DEPARTMENT OF TRANSPORTATION     Revision: ORIGINAL

                                                           Date: 02/03/88

                         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 F-50

 

 

 

 

 

 

 

 

 

 

 

 

 

                         Federal Aviation Administration

                         Flight Standards Division

                         Aircraft Evaluation Group, ANM-270L

                         4340 Donald Douglas Drive

                         Long Beach, CA 90808

 

                         Telephone:  (213) 548-2871

                                     FTS:  796-2871


 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I

         --     Control Page                            II, III

         --     Highlights of Change                    IV

         --     Definitions                             V, VI, VII, VIII

         --     Model Applicability                     IX

         --     Preamble                                X, XI

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

         22     Auto Flight                             22-1

         23     Communications                          23-1, 2, 3, 4

         24     Electrical Power                        24-1, 2

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

         26     Fire Protection                         26-1, 2, 3

         27     Flight Controls                         27-1

         28     Fuel                                    28-1, 2, 3

         29     Hydraulic Power                         29-1, 2

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

         31     Indicating/Recording Systems            31-1, 2, 3

         32     Landing Gear                            32-1

         33     Lights                                  33-1, 2, 3, 4

         34     Navigation                              34-1, 2, 3, 4

         35     Oxygen                                  35-1

         36     Pneumatic                               36-1

         52     Doors                                   52-1

         73     Engine Fuel & Control                   73-1, 2

         77     Engine Indicating                       77-1, 2

         80     Starting                                80-1


 

                       FEDERAL AVIATION ADMINISTRATION     Page: II

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       ORIGINAL 02/03/88

         Table of Contents                        I       ORIGINAL 02/03/88

         Control Page                             II      ORIGINAL 02/03/88

                                                  III     ORIGINAL 02/03/88

         Highlights of Change                     IV      ORIGINAL 02/03/88

         Definitions                              V       ORIGINAL 02/03/88

                                                  VI      ORIGINAL 02/03/88

                                                  VII     ORIGINAL 02/03/88

                                                  VIII    ORIGINAL 02/03/88

         Model Applicability                      IX      ORIGINAL 02/03/88

         Preamble                                 X       ORIGINAL 02/03/88

                                                  XI      ORIGINAL 02/03/88

         21                                       21-1    ORIGINAL 02/03/88

                                                  21-2    ORIGINAL 02/03/88

                                                  21-3    ORIGINAL 02/03/88

                                                  21-4    ORIGINAL 02/03/88

         22                                       22-1    ORIGINAL 02/03/88

         23                                       23-1    ORIGINAL 02/03/88

                                                  23-2    ORIGINAL 02/03/88

                                                  23-3    ORIGINAL 02/03/88

                                                  23-4    ORIGINAL 02/03/88

         24                                       24-1    ORIGINAL 02/03/88

                                                  24-2    ORIGINAL 02/03/88

         25                                       25-1    ORIGINAL 02/03/88

                                                  25-2    ORIGINAL 02/03/88

                                                  25-3    ORIGINAL 02/03/88

                                                  25-4    ORIGINAL 02/03/88

         26                                       26-1    ORIGINAL 02/03/88

                                                  26-2    ORIGINAL 02/03/88

                                                  26-3    ORIGINAL 02/03/88

         27                                       27-1    ORIGINAL 02/03/88

         28                                       28-1    ORIGINAL 02/03/88

                                                  28-2    ORIGINAL 02/03/88

                                                  28-3    ORIGINAL 02/03/88

         29                                       29-1    ORIGINAL 02/03/88

                                                  29-2    ORIGINAL 02/03/88

         30                                       30-1    ORIGINAL 02/03/88

                                                  30-2    ORIGINAL 02/03/88

                                                  30-3    ORIGINAL 02/03/88

         31                                       31-1    ORIGINAL 02/03/88


 

                       FEDERAL AVIATION ADMINISTRATION     Page: III

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  31-2    ORIGINAL 02/03/88

                                                  31-3    ORIGINAL 02/03/88

         32                                       32-1    ORIGINAL 02/03/88

         33                                       33-1    ORIGINAL 02/03/88

                                                  33-2    ORIGINAL 02/03/88

                                                  33-3    ORIGINAL 02/03/88

                                                  33-4    ORIGINAL 02/03/88

         34                                       34-1    ORIGINAL 02/03/88

                                                  34-2    ORIGINAL 02/03/88

                                                  34-3    ORIGINAL 02/03/88

                                                  34-4    ORIGINAL 02/03/88

         35                                       35-1    ORIGINAL 02/03/88

         36                                       36-1    ORIGINAL 02/03/88

         52                                       52-1    ORIGINAL 02/03/88

         73                                       73-1    ORIGINAL 02/03/88

                                                  73-2    ORIGINAL 02/03/88

         77                                       77-1    ORIGINAL 02/03/88

                                                  77-2    ORIGINAL 02/03/88

         80                                       80-1    ORIGINAL 02/03/88


 

                       FEDERAL AVIATION ADMINISTRATION   Page: IV

                                                         Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST    Date: 02/03/88

 

                                FOKKER F-50

 

 

 

                             Highlights of Change

 

 

       EFFECTIVE ABOVE DATE, the Fokker F-50 Master Minimum Equipment List

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

       revision is issued.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

                       FEDERAL AVIATION ADMINISTRATION     Page: V

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

                                 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.

 

                NOTE: - The operator's MEL should list the number installed in

                his particular aircraft.

 

            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.

 

            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.

 

       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 airplane is listed on the applicable Type 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.  Items installed that are

            in excess of the FAR requirements may be permitted by the

            operator's MEL to be inoperative if not otherwise required by the

            MMEL.

 

       4.   Asterisk * symbol in Column 4 indicates the listed item if

            inoperative, must be placarded to inform and remind the crewmembers

            and maintenance personnel of the equipment condition.


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VI

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

                                 Definitions

 

 

            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.   Dash - Symbol in Column 2 indicates a variable number (quantity) of

            the item installed.

 

            NOTE - Operator's MEL must show in Column 2 the number (quantity)

                   of the item installed in the specific aircraft.

 

       6.   "Deleted" after a sequence number indicates the item was previously

            listed but is now required to be operative if installed in the

            aircraft.

 

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

            airplane which has a type design approval for ER operations and

            complies with the provisions of Advisory Circular 120-42.

 

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

            of the Federal Aviation Act and Federal Aviation Regulations.

 

       9.   "Flight Day" - a 24 hour period (from midnight to midnight) during

            which at least one flight is scheduled 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 operation with the

            listed item inoperative.

 

       12.  Notes:  In Column 4 provides additional information for crewmember

            or maintenance consideration.  Notes are to identify applicable

            material which are 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.

 

 

 

 

 

 


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VII

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

                                 Definitions

 

 

       13.  (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, including

            the identification of qualified personnel authorized to accomplish

            them are required to be published as part of the Operator's Manual

            or MEL.

 

            (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, including the identification of

            qualified personnel authorized to accomplish them, are required to

            be published as a part of the Operator's Manual or MEL.

 

       14.  "Secured" and "Deactivated" 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.

 

       15.  "Time In Service" means the time from the moment an aircraft leaves

            the surface of the earth until it touches it at the next point of

            landing (as defined in FAR Part 1).

 

       16.  Visual Flight Rules (VFR) is as defined in FAR Part 91.  This

            precludes a pilot from filing an IFR flight plan.

 

       17.  "Visual Meteorological Conditions" (VMC) - 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.


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

                                 Definitions

 

 

       18.  "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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

                       FEDERAL AVIATION ADMINISTRATION     Page: IX

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 02/03/88

 

                                FOKKER F-50

 

 

                             Model Applicability

 

 

       Aircraft model designations and equipment configurations applicable to

       this MMEL:

 

 

       CERTIFICATED MODEL         COMMON REFERENCE        MMEL DESIGNATION

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

 

       F-27 Mk 050                FOKKER 50 or F-50       F-50

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

                       FEDERAL AVIATION ADMINISTRATION   Page: X

                                                         Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST    Date: 02/03/88

 

                                FOKKER F-50

 

 

                                  Preamble

 

 

       If some deviations from the type certificated configuration and

       equipment required by the operating rules were not permitted,

       the aircraft could not be flown unless all such equipment was

       operable. Experience has proven that the operation of every system

       or component installed on the aircraft is not necessary when the

       remaining operative instruments and equipment provide continued

       safe operations. Therefore certain deviations from these requirements

       are authorized to permit continued or uninterrupted operation

       of the aircraft. The Federal Aviation Regulations permit the

       publication of a MINIMUM EQUIPMENT LIST (MEL) designed to provide

       owners/operators with the authority to operate an aircraft with

       certain items or components inoperative provided the Administrator

       finds an acceptable level of safety maintained by appropriate

       operations limitations, by a transfer of the function to another

       operating component or by reference to other instruments or

       components providing the required information.

 

       For the sake of brevity, the MEL does not include obviously

       required items such as wings, rudders, flaps, engines, landing

       gear, etc. Also, the list may not include items which do not affect

       the airworthiness of the aircraft, such as galley equipment,

       entertainment systems, passenger convenience items, etc. However,

       it is important to note that ALL ITEMS WHICH ARE RELATED TO THE

       AIRWORTHINESS OF THE AIRCRAFT AND NOT INCLUDED ON THE LIST ARE

       AUTOMATICALLY REQUIRED TO BE OPERATIVE.

 

       Unless otherwise specified in the remarks column, the FAA does

       not define "where" or "when" an inoperative item is to be repaired

       or replaced; but rather indicates through approval of MELs those

       instruments and items of equipment that may be inoperative for

       certain flight conditions with the intent that no flight can take

       off from an airport with inoperative equipment other than that

       specified.  The failure of instruments or items of equipment in excess

       of those allowed to be inoperative by the MEL causes the aircraft to be

       unairworthy. The FAA makes no distinction in the MEL for dispatch

       or operation of a flight between points of origin and termination,

       including intermediate stops or flights beyond the scheduled

       termination of the flight. The MEL was never intended to provide for

       continued operation of the aircraft for an indefinite period with

       inoperative items. The basic purpose of the MEL is to permit the

       operation of an aircraft with inoperative equipment within the

 

                                                   Continued on next page


 

                       FEDERAL AVIATION ADMINISTRATION   Page: XI

                                                         Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST    Date: 02/03/88

 

                                FOKKER F-50

 

 

                                  Preamble

 

 

       framework of a controlled and sound program of repairs and parts

       replacement.  It is important that the owner/operator make repairs

       at the first airport where repairs or replacements may be made but,

       in any case, repair should be accomplished at the terminating

       airport, since additional malfunctions may require the aircraft to

       be taken out of service.

 

       Owners/operators are responsible for exercising the necessary

       operational control to assure that no aircraft is dispatched or

       flown with multiple MEL items inoperative without first determining

       that any interface or interrelationship between inoperative systems

       or components will not result in a degradation in the level of

       safety and/or undue increase in crew workload.

 

       The exposure to additional failures during continued operation with

       inoperative systems or components must also be considered in

       determining that an acceptable level of safety is being maintained.

       The MEL may not deviate from requirements of the AFM limitations

       section, emergency procedures or airworthiness directive unless the

       airworthiness directive or AFM provides otherwise.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 21-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

| 23-1 Cabin Air            | 2  | 0  | *                                     |

|      Recirculation        |    |    |                                       |

|      Systems              |    |    |                                       |

|                           |    |    |                                       |

| 23-2 Cabin Air            | 2  | 0  | *                                     |

|      Recirculation        |    |    |                                       |

|      System FAULT Lights  |    |    |                                       |

|                           |    |    |                                       |

| 26-1 Avionics Rack        | 1  | 0  | *May be inoperative provided:         |

|      Cooling Fan          |    |    |      a) Outside Air Temperature       |

|                           |    |    |         (OAT) is less than 35         |

|                           |    |    |         degrees C and                 |

|                           |    |    |      b) Ground operations are         |

|                           |    |    |         limited to 30 minutes or      |

|                           |    |    |         less.                         |

|                           |    |    |                                       |

| 26-2 AHRS Cooling Fan     | 1  | 0  | *May be inoperative provided:         |

|                           |    |    |      a) Outside Air Temperature       |

|                           |    |    |         (OAT) is less than 35         |

|                           |    |    |         degrees C and                 |

|                           |    |    |      b) Ground operations are         |

|                           |    |    |         limited to 30 minutes or      |

|                           |    |    |         less.                         |

|                           |    |    |                                       |

| 26-3 Instrument Cooling   | 1  | 0  | *May be inoperative provided:         |

|      Fan                  |    |    |      a) Outside Air Temperature       |

|                           |    |    |         (OAT) is less than 35         |

|                           |    |    |         degrees C and                 |

|                           |    |    |      b) Ground operations are         |

|                           |    |    |         limited to 30 minutes or      |

|                           |    |    |         less.                         |

|                           |    |    |                                       |

| 26-4 Avionics Cooling     | 1  | 0  | *(M)May be inoperative provided       |

|      Fan INOP Light       |    |    | maintenance procedures are            |

|                           |    |    | established to determine that all     |

|                           |    |    | three avionics systems cooling fans   |

|                           |    |    | are operating normally while on the   |

|                           |    |    | ground.                               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 21-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| AIR CONDITIONING          |    |    |                                       |

|                           |    |    |                                       |

| 30-1 Pressurization       | 1  | 0  | *(M)(O)May be inoperative provided:   |

|      System               |    |    |       a) Maintenance procedures are   |

|                           |    |    |          established to secure both   |

|                           |    |    |          outflow valves OPEN,         |

|                           |    |    |       b) Operations procedures are    |

|                           |    |    |          established for operating    |

|                           |    |    |          aircraft unpressurized and   |

|                           |    |    |       c) Aircraft is operated at      |

|                           |    |    |          10,000 feet MSL altitude     |

|                           |    |    |          or below.                    |

|                           |    |    |                                       |

| 31-1 Automatic Cabin      | 1  | 0  | *May be inoperative provided:         |

|      Pressurization       |    |    |     a) Manual Cabin Pressurization    |

|      Control System       |    |    |        Control is operative,          |

|                           |    |    |     b) Cabin Altitude Indication      |

|                           |    |    |        is operative,                  |

|                           |    |    |     c) Cabin Rate-of-Climb            |

|                           |    |    |        Indication is operative,       |

|                           |    |    |     d) Cabin Differential Pressure    |

|                           |    |    |        Indication is operative and    |

|                           |    |    |     e) Autopilot System is            |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 21-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

| 33-1 Cabin Rate/Cabin     |    |    |                                       |

|      Altitude/Cabin       |    |    |                                       |

|      Differential         |    |    |                                       |

|      Pressure Indication  |    |    |                                       |

|      System               |    |    |                                       |

|                           |    |    |                                       |

|     1) Cabin Rate-of-     | 1  | 0  | *May be inoperative provided all      |

|        Climb Indication   |    |    | other components of the               |

|                           |    |    | Pressurization Control and            |

|                           |    |    | Indication Systems are operative.     |

|                           |    |    |                                       |

|    2) Cabin Altitude      | 1  | 0  | *(O)May be inoperative provided:      |

|       Indication          |    |    |     a) Cabin Differential Pressure    |

|                           |    |    |        portion of the indicator is    |

|                           |    |    |        operative and                  |

|                           |    |    |     b) A chart is provided to         |

|                           |    |    |        convert differential           |

|                           |    |    |        pressure to cabin altitude     |

|                           |    |    |        and operations procedures      |

|                           |    |    |        are established for its use.   |

|                           |    |    |                                       |

|      3) Cabin             | 1  | 0  | *(O)May be inoperative provided:      |

|         Differential      |    |    |     a) Cabin Altitude portion of      |

|         Pressure          |    |    |        the Indicator is operative     |

|         Indication        |    |    |        and                            |

|                           |    |    |     b) A chart is provided to         |

|                           |    |    |        convert cabin altitude to      |

|                           |    |    |        cabin differential pressure    |

|                           |    |    |        and operations procedures      |

|                           |    |    |        are established for its use.   |

|                           |    |    |                                       |

| 33-2 Cabin Pressurization | 1  | 0  | *(O)May be inoperative provided:      |

|      Control FAULT Light  |    |    |     a) All other portions of the      |

|                           |    |    |        Cabin Pressurization Control   |

|                           |    |    |        and Indication Systems are     |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Cabin Altitude Warning         |

|                           |    |    |        System is operative and        |

|                           |    |    |     c) Operations procedures are      |

|                           |    |    |        established to monitor the     |

|                           |    |    |        Cabin Pressurization System.   |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 21-4     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| AIR CONDITIONING          |    |    |                                       |

|                           |    |    |                                       |

| 33-3 CABIN ALT Warning    | 1  | 0  | *(O)May be inoperative provided:      |

|      Light                |    |    |     a) All other portions of the      |

|                           |    |    |        Cabin Pressurization Control   |

|                           |    |    |        and Indication Systems are     |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Cabin Altitude Warning         |

|                           |    |    |        System is operative and        |

|                           |    |    |     c) Operations procedures are      |

|                           |    |    |        established to monitor the     |

|                           |    |    |        Cabin Pressurization System.   |

|                           |    |    |                                       |

| 41-1 Flight Deck Heater   | 1  | 0  | *                                     |

|                           |    |    |                                       |

| 41-2 Flight Deck Heater   | 1  | 0  | *                                     |

|      ON Light             |    |    |                                       |

|                           |    |    |                                       |

| 52-1 Pack FAULT Lights    | 2  | 1  | *(M)One may be inoperative            |

|                           |    |    | provided:                             |

|                           |    |    |     a) Maintenance procedures are     |

|                           |    |    |        established to verify Fault    |

|                           |    |    |        Aural Warning System is        |

|                           |    |    |        operative and                  |

|                           |    |    |     b) No other FAULT lights are      |

|                           |    |    |        inoperative.                   |

|                           |    |    |                                       |

| 60-1 Cabin and Flight     |    |    |                                       |

|      Deck Temperature     |    |    |                                       |

|      Control Systems      |    |    |                                       |

|                           |    |    |                                       |

|      1) Automatic         | 2  | 0  | *Both systems may be inoperative      |

|                           |    |    | provided associated Manual            |

|                           |    |    | Temperature Control System is         |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|      2) Manual            | 2  | 0  | *Both may be inoperative provided     |

|                           |    |    | associated Automatic Temperature      |

|                           |    |    | Control System is operative.          |

|                           |    |    |                                       |

| 63-1 Cockpit/Cabin        | 1  | 0  | *                                     |

|      Temperature Control  |    |    |                                       |

|      Display              |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 22-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22 AUTO FLIGHT            |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Autopilot System     | 1  | 0  | *May be inoperative provided:         |

|                           |    |    |     a) Automatic Cabin                |

|                           |    |    |        Pressurization Control         |

|                           |    |    |        System is operative and        |

|                           |    |    |     b) Approach minimums do not       |

|                           |    |    |        depend on the use of the       |

|                           |    |    |        Autopilot.                     |

|                           |    |    |                                       |

| 11-2 Autopilot/Yaw Damper | 2  | 0  | *Both may be inoperative  provided    |

|      Control Column       |    |    | Autopilot and Yaw Damper Systems      |

|      Manual Disconnect    |    |    | are not used.                         |

|      Switches             |    |    |                                       |

|                           |    |    |                                       |

| 11-3 Yaw Damper System    | 1  | 0  | *May be inoperative provided          |

|                           |    |    | Autopilot/Yaw Damper Systems are      |

|                           |    |    | considered inoperative.               |

|                           |    |    |                                       |

| 11-4 AFCS Status          | 1  | 0  | *May be inoperative provided          |

|      Indication Panel     |    |    | Autopilot/Yaw Damper Systems are      |

|                           |    |    | considered inoperative and not        |

|                           |    |    | used.                                 |

|                           |    |    |                                       |

| 11-5 Autopilot Command    | 2  | 1  | *One may be inoperative provided      |

|      Select Switches      |    |    | affected Autopilot Command Select     |

|                           |    |    | is not used.                          |

|                           |    |    |                                       |

|                           | 2  | 0  | *Both may be inoperative provided     |

|                           |    |    | Autopilot System is considered        |

|                           |    |    | inoperative and is not used.          |

|                           |    |    |                                       |

| 11-6 Autopilot Engage     | 1  | 0  | *May be inoperative provided          |

|      Switch Indication    |    |    | Autopilot System is considered        |

|                           |    |    | inoperative and not used.             |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 23-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Communications       | -  | -  | *As required by FAR.                  |

|      Systems (VHF, HF,    |    |    |                                       |

|      UHF)                 |    |    |                                       |

|                           |    |    |                                       |

| 21-1 Selective Call       | 1  | 0  | *(O)May be inoperative provided:      |

|      System (SELCAL)      |    |    |     a) Operations procedures are      |

|                           |    |    |        established which do not       |

|                           |    |    |        depend on its use.             |

|                           |    |    |               OR                      |

|                           |    |    |     b) Flight Crew continuously       |

|                           |    |    |        monitors appropriate radio     |

|                           |    |    |        frequencies.                   |

|                           |    |    |                                       |

| 22-1 ARINC Communications | 1  | 0  | *(O)May be inoperative provided       |

|      Addressing and       |    |    | operations procedures are             |

|      Reporting  System    |    |    | established that do not depend on     |

|      (ACARS)              |    |    | ACARS for the operations conducted.   |

|                           |    |    |                                       |

| 31-1 Passenger Address    |    |    |                                       |

|      (PA) System          |    |    |                                       |

|                           |    |    |                                       |

|     1) Passenger          | 1  | 0  | *(O)May be inoperative provided:      |

|        Configuration      |    |    |     a) Cabin Interphone System is     |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Flight Attendant Call System   |

|                           |    |    |        is operative,                  |

|                           |    |    |     c) Alternate, normal and          |

|                           |    |    |        emergency operations           |

|                           |    |    |        procedures are established     |

|                           |    |    |        and used and                   |

|                           |    |    |     d) Aircraft is repaired within    |

|                           |    |    |        15 hours time in service for   |

|                           |    |    |        domestic flights or 25 hours   |

|                           |    |    |        time in service for            |

|                           |    |    |        international flights.         |

|                           |    |    |                                       |

|      2) Cargo             | 1  | 0  | *                                     |

|         Configuration     |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 23-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

| 41-1 Cabin Interphone     | 1  | 0  | *(O)May be inoperative provided:      |

|      System               |    |    |     a) Passenger Address System is    |

|                           |    |    |        operative and                  |

|                           |    |    |     b) Alternate normal and           |

|                           |    |    |        emergency operations           |

|                           |    |    |        procedures are established     |

|                           |    |    |        and used.                      |

|                           |    |    |                                       |

| 42-1 Crewmember Alerting  |    |    |                                       |

|      Systems              |    |    |                                       |

|      (Crew Call Light/    |    |    |                                       |

|      Chime)               |    |    |                                       |

|                           |    |    |                                       |

|      1) Flight Deck Call  | 1  | 0  | *May be inoperative provided Flight   |

|         Light             |    |    | Deck Crew Call Chime is operative.    |

|                           |    |    |                                       |

|      2) Flight Attendant  | 1  | 0  | *May be inoperative provided:         |

|         Call Light        |    |    |     a) Passenger Address System is    |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Flight Attendant Call Chime    |

|                           |    |    |        is operative and               |

|                           |    |    |     c) Affected Light is not used     |

|                           |    |    |        for Lavatory Smoke Detector    |

|                           |    |    |        Alerting.                      |

|                           |    |    |                                       |

|      3) Flight Attendant  | 1  | 0  | *May be inoperative provided:         |

|         Call Chime        |    |    |     a) Passenger Address System is    |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Flight Attendant Call Light    |

|                           |    |    |        is operative and               |

|                           |    |    |     c) Affected Chime is not used     |

|                           |    |    |        for Lavatory Smoke Detector    |

|                           |    |    |        Alerting.                      |

|                           |    |    |                                       |

| 51-1 Oxygen Mask          | 3  | 2  | *One may be inoperative provided      |

|      Microphones          |    |    | one is operative for each pilot.      |

|                           |    |    |                                       |

| 51-2 Cockpit Microphones  | -  | 2  | *May be inoperative provided one      |

|      (Boom and Hand-held) |    |    | microphone (boom or hand-held) is     |

|                           |    |    | operative for each flight             |

|                           |    |    | crewmember.                           |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 23-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

| 51-3 Cockpit Headsets     | -  | -  | *May be inoperative provided one is   |

|                           |    |    | operative for each occupied flight    |

|                           |    |    | crew position.                        |

|                           |    |    |                                       |

| 51-4 Audio Selector       |    |    |                                       |

|      Panels (Cockpit)     |    |    |                                       |

|                           |    |    |                                       |

|      1) Normal Amplifiers | 3  | 0  | *All may be inoperative provided      |

|                           |    |    | affected panel's Alternate            |

|                           |    |    | Amplifier is operative.               |

|                           |    |    |                                       |

|      2) Alternate         | 3  | 0  | *All may be inoperative provided      |

|         Amplifiers        |    |    | affected panel's Normal Amplifier     |

|                           |    |    | is operative.                         |

|                           |    |    |                                       |

| 51-5 Flight Deck Speakers | 2  | 0  | *Both may be inoperative provided     |

|                           |    |    | an operative headset is provided      |

|                           |    |    | for and used by each person on        |

|                           |    |    | flight deck duty.                     |

|                           |    |    |                                       |

| 51-6 Interphone/Radio     |    |    |                                       |

|      Transceiver(IC/RT)   |    |    |                                       |

|      Selector Switches    |    |    |                                       |

|                           |    |    |                                       |

|      1) Control Wheel     | 2  | 0  | *Both may be inoperative provided:    |

|                           |    |    |      a) Flight Deck Interphone        |

|                           |    |    |         System is operative and       |

|                           |    |    |      b) Associated hand-held          |

|                           |    |    |         microphone is operative.      |

|                           |    |    |                                       |

|      2) Audio Selector    | 3  | 0  | *All may be inoperative provided      |

|         Panel             |    |    | Flight Deck Interphone System is      |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 23-4     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 23 COMMUNICATIONS         |    |    |                                       |

|                           |    |    |                                       |

| 71-1 Cockpit Voice        | 1  | -  | *(M)May be inoperative provided:      |

|      Recorder (CVR)       |    |    |        a) Flight Data Recorder        |

|      System               |    |    |           (FDR) System is operative   |

|                           |    |    |           and                         |

|                           |    |    |        b) Maintenance procedures      |

|                           |    |    |           are established to          |

|                           |    |    |           appropriately secure or     |

|                           |    |    |           deactivate CVR.             |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 24-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

| 21-1 Generator FAULT      | 2  | 1  | *(O)One may be inoperative            |

|      Lights               |    |    | provided:                             |

|                           |    |    |     a) Voltage and frequency of       |

|                           |    |    |        affected generator is          |

|                           |    |    |        checked after each engine      |

|                           |    |    |        start and                      |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established to monitor the     |

|                           |    |    |        loadmeter of the affected      |

|                           |    |    |        generator.                     |

|                           |    |    |                                       |

| 22-1 Auto AC X-Feed       | 1  | 0  | *(M)May be inoperative provided:      |

|      System               |    |    |     a) Maintenance procedures are     |

|                           |    |    |        established to verify both     |

|                           |    |    |        AC busses are operative and    |

|                           |    |    |        independent,                   |

|                           |    |    |     b) Aircraft is operated in        |

|                           |    |    |        day VMC and                    |

|                           |    |    |     c) Aircraft is not operated in    |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

| 25-1 BUS FAULT Light      | 1  | 0  | *May be inoperative provided GEN      |

|                           |    |    | FAULT Light and TRU FAULT Light are   |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

| 31-1 TRU FAULT Lights     | 2  | 1  | *(M)(O)One may be inoperative         |

|                           |    |    | provided:                             |

|                           |    |    |        a) Maintenance procedures      |

|                           |    |    |           are established to          |

|                           |    |    |           determine that affected     |

|                           |    |    |           TRU is operative by         |

|                           |    |    |           monitoring the loadmeter    |

|                           |    |    |           and                         |

|                           |    |    |        b) Operations procedures are   |

|                           |    |    |           established to monitor      |

|                           |    |    |           the loadmeter of            |

|                           |    |    |           affected TRU.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 24-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

| 32-1 DC X-FEED System     | 1  | 0  | *(O)May be inoperative provided:      |

|                           |    |    |     a) Operations procedures are      |

|                           |    |    |        established to verify that     |

|                           |    |    |        both D.C. Busses are           |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Aircraft is not operated in    |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions and                 |

|                           |    |    |     c) Aircraft is operated in day    |

|                           |    |    |        VMC.                           |

|                           |    |    |                                       |

| 32-2 DC X-FEED ON Light   | 1  | 0  | *                                     |

|                           |    |    |                                       |

| 33-1 Battery Charger      | 2  | 1  | *(M)One may be inoperative            |

|      FAULT Lights         |    |    | provided:                             |

|                           |    |    |     a) Affected battery charger       |

|                           |    |    |        system fault indicator on      |

|                           |    |    |        the Maintenance Test Panel     |

|                           |    |    |        is checked prior to each       |

|                           |    |    |        flight and does not indicate   |

|                           |    |    |        a fault status and             |

|                           |    |    |     b) Maintenance procedures are     |

|                           |    |    |        established to determine       |

|                           |    |    |        that affected battery          |

|                           |    |    |        charger is operative.          |

|                           |    |    |                                       |

| 41-1 External Power       | 1  | 0  | *(O)May be inoperative provided       |

|      AVAIL/ON Light       |    |    | operations procedures are             |

|                           |    |    | established to prevent aircraft       |

|                           |    |    | movement with external power          |

|                           |    |    | connected.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 25-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Crewmember Shoulder  | -  | -  | *As required by FAR.  If a harness    |

|      Harnesses            |    |    | becomes inoperative, the aircraft     |

|                           |    |    | may continue the  flight or series    |

|                           |    |    | of flights, but shall not depart an   |

|                           |    |    | airport where repairs or              |

|                           |    |    | replacements can be made.             |

|                           |    |    |                                       |

| 20-1 Flight Attendant     |    |    |                                       |

|      Seat (Single or      |    |    |                                       |

|      Dual position)       |    |    |                                       |

|                           |    |    |                                       |

|      1) Seats required by | -  | -  | *(M)(O)One single or dual position    |

|         FAR               |    |    | seat may be inoperative provided:     |

|                           |    |    |        a) Affected seat position(s)   |

|                           |    |    |           is not occupied,            |

|                           |    |    |        b) Flight attendant(s)         |

|                           |    |    |           displaced by inoperative    |

|                           |    |    |           seat position(s) occupies   |

|                           |    |    |           the passenger seat(s)       |

|                           |    |    |           most accessible to their    |

|                           |    |    |           assigned exit,              |

|                           |    |    |        c) Alternate operations        |

|                           |    |    |           procedures are              |

|                           |    |    |           established for displaced   |

|                           |    |    |           flight attendant(s),        |

|                           |    |    |        d) Folding type seat that      |

|                           |    |    |           will not stow               |

|                           |    |    |           automatically is stowed     |

|                           |    |    |           or secured in the           |

|                           |    |    |           retracted position,         |

|                           |    |    |        e) Passenger seat(s)           |

|                           |    |    |           assigned to flight          |

|                           |    |    |           attendant(s) is placarded   |

|                           |    |    |           "FOR FLIGHT ATTENDANT USE   |

|                           |    |    |           ONLY" and                   |

|                           |    |    |        f) Aircraft shall not depart   |

|                           |    |    |           an airport where repair     |

|                           |    |    |           can be made.                |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 25-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

| 20-1 Flight Attendant     |    |    |                                       |

|      Seat (Single or      |    |    |                                       |

|      Dual position)       |    |    |                                       |

|          Cont'd           |    |    | NOTE:  A folding seat that will not   |

|                           |    |    |        stow automatically is          |

|                           |    |    |        considered inoperative.        |

|                           |    |    |                                       |

| 2) Seats in excess of the | -  | 0  | *(M)All may be inoperative            |

|    number required by FAR |    |    | provided:                             |

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

|                           |    |    |        not occupied,                  |

|                           |    |    |     b) Folding type seat that will    |

|                           |    |    |        not stow automatically is      |

|                           |    |    |        stowed or secured in the       |

|                           |    |    |        retracted position.            |

|                           |    |    |                                       |

|                           |    |    | NOTE 1: A Folding 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.       |

|                           |    |    |                                       |

| 20-2 Flight Attendant     | -  | -  | *One may be inoperative provided      |

|      Seat Lap Belt        |    |    | associated Flight Attendant seat      |

|                           |    |    | position is considered inoperative.   |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 25-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

| 20-3 Passenger Seats      | -  | 0  | *(M)All may be inoperative            |

|                           |    |    | provided:                             |

|                           |    |    |      a) Maintenance procedures are    |

|                           |    |    |         established to                |

|                           |    |    |         appropriately secure or       |

|                           |    |    |         stow affected seat to not     |

|                           |    |    |         block emergency egress to     |

|                           |    |    |         an aisle or exit and          |

|                           |    |    |      b) Maintenance procedures are    |

|                           |    |    |         established to ensure that    |

|                           |    |    |         affected seat is blocked      |

|                           |    |    |         and placarded "DO NOT         |

|                           |    |    |         OCCUPY".                      |

|                           |    |    |                                       |

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

|                           |    |    |         lap belt is considered to     |

|                           |    |    |         be inoperative.               |

|                           |    |    |                                       |

|                           |    |    | NOTE 2: A seat with an inoperative    |

|                           |    |    |         recline mechanism is          |

|                           |    |    |         considered to be              |

|                           |    |    |         inoperative if the seat can   |

|                           |    |    |         not be secured in the         |

|                           |    |    |         upright position.             |

|                           |    |    |                                       |

|                           |    |    | NOTE 3: Inoperative seats do not      |

|                           |    |    |         affect the number of Flight   |

|                           |    |    |         Attendants required by FAR.   |

|                           |    |    |                                       |

| 20-4 Window Shades        | -  | 0  | *                                     |

|                           |    |    |                                       |

| 20-5 Overhead Storage Bin | -  | -  | *(M)May be inoperative provided:      |

|      Latches              |    |    |     a) Maintenance procedures are     |

|                           |    |    |        established to secure lid      |

|                           |    |    |        CLOSED and                     |

|                           |    |    |     b) Affected bin is not used for   |

|                           |    |    |        storage.                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 25-4     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

| 60-1 Flotation            | -  | -  | *May be inoperative provided          |

|      Equipment (Crew      |    |    | applicable FAR does not require       |

|      and Passenger)       |    |    | affected Flotation Equipment for      |

|                           |    |    | operation conducted.                  |

|                           |    |    |                                       |

| 60-2 Aircraft Emergency   | 1  | -  | *May be inoperative provided          |

|      Location Transmitter |    |    | applicable FAR does not require       |

|      (ELT)                |    |    | affected Emergency Location           |

|                           |    |    | Transmitter for the operation         |

|                           |    |    | conducted.                            |

|                           |    |    |                                       |

| 70-1 "Fasten Seat Belt    | -  | -  | *One or more signs or placards may    |

|      While Seated"Sign    |    |    | be illegible or missing provides a    |

|      or Placard           |    |    | legible sign or placard is readable   |

|                           |    |    | from each occupied passenger seat.    |

|                           |    |    |                                       |

| 70-2 Cabin Emergency      | -  | 0  | *All may be inoperative provided      |

|      Flashlight/Holder    |    |    | cabin crewmember assigned to          |

|      (Flight Attendant    |    |    | affected position has a operative     |

|      Station)             |    |    | flashlight readily available.         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 26-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Engine Fire          |    |    |                                       |

|      Detection Systems    |    |    |                                       |

|      (Detection Loops)    |    |    |                                       |

|                           |    |    |                                       |

|     1) Detection Loops    | 4  | 2  | *One complete loop (1 or 2) on each   |

|                           |    |    | engine may be inoperative provided:   |

|                           |    |    |     a) Maintenance procedures are     |

|                           |    |    |        established to determine       |

|                           |    |    |        that remaining detection       |

|                           |    |    |        loop is operative and          |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established to insure          |

|                           |    |    |        affected Detection Loop is     |

|                           |    |    |        switched OFF prior to each     |

|                           |    |    |        flight.                        |

|                           |    |    |                                       |

|     2) Loop Test Function | 4  | 2  | *One Loop Test Function (1 or 2)      |

|                           |    |    | may be inoperative on each engine     |

|                           |    |    | provided associated Detection         |

|                           |    |    | Loop(s) are also inoperative.         |

|                           |    |    |                                       |

| 11-2 Fuel Lever Fire      | 2  | 0  | *                                     |

|      Detection Lights     |    |    |                                       |

|                           |    |    |                                       |

| 13-1 Cargo Compartment    | 2  | 0  | *Both may be inoperative provided     |

|      Smoke Detection      |    |    | nothing is carried in the affected    |

|      Systems              |    |    | Cargo Compartment.                    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 26-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

| 13-2 Lavatory Smoke       | -  | -  | *(M)(O)For each Lavatory, the         |

|      Detection Systems    |    |    | smoke detection system may be         |

|                           |    |    | inoperative provided:                 |

|                           |    |    |        a) Lavatory Fire               |

|                           |    |    |           Extinguisher system         |

|                           |    |    |           operates normally.          |

|                           |    |    |                   OR                  |

|                           |    |    |        b) Lavatory waste receptacle   |

|                           |    |    |           is empty,                   |

|                           |    |    |        c) Lavatory door is locked     |

|                           |    |    |           CLOSED and placarded,       |

|                           |    |    |           "INOPERATIVE- DO NOT        |

|                           |    |    |           ENTER",                     |

|                           |    |    |        b) 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.         |

|                           |    |    |                                       |

| 23-1 Engine Fire          | 4  | 0  | *(M)All may be inoperative provided   |

|      Extinguisher AGENT   |    |    | affected bottle weight is checked     |

|      "LOW PRESS" Lights   |    |    | prior to the first flight of the      |

|                           |    |    | day.                                  |

|                           |    |    |                                       |

| 24-1 Portable Fire        | -  | -  | *May be inoperative provided          |

|      Extinguishers        |    |    | applicable FAR does not require       |

|                           |    |    | affected Portable Fire Extinguisher   |

|                           |    |    | for the operation conducted.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 26-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

| 24-2 Lavatory Fire        | -  | -  | *(M)(O)For each lavatory, the         |

|      Extinguisher Systems |    |    | fire extinguisher system may be       |

|                           |    |    | inoperative provided:                 |

|                           |    |    |        a) Lavatory Smoke Detector     |

|                           |    |    |           operates normally,          |

|                           |    |    |                 OR                    |

|                           |    |    |        b) Lavatory waste receptacle   |

|                           |    |    |           is empty                    |

|                           |    |    |        c) Lavatory door is locked     |

|                           |    |    |           CLOSED and placarded,       |

|                           |    |    |           "INOPERATIVE-DO NOT         |

|                           |    |    |           ENTER" and                  |

|                           |    |    |        d) Lavatory is not used        |

|                           |    |    |           for any purpose.            |

|                           |    |    |                                       |

|                           |    |    | NOTE 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: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 27-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 27  FLIGHT CONTROLS       |    |    |                                       |

|                           |    |    |                                       |

| 21-1 Rudder Pedal         | 2  | 1  | *(M)One may be inoperative            |

|      Adjustment Systems   |    |    | provided:                             |

|                           |    |    |     a) Pedals are adjusted and        |

|                           |    |    |        secured by an approved         |

|                           |    |    |        maintenance procedure in a     |

|                           |    |    |        suitable position for the      |

|                           |    |    |        individual crewmember          |

|                           |    |    |        assigned to that seat and      |

|                           |    |    |     b) Crewmember for which pedals    |

|                           |    |    |        are adjusted occupies          |

|                           |    |    |        affected seat.                 |

|                           |    |    |                                       |

| 56-1 Flap Position        | 1  | 0  | *(O)May be inoperative provided:      |

|      Indicating System    |    |    |     a) It is determined that flaps    |

|                           |    |    |        are operative through their    |

|                           |    |    |        full range,                    |

|                           |    |    |     b) Visual inspection before       |

|                           |    |    |        each takeoff verifies that     |

|                           |    |    |        both flaps are in the          |

|                           |    |    |        takeoff position and           |

|                           |    |    |     c) Operations procedures are      |

|                           |    |    |        established to verify flap     |

|                           |    |    |        disagreement alerting system   |

|                           |    |    |        is operative.                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 28-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 28  FUEL                  |    |    |                                       |

|                           |    |    |                                       |

| 16-1 Inboard Tank Fuel    | 2  | 0  | *(O)Both may be inoperative           |

|      Transfer System      |    |    | provided:                             |

|                           |    |    |     a) All fuel in affected inboard   |

|                           |    |    |        tank is included in aircraft   |

|                           |    |    |        zero fuel weight and           |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established to maintain fuel   |

|                           |    |    |        asymmetry within limits.       |

|                           |    |    |                                       |

| 16-2 Collector Tank LO    | 2  | 0  | *(O)Both may be inoperative           |

|      LEVEL Indicating     |    |    | provided:                             |

|      System for Inboard   |    |    |     a) Fuel is not carried in         |

|      Tanks                |    |    |        affected inboard tank and      |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established to maintain fuel   |

|                           |    |    |        asymmetry within limits.       |

|                           |    |    |                                       |

| 16-3 Inboard Tank Auto    | 2  | 0  | *May be inoperative provided:         |

|      Feed Systems         |    |    |     a) Affected fuel transfer         |

|                           |    |    |        system is operated in manual   |

|                           |    |    |        and                            |

|                           |    |    |     b) Fuel Quantity Indicating       |

|                           |    |    |        System is operative.           |

|                           |    |    |                                       |

| 21-1 Single Point         | 1  | 0  | *(M)May be inoperative provided       |

|      Pressure Refueling   |    |    | alternate approved fueling            |

|      System               |    |    | procedures are established and        |

|                           |    |    | used.                                 |

|                           |    |    |                                       |

| 22-1 Fuel Boost Pumps     | 4  | 3  | *One may be inoperative               |

|                           |    |    | provided:                             |

|                           |    |    |     a) Jet A-1 type fuel is used,     |

|                           |    |    |     b) Fuel Crossfeed System is       |

|                           |    |    |        operative and                  |

|                           |    |    |     c) Aircraft is operated at        |

|                           |    |    |        FL250 or below.                |

|                           |    |    |                                       |

| 22-2 Fuel Boost Pump      | 4  | 3  | *One may be inoperative provided      |

|      Fault Lights         |    |    | associated Fuel Boost Pump is         |

|                           |    |    | considered inoperative.               |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 28-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 28  FUEL                  |    |    |                                       |

|                           |    |    |                                       |

| 22-3 Fuel System Shut-off | 2  | 0  | *Both may be inoperative provided     |

|      SHUT lights          |    |    | Flow Bar Indication is operative.     |

|                           |    |    |                                       |

| 23-1 Fuel Crossfeed       | 2  | 1  | *One may be inoperative provided      |

|      Valves               |    |    | affected valve is deactivated OPEN.   |

|                           |    |    |                                       |

| 23-2 Fuel Crossfeed ON    | 1  | 0  | *(M)May be inoperative provided       |

|      Light                |    |    | maintenance procedures are            |

|                           |    |    | established to verify Flowbar         |

|                           |    |    | indication is operative prior to      |

|                           |    |    | each flight.                          |

|                           |    |    |                                       |

| 41-1 Cockpit Fuel         |    |    |                                       |

|      Quantity Displays    |    |    |                                       |

|                           |    |    |                                       |

|      1) Outboard Tanks    | 2  | 1  | *(M)One may be inoperative            |

|                           |    |    | provided:                             |

|                           |    |    |     a) Fuel quantity in the           |

|                           |    |    |        affected tank is determined    |

|                           |    |    |        by an alternate approved       |

|                           |    |    |        procedure prior to each        |

|                           |    |    |        flight and                     |

|                           |    |    |     b) Fuel Quantity Totalizer is     |

|                           |    |    |        operative and                  |

|                           |    |    |     d) Both Fuel Used Indicators      |

|                           |    |    |        are operative.                 |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 28-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 28  FUEL                  |    |    |                                       |

|                           |    |    |                                       |

| 41-1 Cockpit Fuel         |    |    |                                       |

|      Quantity Displays    |    |    |                                       |

|      (Cont'd)             |    |    |                                       |

|                           |    |    |                                       |

|     2) Inboard Tanks      | 2  | 1  | *(M)One may be inoperative            |

|                           |    |    | provided:                             |

|                           |    |    |     a) Outboard Tank Fuel Quantity    |

|                           |    |    |        asymmetry is limited to 400    |

|                           |    |    |        pounds until the inboard       |

|                           |    |    |        tanks are empty,               |

|                           |    |    |     b) Fuel quantity in the           |

|                           |    |    |        affected tank is determined    |

|                           |    |    |        by an alternate approved       |

|                           |    |    |        maintenance procedure prior    |

|                           |    |    |        to each flight,                |

|                           |    |    |     c) Auto Feed Transfer System      |

|                           |    |    |        on affected side is            |

|                           |    |    |        operative and                  |

|                           |    |    |     d) Both Outboard Tank Fuel        |

|                           |    |    |        Quantity Displays are          |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|                           | 2  | 0  | *(M)Both may be inoperative           |

|                           |    |    | provided both Inboard Fuel Tanks      |

|                           |    |    | are determined to be empty.           |

|                           |    |    |                                       |

| 41-2 Fuel Quantity        | 1  | 0  | *May be inoperative provided          |

|      Totalizer Indication |    |    | Cockpit Fuel Quantity Displays are    |

|      System               |    |    | operative.                            |

|                           |    |    |                                       |

| 42-1 Magnetic Fuel Level  | -  | 0  | *All may be inoperative provided      |

|      Indicator Sticks     |    |    | all Cockpit Fuel Quantity Displays    |

|                           |    |    | are operative.                        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 29-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 29  HYDRAULIC POWER       |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Hydraulic System     | 1  | 0  | *May be inoperative provided all      |

|      Accumulator          |    |    | hydraulic system indicators are       |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    | NOTE: Indicator on hydraulic ground   |

|                           |    |    |       service panel is considered     |

|                           |    |    |       part of the hydraulic system    |

|                           |    |    |       accumulator.                    |

|                           |    |    |                                       |

| 11-2 Hydraulic System     | 1  | 0  | *May be inoperative provided          |

|      Electric Pump        |    |    | procedures do not depend on its       |

|                           |    |    | use.                                  |

|                           |    |    |                                       |

| 11-3 Hydraulic System     | 1  | 0  | *                                     |

|      Electric Pump ON     |    |    |                                       |

|      Light                |    |    |                                       |

|                           |    |    |                                       |

| 31-1 Cockpit Hydraulic    | 1  | 0  | *(M)May be inoperative provided:      |

|      Quantity Indicating  |    |    |     a) Hydraulic Low Quantity Light   |

|      System               |    |    |        is operative and               |

|                           |    |    |     b) Quantity in the hydraulic      |

|                           |    |    |        reservoir is checked on the    |

|                           |    |    |        ground panel quantity          |

|                           |    |    |        indicator or on the            |

|                           |    |    |        hydraulic reservoir sight      |

|                           |    |    |        glass prior to each flight.    |

|                           |    |    |                                       |

| 31-2 Hydraulic LO QTY     | 1  | 0  | *(O)May be inoperative  provided:     |

|      Light                |    |    |     a) Hydraulic Quantity             |

|                           |    |    |        Indicating System is           |

|                           |    |    |        operative and                  |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established to monitor the     |

|                           |    |    |        Hydraulic System Quantity.     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 29-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 29  HYDRAULIC POWER       |    |    |                                       |

|                           |    |    |                                       |

| 32-1 Hydraulic Reservoir  | 1  | 0  | *(O)May be inoperative provided:      |

|      Pressurization       |    |    |     a) All other Hydraulic System     |

|      System               |    |    |        functions are operative,       |

|                           |    |    |     b) Hydraulic System Pressure      |

|                           |    |    |        Indicating System is           |

|                           |    |    |        operative and                  |

|                           |    |    |     c) Procedures are established     |

|                           |    |    |        to monitor Hydraulic System    |

|                           |    |    |        pressure.                      |

|                           |    |    |                                       |

| 32-2 Hydraulic TANK PR    | 1  | 0  | *(O)May be inoperative provided:      |

|      Light                |    |    |     a) All other Hydraulic System     |

|                           |    |    |        functions are operative,       |

|                           |    |    |     b) Hydraulic System Pressure      |

|                           |    |    |        Indicating System is           |

|                           |    |    |        operative and                  |

|                           |    |    |     c) Procedures are established     |

|                           |    |    |        to monitor Hydraulic System    |

|                           |    |    |        pressure.                      |

|                           |    |    |                                       |

| 33-1 Hydraulic System     | 1  | 0  | *                                     |

|      Pressure Display     |    |    |                                       |

|                           |    |    |                                       |

| 35-1 Hydraulic Reservoir  | 1  | 0  | *May be inoperative provided all      |

|      OVHT Light           |    |    | other hydraulic system indicators     |

|                           |    |    | are operative.                        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 30-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Airframe De-Icing    | 1  | 0  | *May be inoperative provided          |

|      System (Airfoil)     |    |    | aircraft is not operated in known     |

|                           |    |    | or forecast icing conditions.         |

|                           |    |    |                                       |

|      1) Manual Mode       | 1  | 0  | *May be inoperative provided          |

|                           |    |    | Automatic Mode is operative.          |

|                           |    |    |                                       |

|      2) Automatic Mode    | 1  | 0  | *May be inoperative provided          |

|                           |    |    | Manual Mode is operative.             |

|                           |    |    |                                       |

| 11-2 Inner Wing De-Icer   | 2  | 0  | *(M)Both may be inoperative           |

|      Boots                |    |    | provided affected Inner Wing          |

|                           |    |    | De-Icer Boot valve is deactivated     |

|                           |    |    | CLOSED.                               |

|                           |    |    |                                       |

| 11-3 Airframe De-Icing    | 1  | 0  | *May be inoperative provided          |

|      System TIMER FAULT   |    |    | Airframe De-Icing System is           |

|      Light                |    |    | operated in Manual Mode.              |

|                           |    |    |                                       |

| 13-1 Airframe De-Icing    | 1  | 0  | *(M)(O)May be inoperative             |

|      LOW PRESS Light      |    |    | provided:                             |

|                           |    |    |        a) Maintenance procedures      |

|                           |    |    |           are established to verify   |

|                           |    |    |           De-Icing system is          |

|                           |    |    |           operative and               |

|                           |    |    |        b) Operations procedures are   |

|                           |    |    |           established to monitor      |

|                           |    |    |           De-Icing System during      |

|                           |    |    |           icing conditions.           |

|                           |    |    |                                       |

| 21-1 Engine Anti-Icing    | 2  | 1  | *One may be inoperative provided:     |

|      Systems              |    |    |     a) Aircraft is not operated       |

|                           |    |    |        in visible moisture with       |

|                           |    |    |        static air temperature         |

|                           |    |    |        (SAT) below +4 degrees C,      |

|                           |    |    |     b) Aircraft is not operated in    |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions and                 |

|                           |    |    |     c) Aircraft is operated in VMC    |

|                           |    |    |        only.                          |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 30-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 30 ICE AND RAIN           |    |    |                                       |

|    PROTECTION             |    |    |                                       |

|                           |    |    |                                       |

| 21-2 Engine Anti-Icing    | 2  | 0  | *                                     |

|      FAU L Lights         |    |    |                                       |

|                           |    |    |                                       |

| 31-1 Upper Right Hand     | 1  | 0  | *May be inoperative provided:         |

|      Pitot Heater System  |    |    |     a) Aircraft is not operated       |

|                           |    |    |        in visible moisture with       |

|                           |    |    |        static air temperature (SAT)   |

|                           |    |    |        below +4 degrees C,            |

|                           |    |    |     b) Aircraft is not operated       |

|                           |    |    |        in known or forecast icing     |

|                           |    |    |        conditions and                 |

|                           |    |    |     c) All other elements of the      |

|                           |    |    |        Pitot Heat System are          |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

| 31-2 Pitot Heat INOP      | 4  | 3  | *(M)One may be inoperative            |

|      Lights (Overhead     |    |    | provided:                             |

|      Panel)               |    |    |     a) Affected Pitot Heater is       |

|                           |    |    |        determined to be operative     |

|                           |    |    |        by an approved maintenance     |

|                           |    |    |        procedure prior to each        |

|                           |    |    |        flight.                        |

|                           |    |    |                 OR                    |

|                           |    |    |     b) Associated Upper Right Hand    |

|                           |    |    |        Pitot Heater is inoperative.   |

|                           |    |    |                                       |

| 32-1 Angle-of Attack Vane | 1  | 0  | *(M)May be inoperative provided:      |

|      Heater System        |    |    |     a) Aircraft is not operated       |

|                           |    |    |        into known or forecast icing   |

|                           |    |    |        conditions and                 |

|                           |    |    |     b) Aircraft is not operated in    |

|                           |    |    |        visible moisture with the      |

|                           |    |    |        static air temperature (SAT)   |

|                           |    |    |        below +4 degrees C.            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 30-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| 32-2 Angle-of-Attack      | 1  | 0  | *May be inoperative provided:         |

|      Heater FAULT Light   |    |    |     a) Aircraft is not operated       |

|                           |    |    |        into known or forecast icing   |

|                           |    |    |        conditions and                 |

|                           |    |    |     b) Aircraft is not operated in    |

|                           |    |    |        visible moisture with the      |

|                           |    |    |        static air temperature (SAT)   |

|                           |    |    |        below +4 degrees C.            |

|                           |    |    |                                       |

| 41-1 Window Heat Systems  | 2  | 1  | *One may be inoperative provided      |

|                           |    |    | aircraft is not operated in known     |

|                           |    |    | or forecast icing conditions.         |

|                           |    |    |                                       |

|                           |    |    | NOTE: See AFM Limitations.            |

|                           |    |    |                                       |

| 42-1 Windshield Wiper     | 1  | 0  | *May be inoperative provided          |

|      System               |    |    | aircraft is  not operated in          |

|                           |    |    | precipitation within 5 miles of the   |

|                           |    |    | airport of takeoff or intended        |

|                           |    |    | landing.                              |

|                           |    |    |                                       |

| 43-1 Windshield and       | 2  | 0  | *Both may be inoperative provided     |

|      Direct Vision Window |    |    | both Window Heat Systems are          |

|      De-Misting Systems   |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 31-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 31  INDICATING/RECORDING  |    |    |                                       |

|     SYSTEMS               |    |    |                                       |

|                           |    |    |                                       |

| 21-1 Clocks               | -  | 1  | *(O)May be inoperative provided:      |

|      (Cockpit)            |    |    |     a) One clock displaying hours,    |

|                           |    |    |        minutes and seconds with a     |

|                           |    |    |        sweepsecond pointer or         |

|                           |    |    |        digital presentation is        |

|                           |    |    |        installed and operative on     |

|                           |    |    |        either pilot's instrument      |

|                           |    |    |        panel,                         |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established that do not        |

|                           |    |    |        depend on use of the           |

|                           |    |    |        affected clock and             |

|                           |    |    |     c) Affected clock is not needed   |

|                           |    |    |        to provide time data to any    |

|                           |    |    |        other required equipment.      |

|                           |    |    |                                       |

|                           |    |    | NOTE 1: Clock may be required to      |

|                           |    |    |         observe AFM Limitations for   |

|                           |    |    |         engine and other systems,     |

|                           |    |    |         for enroute and approach      |

|                           |    |    |         navigation and other          |

|                           |    |    |         procedures.                   |

|                           |    |    |                                       |

|                           |    |    | NOTE 2: Clock time may be needed      |

|                           |    |    |         for Digital Flight Data       |

|                           |    |    |         Recorder and other            |

|                           |    |    |         equipment.                    |

|                           |    |    |                                       |

| 31-1 Flight Data Recorder | 1  | -  | *(M)May be inoperative provided:      |

|      (FDR) System         |    |    |     a) Cockpit Voice Recorder (CVR)   |

|                           |    |    |        System is operative and        |

|                           |    |    |     b) Maintenance procedures are     |

|                           |    |    |        established to appropriately   |

|                           |    |    |        secure or deactivate FDR.      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 31-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 31  INDICATING/RECORDING  |    |    |                                       |

|     SYSTEMS               |    |    |                                       |

|                           |    |    |                                       |

| 51-1 Integrated Alerting  |    |    |                                       |

|      System               |    |    |                                       |

|                           |    |    |                                       |

|      1) Channels          | 2  | 1  | *One may be inoperative provided      |

|                           |    |    | ALERT SYS self test is performed      |

|                           |    |    | with satisfactory results prior to    |

|                           |    |    | each flight.                          |

|                           |    |    |                                       |

|      2) ALERTS SYS CHAN   | 1  | 0  | *May be inoperative provided:         |

|         FAIL Light        |    |    |     a) It is determined that both     |

|                           |    |    |        Integrated Alerting System     |

|                           |    |    |        Channels are operative prior   |

|                           |    |    |        to each flight and             |

|                           |    |    |     b) Central Annunciator Alert      |

|                           |    |    |        System FAULT Light is          |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 31-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 31  INDICATING/RECORDING  |    |    |                                       |

|     SYSTEMS               |    |    |                                       |

|                           |    |    |                                       |

| 51-2 Central Annunciator  |    |    |                                       |

|      Panel (CAP)          |    |    |                                       |

|                           |    |    |                                       |

|      1) Annunciator Light | -  | -  | *May be inoperative provided one      |

|         Bulbs             |    |    | light bulb is operative in each       |

|                           |    |    | annunciator on the CAP.               |

|                           |    |    |                                       |

|      2) Inhibit Light and | 1  | 0  | *May be inoperative provided:         |

|         Function          |    |    |     a) It is determined that all      |

|                           |    |    |        Integrated Alerts are          |

|                           |    |    |        operative and                  |

|                           |    |    |     b) Inhibit Cancel is selected     |

|                           |    |    |        and indicated.                 |

|                           |    |    |                                       |

|      3) Inhibit Cancel    | 1  | 0  | *(O)May be inoperative provided:      |

|         Light and         |    |    |     a) Inhibit Light and Function     |

|         Function          |    |    |        are operative and              |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established to insure          |

|                           |    |    |        Inhibit Light is               |

|                           |    |    |        extinguished after takeoff.    |

|                           |    |    |                                       |

|      4) Manual Back-Up    | 1  | 0  |                                       |

|         Light and         |    |    |                                       |

|         Function          |    |    |                                       |

|                           |    |    |                                       |

|      5) Integrated Alert  | 1  | 0  | *May be inoperative provided:         |

|         System FAULT      |    |    |     a) Both Integrated Alerting       |

|         Light             |    |    |        System Channels are            |

|                           |    |    |        operative and                  |

|                           |    |    |     b) Central Annunciator Panel      |

|                           |    |    |        ALERT SYS CHAN FAIL Light      |

|                           |    |    |        is operative.                  |

|                           |    |    |                                       |

| 51-3 Master Caution       | 2  | 1  | *One may be inoperative provided:     |

|      Lights               |    |    |     a) Master Caution aural alert     |

|                           |    |    |        is operative and               |

|                           |    |    |     b) All other discrete Caution     |

|                           |    |    |        Lights are operative.          |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 32-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 32  LANDING GEAR          |    |    |                                       |

|                           |    |    |                                       |

| 31-1 Landing Gear         | 1  | 0  | *May be inoperative provided:         |

|      Selector Downlock    |    |    |     a) The solenoid is in the         |

|      Solenoid             |    |    |        locked position and            |

|                           |    |    |     b) The override mechanism is      |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

| 31-2 Nose Gear Door       | 1  | 0  | *(M)May be inoperative provided:      |

|      Isolating Valve      |    |    |     a) Valve is secured in the        |

|                           |    |    |        deactivated position and       |

|                           |    |    |     b) Maintenance procedures are     |

|                           |    |    |        established to determine       |

|                           |    |    |        that the nose gear doors are   |

|                           |    |    |        operative and CLOSED.          |

|                           |    |    |                                       |

| 42-1 Nose Wheel Braking   | 2  | 0  | *(M)Both may be inoperative           |

|      Pads                 |    |    | provided maintenance procedures are   |

|                           |    |    | established to prevent inoperative    |

|                           |    |    | pads from damaging nose wheel         |

|                           |    |    | tires.                                |

|                           |    |    |                                       |

| 45-1 Anti-Skid System     | 1  | 0  | *(M)May be inoperative provided:      |

|                           |    |    |     a) Maintenance procedures         |

|                           |    |    |        are established to             |

|                           |    |    |        properly deactivate the        |

|                           |    |    |        system,                        |

|                           |    |    |     b) Landing Data is adjusted       |

|                           |    |    |        in accordance with AFM         |

|                           |    |    |        Performance Data and           |

|                           |    |    |     c) Anti-Skid System is OFF.       |

|                           |    |    |                                       |

| 45-2 Anti-Skid Test       | 1  | 0  | *(M)May be inoperative provided       |

|      Panel Annunciator    |    |    | Anti-Skid System is operative and     |

|                           |    |    | checked prior to each flight.         |

|                           |    |    |                                       |

| 61-1 Lower Nose Gear      | 1  | 0  | *                                     |

|      Position Indication  |    |    |                                       |

|      (Green) Light        |    |    |                                       |

|                           |    |    |                                       |

| 61-2 Landing Gear         | 1  | 0  | *                                     |

|      Selector Knob In     |    |    |                                       |

|      Transit Light (Blue) |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 33-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Cockpit and          | -  | -  | *May be inoperative provided:         |

|      Instrument Lighting  |    |    |     a) Flight Station emergency       |

|      Systems (Excluding   |    |    |        lighting is operative,         |

|      EFIS)                |    |    |     b) Sufficient lighting is         |

|                           |    |    |        operative to make each         |

|                           |    |    |        instrument, control and        |

|                           |    |    |        other device for which it is   |

|                           |    |    |        provided easily readable,      |

|                           |    |    |     c) Direct rays and reflections    |

|                           |    |    |        do not impair visibility       |

|                           |    |    |        either inside or outside the   |

|                           |    |    |        aircraft,                      |

|                           |    |    |     d) Lighting intensity can be      |

|                           |    |    |        controlled or is preset to a   |

|                           |    |    |        satisfactory level for the     |

|                           |    |    |        expected flight conditions     |

|                           |    |    |        and expected flight            |

|                           |    |    |        conditions and                 |

|                           |    |    |     e) Lighting configuration at      |

|                           |    |    |        dispatch is acceptable to      |

|                           |    |    |        the flight crew.               |

|                           |    |    |                                       |

| 20-1 Cabin Interior       | -  | -  | *May be inoperative provided:         |

|      Illumination         |    |    |     a) Cabin emergency lighting is    |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Sufficient lighting is         |

|                           |    |    |        operative for crew to          |

|                           |    |    |        perform required duties and    |

|                           |    |    |     c) Lighting configuration at      |

|                           |    |    |        dispatch is acceptable to      |

|                           |    |    |        flight crew.                   |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 33-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

| 24-1 No Smoking/Fasten    | -  | -  | *(O)May be inoperative provided:      |

|      Seat Belt Signs      |    |    |     a) Passenger or Flight            |

|                           |    |    |        Attendant Seats from which     |

|                           |    |    |        a readily legible NO           |

|                           |    |    |        SMOKING/FASTEN SEAT BELT       |

|                           |    |    |        sign can not be seen are       |

|                           |    |    |        considered inoperative.        |

|                           |    |    |                  OR                   |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established for alerting the   |

|                           |    |    |        cabin attendants and           |

|                           |    |    |        notifying the passenger by     |

|                           |    |    |        use of the Passenger           |

|                           |    |    |        Address System when seat       |

|                           |    |    |        belts should be fastened and   |

|                           |    |    |        smoking is prohibited.         |

|                           |    |    |                                       |

| 31-1 Cargo Compartment    | -  | 0  | *                                     |

|      Lights               |    |    |                                       |

|                           |    |    |                                       |

| 32-1 Maintenance Area and | -  | 0  | *                                     |

|      Service Panel Lights |    |    |                                       |

|                           |    |    |                                       |

| 41-1 Navigation Lights    | 3  | 0  | *All may be inoperative provided      |

|                           |    |    | aircraft is not operated at night.    |

|                           |    |    |                                       |

| 42-1 Anti Collision       | 3  | 0  | *All may be inoperative provided      |

|      Lights               |    |    | aircraft is not operated at night.    |

|                           |    |    |                                       |

|      1) Fuselage Mounted  | 2  | 0  | *Both may be inoperative provided     |

|         Lights            |    |    | Wing Tip Strobe Lights are            |

|                           |    |    | installed and operative.              |

|                           |    |    |                                       |

| 42-2 Anti-Collision       | 1  | 0  | *                                     |

|      Lights OFF           |    |    |                                       |

|      Annunciator          |    |    |                                       |

|                           |    |    |                                       |

| 43-1 Wing Inspection      | 2  | 1  | *                                     |

|      Lights               |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 33-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

| 43-1 Wing Inspection      | 2  | 0  | *(O)Both may be inoperative           |

|      Lights (Cont'd)      |    |    | provided:                             |

|                           |    |    |     a) Aircraft is not operated in    |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions at night.           |

|                           |    |    |                   OR                  |

|                           |    |    |     b) A portable lamp, adequate to   |

|                           |    |    |        inspect the Wings in flight,   |

|                           |    |    |        is available for night         |

|                           |    |    |        operations and                 |

|                           |    |    |     c) Operations procedures are      |

|                           |    |    |        established for its use.       |

|                           |    |    |                                       |

| 43-2 Wing Inspection      | 1  | 0  | *                                     |

|      Lights ON            |    |    |                                       |

|      Annunciator          |    |    |                                       |

|                           |    |    |                                       |

| 44-1 Landing Lights       | 2  | 1  | *One may be inoperative provided      |

|                           |    |    | Taxi Light is operative.              |

|                           |    |    |                                       |

|                           | 2  | 0  | *Both may be inoperative provided     |

|                           |    |    | aircraft is not operated at night.    |

|                           |    |    |                                       |

| 45-1 Taxi Light           | 1  | 0  | *May be inoperative provided:         |

|                           |    |    |     a) Aircraft is not operated at    |

|                           |    |    |        night.                         |

|                           |    |    |                    OR                 |

|                           |    |    |     b) Both Landing Lights are        |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

| 46-1 Logo Lights          | 2  | 0  | *                                     |

|                           |    |    |                                       |

| 47-1 Wing Tip Strobe      | 1  | 0  | *May be inoperative provided:         |

|      Light System         |    |    |     a) All Anti-Collision Lights      |

|                           |    |    |        are operative.                 |

|                           |    |    |                     OR                |

|                           |    |    |     b) Aircraft is not operated at    |

|                           |    |    |        night.                         |

|                           |    |    |                                       |

| 51-1 Cabin Standby        | 1  | 0  | *                                     |

|      Lighting System      |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 33-4     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

| 52-1 Floor Proximity      | -  | -  | *(M)Individual lights may be          |

|      Emergency Escape     |    |    | inoperative provided maintenance      |

|      Path Marking System  |    |    | procedures are established to         |

|      Lights               |    |    | determine that FAA approved           |

|                           |    |    | minimum acceptable lighting           |

|                           |    |    | level (s) is maintained by            |

|                           |    |    | remaining operative lights.           |

|                           |    |    |                                       |

|                           |    |    | NOTE: Reference the following         |

|                           |    |    |       documents for FAA approved      |

|                           |    |    |       minimum acceptable lighting     |

|                           |    |    |       levels:                         |

|                           |    |    |       a) FAA engineering Approval     |

|                           |    |    |          letter,                      |

|                           |    |    |       b) FAA approved report of the   |

|                           |    |    |          Type Design holder,          |

|                           |    |    |       c) Limitations and Conditions   |

|                           |    |    |          section of the applicable    |

|                           |    |    |          Supplemental Type            |

|                           |    |    |          Certificate (STC).           |

|                           |    |    |       d) FAA approved report          |

|                           |    |    |          incorporated in the Master   |

|                           |    |    |          drawing list for the         |

|                           |    |    |          applicable STC.              |

|                           |    |    |                                       |

| 52-2 Exterior Emergency   | 1  | 0  | *May be inoperative provided          |

|      Lighting System      |    |    | aircraft is not operated at night.    |

|                           |    |    |                                       |

| 52-3 Emergency Lights     | 1  | 0  | *                                     |

|      NOT ARMED            |    |    |                                       |

|      Annunciator          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 34-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

| 12-1 Overspeed Aural      | 1  | 0  | *May be inoperative provided          |

|      Warning System       |    |    | aircraft is not operated in excess    |

|                           |    |    | of 10 knots below the speed           |

|                           |    |    | indicated by the Maximum Allowable    |

|                           |    |    | Pointer.                              |

|                           |    |    |                                       |

| 13-1 First Officer's      | 1  | 0  | *(O)May be inoperative provided       |

|      Altimeter Vibrator   |    |    | operations procedures are             |

|                           |    |    | established to maintain altitude      |

|                           |    |    | using the captain's altimeter.        |

|                           |    |    |                                       |

| 15-1 Altitude Alerting    | 1  | 0  | *(O)May be inoperative provided       |

|      System               |    |    | operations procedures are             |

|                           |    |    | established that do not depend on     |

|                           |    |    | use of the Altitude Altering          |

|                           |    |    | System.                               |

|                           |    |    |                                       |

| 25-1 Flight Director      | 2  | 0  | *(O)Both may be inoperative           |

|      Systems              |    |    | provided:                             |

|                           |    |    |     a) Approach minimums do not       |

|                           |    |    |        depend on use of affected      |

|                           |    |    |        Flight Director and            |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established that do not        |

|                           |    |    |        depend on use of affected      |

|                           |    |    |        flight director.               |

| 25-2 Flight Mode Panel    | 1  | 0  | *May be inoperative provided:         |

|                           |    |    |     a) Automatic Cabin                |

|                           |    |    |        Pressurization Control         |

|                           |    |    |        System is operative,           |

|                           |    |    |     b) Approach minimums do not       |

|                           |    |    |        depend on its use,             |

|                           |    |    |     c) Any mode or function which     |

|                           |    |    |        does not operate normally is   |

|                           |    |    |        not used and                   |

|                           |    |    |     d) Course and Heading Select      |

|                           |    |    |        are operative.                 |

|                           |    |    |                                       |

| 26-1 EFIS DU-XFR Switches | 2  | 0  | *                                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 34-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

| 31-1 Marker Beacon System | 1  | -  | *May be inoperative provided          |

|                           |    |    | applicable FAR does not require       |

|                           |    |    | affected Marker Beacon System for     |

|                           |    |    | operation conducted.                  |

|                           |    |    |                                       |

| 32-1 LOC/GS Systems       | 2  | -  | *(O)May be inoperative provided:      |

|                           |    |    |     a) Applicable FAR does not        |

|                           |    |    |        require affected LOC/GS        |

|                           |    |    |        System for operation           |

|                           |    |    |        conducted and                  |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established that do not        |

|                           |    |    |        depend on use of LOC/GS        |

|                           |    |    |        System.                        |

|                           |    |    |                                       |

| 41-1 Weather Radar System | 1  | -  | *(O)May be inoperative provided:      |

|                           |    |    |     a) Applicable FAR does not        |

|                           |    |    |        require Weather Radar System   |

|                           |    |    |        for operation conducted and    |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established that do not        |

|                           |    |    |        depend on use of Weather       |

|                           |    |    |        Radar System.                  |

|                           |    |    |                                       |

| 41-2 Data Nav. System     | 1  | 0  | *                                     |

|      (Check List)         |    |    |                                       |

|                           |    |    |                                       |

| 42-1 Radio Altimeter      | 1  | 0  | *May be inoperative provided:         |

|      System               |    |    |     a) Approach minimums do not       |

|                           |    |    |        depend on use of radar         |

|                           |    |    |        altimeter and                  |

|                           |    |    |     b) GPWS is considered             |

|                           |    |    |        inoperative.                   |

|                           |    |    |                                       |

|                           |    |    | NOTE: One operative radar altimeter   |

|                           |    |    |       is required to conduct ILS      |

|                           |    |    |       approaches using flight         |

|                           |    |    |       director or autopilot.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 34-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

| 43-1 Ground Proximity     | 1  | 0  | *May be inoperative provided          |

|      Warning System       |    |    | applicable FAR does not require       |

|      (GPWS)               |    |    | GPWS for operations conducted.        |

|                           |    |    |                                       |

| 43-2 GPW FAULT Light      | 1  | 0  | *                                     |

|                           |    |    |                                       |

| 51-1 VOR Navigation       | 2  | -  | *(O)Both may be inoperative           |

|      Systems              |    |    | provided:                             |

|                           |    |    |     a) Applicable FAR does not        |

|                           |    |    |        require affected VOR           |

|                           |    |    |        Navigation System for          |

|                           |    |    |        operation conducted and        |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established that do not        |

|                           |    |    |        depend on use of the           |

|                           |    |    |        affected VOR Navigation        |

|                           |    |    |        System.                        |

|                           |    |    |                                       |

| 51-2 Radio Magnetic       | 2  | 0  | *Both may be inoperative provided     |

|      Indication (RMI)     |    |    | ADF and VOR pointers are available    |

|      Systems              |    |    | on the EFIS Navigation Display        |

|                           |    |    | (ND).                                 |

|                           |    |    |                                       |

| 52-1 Distance Measuring   | 2  | -  | *(O)Both may be inoperative           |

|      Equipment (DME)      |    |    | provided:                             |

|      Systems              |    |    |     a) Applicable FAR does not        |

|                           |    |    |        require affected ADF for       |

|                           |    |    |        operation conducted and        |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established that do not        |

|                           |    |    |        depend on use of the           |

|                           |    |    |        affected DME System.           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 34-4     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

| 53-1 Automatic Direction  | 2  | -  | *(O)Both may be inoperative           |

|      Finding (ADF)        |    |    | provided:                             |

|      Systems              |    |    |     a) Applicable FAR does not        |

|                           |    |    |        require affected ADF for       |

|                           |    |    |        operation conducted and        |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established that do not        |

|                           |    |    |        depend on use of the           |

|                           |    |    |        affected ADF System.           |

|                           |    |    |                                       |

| 54-1 Air Traffic Control  | -  | -  | *May be inoperative provided          |

|      (ATC) Transponder    |    |    | applicable FAR does not require       |

|      Systems              |    |    | affected ATC Transponder for          |

|                           |    |    | operation conducted.                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 35-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 35 OXYGEN                 |    |    |                                       |

|                           |    |    |                                       |

| 30-1 Portable Oxygen      | -  | -  | *May be inoperative provided          |

|      Dispensing Unit      |    |    | applicable FAR does not require       |

|                           |    |    | affected oxygen dispensing unit for   |

|                           |    |    | operation conducted.                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 36-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 36  PNEUMATICS            |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Bleed Air Supply     | 2  | 1  | *One may be inoperative provided:     |

|      and Control Systems  |    |    |     a) Aircraft is not operated in    |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions and                 |

|                           |    |    |     b) Affected Bleed Air Supply      |

|                           |    |    |        and Control System is OFF.     |

|                           |    |    |                                       |

| 11-2 High Pressure Bleed  | 2  | 1  | *(M)One may be inoperative provided   |

|      Valves               |    |    | maintenance procedures are            |

|                           |    |    | established to determine that         |

|                           |    |    | affected valve is CLOSED.             |

|                           |    |    |                                       |

| 20-1 Bleed FAULT Lights   | 2  | 1  | *(M)One may be inoperative            |

|                           |    |    | provided:                             |

|                           |    |    |     a) Maintenance procedures are     |

|                           |    |    |        established to determine       |

|                           |    |    |        that associated fault          |

|                           |    |    |        sensors are operative and      |

|                           |    |    |     b) Affected bleed valve CLOSED    |

|                           |    |    |        Light is operative.            |

|                           |    |    |                                       |

| 20-2 Bleed Valve Closed   | 2  | 1  | *One may be inoperative provided      |

|      Lights               |    |    | associated Bleed FAULT Light is       |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

| 20-3 Economy ON Light     | 1  | 0  | *                                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 52-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 52  DOORS                 |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Passenger Door       | 1  | 0  | *May be inoperative provided door     |

|      Actuator             |    |    | can be raised manually using the      |

|                           |    |    | crank handle.                         |

|                           |    |    |                                       |

| 70-1 Door Warning Lights  | 4  | 0  | *(O)All may be inoperative provided   |

|                           |    |    | operations procedures are             |

|                           |    |    | established to determine that         |

|                           |    |    | affected door(s) is closed and        |

|                           |    |    | locked.                               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 73-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 73  ENGINE FUEL & CONTROL |    |    |                                       |

|                           |    |    |                                       |

| 22-1 Engine Electronic    | 2  | 0  | *Both may be inoperative provided:    |

|      Control (EEC) FAULT  |    |    |     a) Both Central Annunciator       |

|      Lights               |    |    |        Panel Lights are Operative     |

|                           |    |    |        and                            |

|                           |    |    |     b) It is determined that the      |

|                           |    |    |        affected EEC Fault Warning     |

|                           |    |    |        System is operative.           |

|                           |    |    |                                       |

| 22-2 Engine Rating Panel  | 1  | 0  | *May be inoperative provided FLEX     |

|      (ERP) FLEX TEMP      |    |    | Takeoff mode is not used.             |

|      Indication and       |    |    |                                       |

|      Control              |    |    |                                       |

|                           |    |    |                                       |

| 31-1 Fuel Flow, Fuel      |    |    |                                       |

|      Consumed, and        |    |    |                                       |

|      Aircraft Weight      |    |    |                                       |

|      Indicator            |    |    |                                       |

|                           |    |    |                                       |

|      1) Fuel Flow         | 2  | 1  | *(O)One may be inoperative            |

|         Displays          |    |    | provided:                             |

|                           |    |    |     a) Associated TRQ, ITT, Nh, Nl    |

|                           |    |    |        and Fuel Quantity Indicating   |

|                           |    |    |        Systems are operative and      |

|                           |    |    |     b) Operations procedures are      |

|                           |    |    |        established and used to        |

|                           |    |    |        monitor fuel usage.            |

|                           |    |    |                                       |

|                           |    |    | NOTE: Fuel Used/Weight Indicating     |

|                           |    |    |       may be affected.                |

|                           |    |    |                                       |

|      2) Fuel Used System  | 1  | 0  | *(O)May be inoperative provided       |

|                           |    |    | operations procedures are             |

|                           |    |    | established that do not depend on     |

|                           |    |    | use of Fuel Used System.              |

|                           |    |    |                                       |

|      3) Aircraft Weight   | 1  | 0  | *(O)May be inoperative provided       |

|         Indicating System |    |    | operations procedures are             |

|                           |    |    | established that do not depend on     |

|                           |    |    | use of Aircraft Weight Indicating     |

|                           |    |    | System.                               |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 73-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 73  ENGINE FUEL & CONTROL |    |    |                                       |

|                           |    |    |                                       |

| 32-1 Fuel TEMP HIGH Light | 2  | 0  | *                                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 77-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 77  ENGINE INDICATING     |    |    |                                       |

|                           |    |    |                                       |

| 11-1 NH Indicating        | 2  | 1  | *(O)One may be inoperative            |

|      Systems              |    |    | provided:                             |

|                           |    |    |     a) Torque, NL, NP and Fuel Flow   |

|                           |    |    |        indicating system are          |

|                           |    |    |        operative for the affected     |

|                           |    |    |        engine,                        |

|                           |    |    |     b) Engine Electronic Control      |

|                           |    |    |        (EEC) System for the           |

|                           |    |    |        affected engine is             |

|                           |    |    |        operative,                     |

|                           |    |    |     c) EEC FAULT Light for the        |

|                           |    |    |        affected engine is operative   |

|                           |    |    |        and                            |

|                           |    |    |     d) Operations procedures are      |

|                           |    |    |        established for engine start   |

|                           |    |    |        without use of the affected    |

|                           |    |    |        NH Indicator.                  |

|                           |    |    |                                       |

|      1) Digital Display   | 2  | 0  | *                                     |

|         Portions          |    |    |                                       |

|                           |    |    |                                       |

| 11-2 NL Indicating        | 2  | 1  | *May be inoperative provided:         |

|      Systems              |    |    |     a) Torque NH, NP and Fuel Flow    |

|                           |    |    |        indicating systems are         |

|                           |    |    |        operative for the affected     |

|                           |    |    |        engine,                        |

|                           |    |    |     b) Engine Electronic Control      |

|                           |    |    |        (EEC) System for the           |

|                           |    |    |        affected engine is             |

|                           |    |    |        operative,                     |

|                           |    |    |     c) EEC FAULT Light for the        |

|                           |    |    |        affected engine is operative   |

|                           |    |    |        and                            |

|                           |    |    |     d) All components of the Bleed    |

|                           |    |    |        Air System for the affected    |

|                           |    |    |        engine are operative.          |

|                           |    |    |                                       |

|      1) Digital Display   | 2  | 0  | *                                     |

|         Portions          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 77-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 77  ENGINE INDICATING     |    |    |                                       |

|                           |    |    |                                       |

| 13-1 Torque Indicating    | 2  | 0  | *                                     |

|      Systems Digital      |    |    |                                       |

|      Display Portion      |    |    | NOTE: EEC Fault Codes will also be    |

|                           |    |    |       inoperative.                    |

|                           |    |    |                                       |

| 21-1 ITT Indication       | 2  | 0  | *                                     |

|      Systems Digital      |    |    |                                       |

|      Display Portion      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: ORIGINAL | PAGE:    |

|               FOKKER F-50                |                       |          |

|                                          | DATE: 02/03/88        | 80-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 80 STARTING               |    |    |                                       |

|                           |    |    |                                       |

| 12-1 Start Push Button    | 1  | 0  | *(O)May be inoperative provided       |

|      FAULT Light          |    |    | operations procedure is established   |

|                           |    |    | to verify that no started clutch      |

|                           |    |    | fault exists after each engine        |

|                           |    |    | start.                                |

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| 12-1 Continuous Ignition  | 2  | 1  | *                                     |

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