |                           |    |    |                                       | | 13. Emergency Lighting    |    |    |      Deleted Revision 7             | | |     System                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 33-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 14. Exterior Strobe     C | -  | 0  |                                     | | |     Light                 |    |    |                                       | |                           |    |    |                                       | | 15. Floor Proximity     C | -  | -  | (M)Individual lights may be         | | | *** Emergency Escape      |    |    | inoperative provided maintenance    | | |     Path Marking System   |    |    | procedures are established to       | | |     Lights                |    |    | determine that FAA approved         | | |                           |    |    | minimum acceptable lighting         | | |                           |    |    | level(s) is maintained by           | | |                           |    |    | remaining operative lights.         | | |                           |    |    |                                     | | |                           |    |    | NOTE: Reference the following       | | |                           |    |    |       documents for FAA approved    | | Page 35

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|                           |    |    |       minimum acceptable lighting   | | |                           |    |    |       levels:                       | | |                           |    |    |                                       | |                           |    |    |       a) FAA Engineering approval   | | |                           |    |    |          letter,                    | | |                           |    |    |                                       | |                           |    |    |       b) FAA approved report of the | | |                           |    |    |          Type Design holder,        | | |                           |    |    |                                       | |                           |    |    |       c) Limitations and Conditions | | |                           |    |    |          section of the applicable  | | |                           |    |    |          Supplemental Type          | | |                           |    |    |          Certificate (STC), and     | | |                           |    |    |                                       | |                           |    |    |       d) FAA approved report        | | |                           |    |    |          incorporated in the Master | | |                           |    |    |          drawing list for the       | | |                           |    |    |          applicable STC.              | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 34-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 34  NAVIGATION            |    |    |                                       | |                           |    |    |                                       | | 1.  VHF Navigation      C | -  | -  | As required by FAR.                 | | |     (VOR/ILS, LORAN,      |    |    |                                       | |     OMEGA/VLF, INS, GPS,  |    |    |                                       | |     DOPPLER, RNAV)        |    |    |                                       | |                           |    |    |                                       | | 2.  Flight Director     C | 1  | 0  | May be inoperative provided         | | |     Indicator             |    |    | approach minimums do not require    | | |                           |    |    | its use.                            | | |                           |    |    |                                       | | 3.  Glideslope (Part      |    |    |      Deleted Rev. 1 Considered part   | |     of VOR-ILS)           |    |    |      of VHF Navigation.               | |                           |    |    |                                       | | 4.  Marker Beacon       C | 1  | 0  | As required by FAR.                 | | |                           |    |    |                                       | | 5.  Automatic           C | -  | -  | As required by FAR.                 | | |     Direction Finder      |    |    |                                       | Page 36

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|                           |    |    |                                       | | 6.  ATC Transponders    D | -  | -  | Any in excess of those required by  | | |     and Automatic         |    |    | FAR may be inoperative.             | | |     Altitude Reporting    |    |    |                                     | | |     Systems               |    |    |                                     | | |                           |    |    |                                       | | 7.  Machmeter           B | 1  | 0  | May be inoperative provided         | | |                           |    |    | aircraft remains at or below        | | |                           |    |    | FL220.                              | | |                           |    |    |                                       | | 8.  Mach Trim Out       C | 1  | 0  |                                     | | |     Light                 |    |    |                                       | |                           |    |    |                                       | | 9.  Outside Air Temp      |    |    |      Deleted Revision 7             | | |     Indicating System     |    |    |                                       | |                           |    |    |                                       | | 10. INS System            |    |    |      Deleted Revision 7             | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 34-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 34  NAVIGATION            |    |    |                                       | |                           |    |    |                                       | | 11. Turn Indicator      B | 2  | 1  | One may be inoperative on right     | | |                           |    |    | side for all flights.                 | |                           |    |    |                                       | |                         B | 2  | 0  | May be inoperative on left side     | | |                           |    |    | except for IFR, passenger carrying  | | |                           |    |    | VFR over-the-top and passenger      | | |                           |    |    | carrying VFR night flights.         | | |                           |    |    |                                       | | 12. Directional Gyro      |    |    |      Deleted Revision 7             | | |     Compass Systems       |    |    |                                     | | |                           |    |    |                                       | | 13. Distance Measuring  C | -  | 0  | As required by FAR.                 | | |     Equipment             |    |    |                                       | |                           |    |    |                                       | | 14. Weather Radar       C | -  | 0  | As required by FAR.                 | | |                           |    |    |                                       | | 15. Standby Bank-and-     |    |    |      Deleted Revision 7             | | |     Pitch                 |    |    |                                     | | |                           |    |    |                                       | Page 37

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| 16. Altitude Alerting   A | 1  | 0  | (O)May be inoperative provided.     | | |     System                |    |    |     a) Autopilot with altitude        | |                           |    |    |        hold is inoperative, and       | |                           |    |    |     b) Operators are limited to       | |                           |    |    |        not more than three flight     | |                           |    |    |        days before repairs are        | |                           |    |    |        made.                          | |                           |    |    |                                       | | 17. Radio Altimeter     C | 1  | 0  | As required by FAR.                 | | | ***                       |    |    |                                     | | |                           |    |    |                                       | | 18. Vertical Gyros      C | 2  | 1  | One may be inoperative provided:    | | |                           |    |    |     a) INS is installed,            | | |                           |    |    |     b) INS is operative and         | | |                           |    |    |     c) Its gyro can be and is used  | | |                           |    |    |        to power the affected        | | |                           |    |    |        equipment.                   | | |                           |    |    |                                       | | 19. Angle of Attack     C | 1  | 0  |                                     | | | *** System                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 34-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 34  NAVIGATION            |    |    |                                       | |                           |    |    |                                       | | 20. Nonstabilized       B | 1  | 0  | May be inoperative provided any     | | |     Magnetic (Standby)    |    |    | combination of three gyro or INS      | |     Compass               |    |    | (IRU) stabilized compass systems      | |                           |    |    | are operative.                        | |                           |    |    |                                       | |                           |    |    |          OR                           | |                           |    |    |                                       | |                         B | 1  | 0  | May be inoperative provided:        | | |                           |    |    |     a) Any combination of two gyro    | |                           |    |    |        or INS stabilized compass      | |                           |    |    |        systems are operative, and     | |                           |    |    |     b) Aircraft is operated with      | |                           |    |    |        dual independent navigation    | |                           |    |    |        capability and under           | |                           |    |    |        positive radar control by      | |                           |    |    |        ATC on the en route portion    | |                           |    |    |        of the flight.                 | |                           |    |    |                                       | |                           |    |    |          OR                           | |                           |    |    |                                       | |                         B | 1  | 0  | May be inoperative for flights      | | |                           |    |    | that are entirely within areas of     | Page 38

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|                           |    |    | magnetic unreliability provided at    | |                           |    |    | least two stabilized directional      | |                           |    |    | gyro systems are installed,           | |                           |    |    | operative, and used in conjunction    | |                           |    |    | with approved free gyro navigation    | |                           |    |    | techniques.                           | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 34-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 34  NAVIGATION            |    |    |                                       | |                           |    |    |                                       | | 21. Traffic Alert         |    |    |                                       | | *** Collision Avoidance   |    |    |                                       | |     System (TCAS II)      |    |    |                                       | |                           |    |    |                                       | |     1) TCAS System      C | -  | 0  | (M)May be inoperative provided the  | | |                           |    |    | system is deactivated and             | |                           |    |    | secured.                              | |                           |    |    |                                       | |     2) Combined TA and  C | 2  | 1  | (O)May be inoperative on the non-   | | |        RA Dual Displays   |    |    | flying pilot side provided:           | |                           |    |    |      a) TA and RA elements and        | |                           |    |    |         audio functions are           | |                           |    |    |         operative on the flying       | |                           |    |    |         pilot side, and               | |                           |    |    |      b) TA and RA display             | |                           |    |    |         indications are visible to    | |                           |    |    |         the non-flying pilot.         | |                           |    |    |                                       | |    3)  Resolution       C | 2  | 1  | (O)One may be inoperative on non-   | | |        Advisory (RA)      |    |    | flying pilot side.                    | |        Display System (s) |    |    |                                       | |                           |    |    |          OR                           | |                           |    |    |                                       | |                         C | -  | 0  | (O)May be inoperative provided:     | | |                           |    |    |      a) All Traffic Alert (TA)        | Page 39

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|                           |    |    |         display elements and voice    | |                           |    |    |         command audio functions are   | |                           |    |    |         operative, and                | |                           |    |    |      b) TA only mode is selected by   | |                           |    |    |         the crew.                     | |                           |    |    |                                       | |    4) TA Display        C | -  | 0  | (O)May be inoperative provided      | | |       System(s)           |    |    | all installed RA display and          | |                           |    |    | audio functions are operative.        | |                           |    |    |                                       | | 22. Traffic Alert       C | -  | 0  | (M)May be inoperative provided the  | | | *** Collision Avoidance   |    |    | system is deactivated and secured.  | | |     System (TCAS I)       |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 34-5     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 34  NAVIGATION            |    |    |                                       | |                           |    |    |                                       | | 23. Ground Proximity      |    |    |                                     | | | *** Warning System        |    |    |                                     | | |                           |    |    |                                       | |     1) Modes 1-4        A | -  | 0  | (O)May be inoperative provided:     | | |                           |    |    |     a) Alternate Procedures are     | | |                           |    |    |        established, used and        | | |                           |    |    |     b) Repairs are made within      | | |                           |    |    |        two flight days.             | | |                           |    |    |                                       | |     2) Test Mode        A | 1  | 0  | May be inoperative provided:        | | |                           |    |    |     a) GPWS is considered           | | |                           |    |    |        inoperative and              | | |                           |    |    |     b) Repairs are made within two  | | |                           |    |    |        flight days.                 | | |                           |    |    |                                       | |     3) Glideslope       B | 2  | 0  |                                     | | |        Deviation (Mode 5) |    |    |                                     | | |                           |    |    |                                       | |     4) Advisory         C | -  | 0  | (O)May be inoperative provided      | | |   ***  Callouts           |    |    | alternate procedures are            | | |                           |    |    | established and used.               | | |                           |    |    |                                       | |     5) Windshear Mode   C | -  | 0  | (O)May be inoperative provided      | | |                           |    |    | alternate procedures are            | | |                           |    |    | established and used.               | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 40

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 35-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 35  OXYGEN                |    |    |                                       | |                           |    |    |                                       | | 1.  Passenger Oxygen    C | -  | -  | As required by FAR.                 | | |     System and Supply     |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 41

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 49-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 49  AIRBORNE AUXILIARY    |    |    |                                       | |     POWER                 |    |    |                                       | |                           |    |    |                                       | | 1.  Auxiliary Power     C | -  | 0  |                                     | | |     Unit                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 42

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L13_25R2.txt

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 77-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 77  ENGINE INDICATING     |    |    |                                       | |                           |    |    |                                       | | 1.  Fuel Flow           B | 4  | 3  | One may be inoperative provided     | | |     Indicators            |    |    | all other engine indicating         | | |                           |    |    | systems are operative for the       | | |                           |    |    | associated engine.                  | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 43

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L13_25R2.txt

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 2        | PAGE:    | |       LOCKHEED 1329-25 JETSTAR II        |                       |          | |                                          | DATE: 01/30/97        | 78-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 78  ENGINE EXHAUST        |    |    |                                       | |                           |    |    |                                       | | 1. Thrust Reverser      C | 4  | 0  | May be inoperative provided:        | | |    Systems                |    |    |     a) Thrust reverser linkage is     | |                           |    |    |        locked overcenter prior      | | |                           |    |    |        to flight.                   | | |                           |    |    |     b) Associated circuit breaker   | | |                           |    |    |        is pulled,                   | | |                           |    |    |     c) Top and bottom thrust        | | |                           |    |    |        reverser lockout plates are  | | |                           |    |    |        installed, and               | | |                           |    |    |     d) Placard associated thrust    | | |                           |    |    |        reverser lever.              | | |                           |    |    |                                       | | 2.  Reverser            C | 1  | 0  | (M)May be inoperative provided no   | | |     Accumulator           |    |    | external leakage exists.            | | |                           |    |    |                                       | |                           |    |    | NOTE:  Placard accumulator low      | | |                           |    |    |        annunciator light.           | | |                           |    |    |                                       | | 3.  Thrust Reverser     C | 4  | 0  | One required for each operative     | | |     Extend Lights         |    |    | actuator.                           | | |                           |    |    |                                       | | 4.  Thrust Reverser     C | 4  | 0  | One required for each operative     | | |     Unlock Lights         |    |    | actuator.                           | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 44

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L13_25R2.txt

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