DEPARTMENT OF TRANSPORTATION     Revision: 2

                                                           Date: 12/07/2000

                         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

 

 

 

 

 

                                  MARTIN M-404

 

 

 

 

 

 

 

 

 

 

 

 

 

                         Federal Aviation Administration

                         Flight Standards Division

                         AIRCRAFT EVALUATION GROUP, LGB-AEG

                         3960 PARAMOUNT BOULEVARD,

                         LAKEWOOD, CA   90712

 

                         TELEPHONE:  (562) 627-5272

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST      Date: 12/07/2000

 

                                MARTIN M-404

 

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I

         --     Log of Revisions                        II

         --     Control Page                            III, IV

         --     Highlights of Change                    V

         --     Definitions                             VI, VII, VIII, IX

         --     Definitions                             X, XI, XII, XIII

         --     Preamble                                XIV, XV

         21     Air Conditioning                        21-1, 2

         22     Auto Flight                             22-1

         23     Communications                          23-1, 2, 3

         24     Electrical Power                        24-1

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

         25     Equipment/Furnishings                   25-6, 7

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

         27     Flight Controls                         27-1

         28     Fuel                                    28-1

         29     Hydraulic Power                         29-1

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

         31     Indicating/Recording Systems            31-1

         32     Landing Gear                            32-1

         33     Lights                                  33-1, 2, 3, 4

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

         34     Navigation                              34-6

         35     Oxygen                                  35-1

         49     Airborne Auxiliary Power                49-1

         52     Doors                                   52-1

         61     Propellers                              61-1

         73     Engine Fuel & Control                   73-1

         77     Engine Indicating                       77-1, 2

         79     Engine Oil                              79-1

         82     Water Injection                         82-1


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: II

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 12/07/2000

 

                                MARTIN M-404

 

 

 

                               Log of Revisions

 

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                       FEDERAL AVIATION ADMINISTRATION     Page: III

                                                           Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST      Date: 12/07/2000

 

                                MARTIN M-404

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       2        12/07/2000

         Table of Contents                        I       2        12/07/2000

         Log of Revisions                         II      2        12/07/2000

         Control Page                             III     2        12/07/2000

                                                  IV      2        12/07/2000

         Highlights of Change                     V       2        12/07/2000

         Definitions                              VI      6        01/31/1995

                                                  VII     6        01/31/1995

                                                  VIII    6        01/31/1995

                                                  IX      6        01/31/1995

                                                  X       6        01/31/1995

                                                  XI      6        01/31/1995

                                                  XII     6        01/31/1995

                                                  XIII    6        01/31/1995

         Preamble                                 XIV     2        06/14/1989

                                                  XV      2        06/14/1989

         21                                       21-1    2        12/07/2000

                                                  21-2    2        12/07/2000

         22                                       22-1    2        12/07/2000

         23                                       23-1    2        12/07/2000

                                                  23-2    2        12/07/2000

                                                  23-3    2        12/07/2000

         24                                       24-1    2        12/07/2000

         25                                       25-1    2        12/07/2000

                                                  25-2    2        12/07/2000

                                                  25-3    2        12/07/2000

                                                  25-4    2        12/07/2000

                                                  25-5    2        12/07/2000

                                                  25-6    2        12/07/2000

                                                  25-7    2        12/07/2000

         26                                       26-1    2        12/07/2000

                                                  26-2    2        12/07/2000

                                                  26-3    2        12/07/2000

                                                  26-4    2        12/07/2000

         27                                       27-1    2        12/07/2000

         28                                       28-1    2        12/07/2000

         29                                       29-1    2        12/07/2000

         30                                       30-1    2        12/07/2000

                                                  30-2    2        12/07/2000

                                                  30-3    2        12/07/2000


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IV

                                                           Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST      Date: 12/07/2000

 

                                MARTIN M-404

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         31                                       31-1    2        12/07/2000

         32                                       32-1    2        12/07/2000

         33                                       33-1    2        12/07/2000

                                                  33-2    2        12/07/2000

                                                  33-3    2        12/07/2000

                                                  33-4    2        12/07/2000

         34                                       34-1    2        12/07/2000

                                                  34-2    2        12/07/2000

                                                  34-3    2        12/07/2000

                                                  34-4    2        12/07/2000

                                                  34-5    2        12/07/2000

                                                  34-6    2        12/07/2000

         35                                       35-1    2        12/07/2000

         49                                       49-1    2        12/07/2000

         52                                       52-1    2        12/07/2000

         61                                       61-1    2        12/07/2000

         73                                       73-1    2        12/07/2000

         77                                       77-1    2        12/07/2000

                                                  77-2    2        12/07/2000

         79                                       79-1    2        12/07/2000

         82                                       82-1    2        12/07/2000


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: V

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 12/07/2000

 

                                MARTIN M-404

 

 

                            Highlights of Change

 

 

 

       Effective above date, the Martin M-404 Master Minimum Equipment List

       (MMEL) is revised.  This is a complete revision, which is a result of

       an internal Federal Aviation Administration (FAA) review. Several

       new items are given relief in this revision. Current FAA MMEL

       Policy Letters are incorporated into this revision.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

       1.   System Definitions.

 

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

       Specification Number 100 and items are numbered sequentially.

 

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

                      component, or function listed in the "Item"

                      column.

 

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

                      (quantity) of items normally installed in the

                      aircraft.  This number represents the aircraft

                      configuration considered in developing this MMEL.

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

                      cabin items) a number is not required.

                                                                            ¦

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

                      minimum number (quantity) of items required for

                      operation provided the conditions specified in

                      Column 4 are met.

 

       NOTE:  Where the MMEL shows a variable number required for

       dispatch, the MEL must reflect the actual number required for

       dispatch or an alternate means of configuration control approved

       by the Administrator.

 

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

                      includes a statement either prohibiting or

                      permitting operation with a specific number of

                      items inoperative, provisos (conditions and

                      limitations) for such operation, and appropriate

                      notes.

 

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

                      indicates a change, addition or deletion in the

                      adjacent text for the current revision of that

                      page only.  The change bar is dropped at the next

                      revision of that page.

 

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

       required for type certification and approved by the responsible

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

       the specific aircraft is listed on the applicable Type


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

       Certificate Data Sheet.

 

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

       certain provisions (restrictive or permissive) expressed in the

       Federal Aviation Regulations operating rules.  The number of

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

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

       specified by repair category.

 

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

       the crewmembers and maintenance personnel of the equipment

       condition.

 

       NOTE:  To the extent practical, placards should be located

       adjacent to the control or indicator for the item affected;

       however, unless otherwise specified, placard wording and location

       will be determined by the operator.

 

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

       number (quantity) of the item installed.

                                                                           ¦

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

       indicates that the item was previously listed but is now required

       to be operative if installed in the  aircraft.

 

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

       airplane which has a type design approval for ER operations and

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

 

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

       portions of the Federal Aviation Act and Federal Aviation

       Regulations.

 

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

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

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

       is initiated for the affected aircraft.

 

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

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

 

       11.  Alphabetical symbol in Column 4 indicates a proviso

       (condition or limitation) that must be complied with for


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

       operation with the  listed item inoperative.

 

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

       the extent that it does not accomplish its intended purpose

       and/or is not consistently functioning normally within its

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

 

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

       crewmember or maintenance consideration.  Notes are used to

       identify applicable material which is intended to assist with

       compliance, but do not relieve the operator of the responsibility

       for compliance with all applicable requirements.  Notes are not a

       part of the provisos.

 

       14.  Inoperative components of an inoperative system:

       Inoperative items which are components of a system which is

       inoperative are usually considered components directly associated

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

       (Warning/caution systems associated with the inoperative system

       must be operative unless relief is specifically authorized per

       the MMEL).

 

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

       maintenance procedure which must be accomplished prior to

       operation with the listed item inoperative.  Normally these

       procedures are accomplished by maintenance personnel;  however,

       other personnel may be qualified and authorized to perform

       certain functions.  Procedures requiring specialized knowledge or

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

       accomplished by maintenance personnel.  The satisfactory

       accomplishment of all maintenance procedures, regardless of

       who performs them, is the responsibility of the operator.

       Appropriate procedures are required to be published as part of

       the operator's manual or MEL.

 

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

       operations procedure which must be accomplished in planning for

       and/or operating with the listed item inoperative.  Normally

       these procedures are accomplished by the flight crew; however,

       other personnel may be qualified and authorized to perform

       certain functions.  The satisfactory accomplishment of all

       procedures, regardless of who performs them, is the

       responsibility of the operator.  Appropriate procedures are


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

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

       MEL.

 

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

       unless otherwise authorized by the Administrator.

 

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

       component must be put into an acceptable condition for safe

       flight.  An acceptable method of securing or deactivating will be

       established by the operator.

 

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

       This precludes a pilot from filing an Instrument Flight Rules

       (IFR) flight plan.

 

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

       atmospheric environment is such that would allow a flight to

       proceed under the visual flight rules applicable to the flight.

       This does not preclude operating under Instrument Flight Rules.

 

       20.  "Visible Moisture" means an atmospheric environment

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

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

       snow.

 

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

       passenger convenience, comfort or entertainment such as, but not

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

       equipment, overhead reading lamps, etc.

 

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

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

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

       to the repair times established by the following letter

       designators:

 

            Category A.  Items in this category shall be repaired within

       the time interval specified in the remarks column of the

       operator's approved MEL.

 

            Category B.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: X

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

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

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

       26th and end at midnight the 29th.

 

            Category C.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance

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

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

       26th and end at midnight February 5th.

 

            Category D.  Items in this category shall be repaired within

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

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

       aircraft maintenance log and/or record.

 

       The letter designators are inserted adjacent to Column 2.

 

       23. Electronic fault alerting system - General                  ¦

                                                                       ¦

       New generation aircraft display system fault indications to the ¦

       flight crew by use of computerized display systems.  Each       ¦

       aircraft manufacturer has incorporated individual design        ¦

       philosophies in determining the data that would be              ¦

       represented.  The following are customized definitions (specific¦

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

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

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

       23 for their aircraft, if appropriate.                          ¦

                                                                       ¦

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

                                                                       ¦

       Boeing airplanes equipped with Engine Indicating and Crew       ¦

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

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

       MAINTENANCE).  Any messages that affects airplane dispatch      ¦

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

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

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

       operating within its approved operating limits or tolerances.   ¦

                                                                       ¦

       System conditions that result only in a maintenance level       ¦

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


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

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

       addressed within an operators standard maintenance program.     ¦

                                                                       ¦

       b.   DOUGLAS  (MD-11)                                           ¦

                                                                       ¦

       Some Douglas aircraft are equipped with an alerting function    ¦

       which is a subsystem within the Electronic Instrument System    ¦

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

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

       STATUS).                                                        ¦

                                                                       ¦

       Alerts that affect aircraft dispatch will include WARNING,      ¦

       CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are   ¦

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

       maintenance heading.                                            ¦

                                                                       ¦

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

       system fault which can be identified by the Central Fault       ¦

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

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

       MEL must be verified for dispatch purposes.                     ¦

                                                                       ¦

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

                                                                       ¦

       Airbus aircraft equipped with Electronic Centralized Aircraft   ¦

       Monitoring (ECAM) provide different levels of system condition  ¦

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

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

                                                                       ¦

       Any message that effects airplane dispatchability will normally ¦

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

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

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

                                                                       ¦

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

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

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

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

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

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

       MAINTENANCE status messages do not affect dispatch.             ¦

 

       d.   FOKKER  (FK-100)                                           ¦


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

                                                                       ¦

       Fokker aircraft are equipped with Multi Function Display System ¦

       (MFDS) which provides electronic message referring to the       ¦

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

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

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

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

       verified for dispatch capability and maintenance may be         ¦

       required.                                                       ¦

                                                                       ¦

       System conditions that only require maintenance are not         ¦

       presented on the flight deck.  These maintenance                ¦

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

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

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

 

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

       operator in the MEL for tracking and informational purposes.  It

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

       Operations Inspector provided no relief is granted, or provided

       conditions and limitations are contained in an approved document

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

       If relief other than that granted by an approved document is

       sought for an administrative control item, a request must be

       submitted to the Administrator.  If the request results in review

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

       than an administrative control item.

 

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

       required by regulation but which may have been installed on some

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

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

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

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

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

       this policy nor the use of this symbol provide authority to

       install or remove an item from an aircraft.

 

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

       that are redundant to the requirements of the FARs.

 

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

       equipment/instrument malfunction was recorded in the aircraft


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                MARTIN M-404

 

 

                                 Definitions

 

 

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

       calendar days or flight days specified in the MMEL for the

       repair of an inoperative item of equipment. This provision is

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

       D."

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XIV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                                MARTIN M-404

 

 

                                  Preamble

                            (Effective 6/14/89)

 

       The following is applicable for authorized certificate holders operating

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

       FAR require that all equipment installed on an aircraft in compliance

       with the Airworthiness Standards and the Operating Rules must be

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

       Equipment List (MEL) where compliance with certain equipment

       requirements is not necessary in the interests of safety under all

       operating conditions.  Experience has shown that with the various levels

       of redundancy designed into aircraft, operation of every system or

       installed component may not be necessary when the remaining operative

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

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

       aviation industry, to improve aircraft utilization and thereby provide

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

       approved MMEL includes those items of equipment related to airworthiness

       and operating regulations and other items of equipment which the

       Administrator finds may be inoperative and yet maintain an acceptable

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

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

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

       into consideration the operator's particular aircraft equipment

       configuration and operational conditions. Operator MELs, for

       administrative control, may include items not contained in the

       MMEL;  however, relief for administrative control items must be

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

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

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

       operation of the aircraft with inoperative equipment.

 

       Equipment not required by the operation being conducted and equipment in

       excess of FAR requirements are included in the MEL with appropriate

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

       Flight Manual Limitations, Emergency Procedures or with Airworthiness

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

       the airworthiness and the operating regulations of the aircraft not

       listed on the MMEL must be operative.

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                                MARTIN M-404

 

 

                                  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: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 21-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Pressurization        ¦    ¦    ¦     a) Aircraft is operated in an   | ¦

¦     System                ¦    ¦    ¦        accepted unpressurized       | ¦

¦                           ¦    ¦    ¦        configuration, and           | ¦

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

¦                           ¦    ¦    ¦        below 10,000 feet MSL.       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Cabin               C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     Pressurization        ¦    ¦    ¦ aircraft is operated unpressurized. | ¦

¦     Control System        ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Differential          ¦    ¦    ¦ aircraft is operated unpressurized. | ¦

¦     Pressure Indicator    ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Cabin Differential    ¦    ¦    ¦ Combined with item 3.               | ¦

¦     Pressure Indicator    ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     System                ¦    ¦    ¦ aircraft is operated unpressurized. | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Cabin Supercharger  C ¦ 1  ¦ 0  ¦ May be inoperative provided Cabin   | ¦

¦     (S/C)                 ¦    ¦    ¦ Pressurization System is considered | ¦

¦                           ¦    ¦    ¦ inoperative.                        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  S/C Power           C ¦ 1  ¦ 0  ¦ May be inoperative provided Cabin   | ¦

¦     Indicating System     ¦    ¦    ¦ Supercharger is considered          | ¦

¦                           ¦    ¦    ¦ inoperative.                        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  S/C Oil Temperature C ¦ 1  ¦ 0  ¦ May be inoperative provided S/C is  | ¦

¦     Indicating System     ¦    ¦    ¦ considered inoperative.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 21-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  S/C Oil Pressure    C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦

¦     Indicating System     ¦    ¦    ¦     a) S/C Oil Temperature          | ¦

¦                           ¦    ¦    ¦        Indicating System is         | ¦

¦                           ¦    ¦    ¦        operative, and               | ¦

¦                           ¦    ¦    ¦     b) S/C Oil Pressure Warning     | ¦

¦                           ¦    ¦    ¦        Light System is installed    | ¦

¦                           ¦    ¦    ¦        and operative.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided the S/C | ¦

¦                           ¦    ¦    ¦ is considered inoperative.          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. S/C Oil Pressure    C ¦ 1  ¦ 0  ¦ May be inoperative provided the S/C | ¦

¦     Warning Light         ¦    ¦    ¦ Oil Pressure Indicating System is   | ¦

¦     System                ¦    ¦    ¦ operative.                          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided the S/C | ¦

¦                           ¦    ¦    ¦ is considered inoperative.          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Cabin Heating       C ¦ 2  ¦ 1  ¦                                     | ¦

¦     System                ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Temperature Control   ¦    ¦    ¦                                     | ¦

¦     System                ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ Temperature remains above 50 F.     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         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.              | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Vent Fan            C ¦ 2  ¦ 1  ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Cabin Cooling       C ¦ 1  ¦ 0  ¦                                     | ¦

¦     System                ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 22-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Aircraft with only  B ¦ 1  ¦ 0  ¦                                     | ¦

¦ *** one Autopilot         ¦    ¦    ¦                                     | ¦

¦     System installed      ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ *** Aircraft with two   C ¦ 1  ¦ 0  ¦                                     | ¦

¦     or more Autopilot     ¦    ¦    ¦                                     | ¦

¦     Systems installed   B ¦ -  ¦ 0  ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Autopilot           C ¦ 2  ¦ 1  ¦ One may be inoperative provided:    | ¦

¦ *** Disconnect Switch     ¦    ¦    ¦     a) With Autopilot engaged, the  | ¦

¦     (Control Wheel        ¦    ¦    ¦        pilot controlling the        | ¦

¦     Button)               ¦    ¦    ¦        airplane has an operative    | ¦

¦                           ¦    ¦    ¦        Disconnect Switch on his     | ¦

¦                           ¦    ¦    ¦        control wheel, and           | ¦

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

¦                           ¦    ¦    ¦        1500 feet AGL.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 23-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  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.       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Passenger Address     ¦    ¦    ¦                                     | ¦

¦     System                ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

¦                           ¦    ¦    ¦        operative,                   | ¦

¦                           ¦    ¦    ¦     b) Alternate, Normal and        | ¦

¦                           ¦    ¦    ¦        Emergency procedures are     | ¦

¦                           ¦    ¦    ¦        established and used.        | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Configuration     ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Cabin Interphone      ¦    ¦    ¦                                     | ¦

¦     System                ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Configuration     ¦    ¦    ¦     a) Public Address (PA) System   | ¦

¦                           ¦    ¦    ¦        is operative, and            | ¦

¦                           ¦    ¦    ¦     b) Procedures do not required   | ¦

¦                           ¦    ¦    ¦        use of the Cabin Interphone  | ¦

¦                           ¦    ¦    ¦        System.                      | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Configuration     ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Speaker (Cockpit)   C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative          | ¦

¦ ***                       ¦    ¦    ¦ provided:                           | ¦

¦                           ¦    ¦    ¦     a) An operative headset is      | ¦

¦                           ¦    ¦    ¦        available for each person on | ¦

¦                           ¦    ¦    ¦        flight deck duty, and        | ¦

¦                           ¦    ¦    ¦     b) Affected Speaker is not      | ¦

¦                           ¦    ¦    ¦        required for aural warning.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 23-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Cockpit Microphones   ¦    ¦    ¦                                     | ¦

¦ *** (Boom and Handheld)   ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Microphones       ¦    ¦    ¦ associated Boom Microphone is       | ¦

¦                           ¦    ¦    ¦ operative.                          | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦      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.      | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Chime System        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦

¦ ***                       ¦    ¦    ¦     a) PA System is operative, and  | ¦

¦                           ¦    ¦    ¦     b) Alternate, Normal and        | ¦

¦                           ¦    ¦    ¦        Emergency procedures are     | ¦

¦                           ¦    ¦    ¦        established and used.        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 23-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Handset (Cabin)     C ¦ -  ¦ -  ¦ May be inoperative provided one is  | ¦

¦ ***                       ¦    ¦    ¦ operative at each required Flight   | ¦

¦                           ¦    ¦    ¦ Attendant Station.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  ARINC               C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦

¦ *** Communications/       ¦    ¦    ¦     a) Affected System is           | ¦

¦     Addressing and        ¦    ¦    ¦        appropriately secured, and   | ¦

¦     Reporting System      ¦    ¦    ¦     b) Alternate operations         | ¦

¦     (ACARS)               ¦    ¦    ¦        procedures are established   | ¦

¦                           ¦    ¦    ¦        and used.                    | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ *** Recorder (CVR)        ¦    ¦    ¦     a) Flight data recorder is      | ¦

¦                           ¦    ¦    ¦        operative, and               | ¦

¦                           ¦    ¦    ¦     b) Repairs are made within      | ¦

¦                           ¦    ¦    ¦        three flight days.           | ¦

¦                           ¦    ¦    ¦                                       ¦

¦        a) CVR without   A ¦ 1  ¦ 0  ¦ May be inoperative provided repairs | ¦

¦           FDR installed   ¦    ¦    ¦ are made within three flight days.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 24-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Main Inverter       C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided: | ¦

¦                           ¦    ¦    ¦     a) Airplane is operated in Day  | ¦

¦                           ¦    ¦    ¦        VMC only, and                | ¦

¦                           ¦    ¦    ¦     b) Affected Inverter is secured | ¦

¦                           ¦    ¦    ¦        using an accepted procedure. | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Inverter Failure    C ¦ 2  ¦ 1  ¦ One may be inoperative provided AC  | ¦

¦ *** Warning Light         ¦    ¦    ¦ Instrument Power Failure Indication | ¦

¦     System                ¦    ¦    ¦ is installed and operative.         | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ Associated Main Inverter is         | ¦

¦                           ¦    ¦    ¦ considered inoperative.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Alternators         C ¦ 2  ¦ 1  ¦ One may be inoperative in Day VMC   | ¦

¦ *** Instrument            ¦    ¦    ¦ only.                               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  AC Instrument       C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦ *** Power Failure         ¦    ¦    ¦ aircraft is operated in Day VMC     | ¦

¦     Indication System     ¦    ¦    ¦ only.                               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 25-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  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 Position(s) is | ¦

¦                           ¦    ¦    ¦        not occupied,                | ¦

¦                           ¦    ¦    ¦     b) Flight Attendants displaced  | ¦

¦                           ¦    ¦    ¦        by inoperative seat          | ¦

¦                           ¦    ¦    ¦        position(s) occupies the     | ¦

¦                           ¦    ¦    ¦        Passenger Seat(s) most       | ¦

¦                           ¦    ¦    ¦        accessible to their assigned | ¦

¦                           ¦    ¦    ¦        exit,                        | ¦

¦                           ¦    ¦    ¦     c) Alternate operations         | ¦

¦                           ¦    ¦    ¦        procedures are established   | ¦

¦                           ¦    ¦    ¦        for displaced Flight         | ¦

¦                           ¦    ¦    ¦        Attendant(s),                | ¦

¦                           ¦    ¦    ¦     d) Folding type seat that will  | ¦

¦                           ¦    ¦    ¦        not stow automatically is    | ¦

¦                           ¦    ¦    ¦        stowed or secured in the     | ¦

¦                           ¦    ¦    ¦        RETRACTED position, and      | ¦

¦                           ¦    ¦    ¦     e) Passenger Seat(s) assigned   | ¦

¦                           ¦    ¦    ¦        to Flight Attendant(s) is    | ¦

¦                           ¦    ¦    ¦        placarded "FOR FLIGHT        | ¦

¦                           ¦    ¦    ¦        ATTENDANT USE ONLY".         | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 25-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Flight Attendant      ¦    ¦    ¦                                     | ¦

¦     Seats (Single or      ¦    ¦    ¦                                     | ¦

¦     Dual Position)        ¦    ¦    ¦                                     | ¦

¦     (Cont'd)              ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ *** 2) Seats In Excess  C ¦ -  ¦ -  ¦ (M)(O)May be inoperative provided:  | ¦

¦        of Those           ¦    ¦    ¦     a) Affected Seat Position(s) is | ¦

¦        Required By FAR    ¦    ¦    ¦        not occupied, and            | ¦

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

¦                           ¦    ¦    ¦        not stow automatically is    | ¦

¦                           ¦    ¦    ¦        stowed or secured in the     | ¦

¦                           ¦    ¦    ¦        RETRACTED position.          | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦ NOTE 1:  An automatic folding seat  | ¦

¦                           ¦    ¦    ¦          that will not stow         | ¦

¦                           ¦    ¦    ¦          automatically is           | ¦

¦                           ¦    ¦    ¦          considered inoperative.    | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦ NOTE 2:  A seat position with an    | ¦

¦                           ¦    ¦    ¦          inoperative or missing lap | ¦

¦                           ¦    ¦    ¦          belt is considered         | ¦

¦                           ¦    ¦    ¦          inoperative.               | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 3:  Individual Operators, when | ¦

¦                           ¦    ¦    ¦          operating with inoperative | ¦

¦                           ¦    ¦    ¦          seats, will consider the   | ¦

¦                           ¦    ¦    ¦          locations and combinations | ¦

¦                           ¦    ¦    ¦          of seats to ensure that    | ¦

¦                           ¦    ¦    ¦          the proximity to exits and | ¦

¦                           ¦    ¦    ¦          distribution requirements  | ¦

¦                           ¦    ¦    ¦          of the applicable FAR are  | ¦

¦                           ¦    ¦    ¦          met.                       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 25-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Passenger Seats     D ¦ -  ¦ -  ¦ May be inoperative provided:        | ¦

¦                           ¦    ¦    ¦     a) Seat does not block an       | ¦

¦                           ¦    ¦    ¦        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 | ¦

¦                           ¦    ¦    ¦          seat belt is considered    | ¦

¦                           ¦    ¦    ¦          inoperative.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 2:  Inoperative seats 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: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 25-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Crewmember Shoulder C ¦ -  ¦ -  ¦ May be inoperative provided         | ¦

¦ *** Harness               ¦    ¦    ¦ associated seat position is         | ¦

¦                           ¦    ¦    ¦ considered inoperative.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Flotation Equipment C ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

¦     (Crew and             ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦     Passenger)            ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Transmitter (ELT)     ¦    ¦    ¦     a) Affected ELT is deactivated  | ¦

¦                           ¦    ¦    ¦        or removed using accepted    | ¦

¦                           ¦    ¦    ¦        procedures, and              | ¦

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

¦                           ¦    ¦    ¦        time limits.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

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

¦                           ¦    ¦    ¦ from each occupied passenger seat.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Cabin Emergency     C ¦ -  ¦ -  ¦ May be inoperative provided         | ¦

¦     Flashlight and        ¦    ¦    ¦ crewmember assigned to the          | ¦

¦     Holder (Flight        ¦    ¦    ¦ associated position has an          | ¦

¦     Attendant Position)   ¦    ¦    ¦ operative flashlight readily        | ¦

¦                           ¦    ¦    ¦ available.                          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 25-5     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Megaphones            ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Configuration     ¦    ¦    ¦ by FAR may be inoperative provided: | ¦

¦                           ¦    ¦    ¦     a) The inoperative megaphone is | ¦

¦                           ¦    ¦    ¦        removed from the passenger   | ¦

¦                           ¦    ¦    ¦        cabin, and                   | ¦

¦                           ¦    ¦    ¦     b) Required Distribution is     | ¦

¦                           ¦    ¦    ¦        maintained.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦        Configuration      ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Passenger             ¦ -  ¦ -  ¦ Passenger Convenience Items, as     | ¦

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

¦     (Passenger and        ¦    ¦    ¦ related to passenger convenience,   | ¦

¦     Cargo Aircraft)       ¦    ¦    ¦ 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.  (M) and (O)       | ¦

¦                           ¦    ¦    ¦ procedures may be required and      | ¦

¦                           ¦    ¦    ¦ included in the air carrier's       | ¦

¦                           ¦    ¦    ¦ appropriate document.               | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦ NOTE:   Lavatory Ash Trays are not  | ¦

¦                           ¦    ¦    ¦        to be included.              | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. 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.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 25-6     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. First Aid Kit       D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

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

¦                           ¦    ¦    ¦ provided required distribution is   | ¦

¦                           ¦    ¦    ¦ maintained.                         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. 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          ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. 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: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 25-7     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. 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, 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.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 26-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  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.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Fire Extinguisher   C ¦ 2  ¦ 0  ¦ (M)May be missing provided          | ¦

¦ *** Bottle Thermal        ¦    ¦    ¦ associated bottle charge is         | ¦

¦     Discharge Indicator   ¦    ¦    ¦ verified by an accepted maintenance | ¦

¦     Disks                 ¦    ¦    ¦ procedure (such as weighing or      | ¦

¦                           ¦    ¦    ¦ gauge reading) once each flight     | ¦

¦                           ¦    ¦    ¦ day.                                | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 26-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Lavatory Smoke      C ¦ -  ¦ -  ¦ For each lavatory, the Lavatory     | ¦

¦     Detection Systems     ¦    ¦    ¦ Smoke Detection System may be       | ¦

¦                           ¦    ¦    ¦ inoperative provided Lavatory Fire  | ¦

¦                           ¦    ¦    ¦ Extinguisher System is operative.   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the        | ¦

¦                           ¦    ¦    ¦ 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: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 26-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  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)For each lavatory, the        | ¦

¦                           ¦    ¦    ¦ Lavatory Fire Extinguisher 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 Fire Extinguisher | ¦

¦                           ¦    ¦    ¦          Systems are not required   | ¦

¦                           ¦    ¦    ¦          for all-cargo operations.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 26-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Cargo Compartment   C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦

¦ *** Fire Detection/       ¦    ¦    ¦ associated cargo compartment        | ¦

¦     Suppression Systems   ¦    ¦    ¦ remains empty.                      | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 1:  Does not preclude the      | ¦

¦                           ¦    ¦    ¦          carriage of empty cargo    | ¦

¦                           ¦    ¦    ¦          containers, pallets,       | ¦

¦                           ¦    ¦    ¦          ballast, etc.              | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 2:  Class E cargo compartments | ¦

¦                           ¦    ¦    ¦          require only the           | ¦

¦                           ¦    ¦    ¦          installation of smoke or   | ¦

¦                           ¦    ¦    ¦          fire detection systems     | ¦

¦                           ¦    ¦    ¦          (not suppression).         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 27-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ *** Indicating System     ¦    ¦    ¦ procedures are established to       | ¦

¦     (Dual Needle)         ¦    ¦    ¦ visually check flap position before | ¦

¦                           ¦    ¦    ¦ each takeoff after setting takeoff  | ¦

¦                           ¦    ¦    ¦ flaps.                              | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 28-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Under Wing Fuel     C ¦ 4  ¦ 0  ¦ (O)May be inoperative provided:     | ¦

¦ *** Quantity Indicating   ¦    ¦    ¦     a) Fuel Quantity Indicating     | ¦

¦     System                ¦    ¦    ¦        System (Cockpit) for         | ¦

¦                           ¦    ¦    ¦        associated tank is           | ¦

¦                           ¦    ¦    ¦        operative, and               | ¦

¦                           ¦    ¦    ¦     b) Alternate refueling          | ¦

¦                           ¦    ¦    ¦        procedures are established   | ¦

¦                           ¦    ¦    ¦        and used.                    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Cockpit Fuel        C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided  | ¦

¦     Quantity Indicating   ¦    ¦    ¦ fuel quantity in the associated     | ¦

¦     System                ¦    ¦    ¦ tank is determined by an accepted   | ¦

¦                           ¦    ¦    ¦ means before each departure.        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 29-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Main System         C ¦ 2  ¦ 1  ¦     Either the 1500 pound or the    | ¦

¦     Pressure Indicator    ¦    ¦    ¦     3000 pound pressure indicator   | ¦

¦     (Cockpit)             ¦    ¦    ¦     must be operating on the normal | ¦

¦                           ¦    ¦    ¦     system.                         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Electric Pump       C ¦ 1  ¦ 0  ¦     May be inoperative              | ¦

¦ ***                       ¦    ¦    ¦     a) Crew is advised that the     | ¦

¦                           ¦    ¦    ¦        rear pump must be operated   | ¦

¦                           ¦    ¦    ¦        by hand pump, and            | ¦

¦                           ¦    ¦    ¦     b) It is not required by FAR.   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 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.  Wing And Tail       B ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     Anti-Ice System       ¦    ¦    ¦ aircraft is not operated into known | ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Heaters - Thermal   C ¦ 4  ¦ 0  ¦ May be inoperative provided         | ¦

¦ *** Deicing               ¦    ¦    ¦ aircraft not operated in icing      | ¦

¦                           ¦    ¦    ¦ conditions.                         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Propeller Deicing   C ¦ 2  ¦ 0  ¦ May be inoperative provided         | ¦

¦     System                ¦    ¦    ¦ aircraft is not operated into known | ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Windshield Heating    ¦    ¦    ¦                                     | ¦

¦ *** System (NESA          ¦    ¦    ¦                                     | ¦

¦     Panels)               ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      1) Main Panels     C ¦ 2  ¦ 1  ¦ One may be inoperative provided the | ¦

¦         (Pilot's and      ¦    ¦    ¦ pilot's side is operative.          | ¦

¦         Copilot's)        ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ aircraft is not operated in known   | ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) Direct Vision   C ¦ 2  ¦ 1  ¦ One may be inoperative provided     | ¦

¦         (DV) Panels       ¦    ¦    ¦ both Main Panels are operative.     | ¦

¦         (Pilot's and      ¦    ¦    ¦                                     | ¦

¦         Co-Pilot's)       ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ aircraft is not operated in known   | ¦

¦                           ¦    ¦    ¦ or forecast icing conditions.       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 30-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Pitot Heater System C ¦ 2  ¦ 1  ¦ One may be inoperative provided:    | ¦

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

¦                           ¦    ¦    ¦        visible moisture with the    | ¦

¦                           ¦    ¦    ¦        static air temperature (SAT) | ¦

¦                           ¦    ¦    ¦        below +4 Degrees C,          | ¦

¦                           ¦    ¦    ¦     b) Aircraft is not operated     | ¦

¦                           ¦    ¦    ¦        into known or forecast icing | ¦

¦                           ¦    ¦    ¦        conditions,                  | ¦

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

¦                           ¦    ¦    ¦        Conditions only, and         | ¦

¦                           ¦    ¦    ¦     d) Associated pitot heater      | ¦

¦                           ¦    ¦    ¦        switch remains OFF.          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Static Port Heater  C ¦ 4  ¦ 3  ¦ One may be inoperative provided:    | ¦

¦ *** System (For           ¦    ¦    ¦     a) Aircraft is not operated in  | ¦

¦     Airspeed)             ¦    ¦    ¦        visible moisture with the    | ¦

¦                           ¦    ¦    ¦        static air temperature (SAT) | ¦

¦                           ¦    ¦    ¦        below +4 Degrees C,          | ¦

¦                           ¦    ¦    ¦     b) Aircraft is not operated     | ¦

¦                           ¦    ¦    ¦        into known or forecast icing | ¦

¦                           ¦    ¦    ¦        conditions, and              | ¦

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

¦                           ¦    ¦    ¦        Conditions only.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Windshield Wiper    C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     System                ¦    ¦    ¦ aircraft is not operated in         | ¦

¦                           ¦    ¦    ¦ precipitation within 5 miles of the | ¦

¦                           ¦    ¦    ¦ airport of takeoff of intended      | ¦

¦                           ¦    ¦    ¦ landing.                            | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Carburetor Alcohol  C ¦ 2  ¦ 0  ¦ May be inoperative provided         | ¦

¦ *** System                ¦    ¦    ¦ carburetor heat available and       | ¦

¦                           ¦    ¦    ¦ Temperature Indicator is operative. | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 30-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Pitot Heater        B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦

¦ *** Inoperative           ¦    ¦    ¦     a) All other Pitot Heat System  | ¦

¦     Indicating System     ¦    ¦    ¦        Components are verified      | ¦

¦                           ¦    ¦    ¦        operative using an accepted  | ¦

¦                           ¦    ¦    ¦        procedure before each        | ¦

¦                           ¦    ¦    ¦        departure,                   | ¦

¦                           ¦    ¦    ¦     b) Pitot Heater Loadmeter is    | ¦

¦                           ¦    ¦    ¦        operative, and               | ¦

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

¦                           ¦    ¦    ¦        known or forecast icing      | ¦

¦                           ¦    ¦    ¦        conditions.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ associated Pitot Heat System is     | ¦

¦                           ¦    ¦    ¦ considered inoperative.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 31-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦

¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Clocks (Cockpit)    C ¦ -  ¦ 1  ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Flight Data         A ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦

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

¦     System                ¦    ¦    ¦        is operative, and            | ¦

¦                           ¦    ¦    ¦     b) Repair is made within 3      | ¦

¦                           ¦    ¦    ¦        flight days.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Hobbs Hour Meter    C ¦ 1  ¦ 0  ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 32-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Anti-Skid System    C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦

¦ ***                       ¦    ¦    ¦     a) Anti-Skid System is secured  | ¦

¦                           ¦    ¦    ¦        as necessary to assure no    | ¦

¦                           ¦    ¦    ¦        interference with the normal | ¦

¦                           ¦    ¦    ¦        brake systems, and           | ¦

¦                           ¦    ¦    ¦     b) Aircraft is operated in      | ¦

¦                           ¦    ¦    ¦        accordance with AFM          | ¦

¦                           ¦    ¦    ¦        provisions for inoperative   | ¦

¦                           ¦    ¦    ¦        anti-skid.                   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 33-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Exterior Emergency  C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     Exit Light System     ¦    ¦    ¦ aircraft is not operated at night.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Position Light      C ¦ 1  ¦ 0  ¦                                     | ¦

¦     Flasher System        ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Position Light      C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     System (Wing Tips     ¦    ¦    ¦ aircraft is not operated at night.  | ¦

¦     and Tail)             ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Wing Inspection     C ¦ 2  ¦ 0  ¦ May be inoperative provided a       | ¦

¦     Lights                ¦    ¦    ¦ portable lamp/light of adequate     | ¦

¦                           ¦    ¦    ¦ capacity for wing and/or control    | ¦

¦                           ¦    ¦    ¦ surface inspection is available for | ¦

¦                           ¦    ¦    ¦ night operation in icing            | ¦

¦                           ¦    ¦    ¦ conditions.                         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Landing Lights      C ¦ 2  ¦ 1  ¦ One may be inoperative provided a   | ¦

¦                           ¦    ¦    ¦ Taxi Light of 600 watts or greater  | ¦

¦                           ¦    ¦    ¦ is installed and operative.         | ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Anti-Collision      C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     Light System          ¦    ¦    ¦ aircraft is not operated at night   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Taxi Light          C ¦ 1  ¦ 0  ¦ May be inoperative provided both    | ¦

¦                           ¦    ¦    ¦ Landing Lights are operative.       | ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Wheel Well Light    C ¦ 3  ¦ 0  ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 33-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Passenger Loading   C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     Stair Light           ¦    ¦    ¦ lighting sufficient to illuminate   | ¦

¦                           ¦    ¦    ¦ the steps is available.             | ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Cockpit and         C ¦ -  ¦ -  ¦ May be inoperative provided:        | ¦

¦     Instrument Lighting   ¦    ¦    ¦     a) Sufficient lighting is       | ¦

¦     Systems (Excluding    ¦    ¦    ¦        operative to make each       | ¦

¦     EFIS and MFDS and     ¦    ¦    ¦        instrument, control and      | ¦

¦     Emergency Lighting)   ¦    ¦    ¦        other device for which it is | ¦

¦                           ¦    ¦    ¦        provided easily readable,    | ¦

¦                           ¦    ¦    ¦     b) Direct rays and reflections  | ¦

¦                           ¦    ¦    ¦        do not impair visibility     | ¦

¦                           ¦    ¦    ¦        either inside or outside of  | ¦

¦                           ¦    ¦    ¦        the aircraft,                | ¦

¦                           ¦    ¦    ¦     c) Lighting intensity can be    | ¦

¦                           ¦    ¦    ¦        controlled, or is preset to  | ¦

¦                           ¦    ¦    ¦        a satisfactory level for     | ¦

¦                           ¦    ¦    ¦        expected flight conditions,  | ¦

¦                           ¦    ¦    ¦        and                          | ¦

¦                           ¦    ¦    ¦     d) Lighting configuration at    | ¦

¦                           ¦    ¦    ¦        dispatch is acceptable to    | ¦

¦                           ¦    ¦    ¦        the flight crew.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Cabin Interior      C ¦ -  ¦ -  ¦ May be inoperative provided:        | ¦

¦     Lights                ¦    ¦    ¦     a) Cabin emergency lighting is  | ¦

¦                           ¦    ¦    ¦        operative,                   | ¦

¦                           ¦    ¦    ¦     b) Sufficient lighting is       | ¦

¦                           ¦    ¦    ¦        operative for crew to        | ¦

¦                           ¦    ¦    ¦        perform required duties, and | ¦

¦                           ¦    ¦    ¦     c) Lighting configuration at    | ¦

¦                           ¦    ¦    ¦        dispatch is acceptable to    | ¦

¦                           ¦    ¦    ¦        flight crew.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 33-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. No Smoking/ Fasten    ¦    ¦    ¦                                     | ¦

¦     Seat Belt Signs       ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      1) Passenger       C ¦ -  ¦ -  ¦ May be inoperative provided         | ¦

¦         Configuration     ¦    ¦    ¦ Passenger or Flight Attendant Seats | ¦

¦                           ¦    ¦    ¦ from which a readily legible NO     | ¦

¦                           ¦    ¦    ¦ SMOKING/FASTEN SEAT BELT sign       | ¦

¦                           ¦    ¦    ¦ cannot be seen are placarded        | ¦

¦                           ¦    ¦    ¦ inoperative and "DO NOT OCCUPY."    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ -  ¦ (O)May be inoperative provided      | ¦

¦                           ¦    ¦    ¦ Operations procedures are           | ¦

¦                           ¦    ¦    ¦ established for alerting the cabin  | ¦

¦                           ¦    ¦    ¦ attendants and notifying the        | ¦

¦                           ¦    ¦    ¦ passengers by use of the Passenger  | ¦

¦                           ¦    ¦    ¦ Address System when seat belts      | ¦

¦                           ¦    ¦    ¦ should be fastened and smoking is   | ¦

¦                           ¦    ¦    ¦ prohibited.                         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) Cargo           D ¦ -  ¦ 0  ¦                                     | ¦

¦         Configuration     ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Strobe Light System C ¦ 1  ¦ 0  ¦                                     | ¦

¦ *** (Supplemental         ¦    ¦    ¦                                     | ¦

¦     System)               ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Baggage Compartment C ¦ -  ¦ -  ¦ May be inoperative provided         | ¦

¦     Lights                ¦    ¦    ¦ Sufficient Lights are operative to  | ¦

¦                           ¦    ¦    ¦ illuminate the baggage compartment. | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Logo Light Systems  D ¦ -  ¦ -  ¦                                     | ¦

¦ ***                       ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 16. Nacelle             C ¦ 2  ¦ 0  ¦                                     | ¦

¦ *** Illumination Lights   ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 33-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 17. Floor               C ¦ 1  ¦ 1  ¦ *Individual lights may be           | ¦

¦ *** Proximity Escape      ¦    ¦    ¦ inoperative provided FAA approved   | ¦

¦     Path Marking Lights   ¦    ¦    ¦ minimum acceptable lighting levels  | ¦

¦     System Light          ¦    ¦    ¦ in one of the following documents   | ¦

¦                           ¦    ¦    ¦ are complied with:                  | ¦

¦                           ¦    ¦    ¦     a) FAA engineering Approval     | ¦

¦                           ¦    ¦    ¦        letter.                      | ¦

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

¦                           ¦    ¦    ¦        Type Design holder.          | ¦

¦                           ¦    ¦    ¦     c) Limitations and Conditions   | ¦

¦                           ¦    ¦    ¦        section of the applicable    | ¦

¦                           ¦    ¦    ¦        Supplemental Type            | ¦

¦                           ¦    ¦    ¦        Certificate (STC).           | ¦

¦                           ¦    ¦    ¦     d) FAA approved report          | ¦

¦                           ¦    ¦    ¦        incorporated in the Master   | ¦

¦                           ¦    ¦    ¦        drawing list for the         | ¦

¦                           ¦    ¦    ¦        applicable STC.              | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 34-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Turn and Slip       C ¦ 2  ¦ 1  ¦ May be inoperative provided third   | ¦

¦     Indicator (Turn       ¦    ¦    ¦ Gyroscopic Bank and Pitch Indicator | ¦

¦     Indication)           ¦    ¦    ¦ is installed and operative.         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 1  ¦ May be inoperative provided         | ¦

¦                           ¦    ¦    ¦ aircraft is operated in Day VMC.    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Non-Stabilized      C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦

¦     Magnetic Compass      ¦    ¦    ¦     a) Standby Compass is not       | ¦

¦                           ¦    ¦    ¦        required by AFM Limitations, | ¦

¦                           ¦    ¦    ¦        and                          | ¦

¦                           ¦    ¦    ¦     b) Two independent magnetic     | ¦

¦                           ¦    ¦    ¦        stabilized directional       | ¦

¦                           ¦    ¦    ¦        compass systems are          | ¦

¦                           ¦    ¦    ¦        operative.                   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Automatic Direction C ¦ -  ¦ -  ¦ As required by FAR.                 | ¦

¦     Finding (AD) System   ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  VHF Navigation      C ¦ -  ¦ -  ¦ As required by FAR.                 | ¦

¦     Systems (VOR, ILS)    ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Marker Beacon       C ¦ -  ¦ -  ¦ May be inoperative provided Marker  | ¦

¦     Receiver System       ¦    ¦    ¦ Beacon is not required for the      | ¦

¦                           ¦    ¦    ¦ approach to be flown.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Outside Air         C ¦ 1  ¦ -  ¦ May be inoperative provided:        | ¦

¦     Temperature (OAT)     ¦    ¦    ¦     a) OAT data is either available | ¦

¦     Indicating System     ¦    ¦    ¦        to or not required for other | ¦

¦                           ¦    ¦    ¦        required systems, and        | ¦

¦                           ¦    ¦    ¦     b) Applicable FAR does not      | ¦

¦                           ¦    ¦    ¦        require OAT Indicating       | ¦

¦                           ¦    ¦    ¦        system for operation being   | ¦

¦                           ¦    ¦    ¦        conducted.                   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 34-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Altitude Alerting   A ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦

¦     System                ¦    ¦    ¦     a) Autopilot with altitude hold | ¦

¦                           ¦    ¦    ¦        is operative, and            | ¦

¦                           ¦    ¦    ¦     b) Repairs are made within      | ¦

¦                           ¦    ¦    ¦        three flight days.           | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Ground Proximity    A ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦

¦     A Warning System      ¦    ¦    ¦     a) Alternate procedures are     | ¦

¦     (GPWS)                ¦    ¦    ¦        established and used, and    | ¦

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

¦                           ¦    ¦    ¦        flight days.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      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 ¦ -  ¦ 0  ¦ (O) May be inoperative provided     | ¦

¦        Callouts           ¦    ¦    ¦ alternate procedures are            | ¦

¦                           ¦    ¦    ¦ established and used.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ *** 5) Windshear Mode   C ¦ -  ¦ 0  ¦ (O) May be inoperative provided     | ¦

¦                           ¦    ¦    ¦ alternate procedures are            | ¦

¦                           ¦    ¦    ¦ established and used.               | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦ (Continued)                         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 34-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Ground Proximity      ¦    ¦    ¦                                     | ¦

¦     A Warning System      ¦    ¦    ¦                                     | ¦

¦     (GPWS) (Cont'd)       ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***  6) TAWS            C ¦ -  ¦ 0  ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Long Range          C ¦ -  ¦ -  ¦ As required by FAR.                 | ¦

¦     Navigation Systems    ¦    ¦    ¦                                     | ¦

¦     (INS, LORAN, VLF/     ¦    ¦    ¦                                     | ¦

¦     OMEGA, etc.)          ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. TACAN System        C ¦ -  ¦ -  ¦ As required by FAR.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Radio Altimeter     C ¦ -  ¦ -  ¦ (O)May be inoperative provided:     | ¦

¦     System                ¦    ¦    ¦     a) Dispatch deviation for GPWS  | ¦

¦                           ¦    ¦    ¦        is observed, and             | ¦

¦                           ¦    ¦    ¦     b) Radio Altimeter is not       | ¦

¦                           ¦    ¦    ¦        required for the approach to | ¦

¦                           ¦    ¦    ¦        be flown.                    | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦ NOTE:  Radio Altitude may be        | ¦

¦                           ¦    ¦    ¦        required for the Autopilot,  | ¦

¦                           ¦    ¦    ¦        GPWS, or Flight Director.    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Radio Magnetic      C ¦ 2  ¦ 1  ¦ One may be inoperative provided     | ¦

¦     Indicator (RMI)       ¦    ¦    ¦ affected HSI is not a Basic "T"     | ¦

¦                           ¦    ¦    ¦ instrument.                         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Standby Attitude    C ¦ 1  ¦ 0  ¦                                     | ¦

¦     Indicator (Third      ¦    ¦    ¦                                     | ¦

¦     Attitude Indicator)   ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 34-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Flight director     C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦

¦ *** System                ¦    ¦    ¦     a) It is verified that the      | ¦

¦                           ¦    ¦    ¦        Command Bars will remain     | ¦

¦                           ¦    ¦    ¦        retracted, and               | ¦

¦                           ¦    ¦    ¦     b) Affected Flight director is  | ¦

¦                           ¦    ¦    ¦        not required for the         | ¦

¦                           ¦    ¦    ¦        approach to be flown.        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Vertical Speed      C ¦ 2  ¦ 1  ¦ One may be inoperative provided     | ¦

¦     Indicator             ¦    ¦    ¦ aircraft is operated in Day VMC     | ¦

¦                           ¦    ¦    ¦ only.                               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 16. Attitude System     C ¦ -  ¦ 2  ¦ May be inoperative provided         | ¦

¦     Sensors (Vertical     ¦    ¦    ¦ independent Primary Attitude        | ¦

¦     Gyro, AHRS, IRS,      ¦    ¦    ¦ information is available on each    | ¦

¦     etc)                  ¦    ¦    ¦ pilot's panel.                      | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 17. Compass System      C ¦ -  ¦ 2  ¦ May be inoperative provided:        | ¦

¦     Sensors               ¦    ¦    ¦     a) Both Directional Compass     | ¦

¦     (Directional Gyro,    ¦    ¦    ¦        Systems are operative from   | ¦

¦     AHRS, IRS, etc.)      ¦    ¦    ¦        independent sources, and     | ¦

¦                           ¦    ¦    ¦     b) Each pilot's panel has       | ¦

¦                           ¦    ¦    ¦        independent heading          | ¦

¦                           ¦    ¦    ¦        information.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 18. Traffic Alert and   C ¦ -  ¦ 0  ¦ (M)May be inoperative provided the  | ¦

¦     Collision Avoidance   ¦    ¦    ¦ System is deactivated and secured.  | ¦

¦     System (TCAS I)       ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 34-5     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     Traffic Alert and   C ¦ -  ¦ 0  ¦ (M)May be inoperative provided the  | ¦

¦     Collision Avoidance   ¦    ¦    ¦ System is deactivated and secured.  | ¦

¦     System (TCAS II)      ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***  1) Combined        C ¦ 2  ¦ 1  ¦ One may be inoperative on the non-  | ¦

¦         Traffic Alert     ¦    ¦    ¦ flying pilot's side provided TA and | ¦

¦         (TA) and          ¦    ¦    ¦ RA audio functions are operative on | ¦

¦         Resolution        ¦    ¦    ¦ the flying pilot's side.            | ¦

¦         Advisory (RA)     ¦    ¦    ¦                                     | ¦

¦         Dual Display      ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) Resolution      C ¦ 2  ¦ 1  ¦ (O)One may be inoperative on the    | ¦

¦         Advisory (RA)     ¦    ¦    ¦ non-flying pilot's side.            | ¦

¦         Display Systems   ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦

¦                           ¦    ¦    ¦     a) Traffic Alert (TA) visual    | ¦

¦                           ¦    ¦    ¦        display and audio functions  | ¦

¦                           ¦    ¦    ¦        are operative, and           | ¦

¦                           ¦    ¦    ¦     b) TA only mode is selected by  | ¦

¦                           ¦    ¦    ¦        the crew.                    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      3) Traffic Alert   C ¦ -  ¦ 0  ¦ (O)May be inoperative provided all  | ¦

¦         (TA) display      ¦    ¦    ¦ installed RA display and audio      | ¦

¦         System            ¦    ¦    ¦ functions are operative.            | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 19. Distance Measuring  D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

¦     Equipment (DME)       ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦     Systems               ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 20. Weather Radar       C ¦ 1  ¦ -  ¦ As required by FAR.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 21. ATC Transponder and C ¦ -  ¦ -  ¦ As required by FAR.                 | ¦

¦     Automatic Altitude    ¦    ¦    ¦                                     | ¦

¦     Reporting Systems   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: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 34-6     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 22. Windshear Detection C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦

¦ *** and Guidance System   ¦    ¦    ¦ alternate procedures are            | ¦

¦                           ¦    ¦    ¦ established and used.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 23. Global Positioning  D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦

¦ *** System (GPS)          ¦    ¦    ¦ procedures do not require its use.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 35-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 35  OXYGEN                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Oxygen System         ¦    ¦    ¦                                     | ¦

¦     (Cabin)               ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦      1) Passenger       C ¦ -  ¦ -  ¦ As required by FAR.                 | ¦

¦         Configuration     ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) Cargo Only      C ¦ -  ¦ 0  ¦ May be inoperative provided no      | ¦

¦         Configuration     ¦    ¦    ¦ persons are carried in the cabin.   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Portable Oxygen     C ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

¦     Dispensing Unit       ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Protective          D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

¦     Breathing Equipment   ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦     (PBE)                 ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 49-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 49  AIRBORNE AUXILIARY    ¦    ¦    ¦                                       ¦

¦     POWER                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.   Auxiliary Power    C ¦ 1  ¦ 0  ¦                                     | ¦

¦ ***  Unit                 ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 52-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 52  DOORS                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Access Doors -      B ¦ 8  ¦ 8  ¦ *#If a hinge is broken on any of      ¦

¦     Belly Access and      ¦    ¦    ¦   the eight belly access and cargo    ¦

¦     Cargo Doors           ¦    ¦    ¦   doors, the airplane may be          ¦

¦                           ¦    ¦    ¦   dispatched PRESSURIZED provided     ¦

¦                           ¦    ¦    ¦   all of the door locking arms are    ¦

¦                           ¦    ¦    ¦   operating properly. If any          ¦

¦                           ¦    ¦    ¦   locking mechanism malfunctions      ¦

¦                           ¦    ¦    ¦   to the point that it does not       ¦

¦                           ¦    ¦    ¦   engage within the detent, it must   ¦

¦                           ¦    ¦    ¦   either be repaired or the           ¦

¦                           ¦    ¦    ¦   airplane dispatched                 ¦

¦                           ¦    ¦    ¦   UNPRESSURIZED.                      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Aft Passenger Ramp  C ¦ 1  ¦ 1  ¦ *#The aft passenger ramp is not       ¦

¦                           ¦    ¦    ¦   considered an emergency exit. If    ¦

¦                           ¦    ¦    ¦   the ramp is hydraulically or        ¦

¦                           ¦    ¦    ¦   electrically inoperative but can    ¦

¦                           ¦    ¦    ¦   be opened or closed and locked      ¦

¦                           ¦    ¦    ¦   manually, the airplane may be       ¦

¦                           ¦    ¦    ¦   dispatched.                         ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 61-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 61  PROPELLERS            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Synchronization     C ¦ 2  ¦ 0  ¦                                     | ¦

¦     System                ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Reverse Pitch       C ¦ 2  ¦ 1  ¦ One may be inoperative provided     | ¦

¦     Indicating System     ¦    ¦    ¦ associated reverse system is        | ¦

¦                           ¦    ¦    ¦ considered inoperative.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Auto Feathering     C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦     System                ¦    ¦    ¦ aircraft is operated in accordance  | ¦

¦                           ¦    ¦    ¦ with applicable AFM procedures.     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Propeller Pitch       ¦    ¦    ¦                                     | ¦

¦     Limit Lights System   ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***  1) Curtis Electric C ¦ 2  ¦ 0  ¦                                     | ¦

¦      Propellers           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***  2) Hamilton        C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided:     | ¦

¦      Standard             ¦    ¦    ¦     a) Manifold Pressure indicating | ¦

¦        Propellers         ¦    ¦    ¦        System for associated engine | ¦

¦                           ¦    ¦    ¦        is operative, and            | ¦

¦                           ¦    ¦    ¦     b) Alternated operations        | ¦

¦                           ¦    ¦    ¦        procedures are established   | ¦

¦                           ¦    ¦    ¦        and used.                    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Reverse System      A ¦ 2  ¦ 0  ¦ (M)May be inoperative provided      | ¦

¦ ***                       ¦    ¦    ¦ reverse system is deactivated.      | ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦ NOTE:   Reference AFM Procedures    | ¦

¦                           ¦    ¦    ¦        and performance Sections for | ¦

¦                           ¦    ¦    ¦        operations without Reverse.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 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 Pressure       C ¦ 2  ¦ 1  ¦ May be inoperative provided:        | ¦

¦     Indicating System     ¦    ¦    ¦     a) Associated Fuel Flow         | ¦

¦                           ¦    ¦    ¦        indicating System is         | ¦

¦                           ¦    ¦    ¦        operative,                   | ¦

¦                           ¦    ¦    ¦     b) Associated Fuel Pressure     | ¦

¦                           ¦    ¦    ¦        Warning Light System is      | ¦

¦                           ¦    ¦    ¦        operative.                   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Fuel Flow           C ¦ 2  ¦ 0  ¦ Both may be inoperative provided:   | ¦

¦     Indicating System     ¦    ¦    ¦     a) Associated Fuel Quantity     | ¦

¦                           ¦    ¦    ¦        Indicating System is         | ¦

¦                           ¦    ¦    ¦        operative, and               | ¦

¦                           ¦    ¦    ¦     b) Associated Torque Indicating | ¦

¦                           ¦    ¦    ¦        System is operative.         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Fuel Pressure       C ¦ 2  ¦ 1  ¦ May be inoperative provided:        | ¦

¦     Warning Light         ¦    ¦    ¦     a) Associated Fuel Pressure     | ¦

¦     System                ¦    ¦    ¦        indicating System is         | ¦

¦                           ¦    ¦    ¦        operative, and               | ¦

¦                           ¦    ¦    ¦     b) Associate Fuel flow          | ¦

¦                           ¦    ¦    ¦        Indicating System is         | ¦

¦                           ¦    ¦    ¦        operative.                   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 77-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Torque Indicating     ¦    ¦    ¦                                     | ¦

¦     System (BEMP)         ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        | ¦

¦                           ¦    ¦    ¦ provided:                           | ¦

¦                           ¦    ¦    ¦     a) Auto Feathering System is    | ¦

¦                           ¦    ¦    ¦        verified operative before    | ¦

¦                           ¦    ¦    ¦        each flight, and             | ¦

¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦

¦                           ¦    ¦    ¦        established and used to set  | ¦

¦                           ¦    ¦    ¦        Takeoff power.               | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦     a) Auto Feathering is           | ¦

¦                           ¦    ¦    ¦        considered inoperative, and  | ¦

¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦

¦                           ¦    ¦    ¦        established and used to set  | ¦

¦                           ¦    ¦    ¦        Takeoff power.               | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Temperature           ¦    ¦    ¦     a) Associated Manifold Pressure | ¦

¦     Indicating System     ¦    ¦    ¦        Indicating System is         | ¦

¦                           ¦    ¦    ¦        operative,                   | ¦

¦                           ¦    ¦    ¦     b) Fuel Flow Indicating System  | ¦

¦                           ¦    ¦    ¦        for associated engine is     | ¦

¦                           ¦    ¦    ¦        operative,                   | ¦

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

¦                           ¦    ¦    ¦        visible moisture,            | ¦

¦                           ¦    ¦    ¦     d) Aircraft is not operated in  | ¦

¦                           ¦    ¦    ¦        known of forecast icing      | ¦

¦                           ¦    ¦    ¦        conditions.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Cylinder Head       C ¦ 2  ¦ 1  ¦ One may be inoperative provided     | ¦

¦     Temperature           ¦    ¦    ¦ associated Oil Temperature          | ¦

¦     Indicating System     ¦    ¦    ¦ indicating System is operative.     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 77-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Manifold Pressure   C ¦ 2  ¦ 1  ¦ One may be inoperative provided     | ¦

¦     Indicating System     ¦    ¦    ¦ associated Torque Indicating System | ¦

¦                           ¦    ¦    ¦ is operative.                       | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 79-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 79  ENGINE OIL            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Oil Temperature       ¦    ¦    ¦                                     | ¦

¦     Control System        ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***    a) Automatic     C ¦ 1  ¦ 0  ¦ May be inoperative provided Manual  | ¦

¦                           ¦    ¦    ¦ Control System is operative.        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***    b) Manual        C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦                           ¦    ¦    ¦ Automatic Control System is         | ¦

¦                           ¦    ¦    ¦ operative.                          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Pressure Warning    C ¦ 2  ¦ 0  ¦ Both May be inoperative provided    | ¦

¦ *** Lights                ¦    ¦    ¦ associated Oil Pressure Indicators  | ¦

¦                           ¦    ¦    ¦ are operative.                      | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Oil Temperature     C ¦ 2  ¦ 1  ¦ One may be inoperative provided:    | ¦

¦     Indicators            ¦    ¦    ¦     a) Associated Oil Pressure      | ¦

¦                           ¦    ¦    ¦        Indicator is operative, and  | ¦

¦                           ¦    ¦    ¦     b) Associated Cylinder Head     | ¦

¦                           ¦    ¦    ¦        Temperature Indicators are   | ¦

¦                           ¦    ¦    ¦        operative.                   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Oil Dilution        C ¦ 2  ¦ 0  ¦                                     | ¦

¦ ***                       ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Oil Quantity        C ¦ 2  ¦ 0  ¦ Both may be inoperative provided:   | ¦

¦     Indicators            ¦    ¦    ¦     a) Associated Oil Temperature   | ¦

¦                           ¦    ¦    ¦        indicators are operative,    | ¦

¦                           ¦    ¦    ¦     b) Associated Oil Pressure      | ¦

¦                           ¦    ¦    ¦        indicators are operative,    | ¦

¦                           ¦    ¦    ¦        and                          | ¦

¦                           ¦    ¦    ¦     c) Oil Tank Quantity is         | ¦

¦                           ¦    ¦    ¦        verified adequate at each    | ¦

¦                           ¦    ¦    ¦        flight.                      | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦

¦               MARTIN M-404               ¦                       ¦          ¦

¦                                          ¦ DATE: 12/07/2000      ¦ 82-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 82  WATER INJECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Anti-Detonation     C ¦ 2  ¦ 0  ¦ May be inoperative provided         | ¦

¦ *** Inspection (ADI)      ¦    ¦    ¦ aircraft is operated in accordance  | ¦

¦     System                ¦    ¦    ¦ with appropriate AFM procedures.    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  ADI Fluid Quantity  C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided ADI  | ¦

¦ *** Indicating System     ¦    ¦    ¦ Tank quantity is verified adequate  | ¦

¦                           ¦    ¦    ¦ (Full or dipstick) before each      | ¦

¦                           ¦    ¦    ¦ flight.                             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided ADI     | ¦

¦                           ¦    ¦    ¦ System is considered inoperative.   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  ADI Fluid Pressure  C ¦ 1  ¦ 0  ¦ May be inoperative provided ADI     | ¦

¦     Indicating System     ¦    ¦    ¦ System is considered inoperative.   | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      1) ADI Light       C ¦ 1  ¦ 0  ¦ One may be inoperative provided     | ¦

¦ ***                       ¦    ¦    ¦ associated ADI Pressure Gauge is    | ¦

¦                           ¦    ¦    ¦ operative.                          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) ADI Pressure    C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦         Gauge             ¦    ¦    ¦ associated ADI Light is operative.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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