DEPARTMENT OF TRANSPORTATION     Revision: 30 d                                   Date: 06/11/97

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

FAIRCHILD F-27

FH-227 & FOKKER F-27

Federal Aviation Administration

Flight Standards Division

AIRCRAFT EVALUATION GROUP, LGB-AEG

3229 EAST SPRING STREET

LONG BEACH, CA 90806-2425

TELEPHONE: COMM: 310-988-5270

FAX:  310-988-5281



FEDERAL AVIATION ADMINISTRATION     Page: I

Revision: 30 d

MASTER MINIMUM EQUIPMENT LIST      Date: 06/11/97

FAIRCHILD F-27

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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, VI

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

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

22     Auto Flight                             22-1, 2

23     Communications                          23-1, 2, 3

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

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

26     Fire Protection                         26-1, 2, 3, 4

27     Flight Controls                         27-1

28     Fuel                                    28-1, 2, 3

30     Ice and Rain Protection                 30-1, 2

31     Indicating/Recording Systems            31-1

32     Landing Gear                            32-1

33     Lights                                  33-1, 2, 3, 4, 5 34     Navigation                              34-1, 2, 3, 4, 5 34     Navigation                              34-6

35     Oxygen                                  35-1 36     Pneumatic                               36-1 49     Airborne Auxiliary Power                49-1 52     Doors                                   52-1 61     Propellers                              61-1 73     Engine Fuel & Control                   73-1 74     Ignition                                74-1 76     Engine Controls                         76-1 77     Engine Indicating                       77-1 79     Engine Oil                              79-1 80     Starting                                80-1 82     Water Injection                         82-1



FEDERAL AVIATION ADMINISTRATION   Page: II

Revision: 30 d

MASTER MINIMUM EQUIPMENT LIST    Date: 06/11/97

FAIRCHILD F-27

FH-227 & FOKKER F-27

Log of Revisions

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

| 29a      |            | HIGHLIGHTS OF REV.,DEFINITIONS |           | | 29a      |            | PREAMBLE                       |           | | 29a      |            | 21-1,21-2,21-3,21-4,21-5       |           | | 29a      |            | 22-1,23-1,23-2,24-1,24-2       |           | | 29a      |            | 24-3,25-1,25-2,25-3,26-1       |           | | 29a      |            | 26-2,26-3,27-1,28-1,28-2       |           | | 29a      |            | 30-1,30-2,31-1,32-1,33-1       |           | Page 2

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| 29a      |            | 33-2,33-3,34-1,34-2,34-3       |           | | 29a      |            | 35-1,36-1,49-1,52-1,61-1       |           | | 29a      |            | 73-1,77-1,79-1,80-1,82-1       |           | | 30       | 09/04/92   | ALL PAGES                      |           | | 30a      | 03/24/93   | HIGHLIGHTS OF REV.,            |           | | 30a      | 03/24/93   | 61-1,73-1                      |           | | 30b      | 09/14/93   | HIGHLIGHTS OF REV.,DEFINITIONS |           | | 30b      | 09/14/93   | 21-1,21-2,21-3,21-4,21-5       |           | | 30b      | 09/14/93   | 21-6,22-1,22-2,23-1,23-2       |           | | 30b      | 09/14/93   | 23-3,24-1,24-2,24-3,24-4       |           | | 30b      | 09/14/93   | 25-1,25-2,25-3,25-4,26-1       |           | | 30b      | 09/14/93   | 26-2,26-3,26-4,27-1,28-1       |           | | 30b      | 09/14/93   | 28-2,28-3,30-1,30-2,31-1       |           | | 30b      | 09/14/93   | 32-1,33-1,33-2,33-3,33-4       |           | | 30b      | 09/14/93   | 33-5,34-1,34-2,34-3,34-4       |           | | 30b      | 09/14/93   | 34-5,34-6,35-1,36-1,49-1       |           | | 30b      | 09/14/93   | 52-1,61-1,73-1,74-1,76-1       |           | | 30b      | 09/14/93   | 77-1,79-1,80-1,82-1            |           | | 30c      | 04/25/94   | HIGHLIGHTS OF REV.,DEFINITIONS |           | | 30c      | 04/25/94   | 77-1                           |           | | 30d      | 06/11/97   | HIGHLIGHTS OF REV.,DEFINITIONS |           | | 30d      | 06/11/97   | 24-4,32-1                      |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           |



FEDERAL AVIATION ADMINISTRATION     Page: III

Revision: 30 d

MASTER MINIMUM EQUIPMENT LIST      Date: 06/11/97

FAIRCHILD F-27

FH-227 & FOKKER F-27

Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       30 d     06/11/97 Table of Contents                        I       30 d     06/11/97 Log of Revisions                         II      30 d     06/11/97 Control Page                             III     30 d     06/11/97 IV      30 d     06/11/97 Highlights of Change                     V       30 d     06/11/97 VI      30 d     06/11/97 Definitions                              VII     6        01/31/95 VIII    6                                                                   01/31/95

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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 XIV     6        01/31/95 Preamble                                 XV     2        06/14/89 XVI     2        06/14/89 21                                             21-1    30 b     09/14/93 21-2    30 b     09/14/93 21-3    30 b     09/14/93 21-4    30 b     09/14/93 21-5   30 b     09/14/93 21-6    30 b     09/14/93 22                                             22-1    30 b     09/14/93 22-2    30 b     09/14/93 23                                       23-1    30 b     09/14/93 23-2    30 b     09/14/93 23-3    30 b     09/14/93 24                                       24-1    30 b     09/14/93 24-2          30 b     09/14/93 24-3    30 b     09/14/93 24-4    30 d     06/11/97 25                                       25-1    30 b     09/14/93 25-2    30 b     09/14/93 25-3    30 b     09/14/93 25-4   30 b     09/14/93 26                                       26-1          30 b     09/14/93 26-2    30 b     09/14/93 26-3    30 b                                      09/14/93 26-4    30 b     09/14/93



FEDERAL AVIATION ADMINISTRATION     Page: IV

Revision: 30 d

MASTER MINIMUM EQUIPMENT LIST      Date: 06/11/97

FAIRCHILD F-27

FH-227 & FOKKER F-27

Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

27                                       27-1    30 b     09/14/93 28                                       28-1    30 b     09/14/93 28-2    30 b     09/14/93 28-3    30 b     09/14/93 30                                       30-1    30 b     09/14/93 30-2    30 b     09/14/93 31                                       31-1    30 b     09/14/93 32                                       32-1    30 d     06/11/97 33                                       33-1    30 b     09/14/93 33-2    30 b     09/14/93 33-3    30 b     09/14/93 33-4   30 b     09/14/93 33-5    30 b     09/14/93 34                                             34-1    30 b     09/14/93 34-2    30 b                                      09/14/93 34-3    30 b     09/14/93

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34-4    30 b     09/14/93 34-5    30 b     09/14/93 34-6    30 b     09/14/93 35                                       35-1    30 b     09/14/93 36                                       36-1    30 b     09/14/93 49                                       49-1    30 b     09/14/93 52                                       52-1    30 b     09/14/93 61                                       61-1    30 b     09/14/93 73                                       73-1    30 b     09/14/93 74                                       74-1    30 b     09/14/93 76                                       76-1    30 b     09/14/93 77                                       77-1    30 c     04/25/94 79                                       79-1    30 b     09/14/93 80                                       80-1    30 b     09/14/93 82                                       82-1    30 b                                                                09/14/93



FEDERAL AVIATION ADMINISTRATION   Page: V

Revision: 30 d

MASTER MINIMUM EQUIPMENT LIST    Date: 06/11/97

FAIRCHILD F-27

FH-227 & FOKKER F-27

Highlights of Change

EFFECTIVE ABOVE DATE, the Fairchild/Fokker F-27 & FH-227 Master Minimum Equipment List is revised. This revision is to incorporate two STCs and one service bulletin.

NOTE: This revision does not include the latest Global Changes. These will be incorporated at a later date.

24 ELECTRICAL POWER

Item 30-6  New Item.

32 LANDING GEAR

Item 60-1 Added S/B.

Item 60-2 New Item.

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

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FEDERAL AVIATION ADMINISTRATION   Page: VI

Revision: 30 d

MASTER MINIMUM EQUIPMENT LIST    Date: 06/11/97

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FH-227 & FOKKER F-27

Highlights of Change

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FEDERAL AVIATION ADMINISTRATION     Page: VII

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

FAIRCHILD F-27

FH-227 & FOKKER F-27

Definitions

1.   System Definitions.

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

a.        "Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column.

b.        "Number Installed" (Column 2) is the number

(quantity) of items normally installed in the aircraft.  This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is not required.

|

c.        "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met.

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

d.        "Remarks or Exceptions" (Column 4) in this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

e.        A vertical bar (change bar) in the margin

indicates a change, addition or deletion in the adjacent text for the current revision of that page only.  The change bar is dropped at the next revision of that page.

2.  "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification  Office. The FAA approved AFM/RFM for the specific aircraft is listed on the applicable Type



FEDERAL AVIATION ADMINISTRATION     Page: VIII

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     F27R30D.txt FAIRCHILD F-27 FH-227 & FOKKER F-27

Definitions

Certificate Data Sheet.

3.  "As required by FAR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules.  The number of items required by the FAR must be operative.  When the listed item is not required by FAR it may be inoperative for time specified by repair category.

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

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

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

|

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

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

airplane which has a type design approval for ER operations and complies with the provisions of Advisory Circular 120-42A.           |

8.  "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations.

9.  "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

10.  "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s).

11.  Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for



FEDERAL AVIATION ADMINISTRATION     Page: IX

Revision: 6

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FAIRCHILD F-27

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Definitions

operation with the  listed item inoperative. Page 8

 

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

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

14.  Inoperative components of an inoperative system:

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

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

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

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



FEDERAL AVIATION ADMINISTRATION     Page: X

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

FAIRCHILD F-27

FH-227 & FOKKER F-27

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 Page 9

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flight.  An acceptable method of securing or deactivating will be established by the operator.

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

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

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

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

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

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

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



FEDERAL AVIATION ADMINISTRATION     Page: XI

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MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

FAIRCHILD F-27

FH-227 & FOKKER F-27

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.

Page 10

  The letter designators are inserted adjacent to Column 2.

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



FEDERAL AVIATION ADMINISTRATION     Page: XII

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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.                                                                                    | |

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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)                                           |



FEDERAL AVIATION ADMINISTRATION     Page: XIII

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Definitions

|

Fokker aircraft are equipped with Multi Function Display System | (MFDS) which provides electronic message referring to the       | different priority levels of system information (WARNING (red), | CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any      | messages that affects aircraft dispatch will be at the WARNING, | CAUTION or AWARENESS level.  In these cases the MEL must be     | verified for dispatch capability and maintenance may be         | required.                                                       | | System conditions that only require maintenance are not         | presented on the flight deck.  These maintenance                | indications/messages may be presented on the Maintenance & Test | Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by | dedicated Built In Test Evaluation (BITE) of systems.                                                                            |

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

25.  "***" symbol in Column 1 indicates an item which is not Page 12

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

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

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



FEDERAL AVIATION ADMINISTRATION     Page: XIV

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Definitions

maintenance log and or record.  This day is excluded from the calendar days or flight days specified in the MMEL for the repair of an inoperative item of equipment. This provision is applicable to all MMEL items, i.e., categories "A, B, C, and

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MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/89

FAIRCHILD F-27

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Preamble

(Effective 6/14/89)

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

MMEL;  however, relief for administrative control items must be approved by the Administrator.  An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment.

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



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FEDERAL AVIATION ADMINISTRATION   Page: XVI

Revision: 2

MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/89

FAIRCHILD F-27

FH-227 & FOKKER F-27

Preamble

(Effective 6/14/89)

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

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished.  It is important that repairs be accomplished at the earliest opportunity.  In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment.  The MEL provides for release of the aircraft for flight with inoperative equipment.  When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation.  MEL conditions and limitations, do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative.

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

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

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

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



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 21-1     | | --------------------------------------------------------------------------- | Page 15

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|                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-1  Cabin Blower        |    |    |                                       | |       Systems             |    |    |                                       | |                           |    |    |                                       | |       1) Pressurized    C | 2  | 1  | (M)One may be inoperative             | |          Configuration    |    |    | provided:                             | |                           |    |    |     a) The Spill Valve for the        | |                           |    |    |        inoperative blower is          | |                           |    |    |        secured OPEN,                  | |                           |    |    |     b) Cabin altitude is limited to   | |                           |    |    |        10,000 ft,                     | |                           |    |    |     c) Fuel load is based on cruise   | |                           |    |    |        at 10,000 feet MSL or below,   | |                           |    |    |        and                            | |                           |    |    |     d) Route allows flight at         | |                           |    |    |        10,000 feet or below.          | |                           |    |    |                                       | |       2) Unpressurized  C | 2  | 0  | (M)One or both may be inoperative     | |          Configuration    |    |    | provided:                             | |                           |    |    |     a) The Ram Air System (if         | |                           |    |    |        installed) is operative, and   | |                           |    |    |     b) The spill valves are secured   | |                           |    |    |        open.                          | |                           |    |    |                                       | | 10-2  Spill Valve         |    |    |                                       | |       Systems             |    |    |                                       | |                           |    |    |                                       | |       1) Pressurized    C | 2  | 1  | (M)May be inoperative provided:       | |          Configuration    |    |    |     a) Associated Cabin Blower is     | |                           |    |    |        considered inoperative,        | |                           |    |    |     b) Cabin Pressurization Dump      | |                           |    |    |        System is operative, and       | |                           |    |    |     c) Affected Valve is secured      | |                           |    |    |        OPEN.                          | |                           |    |    |                                       | |       2) Unpressurized  C | 2  | 0  |                                       | |          Configuration    |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 21-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | Page 16

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| NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-3  Blower Pressure   C | 2  | 1  | (O)One may be inoperative,            | |       Indicating          |    |    | provided before each flight,          | |       System              |    |    | operation of the associated blower    | |                           |    |    | is established during engine start.   | |                           |    |    |                                       | |                         C | 2  | 0  | (M)One or both may be inoperative     | |                           |    |    | provided associated cabin blower is   | |                           |    |    | not used.                             | |                           |    |    |                                       | | 10-4  Spill Valve       C | 2  | 0  | (O)May be inoperative provided        | | ***   Indicator Light     |    |    | associated Spill Valve is             | |       Systems             |    |    | operative.                            | |                           |    |    |                                       | | 20-1  Recirculation     C | 1  | 0  | (O)May be inoperative provided:       | | ***   Fan System          |    |    |     a) Radio Rack Ventilation         | |                           |    |    |        Cooling Fan is operative.      | |                           |    |    |          OR                           | |                         C |    |    |     b) Outside Air Temperature        | |                           |    |    |        (OAT) is less than 35          | |                           |    |    |        degrees C, and                 | |                           |    |    |     c) Ground operations are          | |                           |    |    |        limited to 30 minutes or       | |                           |    |    |        less.                          | |                           |    |    |                                       | | 21-1  Ground Blower     C | 1  | 0  |                                       | | ***   System              |    |    |                                       | |                           |    |    |                                       | | 30-1  Cabin Pressure    C | 1  | 0  | (O)May be inoperative provided        | |       Control System      |    |    | aircraft is operated in an accepted   | |                           |    |    | unpressurized configuration.          | |                           |    |    |                                       | |       1) Automatic      C | 1  | 0  | (O)May be inoperative provided:       | |          Control          |    |    |     a) Manual Control System is       | |          System (AUTO)    |    |    |        operative, and                 | |                           |    |    |     b) Cabin Altitude, Cabin          | |                           |    |    |        Differential Pressure and      | |                           |    |    |        Cabin rate of Climb            | |                           |    |    |        Indicators are operative.      | |                           |    |    |                                       | |                           |    |    | (Continued)                           |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 21-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | Page 17

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|                           |    |    |                                       | |                           |    |    |                                       | | 30-1  Cabin Pressure      |    |    |                                       | |       Control System      |    |    |                                       | |       (Cont'd)            |    |    |                                       | |                           |    |    |                                       | |       2) Manual         C | 1  | 0  | (O)May be inoperative provided:       | |          Control          |    |    |     a) Automatic Control System is    | |          System           |    |    |        operative, and                 | |          (MANUAL)         |    |    |     b) Both Spill Valves are          | |                           |    |    |        operative, and                 | |                           |    |    |     c) Dump Valve System is           | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 30-2  Cabin             C | -  | 0  | (M)May be inoperative provided:       | | ***   Altitude Caution    |    |    |     a) Cabin Altitude/Cabin           | |       Light System        |    |    |        Differential Pressure          | |                           |    |    |        Indicator is operative.        | |                           |    |    |           OR                          | |                         C |    |    |     b) Aircraft is operated in an     | |                           |    |    |        accepted unpressurized         | |                           |    |    |        configuration.                 | |                           |    |    |                                       | | 30-3  Cabin Altitude    C | 1  | 0  | (O)May be inoperative provided:       | |       Indication          |    |    |     a) Cabin Differential Pressure    | |       System              |    |    |        Indicator is operative, and    | |                           |    |    |     b) A chart is provided for the    | |                           |    |    |        crew to convert cabin          | |                           |    |    |        differential pressure to       | |                           |    |    |        cabin altitude.                | |                           |    |    |                                       | | 30-4  Cabin             C | 1  | 0  | (O)May be inoperative provided:       | |       Differential        |    |    |     a) Cabin Altitude Indicator is    | |       Pressure            |    |    |        operative, and                 | |       Indication          |    |    |     b) A chart is provided for the    | |       System              |    |    |        crew to convert Cabin          | |                           |    |    |        Altitude to Cabin              | |                           |    |    |        Differential Pressure.         | |                         C |    |    |           OR                          | |                           |    |    |     c) Aircraft is operated in an     | |                           |    |    |        accepted unpressurized         | |                           |    |    |        configuration.                 |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 21-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 30-5  Cabin Rate of     C | 1  | 0  | May be inoperative provided:          | Page 18

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|       Climb Indicating    |    |    |     a) Cabin Altitude Indicator is    | |       System              |    |    |        operative, and                 | |                           |    |    |     b) Automatic Cabin Pressure       | |                           |    |    |        Control System is operative.   | |                           |    |    |           OR                          | |                         C |    |    |     b) Aircraft is operated in an     | |                           |    |    |        accepted unpressurized         | |                           |    |    |        configuration.                 | |                           |    |    |                                       | | 30-6  Dump Valve        C | 2  | 1  | (M)One may be inoperative             | |       Systems             |    |    | provided:                             | |                           |    |    |     a) Affected Valve is verified     | |                           |    |    |        CLOSED, and                    | |                           |    |    |     b) All other Instruments and      | |                           |    |    |        Functions of the               | |                           |    |    |        Pressurization Control         | |                           |    |    |        System are operative.          | |                           |    |    |                                       | |                         C | 2  | 0  | (O)Both may be inoperative            | |                           |    |    | provided:                             | |                           |    |    |     a) Aircraft is operated in an     | |                           |    |    |        accepted unpressurized         | |                           |    |    |        configuration, and             | |                           |    |    |     b) Manual Control remains in      | |                           |    |    |        full depress.                  | |                           |    |    |                                       | | 30-7  Outflow Valve     C | 2  | 0  | (M)May be inoperative provided:       | |       Systems             |    |    |     a) Aircraft is operated in an     | |                           |    |    |        accepted unpressurized         | |                           |    |    |        configuration, and             | |                           |    |    |     b) Cabin Dump Valve System is     | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 40-1  Cockpit           D | 1  | 0  | (M)May be inoperative provided        | | ***   Heater System       |    |    | Cockpit Heater is secured OFF.        | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 21-5     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 51-1  Radio Rack        C | 1  | 0  | (O)May be inoperative provided:       | |       Ventilation         |    |    |     a) Outside Air Temperature        | |       Cooling Fan         |    |    |        (OAT) is less than 35          | |       System              |    |    |        degrees C, and                 | Page 19

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|       (Fokker 27)         |    |    |     b) Ground operations are          | |                           |    |    |        limited to 30 minutes or       | |                           |    |    |        less.                          | |                           |    |    |                                       | | 60-1  Cabin             C | 1  | 0  | (O)May be inoperative provided an     | |       Temperature         |    |    | accepted alternate means of           | |       Control System      |    |    | temperature control is developed      | |                           |    |    | and used.                             | |                           |    |    |                                       | |       1) Automatic      C | 1  | 0  | May be inoperative provided Manual    | |          System (AUTO)    |    |    | System is operative.                  | |                           |    |    |                                       | |       2) Manual System  C | 1  | 0  | (M)May be inoperative provided:       | |          (MANUAL)         |    |    |     a) Automatic Temperature          | |                           |    |    |        Control System is operative,   | |                           |    |    |        and                            | |                           |    |    |     b) Spill Valves are verified      | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 61-1  Cabin             D | 1  | 0  |                                       | | ***   Temperature         |    |    |                                       | |       Indicator System    |    |    |                                       | |                           |    |    |                                       | | 61-2  Duct              D | 1  | 0  |                                       | | ***   Temperature         |    |    |                                       | |       Indicating          |    |    |                                       | |       System              |    |    |                                       | |                           |    |    |                                       | | 62-2  Cabin Heater      D | -  | 0  |                                       | | ***   Systems             |    |    |                                       | |       (Fairchild F-27)    |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 21-6     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 62-3  Cabin Choke       C | 1  | 0  | (O)May be inoperative provided:       | |       Valve System        |    |    |     a) Valve has failed in the open   | |                           |    |    |        position, and                  | |                           |    |    |     b) Valve is not required to       | |                           |    |    |        maintain cabin temperature.    | |                           |    |    |                                       | | 62-4  Freon System      D | 1  | 0  |                                       | Page 20

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F27R30D.txt

| ***                       |    |    |                                       | |                           |    |    |                                       | | 62-5  Cabin             C | 1  | 0  | (O)May be inoperative provided:       | | ***   Pressure Door       |    |    |     a) A flight deck window is        | |       Safe-To-Open        |    |    |        opened prior to opening any    | |       Light System        |    |    |        door, and                      | |                           |    |    |     b) Cabin attendants verify with   | |                           |    |    |        the flight deck crew that a    | |                           |    |    |        window is open before          | |                           |    |    |        opening any door.              | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 22-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 22  AUTO FLIGHT           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-1  Autopilot           |    |    |                                       | | ***   System              |    |    |                                       | |                           |    |    |                                       | |       1) Except         D | 1  | 0  |                                       | |          SPZ-600          |    |    |                                       | |                           |    |    |                                       | |       2) SPZ-600        D | 1  | 0  | May be inoperative for provided       | |                           |    |    | approach procedures do not require    | |                           |    |    | its use.                              | Page 21

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F27R30D.txt

|                           |    |    |                                       | | 15-2  Autopilot/Yaw     C | 2  | 1  | One may be inoperative provided:      | | ***   Damper Manual       |    |    |     a) Pilot using Autopilot has an   | |       Disconnect          |    |    |        operative Disconnect Button,   | |       Systems             |    |    |     b) Autopilots are not used        | |                           |    |    |        below 1500 feet AGL, and       | |                           |    |    |     c) Approach minimums do not       | |                           |    |    |        require use of Autopilot.      | |                           |    |    |                                       | |                         C | 2  | 0  | Both may be inoperative provided      | |                           |    |    | the Autopilot/Yaw Damper is           | |                           |    |    | considered inoperative.               | |                           |    |    |                                       | | 15-3  Yaw Damper        D | 1  | 0  |                                       | | ***   System              |    |    |                                       | |                           |    |    |                                       | | 15-4  AP/YD Status      C | 8  | 0  | May be inoperative provided           | | ***   Indication          |    |    | Autopilot is considered               | |       Systems             |    |    | inoperative.                          | |                           |    |    |                                       | | 15-5  COUPLE            C | 1  | 0  | (M)May be inoperative provided:       | | ***   Switch System       |    |    |     a) Selected side is               | |                           |    |    |        illuminated, and               | |                           |    |    |     b) Autopilot is verified          | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 15-6  AP Engage         C | 1  | 0  | May be inoperative provided the       | | ***   Indication          |    |    | Autopilot is considered               | |       System              |    |    | inoperative.                          | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 22-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 22  AUTO FLIGHT           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 15-7  YD Engage         C | 1  | 0  |                                       | | ***   Indication          |    |    |                                       | |       System              |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 22

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F27R30D.txt

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



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 23-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-1  Communications    C | -  | -  | As required by FAR.                   | |       Systems             |    |    |                                       | |       (VHF, HF, UHF)      |    |    |                                       | |                           |    |    |                                       | | 10-2  SELCAL/CALSEL     D | 1  | 0  | May be inoperative provided:          | | ***   System              |    |    |     a) Procedures do not require      | |                           |    |    |        its use.                       | |                           |    |    |           OR                          | |                         D |    |    |     b) Flight Crew monitors           | |                           |    |    |        appropriate HF or VHF          | |                           |    |    |        frequency.                     | |                           |    |    |                                       | | 30-1  Public Address      |    |    |                                       | |       System              |    |    |                                       | Page 23

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F27R30D.txt

|                           |    |    |                                       | |       1) Passenger      A | 1  | 0  | (O)May be inoperative provided:       | |          Configuration    |    |    |     a) Flight Deck to Cabin           | |                           |    |    |        Interphone System is           | |                           |    |    |        operative,                     | |                           |    |    |     b) Flight Attendant Call System   | |                           |    |    |        is operative,                  | |                           |    |    |     c) Alternate Normal, and          | |                           |    |    |        Emergency operations           | |                           |    |    |        procedures are established     | |                           |    |    |        and used, and                  | |                           |    |    |     d) Aircraft is repaired within    | |                           |    |    |        15 flight hours for domestic   | |                           |    |    |        flights or 25 flight hours     | |                           |    |    |        for international flights.     | |                           |    |    |                                       | |       2) Cargo          C | 1  | 0  |                                       | |          Configuration    |    |    |                                       | |                           |    |    |                                       | | 30-2  Emergency         C | -  | -  | As required by FAR.                   | | ***   Locator             |    |    |                                       | |       Transmitter         |    |    |                                       | |       (ELT)               |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 23-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 33-1  Megaphones        C | -  | 1  | Any in excess of those required by    | |                           |    |    | FAR may be inoperative provided:      | |                           |    |    |     a) The inoperative Megaphone is   | |                           |    |    |        removed from the passenger     | |                           |    |    |        cabin, and                     | |                           |    |    |     b) Required distribution is       | |                           |    |    |        maintained.                    | |                           |    |    |                                       | |                           |    |    | NOTE: Not required for All-Cargo      | |                           |    |    |       operations.                     | |                           |    |    |                                       | | 40-1  Service           C | 1  | 0  | (O)May be inoperative provided:       | | ***   Interphone          |    |    |     a) Procedures do not require      | |       System (Flight      |    |    |        its use,                       | |       Deck to Cabin)      |    |    |     b) PA system operates normally,   | |       (Cabin to Flight    |    |    |        and                            | |       Deck) (Flight       |    |    |     c) Alternate, normal and          | Page 24

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F27R30D.txt

|       Deck to Ground)     |    |    |        emergency procedures are       | |                           |    |    |        established and used.          | |                           |    |    |                                       | | 50-1  Flight Deck       D | 2  | 0  | May be inoperative provided:          | | ***   Speakers            |    |    |     a) Operative headphones are       | |       (Communications     |    |    |        available to each flight       | |       Function)           |    |    |        deck crewmember, and           | |                           |    |    |     b) Aural Alert Functions of       | |                           |    |    |        both speakers are operative.   | |                           |    |    |                                       | | 50-2  Observers Audio   A | 1  | 0  | May be inoperative provided:          | | ***   Panel               |    |    |     a) Associated Observer's Seat     | |                           |    |    |        is considered inoperative,     | |                           |    |    |        and                            | |                           |    |    |     b) Repair is made within two      | |                           |    |    |        flight days.                   | |                           |    |    |                                       | | 70-1  Cockpit Voice     A | 1  | 0  | May be inoperative provided:          | |       Recorder (CVR)      |    |    |     a) Flight Data Recorder (FDR)     | |                           |    |    |        operates normally, and         | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days.             | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 23-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 70-2  Observer          A | -  | 0  | May be inoperative provided:          | |       Headphone           |    |    |     a) Associated Observer Seat is    | |                           |    |    |        considered inoperative, and    | |                           |    |    |     b) Repair is made within two      | |                           |    |    |        flight days.                   | |                           |    |    |                                       | | 70-3  Observer          A | -  | 0  | May be inoperative provided:          | |       Microphone (Boom    |    |    |     a) Associated Observer Seat is    | |       or Hand Held)       |    |    |        considered inoperative, and    | |                           |    |    |     b) Repair is made within two      | |                           |    |    |        flight days.                   | |                           |    |    |                                       | | 70-4  Boom              A | -  | 0  | May be inoperative provided:          | | ***   Microphones         |    |    |     a) Flight Data Recorder (FDR)     | |                           |    |    |        operates normally, and         | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days.             | |                           |    |    |                                       | | 70-5  Radio Telephone   D | -  | -  |                                       | |                           |    |    |                                       | Page 25

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F27R30D.txt

|                           |    |    | NOTE: May be used to meet FAR         | |                           |    |    |       Communications requirement.     | |                           |    |    |                                       | | 99-1  Static              |    |    | DELETED in revision 30.  See          | |       Dischargers         |    |    | appropriate CDL.                      | |       (Fokker F-27        |    |    |                                       | |       Only)               |    |    |                                       | |                           |    |    |                                       | | 99-2  Static Discharge    |    |    | DELETED in revision 30.  See          | | ***   Cables on Main      |    |    | appropriate CDL.                      | |       Landing Gear        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 24-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 20-1  Main Invertor     C | -  | 2  | (O)May be inoperative provided        | |       Systems (Static     |    |    | remaining Main Invertors are          | |       or Rotary)          |    |    | verified to power the main AC power   | |                           |    |    | bus.                                  | |                           |    |    |                                       | | 20-2  Essential         C | 1  | 0  | (O)May be inoperative provided:       | |       Invertor System     |    |    |     a) Aircraft is operated in day    | |       (Fokker F27)        |    |    |        VMC, and                       | |                           |    |    |     b) At least two Main Invertors    | |                           |    |    |        are operative.                 | |                           |    |    |                                       | | 20-3  Emergency         C | 2  | 1  | (O)One may be inoperative             | |       Alternator          |    |    | provided:                             | |       Systems             |    |    |     a) Aircraft is operated in day    | |       (Fairchild          |    |    |        VMC, and                       | |       F27/FH227)          |    |    |     b) Both Main Invertors are        | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 20-4  AC Voltmeter        |    |    | DELETED in revision 30.               | |                           |    |    |                                       | | 20-5  Frequency         C | 1  | 0  |                                       | | ***   Meter System        |    |    |                                       | Page 26

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F27R30D.txt

|                           |    |    |                                       | | 20-6  Bus               C | -  | 0  |                                       | | ***   Annunciators On     |    |    |                                       | |       Overhead Panel      |    |    |                                       | |       (OHP) Systems       |    |    |                                       | |                           |    |    |                                       | | 20-7  Power Fail        C | 2  | 1  |                                       | | ***   Indicator On        |    |    |                                       | |       Main Instrument     |    |    |                                       | |       Panel (MIP)         |    |    |                                       | |       Systems             |    |    |                                       | |                           |    |    |                                       | | 20-8  Static            C | 2  | 0  | May be inoperative provided           | | ***   Invertor            |    |    | aircraft is not operated at night.    | |       (Lighting)          |    |    |                                       | |       Systems             |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 24-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 20-9  Alternator/       C | 2  | 1  | (M)(O)One may be inoperative          | |       Generator           |    |    | provided:                             | |       Systems             |    |    |     a) Affected Alternator            | |                           |    |    |        /Generator is verified         | |                           |    |    |        mechanically sound,            | |                           |    |    |     b) Airplane is not operated in    | |                           |    |    |        known or forecast icing        | |                           |    |    |        conditions,                    | |                           |    |    |     c) AFM Limitations for            | |                           |    |    |        associated systems are         | |                           |    |    |        observed, and                  | |                           |    |    |     d) Associated Alternator          | |                           |    |    |        /Generator Overheat Warning    | |                           |    |    |        Light System is operative.     | |                           |    |    |           OR                          | |                         C |    |    |     e) Affected Alternator            | |                           |    |    |        /Generator is verified         | |                           |    |    |        mechanically sound,            | |                           |    |    |     f) Associated Alternator          | |                           |    |    |        /Generator Overheat Warning    | |                           |    |    |        Light System is operative,     | |                           |    |    |        and                            | |                           |    |    |     g) APU Alternator/Generator       | |                           |    |    |        powers the associated bus.     | |                           |    |    |                                       | Page 27

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| 20-11 Alternator/       C | 2  | 1  | (O)One may be inoperative             | | ***   Generator           |    |    | provided:                             | |       Voltmeter           |    |    |     a) All associated AC Alternator   | |       Systems             |    |    |        /Generator System components   | |                           |    |    |        are operative, and             | |                           |    |    |     b) AC Ammeter is operative.       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 24-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 20-13 Alternator/       C | 2  | 1  | (O)One may be inoperative             | | ***   Generator           |    |    | provided:                             | |       Undervoltage/       |    |    |     a) Associated AC                  | |       Caution Systems     |    |    |        Alternator/Generator system    | |                           |    |    |        components are operative,      | |                           |    |    |        and                            | |                           |    |    |     b) AC Ammeter is operative.       | |                           |    |    |           OR                          | |                         C |    |    |     c) Associated Alternator/         | |                           |    |    |        Generator is considered        | |                           |    |    |        inoperative.                   | |                           |    |    |                                       | | 20-14 Alternator/       C | 2  | 1  | (M)One may be inoperative             | | ***   Generator           |    |    | provided:                             | |       Overheat Warning    |    |    |     a) The associated Alternator      | |       Light Systems       |    |    |        has been removed from the      | |                           |    |    |        accessory gear box,            | |                           |    |    |     b) The airplane is not operated   | |                           |    |    |        in known or forecast icing     | |                           |    |    |        conditions, and                | |                           |    |    |     c) AFM Limitations are            | |                           |    |    |        observed.                      | |                           |    |    |                                       | | 20-15 Alternator/       C | 2  | 1  | (O)One may be inoperative             | |       Generator           |    |    | provided:                             | |       Caution Lights      |    |    |     a) Associated AC Alternator       | |                           |    |    |        /Generator system components   | |                           |    |    |        are operative, and             | Page 28

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|                           |    |    |     b) AC Ammeter is operative.       | |                           |    |    |                                       | | 21-1  Battery Systems   C | -  | 2  | (M)May be inoperative provided        | |                           |    |    | affected Battery is isolated.         | |                           |    |    |                                       | | 21-2  Battery           C | -  | -  | (M)May be inoperative provided:       | | ***   Temperature         |    |    |     a) One system is operative for    | |       Monitor Systems     |    |    |        each operating battery, and    | |       (Indicator &        |    |    |     b) Associated Battery is          | |       Caution Light)      |    |    |        electrically disconnected      | |                           |    |    |        and secured.                   | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 d     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 06/11/97        | 24-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 30-1  Engine Driven DC  C | 2  | 1  | (M)(O)One may be inoperative          | |       Generator           |    |    | provided:                             | |       Systems             |    |    |     a) Associated DC Generator is     | |                           |    |    |        verified mechanically sound,   | |                           |    |    |     b) APU Generator System is used   | |                           |    |    |        throughout the flight, and     | |                           |    |    |     c) Aircraft is operated at or     | |                           |    |    |        below FL210.                   | |                           |    |    |                                       | | 30-2  DC Ammeter        B | 2  | 1  | (O)One may be inoperative provided    | |       Systems             |    |    | procedures are established to limit   | |                           |    |    | load if generator fails.              | |                           |    |    |                                       | | 30-3  DC Voltmeter        |    |    | DELETED in revision 30.               | |                           |    |    |                                       | | 30-4  DC Generator      C | 2  | 1  | (M)One may be inoperative             | |       Inoperative         |    |    | provided:                             | |       Caution/Failure     |    |    |     a) Associated DC Generator is     | |       Light Systems       |    |    |        operative, and                 | |                           |    |    |     b) Associated Ammeter and         | |                           |    |    |        Voltmeter are operative.       | |                           |    |    |                                       | | 30-5  DC Generator      C | 2  | 1  | (M)One may be inoperative             | |       Overheat Warning    |    |    | provided:                             | |       Lights              |    |    |     a) Associated Generator has       | |                           |    |    |        been removed from the          | |                           |    |    |        accessory gear box,            | |                           |    |    |     b) APU Generator System is used   | |                           |    |    |        throughout the flight, and     | |                           |    |    |     c) Aircraft is operated at or     | |                           |    |    |        below FL210.                   | Page 29

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|                           |    |    |                                       | | 30-6  External Power    C | 1  | 0  | (M)May be inoperative provided      | | |       Overvolt System     |    |    | system is deactivated by an         | | |      (With STC ST00395SE  |    |    | acceptable procedure.               | | |       Installed)          |    |    |                                     | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 25-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-1  Observer Seat     A | -  | -  | May be inoperative provided:          | |       (Including          |    |    |                                       | |       associated          |    |    |     (a)  A passenger seat in the      | |       equipment)          |    |    |     passenger cabin is made           | |                           |    |    |     available to an FAA inspector     | |                           |    |    |     for the performance of official   | |                           |    |    |     duties, or                        | |                           |    |    |                                       | |                           |    |    |     (c)  Second observer seat is      | |                           |    |    |     available, functional, and        | |                           |    |    |     acceptable, including             | |                           |    |    |     peripheral equipment, to an FAA   | |                           |    |    |     inspector for the performance     | |                           |    |    |     of official duties, and           | |                           |    |    |                                       | |                           |    |    |     (d)  Operations are limited to    | |                           |    |    |     not more than two flight days     | |                           |    |    |     before repairs are made.          | |                           |    |    |                                       | | 10-2  Pilot's Seat      C | 2  | 1  | (M)One may be inoperative             | |       Vertical            |    |    | provided:                             | |       Adjustment Mode     |    |    |     a) Seat is secured at the         | |                           |    |    |        individual crewmembers         | |                           |    |    |        requirements, and              | |                           |    |    |     b) Fore-aft adjustments           | |                           |    |    |        operates normally.             | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 30

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



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 25-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 20-1  Flight Attendant  C | -  | -  | (M)(O)One Single or Dual Position     | |       Seat Assembly       |    |    | Seat may be inoperative provided:     | |       (Single or Dual     |    |    |     a) Affected Seat Position(s) is   | |       Position)           |    |    |        not occupied,                  | |                           |    |    |     b) Flight Attendants 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, and        | |                           |    |    |     e) Passenger Seat(s) assigned     | |                           |    |    |        to Flight Attendant(s) is      | |                           |    |    |        placarded "FOR FLIGHT          | |                           |    |    |        ATTENDANT USE ONLY".           | |                           |    |    |                                       | |                           |    |    | NOTE 1:  A folding type seat that     | |                           |    |    |          will not stow                | |                           |    |    |          automatically is             | |                           |    |    |          considered inoperative.      | |                           |    |    |                                       | |                           |    |    | NOTE 2:  A Flight Attendant Seat      | |                           |    |    |          Position with an             | |                           |    |    |          inoperative Lap Belt is      | |                           |    |    |          considered inoperative.      | |                           |    |    |                                       | | 20-2  Passenger Seat    C | -  | -  | May be inoperative or missing         | |       Belts               |    |    | provided:                             | |                           |    |    |     a) The associated seat is         | Page 31

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|                           |    |    |        considered inoperative, and    | |                           |    |    |     b) The associated seat is         | |                           |    |    |        blocked and placarded "DO      | |                           |    |    |        NOT OCCUPY".                   |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 25-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 20-4  Overhead          C | -  | -  | (M)Bin closed latch may be            | | ***   Stowage Bins        |    |    | inoperative provided bin is not       | |                           |    |    | used for stowage and lid is secured   | |                           |    |    | in the closed position or removed.    | |                           |    |    |                                       | | 61-1  Flotation         C | -  | -  | Any in excess of those required by    | |       Devices             |    |    | FAR may be inoperative.               | |                           |    |    |                                       | | 62-1  "Fasten Seat      C | -  | -  | One or more signs or placards may     | |       Belt While          |    |    | be illegible or missing provided a    | |       Seated" Signs or    |    |    | legible sign or placard is readable   | |       Placards            |    |    | from each occupied passenger seat.    | |                           |    |    |                                       | | 62-2  Passenger Seats   C | -  | -  | (M)May be inoperative provided:       | |                           |    |    |     a) Affected Seat is               | |                           |    |    |        appropriately secured or       | |                           |    |    |        deactivated so that it does    | |                           |    |    |        not block emergency egress     | |                           |    |    |        to an aisle or exit, and       | |                           |    |    |     b) Affected seat is blocked       | |                           |    |    |        using an accepted procedure    | |                           |    |    |        and placarded "DO NOT          | |                           |    |    |        OCCUPY".                       | |                           |    |    |                                       | |                           |    |    | NOTE 1:  A seat with an inoperative   | |                           |    |    |          lap belt is considered       | |                           |    |    |          inoperative.                 | |                           |    |    |                                       | |                           |    |    | NOTE 2:  A seat with an inoperative   | |                           |    |    |          recline mechanism is         | |                           |    |    |          considered to be             | |                           |    |    |          inoperative if the seat      | |                           |    |    |          cannot be secured in the     | |                           |    |    |          upright position.            | |                           |    |    |                                       | |                           |    |    | NOTE 3:  Inoperative seats do not     | |                           |    |    |          affect the number of         | |                           |    |    |          Flight Attendants required   | |                           |    |    |          by FAR.                      | Page 32

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 25-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 62-3  Passenger           | -  | 0  | Passenger convenience items, as       | |       Convenience         |    |    | expressed in this MMEL, are those     | |       Items               |    |    | 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.  Items addressed elsewhere in    | |                           |    |    | this document shall not be            | |                           |    |    | included.  (M) or (O) procedures      | |                           |    |    | may be required and included in the   | |                           |    |    | Air Carrier's appropriate document.   | |                           |    |    |                                       | |                           |    |    | NOTE: Lavatory Door Ash Trays are     | |                           |    |    |       not to be included.             | |                           |    |    |                                       | | 99-1  First Aid Kits    D | -  | -  | Any in excess or those required by    | |                           |    |    | FAR may be inoperative.               | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |

Page 33

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 26-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-1  HPC Handle        C | 2  | 0  |                                       | | ***   Warning Light       |    |    |                                       | |       Systems             |    |    |                                       | |       (Fokker 27)         |    |    |                                       | |                           |    |    |                                       | | 10-2  Alarm Bell        B | 1  | 0  |                                       | | ***   System              |    |    |                                       | |                           |    |    |                                       | | 12-1  Cargo             C | -  | 0  | (O)May be inoperative provided:       | | ***   Compartment         |    |    |     a) Associated Cargo Compartment   | |       Smoke Detection     |    |    |        remains empty.                 | |       Systems             |    |    |           OR                          | |                         C |    |    |     b) Cargo is non-combustible       | |                           |    |    |        material.                      | |                           |    |    |                                       | |       1) Forward Cargo  C | 1  | 0  | (O)May be inoperative provided:       | |          Compartment      |    |    |     a) Crew has unobstructed access   | |                           |    |    |        to Cargo Area, and             | |                           |    |    |     b) Passenger Cabin to Cargo       | |                           |    |    |        Compartment Door remains       | |                           |    |    |        closed.                        | |                           |    |    |                                       | |       2) Aft Cargo      C | 1  | 0  | (O)May be inoperative provided:       | |          Compartment      |    |    |     a) Cargo Compartment to Cabin     | |                           |    |    |        Door is blocked OPEN, and      | |                           |    |    |     b) Cabin attendant is advised     | |                           |    |    |        of the condition.              | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | Page 34

F27R30D.txt

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F27R30D.txt

|                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 26-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 12-2  Lavatory Smoke    C | -  | -  | (M)For each lavatory, the lavatory    | |       Detection           |    |    | smoke detection system may be         | |       Systems             |    |    | inoperative provided:                 | |                           |    |    |     a) Lavatory fire extinguisher     | |                           |    |    |        system is operative.           | |                           |    |    |           OR                          | |                         C |    |    |     b) The 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.        | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | Page 35

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F27R30D.txt

| --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 26-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 12-3  Cargo             C | -  | -  | Individual Detectors may be           | |       Compartment         |    |    | inoperative provided minimum          | |       Smoke Detectors     |    |    | acceptable detector configuration     | |       (Cargo              |    |    | is complied with.                     | |       Configuration       |    |    |                                       | |       Only)               |    |    | NOTE: The above configuration         | |                           |    |    |       should be specified in one of   | |                           |    |    |       the following:                  | |                           |    |    |       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), or        | |                           |    |    |       d) An FAA approved report       | |                           |    |    |          incorporated in the Master   | |                           |    |    |          Drawing List for the         | |                           |    |    |          applicable STC.              | |                           |    |    |                                       | | 22-1  Portable Fire     C | -  | -  | Any in excess of those required by    | |       Extinguishers       |    |    | FAR may be inoperative.               | |                           |    |    |                                       | | 22-2  APU Fire          C | -  | -  | May be inoperative provided APU is    | | ***   Detection System    |    |    | considered inoperative.               | |                           |    |    |                                       | | 22-3  APU Fire          C | -  | -  | May be inoperative provided APU is    | | ***   Extinguishing       |    |    | considered inoperative.               | |       System              |    |    |                                       | |                           |    |    |                                       | | 30-1  Engine Fire       C | 4  | 2  | (O)One loop per engine may be         | | ***   Detection Loops     |    |    | inoperative provided the remaining    | |       (Fairchild          |    |    | loop is operative.                    | |       F27/FH227) Dual     |    |    |                                       | |       Loop System         |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | Page 36

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F27R30D.txt

|           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 26-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 30-2  Lavatory Fire     C | -  | -  | (M)May be inoperative provided the    | |       Extinguisher        |    |    | associated:                           | |       System              |    |    |     a) Lavatory smoke detection       | |                           |    |    |        system(s) operates normally.   | |                           |    |    |           OR                          | |                         C |    |    |     b) Lavatory waste receptacle is   | |                           |    |    |        empty,                         | |                           |    |    |     c) Lavatory door is locked 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:  Not required for all-cargo   | |                           |    |    |          operations.                  | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 27-1     | | --------------------------------------------------------------------------- | Page 37

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F27R30D.txt

|                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 27  FLIGHT CONTROLS       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-1  Trim Tab            |    |    |                                       | |       Indicators          |    |    |                                       | |                           |    |    |                                       | |       1) Aileron        C | 1  | 0  | May be inoperative provided tab is    | |                           |    |    | verified in neutral position before   | |                           |    |    | each takeoff.                         | |                           |    |    |                                       | |       2) Rudder         C | 1  | 0  | May be inoperative provided tab is    | |                           |    |    | verified in neutral position before   | |                           |    |    | each takeoff.                         | |                           |    |    |                                       | | 60-1  Speed Control     C | 1  | 0  |                                       | | ***   Indicator           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 28-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | Page 38

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F27R30D.txt

| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 20-1  Fuel Boost Pump   C | 4  | 2  | (O)One Boost Pump per engine may      | |       Systems             |    |    | be inoperative provided AFM           | |                           |    |    | Limitations are observed.             | |                           |    |    |                                       | | 20-2  Fuel Heater       C | 2  | 0  | (M)(O)Both may be inoperative         | |       Systems             |    |    | provided:                             | |                           |    |    |     a) AFM Limitations are            | |                           |    |    |        observed,                      | |                           |    |    |     b) Hot Air Gate Valve remains     | |                           |    |    |        CLOSED.                        | |                           |    |    |                                       | | 20-3  Inboard Tank      C | 2  | 0  | (O)One or both may be inoperative     | | ***   Fuel Transfer       |    |    | provided:                             | |       Systems (Manual     |    |    |     a) All fuel in affected inboard   | |       System)             |    |    |        tank is included in aircraft   | |                           |    |    |        zero fuel weight, and          | |                           |    |    |     b) Operations procedures are      | |                           |    |    |        established to maintain fuel   | |                           |    |    |        symmetry within AFM            | |                           |    |    |        Limitations.                   | |                           |    |    |                                       | | 20-4  Auto Fuel         C | 2  | 0  | (M)May be inoperative provided:       | |       Transfer Systems    |    |    |     a) Associated Fuel Quantity       | |       (Fokker 27)         |    |    |        Indication System is           | |                           |    |    |        operative, and                 | |                           |    |    |     b) Manual Fuel Transfer is        | |                           |    |    |        verified operative.            | |                           |    |    |                                       | | 22-1  Pressure          C | -  | 0  |                                       | |       Refueling           |    |    |                                       | |       Systems             |    |    | NOTE: Overwing refueling of inboard   | |                           |    |    |       tank is not possible.           | |                           |    |    |                                       | | 22-2  Nacelle Fuel      C | 2  | 0  | (M)May be inoperative provided        | | ***   Quantity            |    |    | fuel quantity is verified by          | |       Indicator           |    |    | alternate means.                      | |       Systems             |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 28-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | Page 39

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| 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 42-1  Fuel Pressure     C | 2  | 0  | May be inoperative provided all       | | ***   Indicator           |    |    | Fuel Pressure Warning Lights are      | |       Systems             |    |    | operative.                            | |                           |    |    |                                       | | 43-1  Fuel Quantity     C | 2  | 1  | (M)(O)One may be inoperative          | |       Indicator           |    |    | provided:                             | |       Systems (Flight     |    |    |     a) Fuel Quantity is verified by   | |       Compartment)        |    |    |        alternate means before each    | |                           |    |    |        departure,                     | |                           |    |    |     b) Associated Fuel Flow Meter     | |                           |    |    |        is operative, and              | |                           |    |    |     c) A Fuel Log is maintained.      | |                           |    |    |                                       | | 43-2  Fuel Quantity     C | 2  | 1  | (M)(O)One may be inoperative          | | ***   Indication          |    |    | provided:                             | |       Inboard Tank        |    |    |     a) Inboard Fuel Quantity is       | |       Systems             |    |    |        verified by alternate means    | |                           |    |    |        before each departure,         | |                           |    |    |     b) Auto Fuel Transfer is used,    | |                           |    |    |        and                            | |                           |    |    |     c) A Fuel Log is maintained.      | |                           |    |    |                                       | |                         C | 2  | 0  | (M)(O)One or both may be              | |                           |    |    | inoperative provided:                 | |                           |    |    |     a) Inboard Fuel Tanks are not     | |                           |    |    |        used,                          | |                           |    |    |     b) Fuel in Inboard Tanks is       | |                           |    |    |        considered to be unusable,     | |                           |    |    |        and                            | |                           |    |    |     c) Fuel in Inboard Tanks is       | |                           |    |    |        considered as payload.         | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 28-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 40

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| 46-1  Fuel Low            |    |    |                                       | |       Pressure Caution    |    |    |                                       | |       Lights Systems      |    |    |                                       | |                           |    |    |                                       | |       1) 4 Light        C | 4  | 2  | (O)Two may be inoperative             | |          System           |    |    | provided:                             | |                           |    |    |     a) One Light is operative on      | |                           |    |    |        each side, and                 | |                           |    |    |     b) Pump with serviceable Light    | |                           |    |    |        Remains ON for single pump     | |                           |    |    |        operations.                    | |                           |    |    |                                       | |       2) 2 Light        C | 2  | 1  | (O)One may be inoperative             | |          System           |    |    | provided:                             | |                           |    |    |     a) Associated Pressure Gauge is   | |                           |    |    |        operative, and                 | |                           |    |    |     b) Four boost pumps remain ON.    | |                           |    |    |                                       | | 46-2  Low Fuel          C | 2  | 0  |                                       | | ***   Level Warning       |    |    |                                       | |       Lights              |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 30-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 30  ICE AND RAIN          |    |    |                                       | |     PROTECTION            |    |    |                                       | |                           |    |    |                                       | | 10-1  Airfoil DeIcing   C | 1  | 0  | May be inoperative provided           | |       System (Wing &      |    |    | aircraft is not operated into known   | Page 41

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|       Empennage)          |    |    | or forecast icing conditions.         | |                           |    |    |                                       | | 30-1  Pilot/Static        |    |    |                                       | |       Heating Systems     |    |    |                                       | |                           |    |    |                                       | |       1) Pitot Heater   B | 2  | 1  | (M)(O)One may be inoperative          | |          Systems          |    |    | provided:                             | |                           |    |    |     a) Affected Pitot Heating         | |                           |    |    |        System is secured,             | |                           |    |    |     b) Aircraft is operated in day    | |                           |    |    |        VMC,                           | |                           |    |    |     c) Aircraft is not operated in    | |                           |    |    |        known or forecast icing        | |                           |    |    |        conditions, and                | |                           |    |    |     d) Associated Pitot Heat          | |                           |    |    |        Switches remain ON for         | |                           |    |    |        operative Heating systems.     | |                           |    |    |                                       | |       2) Static Port    B | 1  | 0  | (M)May be inoperative provided        | |          Heating          |    |    | Static Port Heating System is         | |          System           |    |    | secured.                              | |                           |    |    |                                       | | 40-1  Windshield Wiper  C | 2  | 0  | Both may be inoperative provided      | |       Systems             |    |    | airplane is not operated in           | |                           |    |    | precipitation within 5 nautical       | |                           |    |    | miles of the airport of takeoff or    | |                           |    |    | intended landing.                     | |                           |    |    |                                       | | 41-1  Windshield        C | 2  | 0  | (M)Both may be inoperative            | |       Heating Systems     |    |    | provided:                             | |                           |    |    |     a) Aircraft is not operated in    | |                           |    |    |        known or forecast icing        | |                           |    |    |        conditions, and                | |                           |    |    |     b) AFM Limitations are            | |                           |    |    |        observed.                      | |                           |    |    |                                       | | 42-1  Windshield        D | 1  | 0  |                                       | | ***   Wash System         |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 30-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 30  ICE AND RAIN          |    |    |                                       | |     PROTECTION            |    |    |                                       | |                           |    |    |                                       | | 43-1  Windshield and    D | 2  | 0  |                                       | |       Direct Vision       |    |    |                                       | |       Window Demisting    |    |    |                                       | |       Systems             |    |    |                                       | |       (Fokker 27)         |    |    |                                       | Page 42

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|                           |    |    |                                       | | 60-1  Power Unit        C | 2  | 1  | One may be inoperative provided       | |       Engine/Propeller    |    |    | aircraft is not operated in known     | |       Deicing Systems     |    |    | or forecast icing conditions.         | |                           |    |    |                                       | | 60-2  Rain              D | -  | 0  |                                       | | ***   Repellent           |    |    |                                       | |       Systems             |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 31-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 31  INDICATING/RECORDING  |    |    |                                       | |     SYSTEMS               |    |    |                                       | |                           |    |    |                                       | | 20-1  Clocks (Cockpit)  C | -  | 1  |                                       | |                           |    |    |                                       | | 30-1  Flight Data       A | 1  | 0  |  May be inoperative provided:         | |       Recorder (FDR)      |    |    |     a) Cockpit Voice Recorder (CVR)   | |       System              |    |    |        operates normally, and         | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days.             | Page 43

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|                           |    |    |                                       | | 30-2  Fatigue Meter     D | 1  | 0  |                                       | | ***   System              |    |    |                                       | |       (Fokker 27)         |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 d     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 06/11/97        | 32-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 32  LANDING GEAR          |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 40-1  Anti-Skid System  C | 1  | 0  | (M)May be inoperative provided:       | |                           |    |    |     a) Required runway length is      | |                           |    |    |        increased in accordance with   | |                           |    |    |        AFM performance information,   | |                           |    |    |        and                            | |                           |    |    |     b) Inoperative units are set      | |                           |    |    |        free from the driving track.   | |                           |    |    |                                       | | 40-2  Parking Brake     C | 1  | 0  | (O)May be inoperative provided        | Page 44

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|       System              |    |    | Alternate Brakes System is used to    | |       (Fokker 27)         |    |    | set Brakes.                           | |                           |    |    |                                       | | 50-1  Nosewheel         C | 1  | 0  | (M)May be inoperative provided:       | |       Steering System     |    |    |     a) The nosewheel steering is      | |                           |    |    |        deactivated,                   | |                           |    |    |     b) The takeoff distance is        | |                           |    |    |        increased by 10%, and          | |                           |    |    |     c) Maximum crosswind is limited   | |                           |    |    |        to 10 kts.                     | |                           |    |    |                                       | | 60-1  Nose Gear         C | 2  | 1  |                                       | |       Position Lights     |    |    |                                       | |       (With S/B 32-121    |    |    |                                     | | |        Installed)         |    |    |                                     | | |                           |    |    |                                       | | 60-2  Main Gear         C | 4  | 2  | (M)One Position Light for each main | | | ***   Position Lights     |    |    | gear may be inoperative provided    | | |      (With STC ST00354SE  |    |    | primary or secondary Gear Position  | | |       Installed)          |    |    | system operates normally.           | | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 33-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10-1  Cockpit and       C | -  | -  | May be inoperative provided:          | |       Instrument          |    |    |     a) Sufficient lighting is         | |       Lighting Systems    |    |    |        operative to make each         | |       (Excluding EFIS     |    |    |        instrument, control and        | |       and MFDS and        |    |    |        other device for which it is   | |       Emergency           |    |    |        provided easily readable,      | |       Lighting)           |    |    |     b) Direct rays and reflections    | |                           |    |    |        do not impair visibility       | |                           |    |    |        either inside or outside of    | |                           |    |    |        the aircraft,                  | |                           |    |    |     c) Lighting intensity can be      | Page 45

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|                           |    |    |        controlled, or is preset to    | |                           |    |    |        a satisfactory level for       | |                           |    |    |        expected flight conditions,    | |                           |    |    |        and                            | |                           |    |    |     d) Lighting configuration at      | |                           |    |    |        dispatch is acceptable to      | |                           |    |    |        the flight crew.               | |                           |    |    |                                       | | 10-3  Master            B | 1  | 0  |                                       | | ***   Warning System      |    |    |                                       | |       (Fokker 27)         |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 33-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 20-1  No Smoking/         |    |    |                                       | |       Fasten Seat Belt    |    |    |                                       | |       Signs               |    |    |                                       | |                           |    |    |                                       | |       1) Passenger      C | -  | -  | (O)May be inoperative provided:       | |          Configuration    |    |    |     a) Passenger or Flight            | |                           |    |    |        Attendant Seats from which a   | |                           |    |    |        readily legible NO             | |                           |    |    |        SMOKING/FASTEN SEAT BELT       | |                           |    |    |        sign cannot be seen are        | |                           |    |    |        placarded inoperative and      | |                           |    |    |        "DO NOT OCCUPY."               | |                           |    |    |           OR                          | |                         C |    |    |     b) Operations procedures are      | Page 46

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F27R30D.txt

|                           |    |    |        established for alerting the   | |                           |    |    |        cabin attendants and           | |                           |    |    |        notifying the passengers by    | |                           |    |    |        use of the Passenger Address   | |                           |    |    |        System when seat belts         | |                           |    |    |        should be fastened and         | |                           |    |    |        smoking is prohibited.         | |                           |    |    |                                       | |       2) Cargo          C | -  | 0  |                                       | |          Configuration    |    |    |                                       | |                           |    |    |                                       | | 20-2  Cabin Interior    C | -  | -  |  May be inoperative provided:         | |       Lights              |    |    |     a) Cabin emergency lighting is    | |                           |    |    |        operative,                     | |                           |    |    |     b) Sufficient lighting is         | |                           |    |    |        operative for crew to          | |                           |    |    |        perform required duties, and   | |                           |    |    |     c) Lighting configuration at      | |                           |    |    |        dispatch is acceptable to      | |                           |    |    |        flight crew.                   | |                           |    |    |                                       | | 32-1  Maintenance Area  C | -  | 0  |                                       | |       and Service         |    |    |                                       | |       Panel Lights        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 33-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 40-1  Position Light    C | -  | 0  | May be inoperative provided           | |       Bulbs               |    |    | aircraft is not operated at night.    | |                           |    |    |                                       | |       1) 2 Bulb         C | 6  | 3  | Three may be inoperative provided     | |          Installation     |    |    | one is operative on each wingtip      | |                           |    |    | and one is operative on the tail.     | |                           |    |    |                                       | | 40-2  Landing Light     C | 2  | 1  | One may be inoperative provided       | |       Systems             |    |    | Taxi Light is operative.              | |                           |    |    |                                       | |                         C | 2  | 0  | Both may be inoperative provided      | |                           |    |    | aircraft is not operated at night.    | |                           |    |    |                                       | | 40-3  Taxi Light        C | 1  | 0  | May be inoperative provided:          | |       System              |    |    |     a) Aircraft is not operated at    | |                           |    |    |        night.                         | |                           |    |    |           OR                          | Page 47

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F27R30D.txt

|                         C |    |    |     b) Both Landing Lights are        | |                           |    |    |        operative.                     | |                           |    |    |                                       | | 40-4  Wing Inspection   C | 2  | 0  | May be inoperative provided a         | |       Lights              |    |    | portable lamp/light of adequate       | |                           |    |    | capacity for wing and/or control      | |                           |    |    | surface inspection is available for   | |                           |    |    | night operation in icing              | |                           |    |    | conditions.                           | |                           |    |    |                                       | | 40-5  Anti Collision    C | -  | 0  | May be inoperative provided           | |       Lights              |    |    | aircraft is not operated at night.    | |                           |    |    |                                       | |       1) Vertical       C | -  | 0  | May be inoperative provided Wing      | |          Stabilizer       |    |    | Tip Strobe Lights are installed and   | |          Anti-            |    |    | operative.                            | |          Collision        |    |    |                                       | |          Light            |    |    |                                       | |                           |    |    |                                       | | ***   2) Fuselage       C | 1  | 0  |                                       | |          Anti-            |    |    |                                       | |          Collision        |    |    |                                       | |          Light            |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    | |              FAIRCHILD F-27              |                       |          | |           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 33-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 33  LIGHTS                |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 40-6  Wing Tip Strobe   C | 1  | 0  |  May be inoperative provided:         | | ***   Light System        |    |    |     a) Vertical Stabilizer Anti-      | |                           |    |    |        Collision Light is             | |                           |    |    |        operative.                     | |                           |    |    |           OR                          | |                         C |    |    |   &nb