






                          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
                            FH-227 & FOKKER F-27


                              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       |           |
      | 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
                                                  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
                                                  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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                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/11/97

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                            Highlights of Change
















































                       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
                                                           Revision: 6
                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

                               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
                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

                               FAIRCHILD F-27
                            FH-227 & FOKKER F-27

                                 Definitions


       operation with the  listed item inoperative.

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

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

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

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

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



                       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
       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
                                                           Revision: 6
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                               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.

       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
                                                           Revision: 6
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                            FH-227 & FOKKER F-27

                                 Definitions


       do not affect dispatch and do not require action other than as  |
       addressed within an operators standard maintenance program.     |
                                                                       |
       b.   DOUGLAS  (MD-11)                                           |
                                                                       |
       Some Douglas aircraft are equipped with an alerting function    |
       which is a subsystem within the Electronic Instrument System    |
       (EIS).  The alerting function provides various levels of system |
       condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and   |
       STATUS).                                                        |
                                                                       |
       Alerts that affect aircraft dispatch will include WARNING,      |
       CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are   |
       displayed on the status page of the EIS display panel under the |
       maintenance heading.                                            |
                                                                       |
       A MAINTENANCE alert on the EIS indicates the presence of a      |
       system fault which can be identified by the Central Fault       |
       Display System (CFDS) interrogation.  The systems are designed  |
       to be fault tolerant, however, for any MAINTENANCE alert, the   |
       MEL must be verified for dispatch purposes.                     |
                                                                       |
       c.   AIRBUS  (A-300-600, A-310, A-320/319/321, A-330, A-340     |
                                                                       |
       Airbus aircraft equipped with Electronic Centralized Aircraft   |
       Monitoring (ECAM) provide different levels of system condition  |
       messages (WARNING, CAUTION, STATUS, and ADVISORY). A-320/319/   |
       321, A-330, and A-340 also provide MAINTENANCE status messages. |
                                                                       |
       Any message that effects airplane dispatchability will normally |
       be at the WARNING, CAUTION or STATUS level. MAINTENANCE         |
       messages (A-320/319/321, A-330, and A-340 only) are also        |
       indicated on ECAM Status Page below the white Maintenance label.|
                                                                       |
       A MAINTENANCE status (Class II) message on ECAM indicates the   |
       presence of a system fault which can be identified by CFDS      |
       (A-320/319/321) or CMS (A-330/A-340) interrogation. The systems |
       are designed to be fault tolerant, however for any MAINTENANCE  |
       status (Class II) message, the A-320/319/321 MEL must be        |
       verified for dispatch capability. For the A-330 and A-340,      |
       MAINTENANCE status messages do not affect dispatch.             |

       d.   FOKKER  (FK-100)                                           |



                       FEDERAL AVIATION ADMINISTRATION     Page: XIII
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                               FAIRCHILD F-27
                            FH-227 & FOKKER F-27

                                 Definitions


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

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

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

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

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



                       FEDERAL AVIATION ADMINISTRATION     Page: XIV
                                                           Revision: 6
                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

                               FAIRCHILD F-27
                            FH-227 & FOKKER F-27

                                 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
       D."







































                       FEDERAL AVIATION ADMINISTRATION   Page: XV
                                                         Revision: 2
                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/89

                               FAIRCHILD F-27
                            FH-227 & FOKKER F-27

                                  Preamble
                            (Effective 6/14/89)

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

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









                       FEDERAL AVIATION ADMINISTRATION   Page: 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     |
| --------------------------------------------------------------------------- |
|                        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            |
| 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      |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 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:          |
|       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                 |
|       (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  |                                       |
| ***                       |    |    |                                       |
|                           |    |    |                                       |
| 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.                              |
|                           |    |    |                                       |
| 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              |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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              |    |    |                                       |
|                           |    |    |                                       |
|       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          |
|       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 | -  | -  |                                       |
|                           |    |    |                                       |
|                           |    |    | 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        |    |    |                                       |
|                           |    |    |                                       |
| 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.     |
|                           |    |    |                                       |
| 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             |
|                           |    |    |     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.                   |
|                           |    |    |                                       |
| 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.             |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------

-------------------------------------------------------------------------------
| 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         |
|                           |    |    |        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.                      |
|                           |    |    |                                       |
-------------------------------------------------------------------------------

-------------------------------------------------------------------------------
| 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.               |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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                                           |
|                                                                             |
|                                            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                                             |
| --------------------------------------------------------------------------- |
| 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              |                       |          |
|           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     |
| --------------------------------------------------------------------------- |
|                        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 &                  |    -------------------------------------------- |
| 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              |
| 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                  |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 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   |
|       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)         |    |    |                                       |
|                           |    |    |                                       |
| 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.             |
|                           |    |    |                                       |
| 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        |
|       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      |
|                           |    |    |        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      |
|                           |    |    |        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                          |
|                         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 |    |    |     b) Aircraft is not operated at    |
|                           |    |    |        night.                         |
|                           |    |    |                                       |
| 40-7  High              C | -  | 0  |                                       |
| ***   Intensity           |    |    |                                       |
|       Recognition         |    |    |                                       |
|       Light Systems       |    |    |                                       |
|                           |    |    |                                       |
| 40-8  Logo Light        D | 2  | 0  |                                       |
| ***   Systems             |    |    |                                       |
|                           |    |    |                                       |
| 50-1  Floor             C | 1  | 1  | Individual lights may be              |
| ***   Proximity Escape    |    |    | inoperative provided FAA approved     |
|       Path Marking        |    |    | minimum acceptable lighting levels    |
|       Lights System       |    |    | in one of the following documents     |
|       Lights              |    |    | are complied with:                    |
|                           |    |    |     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).             |
|                           |    |    |     d) FAA approved report            |
|                           |    |    |        incorporated in the Master     |
|                           |    |    |        drawing list for the           |
|                           |    |    |        applicable STC.                |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------

-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION                                           |
|                                                                             |
|                                            MASTER MINIMUM EQUIPMENT LIST    |
| FEDERAL AVIATION ADMINISTRATION                                             |
| --------------------------------------------------------------------------- |
| AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    |
|              FAIRCHILD F-27              |                       |          |
|           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 33-5     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 33  LIGHTS                |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 50-2  Cabin Interior    C | -  | -  | Individual lights may be              |
|       Emergency Lights    |    |    | inoperative provided FAA approved     |
|                           |    |    | minimum acceptable lighting levels    |
|                           |    |    | in one of the following documents     |
|                           |    |    | are complied with:                    |
|                           |    |    |     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).             |
|                           |    |    |     d) FAA approved report            |
|                           |    |    |        incorporated in the Master     |
|                           |    |    |        drawing list for the           |
|                           |    |    |        applicable STC.                |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION                                           |
|                                                                             |
|                                            MASTER MINIMUM EQUIPMENT LIST    |
| FEDERAL AVIATION ADMINISTRATION                                             |
| --------------------------------------------------------------------------- |
| AIRCRAFT:                                | REVISION NO: 30 b     | PAGE:    |
|              FAIRCHILD F-27              |                       |          |
|           FH-227 & FOKKER F-27           | DATE: 09/14/93        | 34-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 34  NAVIGATION            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 10-1 Rate-of-Climb      C | 2  | 1  | One may be inoperative provided the   |
|      Indicators           |    |    | aircraft is operated in day VMC.      |
|                           |    |    |                                       |
| 10-2 Overspeed          B | 1  | 0  | May be inoperative provided:          |
| ***  Warning              |    |    |     a) Both airspeed indicators       |
|                           |    |    |        operate normally, and          |
|                           |    |    |     b) The aircraft is operated at    |
|                           |    |    |        no greater than 15 KIAS less   |
|                           |    |    |        than VMO.                      |
|                           |    |    |                                       |
| 10-3 Outside Air        C | -  | 1  | May be inoperative provided ambient   |
|      Temperature          |    |    | air temperature is readily            |
|      Indication System    |    |    | available to the crew through other   |
|                           |    |    | means (e.g. SAT, RAT, or TAT.)        |
|                           |    |    |                                       |
| 10-4 Altimeters         C | -  | 2  | May be inoperative provided:          |
|                           |    |    |     a) One altimeter operates         |
|                           |    |    |        normally at each pilot         |
|                           |    |    |        station, and                   |
|                           |    |    |     b) At least one of the above is   |
|                           |    |    |        a pneumatic, or servo-         |
|                           |    |    |        pneumatic altimeter.           |
|                           |    |    |                                       |
| 10-5 Altitude           A | -  | 0  | (O)May be inoperative provided:       |
| ***  Alerting System      |    |    |     a) An alternate Operations        |
|                           |    |    |        Procedure is developed and     |
|                           |    |    |        used, and                      |
|                           |    |    |     b) Repair is made within three    |
|                           |    |    |        flight days.                   |
|                           |    |    |                                       |
| 20-1 Compass System     C | -  | 2  | May be inoperative provided:          |
|      Sensors              |    |    |     a) Both Directional Compass       |
|      (Directional Gyro,   |    |    |        Systems are operative from     |
|      AHRS, IRS, etc.)     |    |    |        independent sources, and       |
|                           |    |    |     b) Each pilot's panel has         |
|                           |    |    |        independent heading            |
|                           |    |    |        information.                   |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------

-------------------------------------------------------------------------------
| 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        | 34-2     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 34  NAVIGATION            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 20-2 Non-Stabilized     C | 1  | 0  | May be inoperative provided:          |
|      Magnetic (Standby)   |    |    |     a) Standby Compass is not         |
|      Compass              |    |    |        required by AFM Limitations,   |
|                           |    |    |        and                            |
|                           |    |    |     b) Two independent magnetic       |
|                           |    |    |        stabilized directional         |
|                           |    |    |        compass systems are            |
|                           |    |    |        operative.                     |
|                           |    |    |                                       |
| 20-3 Turn and Slip        |    |    |                                       |
| ***  Indicators           |    |    |                                       |
|                           |    |    |                                       |
|      1) Turn Indicator  C | 2  | 1  | May be inoperative provided:          |
|                           |    |    |     a) Aircraft is operated in Day    |
|                           |    |    |        VMC, and                       |
|                           |    |    |     b) Two independent Attitude       |
|                           |    |    |        Director Indicators are        |
|                           |    |    |        operative.                     |
|                           |    |    |          OR                           |
|                         C |    |    |     c) Standby Attitude Indicator     |
|                           |    |    |        is operative.                  |
|                           |    |    |                                       |
|      2) Slip Indicator  C | -  | 2  | May be inoperative provided one       |
|                           |    |    | operates normally on each pilot's     |
|                           |    |    | panel.                                |
|                           |    |    |                                       |
| 20-4 Flight Director    C | 2  | 0  | May be inoperative provided           |
| ***  Systems              |    |    | approach minimums do not require      |
|                           |    |    | their use.                            |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------

-------------------------------------------------------------------------------
| 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        | 34-3     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 34  NAVIGATION            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 20-5 Standby            B | 1  | 0  | May be inoperative provided:          |
| ***  Attitude Indicator   |    |    |     a) Pilot flying has an            |
|                           |    |    |        operative Turn and Slip        |
|                           |    |    |        Indicator.                     |
|                           |    |    |          OR                           |
|                         B |    |    |     b) Aircraft is operated in Day    |
|                           |    |    |        VMC, and                       |
|                           |    |    |     c) Standby Attitude Gyro is not   |
|                           |    |    |        required by AFM Limitations.   |
|                           |    |    |                                       |
| 20-6 Speed Control      C | 2  | 0  | May be inoperative provided           |
| ***  Indicators           |    |    | approach minimums and/or              |
|                           |    |    | operational procedures do not         |
|                           |    |    | require their use.                    |
|                           |    |    |                                       |
| 20-7 Flight Mode        C | 1  | 0  | May be inoperative provided           |
| ***  Panel                |    |    | Autopilot is not required for the     |
|                           |    |    | approach to be flown.                 |
|                           |    |    |                                       |
| 30-1 VHF Navigation     C | -  | -  | As required by FAR.                   |
|      Systems (VOR/ILS)    |    |    |                                       |
|                           |    |    |                                       |
| 30-2 Marker Beacon      C | -  | -  | May be inoperative provided           |
|      System               |    |    | approach minimums do not require      |
|                           |    |    | its use.                              |
|                           |    |    |                                       |
| 30-3 Radio Altimeter    A | -  | -  | May be inoperative provided:          |
|      Systems              |    |    |     a) Dispatch deviation for         |
|                           |    |    |        ground proximity warning       |
|                           |    |    |        system (GPWS) (if              |
|                           |    |    |        inoperative) is observed,      |
|                           |    |    |     b) Approach minimums or           |
|                           |    |    |        operating procedures do not    |
|                           |    |    |        require their use, and         |
|                           |    |    |     c) Repair is 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        | 34-4     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 34  NAVIGATION            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 40-1 Weather Radar      C | 1  | 0  | As required by FAR.                   |
|      System               |    |    |                                       |
|                           |    |    |                                       |
| 40-3 Ground Proximity     |    |    |                                       |
|      Warning System       |    |    |                                       |
|      (GPWS)               |    |    |                                       |
|                           |    |    |                                       |
|      a) Terrain         A | -  | 0  | May be inoperative provided:          |
|         Avoidance Modes   |    |    |     1) Two VHF Navigation Systems     |
|         1 thru 4)         |    |    |        operate normally.              |
|                           |    |    |                                       |
|                           |    |    |     2) Repairs are made within two    |
|                           |    |    |        flight days.                   |
|                           |    |    |                                       |
|      b) Test Mode       A | 1  | 0  | May be inoperative provided:          |
|                           |    |    |     1) The GPWS is considered         |
|                           |    |    |        inoperative.                   |
|                           |    |    |                                       |
|                           |    |    |     2) Repairs are made within two    |
|                           |    |    |        flight days.                   |
|                           |    |    |                                       |
|      c) Glideslope      B | 2  | 0  | One or both may be inoperative.       |
|         Deviation (Mode   |    |    |                                       |
|         5)                |    |    |                                       |
|                           |    |    |                                       |
|      d) Minimums        C | 1  | 0  |                                       |
|         Warning           |    |    |                                       |
|                           |    |    |                                       |
|      e) Windshear Mode  C | 1  | 0  |                                       |
|                           |    |    |                                       |
| 50-1 Distance Measuring C | -  | -  | As required by FAR.                   |
|      Equipment (DME)      |    |    |                                       |
|                           |    |    |                                       |
| 50-2 ATC Transponder    C | -  | -  | As required by FAR.                   |
|                           |    |    |                                       |
| 50-3 Radio Compass      C | -  | -  | As required by FAR.                   |
|      (ADF) 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        | 34-5     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 34  NAVIGATION            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 60-1 Microwave          D | -  | -  | As required by FAR.                   |
| ***  Landing Systems      |    |    |                                       |
|      (MLS)                |    |    |                                       |
|                           |    |    |                                       |
| 60-2 Area               D | -  | -  | As required by FAR.                   |
| ***  Navigation Systems   |    |    |                                       |
|                           |    |    |                                       |
| 60-3 Long Range         D | -  | 0  | Any in excess of those required by    |
| ***  Navigation Systems   |    |    | FAR may be inoperative.               |
|      (Incl. Omega/VLF     |    |    |                                       |
|      NAV, INS, LORAN C,   |    |    |                                       |
|      etc.)                |    |    |                                       |
|                           |    |    |                                       |
| 60-5 Standby            C | -  | 0  |                                       |
| ***  Airspeed Indicator   |    |    |                                       |
|                           |    |    |                                       |
| 60-6 Traffic Alert      C | 1  | 0  | May be inoperative provided the       |
|      Collision            |    |    | system is deactivated and secured.    |
|      Avoidance System     |    |    |                                       |
|      (TCAS)               |    |    |                                       |
|                           |    |    |                                       |
| ***  1) Combined TA and C | 2  | 1  | One may be inoperative on the non-    |
|         RA Dual           |    |    | flying pilot's side provided:         |
|         Displays          |    |    |     a) TA and RA elements and audio   |
|                           |    |    |        functions are operative on     |
|                           |    |    |        the flying pilot's side, and   |
|                           |    |    |     b) TA and RA display              |
|                           |    |    |        indications are visible to     |
|                           |    |    |        the non-flying pilot.          |
|                           |    |    |                                       |
|                           |    |    | (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        | 34-6     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 34  NAVIGATION            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 60-6 Traffic Alert        |    |    |                                       |
|      Collision            |    |    |                                       |
|      Avoidance System     |    |    |                                       |
|      (TCAS) (Cont'd)      |    |    |                                       |
|                           |    |    |                                       |
|      2) Resolution      C | 2  | 1  | (O)One may be inoperative on the      |
|         Advisory (RA)     |    |    | non-flying pilot's side.              |
|         Display Systems   |    |    |                                       |
|                           |    |    |                                       |
|                         C | -  | 0  | (O)may be inoperative provided:       |
|                           |    |    |     a) All Traffic Alert (TA)         |
|                           |    |    |        Display Elements and voice     |
|                           |    |    |        command audio functions are    |
|                           |    |    |        operative, and                 |
|                           |    |    |     b) TA only mode is selected by    |
|                           |    |    |        the crew.                      |
|                           |    |    |                                       |
|      3) TA Display      C | -  | 0  | (O)May be inoperative provided all    |
|         Systems           |    |    | installed RA Display and audio        |
|                           |    |    | functions are operative.              |
|                           |    |    |                                       |
| 60-7 Windshear          C | -  | 0  | As required by FAR.                   |
| ***  Systems              |    |    |                                       |
|                           |    |    |                                       |
| 60-8 Instrument         C | 1  | 0  | (O)May be inoperative provided        |
| ***  Comparator           |    |    | Instrument Comparator is not          |
|                           |    |    | required for the approach to flown.   |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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        | 35-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 35  OXYGEN                |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 10-1  Observer Oxygen   A | 1  | 0  | May be inoperative provided:          |
|       Systems             |    |    |     a) Observer Seat is not           |
|                           |    |    |        occupied by a person in an     |
|                           |    |    |        official capacity, and         |
|                           |    |    |     b) Repair is made within three    |
|                           |    |    |        flight days.                   |
|                           |    |    |                                       |
| 10-2  Passenger Oxygen  C | 1  | 0  | As required by FAR.                   |
|       System              |    |    |                                       |
|                           |    |    |                                       |
| 30-1  Portable Oxygen   C | -  | -  | Any in excess of those required by    |
|       Systems             |    |    | FAR may be inoperative.               |
|                           |    |    |                                       |
| 30-2  Protective        C | -  | -  | Any in excess of those required by    |
|       Breathing           |    |    | FAR may be inoperative.               |
|       Equipment (PBE)     |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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        | 36-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 36  PNEUMATIC             |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 10-1  Compressor        C | 2  | 1  | (M)One may be inoperative             |
|       Systems             |    |    | provided:                             |
|                           |    |    |     a) Affected Compressor is         |
|                           |    |    |        verified mechanically sound,   |
|                           |    |    |     b) Associated Caution Light is    |
|                           |    |    |        operative, and                 |
|                           |    |    |     c) AFM limitations are            |
|                           |    |    |        observed.                      |
|                           |    |    |                                       |
| ***   1) Caution Light  C | 2  | 1  | One may be inoperative provided       |
|                           |    |    | associated Compressor System is       |
|                           |    |    | considered inoperative.               |
|                           |    |    |                                       |
| 40-1  Main Cabin        C | 1  | 0  | (O)May be inoperative provided        |
| ***   Door Actuator       |    |    | procedures are established to         |
|       System              |    |    | ensure safety of ground personnel     |
|                           |    |    | during door opening.                  |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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        | 49-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 49  AIRBORNE AUXILIARY    |    |    |                                       |
|     POWER                 |    |    |                                       |
|                           |    |    |                                       |
| 10-1  Auxiliary         C | 1  | 0  | May be inoperative provided           |
| ***   Power Unit          |    |    | procedures do not require its use.    |
|                           |    |    |                                       |
|       1) DC Generator   C | 1  | 0  | (M)May be inoperative provided:       |
|                           |    |    |     a) Both engine driven             |
|                           |    |    |        generators are operative,      |
|                           |    |    |        and                            |
|                           |    |    |     b) APU is not used.               |
|                           |    |    |           OR                          |
|                         C |    |    |     c) Both engine driven             |
|                           |    |    |        generators are operative,      |
|                           |    |    |        and                            |
|                           |    |    |     d) APU DC generator is            |
|                           |    |    |        inspected and found            |
|                           |    |    |        mechanically sound.            |
|                           |    |    |                                       |
|       2) Alternator/    C | 1  | 0  | (M)May be inoperative provided:       |
|          Generator        |    |    |     a) APU is not used.               |
|                           |    |    |           OR                          |
|                         C |    |    |     b) APU A/C Alternator             |
|                           |    |    |        /Generator is inspected and    |
|                           |    |    |        found not mechanically         |
|                           |    |    |        sound.                         |
|                           |    |    |                                       |
|       3) APU Generator  C | 2  | 0  | (M)One or both may be inoperative     |
|          Overheat         |    |    | provided the APU is rendered          |
|          Warning          |    |    | inoperative.                          |
|          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        | 52-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 52  DOORS                 |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 10-1  Large Cargo       C | 1  | 0  | (O)May be inoperative provided it     |
| ***   Door Operating      |    |    | is verified by visual inspection      |
|       System              |    |    | that the associated door is closed    |
|                           |    |    | and locked before each departure.     |
|                           |    |    |                                       |
| 70-1  Door Unlocked     C | 1  | 0  | (O)May be inoperative provided        |
|       Caution Light       |    |    | crew door lock pins and cargo door    |
|       System (All         |    |    | locking hooks are visually checked    |
|       except Fokker 27    |    |    | to be in place.                       |
|       Mks 100, 200 &      |    |    |                                       |
|       500F)               |    |    |                                       |
|                           |    |    |                                       |
| 71-1  Door Warning      C | -  | 0  | (O)May be inoperative provided it     |
| ***   Light Systems       |    |    | is verified by visual inspection      |
|                           |    |    | that the associated door(s) is        |
|                           |    |    | closed and locked before each         |
|                           |    |    | departure.                            |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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        | 61-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 61  PROPELLERS            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 40-1  Propeller         C | 2  | 0  |                                       |
| ***   Brake               |    |    |                                       |
|                           |    |    |                                       |
| 40-3  Cruise            C | 2  | 0  | Both may be inoperative provided:     |
| ***   (Flight Safety)     |    |    |     a) TAS does not exceed AFM        |
|       Lock Unlocked       |    |    |        Limitations, and               |
|       Indicator Light     |    |    |     b) HP cocks remain in the "Lock   |
|       System              |    |    |        Out" position during the       |
|                           |    |    |        entire flight.                 |
|                           |    |    |                                       |
| 40-4  Ground Fine       C | 1  | 0  | May be inoperative provided GFP is    |
|       Pitch Warning       |    |    | selected after touch down above 55    |
|       Horn System         |    |    | kt.                                   |
|                           |    |    |                                       |
| 40-5  Cruise Pitch      C | 1  | 0  | May be inoperative provided:          |
| ***   Test Light          |    |    |     a) TAS does not exceed AFM        |
|       System              |    |    |        Limitations, and               |
|       (Fairchild F-27)    |    |    |     b) HP cocks remain in the "Lock   |
|                           |    |    |        Out" position during the       |
|                           |    |    |        entire flight.                 |
|                           |    |    |                                       |
| 40-6  Cruise Lock       C | 1  | 0  | May be inoperative provided:          |
| ***   "Unsafe" Light      |    |    |     a) TAS does not exceed AFM        |
|       (Fokker 27)         |    |    |        Limitations, and               |
|                           |    |    |     b) HP cocks remain in the "Lock   |
|                           |    |    |        Out" position during the       |
|                           |    |    |        entire flight.                 |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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        | 73-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 73  ENGINE FUEL & CONTROL |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 13-1  Fuel Flow         C | 2  | 1  | One may be inoperative provided       |
|       Indication          |    |    | all RPM, TGT, and Fuel Quantity       |
|       Systems             |    |    | Indicating Systems are operative.     |
|                           |    |    |                                       |
|                           |    |    | NOTE: Fuel Consumed Indication may    |
|                           |    |    |       be affected.                    |
|                           |    |    |                                       |
| 13-2  Fuel Consumed     C | 2  | 0  | Both may be inoperative provided      |
| ***   Indication          |    |    | Fuel Quantity Indicating System is    |
|       Systems             |    |    | operative.                            |
|                           |    |    |                                       |
| 13-4  Fuel              D | 1  | 0  | (O)May be inoperative provided a      |
|       Datum/Trimmer       |    |    | procedure to verify takeoff and       |
|       Calculator          |    |    | landing fuel Datum/Trimmer settings   |
|                           |    |    | is established.                       |
|                           |    |    |                                       |
| 13-5  Fuel Pressure       |    |    | DELETED, see item 28-42-1, Fuel       |
|       Indicators          |    |    | Pressure Indicator 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        | 74-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 74  IGNITION              |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 00-1  Igniter Systems   C | 4  | 2  | Two may be inoperative provided       |
|                           |    |    | one is operative on each engine.      |
|                           |    |    |                                       |
| 00-2  Ignition          C | 2  | 0  | May be inoperative provided the       |
| ***   Light Systems       |    |    | starter master switch is switched     |
|                           |    |    | to SAFE when engine has reached       |
|                           |    |    | self sustaining speed.                |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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        | 76-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 76  ENGINE CONTROLS       |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 13-1  RPM Synchronizer  C | 1  | 0  | (M)May be inoperative provided        |
| ***   System              |    |    | System is verified in neutral         |
|                           |    |    | position.                             |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION                                           |
|                                                                             |
|                                            MASTER MINIMUM EQUIPMENT LIST    |
| FEDERAL AVIATION ADMINISTRATION                                             |
| --------------------------------------------------------------------------- |
| AIRCRAFT:                                | REVISION NO: 30 c     | PAGE:    |
|              FAIRCHILD F-27              |                       |          |
|           FH-227 & FOKKER F-27           | DATE: 04/25/94        | 77-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 77  ENGINE INDICATING     |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 11-1 Synchroscope       C | 1  | 0  |                                       |
| ***  System               |    |    |                                       |
|                           |    |    |                                       |
| 11-2 Engine RPM         B | 2  | 1  | One may be inoperative provided       |
| ***  Indicator Digital    |    |    | both analog indications are           |
|      Indication           |    |    | operative.                            |
|                           |    |    |                                       |
| 11-3 Engine Torque      B | 2  | 1  | One may be inoperative provided       |
| ***  Indicator Digital    |    |    | both analog indications are           |
|      Indication           |    |    | 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        | 79-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 79  ENGINE OIL            |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 32-1  Engine Oil        C | 2  | 1  | (O)One may be inoperative provided    |
| ***   Pressure Warning    |    |    | the associated oil pressure and oil   |
|       Light Systems       |    |    | temperature indicators are            |
|                           |    |    | operative.                            |
|                           |    |    |                                       |
| 32-2  Gearbox Oil       C | 2  | 0  | One or both may be inoperative        |
| ***   Pressure Light      |    |    | provided Gearbox Oil Pressure         |
|       Systems             |    |    | Gauges are installed and operative.   |
|                           |    |    |                                       |
| 32-3  Engine/           B | 2  | 1  | (O)One may be inoperative             |
| ***   Gearbox Low Oil     |    |    | provided:                             |
|       Pressure Warning    |    |    |     a) Associated Oil Pressure, Oil   |
|       Light Systems       |    |    |        Temperature and Gear Box       |
|                           |    |    |        Pressure Indicators are        |
|                           |    |    |        operative.                     |
|                           |    |    |           OR                          |
|                         B |    |    |     b) Gear Box Oil Pressure          |
|                           |    |    |        Indicators and both Low Oil    |
|                           |    |    |        Pressure Warning Lights are    |
|                           |    |    |        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        | 80-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 80  STARTING              |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 10-1  Starter Light     C | -  | 0  | (O)May be inoperative provided        |
| ***   (AMBER)             |    |    | Starter Master Switch is switched     |
|                           |    |    | to SAFE when engine has reached       |
|                           |    |    | self-sustaining speed.                |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


-------------------------------------------------------------------------------
| 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        | 82-1     |
| --------------------------------------------------------------------------- |
|                        1. | 2. NUMBER INSTALLED                             |
| SYSTEM &                  |    -------------------------------------------- |
| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            |
| NUMBERS                   |    |    --------------------------------------- |
| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |
| 82  WATER INJECTION       |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
| 20-1  Water Methanol    C | 2  | 0  | (O)One or both pumps may be           |
|       Systems             |    |    | inoperative provided performance      |
|                           |    |    | requirements are met with DRY         |
|                           |    |    | power.                                |
|                           |    |    |                                       |
| 40-1  Water             C | 2  | 0  | (O)One or both may be inoperative     |
| ***   Methanol            |    |    | provided:                             |
|       Quantity            |    |    |     a) Associated Fluid Quantity is   |
|       Indicator           |    |    |        verified before each WET       |
|       Systems             |    |    |        takeoff.                       |
|                           |    |    |           OR                          |
|                         C |    |    |     b) Performance requirements are   |
|                           |    |    |        met with DRY Power.            |
|                           |    |    |                                       |
| 40-2  Water Methanol    C | 2  | 1  | (O)One may be inoperative             |
|       Indicator Light     |    |    | provided:                             |
|       Systems             |    |    |     a) WET Power is indicated on      |
|                           |    |    |        both torque meters prior to    |
|                           |    |    |        takeoff.                       |
|                           |    |    |           OR                          |
|                         C |    |    |     b) Performance requirements are   |
|                           |    |    |        met with DRY Power.            |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
|                           |    |    |                                       |
-------------------------------------------------------------------------------


