DEPARTMENT OF TRANSPORTATION     Revision: 6

                                                           Date: 10/24/96

                         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

 

 

 

 

 

                               BRITISH AEROSPACE

                                    BAE-ATP

                                      /S/

                                 JAMES H. KLING

                          CHAIRMAN, FLIGHT OPERATIONS

                            EVALUATION BOARD (FOEB)

 

 

 

 

 

 

 

 

                         Federal Aviation Administration

                         Flight Standards Division

                         AIRCRAFT EVALUATION OFFICE, ANM-270S

                         1601 Lind Ave. S.W.

 

                         Renton, Washington 98055-4056

 

                         TELEPHONE: (206) 227-2280

                         FAX:       (206) 227-1270

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 10/24/96

 

 

                                  BAe-ATP

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I

         --     Log of Revisions                        II, III

         --     Control Page                            IV, V, VI

         --     Highlights of Change                    VII, VIII, IX

         --     Definitions                             X, XI, XII, XIII

         --     Definitions                             XIV, XV, XVI, XVII

         --     Preamble                                XVIII, XIX

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

         21     Air Conditioning                        21-6

         22     Auto Flight                             22-1, 2

         23     Communications                          23-1, 2, 3

         24     Electrical Power                        24-1, 2, 3, 4, 5

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

         25     Equipment/Furnishings                   25-6, 7, 8

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

         27     Flight Controls                         27-1, 2, 3

         28     Fuel                                    28-1, 2

         29     Hydraulic Power                         29-1

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

         31     Indicating/Recording Systems            31-1

         32     Landing Gear                            32-1, 2, 3, 4

         33     Lights                                  33-1, 2, 3, 4, 5

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

         34     Navigation                              34-6, 7, 8, 9

         35     Oxygen                                  35-1

         38     Water/Waste                             38-1

         49     Airborne Auxiliary Power                49-1

         52     Doors                                   52-1, 2

         56     Windows                                 56-1

         61     Propellers                              61-1

         73     Engine Fuel & Control                   73-1

         74     Ignition                                74-1

         77     Engine Indicating                       77-1

         79     Engine Oil                              79-1, 2, 3

         80     Starting                                80-1

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: II

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 10/24/96

 

 

                                  BAe-ATP

 

 

                               Log of Revisions

 

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

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

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

      | ORIGINAL | 06/22/88   | Original                       |           |

      | 1        | 01/19/90   | ALL PAGES                      |           |

      | 1a       | 10/12/90   | HIGHLIGHTS OF REV.             |           |

      | 1a       | 10/12/90   | 25-1,25-2                      |           |

      | 2        | 10/19/90   | HIGHLIGHTS OF REV.             |           |

      | 2        | 10/19/90   | 24-1,25-4,26-1,26-2,26-3       |           |

      | 2        | 10/19/90   | 26-4,26-5,34-3,35-1,49-1       |           |

      | 2        | 10/19/90   | 79-1                           |           |

      | 3        | 12/18/90   | HIGHLIGHTS OF REV.             |           |

      | 3        | 12/18/90   | 32-2,79-1                      |           |

      | 4        | 05/16/91   | HIGHLIGHTS OF REV.             |           |

      | 4        | 05/16/91   | 21-2,21-3,21-4,21-5,21-6       |           |

      | 4        | 05/16/91   | 22-1,22-2,23-2,24-1,24-2       |           |

      | 4        | 05/16/91   | 24-3,24-4,24-5,25-4,25-5       |           |

      | 4        | 05/16/91   | 26-1,26-2,26-3,26-4,26-5       |           |

      | 4        | 05/16/91   | 26-6,27-1,27-2,27-3,29-1       |           |

      | 4        | 05/16/91   | 30-1,30-2,30-3,30-4,31-1       |           |

      | 4        | 05/16/91   | 32-1,32-2,32-3,32-4,33-4       |           |

      | 4        | 05/16/91   | 34-1,34-3,34-4,34-5,34-6       |           |

      | 4        | 05/16/91   | 34-7,35-1,49-1,52-1,52-2       |           |

      | 4        | 05/16/91   | 73-1,79-1,79-2                 |           |

      | 5        | 01/27/93   | HIGHLIGHTS OF REV.             |           |

      | 5        | 01/27/93   | 21-1,21-2,21-3,21-4,22-1       |           |

      | 5        | 01/27/93   | 23-2,23-3,25-1,25-4,26-2       |           |

      | 5        | 01/27/93   | 26-3,27-1,28-1,33-2,33-3       |           |

      | 5        | 01/27/93   | 34-2,34-3,34-4,34-6,34-7       |           |

      | 5        | 01/27/93   | 61-1,73-1,79-1,79-2,79-3       |           |

      | 5a       | 03/17/94   | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 5a       | 03/17/94   | 26-3                           |           |

      | 5b       | 05/16/96   | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 5b       | 05/16/96   | 74-1                           |           |

      | 6        | 10/24/96   | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 6        | 10/24/96   | 21-1,21-2,21-3,21-4,21-5       |           |

      | 6        | 10/24/96   | 21-6,22-1,22-2,23-1,23-2       |           |

      | 6        | 10/24/96   | 23-3,24-1,24-2,24-3,24-4       |           |

      | 6        | 10/24/96   | 24-5,25-1,25-2,25-3,25-4       |           |

      | 6        | 10/24/96   | 25-5,25-6,25-7,25-8,26-1       |           |

      | 6        | 10/24/96   | 26-2,26-3,26-4,26-5,26-6       |           |

      | 6        | 10/24/96   | 27-1,27-2,27-3,28-1,28-2       |           |

      | 6        | 10/24/96   | 29-1,30-1,30-2,30-3,30-4       |           |

      | 6        | 10/24/96   | 31-1,32-1,32-2,32-3,32-4       |           |

      | 6        | 10/24/96   | 33-1,33-2,33-3,33-4,33-5       |           |

      | 6        | 10/24/96   | 34-1,34-2,34-3,34-4,34-5       |           |

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

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: III

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 10/24/96

 

 

                                  BAe-ATP

 

 

                               Log of Revisions

 

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

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

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

      | 6        | 10/24/96   | 34-6,34-7,34-8,34-9,35-1       |           |

      | 6        | 10/24/96   | 38-1,49-1,52-1,52-2,56-1       |           |

      | 6        | 10/24/96   | 61-1,73-1,74-1,77-1,79-1       |           |

      | 6        | 10/24/96   | 79-2,79-3,80-1                 |           |

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                       FEDERAL AVIATION ADMINISTRATION     Page: IV

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 10/24/96

 

 

                                  BAe-ATP

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       6        10/24/96

         Table of Contents                        I       6        10/24/96

         Log of Revisions                         II      6        10/24/96

                                                  III     6        10/24/96

         Control Page                             IV      6        10/24/96

                                                  V       6        10/24/96

                                                  VI      6        10/24/96

         Highlights of Change                     VII     6        10/24/96

                                                  VIII    6        10/24/96

                                                  IX      6        10/24/96

         Definitions                              X       6        01/31/95

                                                  XI      6        01/31/95

                                                  XII     6        01/31/95

                                                  XIII    6        01/31/95

                                                  XIV     6        01/31/95

                                                  XV      6        01/31/95

                                                  XVI     6        01/31/95

                                                  XVII    6        01/31/95

         Preamble                                 XVIII   2        06/14/89

                                                  XIX     2        06/14/89

         21                                       21-1    6        10/24/96

                                                  21-2    6        10/24/96

                                                  21-3    6        10/24/96

                                                  21-4    6        10/24/96

                                                  21-5    6        10/24/96

                                                  21-6    6        10/24/96

         22                                       22-1    6        10/24/96

                                                  22-2    6        10/24/96

         23                                       23-1    6        10/24/96

                                                  23-2    6        10/24/96

                                                  23-3    6        10/24/96

         24                                       24-1    6        10/24/96

                                                  24-2    6        10/24/96

                                                  24-3    6        10/24/96

                                                  24-4    6        10/24/96

                                                  24-5    6        10/24/96

         25                                       25-1    6        10/24/96

                                                  25-2    6        10/24/96

                                                  25-3    6        10/24/96

                                                  25-4    6        10/24/96


 

                       FEDERAL AVIATION ADMINISTRATION     Page: V

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 10/24/96

 

 

                                  BAe-ATP

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  25-5    6        10/24/96

                                                  25-6    6        10/24/96

                                                  25-7    6        10/24/96

                                                  25-8    6        10/24/96

         26                                       26-1    6        10/24/96

                                                  26-2    6        10/24/96

                                                  26-3    6        10/24/96

                                                  26-4    6        10/24/96

                                                  26-5    6        10/24/96

         27                                       27-1    6        10/24/96

                                                  27-2    6        10/24/96

                                                  27-3    6        10/24/96

         28                                       28-1    6        10/24/96

                                                  28-2    6        10/24/96

         29                                       29-1    6        10/24/96

         30                                       30-1    6        10/24/96

                                                  30-2    6        10/24/96

                                                  30-3    6        10/24/96

                                                  30-4    6        10/24/96

         31                                       31-1    6        10/24/96

         32                                       32-1    6        10/24/96

                                                  32-2    6        10/24/96

                                                  32-3    6        10/24/96

                                                  32-4    6        10/24/96

         33                                       33-1    6        10/24/96

                                                  33-2    6        10/24/96

                                                  33-3    6        10/24/96

                                                  33-4    6        10/24/96

                                                  33-5    6        10/24/96

         34                                       34-1    6        10/24/96

                                                  34-2    6        10/24/96

                                                  34-3    6        10/24/96

                                                  34-4    6        10/24/96

                                                  34-5    6        10/24/96

                                                  34-6    6        10/24/96

                                                  34-7    6        10/24/96

                                                  34-8    6        10/24/96

                                                  34-9    6        10/24/96

         35                                       35-1    6        10/24/96

         38                                       38-1    6        10/24/96


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 10/24/96

 

 

                                  BAe-ATP

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         49                                       49-1    6        10/24/96

         52                                       52-1    6        10/24/96

                                                  52-2    6        10/24/96

         56                                       56-1    6        10/24/96

         61                                       61-1    6        10/24/96

         73                                       73-1    6        10/24/96

         74                                       74-1    6        10/24/96

         77                                       77-1    6        10/24/96

         79                                       79-1    6        10/24/96

                                                  79-2    6        10/24/96

                                                  79-3    6        10/24/96

         80                                       80-1    6        10/24/96

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: VII

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 10/24/96

 

 

                                  BAe-ATP

 

                            Highlights of Change

 

 

 

       Effective above date, the BAe-ATP Master Minimum Equipment List has been

       revised.  Please replace affected pages of the previous list with

       revision 6 for a complete up-to-date MMEL.

 

       Deleted all asterisk (*) symbols in accordance with (IAW) Policy Letter

       (PL) 61.

 

       22  AUTO FLIGHT

 

            10-1  Autopilot System

            COMMENT:  Added proviso c) to sub item 2) to include missing time

                      limitation required for category A designation.

 

 

       23  COMMUNICATIONS

 

            31-1  Passenger Address System

            COMMENT:  Updated IAW PL-9 (CG-13).

 

            51-2  Boom Microphones

            COMMENT:  Added proviso b).

 

            81-1 Touchtone Microphone (DFTM)

            COMMENT:  New item.

 

 

       25  EQUIPMENT/FURNISHINGS

 

            10-1  Observer Seat(s)

            COMMENT:  Updated IAW PL-56 (CG-25).

 

            22-13  Underseat Baggage Restraining Bars

            COMMENT:  New item IAW PL-79 (CG-28).

 

            40-2  Lavatory Door Ashtrays

            COMMENT:  New item IAW AD 74-08-09 R2 and draft policy letter.

 

            60-4  First Aid Kits

            COMMENT:  Updated IAW PL-73 (CG-17).

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: VIII

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 10/24/96

 

 

                                  BAe-ATP

 

                            Highlights of Change

 

 

 

       26  FIRE PROTECTION

 

            11-1  APU Fire Extinguisher System

            COMMENT:  New item.

 

            22-1  Portable Fire Extinguishers

            COMMENT:  Updated IAW PL-75 (CG-19).

 

 

       32  LANDING GEAR

 

            42-7  Brake Temperature Indicating System

            COMMENT:  Corrected sequential lettering of provisos c) through f).

 

 

       33  LIGHTS

 

            13-1  Cockpit/Flight Deck /Flight Compartment and Instrument Panel

                  Lighting Systems

            COMMENT:  Updated IAW PL-77 (CG-21).

 

            44-1  Wing Illumination Lights

            COMMENT:  Revised to comply with Airworthiness Directive 96-09-17.

 

 

       34  NAVIGATION

 

            12-02  ATC Transponders and Automatic Altitude Reporting Systems

            COMMENT:  Updated IAW PL-76 (CG-20).

 

            23-09  Vertical Speed Indication (Primary Flight Display only)

            COMMENT:  Added "(Primary Flight Display only)" for clarification.

 

            42-01  Radio Altimeter System

            COMMENT:  Changed to category A and added proviso e).

 

            43-01  Ground Proximity Warning System (GPWS)

            COMMENT:  Updated IAW PL-54 (CG-10).

 

            44-01  Traffic Alert  Collision Avoidance System (TCAS)

            COMMENT:  Updated IAW PL-32.

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: IX

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 10/24/96

 

 

                                  BAe-ATP

 

                            Highlights of Change

 

 

 

       35  OXYGEN

 

            31-1  Portable Oxygen Dispensing Units (Bottles, masks, lines,

                  gauges and fittings)

            COMMENT:  Revised title for clarification.

 

 

       38  WATER/WASTE

 

            10-1  Potable Water Systems

            COMMENT:  Updated IAW PL-83 (CG-32).

 

            30-1  Lavatory Systems

            COMMENT:  New item IAW PL-83 (CG-32).

 

 

       52  DOORS

 

            60-01  Forward Airstairs System

            COMMENT:  Added proviso c).

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: X

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

 

 

                                  BAe-ATP

 

                                 Definitions

 

 

       1.   System Definitions.

 

       System numbers are based on the Air Transport Association (ATA)

       Specification Number 100 and items are numbered sequentially.

 

            a.        "Item" (Column 1) means the equipment, system,

                      component, or function listed in the "Item"

                      column.

 

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

                      (quantity) of items normally installed in the

                      aircraft.  This number represents the aircraft

                      configuration considered in developing this MMEL.

                      Should the number be a variable (e.g., passenger

                      cabin items) a number is not required.

                                                                            |

            c.        "Number Required for Dispatch" (Column 3) is the

                      minimum number (quantity) of items required for

                      operation provided the conditions specified in

                      Column 4 are met.

 

       NOTE:  Where the MMEL shows a variable number required for

       dispatch, the MEL must reflect the actual number required for

       dispatch or an alternate means of configuration control approved

       by the Administrator.

 

            d.        "Remarks or Exceptions" (Column 4) in this column

                      includes a statement either prohibiting or

                      permitting operation with a specific number of

                      items inoperative, provisos (conditions and

                      limitations) for such operation, and appropriate

                      notes.

 

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

                      indicates a change, addition or deletion in the

                      adjacent text for the current revision of that

                      page only.  The change bar is dropped at the next

                      revision of that page.

 

       2.  "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document

       required for type certification and approved by the responsible

       FAA Aircraft Certification  Office. The FAA approved AFM/RFM for

       the specific aircraft is listed on the applicable Type

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/95

 

 

                                  BAe-ATP

 

                                 Definitions

 

 

       Certificate Data Sheet.

 

       3.  "As required by FAR" means that the listed item is subject to

       certain provisions (restrictive or permissive) expressed in the

       Federal Aviation Regulations operating rules.  The number of

       items required by the FAR must be operative.  When the listed

       item is not required by FAR it may be inoperative for time

       specified by repair category.

 

       4.  Each inoperative item must be placarded to inform and remind

       the crewmembers and maintenance personnel of the equipment

       condition.

 

       NOTE:  To the extent practical, placards should be located

       adjacent to the control or indicator for the item affected;

       however, unless otherwise specified, placard wording and location

       will be determined by the operator.

 

       5.  "-" symbol in Column 2 and/or Column 3 indicates a variable

       number (quantity) of the item installed.

                                                                           |

       6.  "Deleted" in the remarks column after a sequence item

       indicates that the item was previously listed but is now required

       to be operative if installed in the  aircraft.

 

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

       airplane which has a type design approval for ER operations and

       complies with the provisions of Advisory Circular 120-42A.           |

 

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

       portions of the Federal Aviation Act and Federal Aviation

       Regulations.

 

       9.  "Flight Day" means a 24 hour period (from midnight to

       midnight) either Universal Coordinated Time (UCT) or local time,

       as established by the operator, during which at least one flight

       is initiated for the affected aircraft.

 

       10.  "Icing Conditions" means an atmospheric environment that may

       cause ice to form on the aircraft or in the engine(s).

 

       11.  Alphabetical symbol in Column 4 indicates a proviso

       (condition or limitation) that must be complied with for

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XII

                                                           Revision: 6

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                                  BAe-ATP

 

                                 Definitions

 

 

       operation with the  listed item inoperative.

 

       12.  "Inoperative" means a system and/or component malfunction to

       the extent that it does not accomplish its intended purpose

       and/or is not consistently functioning normally within its

       approved operating limit(s) or tolerance(s).

 

       13.  "Notes:" in Column 4 provides additional information for

       crewmember or maintenance consideration.  Notes are used to

       identify applicable material which is intended to assist with

       compliance, but do not relieve the operator of the responsibility

       for compliance with all applicable requirements.  Notes are not a

       part of the provisos.

 

       14.  Inoperative components of an inoperative system:

       Inoperative items which are components of a system which is

       inoperative are usually considered components directly associated

       with and having no other function than to support that system.

       (Warning/caution systems associated with the inoperative system

       must be operative unless relief is specifically authorized per

       the MMEL).

 

       15.  "(M)" symbol indicates a requirement for a specific

       maintenance procedure which must be accomplished prior to

       operation with the listed item inoperative.  Normally these

       procedures are accomplished by maintenance personnel;  however,

       other personnel may be qualified and authorized to perform

       certain functions.  Procedures requiring specialized knowledge or

       skill, or requiring the use of tools or test equipment should be

       accomplished by maintenance personnel.  The satisfactory

       accomplishment of all maintenance procedures, regardless of

       who performs them, is the responsibility of the operator.

       Appropriate procedures are required to be published as part of

       the operator's manual or MEL.

 

       16.  "(O)" symbol indicates a requirement for a specific

       operations procedure which must be accomplished in planning for

       and/or operating with the listed item inoperative.  Normally

       these procedures are accomplished by the flight crew; however,

       other personnel may be qualified and authorized to perform

       certain functions.  The satisfactory accomplishment of all

       procedures, regardless of who performs them, is the

       responsibility of the operator.  Appropriate procedures are

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIII

                                                           Revision: 6

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                                  BAe-ATP

 

                                 Definitions

 

 

       required to be published as a part of the operator's manual or

       MEL.

 

       NOTE:  The (M) and (O) symbols are required in the operator's MEL

       unless otherwise authorized by the Administrator.

 

       17.  "Deactivated" and "Secured" means that the specified

       component must be put into an acceptable condition for safe

       flight.  An acceptable method of securing or deactivating will be

       established by the operator.

 

       18.  "Visual Flight Rules" (VFR) is as defined in FAR Part 91.

       This precludes a pilot from filing an Instrument Flight Rules

       (IFR) flight plan.

 

       19.  "Visual Meteorological Conditions" (VMC) means the

       atmospheric environment is such that would allow a flight to

       proceed under the visual flight rules applicable to the flight.

       This does not preclude operating under Instrument Flight Rules.

 

       20.  "Visible Moisture" means an atmospheric environment

       containing water in any form that can be seen in natural or

       artificial light; for example, clouds, fog, rain, sleet, hail, or

       snow.

 

       21.  "Passenger Convenience Items" means those items related to

       passenger convenience, comfort or entertainment such as, but not

       limited to, galley equipment, movie equipment, ash trays, stereo

       equipment, overhead reading lamps, etc.

 

       22.  Repair Intervals:  All users of an MEL approved under FAR

       121, 125, 129 and 135 must effect repairs of inoperative systems

       or components, deferred in  accordance with the MEL, at or prior

       to the repair times established by the following letter

       designators:

 

            Category A.  Items in this category shall be repaired within

       the time interval specified in the remarks column of the

       operator's approved MEL.

 

            Category B.  Items in this category shall be repaired within

       three (3) consecutive calendar days (72 hours), excluding the day

       the malfunction was recorded in the aircraft maintenance

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIV

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                                  BAe-ATP

 

                                 Definitions

 

 

       record/logbook.  For example, if it were recorded at 10 a.m. on

       January 26th, the three day interval would begin at midnight the

       26th and end at midnight the 29th.

 

            Category C.  Items in this category shall be repaired within

       ten (10) consecutive calendar days (240 hours), excluding the day

       the malfunction was recorded in the aircraft maintenance

       record/logbook.  For example, if it were recorded at 10 a.m. on

       January 26th, the 10 day interval would begin at midnight the

       26th and end at midnight February 5th.

 

            Category D.  Items in this category shall be repaired within

       one hundred and twenty (120) consecutive calendar days (2880

       hours), excluding the day the malfunction was recorded in the

       aircraft maintenance log and/or record.

 

       The letter designators are inserted adjacent to Column 2.

 

       23. Electronic fault alerting system - General                  |

                                                                       |

       New generation aircraft display system fault indications to the |

       flight crew by use of computerized display systems.  Each       |

       aircraft manufacturer has incorporated individual design        |

       philosophies in determining the data that would be              |

       represented.  The following are customized definitions (specific|

       to each manufacturer) to help determine the level of messages   |

       affecting the aircraft's dispatch status.  When preparing the   |

       MEL document, operators are to select the proper Definition No. |

       23 for their aircraft, if appropriate.                          |

                                                                       |

       a.   BOEING  (B-757/767, B-747-400, B-777)                      |

                                                                       |

       Boeing airplanes equipped with Engine Indicating and Crew       |

       Alerting  Systems (EICAS), provide different priority levels of |

       system messages (WARNING,  CAUTION, ADVISORY, STATUS and        |

       MAINTENANCE).  Any messages that affects airplane dispatch      |

       status will be displayed at a STATUS message level or  higher.  |

       The absence of an EICAS STATUS or higher level (WARNING,        |

       CAUTION, ADVISORY) indicates that the system/component is       |

       operating within its approved operating limits or tolerances.   |

                                                                       |

       System conditions that result only in a maintenance level       |

       message, i.e. no correlation with a higher level EICAS message, |

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XV

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                                  BAe-ATP

 

                                 Definitions

 

 

       do not affect dispatch and do not require action other than as  |

       addressed within an operators standard maintenance program.     |

                                                                       |

       b.   DOUGLAS  (MD-11)                                           |

                                                                       |

       Some Douglas aircraft are equipped with an alerting function    |

       which is a subsystem within the Electronic Instrument System    |

       (EIS).  The alerting function provides various levels of system |

       condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and   |

       STATUS).                                                        |

                                                                       |

       Alerts that affect aircraft dispatch will include WARNING,      |

       CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are   |

       displayed on the status page of the EIS display panel under the |

       maintenance heading.                                            |

                                                                       |

       A MAINTENANCE alert on the EIS indicates the presence of a      |

       system fault which can be identified by the Central Fault       |

       Display System (CFDS) interrogation.  The systems are designed  |

       to be fault tolerant, however, for any MAINTENANCE alert, the   |

       MEL must be verified for dispatch purposes.                     |

                                                                       |

       c.   AIRBUS  (A-300-600, A-310, A-320/319/321, A-330, A-340     |

                                                                       |

       Airbus aircraft equipped with Electronic Centralized Aircraft   |

       Monitoring (ECAM) provide different levels of system condition  |

       messages (WARNING, CAUTION, STATUS, and ADVISORY). A-320/319/   |

       321, A-330, and A-340 also provide MAINTENANCE status messages. |

                                                                       |

       Any message that effects airplane dispatchability will normally |

       be at the WARNING, CAUTION or STATUS level. MAINTENANCE         |

       messages (A-320/319/321, A-330, and A-340 only) are also        |

       indicated on ECAM Status Page below the white Maintenance label.|

                                                                       |

       A MAINTENANCE status (Class II) message on ECAM indicates the   |

       presence of a system fault which can be identified by CFDS      |

       (A-320/319/321) or CMS (A-330/A-340) interrogation. The systems |

       are designed to be fault tolerant, however for any MAINTENANCE  |

       status (Class II) message, the A-320/319/321 MEL must be        |

       verified for dispatch capability. For the A-330 and A-340,      |

       MAINTENANCE status messages do not affect dispatch.             |

 

       d.   FOKKER  (FK-100)                                           |

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XVI

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                                  BAe-ATP

 

                                 Definitions

 

 

                                                                       |

       Fokker aircraft are equipped with Multi Function Display System |

       (MFDS) which provides electronic message referring to the       |

       different priority levels of system information (WARNING (red), |

       CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any      |

       messages that affects aircraft dispatch will be at the WARNING, |

       CAUTION or AWARENESS level.  In these cases the MEL must be     |

       verified for dispatch capability and maintenance may be         |

       required.                                                       |

                                                                       |

       System conditions that only require maintenance are not         |

       presented on the flight deck.  These maintenance                |

       indications/messages may be presented on the Maintenance & Test |

       Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by |

       dedicated Built In Test Evaluation (BITE) of systems.           |

 

       24.  "Administrative control item" means an item listed by the

       operator in the MEL for tracking and informational purposes.  It

       may be added to an operator's MEL by approval of the Principal

       Operations Inspector provided no relief is granted, or provided

       conditions and limitations are contained in an approved document

       (i.e. Structural Repair Manual, airworthiness directive, etc.).

       If relief other than that granted by an approved document is

       sought for an administrative control item, a request must be

       submitted to the Administrator.  If the request results in review

       and approval by the FOEB, the item becomes an MMEL item rather

       than an administrative control item.

 

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

       required by regulation but which may have been installed on some

       models of aircraft covered by this MMEL.  This item may be

       included on the operator's MEL after the approving office has

       determined that the item has been installed on one or more of the

       operator's aircraft.  The symbol, however, shall not be carried

       forward into the operator's MEL.  It should be noted that neither

       this policy nor the use of this symbol provide authority to

       install or remove an item from an aircraft.

 

       26.  "Excess Items" means those items that have been installed

       that are redundant to the requirements of the FARs.

 

       27.  "Day of Discovery" is the calendar day an

       equipment/instrument malfunction was recorded in the aircraft

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XVII

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                                  BAe-ATP

 

                                 Definitions

 

 

       maintenance log and or record.  This day is excluded from the

       calendar days or flight days specified in the MMEL for the

       repair of an inoperative item of equipment. This provision is

       applicable to all MMEL items, i.e., categories "A, B, C, and

       D."

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XVIII

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/89

 

 

                                  BAe-ATP

 

                                  Preamble

                            (Effective 6/14/89)

 

       The following is applicable for authorized certificate holders operating

       under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The

       FAR require that all equipment installed on an aircraft in compliance

       with the Airworthiness Standards and the Operating Rules must be

       operative.  However, the Rules also permit the publication of a Minimum

       Equipment List (MEL) where compliance with certain equipment

       requirements is not necessary in the interests of safety under all

       operating conditions.  Experience has shown that with the various levels

       of redundancy designed into aircraft, operation of every system or

       installed component may not be necessary when the remaining operative

       equipment can provide an acceptable level of safety.  A Master Minimum

       Equipment List (MMEL) is developed by the FAA, with participation by the

       aviation industry, to improve aircraft utilization and thereby provide

       more convenient and economic air transportation for the public.  The FAA

       approved MMEL includes those items of equipment related to airworthiness

       and operating regulations and other items of equipment which the

       Administrator finds may be inoperative and yet maintain an acceptable

       level of safety by appropriate conditions and limitations;  it does not

       contain obviously required items such as wings, flaps, and rudders.  The

       MMEL is the basis for development of individual operator MELs which take

       into consideration the operator's particular aircraft equipment

       configuration and operational conditions. Operator MELs, for

       administrative control, may include items not contained in the

       MMEL;  however, relief for administrative control items must be

       approved by the Administrator.  An operator's MEL may differ in

       format from the MMEL, but cannot be less restrictive than the MMEL.

       The individual operator's MEL, when approved and authorized, permits

       operation of the aircraft with inoperative equipment.

 

       Equipment not required by the operation being conducted and equipment in

       excess of FAR requirements are included in the MEL with appropriate

       conditions and limitations.  The MEL must not deviate from the Aircraft

       Flight Manual Limitations, Emergency Procedures or with Airworthiness

       Directives.  It is important to remember that all equipment related to

       the airworthiness and the operating regulations of the aircraft not

       listed on the MMEL must be operative.

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XIX

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/89

 

 

                                  BAe-ATP

 

                                  Preamble

                            (Effective 6/14/89)

 

       Suitable conditions and limitations in the form of placards, maintenance

       procedures, crew operating procedures and other restrictions as

       necessary are specified in the MEL to ensure that an acceptable level of

       safety is maintained.

 

       The MEL is intended to permit operation with inoperative items of

       equipment for a period of time until repairs can be accomplished.  It is

       important that repairs be accomplished at the earliest opportunity.  In

       order to maintain an acceptable level of safety and reliability the MMEL

       establishes limitations on the duration of and conditions for operation

       with inoperative equipment.  The MEL provides for release of the

       aircraft for flight with inoperative equipment.  When an item of

       equipment is discovered to be inoperative, it is reported by making an

       entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR.

       The item is then either repaired or may be deferred per the MEL or other

       approved means acceptable to the Administrator prior to further

       operation.  MEL conditions and limitations, do not relieve the operator

       from determining that the aircraft is in condition for safe operation

       with items of equipment inoperative.

 

       When these requirements are met, an Airworthiness Release, Aircraft

       Maintenance Record/Logbook entry, or other approved documentation is

       issued as prescribed by FAR.  Such documentation is required prior to

       operation with any item of equipment inoperative.

 

       Operators are responsible for exercising the necessary operational

       control to ensure that an acceptable level of safety is maintained.

       When operating with multiple inoperative items, the interrelationships

       between those items and the effect on aircraft operation and crew

       workload will be considered.

 

       Operators are to establish a controlled and sound repair program

       including the parts, personnel, facilities, procedures, and schedules to

       ensure timely repair.

 

       WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE,

       DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS

       REQUIRED.

 

 

 


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 21-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Nacelle Bleed      C | 4  | 3  | (O)One may be inoperative provided: | |

|      Air Valves           |    |    |     a) Pressurization system is       |

|      (HP & LP Bleeds)     |    |    |        operative.                     |

|                           |    |    |          OR                           |

|                         C |    |    |     b) If both ECS packs are          |

|                           |    |    |        inoperative, the operative     |

|                           |    |    |        nacelle bleed air supplies     |

|                           |    |    |        are selected on.               |

|                           |    |    |                                       |

|                         C | 4  | 2  | (O)Two may be inoperative provided: | |

|                           |    |    |     a) Pressurization system is       |

|                           |    |    |        operative.                     |

|                           |    |    |          OR                           |

|                         C |    |    |     b) If both ECS packs are          |

|                           |    |    |        inoperative, the operative     |

|                           |    |    |        nacelle bleed air supplies     |

|                           |    |    |        are selected on, and           |

|                           |    |    |     c) Aircraft is not flown in       |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

| 11-2 Boost Switch       C | 1  | 0  | (M)(O)May be inoperative for        | |

|                           |    |    | pressurized flight provided both      |

|                           |    |    | ECS packs operate normally.           |

|                           |    |    |                                       |

|                         C | 1  | 0  | (O)May be inoperative provided the  | |

|                           |    |    | airplane is flown in an               |

|                           |    |    | unpressurized configuration.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 21-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 11-3 ECS Pack Bleed Air A | 2  | 1  | (O)One may be inoperative provided: | |

|      Leak Detection       |    |    |     a) Press to isolate switch        |

|      System               |    |    |        operates normally,             |

|                           |    |    |     b) Associated ECS pack is off,    |

|                           |    |    |     c) Other ECS pack operates        |

|                           |    |    |        normally,                      |

|                           |    |    |     d) Pressurization system          |

|                           |    |    |        operates normally, and         |

|                           |    |    |     e) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                         A | 2  | 0  | (O)Both may be inoperative          | |

|                           |    |    | provided:                             |

|                           |    |    |     a) Both ECS packs are off,        |

|                           |    |    |     b) The airplane is flown in an    |

|                           |    |    |        unpressurized configuration,   |

|                           |    |    |        and                            |

|                           |    |    |     c) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 23-1 Avionics Cooling     |    |    | Deleted, Rev 5.                       |

|      Fan Indicator        |    |    |                                       |

|      Switches             |    |    |                                       |

|                           |    |    |                                       |

| 30-1 Cabin Pressure     C | 1  | 0  | (O)May be inoperative provided:     | |

|      Control System       |    |    |     a) The airplane is flown in an    |

|                           |    |    |        unpressurized configuration,   |

|                           |    |    |        and                            |

|                           |    |    |     b) Extended overwater             |

|                           |    |    |        operations are prohibited.     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 21-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 30-3 Cabin Pressure     C | 2  | 1  | (M)One may be inoperative for       | |

|      Outflow Valves       |    |    | pressurized flight provided:          |

|                           |    |    |     a) The failed valve is locked     |

|                           |    |    |        closed, and                    |

|                           |    |    |     b) Remaining outflow valve        |

|                           |    |    |        operates normally.             |

|                           |    |    |                                       |

|                         C | 2  | 0  | (M)(O)Both may be inoperative       | |

|                           |    |    | provided the airplane is flown in     |

|                           |    |    | an unpressurized configuration.       |

|                           |    |    |                                       |

| 30-4 Cabin Altitude     C | 1  | 0  | (O)May be inoperative for           | |

|      Indicator            |    |    | pressurized flight provided:          |

|                           |    |    |     a) Cabin differential pressure    |

|                           |    |    |        indicator is operative, and    |

|                           |    |    |     b) A chart or table to convert    |

|                           |    |    |        cabin differential pressure    |

|                           |    |    |        to cabin altitude is           |

|                           |    |    |        available to the crew.         |

|                           |    |    |                                       |

| 30-5 Cabin Differential C | 1  | 0  | (O)May be inoperative for           | |

|      Pressure Indicator   |    |    | pressurized flight provided:          |

|                           |    |    |     a) Cabin altitude indicator is    |

|                           |    |    |        operative, and                 |

|                           |    |    |     b) A chart or table converting    |

|                           |    |    |        cabin altitude versus air-     |

|                           |    |    |        craft altitude to differen-    |

|                           |    |    |        tial pressure is available     |

|                           |    |    |        to the crew.                   |

|                           |    |    |                                       |

|                         C | 1  | 0  | (O)May be inoperative provided the  | |

|                           |    |    | airplane is flown in an               |

|                           |    |    | unpressurized configuration.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 21-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 30-6 Cabin Rate of      C | 1  | 0  | (O)May be inoperative provided:     | |

|      Climb Indicator      |    |    |     a) Automatic cabin                |

|                           |    |    |        pressurization control         |

|                           |    |    |        system operates normally,      |

|                           |    |    |        and                            |

|                           |    |    |     b) Cabin differential pressure    |

|                           |    |    |        indicator and cabin            |

|                           |    |    |        altimeter operate normally.    |

|                           |    |    |                                       |

| 51-1 Environmental      C | 2  | 1  | (O)One may be inoperative provided: | |

|      Control System       |    |    |     a) Pressurization system          |

|      Packs                |    |    |        operates normally, and         |

|                           |    |    |     b) Flight level does not exceed   |

|                           |    |    |        FL 250.                        |

|                           |    |    |                                       |

|                         C | 2  | 0  | (O)Both may be inoperative          | |

|                           |    |    | provided:                             |

|                           |    |    |     a) The airplane is flown in an    |

|                           |    |    |        unpressurized configuration,   |

|                           |    |    |     b) Ram air system operates        |

|                           |    |    |        normally,                      |

|                           |    |    |     c) Flight deck temperature can    |

|                           |    |    |        be maintained in a             |

|                           |    |    |        comfortable range (65-85       |

|                           |    |    |        Degrees F), and                |

|                           |    |    |     d) HP bleed switches must both    |

|                           |    |    |        be selected ON during flight   |

|                           |    |    |        in icing conditions.           |

|                           |    |    |                                       |

| 51-2 Recirculation Fans C | 2  | 1  | (O)One may be inoperative provided  | |

|                           |    |    | affected ECS System is operated in    |

|                           |    |    | manual.                               |

|                           |    |    |                                       |

| 51-3 Cabin Ram Air      C | 1  | 0  | May be inoperative provided both    | |

|      System               |    |    | ECS packs operate normally.           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 21-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 51-4 Bleed Air          C | 1  | 0  | (M)May be inoperative with the      | |

|      Crossfeed Valve      |    |    | crossfeed valve in the closed         |

|                           |    |    | position provided both ECS packs      |

|                           |    |    | operate normally.                     |

|                           |    |    |                                       |

|                         C | 1  | 0  | (M)(O)May be inoperative with both  | |

|                           |    |    | packs inoperative or considered       |

|                           |    |    | inoperative provided:                 |

|                           |    |    |     a) Aircraft is flown in an un-    |

|                           |    |    |        pressurized configuration,     |

|                           |    |    |     b) Ram air system operates        |

|                           |    |    |        normally,                      |

|                           |    |    |     c) Flight deck temperature can    |

|                           |    |    |        be maintained in a             |

|                           |    |    |        comfortable range (65-85       |

|                           |    |    |        degrees F), and                |

|                           |    |    |     d) HP bleed switches must both    |

|                           |    |    |        be selected ON during flight   |

|                           |    |    |        in icing conditions.           |

|                           |    |    |                                       |

| 60-1 ECS Pack Automatic C | 2  | 0  | (O)May be inoperative provided:     | |

|      Temperature          |    |    |     a) Manual temperature control     |

|      Control              |    |    |        for the affected pack          |

|                           |    |    |        operates normally,             |

|                           |    |    |     b) Cabin temperature gauge        |

|                           |    |    |        operates normally, and         |

|                           |    |    |     c) Both ECS pack duct             |

|                           |    |    |        temperatures operate           |

|                           |    |    |        normally.                      |

|                           |    |    |                                       |

| 60-2 ECS Pack Manual    C | 2  | 0  | May be inoperative provided         | |

|      Temperature          |    |    | automatic temperature control on      |

|      Control              |    |    | the affected ECS pack operates        |

|                           |    |    | normally.                             |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 21-6     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 60-3 Cabin Temperature  C | 1  | 0  |                                     | |

|      Indicator            |    |    |                                       |

|                           |    |    |                                       |

| 60-4 Flight Deck        C | 1  | 0  |                                     | |

|      Temperature          |    |    |                                       |

|      Indicator            |    |    |                                       |

|                           |    |    |                                       |

| 60-5 Duct Temperature   C | 2  | 1  | One may be inoperative provided the | |

|      Indicators           |    |    | associated ECS pack auto              |

|                           |    |    | temperature control operates          |

|                           |    |    | normally.                             |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 22-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Autopilot System     |    |    |                                       |

|                           |    |    |                                       |

|      1) CAT II Standard C | 2  | 1  | (M)(O)One may be inoperative        | |

|                           |    |    | provided:                             |

|                           |    |    |     a) Remaining autopilot operates   |

|                           |    |    |        normally, and                  |

|                           |    |    |     b) AFM autopilot limitations      |

|                           |    |    |        are observed.                  |

|                           |    |    |                                       |

|      2) CAT I Standard  C | 2  | 1  | (M)One may be inoperative provided  | |

|                           |    |    | basic mode operates normally on the   |

|                           |    |    | remaining autopilot.                  |

|                           |    |    |                                       |

|                         A | 2  | 0  | (M)(O)Both may be inoperative       | |

|                           |    |    | provided:                             |

|                           |    |    |     a) Operations are limited to      |

|                           |    |    |        not more than 2 flight days    |

|                           |    |    |        before repairs are made, and   |

|                           |    |    |     b) An SCS elevator, aileron,      |

|                           |    |    |        and rudder check is per-       |

|                           |    |    |        formed successfully on both    |

|                           |    |    |        autopilot systems at least     |

|                           |    |    |        once each flight day.          |

|                           |    |    |          OR                           |

|                         A |    |    |     c) Operations are limited to    | |

|                           |    |    |        not more than 2 flight days  | |

|                           |    |    |        before repairs are made, and | |

|                           |    |    |     d) An SCS elevator, aileron,    | |

|                           |    |    |        and rudder check is per-       |

|                           |    |    |        formed successfully on at      |

|                           |    |    |        least one autopilot system     |

|                           |    |    |        before each departure.         |

|                           |    |    |                                       |

| ***  3) CAT II Approach C | 1  | 0  | (O)May be inoperative provided      | |

|         Monitoring        |    |    | approach minimums are not dependent   |

|         System            |    |    | upon its use.                         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 22-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-13  Control Wheel    C | 2  | 1  | One may be inoperative provided     | |

|        Disengage          |    |    | autopilot is not engaged below        |

|        Switches           |    |    | 1,500 feet AGL.                       |

|                           |    |    |                                       |

| 10-15  PFD Autopilot    C | 2  | 1  | One may be inoperative provided     | |

|        Warning            |    |    | autopilot is not engaged below        |

|        Indication         |    |    | 1,500 feet AGL.                       |

|                           |    |    |                                       |

| 10-16  Autopilot        C | 6  | 3  | (M)Filaments may be inoperative     | |

|        Controller-        |    |    | provided:                             |

|        Indicator          |    |    |     a) "AP", "SYS 1", and "SYS 2      |

|        Filaments          |    |    |        selections are displayed on    |

|                           |    |    |        EFIS, and                      |

|                           |    |    |     b) "TURB", "1/2 BANK", and "YD"   |

|                           |    |    |        selector filaments operate/    |

|                           |    |    |        illuminate normally.           |

|                           |    |    |                                       |

| 10-17  Autopilot Mode   C | 16 | 0  | (M)Filament(s) may be inoperative   | |

|        Controller Mode    |    |    | in one or both controllers provided   |

|        Selector           |    |    | the associated EFIS displays the      |

|        Filaments          |    |    | selected mode.                        |

|                           |    |    |                                       |

| 20-1 Yaw Damper         C | 2  | 1  |                                     | |

|                           |    |    |                                       |

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

|                           |    |    | provided:                             |

|                           |    |    |     a) SCS rudder check operates      |

|                           |    |    |        normally on at least one       |

|                           |    |    |        system, and                    |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than two flight       |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 23-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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

|      System (VHF, HF,     |    |    |                                       |

|      UHF)                 |    |    |                                       |

|                           |    |    |                                       |

| 11-2 Selective Call     C | -  | 0  |                                     | |

| ***  System (Selcal/      |    |    |                                       |

|      Calsel)              |    |    |                                       |

|                           |    |    |                                       |

| 12-2 ARINC              C | 1  | 0  |                                     | |

| ***  Communications       |    |    |                                       |

|      Addressing and       |    |    |                                       |

|      Reporting System     |    |    |                                       |

|      (ACARS)              |    |    |                                       |

|                           |    |    |                                       |

| 31-1 Passenger Address    |    |    |                                     | |

|      System               |    |    |                                     | |

|                           |    |    |                                       |

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

|         Configuration     |    |    |     a) Alternate normal and emer-   | |

|                           |    |    |        gency procedures and/or      | |

|                           |    |    |        operating restrictions are   | |

|                           |    |    |        established and used, and    | |

|                           |    |    |     b) Flight Deck/Cabin Interphone | |

|                           |    |    |        system operates normally.    | |

|                           |    |    |                                       |

|      2) Cargo           D | 1  | 0  |                                     | |

|         Configuration     |    |    |                                     | |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 23-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-2 Cabin Chimes       C | -  | 0  | (O)May be inoperative provided:     | |

|                           |    |    |     a) Passenger address system       |

|                           |    |    |        operates normally.             |

|                           |    |    |          OR                           |

|                         C |    |    |     b) Alternate procedures are       |

|                           |    |    |        established and used.          |

|                           |    |    |                                       |

| 41-1 Service Interphone C | 1  | 0  | (O)May be inoperative provided:     | |

|      System (Flight       |    |    |     a) Alternate, normal and          |

|      Deck to Cabin)       |    |    |        emergency procedures and/or    |

|      (Cabin to Flight     |    |    |        operating restrictions are     |

|      Deck)(Flight Deck    |    |    |        established and used, and      |

|      to Ground)           |    |    |     b) PA System operates normally.   |

|                           |    |    |                                       |

| 41-2 Cabin Attendants   C | 1  | 0  | (O)May be inoperative provided:     | |

|      Interphone System    |    |    |     a) Alternate, normal and          |

|                           |    |    |        emergency procedures are       |

|                           |    |    |        established and used           |

|                           |    |    |        (including those dependent     |

|                           |    |    |        upon call signal), and         |

|                           |    |    |     b) Passenger address system       |

|                           |    |    |        operates normally.             |

|                           |    |    |                                       |

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

|                           |    |    |        operations.                    |

|                           |    |    |                                       |

| 51-1 Flight Deck        C | -  | 0  | May be inoperative provided head-   | |

|      Speakers             |    |    | sets for flight deck crewmembers      |

|                           |    |    | (including official observer in       |

|                           |    |    | forward observer's seat) are          |

|                           |    |    | installed and operate normally.       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 23-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 51-2 Boom Microphones   A | -  | 0  | May be inoperative provided:        | |

|                           |    |    |     a) Flight Data Recorder (FDR)     |

|                           |    |    |        operates normally,             |

|                           |    |    |     b) Handheld microphone is       | |

|                           |    |    |        available and operates       | |

|                           |    |    |        normally at inoperative      | |

|                           |    |    |        location, and                | |

|                           |    |    |     c) Repairs are made within      | |

|                           |    |    |        three flight days.             |

|                           |    |    |                                       |

| 71-1 Cockpit Voice      A | 1  | 0  | May be inoperative provided:        | |

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

|                           |    |    |        operates normally, and         |

|                           |    |    |     a) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 81-1 Touchtone          C | -  | 0  | (O)May be inoperative provided      | |

| ***  Microphone (DFTM)    |    |    | alternate procedures are            | |

|                           |    |    | established and used.               | |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 24-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-2 APU Generator      C | 1  | 0  | (M)May be inoperative provided APU  | |

| ***                       |    |    | is considered inoperative and is      |

|                           |    |    | not used.                             |

|                           |    |    |                                       |

|                         C | 1  | 0  | (M)May be inoperative and APU air   | |

|                           |    |    | used provided the quill drive is      |

|                           |    |    | removed.                              |

|                           |    |    |                                       |

| 17-1 Battery Heating    C | 1  | 0  | (M)May be inoperative provided:     | |

|      System               |    |    |     a) Batteries are fully charged,   |

|                           |    |    |     b) Battery Overheat Warning       |

|                           |    |    |        System operates normally,      |

|                           |    |    |        and                            |

|                           |    |    |     c) Aircraft is not flown in       |

|                           |    |    |        known or forecast ambient      |

|                           |    |    |        temperatures below -10         |

|                           |    |    |        degrees C.                     |

|                           |    |    |                                       |

| 21-1 Generator on Line  C | 2  | 1  | One may be inoperative provided the | |

|      OFF Indicators       |    |    | associated generator failure          |

|                           |    |    | warnings on the CWP are operating     |

|                           |    |    | normally.                             |

|                           |    |    |                                       |

| 21-2 Generator Failure  C | 2  | 1  | One may be inoperative provided:    | |

|      Warnings on CWP      |    |    |     a) Both aural attention getters   |

|                           |    |    |        are operating normally, and    |

|                           |    |    |     b) Associated generator on line   |

|                           |    |    |        OFF indicator is operating     |

|                           |    |    |        normally.                      |

|                           |    |    |                                       |

| 21-3 Generator Ammeter  C | 1  | 0  | May be inoperative provided:        | |

|                           |    |    |     a) Both generator on line OFF     |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally, and                  |

|                           |    |    |     b) Associated generator           |

|                           |    |    |        voltmeter is operating         |

|                           |    |    |        normally.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 24-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 21-4 Generator          C | 1  | 0  | May be inoperative provided:        | |

|      Voltmeter            |    |    |     a) Both generator on line OFF     |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally, and                  |

|                           |    |    |     b) Associated generator ammeter   |

|                           |    |    |        is operating normally.         |

|                           |    |    |                                       |

| 22-1 Inverter Failure   C | 2  | 1  | One may be inoperative provided:    | |

|      Warning Lights on    |    |    |     a) Both inverters are operating   |

|      CWP                  |    |    |        normally, and                  |

|                           |    |    |     b) Both attention getters are     |

|                           |    |    |        operating normally for this    |

|                           |    |    |        failure indication.            |

|                           |    |    |                                       |

| 22-2 Inverter On Line   C | 2  | 1  | One may be inoperative provided:    | |

|      OFF Indicators       |    |    |     a) Both inverter failure          |

|                           |    |    |        warning lights on the CWP      |

|                           |    |    |        are operating normally, and    |

|                           |    |    |     b) Voltage and Frequency of       |

|                           |    |    |        associated inverter are        |

|                           |    |    |        indicating normally.           |

|                           |    |    |                                       |

| 22-3 Inverter Voltmeter C | 1  | 0  | May be inoperative provided:        | |

|                           |    |    |     a) Both inverters are operating   |

|                           |    |    |        normally,                      |

|                           |    |    |     b) Associated frequency meter     |

|                           |    |    |        is operating normally,         |

|                           |    |    |     c) Both inverter failure          |

|                           |    |    |        warning lights on the CWP      |

|                           |    |    |        are operating normally, and    |

|                           |    |    |     d) Both inverter on line          |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 24-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 22-4 Inverter Frequency C | 1  | 0  | May be inoperative provided:        | |

|      Meter                |    |    |     a) Both inverters are operating   |

|                           |    |    |        normally,                      |

|                           |    |    |     b) Associated voltmeter is        |

|                           |    |    |        operating normally,            |

|                           |    |    |     c) Both inverter failure          |

|                           |    |    |        warning lights on the CWP      |

|                           |    |    |        are operating normally, and    |

|                           |    |    |     d) Both inverter on line          |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally.                      |

|                           |    |    |                                       |

| 31-1 TRU On Line OFF    C | 2  | 1  | (O)One may be inoperative provided: | |

|      Indicators           |    |    |     a) The associated TRU failure     |

|                           |    |    |        warnings on the CWP are        |

|                           |    |    |        operating normally,            |

|                           |    |    |     b) Undervoltage indicators are    |

|                           |    |    |        operating normally, and        |

|                           |    |    |     c) Both attention getters         |

|                           |    |    |        associated with the failure    |

|                           |    |    |        signal operates normally.      |

|                           |    |    |                                       |

| 31-2 TRU Failure        C | 2  | 1  | (O)One may be inoperative provided: | |

|      Indication On The    |    |    |     a) Both attention getters are     |

|      CWP                  |    |    |        operating normally for this    |

|                           |    |    |        failure signal,                |

|                           |    |    |     b) Both TRU on line OFF           |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally,                      |

|                           |    |    |     c) Both undervoltage indicators   |

|                           |    |    |        are operating normally, and    |

|                           |    |    |     d) Both undervoltage warnings     |

|                           |    |    |        are operating normally.        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 24-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-3 Battery/TRU        C | 1  | 0  | (O)May be inoperative provided:     | |

|      Ammeter              |    |    |     a) Both battery on line OFF       |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally,                      |

|                           |    |    |     b) Both TRU on line OFF           |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally,                      |

|                           |    |    |     c) TRU voltmeter is operating     |

|                           |    |    |        normally, and                  |

|                           |    |    |     d) Undervoltage warning system    |

|                           |    |    |        is operating normally.         |

|                           |    |    |                                       |

| 31-4 Battery/TRU        C | 1  | 0  | (O)May be inoperative provided:     | |

|      Voltmeter            |    |    |     a) Both battery on line OFF       |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally,                      |

|                           |    |    |     b) Both TRU on line OFF           |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally,                      |

|                           |    |    |     c) TRU ammeter is operating       |

|                           |    |    |        normally, and                  |

|                           |    |    |     d) Undervoltage warning system    |

|                           |    |    |        is operating normally.         |

|                           |    |    |                                       |

| 32-1 Battery On Line    B | 2  | 1  | (M)(O)One may be inoperative        | |

|      OFF Indicator        |    |    | provided it is determined that the    |

|                           |    |    | associated battery functions          |

|                           |    |    | normally on the bus bar before each   |

|                           |    |    | departure.                            |

|                           |    |    |                                       |

| 34-1 Low Voltage        C | 2  | 1  | (O)One may be inoperative provided: | |

|      Indicators           |    |    |     a) Both undervoltage detectors    |

|                           |    |    |        are operating normally, and    |

|                           |    |    |     b) Low Volts warning on the CWP   |

|                           |    |    |        is operating normally.         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 24-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 40-1 Ground Power       C | 1  | 0  |                                     | |

|      Supply (GPU)         |    |    |                                       |

|      System 200           |    |    |                                       |

|      Volts AC             |    |    |                                       |

|                           |    |    |                                       |

| 40-2 Ground Power       C | 1  | 0  |                                     | |

|      Supply (GPU)         |    |    |                                       |

|      System 28 Volt DC    |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Observer Seat(s)     |    |    |                                     | |

|                           |    |    |                                     | |

|      1) Primary         A | 1  | 0  | May be inoperative provided:        | |

|         Observer Seat     |    |    |     a) A passenger seat in the      | |

|         (Including        |    |    |        passenger cabin is made      | |

|         associated        |    |    |        available to an FAA          | |

|         equipment)        |    |    |        inspector for the            | |

|                           |    |    |        performance of official      | |

|                           |    |    |        duties, and                  | |

|                           |    |    |     b) Repairs are made within two  | |

|                           |    |    |        flight days.                 | |

|                           |    |    |          OR                         | |

|                         A |    |    |     c) Second observer's seat is    | |

|                           |    |    |        available and acceptable to  | |

|                           |    |    |        an FAA inspector for the     | |

|                           |    |    |        performance of official      | |

|                           |    |    |        duties, and                  | |

|                           |    |    |     d) Repairs are made within two  | |

|                           |    |    |        flight days.                 | |

|                           |    |    |          OR                         | |

|                         A |    |    |     e) Primary observer's seat is   | |

|                           |    |    |        available with the required  | |

|                           |    |    |        minimum safety equipment     | |

|                           |    |    |        (safety belt and oxygen) and | |

|                           |    |    |        acceptable to an FAA         | |

|                           |    |    |        inspector for the            | |

|                           |    |    |        performance of official      | |

|                           |    |    |        duties, and                  | |

|                           |    |    |     f) Repairs are made within two  | |

|                           |    |    |        flight days.                 | |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Observer Seat(s)     |    |    |                                     | |

|      (Cont'd)             |    |    |                                     | |

|                           |    |    |                                     | |

|      1) Primary           |    |    | NOTE 1:  These provisos are         | |

|         Observer Seat     |    |    |          intended to provide for    | |

|         (Including        |    |    |          occupancy of the above     | |

|         associated        |    |    |          seats by an FAA inspector  | |

|         equipment)        |    |    |          when the minimum safety    | |

|         (Cont'd)          |    |    |          equipment (oxygen and      | |

|                           |    |    |          safety belt) is functional | |

|                           |    |    |          and the inspector          | |

|                           |    |    |          determines the conditions  | |

|                           |    |    |          to be acceptable.          | |

|                           |    |    |                                       |

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

|                           |    |    |          determine if the minimum   | |

|                           |    |    |          safety equipment is        | |

|                           |    |    |          functional for other       | |

|                           |    |    |          persons authorized to      | |

|                           |    |    |          occupy any observer        | |

|                           |    |    |          seat(s).                   | |

|                           |    |    |                                       |

| ***  2) Additional      D | -  | 0  |                                     | |

|         Observer          |    |    | NOTE:  The Pilot-in-Command will    | |

|         Seat(s)           |    |    |        determine if the minimum     | |

|         (Including        |    |    |        safety equipment is          | |

|         associated        |    |    |        functional for other persons | |

|         equipment)        |    |    |        authorized to occupy any     | |

|                           |    |    |        observer seat(s).            | |

|                           |    |    |                                       |

| 10-11  Pilot's Seat     C | 2  | 0  | (M)May be inoperative provided:     | |

|        Adjustment         |    |    |     a) Position of the seat(s)        |

|        System             |    |    |        permits normal pilot           |

|                           |    |    |        visibility and full flight     |

|                           |    |    |        control movement, and          |

|                           |    |    |     b) Seat(s) is secured with        |

|                           |    |    |        mechanical stops.              |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-12  Crewmember         |    |    | DELETED, REV 1.                       |

|        Shoulder Harness   |    |    |                                       |

|                           |    |    |                                       |

| 20-1 "Fasten Seat Belt  C | -  | -  | One or more signs or placards may   | |

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

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

|                           |    |    | from each occupied passenger seat.    |

|                           |    |    |                                       |

| 21-1 Flight Attendant   C | -  | -  | (M)(O)One single or one dual        | |

|      Seat Assembly        |    |    | position seat may be inoperative      |

|      (Single or Dual      |    |    | provided:                             |

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

|                           |    |    |        not occupied,                  |

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

|                           |    |    |        displaced by inoperative       |

|                           |    |    |        seat position(s) occupy the    |

|                           |    |    |        passenger seat(s) most         |

|                           |    |    |        accessible to their assigned   |

|                           |    |    |        exit,                          |

|                           |    |    |     c) Alternate procedures are       |

|                           |    |    |        established for displaced      |

|                           |    |    |        flight attendant(s),           |

|                           |    |    |     d) Folding type seat(s) is        |

|                           |    |    |        stowed or secured in the       |

|                           |    |    |        retracted position, and        |

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

|                           |    |    |        to flight attendant(s) is      |

|                           |    |    |        placarded "FOR FLIGHT          |

|                           |    |    |        ATTENDANT USE ONLY".           |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  A folding seat that will     |

|                           |    |    |          not stow automatically is    |

|                           |    |    |          considered inoperative.      |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 21-1 Flight Attendant     |    |    | NOTE 2:  A seat position with an      |

|      Seat Assembly        |    |    |          inoperative or missing lap   |

|      (Single or Dual      |    |    |          belt is considered           |

|      Position) (Cont'd)   |    |    |          inoperative.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 3:  The above provisos apply     |

|                           |    |    |          only to required flight      |

|                           |    |    |          attendant seats.  Seats in   |

|                           |    |    |          excess of those required     |

|                           |    |    |          may be inoperative           |

|                           |    |    |          provided they are properly   |

|                           |    |    |          stowed or secured in the     |

|                           |    |    |          retracted position.          |

|                           |    |    |          Individual operators, when   |

|                           |    |    |          operating with inoperative   |

|                           |    |    |          seats, will consider the     |

|                           |    |    |          locations and combinations   |

|                           |    |    |          of seats to ensure that      |

|                           |    |    |          the proximity to exits and   |

|                           |    |    |          distribution requirements    |

|                           |    |    |          of the applicable FAR are    |

|                           |    |    |          met.                         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 22-12  Passenger Seats    |    |    |                                       |

|        and Belts          |    |    |                                       |

|                           |    |    |                                       |

|      1) Seat Backs      C | -  | -  | (M)May be inoperative secured in    | |

|                           |    |    | the upright position.                 |

|                           |    |    |                                       |

|                         C | -  | -  | (M)May be inoperative in other than | |

|                           |    |    | the upright position provided:        |

|                           |    |    |     a) Does not block an Emergency    |

|                           |    |    |        Exit.                          |

|                           |    |    |     b) Does not restrict any pass-    |

|                           |    |    |        enger from access to the       |

|                           |    |    |        main aircraft aisle,           |

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

|                           |    |    |        blocked and placarded "Do      |

|                           |    |    |        Not Occupy", and               |

|                           |    |    |     d) May not be required by a       |

|                           |    |    |        Flight Attendant who needs     |

|                           |    |    |        to be moved due to an          |

|                           |    |    |        inoperative seat.              |

|                           |    |    |                                       |

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

|                           |    |    |          inoperative or missing lap   |

|                           |    |    |          belt is considered           |

|                           |    |    |          inoperative.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  Inoperative seats do not     |

|                           |    |    |          affect the required number   |

|                           |    |    |          of Flight Attendants.        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-6     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 22-13  Underseat        C | -  | -  | (M)(O)May be inoperative provided:  | |

|        Baggage            |    |    |     a) Baggage is not stowed under  | |

|        Restraining Bars   |    |    |        seat with inoperative        | |

|                           |    |    |        restraining bar,             | |

|                           |    |    |     b) Associated seat is placarded | |

|                           |    |    |        "DO NOT STOW BAGGAGE UNDER   | |

|                           |    |    |        THIS SEAT", and              | |

|                           |    |    |     c) Procedures are established   | |

|                           |    |    |        to alert Cabin Crew of inop- | |

|                           |    |    |        erative restraining bar.     | |

|                           |    |    |                                       |

| 30-1 Passenger            | -  | 0  | Passenger convenience items, as     | |

| ***  Convenience          |    |    | expressed in this MMEL, are those     |

|      Item(s)              |    |    | items related to passenger comfort,   |

|                           |    |    | convenience, or entertainment such    |

|                           |    |    | as, but not limited to: galley        |

|                           |    |    | equipment, movie equipment, ash       |

|                           |    |    | trays, stereo, equipment, overhead    |

|                           |    |    | reading lamps, etc.  Items            |

|                           |    |    | addressed elsewhere in this           |

|                           |    |    | document shall not be included. (M)   |

|                           |    |    | and (O) procedures may be required    |

|                           |    |    | and included in the Air Carrier's     |

|                           |    |    | appropriate document.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE:  Lavatory door ash trays are    |

|                           |    |    |        not considered passenger       |

|                           |    |    |        convenience items.             |

|                           |    |    |                                       |

| 40-1 Lavatory Hot Water C | 1  | 0  | (M)May be inoperative provided      | |

|      Heater               |    |    | heater is deactivated and secured.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-7     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 40-2 Lavatory Door        |    |    |                                     | |

|      Ashtrays             |    |    |                                     | |

|                           |    |    |                                       |

|      1) Airplanes with  A | -  | -  | One may be missing provided it is   | |

|         more than one     |    |    | replaced within 10 calendar days.   | |

|         lavatory door     |    |    |                                     | |

|         ashtray           |    |    |                                     | |

|         installed         |    |    |                                     | |

|                           |    |    |                                       |

|      2) Airplanes with  A | 1  | 0  | May be missing provided it is       | |

|         only one          |    |    | replaced within 3 calendar days.    | |

|         lavatory door     |    |    |                                     | |

|         ashtray           |    |    |                                     | |

|         installed         |    |    |                                     | |

|                           |    |    |                                       |

| 60-1 Emergency Locator  C | -  | -  | As required by FAR.                 | |

|      Transmitter          |    |    |                                       |

|                           |    |    |                                       |

| 60-2 Megaphones         C | -  | 1  | Any in excess of those required by  | |

|                           |    |    | FAR may be inoperative or missing     |

|                           |    |    | provided:                             |

|                           |    |    |     a) Inoperative megaphone is       |

|                           |    |    |        removed from the passenger     |

|                           |    |    |        cabin, and                     |

|                           |    |    |     b) Required distribution is       |

|                           |    |    |        maintained.                    |

|                           |    |    |                                       |

| 60-3 Cabin Emergency    C | -  | -  | May be in operative or missing      | |

|      Flashlight Holder/   |    |    | provided the crewmember assigned to   |

|      Flashlights          |    |    | the affected position has a           |

|                           |    |    | normally operating flashlight         |

|                           |    |    | readily available.                    |

|                           |    |    |                                       |

| 60-4 First Aid Kits     D | -  | -  | Any in excess of those required by  | |

|                           |    |    | FAR may be incomplete or missing    | |

|                           |    |    | provided required distribution is   | |

|                           |    |    | maintained.                         | |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 25-8     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 60-5 Emergency Medical    |    |    | DELETED  REV. 1.                      |

|      Kits                 |    |    |                                       |

|                           |    |    |                                       |

| 60-6 Girt Bar Heater    C | 3  | 0  | (M)May be inoperative provided:     | |

| ***                       |    |    |     a) Associated heater is           |

|                           |    |    |        deactivated and secured, and   |

|                           |    |    |     b) Associated girt bar and        |

|                           |    |    |        arming mechanism operate       |

|                           |    |    |        normally.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 26-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Condition Lever    A | 2  | 1  | One may be inoperative provided:    | |

|      Fire Warning         |    |    |     a) CWP warning and associated     |

|      Indicator            |    |    |        center roof panel fire         |

|                           |    |    |        warning PBSI's operate         |

|                           |    |    |        normally, and                  |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 10-2 APU Fire           C | 1  | 0  | (M)May be inoperative provided APU  | |

| ***  Detection System     |    |    | is considered inoperative and is      |

|                           |    |    | not used.                             |

|                           |    |    |                                       |

| 10-3 APU Fire           C | 1  | 0  | (M)May be inoperative provided APU  | |

| ***  Detection System     |    |    | is considered inoperative and is      |

|      Test Function        |    |    | not used.                             |

|                           |    |    |                                       |

| 10-4 APU Fire           C | 1  | 0  | (M)May be missing provided:         | |

| ***  Extinguisher         |    |    |     a) APU is considered inop-        |

|      Thermal Discharge    |    |    |        ertive and is not used, and    |

|      Disc                 |    |    |     b) APU start control circuit      |

|                           |    |    |        breaker is pulled.             |

|                           |    |    |          OR                           |

|                         C |    |    |     b) Another acceptable means of    |

|                           |    |    |        determining that the bottle    |

|                           |    |    |        is fully charged is used       |

|                           |    |    |        once each flight day.          |

|                           |    |    |                                       |

| 11-0 Engine Fire          |    |    | DELETED, REV 1.                       |

|      Detection Switch     |    |    |                                       |

|      System               |    |    |                                       |

|                           |    |    |                                       |

| 11-1 APU Fire           C | 1  | 0  | (M)May be inoperative provided APU  | |

| ***  Extinguisher         |    |    | is considered inoperative and is    | |

|      System               |    |    | not used.                           | |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 26-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 12-1 APU Fire           C | 1  | 0  | (M)May be inoperative provided:     | |

| ***  Detection Warning    |    |    |     a) Fire warning bell operates     |

|      Horn                 |    |    |        normally,                      |

|                           |    |    |     b) APU control panel fire         |

|                           |    |    |        warning indicators operate     |

|                           |    |    |        normally,                      |

|                           |    |    |     c) Auto shut down system          |

|                           |    |    |        operates normally, and         |

|                           |    |    |     d) A qualified person remains     |

|                           |    |    |        on the flight deck any time    |

|                           |    |    |        the APU is running.            |

|                           |    |    |                                       |

| 12-2 Engine Fire        A | 4  | 2  | (O)One loop on each engine may be     |

| ***  Detection Loops      |    |    | inoperative provided:                 |

|      (Dual Loop System)   |    |    |     a) Inoperative loop is            |

|                           |    |    |        isolated, and                  |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 13-1 Nacelle Bleed Air  C | 2  | 1  | (O)One may be inoperative provided: | |

|      Supply Leak          |    |    |     a) Associated bleed air supply    |

|      Detection System     |    |    |        (both engine and HP bleeds)    |

|                           |    |    |        is off, and                    |

|                           |    |    |     b) The airplane is not flown      |

|                           |    |    |        into known or forecast icing   |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

| 15-1 Forward Cargo      C | 1  | 0  | (O)May be inoperative provided      | |

| ***  Compartment Smoke    |    |    | airflow panel is verified closed.     |

|      Detection System     |    |    |                                       |

|                           |    |    |                                       |

| 15-2 Aft Cargo          C | 1  | 0  | (O)May be inoperative provided      | |

| ***  Compartment Smoke    |    |    | airflow panel is verified closed.     |

|      Detection System     |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 26-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 17-1 Lavatory Smoke     C | -  | 0  | M)(O)For each lavatory, the         | |

|      Detection System     |    |    | lavatory smoke detection system may   |

|                           |    |    | be inoperative provided:              |

|                           |    |    |     a) Lavatory fire extinguisher     |

|                           |    |    |        system operates normally.      |

|                           |    |    |          OR                           |

|                         C |    |    |     b) Lavatory waste receptacle is   |

|                           |    |    |        empty,                         |

|                           |    |    |     c) Lavatory door is locked        |

|                           |    |    |        CLOSED and placarded,          |

|                           |    |    |        "INOPERATIVE - DO NOT          |

|                           |    |    |        ENTER", and                    |

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

|                           |    |    |        purpose.                       |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  These provisos are not       |

|                           |    |    |          intended to prohibit         |

|                           |    |    |          lavatory inspections by      |

|                           |    |    |          crewmembers.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  A lavatory 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: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 26-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 20-1 Lavatory Fire      C | 1  | 0  | (M)(O)For each lavatory, the        | |

|      Extinguisher         |    |    | lavatory fire extinguisher system     |

|      System               |    |    | may be inoperative provided:          |

|                           |    |    |     a) Lavatory smoke detector        |

|                           |    |    |        system operates normally.      |

|                           |    |    |          OR                           |

|                         C |    |    |     b) Lavatory waste receptacle is   |

|                           |    |    |        empty,                         |

|                           |    |    |     c) Lavatory door is locked        |

|                           |    |    |        CLOSED and placarded           |

|                           |    |    |        "INOPERATIVE - DO NOT          |

|                           |    |    |        ENTER", and                    |

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

|                           |    |    |        purpose.                       |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  These provisos are not       |

|                           |    |    |          intended to prohibit         |

|                           |    |    |          lavatory inspections by      |

|                           |    |    |          crewmembers.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  A lavatory fire              |

|                           |    |    |          extinguisher system is not   |

|                           |    |    |          required for all-cargo       |

|                           |    |    |          operations.                  |

|                           |    |    |                                       |

| 21-1 Engine Fire        C | 2  | 0  | (M)One or both may be missing       | |

|      Extinguisher         |    |    | provided an accepted procedure is     |

|      Discharge            |    |    | used to verify adequacy of bottle     |

|      Indicators (Discs)   |    |    | charge before each departure.         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 26-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 21-2 Engine Fire        C | 4  | 3  | (M)(O)One indicator may be inop-    | |

|      Extinguisher         |    |    | erative on the No. 2 Shot system      |

|      Discharged Shot      |    |    | only, provided:                       |

|      Indicator            |    |    |     a) All remaining indicators       |

|                           |    |    |        operate normally before        |

|                           |    |    |        engine start,                  |

|                           |    |    |     b) Discharge Disc is in place     |

|                           |    |    |        before each departure, and     |

|                           |    |    |     c) Fire extinguisher discharge    |

|                           |    |    |        indicator pin is checked       |

|                           |    |    |        once each flight day.          |

|                           |    |    |                                       |

| 22-1 Portable Fire      D | -  | -  | (M)Any in excess of those required  | |

|      Extinguishers        |    |    | by FAR may be inopertative or       | |

|                           |    |    | missing provided:                   | |

|                           |    |    |     a) Inoperative fire             | |

|                           |    |    |        extinguisher is tagged       | |

|                           |    |    |        inoperative, removed from    | |

|                           |    |    |        installed location, and      | |

|                           |    |    |        placed out of sight so it    | |

|                           |    |    |        cannot be mistaken for a     | |

|                           |    |    |        functional unit, and         | |

|                           |    |    |     b) Required distribution is     | |

|                           |    |    |        maintained.                  | |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 27-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 27  FLIGHT CONTROLS       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Trim Tab           C | 3  | 1  | DELETED, REV 1.                       |

|      Indicators           |    |    |                                       |

|      (Aileron & Rudder)   |    |    |                                       |

|                           |    |    |                                       |

| 21-1 Rudder Pedal       C | 2  | 0  | (M)One or both may be inoperative   | |

|      Adjustment System    |    |    | provided:                             |

|                           |    |    |     a) Adjustments can be secured     |

|                           |    |    |        in a position which suits      |

|                           |    |    |        individual pilot(s)            |

|                           |    |    |        requirements, and              |

|                           |    |    |     b) Position of pedal(s) permits   |

|                           |    |    |        normal full flight control     |

|                           |    |    |        movement.                      |

|                           |    |    |                                       |

| 30-1 Electric Trim      C | 2  | 1  | (O)Trim switch assembly on one      | |

|      Switch(es)           |    |    | pilots control column may be          |

|      (Elevator)           |    |    | inoperative provided:                 |

|                           |    |    |     a) Electric trim switch on the    |

|                           |    |    |        other control column           |

|                           |    |    |        operates normally,             |

|                           |    |    |     b) Manual trim system operates    |

|                           |    |    |        normally,                      |

|                           |    |    |     c) Autotrim (autopilot)           |

|                           |    |    |        operates normally,             |

|                           |    |    |     d) Both autopilot disconnect      |

|                           |    |    |        buttons operate normally,      |

|                           |    |    |        and                            |

|                           |    |    |     e) Trim indicator (SCS) on        |

|                           |    |    |        right hand instrument panel    |

|                           |    |    |        operates normally.             |

|                           |    |    |                                       |

| 34-1 Stall Warning      C | 2  | 1  | (M)One may be inoperative provided  | |

|      System               |    |    | remaining system and stick shaker     |

|                           |    |    | operates normally and is checked      |

|                           |    |    | before each departure.                |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 27-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 27  FLIGHT CONTROLS       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 34-2 Stall Warning      A | 2  | 1  | (M)One stall warning vane heater    | |

|      De-Ice System        |    |    | may be inoperative provided:          |

|      Vane Heaters         |    |    |     a) Remaining stall warning        |

|                           |    |    |        de-ice system channel          |

|                           |    |    |        operates normally,             |

|                           |    |    |     b) Remaining (non-associated)     |

|                           |    |    |        stall warning system           |

|                           |    |    |        operates normally, and is      |

|                           |    |    |        checked before each            |

|                           |    |    |        departure, and                 |

|                           |    |    |     c) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 51-1 Flap Motor         A | 1  | 0  | (M)(O)May be inoperative provided:  | |

|      Running Light        |    |    |     a) Flap motor is operating        |

|                           |    |    |        normally before each           |

|                           |    |    |        departure,                     |

|                           |    |    |     b) Associated flap motor is       |

|                           |    |    |        monitored on the right hand    |

|                           |    |    |        TRU ammeter while flaps are    |

|                           |    |    |        running, and                   |

|                           |    |    |     c) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 51-3 Wing Flap          A | 1  | 0  | (M)(O)May be inoperative provided:  | |

|      Position             |    |    |     a) Flap position is verified      |

|      Indicator            |    |    |        before each takeoff,           |

|                           |    |    |     b) Flaps are verified to          |

|                           |    |    |        operate normally throughout    |

|                           |    |    |        the operating range at least   |

|                           |    |    |        once each flight day, and      |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 27-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 27  FLIGHT CONTROLS       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 70-1 Control (Gust)     A | 1  | 0  | (M)(O)May be inoperative provided:  | |

|      Locks System         |    |    |     a) System is inspected to         |

|                           |    |    |        ensure non-interference with   |

|                           |    |    |        throttle and primary flight    |

|                           |    |    |        control systems,               |

|                           |    |    |     b) Alternative methods of         |

|                           |    |    |        securing flight controls are   |

|                           |    |    |        used,                          |

|                           |    |    |     c) Aircraft shall not be taxied   |

|                           |    |    |        in tailwind components         |

|                           |    |    |        greater than 25 knots, and     |

|                           |    |    |     d) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 28-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 28  FUEL                  |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 20-1 Fuel Boost Pumps   C | 4  | 2  | (M)One may be inoperative in each   | |

|                           |    |    | collector tank.                       |

|                           |    |    |                                       |

| 20-4 Pressure           C | 1  | 0  | (M)May be inoperative provided an   | |

|      Refueling System     |    |    | alternate refueling procedure is      |

|                           |    |    | used.                                 |

|                           |    |    |                                       |

| 41-1 Refueling Panel    C | 2  | 0  | (M)May be inoperative provided fuel | |

|      Quantity             |    |    | in associated tank is verified by     |

|      Indicators           |    |    | an alternate procedure before each    |

|                           |    |    | departure.                            |

|                           |    |    |                                       |

| 41-2 Refueling Panel    C | 1  | 0  | (M)May be inoperative provided:     | |

|      Overfull System      |    |    |     a) Alternate procedures are       |

|                           |    |    |        used to prevent overfilling    |

|                           |    |    |        of tanks, and                  |

|                           |    |    |     b) Fuel in tanks is verified by   |

|                           |    |    |        an alternate procedure         |

|                           |    |    |        before each departure.         |

|                           |    |    |                                       |

| 41-3 Main Tank Fuel     C | 2  | 1  | (M)One may be inoperative provided: | |

|      Quantity             |    |    |     a) Both fuel flow meters          |

|      Indicators           |    |    |        operate normally,              |

|      (Flight Deck)        |    |    |     b) Both fuel used indicators      |

|                           |    |    |        operate normally, and          |

|                           |    |    |     c) Fuel quantity in associated    |

|                           |    |    |        tank is determined by an       |

|                           |    |    |        alternate procedure before     |

|                           |    |    |        each departure.                |

|                           |    |    |                                       |

| 41-4 Fuel Indicator     C | 1  | 0  | (M)May be inoperative provided fuel | |

|      Test Switch          |    |    | quantity is determined by an          |

|                           |    |    | alternate procedure.                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 28-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 28  FUEL                  |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 42-1 Magnetic Fuel      C | 8  | 0  | (M)(O)May be inoperative provided   | |

|      Quantity             |    |    | fuel quantity is determined by an     |

|      Indicators           |    |    | alternate procedure.                  |

|      (MFLI's) (Dripless   |    |    |                                       |

|      Sticks)              |    |    |                                       |

|                           |    |    |                                       |

| 43-1 Fuel Tank          C | 1  | 0  | (O)May be inoperative provided:     | |

|      Temperature          |    |    |     a) Total Air Temperature or       |

|      Indicating System    |    |    |        Static Air Temperature is      |

|                           |    |    |        substituted for indication     |

|                           |    |    |        of fuel temperature, and       |

|                           |    |    |     b) AFM limitations are            |

|                           |    |    |        observed.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 29-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 29  HYDRAULIC POWER       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-1 Hydraulic Pump     C | 2  | 0  | (M)(O)Both may be inoperative       | |

|      Depressurizing       |    |    | provided the valve is in the full     |

|      Valve Solenoid       |    |    | pressure position, solenoid           |

|                           |    |    | de-energized.                         |

|                           |    |    |                                       |

| 20-1 Ground Servicing   C | 1  | 0  | (M)May be inoperative provided it   | |

|      Valve                |    |    | is secured in the CLOSED position.    |

|                           |    |    |                                       |

| 31-1 Hydraulic LO LEVEL C | 1  | 0  | (M)May be inoperative provided      | |

|      Warning Light On     |    |    | hydraulic quantity is verified        |

|      CWP                  |    |    | before each departure.                |

|                           |    |    |                                       |

| 31-2 Main Hydraulic     C | 1  | 0  | (M)May be inoperative provided      | |

|      Quantity Low Level   |    |    | hydraulic quantity is verified        |

|      Warning Light        |    |    | before each departure.                |

|                           |    |    |                                       |

| 31-3 Auxiliary          C | 1  | 0  | (M)May be inoperative provided      | |

|      Hydraulic Low        |    |    | hydraulic quantity is verified        |

|      Level Warning        |    |    | before each departure.                |

|      Light                |    |    |                                       |

|                           |    |    |                                       |

| 33-1 Main Hydraulic     C | 1  | 0  | (O)May be inoperative provided:     | |

|      Pressure Indicator   |    |    |     a) Both brake system pressure     |

|                           |    |    |        indicators are operating       |

|                           |    |    |        normally, and                  |

|                           |    |    |     b) Associated hydraulic system    |

|                           |    |    |        pressure is verified before    |

|                           |    |    |        each departure.                |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 30-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| 10-01  Airframe         C | 1  | 0  | (M)(O)May be inoperative provided:  | |

|        De-Icing System    |    |    |     a) The airplane is not flown      |

|        (Wing and          |    |    |        into known or forecast icing   |

|        Empennage)         |    |    |        conditions, and                |

|                           |    |    |     b) De-icing boots are kept in     |

|                           |    |    |        the deflation cycle.           |

|                           |    |    |                                       |

| 10-02  Airframe         C | 1  | 0  | (O)May be inoperative provided:     | |

|        De-Icing           |    |    |     a) Airframe de-icing pressure     |

|        Monitoring         |    |    |        indicator operates normally.   |

|        System (Wing and   |    |    |          OR                           |

|        Empennage)       C |    |    |     b) The airplane is not flown      |

|                           |    |    |        into known or forecast icing   |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

| 10-03  Airframe         C | 1  | 0  | (O)May be inoperative provided:     | |

|        De-Icing Timer     |    |    |     a) Manual de-icing system         |

|                           |    |    |        operates normally.             |

|                           |    |    |          OR                           |

|                         C |    |    |     b) The airplane is not flown      |

|                           |    |    |        into known or forecast icing   |

|                           |    |    |        conditions, and                |

|                           |    |    |     c) De-icing boots are in a        |

|                           |    |    |        deflation cycle.               |

|                           |    |    |                                       |

| 10-04  Airframe         C | 1  | 0  | May be inoperative provided:        | |

|        De-Icing           |    |    |     a) Airframe de-icing monitoring   |

|        Pressure           |    |    |        system operates normally.      |

|        Indicator          |    |    |          OR                           |

|                         C |    |    |     b) The airplane is not flown      |

|                           |    |    |        into known or forecast icing   |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 30-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| 20-00  Engine De-Icing  C | 2  | 1  | One may be inoperative provided the | |

|        Systems            |    |    | airplane is not flown into known or   |

|                           |    |    | forecast icing conditions.            |

|                           |    |    |                                       |

| 20-01  Engine and       C | 2  | 0  | One or both may be inoperative      | |

|        Propeller          |    |    | provided the airplane is not flown    |

|        De-Icing           |    |    | into known or forecast icing          |

|        Transfer Switch    |    |    | conditions.                           |

|                           |    |    |                                       |

| 20-02  Engine De-Icing  C | 1  | 0  |                                     | |

|        Phase Current      |    |    |                                       |

|        Selector           |    |    |                                       |

|                           |    |    |                                       |

| 30-01  Main Pitot Heat  B | 2  | 1  | (M)May be inoperative provided the  | |

|        Systems            |    |    | airplane is not flown into known or   |

|                           |    |    | forecast icing conditions.            |

|                           |    |    |                                       |

| 30-02  Pitot Head       B | 3  | 2  | (O)One may be inoperative provided: | |

|        Heater Warning     |    |    |     a) Associated CWP warning         |

|        Lights             |    |    |        system operates normally,      |

|                           |    |    |        and                            |

|                           |    |    |     b) All other components of the    |

|                           |    |    |        pitot heat system are          |

|                           |    |    |        functioning normally.          |

|                           |    |    |                                       |

| 30-03  Static Port      B | 2  | 1  | One may be inoperative provided the | |

|        Heaters            |    |    | airplane is not flown into known or   |

|                           |    |    | forecast icing conditions.            |

|                           |    |    |                                       |

| 41-01  Windshield       C | 2  | 1  | One may be inoperative provided the | |

|        Heating System     |    |    | airplane is not flown into known or   |

|                           |    |    | forecast icing conditions.            |

|                           |    |    |                                       |

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

|                           |    |    | the airplane is operated in Day VMC   |

|                           |    |    | flight conditions, and temperatures   |

|                           |    |    | remain 6 degrees C or above.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 30-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| 41-03  Windshield Heat  C | 2  | 0  | (O)May be inoperative provided      | |

|        Master PBSI        |    |    | associated windshield heat system     |

|        Lights             |    |    | operates normally.                    |

|                           |    |    |                                       |

| 41-04  Windshield Heat    |    |    |                                       |

|        Overtemp Warning   |    |    |                                       |

|        Lights             |    |    |                                       |

|                           |    |    |                                       |

|        1) Main          C | 2  | 1  | One may be inoperative provided:    | |

|           Windshield      |    |    |     a) Associated windshield master   |

|                           |    |    |        heat switch is selected OFF,   |

|                           |    |    |        and                            |

|                           |    |    |     b) Airplane is not flown into     |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

|        2) Side          C | 2  | 1  | One may be inoperative provided:    | |

|           Windshield      |    |    |     a) Associated windshield master   |

|                           |    |    |        heat switch is selected OFF,   |

|                           |    |    |        and                            |

|                           |    |    |     b) Airplane is not flown into     |

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 30-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| 42-01  Windshield       C | 2  | 0  | May be inoperative provided the     | |

|        Wipers System      |    |    | airplane is not flown in              |

|                           |    |    | precipitation within 5 nautical       |

|                           |    |    | miles of the airport of takeoff or    |

|                           |    |    | intended landing.                     |

|                           |    |    |                                       |

|        1) Windshield    C | 1  | 0  | (M)May be inoperative for all       | |

|           Wiper Park      |    |    | flight conditions provided the        |

|           Function        |    |    | blade(s) can be positioned in a       |

|                           |    |    | location that will not obstruct       |

|                           |    |    | forward vision.                       |

|                           |    |    |                                       |

|        2) Windshield    C | 2  | 2  | Slow function may be inoperative    | |

|           Wiper           |    |    | provided fast function operates       |

|           Fast/Slow       |    |    | normally.                             |

|           Selection       |    |    |                                       |

|                           |    |    |                                       |

| 43-00  Rain             C | 1  | 0  |                                     | |

| ***    Repellent System   |    |    |                                       |

|                           |    |    |                                       |

| 43-01  Windshield       C | 2  | 0  |                                     | |

|        Washer System      |    |    |                                       |

|                           |    |    |                                       |

| 60-01  Propeller        C | 2  | 0  | May be inoperative provided the     | |

|        De-Icing Systems   |    |    | airplane is not flown into known or   |

|                           |    |    | forecast icing conditions.            |

|                           |    |    |                                       |

| 70-01  Drain Mast       C | 1  | 0  | (M)May be inoperative provided:     | |

|        Heater             |    |    |     a) Heater is deactivated and      |

|                           |    |    |        secured, and                   |

|                           |    |    |     b) Associated water supply is     |

|                           |    |    |        shut off.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 31-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 31  INDICATING/RECORDING  |    |    |                                       |

|     SYSTEMS               |    |    |                                       |

|                           |    |    |                                       |

| 21-01  Clock            C | -  | 1  |                                     | |

|                           |    |    |                                       |

| 22-01  Fatigue Meter    C | 1  | 0  |                                     | |

|                           |    |    |                                       |

| 30-00  AIDS             C | 1  | 0  |                                     | |

| ***    Maintenance        |    |    |                                       |

|        Recorder           |    |    |                                       |

|                           |    |    |                                       |

| 30-01  Hour Meter       C | 1  | 0  |                                     | |

|                           |    |    |                                       |

| 31-01  Flight Data      A | 1  | 0  | May be inoperative provided:        | |

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

|                           |    |    |        operates normally, and         |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 51-01  Red Flashing     C | 2  | 1  | One may be inoperative provided     | |

|        Attention          |    |    | master warning aural alert and all    |

|        Getting Lights     |    |    | discrete warning lights operate       |

|                           |    |    | normally.                             |

|                           |    |    |                                       |

| 51-02  Amber Flashing   C | 2  | 1  | One may be inoperative provided     | |

|        Attention          |    |    | master warning aural alert and all    |

|        Getting Lights     |    |    | discrete caution lights operate       |

|                           |    |    | normally.                             |

|                           |    |    |                                       |

| 51-03  Aural Attention  C | 1  | 0  | May be inoperative provided:        | |

|        Warning Horn       |    |    |     a) Both flashing attention        |

|        (CWP)              |    |    |        getting lights operate         |

|                           |    |    |        normally, and                  |

|                           |    |    |     b) All CWP warning lights         |

|                           |    |    |        operate normally.              |

|                           |    |    |                                       |

| 51-04  Central Warning  C | 1  | 0  | May be inoperative so as to remain  | |

|        Panel Dimming      |    |    | in the bright mode for day            |

|        System             |    |    | operations only.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 32-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 32  LANDING GEAR          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 42-1 Brake Isolation    C | 2  | 0  | (M)One or both may be inoperative   | |

|      Cock (Valve)         |    |    | provided isolation cock(s) are        |

|      Indicators           |    |    | checked once each flight day for      |

|                           |    |    | normal operation.                     |

|                           |    |    |                                       |

| 42-2 Brake Pressure     C | 2  | 1  | (O)One may be inoperative provided: | |

|      Supply Indication    |    |    |     a) Main hydraulic pressure        |

|      System               |    |    |        indicator operates normally,   |

|                           |    |    |     b) All four brake line pressure   |

|                           |    |    |        indicators operate normally,   |

|                           |    |    |     c) Brake pressure low pressure    |

|                           |    |    |        warning light(s) operate       |

|                           |    |    |        normally.                      |

|                           |    |    |                                       |

| 42-3 Brake Pressure     A | 1  | 0  | May be inoperative provided:        | |

|      Low Pressure         |    |    |     a) Brake pressure supply          |

|      Warning Light        |    |    |        indicators operate normally,   |

|                           |    |    |        and                            |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 32-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 32  LANDING GEAR          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 42-4 Brake Line         A | 4  | 2  | One may be inoperative in the inner | |

|      Pressure Indicator   |    |    | system and one in the outer system    |

|                           |    |    | provided:                             |

|                           |    |    |     a) Associated brake low           |

|                           |    |    |        pressure lights operate        |

|                           |    |    |        normally,                      |

|                           |    |    |     c) Inoperative indicators are     |

|                           |    |    |        not on the same side, and      |

|                           |    |    |     d) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 42-6 Brake Temperature  A | 4  | 3  | (M)(O)One may be inoperative        | |

|      Sensor               |    |    | provided:                             |

|                           |    |    |     a) Brake temperature gauge        |

|                           |    |    |        (analogue) operates            |

|                           |    |    |        normally.                      |

|                           |    |    |     b) Remaining three brake temp-    |

|                           |    |    |        erature channels indicate a    |

|                           |    |    |        temperature of less than 180   |

|                           |    |    |        degrees C before flight,       |

|                           |    |    |     c) Landing Gear Bay Overheat      |

|                           |    |    |        detection system operates      |

|                           |    |    |        normally,                      |

|                           |    |    |     d) Should a rejected take-off     |

|                           |    |    |        occur, the aircraft must be    |

|                           |    |    |        inspected before the next      |

|                           |    |    |        flight, and                    |

|                           |    |    |     e) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 32-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 32  LANDING GEAR          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 42-7 Brake Temperature  C | 1  | 0  | (M)(O)May be inoperative provided:  | |

|      Indicating System    |    |    |     a) Ambient temperatures are       |

|                           |    |    |        below 50 degrees C,            |

|                           |    |    |     b) A minimum of 20 minutes        |

|                           |    |    |        cooling time has elapsed       |

|                           |    |    |        before dispatch utilizing      |

|                           |    |    |        two engine taxi,               |

|                           |    |    |     c) A minimum of 35 minutes      | |

|                           |    |    |        cooling time has elapsed       |

|                           |    |    |        before dispatch utilizing      |

|                           |    |    |        single engine taxi,            |

|                           |    |    |     d) Landing gear bay overheat    | |

|                           |    |    |        detection system operates      |

|                           |    |    |        normally,                      |

|                           |    |    |     e) It can be verified that a    | |

|                           |    |    |        rejected takeoff, high         |

|                           |    |    |        efficiency stop, or landing    |

|                           |    |    |        involving use of assymetric    |

|                           |    |    |        braking was not utilized on    |

|                           |    |    |        the prior leg, and             |

|                           |    |    |     f) Should a rejected takeoff    | |

|                           |    |    |        occur after dispatch, the      |

|                           |    |    |        aircraft must return for an    |

|                           |    |    |        inspection of wheels, tires,   |

|                           |    |    |        and brakes before the next     |

|                           |    |    |        flight.                        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 32-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 32  LANDING GEAR          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 42-8 Brake Temperature  C | 1  | 0  | (M)(O)May be inoperative, not       | |

|      Indicator Overheat   |    |    | illuminated, provided:                |

|      Light                |    |    |     a) Analogue gauge operates        |

|                           |    |    |        normally,                      |

|                           |    |    |          OR                           |

|                         A |    |    |     b) All operative brake temp-      |

|                           |    |    |        erature channels (analogue)    |

|                           |    |    |        indicate a temperature of      |

|                           |    |    |        less than 180 degrees C        |

|                           |    |    |        before TAXI,                   |

|                           |    |    |     c) Landing gear bay overheat      |

|                           |    |    |        detection system operates      |

|                           |    |    |        normally,                      |

|                           |    |    |     d) Should a rejected take-off     |

|                           |    |    |        occur, the aircraft must be    |

|                           |    |    |        inspected before flight, and   |

|                           |    |    |     e) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                         A | 1  | 0  | (M)(O)May be inoperative,           | |

|                           |    |    | illuminated, provided:                |

|                           |    |    |     a) Analogue gauge operates        |

|                           |    |    |        normally,                      |

|                           |    |    |     b) Light is masked, and           |

|                           |    |    |     c) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |          OR                           |

|                         C |    |    |     d) Light is masked, and           |

|                           |    |    |     e) Brake temperature indicating   |

|                           |    |    |        system is considered           |

|                           |    |    |        inoperative.                   |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 33-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 11-1 Flight Deck        C | 1  | 0  | May be inoperative provided         | |

|      Overhead Flood       |    |    | instrument and distribution panel     |

|      Lights               |    |    | flood lights operate normally.        |

|                           |    |    |                                       |

| 13-1 Cockpit/Flight     C | -  | -  | Individual lights may be            | |

|      Deck /Flight         |    |    | inoperative provided remaining      | |

|      Compartment and      |    |    | lights are:                         | |

|      Instrument Panel     |    |    |     a) Sufficient to clearly        | |

|      Lighting Systems     |    |    |        illuminate all required      | |

|                           |    |    |        instruments, controls, and   | |

|                           |    |    |        other devices for which they | |

|                           |    |    |        are provided,                | |

|                           |    |    |     b) Positioned so that direct    | |

|                           |    |    |        rays are shielded from       | |

|                           |    |    |        flight crewmembers' eyes,    | |

|                           |    |    |        and                          | |

|                           |    |    |     c) Lighting configuration and   | |

|                           |    |    |        intensity is acceptable to   | |

|                           |    |    |        the flight crew.             | |

|                           |    |    |                                     | |

|                           |    |    | Note:  When making above determin-  | |

|                           |    |    |        ation, consideration should  | |

|                           |    |    |        be given to lighting avail-  | |

|                           |    |    |        able with only the Emergency | |

|                           |    |    |        busbar powered.              | |

|                           |    |    |                                       |

| 14-1 Distribution Panel C | 2  | 0  | All may be inoperative provided     | |

|      Flood Light(s)       |    |    | overhead flood light(s) operate       |

|                           |    |    | normally.                             |

|                           |    |    |                                       |

|                         C | 2  | 0  | All may be inoperative for day      | |

|                           |    |    | operations.                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 33-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 17-1 Filament Test      C | 1  | 0  | (O)Master or individual push-to-    | |

|      System               |    |    | test feature may be inoperative       |

|                           |    |    | provided the lights intended          |

|                           |    |    | purpose can be confirmed by           |

|                           |    |    | operations or system test.            |

|                           |    |    |                                       |

| 17-2 Legend Dimming     C | 1  | 0  | Dim function may be inoperative for | |

|      System               |    |    | day operations so as to remain in     |

|                           |    |    | the bright mode.                      |

|                           |    |    |                                       |

| 20-1 Passenger Interior C | 1  | 1  | Lights must be sufficient for cabin | |

|      Illumination         |    |    | attendants to perform their duties.   |

|      Lights               |    |    |                                       |

|                           |    |    |                                       |

| 20-2 Passenger Notice     |    |    |                                       |

|      System               |    |    |                                       |

|                           |    |    |                                       |

|      1) "No Smoking/    C | -  | -  | (M)(O)A passenger seat from which a | |

|         Fasten Seat       |    |    | "No Smoking/Fasten Seat Belt" sign    |

|         Belt" Signs       |    |    | is not readily legible is             |

|                           |    |    | considered inoperative and must be    |

|                           |    |    | blocked.                              |

|                           |    |    |                                       |

|                         C | -  | -  | (O)If one or more "No Smoking/      | |

|                           |    |    | Fasten Seat Belt" signs are           |

|                           |    |    | inoperative, the affected passenger   |

|                           |    |    | seat(s) may be occupied provided:     |

|                           |    |    |     a) Passenger Address System       |

|                           |    |    |        operates normally, and can     |

|                           |    |    |        be heard clearly throughout    |

|                           |    |    |        the cabin during flight, and   |

|                           |    |    |     b) PA System is used to notify    |

|                           |    |    |        the passengers when seat       |

|                           |    |    |        belts should be fastened,      |

|                           |    |    |        and smoking is prohibited.     |

|                           |    |    |                                       |

|                         C | -  | 0  | May be inoperative for all cargo    | |

|                           |    |    | operations.                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 33-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-1 Compartment Lights C | -  | 0  |                                     | |

|      (Nose/Tail, Cargo    |    |    |                                       |

|      and Lavatory)        |    |    |                                       |

|                           |    |    |                                       |

| 32-1 Service Lights     C | -  | 0  | May be inoperative provided         | |

|                           |    |    | procedures are not dependent upon     |

|                           |    |    | its use.                              |

|                           |    |    |                                       |

| 41-1 Position Lights    C | -  | 1  | One light on each wing and one      | |

|      System               |    |    | light on the tail must operate        |

|                           |    |    | normally for night operations.        |

|                           |    |    |                                       |

|                         C | -  | 0  | All may be inoperative for day      | |

|                           |    |    | operations.                           |

|                           |    |    |                                       |

| 42-1 Anti-Collision     C | 2  | 0  | One or both may be inoperative for  | |

|      Lights (Fuselage/    |    |    | night operations provided wing tip    |

|      Vertical Fin)        |    |    | strobe lights operate normally.       |

|                           |    |    |                                       |

| 43-1 Landing Lights     B | 2  | 1  | One may be inoperative for night    | |

|                           |    |    | operations provided the associated    |

|                           |    |    | taxi light operates normally.         |

|                           |    |    |                                       |

|                         C | 2  | 0  | One or both may be inoperative for  | |

|                           |    |    | day operations.                       |

|                           |    |    |                                       |

| 43-2 Taxi Lights        C | 2  | 0  |                                     | |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 33-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 44-1 Wing Illumination  C | 2  | 0  | May be inoperative for night        | |

|      Lights               |    |    | operations provided airplane is not | |

|                           |    |    | operated in known or forecast icing | |

|                           |    |    | conditions.                         | |

|                           |    |    |                                       |

|                         C | 2  | 0  | May be inoperative for day          | |

|                           |    |    | operations.                           |

|                           |    |    |                                       |

| 45-1 Wing Strobe Light  C | 1  | 0  |                                     | |

|      System               |    |    |                                       |

|                           |    |    |                                       |

| 46-1 Logo Lights        C | -  | 0  |                                     | |

|                           |    |    |                                       |

| 52-1 Floor Proximity    C | 1  | 1  | Individual lights may be            | |

|      Emergency Escape     |    |    | inoperative provided FAA approved     |

|      Path Marking         |    |    | minimum acceptable lighting levels    |

|      System               |    |    | specified in one of the following     |

|                           |    |    | documents are complied with:          |

|                           |    |    |     a) FAA engineering approval       |

|                           |    |    |        letter.                        |

|                           |    |    |          OR                           |

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

|                           |    |    |        Type Design holder,            |

|                           |    |    |          OR                           |

|                         C |    |    |     c) Limitations and Conditions     |

|                           |    |    |        section of the applicable      |

|                           |    |    |        Supplemental Type              |

|                           |    |    |        Certificate (STC),             |

|                           |    |    |          OR                           |

|                         C |    |    |     d) An FAA approved report         |

|                           |    |    |        incorporated in the Master     |

|                           |    |    |        Drawing List for the           |

|                           |    |    |        applicable STC.                |

|                           |    |    |                                       |

|                         C | 1  | 0  | May be inoperative for all-cargo    | |

|                           |    |    | operations.                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 33-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 52-2 Exit Locator Sign  C | 5  | 5  | Two filaments/bulbs may be          | |

|      System               |    |    | inoperative in each light.            |

|                           |    |    |                                       |

| 52-3 Interior Emergency C | 1  | 0  | May be inoperative in cargo areas   | |

|      Exit Light System    |    |    | for mixed or all-cargo                |

|                           |    |    | configurations provided:              |

|                           |    |    |     a) No persons occupy that area,   |

|                           |    |    |        and                            |

|                           |    |    |     b) Forward entrance door light    |

|                           |    |    |        must operate normally at all   |

|                           |    |    |        times.                         |

|                           |    |    |                                       |

| 52-4 Exterior Emergency C | -  | 0  | May be inoperative for day          | |

|      Lights               |    |    | operations.                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 34-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 12-01  TAS Indicator    C | 1  | 0  |                                     | |

|                           |    |    |                                       |

| 12-02  ATC Transponders C | -  | -  | As required by FAR.                 | |

|        and Automatic      |    |    |                                     | |

|        Altitude         D | -  | -  | Any in excess of those required by  | |

|        Reporting          |    |    | FAR may be inoperative.             | |

|        Systems            |    |    |                                     | |

|                           |    |    |                                       |

| 12-04  Total Air        C | 1  | 0  | May be inoperative provided Static  | |

|        Temperature        |    |    | Air Temperature (SAT) operates        |

|        Indicator          |    |    | normally.                             |

|                           |    |    |                                       |

| 13-01  Standby          C | 1  | 0  | May be inoperative provided VMC     | |

|        Altimeter          |    |    | exists at both departure and          |

|        Vibrator           |    |    | arrival airports.                     |

|                           |    |    |                                       |

| 21-00  RMI                |    |    |                                       |

|                           |    |    |                                       |

|        1) Heading       C | -  | 1  | May be inoperative provided         | |

|           Indication      |    |    | stabilized heading indication on      |

|                           |    |    | the associated pilot's panel          |

|                           |    |    | operates normally.                    |

|                           |    |    |                                       |

|        2) VOR/ADF       C | -  | 1  | May be inoperative provided other   | |

|           Pointer         |    |    | VOR/ADF system(s) operate normally    |

|           Indication      |    |    | and meet FAR requirments.             |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 34-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 21-02  Non-Stabilized   B | 1  | 0  | (O)May be inoperative provided:     | |

|        Magnetic Compass   |    |    |     a) Any combination of two gyro    |

|                           |    |    |        stabilized or AHRS compass     |

|                           |    |    |        systems operate normally,      |

|                           |    |    |        and                            |

|                           |    |    |     b) Airplane is operated with      |

|                           |    |    |        dual independent navigation    |

|                           |    |    |        capability, and under          |

|                           |    |    |        positive radar control by      |

|                           |    |    |        ATC on the en route portion    |

|                           |    |    |        of the flight.                 |

|                           |    |    |                                       |

|                         C | 1  | 0  | (O)May be inoperative for flights   | |

|                           |    |    | that are entirely within areas of     |

|                           |    |    | magnetic unreliablity provided at     |

|                           |    |    | least two stabilized directional      |

|                           |    |    | gyro systems are installed, operate   |

|                           |    |    | normally, and are used in             |

|                           |    |    | conjunction with approved free gyro   |

|                           |    |    | navigation techniques.                |

|                           |    |    |                                       |

| 23-00  Turn and Slip      |    |    | DELETED, REV 1.                       |

|        Indicators         |    |    |                                       |

|                           |    |    |                                       |

| 23-01  EFIS Overspeed   B | 2  | 1  | One may be inoperative provided VMO | |

|        Warning            |    |    | aural warning operates normally.      |

|        Indicator          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 34-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 23-02  Flight Director  C | -  | 0  | May be inoperative provided         | |

|        System             |    |    | approach minimums are not dependent   |

|                           |    |    | upon its use.                         |

|                           |    |    |                                       |

| 23-04  EFIS Low Speed     |    |    | DELETED, REV 1.                       |

|        Warning            |    |    |                                       |

|        Indicator          |    |    |                                       |

|                           |    |    |                                       |

| 23-05  EFIS Speed Trend C | 2  | 0  |                                     | |

|        Indicator          |    |    |                                       |

|                           |    |    |                                       |

| 23-06  EFIS Airspeed    A | 1  | 0  | May be inoperative provided         | |

|        Indicator (Bugs)   |    |    | operations are limited to not more    |

|        System             |    |    | than three flight days before         |

|                           |    |    | repair is made.                       |

|                           |    |    |                                       |

| 23-07  Instrument       B | -  | 0  | May be inoperative provided         | |

|        Comparator         |    |    | approach minimums are not dependent   |

|                           |    |    | upon its use.                         |

|                           |    |    |                                       |

| 23-08  Altitude Alert   A | -  | 0  | (O)May be inoperative provided:     | |

|        System             |    |    |     a) Autopilot with altitude hold   |

|                           |    |    |        operates normally, and         |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 6        | PAGE:    |

|                                          |                       |          |

|                 BAe-ATP                  | DATE: 10/24/96        | 34-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 23-09  Vertical Speed   C | 2  | 1  | One may be inoperative for day VMC  | |

|        Indication         |    |    | only.                                 |

|        (Primary Flight    |    |    |                                     | |

|        Display only)      |    |    |                                     | |

|                           |    |    |                                       |

| 23-10  Voice            C | 1  | 0  | May be inoperative provided         | |

|        Advisory/Flight    |    |    | procedures are not dependent upon     |

|        Profile Advisory   |    |    | its use.                              |

|                           |    |    |                                       |

| 23-11  EFIS VOR/ADF     A | 4  | 0  | May be inoperative provided:        | |

|        Bearing Pointer    |    |    |     a) Standby RMI and Standby RMI    |

|        Selector Switch    |    |    |        bearing pointers operate       |

|                           |    |    |        normally, and                  |

|                           |    |    |     b) Operations are limited to      |

|                           |    |    |        not more than three flight     |

|                           |    |    |        days before repair is made.    |

|                           |    |    |                                       |

| 23-12  EFIS Nav.        A | 2  | 0  | May be inoperative "stuck" in an    | |

|        Display (ND)       |    |    | operational mode provided:            |

|        Mode Selector      |    |    |     a) Either Map, Map + Weather,     |

|                           |    |    |        or Rose modes are displayed,   |

|                           |    |    |     b) Test Mode operates normally,   |

|                           |    |    |        and                            |

|                           |    |    |     c) Operations are limited to      |

|                           |    |    |        three flight days before       |

|                           |    |    |        repair is made.                |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |