DEPARTMENT OF TRANSPORTATION     Revision: ORIGINAL

                                                           Date: 01/15/2003

                         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

 

 

 

 

 

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                         Federal Aviation Administration

                         Flight Standards Division

                         AIRCRAFT EVALUATION GROUP, LGB-AEG

                         3960 PARAMOUNT BOULEVARD

                         LONG BEACH, CA 90712-4137

 

                         TELEPHONE:  (562) 627-5273

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/15/2003

 

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                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I

         --     Log of Revisions                        II

         --     Control Page                            III, IV

         --     Highlights of Change                    V, VI, VII

         --     Definitions                             VIII, IX, X, XI

         --     Definitions                             XII, XIII, XIV, XV

         --     Preamble                                XVI, XVII

         21     Air Conditioning                        21-1

         22     Auto Flight                             22-1

         23     Communications                          23-1

         24     Electrical Power                        24-1

         25     Equipment/Furnishings                   25-1, 2

         26     Fire Protection                         26-1

         28     Fuel                                    28-1, 2

         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

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

         35     Oxygen                                  35-1

         49     Airborne Auxiliary Power                49-1

         52     Doors                                   52-1

         61     Propellers                              61-1

         73     Engine Fuel & Control                   73-1

         74     Ignition                                74-1

         77     Engine Indicating                       77-1

         79     Engine Oil                              79-1


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: II

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                        MASTER MINIMUM EQUIPMENT LIST    Date: 01/15/2003

 

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                               Log of Revisions

 

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                       FEDERAL AVIATION ADMINISTRATION     Page: III

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                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       ORIGINAL 01/15/2003

         Table of Contents                        I       ORIGINAL 01/15/2003

         Log of Revisions                         II      ORIGINAL 01/15/2003

         Control Page                             III     ORIGINAL 01/15/2003

                                                  IV      ORIGINAL 01/15/2003

         Highlights of Change                     V       ORIGINAL 01/15/2003

                                                  VI      ORIGINAL 01/15/2003

                                                  VII     ORIGINAL 01/15/2003

         Definitions                              VIII    6        01/31/1995

                                                  IX      6        01/31/1995

                                                  X       6        01/31/1995

                                                  XI      6        01/31/1995

                                                  XII     6        01/31/1995

                                                  XIII    6        01/31/1995

                                                  XIV     6        01/31/1995

                                                  XV      6        01/31/1995

         Preamble                                 XVI     2        06/14/1989

                                                  XVII    2        06/14/1989

         21                                       21-1    ORIGINAL 01/15/2003

         22                                       22-1    ORIGINAL 01/15/2003

         23                                       23-1    ORIGINAL 01/15/2003

         24                                       24-1    ORIGINAL 01/15/2003

         25                                       25-1    ORIGINAL 01/15/2003

                                                  25-2    ORIGINAL 01/15/2003

         26                                       26-1    ORIGINAL 01/15/2003

         28                                       28-1    ORIGINAL 01/15/2003

                                                  28-2    ORIGINAL 01/15/2003

         29                                       29-1    ORIGINAL 01/15/2003

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                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

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                       FEDERAL AVIATION ADMINISTRATION   Page: V

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                            Highlights of Change

 

 

 

       Effective this date the original document for the Lockheed P-3 (Orion)

       MMEL is issued. This document was prepared by the Seattle Aircraft

       Evaluation Group (SEA-AEG) on behalf of the Long Beach Aircraft

       Evaluation Group (LGB-AEG). Questions or comments on this original

       document may be addressed to the SEA-AEG or directly to the LGB-AEG.

 

       Telephone: LGB-AEG (562) 627-5273

                  SEA-AEG (425) 227-2273 or 2280

 

 

 

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

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

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: VI

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                            Highlights of Change

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: VII

                                                         Revision: ORIGINAL

                        MASTER MINIMUM EQUIPMENT LIST    Date: 01/15/2003

 

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                            Highlights of Change

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

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                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

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                                 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: IX

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                                 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: X

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                                 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: XI

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                                 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: XII

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                                 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: XIII

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                                 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: XIV

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                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

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                                 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: XV

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                                    P-3

 

 

                                 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: XVI

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                                    P-3

 

 

                                  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: XVII

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                                    P-3

 

 

                                  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: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 21-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Vapor Cycle         C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦

¦     (Freon) Environment   ¦    ¦    ¦ cabin exhaust fan and flight          ¦

¦     Control System (ECS)  ¦    ¦    ¦ station auxiliary vent valve are      ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Cabin Exhaust Fan   C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦

¦                           ¦    ¦    ¦ smoke removal hatch is operative.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Flight Station      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦

¦     Auxiliary Vent        ¦    ¦    ¦ ECS (Freon) cooling system and the    ¦

¦     Valve                 ¦    ¦    ¦ cabin exhaust fan are operative.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 22-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Autopilot System    B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦

¦                           ¦    ¦    ¦ approach minimums or operating        ¦

¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE: Any mode that operates          ¦

¦                           ¦    ¦    ¦       normally may be used.           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Control Wheel       C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦     Disengage Switches    ¦    ¦    ¦ autopilot is not used below initial   ¦

¦                           ¦    ¦    ¦ approach altitude.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 23-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Systems (VHF,HF,      ¦    ¦    ¦ FAR, and not powered by an            ¦

¦     UHF, etc.)            ¦    ¦    ¦ Emergency bus, may be inoperative.    ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ *** Speakers              ¦    ¦    ¦     a) They are not required for      ¦

¦                           ¦    ¦    ¦        emergency procedures, and      ¦

¦                           ¦    ¦    ¦     b) Headsets are installed and     ¦

¦                           ¦    ¦    ¦        operative for all required     ¦

¦                           ¦    ¦    ¦        flight deck crewmembers.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Radio Rack          B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦     Cooling Fan           ¦    ¦    ¦     a) Ground operations are          ¦

¦                           ¦    ¦    ¦        limited to 20 minutes, and     ¦

¦                           ¦    ¦    ¦     b) Cockpit cooling (ECS)          ¦

¦                           ¦    ¦    ¦        system is operative.           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Audio Amplifier     C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦

¦                           ¦    ¦    ¦ required flight crew members have     ¦

¦                           ¦    ¦    ¦ operative headsets.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Control Yoke Press  C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦     to Talk Switches      ¦    ¦    ¦ alternate procedures are              ¦

¦                           ¦    ¦    ¦ established and used.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Cockpit Voice         ¦    ¦    ¦                                       ¦

¦ *** Recorder System       ¦    ¦    ¦                                       ¦

¦     (CVR)                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) With FDR         A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

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

¦                           ¦    ¦    ¦        operates normally, and         ¦

¦                           ¦    ¦    ¦     b) Repairs are made within        ¦

¦                           ¦    ¦    ¦        three flight days.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Without FDR      A ¦ 1  ¦ 0  ¦ May be inoperative provided repairs   ¦

¦        Installed          ¦    ¦    ¦ are made within three flight days.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 24-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  AC Generator        A ¦ 3  ¦ 2  ¦ (M)One may be inoperative provided:   ¦

¦     Systems               ¦    ¦    ¦     a) The cause of the malfunction   ¦

¦                           ¦    ¦    ¦        is determined,                 ¦

¦                           ¦    ¦    ¦     b) Appropriate action is taken    ¦

¦                           ¦    ¦    ¦        to assure that no hazard       ¦

¦                           ¦    ¦    ¦        exists, and                    ¦

¦                           ¦    ¦    ¦     c) Repairs are made within        ¦

¦                           ¦    ¦    ¦        three flight days.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Generator Caution     ¦    ¦    ¦                                       ¦

¦     Lights                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Generator OFF    B ¦ -  ¦ -  ¦ (M)May be inoperative provided:       ¦

¦        Lights             ¦    ¦    ¦     a) Associated generator is        ¦

¦                           ¦    ¦    ¦        inoperative, and               ¦

¦                           ¦    ¦    ¦     b) Associated Mechanical          ¦

¦                           ¦    ¦    ¦        Failure Light is operative.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Mechanical       B ¦ 3  ¦ 2  ¦ (M)One may be inoperative provided    ¦

¦        Failure Lights     ¦    ¦    ¦ associated generator is removed or    ¦

¦                           ¦    ¦    ¦ disengaged and secured by an          ¦

¦                           ¦    ¦    ¦ acceptable procedure.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Transformer         B ¦ 3  ¦ 2  ¦ (M)TRU #3 may be inoperative          ¦

¦     Rectifier Units       ¦    ¦    ¦ provided TRU #1 and TRU #2 are        ¦

¦     (TRU)s                ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  External Power      C ¦ 1  ¦ 0  ¦                                       ¦

¦ ***                       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 25-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

¦                           ¦    ¦    ¦        or removed using accepted      ¦

¦                           ¦    ¦    ¦        procedures, and                ¦

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

¦                           ¦    ¦    ¦        time limits.                   ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Flashlights/Holders   ¦    ¦    ¦ provided cabin crewmember assigned    ¦

¦                           ¦    ¦    ¦ to affected position has an           ¦

¦                           ¦    ¦    ¦ operative flashlight readily          ¦

¦                           ¦    ¦    ¦ available.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Airborne            D ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦     Application           ¦    ¦    ¦ system is deactivated and secured     ¦

¦     System (Retardant/    ¦    ¦    ¦ by an acceptable procedure.           ¦

¦     Spray)                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Seat (Including       ¦    ¦    ¦     a) An acceptable seat in the      ¦

¦     Associated            ¦    ¦    ¦        main cabin is made             ¦

¦     Equipment)            ¦    ¦    ¦        available to an FAA            ¦

¦                           ¦    ¦    ¦        inspector for the              ¦

¦                           ¦    ¦    ¦        performance of official        ¦

¦                           ¦    ¦    ¦        duties, and                    ¦

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

¦                           ¦    ¦    ¦        flight days.                   ¦

¦                           ¦    ¦    ¦          OR                           ¦

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

¦                           ¦    ¦    ¦        available with the required    ¦

¦                           ¦    ¦    ¦        minimum safety equipment       ¦

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

¦                           ¦    ¦    ¦        acceptable to the FAA for      ¦

¦                           ¦    ¦    ¦        the performance of official    ¦

¦                           ¦    ¦    ¦        duties, and                    ¦

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

¦                           ¦    ¦    ¦        flight days.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 25-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Forward Observer      ¦    ¦    ¦                                       ¦

¦     Seat (Including       ¦    ¦    ¦                                       ¦

¦     Associated            ¦    ¦    ¦                                       ¦

¦     Equipment) (Cont'd)   ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE 1:  These provisos are           ¦

¦                           ¦    ¦    ¦          intended to provide for      ¦

¦                           ¦    ¦    ¦          occupancy of the above       ¦

¦                           ¦    ¦    ¦          seat by an FAA inspector     ¦

¦                           ¦    ¦    ¦          when the minimum safety      ¦

¦                           ¦    ¦    ¦          equipment (oxygen and        ¦

¦                           ¦    ¦    ¦          safety belt) is functional   ¦

¦                           ¦    ¦    ¦          and the inspector            ¦

¦                           ¦    ¦    ¦          determines the conditions    ¦

¦                           ¦    ¦    ¦          to be acceptable.            ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦          determine if the minimum     ¦

¦                           ¦    ¦    ¦          safety equipment is          ¦

¦                           ¦    ¦    ¦          functional for other         ¦

¦                           ¦    ¦    ¦          persons authorized to        ¦

¦                           ¦    ¦    ¦          occupy any observer seat.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 26-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  APU Fire Detection  C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦     Control and           ¦    ¦    ¦     a) Visual check of APU            ¦

¦     Extinguishing System  ¦    ¦    ¦        compartment is accomplished    ¦

¦                           ¦    ¦    ¦        prior to APU start,            ¦

¦                           ¦    ¦    ¦     a) APU is used for engine         ¦

¦                           ¦    ¦    ¦        starting only, and             ¦

¦                           ¦    ¦    ¦     b) A fire guard is stationed on   ¦

¦                           ¦    ¦    ¦        the ground adjacent to the     ¦

¦                           ¦    ¦    ¦        APU at all times while it      ¦

¦                           ¦    ¦    ¦        is being operated, and         ¦

¦                           ¦    ¦    ¦        for at least 3 minutes         ¦

¦                           ¦    ¦    ¦        after APU shut down.           ¦

¦                           ¦    ¦    ¦           OR                          ¦

¦                         C ¦    ¦    ¦     c) APU is considered              ¦

¦                           ¦    ¦    ¦        inoperative, and not used.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Portable Fire       D ¦ -  ¦ -  ¦ (M)Any in excess of those required    ¦

¦     Extinguishers         ¦    ¦    ¦ by FAR may be inoperative or          ¦

¦                           ¦    ¦    ¦ missing provided:                     ¦

¦                           ¦    ¦    ¦     a) The inoperative fire           ¦

¦                           ¦    ¦    ¦        extinguisher is tagged         ¦

¦                           ¦    ¦    ¦        inoperative, removed from      ¦

¦                           ¦    ¦    ¦        the installed location, and    ¦

¦                           ¦    ¦    ¦        placed out of sight so it      ¦

¦                           ¦    ¦    ¦        cannot be mistaken for a       ¦

¦                           ¦    ¦    ¦        functional unit, and           ¦

¦                           ¦    ¦    ¦     b) Required distribution is       ¦

¦                           ¦    ¦    ¦        maintained.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Engine Fire         B ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦

¦     Warning Horn          ¦    ¦    ¦ Engine Fire Warning Lights are        ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 28-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Fuel Tank Boost     B ¦ 4  ¦ 3  ¦ (O)One may be inoperative provided    ¦

¦     Pumps                 ¦    ¦    ¦ aircraft is operated at or below      ¦

¦                           ¦    ¦    ¦ 18,000 feet MSL.                      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Fuel Quantity       C ¦ 4  ¦ 3  ¦ (M)(O)One may be inoperative          ¦

¦     Indicators (Flight    ¦    ¦    ¦ provided:                             ¦

¦     Station)              ¦    ¦    ¦     a) Fuel quantity is determined    ¦

¦                           ¦    ¦    ¦        by other approved means        ¦

¦                           ¦    ¦    ¦        after each refueling,          ¦

¦                           ¦    ¦    ¦     b) All Fuel Flow Meters are       ¦

¦                           ¦    ¦    ¦        operative, and                 ¦

¦                           ¦    ¦    ¦     c) Fuel consumed is recorded.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Fuel Quantity       C ¦ 4  ¦ 0  ¦ (M)May be inoperative provided fuel   ¦

¦     Indicators (Fueling   ¦    ¦    ¦ quantity is determined by an          ¦

¦     Panel)                ¦    ¦    ¦ approved means at each refueling.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Fuel Crossfeed      C ¦ 4  ¦ 3  ¦ (M)One may be inoperative provided    ¦

¦     Valve Position        ¦    ¦    ¦ Fuel Manifold Pressure Indicator      ¦

¦     Lights                ¦    ¦    ¦ is operative.                         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Single Point        D ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦     Refuel System (SPR)   ¦    ¦    ¦ alternate refueling procedures are    ¦

¦                           ¦    ¦    ¦ established and used.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Fueling Panel       B ¦ 1  ¦ 0  ¦ (M)May be missing provided:           ¦

¦     Fuel Cap              ¦    ¦    ¦     a) Refueling receptacle is        ¦

¦                           ¦    ¦    ¦        verified to be free of         ¦

¦                           ¦    ¦    ¦        contamination prior to each    ¦

¦                           ¦    ¦    ¦        refueling,                     ¦

¦                           ¦    ¦    ¦     b) Receptacle is verified to      ¦

¦                           ¦    ¦    ¦        have no leakage afterwards,    ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     c) All Fuel Tank Quantity         ¦

¦                           ¦    ¦    ¦        Indicators are operative.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 28-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Fuel Dump System    B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦ *** (P-3B/P-3C)           ¦    ¦    ¦     a) Takeoff weight does not        ¦

¦                           ¦    ¦    ¦        exceed 114,000 pounds,         ¦

¦                           ¦    ¦    ¦     b) All Fuel Dump Valves are       ¦

¦                           ¦    ¦    ¦        verified closed,               ¦

¦                           ¦    ¦    ¦     c) Performance is not             ¦

¦                           ¦    ¦    ¦        predicated on fuel dumping     ¦

¦                           ¦    ¦    ¦        for enroute engine(s)          ¦

¦                           ¦    ¦    ¦        inoperative procedures, and    ¦

¦                           ¦    ¦    ¦     d) AFM Limitations and            ¦

¦                           ¦    ¦    ¦        Procedures are followed.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 29-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  AC Hydraulic        B ¦ 3  ¦ 2  ¦ (M)Hydraulic Pump #2 may be           ¦

¦     Pumps                 ¦    ¦    ¦ inoperative provided both Pump #1     ¦

¦                           ¦    ¦    ¦ and Pump #1A are operative.           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Battery Powered     C ¦ 1  ¦ 0  ¦                                       ¦

¦     DC Pump (1b Pump)     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Hydraulic System    B ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦

¦     Pressure              ¦    ¦    ¦ Hydraulic Low Pressure Warning        ¦

¦     Indications           ¦    ¦    ¦ Lights are operative.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Hydraulic Low       C ¦ 3  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦     Pressure Warning      ¦    ¦    ¦ associated system pressure            ¦

¦     Lights                ¦    ¦    ¦ indicator is operative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 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.  Engine Air Scoop    B ¦ 8  ¦ 7  ¦ (M)(O)May be inoperative provided:    ¦

¦     and Inlet Vane        ¦    ¦    ¦     a) Solenoid Valves are verified   ¦

¦     Systems               ¦    ¦    ¦        in the OPEN position,          ¦

¦                           ¦    ¦    ¦     b) Remaining three Engine Anti-   ¦

¦                           ¦    ¦    ¦        Ice Systems are operative,     ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     c) Associated Engine Air Scoop    ¦

¦                           ¦    ¦    ¦        and Inlet Vane Icing Light     ¦

¦                           ¦    ¦    ¦        is operative.                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Engine Air Scoop    B ¦ 4  ¦ 2  ¦ (M)Two may be inoperative provided    ¦

¦     and Inlet Vane        ¦    ¦    ¦ associated TIT and Horsepower         ¦

¦     Icing Lights          ¦    ¦    ¦ indicators are operative.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Propeller Anti-     C ¦ 4  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦     Icing (Including      ¦    ¦    ¦     a) AFM approved "ICEX" (or        ¦

¦     Spinner and           ¦    ¦    ¦        equivalent product) anti-      ¦

¦     Islands)              ¦    ¦    ¦        icing procedure is used.       ¦

¦                           ¦    ¦    ¦            OR                         ¦

¦                         C ¦    ¦    ¦     b) Aircraft is not operated       ¦

¦                           ¦    ¦    ¦        in known or forecast icing.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Wing and Empennage    ¦    ¦    ¦                                       ¦

¦     De-icing and          ¦    ¦    ¦                                       ¦

¦     Anti-icing Systems    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Wing System      C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦                           ¦    ¦    ¦     a) Valves are verified in the     ¦

¦                           ¦    ¦    ¦        CLOSED position, and           ¦

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

¦                           ¦    ¦    ¦        known or forecast icing.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 30-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Wing and Empennage    ¦    ¦    ¦                                       ¦

¦     De-icing and          ¦    ¦    ¦                                       ¦

¦     Anti-icing Systems    ¦    ¦    ¦                                       ¦

¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Empennage        C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦        System             ¦    ¦    ¦     a) System is secured by an        ¦

¦                           ¦    ¦    ¦        acceptable procedure, and      ¦

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

¦                           ¦    ¦    ¦        known or forecast icing.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Icing Light         C ¦ 1  ¦ 0  ¦                                       ¦

¦ ***                       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Engine Bleed Air    C ¦ 6  ¦ 5  ¦ One may be inoperative provided       ¦

¦     Valve Lights          ¦    ¦    ¦ manifold pressure indicator is        ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Fuselage Duct       B ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦     Hot Warning Light     ¦    ¦    ¦     a) Both fuselage bleed air        ¦

¦                           ¦    ¦    ¦        valves are verified closed,    ¦

¦                           ¦    ¦    ¦        and                            ¦

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

¦                           ¦    ¦    ¦        known or forecast icing        ¦

¦                           ¦    ¦    ¦        conditions.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Pitot Heaters       B ¦ 2  ¦ 1  ¦ One may be inoperative for day VMC    ¦

¦                           ¦    ¦    ¦ provided aircraft is not operated     ¦

¦                           ¦    ¦    ¦ in visible moisture or known or       ¦

¦                           ¦    ¦    ¦ forecast icing conditions.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 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.  Electric Windshield B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦

¦     Heat (Does Not        ¦    ¦    ¦     a) Aircraft is not operated in    ¦

¦     Apply To Aft          ¦    ¦    ¦        known or forecast icing        ¦

¦     Stationary Panels)    ¦    ¦    ¦        conditions,                    ¦

¦                           ¦    ¦    ¦     b) Maximum speed is limited to    ¦

¦                           ¦    ¦    ¦        240 kts. IAS below 10,000      ¦

¦                           ¦    ¦    ¦        feet MSL, and                  ¦

¦                           ¦    ¦    ¦     c) The ECS System is operative.   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Windshield Wipers   B ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦

¦                           ¦    ¦    ¦ aircraft is not operated in           ¦

¦                           ¦    ¦    ¦ precipitation within 5 miles of the   ¦

¦                           ¦    ¦    ¦ airport of takeoff or intended        ¦

¦                           ¦    ¦    ¦ landing.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. Anti-Ice Manifold   B ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦     Leakage Test System   ¦    ¦    ¦ system operation is verified by       ¦

¦     (Accept Leak Light)   ¦    ¦    ¦ checking the manifold gauge and       ¦

¦                           ¦    ¦    ¦ verifing that leakage decay time is   ¦

¦                           ¦    ¦    ¦ within acceptable limits (from 24.5   ¦

¦                           ¦    ¦    ¦ PSI to 14.5 PSI in 8 or more          ¦

¦                           ¦    ¦    ¦ seconds).                             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Pitot Heat          B ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided:   ¦

¦     Annunciator Lights    ¦    ¦    ¦     a) Both heaters are verified      ¦

¦                           ¦    ¦    ¦        operative before each          ¦

¦                           ¦    ¦    ¦        departure.                     ¦

¦                           ¦    ¦    ¦          OR                           ¦

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

¦                           ¦    ¦    ¦        visible moisture, and          ¦

¦                           ¦    ¦    ¦     c) 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: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 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 with Sweep   D ¦ -  ¦ 1  ¦ Any in excess of those required by    ¦

¦     Second Hand (Or       ¦    ¦    ¦ FAR may be inoperative.               ¦

¦     Equivalent)           ¦    ¦    ¦                                       ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦                           ¦    ¦    ¦ operations are conducted under VFR    ¦

¦                           ¦    ¦    ¦ only.                                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Digital Flight      A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦

¦ *** Data Recorder         ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR)   ¦

¦     System (DFDRS)        ¦    ¦    ¦        operates normally,             ¦

¦                           ¦    ¦    ¦     b) Airplane is not dispatched     ¦

¦                           ¦    ¦    ¦        from a designated airport      ¦

¦                           ¦    ¦    ¦        where repairs or               ¦

¦                           ¦    ¦    ¦        replacements can be made,      ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     c) Repairs are made within        ¦

¦                           ¦    ¦    ¦        threee flight days.            ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 32-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Air Brake Pressure  C ¦ 2  ¦ 1  ¦ (M)May be inoperative provided        ¦

¦     Indicator             ¦    ¦    ¦ Cockpit Indicator is operative.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 33-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Cockpit and         C ¦ -  ¦ -  ¦ May be inoperative provided:          ¦

¦     Instrument Lighting   ¦    ¦    ¦     a) Flight Station Lighting on     ¦

¦     Systems               ¦    ¦    ¦        Essential Busses is            ¦

¦                           ¦    ¦    ¦        operative,                     ¦

¦                           ¦    ¦    ¦     b) Sufficient lighting is         ¦

¦                           ¦    ¦    ¦        operative to make each         ¦

¦                           ¦    ¦    ¦        instrument, control, and       ¦

¦                           ¦    ¦    ¦        other device for which it is   ¦

¦                           ¦    ¦    ¦        provided easily readable,      ¦

¦                           ¦    ¦    ¦     c) Direct rays and reflections    ¦

¦                           ¦    ¦    ¦        do not impair visibility       ¦

¦                           ¦    ¦    ¦        either inside or outside the   ¦

¦                           ¦    ¦    ¦        aircraft,                      ¦

¦                           ¦    ¦    ¦     d) Lighting intensity can be      ¦

¦                           ¦    ¦    ¦        controlled or is preset to a   ¦

¦                           ¦    ¦    ¦        satisfactory level for the     ¦

¦                           ¦    ¦    ¦        expected flight conditions,    ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     e) Lighting configuration at      ¦

¦                           ¦    ¦    ¦        dispatch is acceptable to      ¦

¦                           ¦    ¦    ¦        the flight crew.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Cabin Interior      C ¦ -  ¦ -  ¦ May be inoperative provided:          ¦

¦     Illumination System   ¦    ¦    ¦     a) Cabin Emergency Lighting is    ¦

¦                           ¦    ¦    ¦        operative,                     ¦

¦                           ¦    ¦    ¦     b) Sufficient lighting is         ¦

¦                           ¦    ¦    ¦        operative for the crew to      ¦

¦                           ¦    ¦    ¦        perform required duties, and   ¦

¦                           ¦    ¦    ¦     c) Lighting configuration at      ¦

¦                           ¦    ¦    ¦        dispatch is acceptable to      ¦

¦                           ¦    ¦    ¦        flight crew.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 33-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Anti-Collision      C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦

¦     Beacon Lights         ¦    ¦    ¦     a) A Strobe Light System          ¦

¦                           ¦    ¦    ¦        meeting the requirements of    ¦

¦                           ¦    ¦    ¦        FAR 25.1401 (Anti-Collision    ¦

¦                           ¦    ¦    ¦        Beacon System) is installed    ¦

¦                           ¦    ¦    ¦        and operative.                 ¦

¦                           ¦    ¦    ¦            OR                         ¦

¦                         C ¦    ¦    ¦     b) Aircraft is not operated at    ¦

¦                           ¦    ¦    ¦        night.                         ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Landing Lights      C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦

¦                           ¦    ¦    ¦ aircraft has dual taxi lights         ¦

¦                           ¦    ¦    ¦ installed and both are operative.     ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Taxi Lights         C ¦ 2  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Position Lights     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 34-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Standby Attitude    C ¦ 1  ¦ 0  ¦ May be inoperative for day VMC        ¦

¦ *** Gyro (Third           ¦    ¦    ¦ operations only.                      ¦

¦     Indicator)            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Turn & Bank         C ¦ 2  ¦ 1  ¦ One may be inoperative for day VMC    ¦

¦ *** Indicators            ¦    ¦    ¦ operations only.                      ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ independent attitude indicators are   ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Compass System      D ¦ -  ¦ 2  ¦ May be inoperative provided:          ¦

¦     Sensors               ¦    ¦    ¦     a) Both Pilot's Directional       ¦

¦     (Directional Gyro,    ¦    ¦    ¦        Compass Systems are            ¦

¦     AHRS, IRS, etc.)      ¦    ¦    ¦        operative from independent     ¦

¦                           ¦    ¦    ¦        sources, and                   ¦

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

¦                           ¦    ¦    ¦        independent heading            ¦

¦                           ¦    ¦    ¦        indications.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Non-Stabilized      B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided any    ¦

¦     Magnetic Compass      ¦    ¦    ¦ combination of three gyro or INS      ¦

¦                           ¦    ¦    ¦ (IRU) stabilized compass systems      ¦

¦                           ¦    ¦    ¦ operate normally.                     ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦     a) Any combination of two gyro    ¦

¦                           ¦    ¦    ¦        stabilized compass systems     ¦

¦                           ¦    ¦    ¦        are operative, and             ¦

¦                           ¦    ¦    ¦     b) Airplane is operated with      ¦

¦                           ¦    ¦    ¦        dual independent navigation    ¦

¦                           ¦    ¦    ¦        capability and under           ¦

¦                           ¦    ¦    ¦        positive radar control by      ¦

¦                           ¦    ¦    ¦        ATC during the enroute         ¦

¦                           ¦    ¦    ¦        flight phase.                  ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 34-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Non-Stabilized        ¦    ¦    ¦                                       ¦

¦     Magnetic Compass      ¦    ¦    ¦                                       ¦

¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         B ¦ 1  ¦ 0  ¦ (O)May be inoperative for flights     ¦

¦                           ¦    ¦    ¦ that are entirely within areas of     ¦

¦                           ¦    ¦    ¦ magnetic unreliability provided at    ¦

¦                           ¦    ¦    ¦ least two stabilized directional      ¦

¦                           ¦    ¦    ¦ gyro systems are installed,           ¦

¦                           ¦    ¦    ¦ operative, and used in conjunction    ¦

¦                           ¦    ¦    ¦ with approved free gyro navigation    ¦

¦                           ¦    ¦    ¦ techniques.                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Flight Director     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦ *** System                ¦    ¦    ¦ approach minimums do not require      ¦

¦                           ¦    ¦    ¦ its use.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Distance Measuring  C ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Marker Beacon       C ¦ -  ¦ 0  ¦ May be inoperative provided           ¦

¦     Systems               ¦    ¦    ¦ approach minimums do not require      ¦

¦                           ¦    ¦    ¦ its use.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Long Range          C ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦ *** Navigation Systems    ¦    ¦    ¦ FAR may be inoperative.               ¦

¦     (INS, LORAN, GPS,     ¦    ¦    ¦                                       ¦

¦     etc.)                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Weather Radar       C ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦ ***                       ¦    ¦    ¦ FAR may be inoperative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 10. Radio Compass       C ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦     (ADF) System          ¦    ¦    ¦ FAR may be inoperative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 11. VHF Navigation      C ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦     Systems (VOR/ILS)     ¦    ¦    ¦ FAR may be inoperative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 34-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. ATC Transponders/   C ¦ -  ¦ -  ¦ As required by FAR.                   ¦

¦     Automatic Altitude    ¦    ¦    ¦                                       ¦

¦     Reporting System      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦

¦                           ¦    ¦    ¦ FAR may be inoperative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Ground Proximity      ¦    ¦    ¦                                       ¦

¦ *** Warning System        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦      1) Modes 1-4       A ¦ -  ¦ 0  ¦ (O)May be inoperative 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:          ¦

¦         Function          ¦    ¦    ¦     a) GPWS is considered             ¦

¦                           ¦    ¦    ¦        inoperative, and               ¦

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

¦                           ¦    ¦    ¦        flight days.                   ¦

¦                           ¦    ¦    ¦                                       ¦

¦      3) Glideslope      B ¦ 2  ¦ 0  ¦                                       ¦

¦         Deviation         ¦    ¦    ¦                                       ¦

¦         Lights (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.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ *** 6) Enhanced GPWS    C ¦ -  ¦ 0  ¦                                       ¦

¦        (TAWS)             ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 34-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Traffic Collision     ¦    ¦    ¦                                       ¦

¦ *** and Avoidance         ¦    ¦    ¦                                       ¦

¦     System (TCAS)         ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) TCAS System      C ¦ -  ¦ 0  ¦ (M)May be inoperative provided the    ¦

¦                           ¦    ¦    ¦ system is deactivated and secured.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***  2) Combined TA     C ¦ 2  ¦ 1  ¦ (O)One may be inoperative on the      ¦

¦         and RA Dual       ¦    ¦    ¦ non-flying pilot side provided TA     ¦

¦         Displays          ¦    ¦    ¦ and RA elements and audio functions   ¦

¦                           ¦    ¦    ¦ are operative on the flying pilot     ¦

¦                           ¦    ¦    ¦ side.                                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦      3) Resolution      C ¦ -  ¦ 0  ¦ (O)One may be inoperative on the      ¦

¦         Advisory (RA)     ¦    ¦    ¦ non-flying pilot side.                ¦

¦         Display           ¦    ¦    ¦                                       ¦

¦         System(s)         ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦     a) All Traffic Alert (TA)         ¦

¦                           ¦    ¦    ¦        display elements and voice     ¦

¦                           ¦    ¦    ¦        command audio functions are    ¦

¦                           ¦    ¦    ¦        operative, and                 ¦

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

¦                           ¦    ¦    ¦        the crew.                      ¦

¦                           ¦    ¦    ¦                                       ¦

¦     4) TA Display       C ¦ -  ¦ 0  ¦ (O)May be inoperative provided all    ¦

¦        System(s)          ¦    ¦    ¦ installed RA displays and audio       ¦

¦                           ¦    ¦    ¦ functions are operative.              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Altitude Alerting/  A ¦ -  ¦ 0  ¦ (O)Except where enroute operations    ¦

¦     Pre-selector System   ¦    ¦    ¦ require their use, may be             ¦

¦                           ¦    ¦    ¦ inoperative provided:                 ¦

¦                           ¦    ¦    ¦     a) Autopilot with altitude hold   ¦

¦                           ¦    ¦    ¦        is operative, and              ¦

¦                           ¦    ¦    ¦     b) Repairs are made within        ¦

¦                           ¦    ¦    ¦        three flight days.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 34-5     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 16. Radio Altimeter     A ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦    (Radar Altimeter)      ¦    ¦    ¦     a) Dispatch deviation for GPWS    ¦

¦                           ¦    ¦    ¦        is observed,                   ¦

¦                           ¦    ¦    ¦     b) Approach minimums or           ¦

¦                           ¦    ¦    ¦        operating procedures do not    ¦

¦                           ¦    ¦    ¦        require its use, and           ¦

¦                           ¦    ¦    ¦     c) Repairs are made within        ¦

¦                           ¦    ¦    ¦        three flight days.             ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 17.  Traffic Collision  C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦ ***  Avoidance and        ¦    ¦    ¦ system is secured.                    ¦

¦      Detection (TCAD)     ¦    ¦    ¦                                       ¦

¦      System               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 18.  Flight Watch       D ¦ 1  ¦ 0  ¦                                       ¦

¦ *** (Tracker) System      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 19.  Angle of Attack    D ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦ *** (AOA) System          ¦    ¦    ¦ system is secured.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 35-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 35  OXYGEN                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Crew Portable       D ¦ -  ¦ 0  ¦ Any in excess of those required by    ¦

¦     Oxygen System         ¦    ¦    ¦ FAR may be inoperative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 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  ¦ (M)May be inoperative provided APU    ¦

¦     Unit (APU)            ¦    ¦    ¦ is secured by an acceptable           ¦

¦                           ¦    ¦    ¦ procedure.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) APU Generator    C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦

¦                           ¦    ¦    ¦ Generator is secured by an            ¦

¦                           ¦    ¦    ¦ acceptable procedure.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) APU Bleed Air    C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦

¦                           ¦    ¦    ¦ APU Bleed valve remains closed.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  APU Advisory          ¦    ¦    ¦                                       ¦

¦     Lights                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Doors Open       C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦

¦                           ¦    ¦    ¦ Exhaust Door is verified closed.      ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Generator Off    C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦

¦                           ¦    ¦    ¦ Generator is considered inop-         ¦

¦                           ¦    ¦    ¦ erative.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦     3) Armed            C ¦ 1  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  APU Exhaust           ¦    ¦    ¦                                       ¦

¦     Door System           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Failed Closed    C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided APU    ¦

¦                           ¦    ¦    ¦ is not used.                          ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Failed Open      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦                           ¦    ¦    ¦ operations are limited to 225 KIAS    ¦

¦                           ¦    ¦    ¦ or less.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 52-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 52  DOORS                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Main Cabin Door     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦

¦     Caution Light         ¦    ¦    ¦ Door(s) are verified closed prior     ¦

¦     System                ¦    ¦    ¦ to each departure.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 61-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 61  PROPELLERS            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Propeller             ¦    ¦    ¦                                       ¦

¦     Synchronizing         ¦    ¦    ¦                                       ¦

¦     System                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Synchronizing/   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦

¦        Syncrophase        ¦    ¦    ¦ switch(s) remain in the OFF           ¦

¦        Function           ¦    ¦    ¦ position.                             ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 73-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 73  ENGINE FUEL & CONTROL ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Temperature Datum   C ¦ 4  ¦ 0  ¦ (M)May be inoperative provided:       ¦

¦     System                ¦    ¦    ¦     a) Associated Fuel Flow and TIT   ¦

¦                           ¦    ¦    ¦        indicating systems are         ¦

¦                           ¦    ¦    ¦        operative, and                 ¦

¦                           ¦    ¦    ¦     b) Associated TD control valve    ¦

¦                           ¦    ¦    ¦        switch remains in null.        ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Fuel Flow           B ¦ 4  ¦ 3  ¦ One may be inoperative provided:      ¦

¦     Indicators            ¦    ¦    ¦     a) Associated Engine              ¦

¦                           ¦    ¦    ¦        Instruments are operative,     ¦

¦                           ¦    ¦    ¦        and                            ¦

¦                           ¦    ¦    ¦     b) All Fuel Quantity Indicators   ¦

¦                           ¦    ¦    ¦        are operative.                 ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Fuel Flow           A ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦     Indicators            ¦    ¦    ¦     a) All remaining Engine           ¦

¦     Power Supply          ¦    ¦    ¦        Instruments are operative,     ¦

¦                           ¦    ¦    ¦     b) All Fuel Low Pressure Lights   ¦

¦                           ¦    ¦    ¦        are verified Out after         ¦

¦                           ¦    ¦    ¦        engine start and are           ¦

¦                           ¦    ¦    ¦        monitored during flight,       ¦

¦                           ¦    ¦    ¦     c) All fuel quantity indicators   ¦

¦                           ¦    ¦    ¦        are operative, 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: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 74-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 74  IGNITION              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Speed Sensitive     A ¦ 4  ¦ 3  ¦ (M)(O)One may be inoperative          ¦

¦     Control (65%          ¦    ¦    ¦ provided:                             ¦

¦     Switch)               ¦    ¦    ¦     a) It is verified to be the       ¦

¦                           ¦    ¦    ¦        65% Switch by an acceptable    ¦

¦                           ¦    ¦    ¦        procedure, and                 ¦

¦                           ¦    ¦    ¦     b) Repairs are made within one    ¦

¦                           ¦    ¦    ¦        flight day.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 77-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  TIT Indicators      B ¦ 4  ¦ 0  ¦                                       ¦

¦ *** (Digital Function)    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Torque (Horse-      A ¦ 4  ¦ 3  ¦ (M)One may be inoperative provided:   ¦

¦     power) Indicators     ¦    ¦    ¦     a) Associated fuel flow, TIT,     ¦

¦                           ¦    ¦    ¦        and tachometer indicating      ¦

¦                           ¦    ¦    ¦        systems are operative, and     ¦

¦                           ¦    ¦    ¦     b) Repairs are made within one    ¦

¦                           ¦    ¦    ¦        flight day.                    ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦

¦                   P-3                    ¦                       ¦          ¦

¦                                          ¦ DATE: 01/15/2003      ¦ 79-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 79  ENGINE OIL            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Engine Oil          B ¦ 4  ¦ 2  ¦ May be inoperative provided the       ¦

¦     Pressure Caution      ¦    ¦    ¦ associated Power Section and Gear     ¦

¦     Lights                ¦    ¦    ¦ Box Oil Pressure Indicators are       ¦

¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Oil Quantity        B ¦ 4  ¦ 2  ¦ (M)May be inoperative provided:       ¦

¦     Indicators            ¦    ¦    ¦     a) Associated Power Section       ¦

¦                           ¦    ¦    ¦        and Gear Box Oil Pressure      ¦

¦                           ¦    ¦    ¦        Indicators are operative,      ¦

¦                           ¦    ¦    ¦     b) Associated Oil                 ¦

¦                           ¦    ¦    ¦        Temperature Indicators are     ¦

¦                           ¦    ¦    ¦        operative,                     ¦

¦                           ¦    ¦    ¦     c) Associated Low Pressure        ¦

¦                           ¦    ¦    ¦        Warning Lights are             ¦

¦                           ¦    ¦    ¦        operative,                     ¦

¦                           ¦    ¦    ¦     d) There is no evidence of        ¦

¦                           ¦    ¦    ¦        above normal oil consumption   ¦

¦                           ¦    ¦    ¦        or leakage, and                ¦

¦                           ¦    ¦    ¦     e) Associated Oil Quantity        ¦

¦                           ¦    ¦    ¦        is verified adequate before    ¦

¦                           ¦    ¦    ¦        each departure.                ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Oil Cooler          A ¦ 4  ¦ 0  ¦ (O)May be inoperative provided:       ¦

¦     Inducers              ¦    ¦    ¦     a) Associated Oil Temperature     ¦

¦                           ¦    ¦    ¦        Indicator is operative,        ¦

¦                           ¦    ¦    ¦     b) Oil Temperature is closely     ¦

¦                           ¦    ¦    ¦        monitored during ground        ¦

¦                           ¦    ¦    ¦        operations, and                ¦

¦                           ¦    ¦    ¦     c) Repairs are made within        ¦

¦                           ¦    ¦    ¦        three flight days              ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Oil Cooler Flap     C ¦ 4  ¦ 2  ¦ May be inoperative provided the       ¦

¦     Position Indicator    ¦    ¦    ¦ associated Oil Temperature            ¦

¦                           ¦    ¦    ¦ Indicator is operative.               ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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