DEPARTMENT OF TRANSPORTATION     Revision: 11 c

                                                           Date: 08/21/2000

                         FEDERAL AVIATION ADMINISTRATION

 

                                WASHINGTON, D.C.

 

 

 

 

 

 

 

 

 

 

 

            M A S T E R   M I N I M U M   E Q U I P M E N T   L I S T

 

 

 

 

 

                            ALLISON CONVAIR 340/440

                               (CV-580, CV-5800)

                                  (TURBO PROP)

 

 

 

 

 

 

 

 

 

 

 

                         Federal Aviation Administration

                         Flight Standards Division

                         AIRCRAFT EVALUATION GROUP, LGB-AEG

                         3229 East Spring Street

                         Long Beach, CA 90806-2425

 

                         TELEPHONE:  (310) 988-5270

                               FAX:  (310) 988-5281


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 11 c

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/21/2000

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I, II

         --     Log of Revisions                        III

         --     Control Page                            IV, V

         --     Highlights of Change                    VI

         --     Definitions                             VII, VIII, IX, X

         --     Definitions                             XI, XII, XIII, XIV

         --     Preamble                                XV, XVI

         21     Air Conditioning                        21-1, 2

         22     Auto Flight                             22-1, 2, 3

         23     Communications                          23-1, 2, 3, 4, 5

         23     Communications                          23-6

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

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

         25     Equipment/Furnishings                   25-6, 7

         26     Fire Protection                         26-1, 2, 3

         27     Flight Controls                         27-1

         28     Fuel                                    28-1

         29     Hydraulic Power                         29-1

         30     Ice and Rain Protection                 30-1, 2

         31     Indicating/Recording Systems            31-1

         32     Landing Gear                            32-1

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

         33     Lights                                  33-6

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

         34     Navigation                              34-6  THRU 10

         34     Navigation                              34-11  THRU 12

         35     Oxygen                                  35-1

         36     Pneumatic                               36-1

         49     Airborne Auxiliary Power                49-1

         52     Doors                                   52-1

         61     Propellers                              61-1

         72     Engine                                  72-1

         73     Engine Fuel & Control                   73-1

         76     Engine Controls                         76-1

         77     Engine Indicating                       77-1


 

                       FEDERAL AVIATION ADMINISTRATION     Page: II

                                                           Revision: 11 c

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/21/2000

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         79     Engine Oil                              79-1

         82     Water Injection                         82-1


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: III

                                                         Revision: 11 c

                        MASTER MINIMUM EQUIPMENT LIST    Date: 08/21/2000

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

 

                               Log of Revisions

 

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

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

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

      | 11       | 03/08/1994 | ALL PAGES                      |           |

      | 11a      | 09/26/1994 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 11a      | 09/26/1994 | 21-1,21-2,22-1,22-2,22-3       |           |

      | 11a      | 09/26/1994 | 23-1,23-2,23-3,23-4,23-5       |           |

      | 11a      | 09/26/1994 | 23-6,24-1,24-2,24-3,26-1       |           |

      | 11a      | 09/26/1994 | 26-2,33-1,33-2,33-3,33-4       |           |

      | 11a      | 09/26/1994 | 33-5,33-6,34-1,34-2,34-3       |           |

      | 11a      | 09/26/1994 | 34-4,34-5,34-6,34-7,34-8       |           |

      | 11a      | 09/26/1994 | 34-9,34-10,49-1,77-1           |           |

      | 11b      | 10/01/1998 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 11b      | 10/01/1998 | 21-1,21-2,24-1,24-2,24-3       |           |

      | 11b      | 10/01/1998 | 24-4,26-2,26-3,28-1,30-1       |           |

      | 11b      | 10/01/1998 | 30-2,33-2,33-3,33-4,33-5       |           |

      | 11b      | 10/01/1998 | 33-6,34-2,34-3,34-4,34-5       |           |

      | 11b      | 10/01/1998 | 34-6,34-7,34-8,34-9,34-10      |           |

      | 11b      | 10/01/1998 | 49-1                           |           |

      | 11c      | 08/21/2000 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 11c      | 08/21/2000 | 23-1,23-2,23-3,23-4,23-5       |           |

      | 11c      | 08/21/2000 | 23-6,25-1,25-2,25-5,25-6       |           |

      | 11c      | 08/21/2000 | 25-7,26-1,26-2,26-3,31-1       |           |

      | 11c      | 08/21/2000 | 33-1,33-2,33-3,33-4,33-5       |           |

      | 11c      | 08/21/2000 | 33-6,34-1,34-2,34-3,34-4       |           |

      | 11c      | 08/21/2000 | 34-5,34-6,34-7,34-8,34-9       |           |

      | 11c      | 08/21/2000 | 34-10,34-11,34-12,35-1         |           |

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


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IV

                                                           Revision: 11 c

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/21/2000

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       11 c     08/21/2000

         Table of Contents                        I       11 c     08/21/2000

                                                  II      11 c     08/21/2000

         Log of Revisions                         III     11 c     08/21/2000

         Control Page                             IV      11 c     08/21/2000

                                                  V       11 c     08/21/2000

         Highlights of Change                     VI      11 c     08/21/2000

         Definitions                              VII     6        01/31/1995

                                                  VIII    6        01/31/1995

                                                  IX      6        01/31/1995

                                                  X       6        01/31/1995

                                                  XI      6        01/31/1995

                                                  XII     6        01/31/1995

                                                  XIII    6        01/31/1995

                                                  XIV     6        01/31/1995

         Preamble                                 XV      2        06/14/1989

                                                  XVI     2        06/14/1989

         21                                       21-1    11 b     10/01/1998

                                                  21-2    11 b     10/01/1998

         22                                       22-1    11 a     09/26/1994

                                                  22-2    11 a     09/26/1994

                                                  22-3    11 a     09/26/1994

         23                                       23-1    11 c     08/21/2000

                                                  23-2    11 c     08/21/2000

                                                  23-3    11 c     08/21/2000

                                                  23-4    11 c     08/21/2000

                                                  23-5    11 c     08/21/2000

                                                  23-6    11 c     08/21/2000

         24                                       24-1    11 b     10/01/1998

                                                  24-2    11 b     10/01/1998

                                                  24-3    11 b     10/01/1998

                                                  24-4    11 b     10/01/1998

         25                                       25-1    11 c     08/21/2000

                                                  25-2    11 c     08/21/2000

                                                  25-3    11       03/08/1994

                                                  25-4    11       03/08/1994

                                                  25-5    11 c     08/21/2000

                                                  25-6    11 c     08/21/2000

                                                  25-7    11 c     08/21/2000

         26                                       26-1    11 c     08/21/2000


 

                       FEDERAL AVIATION ADMINISTRATION     Page: V

                                                           Revision: 11 c

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/21/2000

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  26-2    11 c     08/21/2000

                                                  26-3    11 c     08/21/2000

         27                                       27-1    11       03/08/1994

         28                                       28-1    11 b     10/01/1998

         29                                       29-1    11       03/08/1994

         30                                       30-1    11 b     10/01/1998

                                                  30-2    11 b     10/01/1998

         31                                       31-1    11 c     08/21/2000

         32                                       32-1    11       03/08/1994

         33                                       33-1    11 c     08/21/2000

                                                  33-2    11 c     08/21/2000

                                                  33-3    11 c     08/21/2000

                                                  33-4    11 c     08/21/2000

                                                  33-5    11 c     08/21/2000

                                                  33-6    11 c     08/21/2000

         34                                       34-1    11 c     08/21/2000

                                                  34-2    11 c     08/21/2000

                                                  34-3    11 c     08/21/2000

                                                  34-4    11 c     08/21/2000

                                                  34-5    11 c     08/21/2000

                                                  34-6    11 c     08/21/2000

                                                  34-7    11 c     08/21/2000

                                                  34-8    11 c     08/21/2000

                                                  34-9    11 c     08/21/2000

                                                  34-10   11 c     08/21/2000

                                                  34-11   11 c     08/21/2000

                                                  34-12   11 c     08/21/2000

         35                                       35-1    11 c     08/21/2000

         36                                       36-1    11       03/08/1994

         49                                       49-1    11 b     10/01/1998

         52                                       52-1    11       03/08/1994

         61                                       61-1    11       03/08/1994

         72                                       72-1    11       03/08/1994

         73                                       73-1    11       03/08/1994

         76                                       76-1    11       03/08/1994

         77                                       77-1    11 a     09/26/1994

         79                                       79-1    11       03/08/1994

         82                                       82-1    11       03/08/1994


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: VI

                                                         Revision: 11 c

                        MASTER MINIMUM EQUIPMENT LIST    Date: 08/21/2000

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                            Highlights of Change

 

 

 

       EFFECTIVE ABOVE DATE the Allison Conviar 340/440 (CV-580, CV-5800)

       Master Minimum Equipment List is revised.

       )

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

           Please retain this sheet until the next revision has been issued.

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

 

       Revision 11c incorporates Policy Letters through PL 104.

 

       The following sections have been revised:

       Section 23, 25, 26, 31, 33, 34, 35.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

       1.   System Definitions.

 

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

       Specification Number 100 and items are numbered sequentially.

 

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

                      component, or function listed in the "Item"

                      column.

 

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

                      (quantity) of items normally installed in the

                      aircraft.  This number represents the aircraft

                      configuration considered in developing this MMEL.

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

                      cabin items) a number is not required.

                                                                            |

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

                      minimum number (quantity) of items required for

                      operation provided the conditions specified in

                      Column 4 are met.

 

       NOTE:  Where the MMEL shows a variable number required for

       dispatch, the MEL must reflect the actual number required for

       dispatch or an alternate means of configuration control approved

       by the Administrator.

 

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

                      includes a statement either prohibiting or

                      permitting operation with a specific number of

                      items inoperative, provisos (conditions and

                      limitations) for such operation, and appropriate

                      notes.

 

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

                      indicates a change, addition or deletion in the

                      adjacent text for the current revision of that

                      page only.  The change bar is dropped at the next

                      revision of that page.

 

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

       required for type certification and approved by the responsible

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

       the specific aircraft is listed on the applicable Type


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

       Certificate Data Sheet.

 

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

       certain provisions (restrictive or permissive) expressed in the

       Federal Aviation Regulations operating rules.  The number of

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

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

       specified by repair category.

 

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

       the crewmembers and maintenance personnel of the equipment

       condition.

 

       NOTE:  To the extent practical, placards should be located

       adjacent to the control or indicator for the item affected;

       however, unless otherwise specified, placard wording and location

       will be determined by the operator.

 

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

       number (quantity) of the item installed.

                                                                           |

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

       indicates that the item was previously listed but is now required

       to be operative if installed in the  aircraft.

 

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

       airplane which has a type design approval for ER operations and

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

 

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

       portions of the Federal Aviation Act and Federal Aviation

       Regulations.

 

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

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

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

       is initiated for the affected aircraft.

 

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

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

 

       11.  Alphabetical symbol in Column 4 indicates a proviso

       (condition or limitation) that must be complied with for


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

       operation with the  listed item inoperative.

 

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

       the extent that it does not accomplish its intended purpose

       and/or is not consistently functioning normally within its

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

 

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

       crewmember or maintenance consideration.  Notes are used to

       identify applicable material which is intended to assist with

       compliance, but do not relieve the operator of the responsibility

       for compliance with all applicable requirements.  Notes are not a

       part of the provisos.

 

       14.  Inoperative components of an inoperative system:

       Inoperative items which are components of a system which is

       inoperative are usually considered components directly associated

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

       (Warning/caution systems associated with the inoperative system

       must be operative unless relief is specifically authorized per

       the MMEL).

 

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

       maintenance procedure which must be accomplished prior to

       operation with the listed item inoperative.  Normally these

       procedures are accomplished by maintenance personnel;  however,

       other personnel may be qualified and authorized to perform

       certain functions.  Procedures requiring specialized knowledge or

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

       accomplished by maintenance personnel.  The satisfactory

       accomplishment of all maintenance procedures, regardless of

       who performs them, is the responsibility of the operator.

       Appropriate procedures are required to be published as part of

       the operator's manual or MEL.

 

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

       operations procedure which must be accomplished in planning for

       and/or operating with the listed item inoperative.  Normally

       these procedures are accomplished by the flight crew; however,

       other personnel may be qualified and authorized to perform

       certain functions.  The satisfactory accomplishment of all

       procedures, regardless of who performs them, is the

       responsibility of the operator.  Appropriate procedures are


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: X

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

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

       MEL.

 

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

       unless otherwise authorized by the Administrator.

 

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

       component must be put into an acceptable condition for safe

       flight.  An acceptable method of securing or deactivating will be

       established by the operator.

 

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

       This precludes a pilot from filing an Instrument Flight Rules

       (IFR) flight plan.

 

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

       atmospheric environment is such that would allow a flight to

       proceed under the visual flight rules applicable to the flight.

       This does not preclude operating under Instrument Flight Rules.

 

       20.  "Visible Moisture" means an atmospheric environment

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

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

       snow.

 

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

       passenger convenience, comfort or entertainment such as, but not

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

       equipment, overhead reading lamps, etc.

 

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

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

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

       to the repair times established by the following letter

       designators:

 

            Category A.  Items in this category shall be repaired within

       the time interval specified in the remarks column of the

       operator's approved MEL.

 

            Category B.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

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

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

       26th and end at midnight the 29th.

 

            Category C.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance

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

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

       26th and end at midnight February 5th.

 

            Category D.  Items in this category shall be repaired within

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

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

       aircraft maintenance log and/or record.

 

       The letter designators are inserted adjacent to Column 2.

 

       23. Electronic fault alerting system - General                  |

                                                                       |

       New generation aircraft display system fault indications to the |

       flight crew by use of computerized display systems.  Each       |

       aircraft manufacturer has incorporated individual design        |

       philosophies in determining the data that would be              |

       represented.  The following are customized definitions (specific|

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

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

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

       23 for their aircraft, if appropriate.                          |

                                                                       |

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

                                                                       |

       Boeing airplanes equipped with Engine Indicating and Crew       |

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

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

       MAINTENANCE).  Any messages that affects airplane dispatch      |

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

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

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

       operating within its approved operating limits or tolerances.   |

                                                                       |

       System conditions that result only in a maintenance level       |

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


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

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

       addressed within an operators standard maintenance program.     |

                                                                       |

       b.   DOUGLAS  (MD-11)                                           |

                                                                       |

       Some Douglas aircraft are equipped with an alerting function    |

       which is a subsystem within the Electronic Instrument System    |

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

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

       STATUS).                                                        |

                                                                       |

       Alerts that affect aircraft dispatch will include WARNING,      |

       CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are   |

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

       maintenance heading.                                            |

                                                                       |

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

       system fault which can be identified by the Central Fault       |

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

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

       MEL must be verified for dispatch purposes.                     |

                                                                       |

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

                                                                       |

       Airbus aircraft equipped with Electronic Centralized Aircraft   |

       Monitoring (ECAM) provide different levels of system condition  |

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

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

                                                                       |

       Any message that effects airplane dispatchability will normally |

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

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

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

                                                                       |

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

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

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

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

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

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

       MAINTENANCE status messages do not affect dispatch.             |

 

       d.   FOKKER  (FK-100)                                           |


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

                                                                       |

       Fokker aircraft are equipped with Multi Function Display System |

       (MFDS) which provides electronic message referring to the       |

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

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

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

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

       verified for dispatch capability and maintenance may be         |

       required.                                                       |

                                                                       |

       System conditions that only require maintenance are not         |

       presented on the flight deck.  These maintenance                |

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

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

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

 

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

       operator in the MEL for tracking and informational purposes.  It

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

       Operations Inspector provided no relief is granted, or provided

       conditions and limitations are contained in an approved document

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

       If relief other than that granted by an approved document is

       sought for an administrative control item, a request must be

       submitted to the Administrator.  If the request results in review

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

       than an administrative control item.

 

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

       required by regulation but which may have been installed on some

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

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

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

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

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

       this policy nor the use of this symbol provide authority to

       install or remove an item from an aircraft.

 

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

       that are redundant to the requirements of the FARs.

 

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

       equipment/instrument malfunction was recorded in the aircraft


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIV

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                 Definitions

 

 

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

       calendar days or flight days specified in the MMEL for the

       repair of an inoperative item of equipment. This provision is

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

       D."

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                  Preamble

                            (Effective 6/14/89)

 

       The following is applicable for authorized certificate holders operating

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

       FAR require that all equipment installed on an aircraft in compliance

       with the Airworthiness Standards and the Operating Rules must be

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

       Equipment List (MEL) where compliance with certain equipment

       requirements is not necessary in the interests of safety under all

       operating conditions.  Experience has shown that with the various levels

       of redundancy designed into aircraft, operation of every system or

       installed component may not be necessary when the remaining operative

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

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

       aviation industry, to improve aircraft utilization and thereby provide

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

       approved MMEL includes those items of equipment related to airworthiness

       and operating regulations and other items of equipment which the

       Administrator finds may be inoperative and yet maintain an acceptable

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

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

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

       into consideration the operator's particular aircraft equipment

       configuration and operational conditions. Operator MELs, for

       administrative control, may include items not contained in the

       MMEL;  however, relief for administrative control items must be

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

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

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

       operation of the aircraft with inoperative equipment.

 

       Equipment not required by the operation being conducted and equipment in

       excess of FAR requirements are included in the MEL with appropriate

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

       Flight Manual Limitations, Emergency Procedures or with Airworthiness

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

       the airworthiness and the operating regulations of the aircraft not

       listed on the MMEL must be operative.

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XVI

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                  ALLSON CONVAIR 340/440 (CV-580, CV-5800)

                                (TURBO PROP)

 

                                  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: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 21-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Engine Driven       C | -  | 0  | May be inoperative provided:          |

|     Compressor            |    |    |     a) Aircraft is operated in an     |

|                           |    |    |        accepted unpressurized         |

|                           |    |    |        configuration.                 |

|                           |    |    |                                       |

|                         C | -  | 0  | May be inoperative provided an        |

|                           |    |    | acceptable Airborne Auxiliary         |

|                           |    |    | Pneumatic Power source is             |

|                           |    |    | available.                            |

|                           |    |    |                                       |

| 2.  Cabin Altitude and  C | 1  | 0  | May be inoperative provided           |

|     Differential          |    |    | aircraft is operated unpressurized.   |

|     Pressure Indicator    |    |    |                                       |

|                           |    |    |                                       |

| 3.  Cabin               C | 1  | 0  | May be inoperative provided           |

|     Pressurization        |    |    | aircraft is operated unpressurized.   |

|     Control System        |    |    |                                       |

|                           |    |    |                                       |

| 4.  Cabin Rate Climb    C | 1  | 0  | May be inoperative provided           |

|     System                |    |    | aircraft is operated unpressurized.   |

|                           |    |    |                                       |

| 5.  Cabin Differential  C | 1  | 0  | May be inoperative provided           |

| *** Pressure Warning      |    |    | aircraft is operated unpressurized.   |

|                           |    |    |                                       |

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

|                           |    |    |     a) Alternate procedures are       |

|                           |    |    |        established to assure          |

|                           |    |    |        aircraft is depressurized      |

|                           |    |    |        before opening the cabin       |

|                           |    |    |        door, and                      |

|                           |    |    |     b) An additional placard is       |

|                           |    |    |        placed at Main Door Warning    |

|                           |    |    |        Light.                         |

|                           |    |    |                                       |

| 6.  Cockpit Electric    C | 1  | 0  |                                       |

|     Heater (DC)           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 21-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 7.  Temperature Control C | 1  | 0  | May be inoperative provided Cockpit   |

|     System                |    |    | Temperature remains above 50 F.       |

|                           |    |    |                                       |

|     1) Manual Function  C | 1  | 0  | May be inoperative provided           |

|                           |    |    | Automatic Temperature Control is      |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|     2) Automatic        C | 1  | 0  | May be inoperative provided Manual    |

|        Function           |    |    | Function is operative.                |

|                           |    |    |                                       |

| 8.  Air Cycle Machine   C | 1  | 0  |                                       |

|                           |    |    |                                       |

| 9.  Pressurization      C | 1  | 0  | May be inoperative provided           |

|     System                |    |    | aircraft is operated unpressurized.   |

|                           |    |    |                                       |

| 10. Cabin Electric      C | 1  | 0  |                                       |

|     Heating System (AC)   |    |    |                                       |

|                           |    |    |                                       |

| 11. Cockpit Heater Fan  C | 1  | 0  |                                       |

| ***                       |    |    |                                       |

|                           |    |    |                                       |

| 12. Radio Rack Ground   C | 1  | 0  |                                       |

| *** Blower                |    |    |                                       |

|                           |    |    |                                       |

| 13. Ground Blower       C | 1  | 0  | May be inoperative provided           |

|                           |    |    | Pressurization and Air Conditioning   |

|                           |    |    | Systems are not used on the ground.   |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 a     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 09/26/1994      | 22-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Auto Pilot Systems    |    |    |                                       |

| ***                       |    |    |                                       |

|                           |    |    |                                       |

|     1) Sperry SP-20     C | -  | 0  |                                       |

|        System             |    |    |                                       |

|                           |    |    |                                       |

|        a) Altitude      C | 1  | 0  |                                       |

|           Control         |    |    |                                       |

|           Switch          |    |    |                                       |

|                           |    |    |                                       |

|        b) Turn Knob     C | 1  | 0  | (M)May be inoperative provided it     |

|                           |    |    | is verified that directional          |

|                           |    |    | control is not impaired.              |

|                           |    |    |                                       |

|        c) Pitch Control C | 1  | 0  | (M)may be inoperative provided it     |

|           Wheel           |    |    | is verified that vertical control     |

|                           |    |    | is not impaired.                      |

|                           |    |    |                                       |

|     2) Control Wheel    B | 2  | 1  | One may be inoperative provided:      |

|        Autopilot          |    |    |     a) Autopilot is not used at       |

|        Disconnect         |    |    |        less than initial approach     |

|                           |    |    |        altitude, and                  |

|                           |    |    |     b) Pilot flying has an            |

|                           |    |    |        operative Control Wheel        |

|                           |    |    |        Disconnect Switch.             |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 a     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 09/26/1994      | 22-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Auto Pilot Systems    |    |    |                                       |

| *** (Cont'd)              |    |    |                                       |

|                           |    |    |                                       |

|     3) SPZ-4500 System  C | -  | 0  |                                       |

|                           |    |    |                                       |

|        a) Altitude      C | 1  | 0  |                                       |

|           Control         |    |    |                                       |

|           Switch          |    |    |                                       |

|                           |    |    |                                       |

|        b) Turn Knob     C | 1  | 0  | (M)May be inoperative provided:       |

|                           |    |    |     a) It is verified that            |

|                           |    |    |        directional control is not     |

|                           |    |    |        impaired, and                  |

|                           |    |    |     b) Touch control Steering is      |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|        c) Pitch Control C | 1  | 0  | (M)may be inoperative provided:       |

|           Wheel           |    |    |     a) It is verified that vertical   |

|                           |    |    |        control is not impaired, and   |

|                           |    |    |     b) Touch Control Steering is      |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|        d) Couple Switch C | -  | 0  | May be inoperative provided           |

|           (1/2)           |    |    | available flight computer is          |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|        e) Soft Ride     C | -  | 0  |                                       |

|           Switch          |    |    |                                       |

|                           |    |    |                                       |

|        f) Touch Control C | -  | 0  | May be inoperative provided:          |

|           Steering        |    |    |     a) Pitch Wheel is operative,      |

|                           |    |    |        and                            |

|                           |    |    |     b) Turn Knob is operative.        |

|                           |    |    |                                       |

| 2.  Yaw Damper          C | -  | 0  |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 a     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 09/26/1994      | 22-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 3.  Digital Flight      C | -  | 0  |                                       |

| *** Control Computer      |    |    |                                       |

|     (SPZ-4500)            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 23-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Passenger Address     |    |    |                                     ] |

|     System                |    |    |                                       |

|                           |    |    |                                       |

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

|         Configuration     |    |    |     a) Alternate, normal, emergency   |

|                           |    |    |        procedures and/or operating    |

|                           |    |    |        restrictions are established   |

|                           |    |    |        and used, and                  |

|                           |    |    |     b) Flight Deck/Cabin interphone ] |

|                           |    |    |        and aural alerting (chime)   ] |

|                           |    |    |        operates normally.           ] |

|                           |    |    |                                       |

|                           |    |    | NOTE:  Any Station that operates    ] |

|                           |    |    |        normally may be used.        ] |

|                           |    |    |                                       |

|      2) Cargo           D | 1  | 0  |                                       |

|         Configuration     |    |    |                                       |

|                           |    |    |                                       |

| 2.  DELETED               |    |    | Deleted before revision 10.           |

|                           |    |    |                                       |

| 3.  Audio Selector      D | -  | -  | Any in excess of those required for   |

|     Panels                |    |    | flight deck crewmembers (including    |

|                           |    |    | official observer in Forward          |

|                           |    |    | Observer's Seat) may be               |

|                           |    |    | inoperative.                          |

|                           |    |    |                                       |

|      1) Audio Selector  C | -  | -  | One amplifier associated each panel   |

|         Panel Amplifier   |    |    | may be inoperative provided one       |

|                           |    |    | amplifier remains operative at each   |

|                           |    |    | flight crew station.                  |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 23-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 3.  Audio Selector        |    |    |                                       |

|     Panels (Cont'd)       |    |    |                                       |

|                           |    |    |                                       |

|      2) Audio Selector  C | -  | -  | One switch on each audio selector     |

|         Panel Switches    |    |    | panel may be inoperative provided:    |

|         (VHF, ADF, HF,    |    |    |     a) The flight crew interphone     |

|         NAV, MKR,         |    |    |        function is operative, and     |

|         VOICE, RANGE      |    |    |     b) Alternate procedures for       |

|         SWITCHES)         |    |    |        monitoring and identifying     |

|                           |    |    |        radios are established and     |

|                           |    |    |        used.                          |

|                           |    |    |                                       |

|                         C | -  | -  | May be inoperative provided:          |

|                           |    |    |     a) Flight Crew Inter              |

|                           |    |    |        Communications Function is     |

|                           |    |    |        operative, and                 |

|                           |    |    |     b) Alternate switching is used    |

|                           |    |    |        for affected communications    |

|                           |    |    |        functions.                     |

|                           |    |    |                                       |

| 4.  Communications      D | -  | 1  | Any in excess of those required by    |

|     Systems (VHF, HF      |    |    | FAR may be inoperative provided one   |

|     UHF, etc.)            |    |    | Communications System powered by      |

|                           |    |    | Essential Buses is operative.         |

|                           |    |    |                                       |

| 5.  Flight Deck         C | -  | 0  | May be inoperative provided           |

|     Speakers              |    |    | associated headset is operative.      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 23-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 6.  Crewmember            |    |    |                                     ] |

| *** Interphone System     |    |    |                                     ] |

|                           |    |    |                                       |

|     1) Flight Deck to   B | 1  | 0  | (O)May be inoperative provided:     ] |

|        Cabin, Cabin to    |    |    |     a) Public address system        ] |

|        Flight Deck,       |    |    |        operates normally, and can   ] |

|        Cabin to Cabin     |    |    |        be used as an alternate      ] |

|                           |    |    |        communications link between  ] |

|                           |    |    |        the flight deck and the      ] |

|                           |    |    |        cabin, and                   ] |

|                           |    |    |     b) Alternate communications     ] |

|                           |    |    |        procedures between the       ] |

|                           |    |    |        affected Flight Attendants   ] |

|                           |    |    |        station(s) and the flight    ] |

|                           |    |    |        deck are established and     ] |

|                           |    |    |        used.                        ] |

|                           |    |    |                                       |

|                           |    |    | NOTE:  Any station that operates    ] |

|                           |    |    |        normally may be used.        ] |

|                           |    |    |                                       |

|     2) Flight Deck to   C | 1  | 0  | (O)May be inoperative provided      ] |

|        Ground             |    |    | alternate procedures are            ] |

|                           |    |    | established and used.               ] |

|                           |    |    |                                       |

| 7.  Static Dischargers  C | 12 | 8  | Four may be missing provided one      |

|                           |    |    | remains in the outer position on      |

|                           |    |    | the aileron, elevator and rudder.     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 23-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 8.  Crew Alerting         |    |    |                                     ] |

|     Systems               |    |    |                                     ] |

|     (chime/light)         |    |    |                                     ] |

|                           |    |    |                                       |

|      1) Flight Deck     B | 1  | 0  | May be inoperative provided the     ] |

|         Call Light        |    |    | flight deck chime is operative.     ] |

|                           |    |    |                                       |

|                           |    |    | NOTE:  The flight deck chime must   ] |

|                           |    |    |        always be operative.         ] |

|                           |    |    |                                       |

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

|        Call Light         |    |    |     a) PA system is operative, and  ] |

|                           |    |    |     b) Affected light is not used   ] |

|                           |    |    |        for Lavatory Smoke Detector  ] |

|                           |    |    |        Alerting.                    ] |

|                           |    |    |                                       |

|     3) Flight Attendant B | -  | 0  | May be inoperative provided:        ] |

|        Chime              |    |    |     a) PA system is operative, and  ] |

|                           |    |    |     b) Affected Chime is not used   ] |

|                           |    |    |        for Lavatory Smoke Detector  ] |

|                           |    |    |        Alerting.                    ] |

|                           |    |    |                                       |

|     4) Cargo            D | -  | 0  | May be inoperative provided         ] |

|        Configuration      |    |    | affected chime/light is not used    ] |

|                           |    |    | for Lavatory Smoke Detector         ] |

|                           |    |    | Alerting.                           ] |

|                           |    |    |                                       |

| 9.  Cockpit Microphones   |    |    |                                       |

|     (Boom and Handheld)   |    |    |                                       |

|                           |    |    |                                       |

|      1) Handheld        D | -  | 0  | May be inoperative provided           |

|         Microphones       |    |    | associated Boom Microphone is         |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 23-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 9.  Cockpit Microphones   |    |    |                                       |

|     (Boom and Handheld)   |    |    |                                       |

|     (Cont'd)              |    |    |                                       |

|                           |    |    |                                       |

|      2) Boom Microphone   |    |    |                                       |

|                           |    |    |                                       |

|        a) Cockpit Voice A | -  | 0  | May be inoperative provided:          |

|           Recorder        |    |    |     a) Associated Hand Held Mike is   |

|           Equipped to     |    |    |        operative,                     |

|           Record Boom     |    |    |     b) Flight Data Recorder (FDR)     |

|           Microphone      |    |    |        is operative, and              |

|           per FAR         |    |    |     c) Repairs are made within        |

|           121.359(e),     |    |    |        three flight days.             |

|           135.151(d),     |    |    |                                       |

|           125.227(e)      |    |    |                                       |

|                           |    |    |                                       |

|        b) Cockpit Voice D | -  | 0  | May be inoperative provided           |

|           Recorder Not    |    |    | associated Hand Held Mike is          |

|           Equipped to     |    |    | operative.                            |

|           Record Boom     |    |    |                                       |

|           Microphone      |    |    |                                       |

|                           |    |    |                                       |

| *** 3) Mask/Boom        D | -  | 0  | May be inoperative provided:          |

|        Microphone         |    |    |     a) Boom Mike is not required      |

|        Selector SW        |    |    |        for Cockpit Voice Recorder,    |

|                           |    |    |        and                            |

|                           |    |    |     b) Mask Mike is operative.        |

|                           |    |    |                                       |

| 10. Cockpit Headsets    C | -  | 0  | May be inoperative provided           |

|                           |    |    | associated Flight Deck Speaker is     |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 23-6     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 11. Flight Attendant      |    |    |                                       |

| *** Handsets              |    |    |                                       |

|                           |    |    |                                       |

|      1) Passenger       C | -  | 1  | Handset used when cabin attendant     |

|         Configuration     |    |    | is seated, must be operative for PA   |

|                           |    |    | and interphone.                       |

|                           |    |    |                                       |

|      2) Cargo           D | -  | 0  |                                       |

|         Configuration     |    |    |                                       |

|                           |    |    |                                       |

| 12. Radio Management    A | 2  | 1  | One may be inoperative provided:      |

|     Units (RMU)           |    |    |     a) Clearance Delivery Unit        |

|     (CV-5800)             |    |    |        (CDU) is operative, and        |

|                           |    |    |     b) Repair is made within three    |

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

| 13. Clearance Delivery  A | 1  | 0  | May be inoperative provided:          |

|     Unit (CDU)            |    |    |     a) Both Radio Management Units    |

|     (CV-5800)             |    |    |        (RMU) are operative, and       |

|                           |    |    |     b) Repair is made within three    |

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

| 14. Cockpit Voice       A | 1  | 0  | May be inoperative provided:          |

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

|                           |    |    |        operates normally, and         |

|                           |    |    |     b) Repair is made within three    |

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

|     1) Aircraft only    A | 1  | 0  | May be inoperative provided repairs ] |

|        equipped with a    |    |    | are made within three flight days.  ] |

|        Cockpit Voice      |    |    |                                     ] |

|        Recorder (CVR)     |    |    |                                     ] |

|                           |    |    |                                       |

| 15. Radio Tuning Units  A | 2  | 1  | One may be inoperative provided       |

|     (RTU) (STC N49)       |    |    | repair is made within three flight    |

|                           |    |    | days.                                 |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 24-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Inverter              |    |    |  DELETED in Revision 9.               |

|                           |    |    |                                       |

| 2.  Transformer         B | 1  | 0  | May be inoperative provided both      |

|     Rectifier Unit        |    |    | Generators (DC) are operative.        |

|     (TRU)                 |    |    |                                       |

|                           |    |    |                                       |

| 3.  Generator (DC)      B | 2  | 1  | One may be inoperative provided:      |

|     (Engine Driven)       |    |    |     a) APU Generator (DC) of          |

|                           |    |    |        equivalent rating is           |

|                           |    |    |        operated for the entire        |

|                           |    |    |        flight, and                    |

|                           |    |    |     b) Aircraft is operated within    |

|                           |    |    |        the APU altitude limitations   |

|                           |    |    |        for starting and operating.    |

|                           |    |    |                                       |

| *** 1) Aircraft with 35 B | 2  | 1  | (M)One may be inoperative provided:   |

|        or less Amp TRU    |    |    |     a) Aircraft is operated in VMC,   |

|        (GTC 85-90F)       |    |    |     b) The Cockpit Heater and         |

|                           |    |    |        Coffee Maker are disabled,     |

|                           |    |    |     c) Load on the good DC            |

|                           |    |    |        generator is maintained at     |

|                           |    |    |        80% or less, and               |

|                           |    |    |     d) The Transformer Rectifier      |

|                           |    |    |        Unit is operative.             |

|                           |    |    |                                       |

| *** 2) Aircraft with    B | 2  | 1  | (M)One may be inoperative provided:   |

|        200 or more Amp    |    |    |     a) The Cockpit Heater and         |

|        TRU                |    |    |        Coffee Maker are disabled,     |

|                           |    |    |     b) Load on the good DC            |

|                           |    |    |        generator is maintained at     |

|                           |    |    |        80% or less, and               |

|                           |    |    |     c) The Transformer Rectifier      |

|                           |    |    |        Unit is operative.             |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 24-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 3. Generator (DC)         |    |    |                                       |

|    (Engine Driven)        |    |    |                                       |

|    (Cont'd)               |    |    |                                       |

|                           |    |    |                                       |

| *** 3) Generator (DC)   B | 2  | 1  | One may be inoperative provided:      |

|        (Engine Driven)    |    |    |     a) APU Generator is operated      |

|        (Airplanes with    |    |    |        in flight and on the ground    |

|        APU GTC 85-90F)    |    |    |        as needed, and                 |

|                           |    |    |     b) Airplane is operated           |

|                           |    |    |        within the APU altitude        |

|                           |    |    |        limitations for starting       |

|                           |    |    |        and operating.                 |

|                           |    |    |                                       |

|                         A | 2  | 1  | (O)One may be inoperative provided:   |

|                           |    |    |     a) VHF Transceivers, DG Compass   |

|                           |    |    |        System,and VOR System are      |

|                           |    |    |        operative,                     |

|                           |    |    |     b) The circuit brakers on the     |

|                           |    |    |        Cockpit Heater and Coffee      |

|                           |    |    |        Maker are pulled,              |

|                           |    |    |     c) The load on the operative      |

|                           |    |    |        generator is maintained at     |

|                           |    |    |        80% or less,                   |

|                           |    |    |     d) The Transformer Rrectifier     |

|                           |    |    |        Unit (TRU) is operative, and   |

|                           |    |    |     e) Repair is made within three    |

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

| 4.  Inverter Fail Light C | 1  | 0  | May be inoperative provided the       |

|     System                |    |    | Instrument Power Failure              |

|                           |    |    | Indicators are operative.             |

|                           |    |    |                                       |

|                         C | 1  | 0  | May be inoperative provided the       |

|                           |    |    | Inverter ON Indicator Light is        |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                         C | 1  | 0  | May be inoperative provided EFIS      |

|                           |    |    | Power Failure is displayed when       |

|                           |    |    | Inverter fails.                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 24-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 5.  Alternators (Engine B | 2  | 1  | One may be inoperative provided:      |

|     Driven) (Aircraft     |    |    |     a) APU Alternator is operative,   |

|     with STC SA4-1343)    |    |    |     b) APU Alternator can be used     |

|                           |    |    |        to Feather prop of the         |

|                           |    |    |        unassociated engine, and       |

|                           |    |    |     c) APU Alternator is operated     |

|                           |    |    |        during Takeoff.                |

|                           |    |    |                                       |

| 6.  Voltmeters (DC)       |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 7.  Loadmeters (DC)       |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 8.  Fuses                 |    |    | DELETED in Revision 11.               |

|                           |    |    |                                       |

| 9.  Voltmeter (AC)        |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 10. Alternator          C | 2  | 1  | One may be inoperative provided the   |

|     Inoperative Light     |    |    | AC voltmeters and ammeters are        |

|     System                |    |    | operative in all positions.           |

|                           |    |    |                                       |

| 11. Batteries             |    |    | DELETED in Revision 11.               |

|                           |    |    |                                       |

| 12. Battery Temperature D | 1  | 0  | May be inoperative provided Nicad     |

| *** Monitoring System     |    |    | Batteries are not installed.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 13. Compass Power       A | 1  | 0  | May be inoperative provided:          |

| *** Failure Indicator     |    |    |     a) Aircraft is operated in Day    |

|                           |    |    |        VC, and                        |

|                           |    |    |     b) Repair is made within three    |

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

| 14. Essential Bus       C | 1  | 0  | (O)May be inoperative provided        |

| *** Warning Light         |    |    | essential bus power is monitored on   |

|     System                |    |    | voltmeter.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 24-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 24  ELECTRICAL POWER      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 15. ATM Alternator      C | 1  | 0  |                                       |

| ***                       |    |    |                                       |

|                           |    |    |                                       |

| 16. APU Alternator      C | 1  | 0  | May be inoperative provided both      |

| *** (STC SA4-1343)        |    |    | Engine Driven Alternators are         |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

| 17. Frequency Meter     C | 1  | 0  |                                       |

| ***                       |    |    |                                       |

|                           |    |    |                                       |

| 18. GTC Alternator (DC) C | 1  | 0  |                                       |

| *** (STC SA4-1343)        |    |    |                                       |

|                           |    |    |                                       |

| 19. Generator (DC)      B | 1  | 0  | May be inoperative provided both      |

|     (APU)                 |    |    | Engine Driven Generators (DC) are     |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 25-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Emergency Locator   A | -  | 0  | (M)May be inoperative provided:       |

| *** Transmitter           |    |    |     a) Affected ELT is deactivated    |

|                           |    |    |        or removed using accepted      |

|                           |    |    |        procedures, and                |

|                           |    |    |     b) Repair is made within FAR      |

|                           |    |    |        time limits.                   |

|                           |    |    |                                       |

| 2.  Flight Attendant      |    |    |                                       |

|     Seat Assembly         |    |    |                                       |

|     (Single or Dual       |    |    |                                       |

|     Position)             |    |    |                                       |

|                           |    |    |                                       |

|      1) Seats Required  B | -  | -  | (M)(O)One Single or one Dual          |

|         by FAR            |    |    | Position Seat Assembly may be         |

|                           |    |    | inoperative provided:                 |

|                           |    |    |     a) Affected seat(s) is not        |

|                           |    |    |        occupied,                      |

|                           |    |    |     b) Flight Attendant(s)            |

|                           |    |    |        displaced by inoperative       |

|                           |    |    |        seat(s) occupies 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:  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: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 25-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 2.  Flight Attendant      |    |    |                                       |

|     Seat Assembly         |    |    |                                       |

|     (Single or Dual       |    |    |                                       |

|     Position) (Cont'd)    |    |    |                                       |

|                           |    |    |                                       |

| ***  2) Seats in Excess D | -  | -  | (M)(O)May be inoperative provided:    |

|      of the Number        |    |    |     a) Affected seat(s) is not        |

|      Required by FAR      |    |    |        occupied, and                  |

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

|                           |    |    |        stowed or secured in the       |

|                           |    |    |        retracted position.            |

|                           |    |    |                                       |

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

|                           |    |    |          not stow automatically is    |

|                           |    |    |          considered inoperative.      |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  Individual operator MELs     |

|                           |    |    |          will be specific as to the   |

|                           |    |    |          numbers and locations of     |

|                           |    |    |          inoperative seats and        |

|                           |    |    |          combinations of seats to     |

|                           |    |    |          ensure the proximity to      |

|                           |    |    |          exits and distribution       |

|                           |    |    |          requirements of the          |

|                           |    |    |          applicable FAR are met.      |

|                           |    |    |                                       |

| 3.  Shoulder Harnesses  B | -  | -  | May be inoperative provided           |

|                           |    |    | associated seat position is           |

|                           |    |    | considered inoperative.               |

|                           |    |    |                                       |

| 4.  "Fasten Seat Belt   C | -  | -  | One or more signs or placards may     |

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

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

|                           |    |    | from each occupied passenger seat.    |

|                           |    |    |                                       |

| 5.  Flight Attendant    B | -  | -  | May be inoperative provided           |

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

|                           |    |    | Position is considered inoperative.   |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 25-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 6.  Observer Seat       A | -  | 1  | May be inoperative provided:          |

|     (Including            |    |    |     a) A passenger seat in the        |

|     Associated            |    |    |        passenger cabin is available   |

|     Equipment)            |    |    |        to an FAA inspector for the    |

|                           |    |    |        performance of official        |

|                           |    |    |        duties, and                    |

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

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

| 7.  Megaphones            |    |    |                                       |

|                           |    |    |                                       |

|      1) Passenger       D | -  | -  | (M)Any in excess of those required    |

|         Configuration     |    |    | by FAR may be inoperative or          |

|                           |    |    | missing provided:                     |

|                           |    |    |     a) The inoperative megaphone is   |

|                           |    |    |        removed from the passenger     |

|                           |    |    |        cabin, and                     |

|                           |    |    |     b) Required Distribution is       |

|                           |    |    |        maintained.                    |

|                           |    |    |                                       |

| *** 2) Cargo            D | -  | O  |                                       |

|        Configuration      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 25-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 8.  Passenger             | -  | 0  | Passenger convenience items, as       |

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

|                           |    |    | related to passenger convenience,     |

|                           |    |    | comfort or entertainment such as,     |

|                           |    |    | but not limited to, galley            |

|                           |    |    | equipment, movie equipment, ash       |

|                           |    |    | trays, stereo equipment, overhead     |

|                           |    |    | reading lamps.  Items addressed       |

|                           |    |    | elsewhere in this document shall      |

|                           |    |    | not be included.                      |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  (M) and (O) procedures may   |

|                           |    |    |          be required and included     |

|                           |    |    |          in the air carrier's         |

|                           |    |    |          appropriate document.        |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  LAVATORY DOOR ASH TRAYS      |

|                           |    |    |          ARE NOT CONSIDERED           |

|                           |    |    |          CONVENIENCE ITEMS.           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 25-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 9.  Passenger Seat(s)   D | -  | -  | May be inoperative provided:        ] |

|                           |    |    |     a) Seat does not block          ] |

|                           |    |    |        emergency exit,              ] |

|                           |    |    |     b) Seat does not restrict any   ] |

|                           |    |    |        passenger from access to the ] |

|                           |    |    |        main aircraft aisle, and     ] |

|                           |    |    |     b) The affected seat(s) are     ] |

|                           |    |    |        blocked and placarded "DO    ] |

|                           |    |    |        NOT OCCUPY".                 ] |

|                           |    |    |                                       |

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

|                           |    |    |          lap belt is considered     ] |

|                           |    |    |          inoperative.               ] |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  Inoperative seat(s) do not ] |

|                           |    |    |          affect the required number ] |

|                           |    |    |          of Flight Attendants.      ] |

|                           |    |    |                                       |

|                           |    |    | NOTE 3:  Affected seat(s) may       ] |

|                           |    |    |          include the seat(s) behind ] |

|                           |    |    |          and/or adjacent outboard   ] |

|                           |    |    |          seats.                     ] |

|                           |    |    |                                       |

|     1) Recline          D | -  | -  | May be inoperative and seat         ] |

|        Mechanism          |    |    | occupied provided seat is secured   ] |

|                           |    |    | in the up-right position.           ] |

|                           |    |    |                                       |

|     2) Underseat        D | -  | -  | (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       ] |

|                           |    |    |        inoperative restraining bar. ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 25-6     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10. First Aid Kits      D | -  | -  | Any in excess of those required by  ] |

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

|                           |    |    | provided required distribution is   ] |

|                           |    |    | maintained.                         ] |

|                           |    |    |                                       |

| 11. Exterior Lavatory     |    |    |                                     ] |

|     Door Ashtrays         |    |    |                                     ] |

|                           |    |    |                                     ] |

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

|        more then one      |    |    | replaced within 10 calendar days.   ] |

|        exterior           |    |    |                                     ] |

|        lavatory door      |    |    |                                     ] |

|        ashtray            |    |    |                                     ] |

|        installed          |    |    |                                     ] |

|                           |    |    |                                     ] |

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

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

|        exterior           |    |    |                                     ] |

|        lavatory door      |    |    |                                     ] |

|        ashtray            |    |    |                                     ] |

|        installed          |    |    |                                     ] |

|                           |    |    |                                       |

| 12. Galley Waste        C | -  | -  | (M)May be inoperative provided the  ] |

|     Receptacles Access    |    |    | container is empty and the access   ] |

|     Doors/Covers          |    |    | is secured to prevent waste         ] |

|                           |    |    | introduction into the compartment.  ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 25-7     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 25  EQUIPMENT/FURNISHINGS |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 13. Cargo Restraint     C | -  | -  | (M)May be inoperative or missing    ] |

|     Systems               |    |    | such that the effect is that the    ] |

|                           |    |    | item must be considered             ] |

|                           |    |    | inoperative, provided acceptable    ] |

|                           |    |    | cargo loading limits from an        ] |

|                           |    |    | approved source, i.e.,an Approved   ] |

|                           |    |    | Cargo Loading Manual, Cargo         ] |

|                           |    |    | Handling Manual, or Weight and      ] |

|                           |    |    | Balance Document are observed.      ] |

|                           |    |    |                                       |

|                         C | -  | -  | May be inoperative or missing such  ] |

|                           |    |    | that the effect is that the item    ] |

|                           |    |    | must be considered inoperative,     ] |

|                           |    |    | provided cargo compartment remains  ] |

|                           |    |    | empty.                              ] |

|                           |    |    |                                       |

|                         C | -  | -  | May be inoperative or missing such  ] |

|                           |    |    | that the effect is that the item    ] |

|                           |    |    | must be considered inoperative,     ] |

|                           |    |    | provided pallet with inoperative    ] |

|                           |    |    | lock(s) is removed.                 ] |

|                           |    |    |                                       |

| 14. Overhead Storage    C | -  | -  | May be inoperative provided:        ] |

|     Bin(s)/Cabin and      |    |    |     a) Procedures are established   ] |

|     Galley Storage        |    |    |        to secure compartment        ] |

|     Compartment/Closets   |    |    |        CLOSED,                      ] |

|                           |    |    |     b) Compartment is not used for  ] |

|                           |    |    |        storage of emergency         ] |

|                           |    |    |        equipment, and               ] |

|                           |    |    |     c) Affected compartment is not  ] |

|                           |    |    |        used for storage of any      ] |

|                           |    |    |        item(s) except for those     ] |

|                           |    |    |        permanently affixed.         ] |

|                           |    |    |                                     ] |

|                           |    |    | NOTE:  If no partitions are         ] |

|                           |    |    |        installed, the entire        ] |

|                           |    |    |        overhead storage compartment ] |

|                           |    |    |        is considered one bin.       ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 26-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Engine Fire Warning   |    |    |  DELETED in Revision 9.               |

|     And Detection         |    |    |                                       |

|     System                |    |    |                                       |

|                           |    |    |                                       |

| 2.  Upper Aft Baggage     |    |    | DELETED in Revision 9.                |

|     Compartment Viewing   |    |    |                                       |

|     Window                |    |    |                                       |

|                           |    |    |                                       |

| 3.  Baggage Compartment C | -  | -  | May be inoperative provided           |

| *** Lighting System       |    |    | remaining lighting provides           |

|     Lights                |    |    | sufficient illumination of the        |

|                           |    |    | baggage area for smoke detection.     |

|                           |    |    |                                       |

| 4.  Engine Fire           |    |    | DELETED in Revision 9.                |

|     Extinguisher System   |    |    |                                       |

|                           |    |    |                                       |

| 5.  Portable Fire       D | -  | -  | Any in excess of those required by    |

|     Extinguisher          |    |    | FAR may be inoperative provided:      |

|                           |    |    |     a) The inoperative fire         ] |

|                           |    |    |        extinguisher is tagged       ] |

|                           |    |    |        inoperative, removed from    ] |

|                           |    |    |        the installed location, and  ] |

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

|                           |    |    |        can not be mistaken for a    ] |

|                           |    |    |        functional unit, and         ] |

|                           |    |    |     b) Required distribution is     ] |

|                           |    |    |        maintained                   ] |

|                           |    |    |                                       |

| 6.  Fire Extinguisher   C | 4  | 0  | (M)May be missing provided prior to   |

| *** Thermal Discharge     |    |    | first flight of each day bottles      |

|     Discs                 |    |    | are weighed or gauge readings made    |

|                           |    |    | to determine adequate charge.         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 26-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 7.  Lavatory Smoke      C | -  | -  | (M)(O)For each lavatory, the          |

|     Detection Systems     |    |    | lavatory smoke detection system may ] |

|                           |    |    | be inoperative provided:            ] |

|                           |    |    |     a) Lavatory waste receptacle is   |

|                           |    |    |        empty,                         |

|                           |    |    |     b) Lavatory door is locked        |

|                           |    |    |        CLOSED and placarded,          |

|                           |    |    |        "INOPERATIVE - DO NOT          |

|                           |    |    |        ENTER", and                    |

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

|                           |    |    |        purpose.                       |

|                           |    |    |                                       |

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

|                           |    |    |          intended to preclude         |

|                           |    |    |          lavatory inspections by      |

|                           |    |    |          crewmembers.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  Lavatory Smoke Detection     |

|                           |    |    |          Systems are not required     |

|                           |    |    |          for all-cargo operations.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 26-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 26  FIRE PROTECTION       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 8.  Lavatory Fire       C | -  | -  | For each lavatory, the Lavatory       |

|     Extinguisher          |    |    | Fire Extinguisher System may be       |

|     Systems               |    |    | inoperative provided Lavatory Smoke   |

|                           |    |    | Detection System is operative.        |

|                           |    |    |                                       |

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

|                           |    |    |     a) Lavatory waste receptacle is   |

|                           |    |    |        empty,                         |

|                           |    |    |     b) Lavatory door is locked        |

|                           |    |    |        CLOSED and placarded,          |

|                           |    |    |        "INOPERATIVE - DO NOT          |

|                           |    |    |        ENTER", and                    |

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

|                           |    |    |        purpose.                       |

|                           |    |    |                                       |

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

|                           |    |    |          intended to preclude         |

|                           |    |    |          lavatory inspections by      |

|                           |    |    |          crewmembers.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  Lavatory Fire Extinguisher   |

|                           |    |    |          Systems are not required     |

|                           |    |    |          for all- cargo operations.   |

|                           |    |    |                                       |

| 9.  Cargo Compartment   C | -  | 0  | May be inoperative provided         ] |

|     Fire Detection/       |    |    | associated cargo compartment        ] |

|     Suppression Systems   |    |    | remains empty.                      ] |

|                           |    |    |                                     ] |

|                           |    |    | NOTE:  Does not preclude the        ] |

|                           |    |    |        carriage of empty cargo      ] |

|                           |    |    |        containers, pallets,         ] |

|                           |    |    |        ballast, ect.                ] |

|                           |    |    |                                     ] |

|                           |    |    | NOTE:  Class E cargo compartments   ] |

|                           |    |    |        require only the             ] |

|                           |    |    |        installation of smoke or     ] |

|                           |    |    |        fire detection systems (not  ] |

|                           |    |    |        suppression).                ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 27-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 27  FLIGHT CONTROLS       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Wing Flaps          B | 1  | 0  | (O)May be inoperative provided:       |

|     Electrical Control    |    |    |     a) The retraction (up) side is    |

|     System, Downside      |    |    |        operative,                     |

|     Solenoid              |    |    |     b) The Wing Flap Position         |

|                           |    |    |        Indication System is           |

|                           |    |    |        operative,                     |

|                           |    |    |     c) Flaps are operated in          |

|                           |    |    |        accordance with applicable     |

|                           |    |    |        AFM.                           |

|                           |    |    |                                       |

| 2.  Wing Flap Position  B | 2  | 1  | (O)One may be inoperative provided:   |

|     Indication System     |    |    |     a) A visual inspection of wing    |

|     Needles               |    |    |        flap position is               |

|                           |    |    |        accomplished before each       |

|                           |    |    |        takeoff, and                   |

|                           |    |    |     b) The wing flaps electrical      |

|                           |    |    |        control system is operative.   |

|                           |    |    |                                       |

| 3.  Flap/Landing Gear     |    |    | DELETED in Revision 9.                |

|     Aural Warning         |    |    |                                       |

|     System                |    |    |                                       |

|                           |    |    |                                       |

| 4.  Takeoff Warning       |    |    | DELETED in Revision 9.                |

|     Horn System           |    |    |                                       |

|                           |    |    |                                       |

| 5.  Electric Trim       C | 1  | 0  | (M)May be inoperative provided it     |

| *** System                |    |    | is verified that the Manual Trim      |

|                           |    |    | System is operative.                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 28-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 28  FUEL                  |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Fuel Quantity       C | 2  | 1  | (M)One may be inoperative provided:   |

|     Indicators            |    |    |     a) Both fuel flow meters are      |

|     (Cockpit)             |    |    |        operative, and                 |

|                           |    |    |     b) Fuel quantity is checked by    |

|                           |    |    |        an alternate measuring         |

|                           |    |    |        device before each takeoff.    |

|                           |    |    |                                       |

| 2.  DELETED               |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 3.  DELETED               |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 4.  Fuel Quantity       D | 2  | 0  |                                       |

| *** Indicators (Under     |    |    |                                       |

|     Wing)                 |    |    |                                       |

|                           |    |    |                                       |

| 5.  Electric Fuel       D | 4  | 2  | (O)One per side may be inoperative    |

| *** Boast Pumps           |    |    |    provided:                          |

|     (S/N 454 ONLY)        |    |    |     a) The operative Fuel Boast       |

|                           |    |    |        Pump is selected, and          |

|                           |    |    |     b) The Fuel Boast Pump Low        |

|                           |    |    |        Pressure Light is              |

|                           |    |    |        extinguished.                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 29-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 29  HYDRAULIC POWER       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Hydraulic Pumps       |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 2.  Quantity Indicator    |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 3.  System Pressure       |    |    | DELETED in Revision 11.               |

|     Indication System     |    |    |                                       |

|     (Single Indicator     |    |    |                                       |

|     System)               |    |    |                                       |

|                           |    |    |                                       |

| 4.  Main Pressure       C | 1  | 0  |                                       |

|     Indication System     |    |    |                                       |

|     (2 Indicator          |    |    |                                       |

|     System)               |    |    |                                       |

|                           |    |    |                                       |

| 5.  AC Hydraulic Pump   C | 1  | 0  | (O)May be inoperative provided the    |

|     Pressure Indicating   |    |    | AC Hydraulic Pump output is checked   |

|     Light (Green)         |    |    | before each takeoff.                  |

|                           |    |    |                                       |

| 6.  Brake Pressure        |    |    | DELETED in Revision 11.               |

|     Indication System     |    |    |                                       |

|                           |    |    |                                       |

| 7.  Left Engine Driven  C | 1  | 0  |                                       |

| *** Hydraulic Pump        |    |    |                                       |

|     Warning Light         |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 30-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| 1.  Windshield Wipers   C | 2  | 0  | Both may be inoperative provided      |

|                           |    |    | aircraft is not operated in           |

|                           |    |    | precipitation within 5 miles of the   |

|                           |    |    | airport of departure or arrival.      |

|                           |    |    |                                       |

| 2.  Propeller           B | 2  | 0  | (M)(O)May be inoperative provided     |

|     Electrical Anti-      |    |    | an approved compound is utilized      |

|     Icing and De-Icing    |    |    | in accordance with the AFM.           |

|     System                |    |    |                                       |

|                         C | 2  | 0  | May be inoperative provided           |

|                           |    |    | Aircraft is not operated in known     |

|                           |    |    | or forecast icing conditions.         |

|                           |    |    |                                       |

| 3.  Wing and Tail       C | 1  | 0  | (O)May be inoperative provided        |

|     Anti-Icing System     |    |    | aircraft is not operated in known     |

|                           |    |    | or forecast icing conditions.         |

|                           |    |    |                                       |

| 4.  Automatic           C | 1  | 0  |                                       |

| *** Temperature           |    |    |                                       |

|     Control, Wing and     |    |    |                                       |

|     Tail Anti-Icing       |    |    |                                       |

|                           |    |    |                                       |

| 5.  Captain's Pitot     B | 1  | 0  | May be inoperative provided:          |

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

|                           |    |    |        known of forecast icing        |

|                           |    |    |        conditions, and                |

|                           |    |    |     b) Aircraft is operated in VMC.   |

|                           |    |    |                                       |

| 6.  NESA Panels Systems C | 3  | 0  | (O)May be inoperative provided        |

|                           |    |    | aircraft is not operated in known     |

|                           |    |    | or forecast icing conditions.         |

|                           |    |    |                                       |

|     1) Left Direct      C | 1  | 0  |                                       |

|        Vision Window      |    |    |                                       |

|                           |    |    |                                       |

| 7.  Windshield Rain     D | 1  | 0  |                                       |

| *** Repellent System      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 8.  Windshield NESA     C | 1  | 0  |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 30-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 30  ICE AND RAIN          |    |    |                                       |

|     PROTECTION            |    |    |                                       |

|                           |    |    |                                       |

| *** Indicator             |    |    |                                       |

|                           |    |    |                                       |

| 9.  Engine Ice Detector C | 2  | 1  | One may be inoperative.               |

|     Light System          |    |    |                                       |

|                           |    |    |                                       |

| 10. Frost Shield-       C | 2  | 0  |                                       |

| *** Cockpit Sliding       |    |    |                                       |

|     Window                |    |    |                                       |

|                           |    |    |                                       |

| 11. Visual Icing        C | -  | 0  |                                       |

| *** Indicator             |    |    |                                       |

|                           |    |    |                                       |

| 12. Pitot Heat INOP     C | 1  | 0  | (O)May be inoperative provided:       |

|     Warning Light         |    |    |     a) All other elements are         |

|     System                |    |    |        verified operative before      |

|                           |    |    |        each takeoff, and              |

|                           |    |    |     b) The aircraft is not operated   |

|                           |    |    |        in known or forecast icing     |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

| 13. Pitot Heat Ammeter  B | 1  | 0  | (M)May be inoperative provided all    |

|                           |    |    | heater elements are verified          |

|                           |    |    | operative before each takeoff.        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 31-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 31  INDICATING/RECORDING  |    |    |                                       |

|     SYSTEMS               |    |    |                                       |

|                           |    |    |                                       |

| 1.  Clock (Cockpit)     D | -  | 1  | Any in excess of those required by    |

|                           |    |    | FAR may be inoperative.               |

|                           |    |    |                                       |

| 2.  Flight Data         A | 1  | 0  | May be inoperative provided:          |

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

|     System                |    |    |        is operative,                  |

|                           |    |    |     b) Airplane is not dispatched   ] |

|                           |    |    |        from a designated airport    ] |

|                           |    |    |        where repairs or             ] |

|                           |    |    |        replacements can be made,    ] |

|                           |    |    |        and                          ] |

|                           |    |    |     c) Repairs are made within        |

|                           |    |    |        three flight days.             |

|                           |    |    |                                       |

| 3.  Cockpit Voice         |    |    | Moved to Chapter 23.                  |

|     Recorder              |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 32-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 32  LANDING GEAR          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Warning and           |    |    | DELETED in Revision 9.                |

|     Indicating System     |    |    |                                       |

|     (Lights and Horn)     |    |    |                                       |

|                           |    |    |                                       |

| 2.  Emergency Brake       |    |    | DELETED in Revision 9.                |

|     System                |    |    |                                       |

|                           |    |    |                                       |

| 3.  Anti-Skid System    C | -  | 0  | (O)May be inoperative provided        |

| ***                       |    |    | operations are conducted in           |

|                           |    |    | compliance with the AFM.              |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 33-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Emergency Interior    |    |    |  DELETED in Revision 9.               |

|     Exit Lighting         |    |    |                                       |

|     System                |    |    |                                       |

|                           |    |    |                                       |

| 2.  Emergency Exterior    |    |    |                                       |

|     Exit Lighting         |    |    |                                       |

|     System                |    |    |                                       |

|                           |    |    |                                       |

|      1) Passenger       B | 1  | 0  | May be inoperative provided           |

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

|                           |    |    |                                       |

|      2) Cargo           D | -  | 0  |                                       |

|         Configuration     |    |    |                                       |

|                           |    |    |                                       |

| 3.  Position Light      C | -  | 0  |                                       |

| *** Flasher               |    |    |                                       |

|                           |    |    |                                       |

| 4.  Position Lights       |    |    |                                       |

|                           |    |    |                                       |

|      1) Position        C | -  | 3  | May be inoperative provided the     ] |

|         Lights, Wing      |    |    | following minimum light bulbs       ] |

|         Tips and Tail     |    |    | operate normally:                   ] |

|         (Bulbs)           |    |    |     a) One red wing tip bulb,       ] |

|                           |    |    |     b) One green wing tip bulb, and ] |

|                           |    |    |     c) One white tail bulb.         ] |

|                           |    |    |                                       |

|                         C | -  | 0  | May be inoperative provided         ] |

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

|                           |    |    |                                       |

| *** 2) Fuselage Lights  C | 2  | 0  |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 33-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 5.  Wing Illumination   C | 2  | 1  |                                     ] |

|     Lights                |    |    |                                       |

|                           |    |    |                                       |

|                         C | 2  | 0  | (O)May be inoperative provided:     ] |

|                           |    |    |     a) Ground deicing procedures do ] |

|                           |    |    |        not require their use, and   ] |

|                           |    |    |     b) A portable lamp/light of     ] |

|                           |    |    |        adequate capacity for wing   ] |

|                           |    |    |        and/or control surface       ] |

|                           |    |    |        inspection is available for  ] |

|                           |    |    |        night operation in icing     ] |

|                           |    |    |        conditions.                  ] |

|                           |    |    |                                       |

| 6.  Landing Lights      C | 2  | 0  | May be inoperative provided           |

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

|                           |    |    |                                       |

|                         C | 2  | 1  | May be inoperative provided an        |

|                           |    |    | approved Taxi Light of at least 600   |

|                           |    |    | watts is installed and operative.     |

|                           |    |    |                                       |

| 7.  Taxi Light          C | 1  | 0  | May be inoperative provided both      |

|                           |    |    | Landing Lights are opertive.          |

|                           |    |    |                                       |

|                         C | 1  | 0  | May be inoperative provided           |

|                           |    |    | airplane is not operated at night.    |

|                           |    |    |                                       |

| 8.  Wheel Well Lights   C | 1  | 0  | May be inoperative provided no        |

|                           |    |    | procedures require their use.         |

|                           |    |    |                                       |

| 9.  Passenger Loading   C | 1  | 0  | (M)May be inoperative provided        |

|     Stair Light System    |    |    | light sufficient to illuminate        |

|                           |    |    | steps is provided for loading and     |

|                           |    |    | unloading of passengers at night.     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 33-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10. Cockpit and         C | -  | -  | (M)(O)May be inoperative provided:    |

|     Instrument Light      |    |    |     a) Flight Station Essential Bus   |

|     System Lights         |    |    |        Lighting is operative, and     |

|                           |    |    |     b) Sufficient lighting is         |

|                           |    |    |        operative to make each         |

|                           |    |    |        instrument, control and        |

|                           |    |    |        other device for which it is   |

|                           |    |    |        provided easily readable,      |

|                           |    |    |        and                            |

|                           |    |    |     c) Direct rays and reflections    |

|                           |    |    |        do not impair visibility       |

|                           |    |    |        either inside or outside the   |

|                           |    |    |        aircraft, and                  |

|                           |    |    |     d) Lighting intensity can be      |

|                           |    |    |        controlled or preset to a      |

|                           |    |    |        satisfactory level for         |

|                           |    |    |        expected flight conditions,    |

|                           |    |    |        and                            |

|                           |    |    |     e) Light configuration at         |

|                           |    |    |        departure is acceptable to     |

|                           |    |    |        the flight crew.               |

|                           |    |    |                                       |

| 11. Cabin Interior      C | -  | -  | May be inoperative provided:          |

|     Lighting System       |    |    |     a) Cabin emergency lighting is    |

|     Lights                |    |    |        operative,                     |

|                           |    |    |     b) Sufficient lighting is         |

|                           |    |    |        operative for crew to          |

|                           |    |    |        perform required duties, and   |

|                           |    |    |     c) Lighting configuration at      |

|                           |    |    |        dispatch is acceptable to      |

|                           |    |    |        the flight crew.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 33-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 12. Passenger Notice      |    |    |                                       |

|     System (No Smoking    |    |    |                                       |

|     and Fasten Seat       |    |    |                                       |

|     Belt Signs)           |    |    |                                       |

|                           |    |    |                                       |

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

|         Configuration     |    |    |     a) Operations procedures are      |

|                           |    |    |        established for alerting the   |

|                           |    |    |        Flight Attendants and          |

|                           |    |    |        notifying the passengers by    |

|                           |    |    |        use of the Public Address      |

|                           |    |    |        System when Seat Belts         |

|                           |    |    |        should be fastened, Smoking    |

|                           |    |    |        prohibited, and passengers     |

|                           |    |    |        should return to cabin from    |

|                           |    |    |        lavatories,                    |

|                           |    |    |     b) Call Bells and Cockpit-to-     |

|                           |    |    |        Cabin interphone systems are   |

|                           |    |    |        operative, and                 |

|                           |    |    |     c) Public Address System is       |

|                           |    |    |        operative and can be clearly   |

|                           |    |    |        heard throughout the cabin     |

|                           |    |    |        and lavatories during          |

|                           |    |    |        flight.                        |

|                           |    |    |                                       |

|      2) Cargo           D | -  | -  |                                       |

|         Configuration     |    |    |                                       |

|                           |    |    |                                       |

| 13. Door Warning Lights C | -  | 0  | (O)May be inoperative provided:       |

|                           |    |    |     a) All Bayonets and Hooks for a   |

|                           |    |    |        door associated with an        |

|                           |    |    |        inoperative Light can be       |

|                           |    |    |        visually checked from inside   |

|                           |    |    |        the cabin, and                 |

|                           |    |    |     b) All associated bayonets and    |

|                           |    |    |        hooks are in locked            |

|                           |    |    |        positions before each          |

|                           |    |    |        departure.                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 33-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 14. Anti-Collision      C | 1  | 0  | May be inoperative provided           |

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

|                           |    |    |                                       |

|      1) Individual      C | -  | -  | May be inoperative provided the       |

|         Bulbs             |    |    | requirements of FAR 25.1401 are       |

|                           |    |    | satisfied.                            |

|                           |    |    |                                       |

| 15. Supplemental Strobe C | 1  | 0  |                                       |

| *** Light System          |    |    |                                       |

|                           |    |    | NOTE:  These lights are not           |

|                           |    |    |        installed to meet the          |

|                           |    |    |        requirements of FAR 25.1401.   |

|                           |    |    |                                       |

| 16. Nacelle             C | 2  | 0  |                                       |

| *** Illumination Lights   |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 17. Master Caution      A | -  | 0  | (O)May be inoperative provided:       |

| *** System                |    |    |     a) Procedures are established     |

|                           |    |    |        and used to monitor            |

|                           |    |    |        associated lights, and         |

|                           |    |    |     b) Repair is made within three    |

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 33-6     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 33  LIGHTS                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 18. Floor Proximity     C | -  | 0  | (M)Individual lights may be           |

| *** Emergency Escape      |    |    | inoperative provided FAA approved     |

|     Path Marking System   |    |    | minimum acceptable lighting levels    |

|     Lights                |    |    | specified in one of the following     |

|                           |    |    | documents are complied with:          |

|                           |    |    |     a) FAA Engineering Approval       |

|                           |    |    |        letter.                        |

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

|                           |    |    |        Type Design holder.            |

|                           |    |    |     c) Limitations and conditions     |

|                           |    |    |        section of the applicable      |

|                           |    |    |        Supplemental Type              |

|                           |    |    |        Certificate (STC).             |

|                           |    |    |     d) An FAA approved report         |

|                           |    |    |        incorporated in the Master     |

|                           |    |    |        Drawing List for the           |

|                           |    |    |        Applicable STC.                |

|                           |    |    |                                       |

| 19. Logo Lights         D | -  | 0  |                                       |

| ***                       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  EFIS Airspeed       D | 2  | 0  |                                       |

| *** Indicator             |    |    |                                     ] |

|     (Honeywell            |    |    |                                       |

|     Installation)         |    |    |                                       |

|                           |    |    |                                       |

| 2.  Standby Altimeter   B | 1  | 0  |                                       |

| *** (Mechanical Primary   |    |    |                                       |

|     Altimeter System)     |    |    |                                       |

|                           |    |    |                                       |

| 3.  Compass System      D | -  | 2  | May be inoperative provided:          |

|     Sensors               |    |    |     a) Both Pilot's Directional       |

|     (Directional Gyro,    |    |    |        Compass Systems are            |

|     AHRS, IRS, etc.)      |    |    |        operative from independent     |

|                           |    |    |        sources, and                   |

|                           |    |    |     b) Each pilot's panel has         |

|                           |    |    |        independent heading            |

|                           |    |    |        information.                   |

|                           |    |    |                                       |

| 4.  Standby Horizon     B | 1  | 0  | May be inoperative provided:          |

| *** Indicator             |    |    |     a) Day VMC is forecast for the    |

|                           |    |    |        entire route, and              |

|                           |    |    |     b) Standby Attitude Gyro is not   |

|                           |    |    |        required by AFM Limitations.   |

|                           |    |    |                                       |

| 5.  Turn and Slip         |    |    |                                       |

|     Indicators            |    |    |                                       |

|                           |    |    |                                       |

|      1) Slip Indication C | 2  | 0  | May be inoperative provided Slip      |

|                           |    |    | Indications are provided in each      |

|                           |    |    | pilot's panel.                        |

|                           |    |    |                                       |

|      2) Turn Indication C | 2  | 1  |                                       |

|                           |    |    |                                       |

|                         C | 2  | 0  | May be inoperative provided Standby   |

|                           |    |    | Attitude Gyro is installed and        |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-2     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 6.  Rate of Climb       D | -  | 2  | May be inoperative provided one is    |

|     Indicator (Vertical   |    |    | operative on each pilots instrument   |

|     Speed Indicator)      |    |    | panel.                                |

|                           |    |    |                                       |

| ***  1) EFIS Vertical   D | -  | 0  |                                     ] |

|         Speed             |    |    |                                       |

|         Indication        |    |    |                                       |

|         (Honeywell        |    |    |                                       |

|         Installation)     |    |    |                                       |

|                           |    |    |                                       |

| 7.  Non-Stabilized      B | 1  | 0  | (O)May be inoperative provided any  ] |

|     Magnetic (Standby)    |    |    | combination of three Gyro or INS    ] |

|     Compass               |    |    | (IRU) Stabilized Compass Systems    ] |

|                           |    |    | are operative.                      ] |

|                           |    |    |                                       |

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

|                           |    |    |     a) Any combination of two Gyro  ] |

|                           |    |    |        or INS (IRU) Stabilized      ] |

|                           |    |    |        Compass Systems operate      ] |

|                           |    |    |        normally, and                ] |

|                           |    |    |     b) Airplane is operated with    ] |

|                           |    |    |        Dual Independent Navigation  ] |

|                           |    |    |        Capability and under         ] |

|                           |    |    |        Positive Radar Control by    ] |

|                           |    |    |        ATC on the enroute portion   ] |

|                           |    |    |        of the flight.               ] |

|                           |    |    |                                       |

|                         B | 1  | 0  | (O)May be inoperative for flights   ] |

|                           |    |    | that are entirely within areas of   ] |

|                           |    |    | magnetic unreliability provided at  ] |

|                           |    |    | least two Stabilized Directional    ] |

|                           |    |    | Gyro Systems are installed, operate ] |

|                           |    |    | normally, and used in conjunction   ] |

|                           |    |    | with approved Free Gyro Navigation  ] |

|                           |    |    | Techniques.                         ] |

|                           |    |    |                                       |

| 8.  Distance Measuring  D | -  | -  | Any in excess of those required by    |

|     Equipment (DME)       |    |    | FAR may be inoperative.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-3     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 9.  Weather Radar       C | 1  | -  | Any in excess of those required by    |

|                           |    |    | FAR may be inoperative.               |

|                           |    |    |                                       |

|      1) Turbulence Mode D | -  | 0  |                                       |

|                           |    |    |                                       |

|      2) Ground Clutter  C | -  | 0  |                                       |

|         Reduction (GCR)   |    |    |                                       |

|                           |    |    |                                       |

|      3) Target (TGT)    D | -  | 0  |                                       |

|                           |    |    |                                       |

|      4) Sector Scan     D | -  | 0  |                                       |

|         (SECT)            |    |    |                                       |

|                           |    |    |                                       |

|      5) Slave           C | -  | 0  |                                       |

|         Annunciation      |    |    |                                       |

|                           |    |    |                                       |

|      6) Test Mode       C | -  | 0  | May be inoperative provided           |

|                           |    |    | alternate means is developed and      |

|                           |    |    | used to verify the system is          |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|      7) Flight Plan     D | -  | 0  |                                       |

|         Mode              |    |    |                                       |

|                           |    |    |                                       |

|      8) Ground Map Mode D | -  | 0  |                                       |

|                           |    |    |                                       |

|      9) Rain Echo       D | -  | 0  |                                       |

|         Attenuation       |    |    |                                       |

|         Mode (RCT)        |    |    |                                       |

|                           |    |    |                                       |

| 10. ATC Transponder and C | -  | -  | As required by FAR.                 ] |

|     Automatic Altitude    |    |    |                                       |

|     Reporting Systems   D | -  | -  | Any in excess of those required by    |

|                           |    |    | FAR may be inoperative.               |

|                           |    |    |                                       |

| 11. Radio Compass (ADF) D | -  | -  | Any in excess of those required by    |

|                           |    |    | FAR may be inoperative.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-4     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 12. VHF Navigation      D | -  | -  | Any in excess of those required by    |

|     Systems (VOR, ILS)    |    |    | FAR may be inoperative.               |

|                           |    |    |                                       |

| 13. Microwave Landing   D | -  | -  | Any in excess of those required by    |

| *** System (MLS)          |    |    | FAR may be inoperative.             ] |

|                           |    |    |                                       |

| 14. Marker Beacon       C | -  | -  | May be inoperative provided           |

|                           |    |    | affected Marker Beacon is not         |

|                           |    |    | required for the approach to be       |

|                           |    |    | flown.                                |

|                           |    |    |                                       |

| 15. Outside Air         D | -  | 1  | Any in excess of those required by    |

|     Temperature           |    |    | FAR may be inoperative.               |

|     Indicator             |    |    |                                       |

|                           |    |    |                                       |

| 16. Overspeed Warning   C | 1  | 0  | (O)May be inoperative provided:       |

|     Device (VMO)          |    |    |     a) Both Airspeed Indicators are   |

|                           |    |    |        operative, and                 |

|                           |    |    |     b) Indicated Airspeed is          |

|                           |    |    |        maintained at least 20 knots   |

|                           |    |    |        below indicated Vmo.           |

|                           |    |    |                                       |

| 17. Altitude Alerting   A | -  | 0  | (O)May be inoperative provided:     ] |

| *** System                |    |    |     a) Autopilot with altitude hold   |

|                           |    |    |        is operative, and              |

|                           |    |    |     b) Repair is made within three    |

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

| 18. Automatic Pressure    |    |    | DELETED in Revision 11c.            ] |

| *** Altitude Reporting    |    |    | Moved to Item 34-10.                ] |

|     Equipment System      |    |    |                                     ] |

|                           |    |    |                                       |

| 19. Flight Director     C | -  | -  | May be inoperative provided the       |

| *** Systems               |    |    | Flight Director is not required for   |

|                           |    |    | the approach to be flown.             |

|                           |    |    |                                       |

| 20. Radio Altimeter     C | -  | -  | Any in excess of those required by    |

| ***                       |    |    | FAR may be inoperative.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-5     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 21. Ground Proximity      |    |    |                                       |

| *** Warning System        |    |    |                                       |

|                           |    |    |                                       |

|      1) Modes 1 - 4     A | -  | 0  | (O)May be operative provided:         |

|                           |    |    |     a) Alternate procedures are       |

|                           |    |    |        established and used, and      |

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

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

|      2) Test Mode       A | 1  | 0  | May be inoperative provided:          |

|                           |    |    |     a) The GPWS is considered         |

|                           |    |    |        inoperative, and               |

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

|                           |    |    |        flight days.                   |

|                           |    |    |                                       |

|      3) Glideslope      B | 2  | 0  |                                       |

|         Deviation (Mode   |    |    |                                       |

|         5)                |    |    |                                       |

|                           |    |    |                                       |

| *** 4) Advisory         C | 1  | 0  | (O)May be inoperative provided        |

|        Callouts           |    |    | alternate procedures are              |

|                           |    |    | established and used.                 |

|                           |    |    |                                       |

| *** 5) Windshear Mode   C | 1  | 0  | (O)May be inoperative provided        |

|                           |    |    | alternate procedures are              |

|                           |    |    | established and used.                 |

|                           |    |    |                                       |

| *** 6) TAWS             C | 1  | 0  |                                     ] |

|                           |    |    |                                       |

| 22. Long Range          C | -  | 0  | Any in excess of those required by    |

| *** Navigation Systems    |    |    | FAR may be inoperative.               |

|     (VLF/Omega, INS,      |    |    |                                       |

|     Loran, etc.)          |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-6     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 23. Flight Management   C | -  | 0  |                                       |

| *** Systems (FMS)         |    |    |                                       |

|                           |    |    |                                       |

|      1) Radio Tuning    C | -  | 0  |                                       |

|         Unit              |    |    |                                       |

|                           |    |    |                                       |

|      2) Data Transfer   C | 1  | 0  |                                       |

|         Unit              |    |    |                                       |

|                           |    |    |                                       |

| 24. Individual EFIS       |    |    |                                       |

| *** Display Controller    |    |    |                                       |

|     Selection             |    |    |                                       |

|                           |    |    |                                       |

|      1) FULL/ARC Button C | 2  | 0  | May be inoperative provided           |

|                           |    |    | associated display is in Full.        |

|                           |    |    |                                       |

|      2) MAP Mode        C | 2  | 0  |                                       |

|                           |    |    |                                       |

|      3) Weather (WX)    C | 2  | 1  | One may be inoperative.               |

|                           |    |    |                                       |

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

|                           |    |    | Weather Radar is not required by      |

|                           |    |    | FAR.                                  |

|                           |    |    |                                       |

|      4) GS/TTG/ET       C | 2  | 0  |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|      5) MLS             C | -  | 0  | May be inoperative provided MLS is    |

|                           |    |    | not required for the approach to      |

|                           |    |    | flown.                                |

|                           |    |    |                                       |

|      6) V/L             C | 2  | 1  | One may be inoperative.               |

|                           |    |    |                                       |

|      7) FMS             C | 2  | 0  |                                       |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-7     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 24. Individual EFIS       |    |    |                                       |

| *** Display Controller    |    |    |                                       |

|     Selection (Cont'd)    |    |    |                                       |

|                           |    |    |                                       |

|      8) Bearing Pointer C | 4  | 3  |                                       |

|                           |    |    |                                       |

|      9) DH              C | 2  | 0  | May be inoperative provided DH is     |

|                           |    |    | not required for the approach to be   |

|                           |    |    | flown.                                |

|                           |    |    |                                       |

| 25. Traffic Alert       B | -  | 0  | (M)(O)May be inoperative provided:  ] |

| *** Collision Avoidance   |    |    |     a) System is deactivated and    ] |

|     System (TCAS II)      |    |    |        secured, and                 ] |

|                           |    |    |     b) Enroute or approach          ] |

|                           |    |    |        procedures do not require    ] |

|                           |    |    |        its use.                     ] |

|                           |    |    |                                       |

|                         C | -  | 0  | (M)(O)May be inoperative provided:  ] |

|                           |    |    |     a) Not required by FAR,         ] |

|                           |    |    |     b) System is deactivated and    ] |

|                           |    |    |        secured, and                 ] |

|                           |    |    |     c) Enroute or approach          ] |

|                           |    |    |        procedures do not require    ] |

|                           |    |    |        its use.                     ] |

|                           |    |    |                                       |

| *** 1) Combined Traffic C | 2  | 1  | May be inoperative on the           ] |

|        Alert (TA) and     |    |    | non-flying pilot side provided:     ] |

|        Resolution         |    |    |     a) TA and RA visual display is  ] |

|        Advisory (RA)      |    |    |        operative on flying pilot    ] |

|        Dual Displays      |    |    |        side, and                    ] |

|                           |    |    |     b) TA and RA audio function is  ] |

|                           |    |    |        operative on flying pilot    ] |

|                           |    |    |        side.                        ] |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-8     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25. Traffic Alert         |    |    |                                       |

| *** Collision Avoidance   |    |    |                                       |

|     System (TCAS II)      |    |    |                                       |

|     (Cont'd)              |    |    |                                       |

|                           |    |    |                                       |

|      2) Resolution      C | 2  | 1  | May be inoperative on non- flying   ] |

|         Advisory (RA)     |    |    | pilot side.                         ] |

|         Display           |    |    |                                       |

|         System(s)         |    |    |                                       |

|                           |    |    |                                       |

|                         C | -  | 0  | (O)May be inoperative provided:     ] |

|                           |    |    |     a) Traffic Alert (TA) visual    ] |

|                           |    |    |        display and audio functions  ] |

|                           |    |    |        are operative,               ] |

|                           |    |    |     b) TA only mode is selected by  ] |

|                           |    |    |        the crew, and                ] |

|                           |    |    |     c) Enroute or approach          ] |

|                           |    |    |        procedures do not require    ] |

|                           |    |    |        its use.                     ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-9     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25. Traffic Alert         |    |    |                                       |

| *** Collision Avoidance   |    |    |                                       |

|     System (TCAS)         |    |    |                                       |

|     (Cont'd)              |    |    |                                       |

|                           |    |    |                                       |

|      3) Traffic Alert   C | -  | 0  | (O)May be inoperative provided:     ] |

|         (TA) Display      |    |    |     a) RA visual display and audio  ] |

|         Systems(s)        |    |    |        functions are operative, and ] |

|                           |    |    |     b) Enroute or approach          ] |

|                           |    |    |        procedures do not require    ] |

|                           |    |    |        its use.                     ] |

|                           |    |    |                                       |

| 26. TACAN               D | -  | -  | May be inoperative provided TACAN     |

| ***                       |    |    | is not required for the approach to   |

|                           |    |    | be flown.                             |

|                           |    |    |                                       |

| 27. Radio Magnetic      C | -  | -  | May be inoperative provided both      |

|     Indicators (RMI)      |    |    | pilot's Primary Heading Indicators    |

|     and Bearing           |    |    | are operative.                        |

|     Distance Heading      |    |    |                                       |

|     Indicators (BDHI)     |    |    |                                       |

|                           |    |    |                                       |

| 28. Airspeed Indicator  D | -  | 0  |                                       |

| *** Speed Bugs            |    |    |                                       |

|     (External)            |    |    |                                       |

|                           |    |    |                                       |

| 29. Attitude System     D | -  | 2  | May be inoperative provided:          |

|     Sensors (Vertical     |    |    |     a) Both Pilot's Attitude          |

|     Gyro, AHRS, IRS,      |    |    |        Systems are operative from     |

|     etc.)                 |    |    |        independent sources, and       |

|                           |    |    |     b) Each pilot's panel has         |

|                           |    |    |        independent attitude           |

|                           |    |    |        information.                   |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-10    |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 30. Electronic Flight     |    |    |                                       |

| *** Information Systems   |    |    |                                       |

|     (EFIS)                |    |    |                                       |

|                           |    |    |                                       |

|      1) Multifunction   C | -  | 0  |                                       |

|         Display (MFD)     |    |    |                                       |

|                           |    |    |                                       |

| *** 2) Symbol Generator B | 3  | 2  | One may be inoperative.               |

|        (SG/MG)            |    |    |                                       |

|                           |    |    |                                       |

|      3) Single or Dual  C | 2  | 1  | May be inoperative provided display   |

|         Cue Selector      |    |    | is acceptable to the affected         |

|         Switch            |    |    | pilot.                                |

|                           |    |    |                                       |

| 31. Multifunction       C | 2  | 0  | (M)May be inoperative provided the    |

| *** Display Cooling       |    |    | associated Multifunction Display is ] |

|     Fans (EFIS)           |    |    | rendered inoperative.                 |

|                           |    |    |                                       |

| 32. Storm Scope and     C | -  | 0  |                                       |

| *** Lightning Detectors   |    |    |                                       |

|                           |    |    |                                       |

| 33. Individual MFD        |    |    |                                       |

| *** Display Controller    |    |    |                                     ] |

|     Selections            |    |    |                                       |

|                           |    |    |                                       |

|      1) Map/Plan        C | 1  | 0  | May be inoperative provided           |

|                           |    |    | affected mode is not required for     |

|                           |    |    | the anticipated flight.               |

|                           |    |    |                                       |

|      2) SRC             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|      3) WX              C | 1  | 0  |                                       |

|                           |    |    |                                       |

|      4) Norm/Emerg      C | 1  | 0  |                                       |

|                           |    |    |                                       |

|      5) Range Select    C | 1  | 0  |                                       |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-11    |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 33. Individual MFD        |    |    |                                       |

|     Display Controller    |    |    |                                       |

|     Selections (Cont'd)   |    |    |                                       |

|                           |    |    |                                       |

|      6) MFD             C | 1  | 0  |                                       |

|         Reversionary      |    |    |                                       |

|         Mode              |    |    |                                       |

|                           |    |    |                                       |

|      7) Joystick        C | 1  | 0  |                                       |

|                           |    |    |                                       |

|      8) VOR             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|      9) APT             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|     10) DAT             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|     11) RCL             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|     12) SKP             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|     13) PAG             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|     14) ENT             C | 1  | 0  |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 34-12    |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 34  NAVIGATION            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 34. EFIS Source           |    |    |                                       |

| *** Selectors             |    |    |                                     ] |

|                           |    |    |                                       |

|      1) HDG REV         B | 2  | 1  | One may be inoperative provided:      |

|                           |    |    |     a) Both pilots have independent   |

|                           |    |    |        sources for Heading            |

|                           |    |    |        Reference , and                |

|                           |    |    |     b) Affected Switch is not         |

|                           |    |    |        operated in flight.            |

|                           |    |    |                                       |

|      2) ATT REV         B | 2  | 1  | One may be inoperative provided:      |

|                           |    |    |     a) both pilots have independent   |

|                           |    |    |        sources for Attitude           |

|                           |    |    |        reference, and                 |

|                           |    |    |     b) Affected Switch is not         |

|                           |    |    |        operated in flight.            |

|                           |    |    |                                       |

| 35. Global Positioning  D | -  | 0  | May be inoperative provided         ] |

| *** System (GPS)          |    |    | procedures do not require its use.  ] |

|                           |    |    |                                       |

| 36. Windshear Detection C | -  | 0  | (O)May be inoperative provided      ] |

| *** and Guidance          |    |    | alternate procedures are            ] |

|     Systems               |    |    | established and used.               ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 c     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 08/21/2000      | 35-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 35  OXYGEN                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Passenger Oxygen    C | -  | 0  | May be inoperative when not           |

| *** System                |    |    | required by FAR.                      |

|                           |    |    |                                       |

| 2.  Protective          D | -  | -  | Any in excess of those required by  ] |

| *** Breathing Equipment   |    |    | FAR may be inoperative.             ] |

|     (PBE)                 |    |    |                                     ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 36-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 36  PNEUMATIC             |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Fire Wall Bleed     B | 2  | 0  | (M)Both may be inoperative            |

|     Valve                 |    |    | provided:                             |

|                           |    |    |     a) Valve(s) are positioned        |

|                           |    |    |        CLOSED after engine start,     |

|                           |    |    |        and                            |

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

|                           |    |    |        known or forecast icing        |

|                           |    |    |        conditions.                    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 b     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 10/01/1998      | 49-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 49  AIRBORNE AUXILIARY    |    |    |                                       |

|     POWER                 |    |    |                                       |

|                           |    |    |                                       |

| 1.  Gas Turbine         D | 1  | 0  | (M)May be inoperative provided:       |

| *** Compressor Unit       |    |    |     a) Procedures do not require      |

|     (GTC and GTCP)        |    |    |        its use, and                   |

|                           |    |    |     b) It is secured.                 |

|                           |    |    |                                       |

| 2.  Auxiliary Power     D | 1  | 0  | May be inoperative provided:          |

| *** Unit (APU)            |    |    |     a) Both engine driven AC          |

|                           |    |    |        Alternators are operative,     |

|                           |    |    |        and                            |

|                           |    |    |     b) APU is not required for        |

|                           |    |    |        Airborne Pneumatic power.      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 52-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 52  DOORS                 |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Cargo Door          C | 1  | 0  | (O)May be inoperative provided all    |

| ***                       |    |    | bayonets and hooks are verified       |

|                           |    |    | locked before each departure.         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 61-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 61  PROPELLERS            |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Synchronization     C | 1  | 0  |                                       |

|     Automatic Control     |    |    |                                       |

|     System (Aero          |    |    | NOTE:  May be operated with           |

|     products              |    |    |        hydraulic governors only.      |

|     A6441FN-606A          |    |    |                                       |

|     propellers)           |    |    |                                       |

|                           |    |    |                                       |

| 2.  DELETED               |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 3.  DELETED               |    |    | DELETED in Revision 9.                |

|                           |    |    |                                       |

| 4.  Synchrophaser         |    |    |                                       |

|     (Hamilton Standard    |    |    |                                       |

|     54H60-77 and -164     |    |    |                                       |

|     propellers)           |    |    |                                       |

|                           |    |    |                                       |

|     1) Synchrophaser    C | 1  | 0  |                                       |

|        Function           |    |    |                                       |

|                           |    |    |                                       |

|     2) Normal Governing C | 2  | 0  |                                       |

|        Function           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 72-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 72  ENGINE                |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Rear Turbine        B | 2  | 1  | (M)One may be missing provided the    |

|     Scavenge Pump         |    |    | turbine is inspected for              |

|     Insulator and Cone    |    |    | indications of vibration and          |

|                           |    |    | leakage.                              |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 73-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 73  ENGINE FUEL & CONTROL |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Fuel Flow Meters    B | 2  | 1  | One may be inoperative provided       |

|                           |    |    | Torque, TIT and all Fuel Quantity     |

|                           |    |    | Indicators are operative.             |

|                           |    |    |                                       |

| 2.  Temperature Datum   C | 2  | 0  | (O)May be inoperative provided AFM    |

|     System                |    |    | procedures are followed.              |

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| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11       | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 03/08/1994      | 76-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 76  ENGINE CONTROLS       |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Low Speed Ground    B | 2  | 0  |                                       |

|     Idle System (LSGI)    |    |    |                                       |

|                           |    |    |                                       |

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| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

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

| AIRCRAFT:                                | REVISION NO: 11 a     | PAGE:    |

| ALLSON CONVAIR 340/440 (CV-580, CV-5800) |                       |          |

|               (TURBO PROP)               | DATE: 09/26/1994      | 77-1     |

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

|                        1. | 2. NUMBER INSTALLED                             |

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

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

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

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

| 77  ENGINE INDICATING     |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 1.  Turbine Inlet       B | 2  | 1  | (M)One may be inoperative provided    |

| *** Temperature (TIT)     |    |    | analog indication is verified         |

|     Indicator Digital     |    |    | operative.                            |

|     Indication            |    |    |                                       |

|                           |    |    |                                       |

| 2.  Horsepower          B | 2  | 1  | (M)One may be inoperative provided    |

| *** Indicator Digital     |    |    | analog indication is verified         |

|     Indication            |    |    | operative.                            |

|                           |    |    |                                       |

| 3.  RPM Indicator       B | 2  | 1  | (M)One may be inoperative provided    |

| *** Digital Indication    |    |    | analog indication is verified         |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

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