DEPARTMENT OF TRANSPORTATION     Revision: 11 a

                                                           Date: 10/23/2000

                         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

 

 

 

 

 

                                   FOKKER 28

                             F-28 MK 1000/2000/4000

 

                                RICHARD G. HAMM

                          CHAIRMAN, FLIGHT OPERATIONS

                            EVALUATION BOARD (FOEB)

 

 

 

 

 

 

 

 

                         Federal Aviation Administration

                         Flight Standards Division

                         AIRCRAFT EVALUATION GROUP, LGB-AEG

                         3900 PARAMOUNT BLVD.

                         LAKEWOOD, CALIFORNIA 90712-4137

 

                         TELEPHONE:  (562) 627-5276

                               FAX:  (562) 627-5281


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 11 a

                        MASTER MINIMUM EQUIPMENT LIST      Date: 10/23/2000

 

                                 FOKKER 28

 

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I

         --     Log of Revisions                        II

         --     Control Page                            III, IV

         --     Highlights of Change                    V

         --     Definitions                             VI, VII, VIII, IX

         --     Definitions                             X, XI, XII, XIII

         --     Preamble                                XIV, XV

         21     Air Conditioning                        21-1, 2, 3

         22     Auto Flight                             22-1, 2

         23     Communications                          23-1, 2, 3, 4

         24     Electrical Power                        24-1, 2

         25     Equipment/Furnishings                   25-1, 2, 3, 4, 5

         25     Equipment/Furnishings                   25-6

         26     Fire Protection                         26-1, 2, 3, 4, 5

         26     Fire Protection                         26-6, 7, 8

         27     Flight Controls                         27-1, 2, 3

         28     Fuel                                    28-1, 2, 3, 4

         29     Hydraulic Power                         29-1, 2

         30     Ice and Rain Protection                 30-1, 2, 3, 4, 5

         31     Indicating/Recording Systems            31-1

         32     Landing Gear                            32-1, 2

         33     Lights                                  33-1, 2, 3, 4

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

         34     Navigation                              34-6

         35     Oxygen                                  35-1, 2

         36     Pneumatic                               36-1, 2

         49     Airborne Auxiliary Power                49-1, 2

         52     Doors                                   52-1

         73     Engine Fuel & Control                   73-1, 2

         74     Ignition                                74-1

         77     Engine Indicating                       77-1

         80     Starting                                80-1


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: II

                                                         Revision: 11 a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 10/23/2000

 

                                 FOKKER 28

 

 

 

                               Log of Revisions

 

      ----------------------------------------------------------------------

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

      ----------------------------------------------------------------------

      ¦ 7        ¦ 08/31/1990 ¦ ALL PAGES                      ¦           ¦

      ¦ 7a       ¦ 07/30/1992 ¦ HIGHLIGHTS OF REV.             ¦           ¦

      ¦ 7a       ¦ 07/30/1992 ¦ 23-1,23-2,23-3,23-4,24-1       ¦           ¦

      ¦ 7a       ¦ 07/30/1992 ¦ 24-2,25-1,25-2,25-3,25-4       ¦           ¦

      ¦ 7a       ¦ 07/30/1992 ¦ 25-5,30-4,31-1,34-1,34-2       ¦           ¦

      ¦ 7a       ¦ 07/30/1992 ¦ 34-3,34-4,34-5,35-1,35-2       ¦           ¦

      ¦ 7b       ¦ 11/28/1994 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 7b       ¦ 11/28/1994 ¦ 30-1,30-2,30-3,30-4            ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 21-1,21-2,21-3,22-1,23-1       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 23-2,23-3,23-4,24-1,24-2       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 25-1,25-2,25-3,25-4,25-5       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 25-6,26-1,26-2,26-3,27-1       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 27-2,27-3,28-1,28-2,28-3       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 28-4,29-1,29-2,31-1,32-1       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 32-2,33-1,33-2,33-3,34-1       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 35-1,35-2,36-1,36-2,49-1       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 49-2,52-1,73-1,73-2,74-1       ¦           ¦

      ¦ 8        ¦ 09/24/1996 ¦ 77-1,80-1                      ¦           ¦

      ¦ 9        ¦ 04/14/1997 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 9        ¦ 04/14/1997 ¦ 22-1,22-2,24-1,24-2,25-1       ¦           ¦

      ¦ 9        ¦ 04/14/1997 ¦ 25-2,25-3,25-4,25-5,25-6       ¦           ¦

      ¦ 9        ¦ 04/14/1997 ¦ 26-1,26-2,26-3,34-1,34-2       ¦           ¦

      ¦ 9        ¦ 04/14/1997 ¦ 34-3,34-4,34-5,34-6            ¦           ¦

      ¦ 10       ¦ 12/14/1998 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 10       ¦ 12/14/1998 ¦ 22-1,23-4,28-2,28-3,28-4       ¦           ¦

      ¦ 10       ¦ 12/14/1998 ¦ 30-4,30-5,31-1,34-6            ¦           ¦

      ¦ 10a      ¦ 08/16/1999 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 10a      ¦ 08/16/1999 ¦ 33-4                           ¦           ¦

      ¦ 11       ¦ 03/03/2000 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 11       ¦ 03/03/2000 ¦ 26-4,26-5,26-6,26-7,26-8       ¦           ¦

      ¦ 11a      ¦ 10/23/2000 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 11a      ¦ 10/23/2000 ¦ 28-1                           ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ----------------------------------------------------------------------


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: III

                                                           Revision: 11 a

                        MASTER MINIMUM EQUIPMENT LIST      Date: 10/23/2000

 

                                 FOKKER 28

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       11 a     10/23/2000

         Table of Contents                        I       11 a     10/23/2000

         Log of Revisions                         II      11 a     10/23/2000

         Control Page                             III     11 a     10/23/2000

                                                  IV      11 a     10/23/2000

         Highlights of Change                     V       11 a     10/23/2000

         Definitions                              VI      6        01/31/1995

                                                  VII     6        01/31/1995

                                                  VIII    6        01/31/1995

                                                  IX      6        01/31/1995

                                                  X       6        01/31/1995

                                                  XI      6        01/31/1995

                                                  XII     6        01/31/1995

                                                  XIII    6        01/31/1995

         Preamble                                 XIV     2        06/14/1989

                                                  XV      2        06/14/1989

         21                                       21-1    8        09/24/1996

                                                  21-2    8        09/24/1996

                                                  21-3    8        09/24/1996

         22                                       22-1    10       12/14/1998

                                                  22-2    9        04/14/1997

         23                                       23-1    8        09/24/1996

                                                  23-2    8        09/24/1996

                                                  23-3    8        09/24/1996

                                                  23-4    10       12/14/1998

         24                                       24-1    9        04/14/1997

                                                  24-2    9        04/14/1997

         25                                       25-1    9        04/14/1997

                                                  25-2    9        04/14/1997

                                                  25-3    9        04/14/1997

                                                  25-4    9        04/14/1997

                                                  25-5    9        04/14/1997

                                                  25-6    9        04/14/1997

         26                                       26-1    9        04/14/1997

                                                  26-2    9        04/14/1997

                                                  26-3    9        04/14/1997

                                                  26-4    11       03/03/2000

                                                  26-5    11       03/03/2000

                                                  26-6    11       03/03/2000

                                                  26-7    11       03/03/2000


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IV

                                                           Revision: 11 a

                        MASTER MINIMUM EQUIPMENT LIST      Date: 10/23/2000

 

                                 FOKKER 28

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  26-8    11       03/03/2000

         27                                       27-1    8        09/24/1996

                                                  27-2    8        09/24/1996

                                                  27-3    8        09/24/1996

         28                                       28-1    11 a     10/23/2000

                                                  28-2    10       12/14/1998

                                                  28-3    10       12/14/1998

                                                  28-4    10       12/14/1998

         29                                       29-1    8        09/24/1996

                                                  29-2    8        09/24/1996

         30                                       30-1    8        09/24/1996

                                                  30-2    8        09/24/1996

                                                  30-3    8        09/24/1996

                                                  30-4    10       12/14/1998

                                                  30-5    10       12/14/1998

         31                                       31-1    10       12/14/1998

         32                                       32-1    8        09/24/1996

                                                  32-2    8        09/24/1996

         33                                       33-1    8        09/24/1996

                                                  33-2    8        09/24/1996

                                                  33-3    8        09/24/1996

                                                  33-4    10 a     08/16/1999

         34                                       34-1    9        04/14/1997

                                                  34-2    9        04/14/1997

                                                  34-3    9        04/14/1997

                                                  34-4    9        04/14/1997

                                                  34-5    9        04/14/1997

                                                  34-6    10       12/14/1998

         35                                       35-1    8        09/24/1996

                                                  35-2    8        09/24/1996

         36                                       36-1    8        09/24/1996

                                                  36-2    8        09/24/1996

         49                                       49-1    8        09/24/1996

                                                  49-2    8        09/24/1996

         52                                       52-1    8        09/24/1996

         73                                       73-1    8        09/24/1996

                                                  73-2    8        09/24/1996

         74                                       74-1    8        09/24/1996

         77                                       77-1    8        09/24/1996

         80                                       80-1    8        09/24/1996


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: V

                                                         Revision: 11 a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 10/23/2000

 

                                 FOKKER 28

 

 

                            Highlights of Change

 

 

 

       EFFECTIVE ABOVE DATE, The Fokker 28 Master Minimum Equipment List has

       been revised.  This MMEL applies to the series Mk 1000, 2000, and 4000.

 

       Item 28-1  Clearifies type of fuel with one Boost Pump inoperative,

                  Kerosene Type Fuel (e.g. Jet A, Jet A-1, etc.).

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: VII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: VIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: IX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: X

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: XI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: XII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: XIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                 FOKKER 28

 

 

                                 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: XIV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                                 FOKKER 28

 

 

                                  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: XV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                                 FOKKER 28

 

 

                                  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: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 21-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Air Conditioning    C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦     Pack Systems          ¦    ¦    ¦     a) Affected Pack remains Off,     ¦

¦                           ¦    ¦    ¦     b) Ram Air Valve is operative,    ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     c) Aircraft is operated at or     ¦

¦                           ¦    ¦    ¦        below FL250.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 0  ¦ Both may be inoperative provided:     ¦

¦                           ¦    ¦    ¦      a) Ram Air Valve is operative,   ¦

¦                           ¦    ¦    ¦      b) Dump switch is OPEN, and      ¦

¦                           ¦    ¦    ¦      c) Aircraft is operated in an    ¦

¦                           ¦    ¦    ¦         unpressurized configuration   ¦

¦                           ¦    ¦    ¦         at or below 10,000 ft. MSL.   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Air Conditioning    C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative            ¦

¦     Main Valve            ¦    ¦    ¦ provided:                             ¦

¦     Indicators            ¦    ¦    ¦     a) All other components of the    ¦

¦                           ¦    ¦    ¦        associated system are          ¦

¦                           ¦    ¦    ¦        operative, and                 ¦

¦                           ¦    ¦    ¦     b) It is verified before each     ¦

¦                           ¦    ¦    ¦        takeoff that the associated    ¦

¦                           ¦    ¦    ¦        valve is operative.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Cabin and Flight      ¦    ¦    ¦                                       ¦

¦     Deck Temperature      ¦    ¦    ¦                                       ¦

¦     Control Systems       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Manual Control   C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦        System             ¦    ¦    ¦ associated Automatic Temperature      ¦

¦                           ¦    ¦    ¦ Control System is operative.          ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Automatic        C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦        Control System     ¦    ¦    ¦ associated Manual Temperature         ¦

¦                           ¦    ¦    ¦ Control System operative.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Air Conditioning    C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦     Bypass Valve          ¦    ¦    ¦ the associated Duct Temperature       ¦

¦     Indicators            ¦    ¦    ¦ Indicator is operative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 21-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Air Conditioning    C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦     Duct Temperature      ¦    ¦    ¦ associated Air Conditioning Bypass    ¦

¦     Indicators            ¦    ¦    ¦ Valve Indicator is operative.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Cabin Temperature   C ¦ 1  ¦ 0  ¦                                       ¦

¦     Indicator             ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Automatic Duct      C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦     Overheat              ¦    ¦    ¦ associated Automatic Temperature      ¦

¦     Protective Systems    ¦    ¦    ¦ Control and limit systems are         ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Automatic Shutoff   C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦     System                ¦    ¦    ¦     a) Both Air Conditioning Packs    ¦

¦                           ¦    ¦    ¦        are turned OFF for engine      ¦

¦                           ¦    ¦    ¦        start, takeoff and landing,    ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     b) Engine Anti-Ice is not used    ¦

¦                           ¦    ¦    ¦        for takeoff and landing.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Ram Air Valve       C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦                           ¦    ¦    ¦ valve is secured OPEN by an           ¦

¦                           ¦    ¦    ¦ accepted procedure.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Pressurization      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦     System                ¦    ¦    ¦     a) Dump Switch is OPEN, and       ¦

¦                           ¦    ¦    ¦     b) Aircraft is operated in an     ¦

¦                           ¦    ¦    ¦        unpressurized configuration    ¦

¦                           ¦    ¦    ¦        at or below 10,000 ft. MSL.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1)  Automatic       C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦         Pressurization    ¦    ¦    ¦     a) Manual Pressurization          ¦

¦         Control           ¦    ¦    ¦        Control System is operative,   ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     b) Autopilot is operative.        ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 21-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Dump Switch         C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦

¦                           ¦    ¦    ¦ other components of the               ¦

¦                           ¦    ¦    ¦ Pressurization System are             ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Cabin Rate-of-      C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦     Climb Indicator       ¦    ¦    ¦ Automatic Pressurization Control      ¦

¦                           ¦    ¦    ¦ System is operative.                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Cabin Altitude      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦     Indicator             ¦    ¦    ¦     a) Cabin Differential Pressure    ¦

¦                           ¦    ¦    ¦        Indicator is operative, and    ¦

¦                           ¦    ¦    ¦     b) A chart is provided to         ¦

¦                           ¦    ¦    ¦        convert Cabin Differential     ¦

¦                           ¦    ¦    ¦        Pressure to Cabin Altitude.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Cabin Differential  C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦     Pressure Indicator    ¦    ¦    ¦     a) Cabin Altitude Indicator is    ¦

¦                           ¦    ¦    ¦        operative, and                 ¦

¦                           ¦    ¦    ¦     b) A chart is provided to         ¦

¦                           ¦    ¦    ¦        convert Cabin altitude to      ¦

¦                           ¦    ¦    ¦        Cabin Differential Pressure.   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Cabin Altitude      C ¦ 2  ¦ 1  ¦                                       ¦

¦     Warning Lights        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦                           ¦    ¦    ¦ aircraft is operated at or below      ¦

¦                           ¦    ¦    ¦ 10,000 feet MSL.                      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 22-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Autopilot System    C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦                           ¦    ¦    ¦     a) Automatic Pressurization       ¦

¦                           ¦    ¦    ¦        System is operative, and       ¦

¦                           ¦    ¦    ¦     b) Approach minimums do not       ¦

¦                           ¦    ¦    ¦        depend on use of the           ¦

¦                           ¦    ¦    ¦        Autopilot.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1)  Control Wheel   C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦         Disengage         ¦    ¦    ¦     a) Pilot using Autopilot has an   ¦

¦         Switches          ¦    ¦    ¦        operative disengage switch,    ¦

¦                           ¦    ¦    ¦     b) Autopilot is not used below    ¦

¦                           ¦    ¦    ¦        1500 feet AGL, and             ¦

¦                           ¦    ¦    ¦     c) Approach minimums do not       ¦

¦                           ¦    ¦    ¦        depend on use of the           ¦

¦                           ¦    ¦    ¦        Autopilot.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Yaw Damper System   C ¦ 1  ¦ 0  ¦ May be inoperative provided AFM       ¦

¦                           ¦    ¦    ¦ Limitations are followed.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Autopilot           C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦     Progress              ¦    ¦    ¦     a) Approach minimums do not       ¦

¦     Annunciators          ¦    ¦    ¦        require its use, and           ¦

¦                           ¦    ¦    ¦     b) Alternate procedures are       ¦

¦                           ¦    ¦    ¦        established and used.          ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 22-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 23-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Communications      D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦     Systems               ¦    ¦    ¦ FAR, and not powered by an            ¦

¦     (VHF, HF, UHF)        ¦    ¦    ¦ Emergency or Essential Bus may be     ¦

¦                           ¦    ¦    ¦ inoperative.                          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Passenger Address     ¦    ¦    ¦                                       ¦

¦     System                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Passenger        B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦        Configuration      ¦    ¦    ¦     a) Alternate normal, and          ¦

¦                           ¦    ¦    ¦        emergency procedures, and/or   ¦

¦                           ¦    ¦    ¦        operating restrictions are     ¦

¦                           ¦    ¦    ¦        established and used, and      ¦

¦                           ¦    ¦    ¦     b) Flight Deck/Cabin Interphone   ¦

¦                           ¦    ¦    ¦        system is operative.           ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Cargo            D ¦ 1  ¦ 0  ¦                                       ¦

¦        Configuration      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Flight Deck         C ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦

¦     Speakers              ¦    ¦    ¦     a) Affected Speaker is not        ¦

¦                           ¦    ¦    ¦        required for aural warnings    ¦

¦                           ¦    ¦    ¦        or procedures, and             ¦

¦                           ¦    ¦    ¦     b) An operative headset is        ¦

¦                           ¦    ¦    ¦        provided for each person on    ¦

¦                           ¦    ¦    ¦        cockpit duty.                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Service Interphone  C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦     System                ¦    ¦    ¦     a) Alternate, Normal and          ¦

¦                           ¦    ¦    ¦        Emergency procedures are       ¦

¦                           ¦    ¦    ¦        established and used, and      ¦

¦                           ¦    ¦    ¦     b) Passenger Address System is    ¦

¦                           ¦    ¦    ¦        operative.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 23-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Static Dischargers    ¦    ¦    ¦ DELETED in Revision 7.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Flight Deck           ¦    ¦    ¦ DELETED in Revision 7.                ¦

¦     Interphone System     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Audio Selector        ¦    ¦    ¦ DELETED in Revision 8.                ¦

¦     Panels                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Cockpit Voice       A ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦     Recorder (CVR)        ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦

¦     System                ¦    ¦    ¦        operates normally, and         ¦

¦                           ¦    ¦    ¦     b) Repairs are made within        ¦

¦                           ¦    ¦    ¦        three flight days.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Passenger           C ¦ 1  ¦ 0  ¦                                       ¦

¦     Entertainment         ¦    ¦    ¦                                       ¦

¦     System                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. ARINC               C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦ *** Communications        ¦    ¦    ¦     a) Alternate procedures are       ¦

¦     Addressing and        ¦    ¦    ¦        established and used.          ¦

¦     Reporting System      ¦    ¦    ¦           OR                          ¦

¦     (ACARS)               ¦    ¦    ¦     b) Procedures do not require      ¦

¦                           ¦    ¦    ¦        its use.                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 23-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Crewmember            ¦    ¦    ¦                                       ¦

¦     Alerting System       ¦    ¦    ¦                                       ¦

¦     (Crew Call            ¦    ¦    ¦                                       ¦

¦     Light/Chime)          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Flight Crew      C ¦ 1  ¦ 0  ¦                                       ¦

¦        Call Light         ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Flight           C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦        Attendant Call     ¦    ¦    ¦     a) Passenger Address System is    ¦

¦        Light System       ¦    ¦    ¦        operative,                     ¦

¦                           ¦    ¦    ¦     b) Flight Attendant Call Chime    ¦

¦                           ¦    ¦    ¦        is operative, and              ¦

¦                           ¦    ¦    ¦     c) Affected Light is not          ¦

¦                           ¦    ¦    ¦        required for Lavatory Smoke    ¦

¦                           ¦    ¦    ¦        Detector Alerting.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦     3) Flight           C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦        Attendant Call     ¦    ¦    ¦     a) Passenger Address System is    ¦

¦        Chime System       ¦    ¦    ¦        operative,                     ¦

¦                           ¦    ¦    ¦     b) Flight Attendant Call Light    ¦

¦                           ¦    ¦    ¦        is operative,                  ¦

¦                           ¦    ¦    ¦     c) Affected Chime is not          ¦

¦                           ¦    ¦    ¦        required for lavatory Smoke    ¦

¦                           ¦    ¦    ¦        Detector Alerting, and         ¦

¦                           ¦    ¦    ¦     d) Alternate Normal and           ¦

¦                           ¦    ¦    ¦        Emergency operations           ¦

¦                           ¦    ¦    ¦        procedures are established     ¦

¦                           ¦    ¦    ¦        and used.                      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Selective Call      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦

¦ *** System (SELCAL)       ¦    ¦    ¦ alternate normal procedures are       ¦

¦                           ¦    ¦    ¦ established and used.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Flite Phone         C ¦ -  ¦ 0  ¦                                       ¦

¦ *** Systems               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 23-4     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Air Phone Systems   C ¦ -  ¦ 0  ¦                                       ¦

¦ ***                       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Cockpit Headsets/   D ¦ -  ¦ -  ¦ Any in excess of those required       ¦

¦     Microphones           ¦    ¦    ¦ for flight deck crewmembers           ¦

¦                           ¦    ¦    ¦ (including official observer in       ¦

¦                           ¦    ¦    ¦ observer's seat) may be               ¦

¦                           ¦    ¦    ¦ inoperative.                          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 16. Boom Microphones      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Input To Cockpit A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦

¦        Voice Recorder     ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦

¦        Required By FAR    ¦    ¦    ¦        operates normally, and         ¦

¦                           ¦    ¦    ¦     b) Operations are limited to      ¦

¦                           ¦    ¦    ¦        not more than three flight     ¦

¦                           ¦    ¦    ¦        days before repair is made.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ *** 2) Input To Cockpit D ¦ -  ¦ 0  ¦                                       ¦

¦        Voice Recorder     ¦    ¦    ¦                                       ¦

¦        Not Required By    ¦    ¦    ¦                                       ¦

¦        FAR                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 17. Boom Microphone     C ¦ 4  ¦ 2  ¦ May be inoperative provided one       ¦

¦     Push to Talk          ¦    ¦    ¦ switch at each required flight        ¦

¦     Switches (Control     ¦    ¦    ¦ crew member station operates          ¦

¦     Yoke and Center       ¦    ¦    ¦ normally.                             ¦

¦     Console)              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 24-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Engine Driven       B ¦ 2  ¦ 1  ¦ (M)One may be inoperative             ¦

¦     Generator Systems     ¦    ¦    ¦ provided:                             ¦

¦     (Including CSD)       ¦    ¦    ¦     a) Associated CSD is dis-         ¦

¦                           ¦    ¦    ¦        connected and verified fully   ¦

¦                           ¦    ¦    ¦        serviced by an acceptable      ¦

¦                           ¦    ¦    ¦        procedure, and                 ¦

¦                           ¦    ¦    ¦     b) APU Generator is operative     ¦

¦                           ¦    ¦    ¦        and supplies power to the      ¦

¦                           ¦    ¦    ¦        associated bus.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  CSD Oil             C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦     Temperature           ¦    ¦    ¦ the associated CSD Central Warning    ¦

¦     Indicating Systems    ¦    ¦    ¦ System, Frequency Meter and AC        ¦

¦                           ¦    ¦    ¦ Voltmeter are operative.              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  CSD Central         C ¦ 2  ¦ 0  ¦ May be inoperative provided the       ¦

¦     Warning Systems       ¦    ¦    ¦ associated CSD Oil Temperature        ¦

¦                           ¦    ¦    ¦ Indicating System, Frequency Meter,   ¦

¦                           ¦    ¦    ¦ and AC Voltmeter are operative, and   ¦

¦                           ¦    ¦    ¦ are monitored during flight.          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  DC Voltmeter          ¦    ¦    ¦ DELETED in Revision 7.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  AC Voltmeter        C ¦ 1  ¦ 0  ¦ May be inoperative provided AC bus    ¦

¦                           ¦    ¦    ¦ indicator lights are operative.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  AC Frequency Meter  C ¦ 1  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  BUS Indicator         ¦    ¦    ¦                                       ¦

¦     Lights                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) AC Busses        C ¦ 3  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) DC Busses        C ¦ 3  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 24-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Bus Tie Contactor   B ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦                           ¦    ¦    ¦     a) Contactor is verified OPEN,    ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     b) APU Generator is operated as   ¦

¦                           ¦    ¦    ¦        a standby power source         ¦

¦                           ¦    ¦    ¦        throughout the flight.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Main Ships            ¦    ¦    ¦ DELETED in Revision 8.                ¦

¦     Batteries             ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Essential           B ¦ 1  ¦ 0  ¦                                       ¦

¦ *** Transformer           ¦    ¦    ¦                                       ¦

¦     Rectifier Unit        ¦    ¦    ¦                                       ¦

¦     (TRU)                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. External Power      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦     System                ¦    ¦    ¦     a) Fault is verified to be        ¦

¦                           ¦    ¦    ¦        isolated by an accepted        ¦

¦                           ¦    ¦    ¦        procedure,                     ¦

¦                           ¦    ¦    ¦     b) It is verified that            ¦

¦                           ¦    ¦    ¦        electrical power from the      ¦

¦                           ¦    ¦    ¦        APU or another source can be   ¦

¦                           ¦    ¦    ¦        safely applied, and            ¦

¦                           ¦    ¦    ¦     c) No associated warnings or      ¦

¦                           ¦    ¦    ¦        faults appear on overhead or   ¦

¦                           ¦    ¦    ¦        annunciator panels.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 25-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Crewmember            ¦    ¦    ¦ DELETED in revision 7.                ¦

¦     Shoulder Harnesses    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Flotation           D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦     Equipment (Crew       ¦    ¦    ¦ FAR may be inoperative or missing     ¦

¦     and Passenger)        ¦    ¦    ¦ provided required distribution is     ¦

¦                           ¦    ¦    ¦ maintained.                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Megaphones          D ¦ -  ¦ 1  ¦ Any in excess of those required       ¦

¦                           ¦    ¦    ¦ by FAR may be inoperative or          ¦

¦                           ¦    ¦    ¦ missing provided:                     ¦

¦                           ¦    ¦    ¦     a) The inoperative Megaphone is   ¦

¦                           ¦    ¦    ¦        removed from the passenger     ¦

¦                           ¦    ¦    ¦        cabin, and                     ¦

¦                           ¦    ¦    ¦     b) Required distribution is       ¦

¦                           ¦    ¦    ¦        maintained.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE: Not required for all-cargo      ¦

¦                           ¦    ¦    ¦       operations.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Emergency Locator   C ¦ -  ¦ -  ¦ As required by FAR.                   ¦

¦     Transmitter (ELT)     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 25-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Forward Observer    A ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦     Seat (Including       ¦    ¦    ¦     a) A passenger seat in the        ¦

¦     Associated            ¦    ¦    ¦        passenger cabin is made        ¦

¦     Equipment)            ¦    ¦    ¦        available to an FAA            ¦

¦                           ¦    ¦    ¦        inspector for the              ¦

¦                           ¦    ¦    ¦        performance of official        ¦

¦                           ¦    ¦    ¦        duties, and                    ¦

¦                           ¦    ¦    ¦     b) Repairs are made within two    ¦

¦                           ¦    ¦    ¦        flight days.                   ¦

¦                           ¦    ¦    ¦           OR                          ¦

¦                         A ¦    ¦    ¦     c) Forward Observer's Seat is     ¦

¦                           ¦    ¦    ¦        available with the required    ¦

¦                           ¦    ¦    ¦        minimum safety equipment       ¦

¦                           ¦    ¦    ¦        (safety belt and oxygen) and   ¦

¦                           ¦    ¦    ¦        acceptable to the FAA for      ¦

¦                           ¦    ¦    ¦        the performance of official    ¦

¦                           ¦    ¦    ¦        duties, and                    ¦

¦                           ¦    ¦    ¦     d) Repairs are made within two    ¦

¦                           ¦    ¦    ¦        flight days.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 1: These provisos are intended   ¦

¦                           ¦    ¦    ¦         to provide for occupancy      ¦

¦                           ¦    ¦    ¦         of the above seat by an       ¦

¦                           ¦    ¦    ¦         FAA inspector when the        ¦

¦                           ¦    ¦    ¦         minimum safety equipment      ¦

¦                           ¦    ¦    ¦         (oxygen and safety belt) is   ¦

¦                           ¦    ¦    ¦         functional and the            ¦

¦                           ¦    ¦    ¦         inspector determines the      ¦

¦                           ¦    ¦    ¦         conditions to be              ¦

¦                           ¦    ¦    ¦         acceptable.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 2: The pilot-in-command will     ¦

¦                           ¦    ¦    ¦         determine if the minimum      ¦

¦                           ¦    ¦    ¦         safety equipment is           ¦

¦                           ¦    ¦    ¦         functional for other          ¦

¦                           ¦    ¦    ¦         persons authorized to         ¦

¦                           ¦    ¦    ¦         occupy any observer seat.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 25-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Flight Attendant      ¦    ¦    ¦                                       ¦

¦     Seats (Single or      ¦    ¦    ¦                                       ¦

¦     Dual Position)        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Seats Required   B ¦ -  ¦ -  ¦ (M)(O)One single or dual position     ¦

¦        by FAR             ¦    ¦    ¦ seat may be inoperative provided:     ¦

¦                           ¦    ¦    ¦     a) Affected seat position(s) is   ¦

¦                           ¦    ¦    ¦        not occupied,                  ¦

¦                           ¦    ¦    ¦     b) Flight Attendant 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,        ¦

¦                           ¦    ¦    ¦        except for the AFT seat, 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:  Except for the AFT seat, 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.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 25-4     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Flight Attendant      ¦    ¦    ¦                                       ¦

¦     Seats (Single or      ¦    ¦    ¦                                       ¦

¦     Dual Position)        ¦    ¦    ¦                                       ¦

¦     (Continued)           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Seats in Excess  C ¦ -  ¦ 0  ¦ (M)All may be inoperative             ¦

¦        Of Number          ¦    ¦    ¦ provided:                             ¦

¦        Required By        ¦    ¦    ¦     a) Affected seat position(s) is   ¦

¦        FAR.               ¦    ¦    ¦        not occupied, and              ¦

¦                           ¦    ¦    ¦     b) Folding type seat that will    ¦

¦                           ¦    ¦    ¦        not stow automatically,        ¦

¦                           ¦    ¦    ¦        except for the AFT seat, is    ¦

¦                           ¦    ¦    ¦        stowed or secured in the       ¦

¦                           ¦    ¦    ¦        RETRACTED position.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 1:  Except for the AFT Seat, a   ¦

¦                           ¦    ¦    ¦          folding type seat that       ¦

¦                           ¦    ¦    ¦          will not stow                ¦

¦                           ¦    ¦    ¦          automatically is             ¦

¦                           ¦    ¦    ¦          considered inoperative.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 2:  Individual operator MELs     ¦

¦                           ¦    ¦    ¦          will be specific as to the   ¦

¦                           ¦    ¦    ¦          numbers and locations of     ¦

¦                           ¦    ¦    ¦          inoperative seats and        ¦

¦                           ¦    ¦    ¦          combinations of seats to     ¦

¦                           ¦    ¦    ¦          ensure the proximity to      ¦

¦                           ¦    ¦    ¦          exits and distribution       ¦

¦                           ¦    ¦    ¦          requirements of the          ¦

¦                           ¦    ¦    ¦          applicable FAR are met.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 3:  A Flight Attendant Seat      ¦

¦                           ¦    ¦    ¦          Position with an             ¦

¦                           ¦    ¦    ¦          inoperative lap belt is      ¦

¦                           ¦    ¦    ¦          considered inoperative.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 25-5     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Passenger Seats     D ¦ -  ¦ -  ¦ (M)May be inoperative secured in      ¦

¦     (Including Seat       ¦    ¦    ¦ the up-right position.                ¦

¦     Backs)                ¦    ¦    ¦                                       ¦

¦                         D ¦ -  ¦ -  ¦ (M)May be inoperative in other than   ¦

¦                           ¦    ¦    ¦ the up-right position provided:       ¦

¦                           ¦    ¦    ¦     a) Does not block an Emergency    ¦

¦                           ¦    ¦    ¦        Exit,                          ¦

¦                           ¦    ¦    ¦     b) Does not restrict any pas-     ¦

¦                           ¦    ¦    ¦        senger from access to the      ¦

¦                           ¦    ¦    ¦        main aircraft aisle, and       ¦

¦                           ¦    ¦    ¦     c) The affected seat(s) is        ¦

¦                           ¦    ¦    ¦        blocked and placarded          ¦

¦                           ¦    ¦    ¦        "DO NOT OCCUPY".               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 1: A seat with an inoperative    ¦

¦                           ¦    ¦    ¦         seat belt is considered       ¦

¦                           ¦    ¦    ¦         inoperative.                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 2: Inoperative seat(s) do not    ¦

¦                           ¦    ¦    ¦         affect the required number    ¦

¦                           ¦    ¦    ¦         of Flight Attendants.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  "Fasten Seat Belt   C ¦ -  ¦ -  ¦ One or more signs or placards may     ¦

¦     While Seated"         ¦    ¦    ¦ be illegible or missing provided a    ¦

¦     Signs or Placards     ¦    ¦    ¦ legible sign or placard is readable   ¦

¦                           ¦    ¦    ¦ from each occupied passenger seat.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Cabin Emergency     C ¦ -  ¦ 0  ¦ May be inoperative or missing         ¦

¦     Flashlight/Holder     ¦    ¦    ¦ provided cabin crewmember assigned    ¦

¦     (Flight Attendant     ¦    ¦    ¦ to affected position has an           ¦

¦     Station)              ¦    ¦    ¦ operative flashlight readily          ¦

¦                           ¦    ¦    ¦ available.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 25-6     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Passenger             ¦ -  ¦ 0  ¦ Passenger convenience items, as       ¦

¦     Convenience Items     ¦    ¦    ¦ expressed in this MMEL, are those     ¦

¦                           ¦    ¦    ¦ related to passenger convenience,     ¦

¦                           ¦    ¦    ¦ comfort or entertainment such as,     ¦

¦                           ¦    ¦    ¦ but not limited to, galley            ¦

¦                           ¦    ¦    ¦ equipment, movie equipment, ash       ¦

¦                           ¦    ¦    ¦ trays, stereo equipment, overhead     ¦

¦                           ¦    ¦    ¦ reading lamps, etc.  Items            ¦

¦                           ¦    ¦    ¦ addressed elsewhere in this           ¦

¦                           ¦    ¦    ¦ document shall not be included.       ¦

¦                           ¦    ¦    ¦ (M) and (O) procedures may be         ¦

¦                           ¦    ¦    ¦ required and included in the air      ¦

¦                           ¦    ¦    ¦ carrier's appropriate document.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE: Lavatory Door Ash Trays are     ¦

¦                           ¦    ¦    ¦       not to be included.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Underseat Baggage   C ¦ -  ¦ -  ¦ (M)(O)May be inoperative provided:    ¦

¦     Restraining Bars      ¦    ¦    ¦     a) Baggage is not stowed under    ¦

¦                           ¦    ¦    ¦        seat with inoperative          ¦

¦                           ¦    ¦    ¦        restraining bar,               ¦

¦                           ¦    ¦    ¦     b) Associated Seat is placarded   ¦

¦                           ¦    ¦    ¦        "DO NOT STOW BAGGAGE UNDER     ¦

¦                           ¦    ¦    ¦         THIS SEAT", and               ¦

¦                           ¦    ¦    ¦     c) Procedures are established     ¦

¦                           ¦    ¦    ¦        to alert Cabin Crew of         ¦

¦                           ¦    ¦    ¦        inoperative restraining bar.   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. First Aid Kits      D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦                           ¦    ¦    ¦ FAR may be incomplete or missing      ¦

¦                           ¦    ¦    ¦ provided required distribution is     ¦

¦                           ¦    ¦    ¦ maintained.                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 26-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Engine/APU Fire     C ¦ 5  ¦ 0  ¦ May be missing provided               ¦

¦     Extinguisher          ¦    ¦    ¦ associated gauge reading is           ¦

¦     Discharger            ¦    ¦    ¦ verified to be adequate before        ¦

¦     Indicator Disks       ¦    ¦    ¦ the first flight of the day.          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  APU Fire            C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦     Extinguishing         ¦    ¦    ¦     a) APU is continuously            ¦

¦     System                ¦    ¦    ¦        monitored by ground crew       ¦

¦                           ¦    ¦    ¦        during operation,              ¦

¦                           ¦    ¦    ¦     b) Adequate ground Fire           ¦

¦                           ¦    ¦    ¦        Extinguishing Systems are      ¦

¦                           ¦    ¦    ¦        available,                     ¦

¦                           ¦    ¦    ¦     c) No passenger are permitted     ¦

¦                           ¦    ¦    ¦        in the aircraft during APU     ¦

¦                           ¦    ¦    ¦        operation, and                 ¦

¦                           ¦    ¦    ¦     d) APU is shut down before        ¦

¦                           ¦    ¦    ¦        taxi.                          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  APU Fire Warning    C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦     External Horn         ¦    ¦    ¦     a) APU fire Detection System is   ¦

¦                           ¦    ¦    ¦        operative, and                 ¦

¦                           ¦    ¦    ¦     b) APU Flight Deck Control        ¦

¦                           ¦    ¦    ¦        Panel is closely monitored     ¦

¦                           ¦    ¦    ¦        during all ground              ¦

¦                           ¦    ¦    ¦        operations.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Engine Fire           ¦    ¦    ¦ DELETED in Revision 7.                ¦

¦     Warning Lights        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Fire Bell           B ¦ 1  ¦ 0  ¦ May be inoperative provided an        ¦

¦                           ¦    ¦    ¦ engine and APU Fire Test is           ¦

¦                           ¦    ¦    ¦ performed before each flight to       ¦

¦                           ¦    ¦    ¦ verify that all Fire Warning Lights   ¦

¦                           ¦    ¦    ¦ are operative.                        ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Integral (HPC)      B ¦ 2  ¦ 0  ¦                                       ¦

¦     Fuel Lever Lights     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 26-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Hand Fire           D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦     Extinguishers         ¦    ¦    ¦ FAR may be inoperative or missing     ¦

¦                           ¦    ¦    ¦ provided:                             ¦

¦                           ¦    ¦    ¦     a) The inoperative fire           ¦

¦                           ¦    ¦    ¦        extinguisher is tagged         ¦

¦                           ¦    ¦    ¦        inoperative, removed from      ¦

¦                           ¦    ¦    ¦        the installed location, and    ¦

¦                           ¦    ¦    ¦        placed out of sight so it      ¦

¦                           ¦    ¦    ¦        cannot be mistaken for a       ¦

¦                           ¦    ¦    ¦        functional unit, and           ¦

¦                           ¦    ¦    ¦     b) Required distribution is       ¦

¦                           ¦    ¦    ¦        maintained.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Lavatory Smoke      C ¦ -  ¦ -  ¦ (M)(O)For each Lavatory, the          ¦

¦     Detection Systems     ¦    ¦    ¦ Lavatory Smoke Detection System may   ¦

¦                           ¦    ¦    ¦ be inoperative provided:              ¦

¦                           ¦    ¦    ¦     a) Lavatory Fire Extinguisher     ¦

¦                           ¦    ¦    ¦        System is operative.           ¦

¦                           ¦    ¦    ¦           OR                          ¦

¦                         C ¦    ¦    ¦     b) Lavatory waste receptacle is   ¦

¦                           ¦    ¦    ¦        empty,                         ¦

¦                           ¦    ¦    ¦     c) Lavatory door is locked        ¦

¦                           ¦    ¦    ¦        CLOSED and placarded,          ¦

¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT          ¦

¦                           ¦    ¦    ¦        ENTER", and                    ¦

¦                           ¦    ¦    ¦     d) Lavatory is not used for any   ¦

¦                           ¦    ¦    ¦        purpose.                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 1: These Provisos are not        ¦

¦                           ¦    ¦    ¦         intended to prohibit          ¦

¦                           ¦    ¦    ¦         lavatory inspections by       ¦

¦                           ¦    ¦    ¦         crewmembers.                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 2: A Lavatory Smoke Detection    ¦

¦                           ¦    ¦    ¦         System is not required for    ¦

¦                           ¦    ¦    ¦         all-cargo operations.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 04/14/1997      ¦ 26-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Lavatory Fire       C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the          ¦

¦     Extinguisher          ¦    ¦    ¦ Lavatory Fire Detection System may    ¦

¦     Systems               ¦    ¦    ¦ be inoperative provided:              ¦

¦                           ¦    ¦    ¦     a) Lavatory Smoke Detection       ¦

¦                           ¦    ¦    ¦        System is operative.           ¦

¦                           ¦    ¦    ¦           OR                          ¦

¦                         C ¦    ¦    ¦     b) Lavatory waste receptacle is   ¦

¦                           ¦    ¦    ¦        empty,                         ¦

¦                           ¦    ¦    ¦     c) Lavatory door is locked        ¦

¦                           ¦    ¦    ¦        CLOSED and placarded,          ¦

¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT          ¦

¦                           ¦    ¦    ¦        ENTER", and                    ¦

¦                           ¦    ¦    ¦     d) Lavatory is not used for any   ¦

¦                           ¦    ¦    ¦        purpose.                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 1: These Provisos are not        ¦

¦                           ¦    ¦    ¦         intended to prohibit          ¦

¦                           ¦    ¦    ¦         lavatory inspections by       ¦

¦                           ¦    ¦    ¦         crewmembers.                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 2: A Lavatory Fire               ¦

¦                           ¦    ¦    ¦         Extinguisher System is not    ¦

¦                           ¦    ¦    ¦         required for all-cargo        ¦

¦                           ¦    ¦    ¦         operations.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 11       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 03/03/2000      ¦ 26-4     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Cargo Bay Fire        ¦    ¦    ¦                                       ¦

¦     Protection System     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Forward          C ¦ 2  ¦ 0  ¦ (M) (O) Both may be inoperative       ¦

¦        Compartment Smoke  ¦    ¦    ¦   provided:                           ¦

¦        Detection Channels ¦    ¦    ¦      a) Before each flight, the       ¦

¦                           ¦    ¦    ¦         crew is to ensure that no     ¦

¦                           ¦    ¦    ¦         cargo is carried in the       ¦

¦                           ¦    ¦    ¦         forward cargo compartment.    ¦

¦                           ¦    ¦    ¦      b) Place a placard next to the   ¦

¦                           ¦    ¦    ¦         Cargo Bay Fire Protection     ¦

¦                           ¦    ¦    ¦         panel.  The placard will      ¦

¦                           ¦    ¦    ¦         read: "BOTH FWD CARGO BAY     ¦

¦                           ¦    ¦    ¦         FIRE PROTECTION SYSTEM        ¦

¦                           ¦    ¦    ¦         SMOKE DETECTION CHANNELS      ¦

¦                           ¦    ¦    ¦         INOP."                        ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 1  ¦ (M)(0) One channel may be             ¦

¦                           ¦    ¦    ¦   inoperative provided:               ¦

¦                           ¦    ¦    ¦     a) The operative channel is       ¦

¦                           ¦    ¦    ¦        verified to operate            ¦

¦                           ¦    ¦    ¦        normally.                      ¦

¦                           ¦    ¦    ¦     b) The operative channel is       ¦

¦                           ¦    ¦    ¦        selected.                      ¦

¦                           ¦    ¦    ¦     c) Place  a placard next to the   ¦

¦                           ¦    ¦    ¦        Cargo Bay Fire Protection      ¦

¦                           ¦    ¦    ¦        panel.  The placard will       ¦

¦                           ¦    ¦    ¦        read: "(specify which) FWD     ¦

¦                           ¦    ¦    ¦        CARGO BAY FIRE PROTECTION      ¦

¦                           ¦    ¦    ¦        SYSTEM SMOKE DETECTION         ¦

¦                           ¦    ¦    ¦        CHANNEL INOP."                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 11       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 03/03/2000      ¦ 26-5     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10.  Cargo Bay Fire       ¦    ¦    ¦                                       ¦

¦      Protection System    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) Aft Compartment C ¦ 2  ¦ 0  ¦ (M)(O) Both may be inoperative        ¦

¦         Smoke Detection   ¦    ¦    ¦   provided:                           ¦

¦         Channels          ¦    ¦    ¦      a) Before each flight, the       ¦

¦                           ¦    ¦    ¦         flight crew is to ensure      ¦

¦                           ¦    ¦    ¦         that no cargo is carried in   ¦

¦                           ¦    ¦    ¦         aft cargo compartment.        ¦

¦                           ¦    ¦    ¦      b) Place a placard next to the   ¦

¦                           ¦    ¦    ¦         Cargo Bay Fire Protection     ¦

¦                           ¦    ¦    ¦         panel.  The placard will      ¦

¦                           ¦    ¦    ¦         read: "BOTH CARGO BAY FIRE    ¦

¦                           ¦    ¦    ¦         PROTECTION SYSTEM SMOKE       ¦

¦                           ¦    ¦    ¦         DETECTION CHANNELS INOP."     ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 1  ¦ (M)(O) One channel may be             ¦

¦                           ¦    ¦    ¦    inoperative provided:              ¦

¦                           ¦    ¦    ¦         a) The operative channel is   ¦

¦                           ¦    ¦    ¦            verified to operate        ¦

¦                           ¦    ¦    ¦            normally.                  ¦

¦                           ¦    ¦    ¦         b) The operative channel is   ¦

¦                           ¦    ¦    ¦            selected.                  ¦

¦                           ¦    ¦    ¦         c) Place a placard next to    ¦

¦                           ¦    ¦    ¦            the Cargo Bay Fire         ¦

¦                           ¦    ¦    ¦            Protection panel.  The     ¦

¦                           ¦    ¦    ¦            placard will read:         ¦

¦                           ¦    ¦    ¦            "(specify which) AFT       ¦

¦                           ¦    ¦    ¦            CARGO BAY FIRE             ¦

¦                           ¦    ¦    ¦            PROTECTION SYSTEM SMOKE    ¦

¦                           ¦    ¦    ¦            DETECTION CHANNEL INOP."   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 11       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 03/03/2000      ¦ 26-6     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10.  Cargo Bay Fire       ¦    ¦    ¦                                       ¦

¦        Protection System  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦      3) Forward         C ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦

¦         Compartment       ¦    ¦    ¦     a) Before each flight, the        ¦

¦         Cargo Electronics ¦    ¦    ¦        flight crew is to ensure       ¦

¦         Units             ¦    ¦    ¦        that no cargo is carried in    ¦

¦                           ¦    ¦    ¦        the forward cargo              ¦

¦                           ¦    ¦    ¦        compartment.                   ¦

¦                           ¦    ¦    ¦     b) Place a placard next to the    ¦

¦                           ¦    ¦    ¦        Cargo Bay Fire Protection      ¦

¦                           ¦    ¦    ¦        panel.  The placard will       ¦

¦                           ¦    ¦    ¦        read: "BOTH FWD CARGO BAY      ¦

¦                           ¦    ¦    ¦        FIRE PROTECTION SYSTEM SMOKE   ¦

¦                           ¦    ¦    ¦        DETECTION CHANNELS INOP."      ¦

¦                           ¦    ¦    ¦                                       ¦

¦      4) AFT Compartment C ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦

¦         Cargo Electronics ¦    ¦    ¦     a) Before each flight, the        ¦

¦         Unit              ¦    ¦    ¦        flight crew is to ensure       ¦

¦                           ¦    ¦    ¦        that no cargo is carried in    ¦

¦                           ¦    ¦    ¦        the aft cargo compartment.     ¦

¦                           ¦    ¦    ¦     b) Place a placard next to the    ¦

¦                           ¦    ¦    ¦        cargo Bay Fire Protection      ¦

¦                           ¦    ¦    ¦        Panel. The placard will        ¦

¦                           ¦    ¦    ¦        read: "BOTH AFT CARGO BAY      ¦

¦                           ¦    ¦    ¦        FIRE PROTECTION SYSTEM SMOKE   ¦

¦                           ¦    ¦    ¦        DETECTION CHANNELS INOP."      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 11       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 03/03/2000      ¦ 26-7     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Cargo Bay Fire        ¦    ¦    ¦                                       ¦

¦     Protection System     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     5) Fire Bottle(s)   C ¦ 2  ¦ 1  ¦ (M)(O) One Bottle may be              ¦

¦        Pressure Loss      ¦    ¦    ¦        inoperative provided:          ¦

¦                           ¦    ¦    ¦      a) Before each flight, the       ¦

¦                           ¦    ¦    ¦         flight crew is to ensure      ¦

¦                           ¦    ¦    ¦         that no cargo is loaded in    ¦

¦                           ¦    ¦    ¦         either forward or aft         ¦

¦                           ¦    ¦    ¦         compartment.                  ¦

¦                           ¦    ¦    ¦      b) Place a placard next to the   ¦

¦                           ¦    ¦    ¦         Cargo Bay Fire Protection     ¦

¦                           ¦    ¦    ¦         panel. The placard will       ¦

¦                           ¦    ¦    ¦         read: "CARGO BAY FIRE         ¦

¦                           ¦    ¦    ¦         PROTECTION SYSTEM FIRE        ¦

¦                           ¦    ¦    ¦         BOTTLE INOP."                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦     6) Fire Bottle      C ¦ 2  ¦ 0  ¦ (M)(O) One cartridge may be           ¦

¦        Forward            ¦    ¦    ¦        inoperative provided:          ¦

¦        Cartridge(s)       ¦    ¦    ¦     a) Before each flight, the        ¦

¦                           ¦    ¦    ¦        flight crew is to ensure       ¦

¦                           ¦    ¦    ¦        that no cargo is carried in    ¦

¦                           ¦    ¦    ¦        the forward cargo              ¦

¦                           ¦    ¦    ¦        compartment.                   ¦

¦                           ¦    ¦    ¦     b) Place a placard next to the    ¦

¦                           ¦    ¦    ¦        Cargo Bay Fire Protection      ¦

¦                           ¦    ¦    ¦        panel. The placard will        ¦

¦                           ¦    ¦    ¦        read: "FWD CARGO BAY FIRE      ¦

¦                           ¦    ¦    ¦        BOTTLE CARTRIDGE(S) INOP."     ¦

¦                           ¦    ¦    ¦                                       ¦

¦     7) Fire Bottle AFT  C ¦ 2  ¦ 0  ¦ (M)(O) One cartridge may be           ¦

¦        Cartridge(s)       ¦    ¦    ¦        inoperative provided:          ¦

¦                           ¦    ¦    ¦     a) Before each flight, the        ¦

¦                           ¦    ¦    ¦        flight crew is to ensure       ¦

¦                           ¦    ¦    ¦        that no cargo is carried in    ¦

¦                           ¦    ¦    ¦        the aft cargo compartment.     ¦

¦                           ¦    ¦    ¦     b) Place a placard next to the    ¦

¦                           ¦    ¦    ¦        Cargo Bay Fire Protection      ¦

¦                           ¦    ¦    ¦        panel.The placard will read:   ¦

¦                           ¦    ¦    ¦        "AFT CARGO BAY FIRE BOTTLE     ¦

¦                           ¦    ¦    ¦        CARTRI000(S) INOP."            ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 11       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 03/03/2000      ¦ 26-8     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10.  Cargo Bay Fire       ¦    ¦    ¦                                       ¦

¦      Protection           ¦    ¦    ¦                                       ¦

¦      System               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦      8) Control Panel   C ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦

¦                           ¦    ¦    ¦      a) Before each flight, the       ¦

¦                           ¦    ¦    ¦         flight crew is to ensure      ¦

¦                           ¦    ¦    ¦         that no cargo is carried in   ¦

¦                           ¦    ¦    ¦         the forward or aft cargo      ¦

¦                           ¦    ¦    ¦         compartment.                  ¦

¦                           ¦    ¦    ¦      b) Place a placard next to the   ¦

¦                           ¦    ¦    ¦         Cargo Bay Fire Protection     ¦

¦                           ¦    ¦    ¦         panel. The placard will       ¦

¦                           ¦    ¦    ¦         read: "CARGO BAY FIRE         ¦

¦                           ¦    ¦    ¦         PROTECTION SYSTEM CONTROL     ¦

¦                           ¦    ¦    ¦         PANEL INOP."                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦      9) External        C ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦

¦         CARGO             ¦    ¦    ¦     a) Before each flight, the        ¦

¦         SMOKE             ¦    ¦    ¦        flight crew is to ensure       ¦

¦         Interface         ¦    ¦    ¦        that no cargo is carried in    ¦

¦                           ¦    ¦    ¦        the forward  or aft cargo      ¦

¦                           ¦    ¦    ¦        compartment.                   ¦

¦                           ¦    ¦    ¦     b) Place a placard next to the    ¦

¦                           ¦    ¦    ¦        Cargo Bay Fire Protection      ¦

¦                           ¦    ¦    ¦        panel. The placard will        ¦

¦                           ¦    ¦    ¦        read:"CARGO BAY FIRE           ¦

¦                           ¦    ¦    ¦        PROTECTION EXTERNAL CARGO      ¦

¦                           ¦    ¦    ¦        SMOKE ALARM INTERFACE INOP."   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 27-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Stabilizer          C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦

¦     Position Indicator    ¦    ¦    ¦ Mechanical Position Indicator on      ¦

¦     (Electric)            ¦    ¦    ¦ the trim wheel is operative.          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Stabilizer          C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided it     ¦

¦     Electric Motor        ¦    ¦    ¦ is verified that the stabilizer       ¦

¦                           ¦    ¦    ¦ moves freely to the normal limits     ¦

¦                           ¦    ¦    ¦ of its travel.                        ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Speedbrake System   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦                           ¦    ¦    ¦     a) Speedbrakes are secured        ¦

¦                           ¦    ¦    ¦        CLOSED, and                    ¦

¦                           ¦    ¦    ¦     b) Aircraft is operated at or     ¦

¦                           ¦    ¦    ¦        below FL250.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Speedbrake          C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided it     ¦

¦     Accumulator           ¦    ¦    ¦ is verified that the malfunction      ¦

¦                           ¦    ¦    ¦ does not affect operation of the      ¦

¦                           ¦    ¦    ¦ Speedbrake System.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Speedbrake          C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦     Position Indicator    ¦    ¦    ¦     a) Speedbrake System is           ¦

¦                           ¦    ¦    ¦        verified to be operative,      ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     b) Speedbrake Blue Indicating     ¦

¦                           ¦    ¦    ¦        Light is operative.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Speedbrake Blue     C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦

¦     Indicating Light      ¦    ¦    ¦ Speedbrake Position Indicator is      ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Speedbrake Lever    C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦

¦     "No Back"             ¦    ¦    ¦ Speedbrake Accumulator is             ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 27-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Liftdumper System   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦                           ¦    ¦    ¦     a) Liftdumper Lock Switch is      ¦

¦                           ¦    ¦    ¦        selected to LOCK,              ¦

¦                           ¦    ¦    ¦     b) Liftdumper extension by        ¦

¦                           ¦    ¦    ¦        means of the Liftdumper        ¦

¦                           ¦    ¦    ¦        Lever (or the override         ¦

¦                           ¦    ¦    ¦        switch for pre SB 28/27-101)   ¦

¦                           ¦    ¦    ¦        is verified to be              ¦

¦                           ¦    ¦    ¦        inoperative,                   ¦

¦                           ¦    ¦    ¦     c) Performance correction is      ¦

¦                           ¦    ¦    ¦        applied in accordance with     ¦

¦                           ¦    ¦    ¦        the AFM, and                   ¦

¦                           ¦    ¦    ¦     d) Liftdumper System is           ¦

¦                           ¦    ¦    ¦        deactivated and Cockpit        ¦

¦                           ¦    ¦    ¦        warnings removed using an      ¦

¦                           ¦    ¦    ¦        accepted procedure.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Flight Control        ¦    ¦    ¦                                       ¦

¦     Hydraulic Bypass      ¦    ¦    ¦                                       ¦

¦     Indication Systems    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1)  Central Flight  C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦

¦                           ¦    ¦    ¦ Individual Bypass Caution Lights      ¦

¦                           ¦    ¦    ¦ are operative.                        ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2)  Individual      C ¦ 6  ¦ 5  ¦ (M)One may be inoperative             ¦

¦         Bypass Caution    ¦    ¦    ¦ provided:                             ¦

¦         Lights (AILERON,  ¦    ¦    ¦     a) It is verified by an           ¦

¦         STABIL, RUDDER)   ¦    ¦    ¦        accepted procedure that the    ¦

¦                           ¦    ¦    ¦        malfunction is in the          ¦

¦                           ¦    ¦    ¦        Caution System, and            ¦

¦                           ¦    ¦    ¦     b) Central Flight Control         ¦

¦                           ¦    ¦    ¦        Caution Light is operative.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE: ELEVATOR Caution Lights must    ¦

¦                           ¦    ¦    ¦       be operative.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 27-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Liftdumper Arming   C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦     Function              ¦    ¦    ¦     a) Liftdumper is not              ¦

¦                           ¦    ¦    ¦        inoperative ARMED and the      ¦

¦                           ¦    ¦    ¦        "IN" indication is present,    ¦

¦                           ¦    ¦    ¦     b) Manual Liftdumper is           ¦

¦                           ¦    ¦    ¦        verified operative, and        ¦

¦                           ¦    ¦    ¦     c) Applicable AFM performance     ¦

¦                           ¦    ¦    ¦        chart is used.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Liftdumper          C ¦ 1  ¦ 0  ¦ May be inoperative provided AFM       ¦

¦     Accumulator System    ¦    ¦    ¦ performance correction for            ¦

¦                           ¦    ¦    ¦ Liftdumpers inoperative is used.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Liftdumper          C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦     Accumulator           ¦    ¦    ¦     a) Accumulator Pressure is        ¦

¦     Pressure Indicator    ¦    ¦    ¦        verified correct before each   ¦

¦     (On Accumulator       ¦    ¦    ¦        flight.                        ¦

¦     Service Panel         ¦    ¦    ¦           OR                          ¦

¦                         C ¦    ¦    ¦     b) AFM Performance correction     ¦

¦                           ¦    ¦    ¦        for Liftdumpers inoperative    ¦

¦                           ¦    ¦    ¦        is used.                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Rudder Pedal        C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦

¦     Adjustment            ¦    ¦    ¦ pedals are adjusted and secured       ¦

¦                           ¦    ¦    ¦ using an accepted maintenance         ¦

¦                           ¦    ¦    ¦ procedure in a position suitable to   ¦

¦                           ¦    ¦    ¦ the crewmember assigned to the        ¦

¦                           ¦    ¦    ¦ seat.                                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Alternate Flap      C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦     Control System        ¦    ¦    ¦ Liftdumper Accumulator System is      ¦

¦                           ¦    ¦    ¦ pressurized.                          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Flap Auto-Reset     C ¦ 1  ¦ 0  ¦ May be inoperative provided that      ¦

¦     System                ¦    ¦    ¦ Normal Flap Control System is         ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 11 a     ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 10/23/2000      ¦ 28-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Main Tank Fuel      C ¦ 4  ¦ 3  ¦ (O)One may be inoperative provided:   ¦

¦     Booster Pumps         ¦    ¦    ¦     a) Crossfeed System is verified   ¦

¦                           ¦    ¦    ¦        operative before each          ¦

¦                           ¦    ¦    ¦        departure,                     ¦

¦                           ¦    ¦    ¦     b) Approved Kerosene Type Fuel  | ¦

¦                           ¦    ¦    ¦        is used,                     | ¦

¦                           ¦    ¦    ¦     c) Required fuel for dispatch     ¦

¦                           ¦    ¦    ¦        is increased by the amount     ¦

¦                           ¦    ¦    ¦        of unusable fuel with both     ¦

¦                           ¦    ¦    ¦        pumps inoperative, and         ¦

¦                           ¦    ¦    ¦     d) AFM limitations are applied.   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Center Tank Fuel    C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦ *** Transfer Pumps        ¦    ¦    ¦     a) Fuel quantity in main Tanks    ¦

¦                           ¦    ¦    ¦        at any point in flight is      ¦

¦                           ¦    ¦    ¦        adequate to reach an en        ¦

¦                           ¦    ¦    ¦        route alternate with           ¦

¦                           ¦    ¦    ¦        appropriate reserves,          ¦

¦                           ¦    ¦    ¦     b) Fuel in Center Tank is         ¦

¦                           ¦    ¦    ¦        considered Payload, and        ¦

¦                           ¦    ¦    ¦     c) All cockpit fuel quantity      ¦

¦                           ¦    ¦    ¦        indicators are operative.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 0  ¦ Both may be inoperative provided:     ¦

¦                           ¦    ¦    ¦     a) Fuel in center Tank is         ¦

¦                           ¦    ¦    ¦        considered payload, and        ¦

¦                           ¦    ¦    ¦     b) All Cockpit Fuel Quantity      ¦

¦                           ¦    ¦    ¦        indicators are operative.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Main Tank Transfer  C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦     Jetpumps              ¦    ¦    ¦     a) Fuel Quantity Indicating       ¦

¦                           ¦    ¦    ¦        System of the associated       ¦

¦                           ¦    ¦    ¦        tank is operative, and         ¦

¦                           ¦    ¦    ¦     b) Both Booster Pumps in          ¦

¦                           ¦    ¦    ¦        associated tanks are           ¦

¦                           ¦    ¦    ¦        operative.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 28-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Electrically        C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦

¦     Operated Fuel         ¦    ¦    ¦ the affected valve is deactivated     ¦

¦     Crossfeed Valves      ¦    ¦    ¦ OPEN.                                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Main Tank Fuel      C ¦ 2  ¦ 1  ¦ (O)One may be inoperative             ¦

¦     Quantity Indicators   ¦    ¦    ¦ provided:                             ¦

¦                           ¦    ¦    ¦     a) Fuel quantity is verified      ¦

¦                           ¦    ¦    ¦        by magnetic level indicators   ¦

¦                           ¦    ¦    ¦        or other accepted procedures   ¦

¦                           ¦    ¦    ¦        before each flight,            ¦

¦                           ¦    ¦    ¦     b) Minimum fuel reserves are      ¦

¦                           ¦    ¦    ¦        increased by five percent      ¦

¦                           ¦    ¦    ¦        before dispatch,               ¦

¦                           ¦    ¦    ¦     c) Both Fuel Flow Indicating      ¦

¦                           ¦    ¦    ¦        Systems are operative, and     ¦

¦                           ¦    ¦    ¦     d) Flight crew either             ¦

¦                           ¦    ¦    ¦        periodically computes the      ¦

¦                           ¦    ¦    ¦        actual fuel remaining or       ¦

¦                           ¦    ¦    ¦        checks fuel remaining          ¦

¦                           ¦    ¦    ¦        against a precomputed fuel     ¦

¦                           ¦    ¦    ¦        burn chart.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Collector Tank      C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦     Quantity Indicators   ¦    ¦    ¦     a) Float Switch in the affected   ¦

¦                           ¦    ¦    ¦        tank is operative,             ¦

¦                           ¦    ¦    ¦     b) Fuel quantity is verified      ¦

¦                           ¦    ¦    ¦        by magnetic level indicators   ¦

¦                           ¦    ¦    ¦        or other accepted procedures   ¦

¦                           ¦    ¦    ¦        before each flight,            ¦

¦                           ¦    ¦    ¦     c) Minimum fuel reserves are      ¦

¦                           ¦    ¦    ¦        increased by five percent      ¦

¦                           ¦    ¦    ¦        before dispatch,               ¦

¦                           ¦    ¦    ¦     d) Both Fuel Flow Indicating      ¦

¦                           ¦    ¦    ¦        Systems are operative, and     ¦

¦                           ¦    ¦    ¦     e) Flight crew either             ¦

¦                           ¦    ¦    ¦        periodically computes the      ¦

¦                           ¦    ¦    ¦        actual fuel remaining or       ¦

¦                           ¦    ¦    ¦        checks fuel remaining          ¦

¦                           ¦    ¦    ¦        against a precomputed fuel     ¦

¦                           ¦    ¦    ¦        burn chart.                    ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 28-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Collector Tank      C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦     Float Switches        ¦    ¦    ¦ associated Total and Collector Tank   ¦

¦                           ¦    ¦    ¦ Quantity Indicating System is         ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Center Tank         C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦ *** Quantity              ¦    ¦    ¦     a) Both Center Tank Transfer      ¦

¦     Indicating Systems    ¦    ¦    ¦        Pumps are operative,           ¦

¦                           ¦    ¦    ¦     b) Center tank fuel quantity is   ¦

¦                           ¦    ¦    ¦        verified before each takeoff   ¦

¦                           ¦    ¦    ¦        by other accepted              ¦

¦                           ¦    ¦    ¦        procedures, and                ¦

¦                           ¦    ¦    ¦     c) Both Fuel Flow Indicator       ¦

¦                           ¦    ¦    ¦        Systems are verified to be     ¦

¦                           ¦    ¦    ¦        operative.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Fuel Used Counters  C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦ ***                       ¦    ¦    ¦ all Fuel Quantity Indicating          ¦

¦                           ¦    ¦    ¦ Systems are operative.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Fuel Booster Pump   C ¦ 4  ¦ 2  ¦ Two may be inoperative provided:      ¦

¦     Low Pressure          ¦    ¦    ¦     a) One is operative for each      ¦

¦     Caution Lights        ¦    ¦    ¦        Main Tank, and                 ¦

¦                           ¦    ¦    ¦     b) Remaining Caution Lights and   ¦

¦                           ¦    ¦    ¦        associated pumps are           ¦

¦                           ¦    ¦    ¦        verified operative.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Center Tank         C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦ *** Transfer Pump Low     ¦    ¦    ¦     a) Fuel Quantity Indicating       ¦

¦     Pressure Caution      ¦    ¦    ¦        System is operative, and       ¦

¦     Lights                ¦    ¦    ¦     b) Low Pressure Caution Light     ¦

¦                           ¦    ¦    ¦        associated with the            ¦

¦                           ¦    ¦    ¦        remaining pump is verified     ¦

¦                           ¦    ¦    ¦        to be operative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Magnetic Fuel       C ¦ 6  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦     Level Indicators      ¦    ¦    ¦ fuel quantity in affected tank(s)     ¦

¦     (Sticks)              ¦    ¦    ¦ is verified by other accepted         ¦

¦                           ¦    ¦    ¦ procedures.                           ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 28-4     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Center Tank Fuel    C ¦ 1  ¦ 0  ¦ May be inoperative provided Center    ¦

¦     System                ¦    ¦    ¦ Tank remains empty.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Pressure Refueling  C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦     System                ¦    ¦    ¦ accepted alternate refueling          ¦

¦                           ¦    ¦    ¦ procedure is used.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Fueling Control     C ¦ -  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦     Panel Fuel            ¦    ¦    ¦     a) Fuel Tanks are refueled        ¦

¦     Quantity              ¦    ¦    ¦        using accepted alternate       ¦

¦     Indication            ¦    ¦    ¦        procedure,                     ¦

¦                           ¦    ¦    ¦     b) Fuel Tank Quantity is          ¦

¦                           ¦    ¦    ¦        monitored during refueling     ¦

¦                           ¦    ¦    ¦        using Magnetic Fuel Level      ¦

¦                           ¦    ¦    ¦        Indicators or other accepted   ¦

¦                           ¦    ¦    ¦        procedure, and                 ¦

¦                           ¦    ¦    ¦     c) Fuel quantity in the Center    ¦

¦                           ¦    ¦    ¦        Tank is verified before        ¦

¦                           ¦    ¦    ¦        refueling.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 16. Fueling Control     C ¦ -  ¦ 0  ¦ May be inoperative provided Manual    ¦

¦     Panel Fuel Load       ¦    ¦    ¦ refueling procedure is used.          ¦

¦     Pre-Select            ¦    ¦    ¦                                       ¦

¦     Function              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 17. Fuel Consumed       C ¦ 1  ¦ 0  ¦ May be inoperative provided both      ¦

¦     Weight Indication     ¦    ¦    ¦ Main Tank Fuel Quantity indicators    ¦

¦     (Digital)             ¦    ¦    ¦ are operative.                        ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 29-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Pump Low Pressure   C ¦ 4  ¦ 2  ¦ (O)Two may be inoperative             ¦

¦     Warning Lights        ¦    ¦    ¦ provided:                             ¦

¦                           ¦    ¦    ¦     a) One is operative in each       ¦

¦                           ¦    ¦    ¦        system affected, and           ¦

¦                           ¦    ¦    ¦     b) Pump output pressure is        ¦

¦                           ¦    ¦    ¦        checked on system pressure     ¦

¦                           ¦    ¦    ¦        indicator before each flight   ¦

¦                           ¦    ¦    ¦        with remaining pump in that    ¦

¦                           ¦    ¦    ¦        system OFF.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  System Pressure     C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦     Gauges                ¦    ¦    ¦ all other components and indicators   ¦

¦                           ¦    ¦    ¦ for the associated system are         ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Reservoir Low       C ¦ 2  ¦ 0  ¦                                       ¦

¦     Pressure Warning      ¦    ¦    ¦                                       ¦

¦     Systems               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Hydraulic Fluid     C ¦ 2  ¦ 0  ¦ (M)Both may be inoperative            ¦

¦     Quantity              ¦    ¦    ¦ provided each reservoir is checked    ¦

¦     Indicating System     ¦    ¦    ¦ for proper quantity before each       ¦

¦                           ¦    ¦    ¦ takeoff.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  DELETED               ¦    ¦    ¦ DELETED before revision 7.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  System 2 Engine     C ¦ 2  ¦ 1  ¦ (M)One may be inoperative             ¦

¦     Driven Hydraulic      ¦    ¦    ¦ provided:                             ¦

¦     Pumps                 ¦    ¦    ¦     a) Associated Hydraulic System    ¦

¦                           ¦    ¦    ¦        is verified free of leaks,     ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     b) Affected pump remains OFF.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Electric Hydraulic  C ¦ -  ¦ 0  ¦                                       ¦

¦     Pumps                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Hydraulic System    C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦     Overheat Lights       ¦    ¦    ¦ all other Hydraulic System            ¦

¦                           ¦    ¦    ¦ indications are operative.            ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 29-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Utility and Flight  C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦     Control Hydraulic     ¦    ¦    ¦ all other Hydraulic System            ¦

¦     System Accumulator    ¦    ¦    ¦ Indicators are operative.             ¦

¦     Systems               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE: Accumulator is considered       ¦

¦                           ¦    ¦    ¦       inoperative if the associated   ¦

¦                           ¦    ¦    ¦       Service Panel indicator is      ¦

¦                           ¦    ¦    ¦       inoperative.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 30-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Ice Detection       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦

¦     System                ¦    ¦    ¦ operations procedures do not depend   ¦

¦                           ¦    ¦    ¦ on its use.                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Engine Anti-Ice     C ¦ 4  ¦ 2  ¦ (M)One on each engine may be          ¦

¦     Valves                ¦    ¦    ¦ inoperative provided:                 ¦

¦                           ¦    ¦    ¦     a) Affected Valve is secured      ¦

¦                           ¦    ¦    ¦        CLOSED, and                    ¦

¦                           ¦    ¦    ¦     b) Aircraft is not operated in    ¦

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Engine Anti-Ice     C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦

¦     Pressure Indicators   ¦    ¦    ¦ associated Engine Anti-Ice System     ¦

¦                           ¦    ¦    ¦ is verified operative.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 1  ¦ One may be inoperative provided the   ¦

¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Airfoil Anti-Ice    C ¦ 2  ¦ 0  ¦ (M)Both may be inoperative            ¦

¦     Shutoff Valve         ¦    ¦    ¦ provided:                             ¦

¦     Systems               ¦    ¦    ¦     a) Associated Modulating Valve    ¦

¦                           ¦    ¦    ¦        is secured CLOSED, and         ¦

¦                           ¦    ¦    ¦     b) Airplane is not operated in    ¦

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Airfoil Anti-Ice    C ¦ 2  ¦ 0  ¦ (M)Both may be inoperative provided   ¦

¦     Shutoff Valve         ¦    ¦    ¦ associated Airfoil Anti-ice           ¦

¦     Position Indicators   ¦    ¦    ¦ Temperature Indicators are verified   ¦

¦                           ¦    ¦    ¦ operative before each departure.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦

¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 30-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Airfoil Anti-Ice    C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦     Modulating Valve      ¦    ¦    ¦     a) Associated Anti-Ice Shutoff    ¦

¦     Systems               ¦    ¦    ¦        Valve remains CLOSED, and      ¦

¦                           ¦    ¦    ¦     b) Airplane is not operated in    ¦

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Airfoil Anti-Ice    C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative provided   ¦

¦     Modulating Valve      ¦    ¦    ¦ associated Airfoil Anti-ice           ¦

¦     Indicators            ¦    ¦    ¦ Temperature Indicators are verified   ¦

¦                           ¦    ¦    ¦ operative before each departure.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦

¦                           ¦    ¦    ¦ or forecast icing conditions          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Airfoil Anti-Ice    C ¦ 2  ¦ 0  ¦ (M)Both may be inoperative provided   ¦

¦     Temperature           ¦    ¦    ¦ all other components of the           ¦

¦     Indicators            ¦    ¦    ¦ associated Airfoil Anti-Ice System    ¦

¦                           ¦    ¦    ¦ are verified operative before each    ¦

¦                           ¦    ¦    ¦ departure.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Primary Leading     C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦

¦     Edge Overheat         ¦    ¦    ¦ all other components of the           ¦

¦     Protection Systems    ¦    ¦    ¦ associated Airfoil Anti-Ice System    ¦

¦                           ¦    ¦    ¦ are verified operative before each    ¦

¦                           ¦    ¦    ¦ departure.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 30-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Windshield Heating  C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦     Systems               ¦    ¦    ¦     a) Airplane is not operated in    ¦

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions, and                ¦

¦                           ¦    ¦    ¦     b) AFM Limitations are            ¦

¦                           ¦    ¦    ¦        observed.                      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Sliding Window      C ¦ 2  ¦ 0  ¦ (M)Both may be inoperative provided   ¦

¦     Heating Systems       ¦    ¦    ¦ electrical power is removed from      ¦

¦                           ¦    ¦    ¦ the affected systems.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Pitot Heaters       B ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦                           ¦    ¦    ¦     a) Aircraft is operated in day    ¦

¦                           ¦    ¦    ¦        VMC,                           ¦

¦                           ¦    ¦    ¦     b) Aircraft is not operated in    ¦

¦                           ¦    ¦    ¦        visible moisture, and          ¦

¦                           ¦    ¦    ¦     c) Aircraft is not operated in    ¦

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Pitot Heat Failure  B ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦

¦     Lights                ¦    ¦    ¦ both heaters are verified operative   ¦

¦                           ¦    ¦    ¦ before each departure.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         B ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦                           ¦    ¦    ¦     a) Aircraft is not operated in    ¦

¦                           ¦    ¦    ¦        visible moisture, and          ¦

¦                           ¦    ¦    ¦     b) Aircraft is not operated in    ¦

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Angle of Attack     C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦     Vane Heaters          ¦    ¦    ¦ aircraft is not operated in known     ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 30-4     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Static Port         C ¦ 2  ¦ 0  ¦ Both may be inoperative provided:     ¦

¦     Heaters               ¦    ¦    ¦     a) Ambient temperature is at or   ¦

¦                           ¦    ¦    ¦        above +40 degrees F (+5        ¦

¦                           ¦    ¦    ¦        degrees C), and                ¦

¦                           ¦    ¦    ¦     b) Runways or taxiways are not    ¦

¦                           ¦    ¦    ¦        covered with slush or          ¦

¦                           ¦    ¦    ¦        standing water.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 16. Windshield Wiper    C ¦ 2  ¦ 0  ¦ Both may be inoperative provided      ¦

¦     Systems               ¦    ¦    ¦ airplane is not operated in           ¦

¦                           ¦    ¦    ¦ precipitation with in 5 miles of      ¦

¦                           ¦    ¦    ¦ the airport of takeoff or intended    ¦

¦                           ¦    ¦    ¦ landing.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 17. Rain Repellant      D ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦ *** System                ¦    ¦    ¦ approach procedures do not require    ¦

¦                           ¦    ¦    ¦ its use.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 18. Wing Anti-Icing       ¦    ¦    ¦                                       ¦

¦     System                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) In-Flight        C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦        System (Without    ¦    ¦    ¦     a) Wing Modulating and Shutoff    ¦

¦        SB F28-30-31)      ¦    ¦    ¦        Valve or Wing Shut-off Valve   ¦

¦        or In-Flight and   ¦    ¦    ¦        is secured CLOSED,             ¦

¦        On-Ground System   ¦    ¦    ¦     b) If ground icing conditions     ¦

¦        (With SB F28-      ¦    ¦    ¦        exist, a tactile check is      ¦

¦        30-31)             ¦    ¦    ¦        performed before take-off or   ¦

¦                           ¦    ¦    ¦        alternate take-off technique   ¦

¦                           ¦    ¦    ¦        is used per AFM, and           ¦

¦                           ¦    ¦    ¦     c) Aircraft is not operated in    ¦

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ (Continued                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 30-5     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 18. Wing Anti-Ice         ¦    ¦    ¦                                       ¦

¦     System                ¦    ¦    ¦                                       ¦

¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ *** 2) On-Ground        C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦        System             ¦    ¦    ¦     a) In-Flight System is verified   ¦

¦                           ¦    ¦    ¦        to function normally, and      ¦

¦                           ¦    ¦    ¦     b) If ground icing conditions     ¦

¦                           ¦    ¦    ¦        exist, a tactile check is      ¦

¦                           ¦    ¦    ¦        performed before take-off or   ¦

¦                           ¦    ¦    ¦        alternate take-off technique   ¦

¦                           ¦    ¦    ¦        is used per AFM.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 12/14/1998      ¦ 31-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦

¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Flight Data         A ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦     Recorder (FDR)        ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR)   ¦

¦                           ¦    ¦    ¦        operates normally, and         ¦

¦                           ¦    ¦    ¦     b) Airplane is not dispatched     ¦

¦                           ¦    ¦    ¦        from a designated airport      ¦

¦                           ¦    ¦    ¦        where repairs or               ¦

¦                           ¦    ¦    ¦        replacements can be made,      ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     c) Repairs are made within        ¦

¦                           ¦    ¦    ¦        three flight days.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) DFDRS            C ¦ -  ¦ 0  ¦                                       ¦

¦        Recording          ¦    ¦    ¦                                       ¦

¦        Parameters not     ¦    ¦    ¦                                       ¦

¦        required by FAR.   ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Clocks (Cockpit)    C ¦ -  ¦ 1  ¦ One may be inoperative at either      ¦

¦                           ¦    ¦    ¦ the pilot's or copilot's station.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 32-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Mechanical          C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦

¦     Downlock              ¦    ¦    ¦ other portions of the gear position   ¦

¦     Indicating System     ¦    ¦    ¦ indicating system are operative.      ¦

¦     (Nose Gear)           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Nose Wheel          C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦     Steering Shut Off     ¦    ¦    ¦     a) Valve is failed OPEN, and      ¦

¦     Valve                 ¦    ¦    ¦     b) Procedures are established     ¦

¦                           ¦    ¦    ¦        and used for pushback with     ¦

¦                           ¦    ¦    ¦        the Utility Hydraulic System   ¦

¦                           ¦    ¦    ¦        inoperative.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Brake Cooling Fans  C ¦ 4  ¦ 0  ¦                                       ¦

¦ ***                       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Anti-Skid System    C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦                           ¦    ¦    ¦     a) System is electrically         ¦

¦                           ¦    ¦    ¦        isolated or remains OFF,       ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     b) Aircraft is operated using     ¦

¦                           ¦    ¦    ¦        AFM Limitations, Performance   ¦

¦                           ¦    ¦    ¦        and Procedures for             ¦

¦                           ¦    ¦    ¦        inoperative Anti-Skid.         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Brake Temperature   C ¦ 4  ¦ 2  ¦ One may be inoperative on each        ¦

¦ *** Indicators            ¦    ¦    ¦ Main Gear.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Normal Brake        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦     Pressure              ¦    ¦    ¦ Utility System Hydraulic Pressure     ¦

¦     Indicating System     ¦    ¦    ¦ Indicator is operative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Alternate Brake     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦     Pressure              ¦    ¦    ¦ associated Hydraulic System           ¦

¦     Indicating System     ¦    ¦    ¦ Pressure Indicator is operative.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Main Landing Gear   A ¦ 4  ¦ 3  ¦ One may be inoperative provided       ¦

¦     Downlock (Green)      ¦    ¦    ¦ repair is completed within 10         ¦

¦     Indicating Lights     ¦    ¦    ¦ flight hours.                         ¦

¦     (Ten Light System)    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 32-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Gear Handle         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦     Downlock Solenoid     ¦    ¦    ¦     a) Downlock Solenoid is           ¦

¦                           ¦    ¦    ¦        inoperative LOCKED,            ¦

¦                           ¦    ¦    ¦     b) Override mechanism is          ¦

¦                           ¦    ¦    ¦        operative, and                 ¦

¦                           ¦    ¦    ¦     c) Both Airfoil anti-Ice          ¦

¦                           ¦    ¦    ¦        Systems are verified           ¦

¦                           ¦    ¦    ¦        operative before Landing       ¦

¦                           ¦    ¦    ¦        Gear retraction.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Nose Tire           D ¦ 2  ¦ 0  ¦ (M)May be inoperative provided it     ¦

¦     Brakes                ¦    ¦    ¦ is verified that no hazard exists.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 33-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Flight Deck/Flight  C ¦ -  ¦ -  ¦ Individual lights may be              ¦

¦     Compartment and       ¦    ¦    ¦ inoperative provided remaining        ¦

¦     Instrument Lighting   ¦    ¦    ¦ lights are:                           ¦

¦     System                ¦    ¦    ¦     a) Sufficient to clearly          ¦

¦                           ¦    ¦    ¦        illuminate all required        ¦

¦                           ¦    ¦    ¦        instruments, controls, and     ¦

¦                           ¦    ¦    ¦        other devices for which they   ¦

¦                           ¦    ¦    ¦        are provided,                  ¦

¦                           ¦    ¦    ¦     b) Positioned so that direct      ¦

¦                           ¦    ¦    ¦        rays are shielded from         ¦

¦                           ¦    ¦    ¦        flight crew member's eyes,     ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     c) Lighting configuration and     ¦

¦                           ¦    ¦    ¦        intensity is acceptable to     ¦

¦                           ¦    ¦    ¦        the flight crew.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Cabin Interior      C ¦ -  ¦ -  ¦ May be inoperative provided:          ¦

¦     Illumination          ¦    ¦    ¦     a) Cabin Emergency lighting is    ¦

¦     System                ¦    ¦    ¦        operative,                     ¦

¦                           ¦    ¦    ¦     b) Sufficient lighting is         ¦

¦                           ¦    ¦    ¦        operative for crew to          ¦

¦                           ¦    ¦    ¦        perform required duties, and   ¦

¦                           ¦    ¦    ¦     c) Lighting configuration at      ¦

¦                           ¦    ¦    ¦        dispatch is acceptable to      ¦

¦                           ¦    ¦    ¦        the flight crew.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Cargo Compartment   C ¦ 1  ¦ 0  ¦                                       ¦

¦     Light System          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 33-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  No Smoking/Fasten   C ¦ -  ¦ -  ¦ (O)May be inoperative provided:       ¦

¦     Seat Belt Signs       ¦    ¦    ¦     a) Passenger or Flight            ¦

¦                           ¦    ¦    ¦        Attendant Seats from which a   ¦

¦                           ¦    ¦    ¦        NO SMOKING or FASTEN SEAT      ¦

¦                           ¦    ¦    ¦        BELT sign cannot be seen are   ¦

¦                           ¦    ¦    ¦        considered inoperative.        ¦

¦                           ¦    ¦    ¦           OR                          ¦

¦                         C ¦    ¦    ¦     b) Procedures are established     ¦

¦                           ¦    ¦    ¦        for alerting the Flight        ¦

¦                           ¦    ¦    ¦        Attendants and notifying the   ¦

¦                           ¦    ¦    ¦        passengers by use of the       ¦

¦                           ¦    ¦    ¦        Passenger Address System       ¦

¦                           ¦    ¦    ¦        when seat belts should be      ¦

¦                           ¦    ¦    ¦        fastened and smoking is        ¦

¦                           ¦    ¦    ¦        prohibited.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Anti Collision      C ¦ 2  ¦ 0  ¦ Both may be inoperative provided:     ¦

¦     Lights                ¦    ¦    ¦     a) A Strobe Light System          ¦

¦                           ¦    ¦    ¦        meeting the FAR requirements   ¦

¦                           ¦    ¦    ¦        of an Anti-Collision Beacon    ¦

¦                           ¦    ¦    ¦        System is installed and        ¦

¦                           ¦    ¦    ¦        operative.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦    ¦    ¦     b) May be inoperative for day     ¦

¦                           ¦    ¦    ¦        operations.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Logo Lights         D ¦ 2  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Wing Illumination   C ¦ 2  ¦ 0  ¦ (O)May be inoperative for night       ¦

¦     Lights                ¦    ¦    ¦ operations provided ground            ¦

¦                           ¦    ¦    ¦ de-icing procedures do not            ¦

¦                           ¦    ¦    ¦ require their use.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦

¦                FOKKER 28                 ¦                       ¦          ¦

¦                                          ¦ DATE: 09/24/1996      ¦ 33-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Landing and         C ¦ 3  ¦ 2  ¦                                       ¦

¦     Flare-Out Lights      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 3  ¦ 0  ¦ May be inoperative provided the       ¦

¦                           ¦    ¦    ¦ aircraft is not operated at night.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Taxi Light          C ¦ 1  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦