DEPARTMENT OF TRANSPORTATION     Revision: 5

                                                           Date: 12/27/1995

                         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

 

                        ************************************

                        *   FOR PART 91 OPERATIONS ONLY!   *

                        ************************************

 

                              Grumman G-159 Models

 

 

 

 

 

 

 

 

 

 

 

 

 

                         Federal Aviation Administration

                         Flight Standards Division

                         AIRCRAFT EVALUATION GROUP, LGB AEG

                         3960 PARAMOUNT BLVD.

                         LAKEWOOD, CA 90712-4137

 

 

                         TELEPHONE:  (310) 627-5272

                               FAX:  (310) 627-5281


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 5

                        MASTER MINIMUM EQUIPMENT LIST      Date: 12/27/1995

 

 

                                   G-159

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I

         --     Log of Revisions                        II

         --     Control Page                            III, IV

         --     Highlights of Change                    V

         --     Definitions                             VI, VII, VIII, IX

         --     Definitions                             X, XI, XII, XIII

         --     Preamble                                XIV, XV, XVI

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

         21     Air Conditioning                        21-6, 7

         22     Auto Flight                             22-1

         23     Communications                          23-1, 2, 3, 4

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

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

         26     Fire Protection                         26-1, 2, 3

         27     Flight Controls                         27-1

         28     Fuel                                    28-1, 2, 3

         29     Hydraulic Power                         29-1

         30     Ice and Rain Protection                 30-1, 2

         31     Indicating/Recording Systems            31-1

         32     Landing Gear                            32-1

         33     Lights                                  33-1, 2, 3, 4

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

         34     Navigation                              34-6, 7

         35     Oxygen                                  35-1

         49     Airborne Auxiliary Power                49-1, 2

         52     Doors                                   52-1

         61     Propellers                              61-1

         73     Engine Fuel & Control                   73-1

         77     Engine Indicating                       77-1

         79     Engine Oil                              79-1

         80     Starting                                80-1

         82     Water Injection                         82-1


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: II

                                                         Revision: 5

                        MASTER MINIMUM EQUIPMENT LIST    Date: 12/27/1995

 

 

                                   G-159

 

 

                               Log of Revisions

 

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                       FEDERAL AVIATION ADMINISTRATION     Page: III

                                                           Revision: 5

                        MASTER MINIMUM EQUIPMENT LIST      Date: 12/27/1995

 

 

                                   G-159

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       5        12/27/1995

         Table of Contents                        I       5        12/27/1995

         Log of Revisions                         II      5        12/27/1995

         Control Page                             III     5        12/27/1995

                                                  IV      5        12/27/1995

         Highlights of Change                     V       5        12/27/1995

         Definitions                              VI      6        01/31/1995

                                                  VII     6        01/31/1995

                                                  VIII    6        01/31/1995

                                                  IX      6        01/31/1995

                                                  X       6        01/31/1995

                                                  XI      6        01/31/1995

                                                  XII     6        01/31/1995

                                                  XIII    6        01/31/1995

         Preamble                                 XIV     1        07/05/1990

                                                  XV      1        07/05/1990

                                                  XVI     1        07/05/1990

         21                                       21-1    5        12/27/1995

                                                  21-2    5        12/27/1995

                                                  21-3    5        12/27/1995

                                                  21-4    5        12/27/1995

                                                  21-5    5        12/27/1995

                                                  21-6    5        12/27/1995

                                                  21-7    5        12/27/1995

         22                                       22-1    5        12/27/1995

         23                                       23-1    5        12/27/1995

                                                  23-2    5        12/27/1995

                                                  23-3    5        12/27/1995

                                                  23-4    5        12/27/1995

         24                                       24-1    5        12/27/1995

                                                  24-2    5        12/27/1995

                                                  24-3    5        12/27/1995

                                                  24-4    5        12/27/1995

         25                                       25-1    5        12/27/1995

                                                  25-2    5        12/27/1995

                                                  25-3    5        12/27/1995

                                                  25-4    5        12/27/1995

         26                                       26-1    5        12/27/1995

                                                  26-2    5        12/27/1995

                                                  26-3    5        12/27/1995


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IV

                                                           Revision: 5

                        MASTER MINIMUM EQUIPMENT LIST      Date: 12/27/1995

 

 

                                   G-159

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         27                                       27-1    5        12/27/1995

         28                                       28-1    5        12/27/1995

                                                  28-2    5        12/27/1995

                                                  28-3    5        12/27/1995

         29                                       29-1    5        12/27/1995

         30                                       30-1    5        12/27/1995

                                                  30-2    5        12/27/1995

         31                                       31-1    5        12/27/1995

         32                                       32-1    5        12/27/1995

         33                                       33-1    5        12/27/1995

                                                  33-2    5        12/27/1995

                                                  33-3    5        12/27/1995

                                                  33-4    5        12/27/1995

         34                                       34-1    5        12/27/1995

                                                  34-2    5        12/27/1995

                                                  34-3    5        12/27/1995

                                                  34-4    5        12/27/1995

                                                  34-5    5        12/27/1995

                                                  34-6    5        12/27/1995

                                                  34-7    5        12/27/1995

         35                                       35-1    5        12/27/1995

         49                                       49-1    5        12/27/1995

                                                  49-2    5        12/27/1995

         52                                       52-1    5        12/27/1995

         61                                       61-1    5        12/27/1995

         73                                       73-1    5        12/27/1995

         77                                       77-1    5        12/27/1995

         79                                       79-1    5        12/27/1995

         80                                       80-1    5        12/27/1995

         82                                       82-1    5        12/27/1995


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: V

                                                         Revision: 5

                        MASTER MINIMUM EQUIPMENT LIST    Date: 12/27/1995

 

 

                                   G-159

 

                            Highlights of Change

 

 

 

       EFFECTIVE ABOVE DATE, the Gulfstream G-159 Master Minimum Equipment List

       (MMEL) is revised. Revision 5 is a STANDARD revision which is the result

       of a public Flight Operations Evaluation Board (FOEB) meeting held on

       September 15, 1994 to consider approximately 400 proposals for MMEL

       relief. Many new items are given relief in this revision. Some relief

       that was granted in the past has been removed as a result of FAA policy

       changes since the last MMEL revision. FAA Policy Letters 1-78 and FAA

       Global Changes 2-26 have been reviewed and incorporated in this revision

       This revision also incorporates the four column MMEL format and Category

       A-D repair intervals.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

       1.   System Definitions.

 

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

       Specification Number 100 and items are numbered sequentially.

 

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

                      component, or function listed in the "Item"

                      column.

 

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

                      (quantity) of items normally installed in the

                      aircraft.  This number represents the aircraft

                      configuration considered in developing this MMEL.

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

                      cabin items) a number is not required.

                                                                            ¦

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

                      minimum number (quantity) of items required for

                      operation provided the conditions specified in

                      Column 4 are met.

 

       NOTE:  Where the MMEL shows a variable number required for

       dispatch, the MEL must reflect the actual number required for

       dispatch or an alternate means of configuration control approved

       by the Administrator.

 

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

                      includes a statement either prohibiting or

                      permitting operation with a specific number of

                      items inoperative, provisos (conditions and

                      limitations) for such operation, and appropriate

                      notes.

 

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

                      indicates a change, addition or deletion in the

                      adjacent text for the current revision of that

                      page only.  The change bar is dropped at the next

                      revision of that page.

 

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

       required for type certification and approved by the responsible

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

       the specific aircraft is listed on the applicable Type


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

       Certificate Data Sheet.

 

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

       certain provisions (restrictive or permissive) expressed in the

       Federal Aviation Regulations operating rules.  The number of

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

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

       specified by repair category.

 

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

       the crewmembers and maintenance personnel of the equipment

       condition.

 

       NOTE:  To the extent practical, placards should be located

       adjacent to the control or indicator for the item affected;

       however, unless otherwise specified, placard wording and location

       will be determined by the operator.

 

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

       number (quantity) of the item installed.

                                                                           ¦

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

       indicates that the item was previously listed but is now required

       to be operative if installed in the  aircraft.

 

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

       airplane which has a type design approval for ER operations and

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

 

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

       portions of the Federal Aviation Act and Federal Aviation

       Regulations.

 

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

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

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

       is initiated for the affected aircraft.

 

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

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

 

       11.  Alphabetical symbol in Column 4 indicates a proviso

       (condition or limitation) that must be complied with for


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

       operation with the  listed item inoperative.

 

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

       the extent that it does not accomplish its intended purpose

       and/or is not consistently functioning normally within its

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

 

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

       crewmember or maintenance consideration.  Notes are used to

       identify applicable material which is intended to assist with

       compliance, but do not relieve the operator of the responsibility

       for compliance with all applicable requirements.  Notes are not a

       part of the provisos.

 

       14.  Inoperative components of an inoperative system:

       Inoperative items which are components of a system which is

       inoperative are usually considered components directly associated

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

       (Warning/caution systems associated with the inoperative system

       must be operative unless relief is specifically authorized per

       the MMEL).

 

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

       maintenance procedure which must be accomplished prior to

       operation with the listed item inoperative.  Normally these

       procedures are accomplished by maintenance personnel;  however,

       other personnel may be qualified and authorized to perform

       certain functions.  Procedures requiring specialized knowledge or

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

       accomplished by maintenance personnel.  The satisfactory

       accomplishment of all maintenance procedures, regardless of

       who performs them, is the responsibility of the operator.

       Appropriate procedures are required to be published as part of

       the operator's manual or MEL.

 

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

       operations procedure which must be accomplished in planning for

       and/or operating with the listed item inoperative.  Normally

       these procedures are accomplished by the flight crew; however,

       other personnel may be qualified and authorized to perform

       certain functions.  The satisfactory accomplishment of all

       procedures, regardless of who performs them, is the

       responsibility of the operator.  Appropriate procedures are


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

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

       MEL.

 

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

       unless otherwise authorized by the Administrator.

 

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

       component must be put into an acceptable condition for safe

       flight.  An acceptable method of securing or deactivating will be

       established by the operator.

 

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

       This precludes a pilot from filing an Instrument Flight Rules

       (IFR) flight plan.

 

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

       atmospheric environment is such that would allow a flight to

       proceed under the visual flight rules applicable to the flight.

       This does not preclude operating under Instrument Flight Rules.

 

       20.  "Visible Moisture" means an atmospheric environment

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

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

       snow.

 

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

       passenger convenience, comfort or entertainment such as, but not

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

       equipment, overhead reading lamps, etc.

 

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

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

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

       to the repair times established by the following letter

       designators:

 

            Category A.  Items in this category shall be repaired within

       the time interval specified in the remarks column of the

       operator's approved MEL.

 

            Category B.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: X

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

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

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

       26th and end at midnight the 29th.

 

            Category C.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance

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

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

       26th and end at midnight February 5th.

 

            Category D.  Items in this category shall be repaired within

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

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

       aircraft maintenance log and/or record.

 

       The letter designators are inserted adjacent to Column 2.

 

       23. Electronic fault alerting system - General                  ¦

                                                                       ¦

       New generation aircraft display system fault indications to the ¦

       flight crew by use of computerized display systems.  Each       ¦

       aircraft manufacturer has incorporated individual design        ¦

       philosophies in determining the data that would be              ¦

       represented.  The following are customized definitions (specific¦

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

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

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

       23 for their aircraft, if appropriate.                          ¦

                                                                       ¦

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

                                                                       ¦

       Boeing airplanes equipped with Engine Indicating and Crew       ¦

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

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

       MAINTENANCE).  Any messages that affects airplane dispatch      ¦

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

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

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

       operating within its approved operating limits or tolerances.   ¦

                                                                       ¦

       System conditions that result only in a maintenance level       ¦

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


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

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

       addressed within an operators standard maintenance program.     ¦

                                                                       ¦

       b.   DOUGLAS  (MD-11)                                           ¦

                                                                       ¦

       Some Douglas aircraft are equipped with an alerting function    ¦

       which is a subsystem within the Electronic Instrument System    ¦

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

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

       STATUS).                                                        ¦

                                                                       ¦

       Alerts that affect aircraft dispatch will include WARNING,      ¦

       CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are   ¦

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

       maintenance heading.                                            ¦

                                                                       ¦

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

       system fault which can be identified by the Central Fault       ¦

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

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

       MEL must be verified for dispatch purposes.                     ¦

                                                                       ¦

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

                                                                       ¦

       Airbus aircraft equipped with Electronic Centralized Aircraft   ¦

       Monitoring (ECAM) provide different levels of system condition  ¦

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

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

                                                                       ¦

       Any message that effects airplane dispatchability will normally ¦

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

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

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

                                                                       ¦

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

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

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

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

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

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

       MAINTENANCE status messages do not affect dispatch.             ¦

 

       d.   FOKKER  (FK-100)                                           ¦


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

                                                                       ¦

       Fokker aircraft are equipped with Multi Function Display System ¦

       (MFDS) which provides electronic message referring to the       ¦

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

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

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

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

       verified for dispatch capability and maintenance may be         ¦

       required.                                                       ¦

                                                                       ¦

       System conditions that only require maintenance are not         ¦

       presented on the flight deck.  These maintenance                ¦

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

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

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

 

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

       operator in the MEL for tracking and informational purposes.  It

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

       Operations Inspector provided no relief is granted, or provided

       conditions and limitations are contained in an approved document

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

       If relief other than that granted by an approved document is

       sought for an administrative control item, a request must be

       submitted to the Administrator.  If the request results in review

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

       than an administrative control item.

 

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

       required by regulation but which may have been installed on some

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

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

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

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

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

       this policy nor the use of this symbol provide authority to

       install or remove an item from an aircraft.

 

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

       that are redundant to the requirements of the FARs.

 

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

       equipment/instrument malfunction was recorded in the aircraft


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                                   G-159

 

                                 Definitions

 

 

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

       calendar days or flight days specified in the MMEL for the

       repair of an inoperative item of equipment. This provision is

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

       D."

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XIV

                                                         Revision: 1

                        MASTER MINIMUM EQUIPMENT LIST    Date: 07/05/1990

 

 

                                   G-159

 

                                  Preamble

                             (Effective 7/5/90)

 

 

       This preamble is applicable to, and will be included in, master

       minimum equipment lists (MMEL) issued under the provisions of

       Section 91.30(a) ¢NEW Section 91.213(a)(2)|.  It is not

       applicable to MMEL's issued under the provisions of Parts 121,

       125, 129, and 135 of the FAR.

 

       Except as provided in Section 91.30(d) ¢NEW Section 91.213(d)|,

       or under the provisions of an approved MMEL, all equipment

       installed on an aircraft in compliance with the airworthiness

       standards or operating rules must be operative.  Experience has

       shown that with the various levels of redundancy designed into

       modern aircraft, operation of every system or component installed

       may not be necessary when the remaining equipment can provide an

       acceptable level of safety.

 

       An 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 only those items of

       equipment which the Administrator finds may be inoperative and

       yet maintain an acceptable level of safety by appropriate

       conditions and limitations.  The MMEL and FAA-issued letter of

       authorization are used as an MEL by an operator and permit

       operation of the aircraft with inoperative equipment.

 

       The MMEL includes all items of installed equipment that are

       permitted to be inoperative.  Equipment required by the FAR, and

       optional equipment in excess of FAR requirements, is included

       with appropriate conditions and limitations.  For each listed

       item, the installed equipment configuration considered to be

       normal for the aircraft is specified.  Items of equipment

       installed on aircraft (except for passenger convenience items

       such as galley equipment and passenger entertainment devices),

       such as "TCAS," windshear detection devices, and ground proximity

       warning systems (GPWS) that are in excess of what is required,

       and are not listed on the MMEL, must be operational for dispatch

       unless MMEL relief is sought through the FSDO having jurisdiction

       for the operator.  If MMEL relief is sought, the operator must

       notify the FSDO who will make a request of the FOEB to convene

       and consider adding the equipment to the MMEL.  The operator may

       then dispatch with the equipment disabled, or rendered


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XV

                                                         Revision: 1

                        MASTER MINIMUM EQUIPMENT LIST    Date: 07/05/1990

 

 

                                   G-159

 

                                  Preamble

                             (Effective 7/5/90)

 

       inoperative, in accordance with all FAR.  It is incumbent on the

       operator to endeavor to determine if O and/or M procedures for

       that equipment must be developed.  If so, any procedures

       developed must comply with all FAR.  Procedures developed to use

       the MMEL must not conflict with either the aircraft flight manual

       limitations, emergency procedures, or with airworthiness

       directives (AD), all of which take precedence over the MMEL and

       those procedures.  Suitable conditions and limitations in the

       form of placards, maintenance procedures, crew operating

       procedures, and other restrictions, as necessary, are required to

       be accomplished by the operator to ensure that an acceptable

       level of safety is maintained.  Those procedures should be

       developed from guidance provided in the manufacturer's aircraft

       flight and/or maintenance manuals, manufacturer's

       recommendations, engineering specifications, and other

       appropriate sources.  Procedures must not be contrary to any FAR.

       Wherever the statement "as required by FAR" appears in the MMEL,

       the operator must either list the specific FAR by part and

       section and carry the FAR on board the aircraft or specify the

       requirements and/or limitations to conduct the flight in

       accordance with the appropriate FAR.

 

       The MMEL is intended to permit operations with inoperative items

       of equipment for the minimum period of time necessary until

       repairs can be accomplished.  It is important that repairs be

       accomplished at the earliest opportunity in order to return the

       aircraft to its design level of safety and reliability.

       Inoperative equipment in all cases must be repaired, or inspected

       and deferred, by qualified maintenance personnel at the next

       required inspection ¢Section 91.165(c), NEW Section 91.405(c)|.

       The repair intervals indicated by the Letters A, B, and C

       inserted adjacent to column 2 are NOT applicable to this MMEL.

 

       The MMEL 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 records.  The item is then either repaired

       or deferred per the MMEL or other approved means acceptable to

       the Administrator prior to further operation.  In addition to the

       specific MMEL conditions and limitations, determination by the

       operator that the aircraft is in condition for safe operations

       under anticipated flight conditions must be made for all items of

       inoperative equipment.  When these requirements are met, the


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XVI

                                                         Revision: 1

                        MASTER MINIMUM EQUIPMENT LIST    Date: 07/05/1990

 

 

                                   G-159

 

                                  Preamble

                            (Effective  7/5/90)

 

       inoperative equipment.  When these requirements are met, the

       aircraft may be considered airworthy and returned to service.

       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 interrelationship between those items, and the effect on

       aircraft operation and crew workload, must be considered.

       Operators are expected to establish a controlled and sound repair

       program, including the parts, personnel, facilities, procedures,

       and schedules to ensure timely repair.

 

       WHEN USING THE MMEL, COMPLIANCE WITH THE STATED INTENT OF THE

       PREAMBLE, DEFINITIONS, CONDITIONS, AND LIMITATIONS SPECIFIED IN

       THE MMEL IS REQUIRED.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 21-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Cabin Blower          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Configuration     ¦    ¦    ¦     a) Blower Dump System is        ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     b) APU is operative, and        ¦ ¦

¦                           ¦    ¦    ¦     c) APU Air Load System is       ¦ ¦

¦                           ¦    ¦    ¦        operative.                   ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     d) Blower drive shaft is        ¦ ¦

¦                           ¦    ¦    ¦        removed,                     ¦ ¦

¦                           ¦    ¦    ¦     e) APU is operative, and        ¦ ¦

¦                           ¦    ¦    ¦     f) APU Air Load System is       ¦ ¦

¦                           ¦    ¦    ¦        operative.                   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Configuration     ¦    ¦    ¦     a) Blower Dump System is        ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

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

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     c) Blower drive shaft is        ¦ ¦

¦                           ¦    ¦    ¦        removed, and                 ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 21-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Cabin Pressure      C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  ¦ ¦

¦     Warning System        ¦    ¦    ¦     a) Cabin Altitude Indicator is  ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     b) Manual Pressure Control      ¦ ¦

¦                           ¦    ¦    ¦        System is operative.         ¦ ¦

¦                           ¦    ¦    ¦          OR                         ¦ ¦

¦                         C ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦     a) Cabin Differential Pressure  ¦ ¦

¦                           ¦    ¦    ¦        Indicator is operative, and  ¦ ¦

¦                           ¦    ¦    ¦     b) Manual Pressure Control      ¦ ¦

¦                           ¦    ¦    ¦        System is operative.         ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 21-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Cockpit Temperature C ¦ 4  ¦ 0  ¦ (O)All may be inoperative provided: ¦ ¦

¦     Control System &      ¦    ¦    ¦     a) Aircraft is operated in      ¦ ¦

¦     Cabin Temperature     ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦     Control Systems       ¦    ¦    ¦        and                          ¦ ¦

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

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦      1) Automatic       C ¦ 2  ¦ 0  ¦ Both Systems may be inoperative     ¦ ¦

¦         Systems           ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Associated Manual Control    ¦ ¦

¦                           ¦    ¦    ¦        System is operative, and     ¦ ¦

¦                           ¦    ¦    ¦     b) Cabin Temperature Indicator  ¦ ¦

¦                           ¦    ¦    ¦        is operative.                ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) Manual Systems  C ¦ 2  ¦ 0  ¦ Both Systems may be inoperative     ¦ ¦

¦                           ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦   a) Associated Automatic Control   ¦ ¦

¦                           ¦    ¦    ¦      System is operative, and       ¦ ¦

¦                           ¦    ¦    ¦   b) Cabin Temperature Indicator    ¦ ¦

¦                           ¦    ¦    ¦        is operative.                ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Cabin Pressure      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Differential          ¦    ¦    ¦     a) Cabin Altitude Indicator is  ¦ ¦

¦     Indicator             ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     b) A chart is provided for the  ¦ ¦

¦                           ¦    ¦    ¦        crew to convert Cabin        ¦ ¦

¦                           ¦    ¦    ¦        Altitude to Differential     ¦ ¦

¦                           ¦    ¦    ¦        Pressure.                    ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 21-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Blower Dump System    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Pressurized      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:     ¦ ¦

¦        Configuration      ¦    ¦    ¦     a) Spill valve is secured OPEN, ¦ ¦

¦                           ¦    ¦    ¦     b) APU is operative, and        ¦ ¦

¦                           ¦    ¦    ¦     c) APU Air Load System is       ¦ ¦

¦                           ¦    ¦    ¦        operative.                   ¦ ¦

¦                         C ¦    ¦    ¦           OR                        ¦ ¦

¦                           ¦    ¦    ¦     d) Blower drive shaft is        ¦ ¦

¦                           ¦    ¦    ¦        REMOVED,                     ¦ ¦

¦                           ¦    ¦    ¦     e) APU is operative, and        ¦ ¦

¦                           ¦    ¦    ¦     f) APU Air Load System is       ¦ ¦

¦                           ¦    ¦    ¦        operative.                   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦        Configuration      ¦    ¦    ¦     a) Spill valve is secured OPEN, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

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

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     c) Blower Drive Shaft is        ¦ ¦

¦                           ¦    ¦    ¦        removed, and                 ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Cockpit Temperature C ¦ 1  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦ *** Indicator             ¦    ¦    ¦     a) Cockpit Automatic            ¦ ¦

¦                           ¦    ¦    ¦        Temperature Control System   ¦ ¦

¦                           ¦    ¦    ¦        is operative, and            ¦ ¦

¦                           ¦    ¦    ¦     b) Cabin Temperature indicator  ¦ ¦

¦                           ¦    ¦    ¦        is operative.                ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Ground Cooling Fan  C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  ¦ ¦

¦     System                ¦    ¦    ¦     a) Ram Air Limiter doors are    ¦ ¦

¦                           ¦    ¦    ¦        secured in full OPEN         ¦ ¦

¦                           ¦    ¦    ¦        position, and                ¦ ¦

¦                           ¦    ¦    ¦     b) APU Air Load System is       ¦ ¦

¦                           ¦    ¦    ¦        utilized inflight only.      ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 21-5     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  Cabin Temperature   C ¦ 1  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦     Indicator             ¦    ¦    ¦     a) Cabin Automatic Temperature  ¦ ¦

¦                           ¦    ¦    ¦        Control System is operative, ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     b) Cabin Manual Temperature     ¦ ¦

¦                           ¦    ¦    ¦        Control System is operative. ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  Cooling Turbine     C ¦ 1  ¦ 0  ¦ (0)May be inoperative provided:     ¦ ¦

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

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦     b) Blower Dump System is        ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     c) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     d) Aircraft is operated in an   ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦     e) Blower drive shaft is        ¦ ¦

¦                           ¦    ¦    ¦        removed,                     ¦ ¦

¦                           ¦    ¦    ¦     f) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 Outflow Valve       C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  ¦ ¦

¦     System                ¦    ¦    ¦     a) Valve is secured OPEN,       ¦ ¦

¦                           ¦    ¦    ¦     b) Blower Dump System is        ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 21-6     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 Safety Valve        C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  ¦ ¦

¦                           ¦    ¦    ¦     a) Valve is secured OPEN,       ¦ ¦

¦                           ¦    ¦    ¦     b) Blower Dump System is        ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -12 Cabin Altitude      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Indication System     ¦    ¦    ¦     a) Cabin Differential Pressure  ¦ ¦

¦                           ¦    ¦    ¦        Indicator is operative, and  ¦ ¦

¦                           ¦    ¦    ¦     b) A chart is provided for the  ¦ ¦

¦                           ¦    ¦    ¦        crew to convert differential ¦ ¦

¦                           ¦    ¦    ¦        pressure to cabin altitude.  ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -13 Cabin Rate of Climb C ¦ 1  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦     Indication System     ¦    ¦    ¦     a) Cabin Altitude Indicator is  ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     b) Automatic Cabin Pressure     ¦ ¦

¦                           ¦    ¦    ¦        Control System is operative. ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 21-7     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -14 Automatic Cabin     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Pressure Control      ¦    ¦    ¦     a) Cabin Altitude Indicator is  ¦ ¦

¦     System                ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     b) Cabin Differential Pressure  ¦ ¦

¦                           ¦    ¦    ¦        Indicator is operative,      ¦ ¦

¦                           ¦    ¦    ¦     c) Cabin Rate of Climb          ¦ ¦

¦                           ¦    ¦    ¦        Indicator is operative, and  ¦ ¦

¦                           ¦    ¦    ¦     d) Cabin Pressure Warning       ¦ ¦

¦                           ¦    ¦    ¦        System is operative.         ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 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    C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided   ¦ ¦

¦ ***                       ¦    ¦    ¦ approach procedures do not require  ¦ ¦

¦                           ¦    ¦    ¦ its use.                            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Yaw Damper System   C ¦ 1  ¦ 0  ¦ (M)                                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Yaw Damper Engage   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided Yaw  ¦ ¦

¦ *** Indication System     ¦    ¦    ¦ Damper is considered inoperative.   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Electric Trim       C ¦ -  ¦ 0  ¦ (M)May be inoperative provided:     ¦ ¦

¦ *** Systems               ¦    ¦    ¦     a) System(s) are mechanically   ¦ ¦

¦                           ¦    ¦    ¦        and electrically locked out, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     b) All Mechanical Trim Systems  ¦ ¦

¦                           ¦    ¦    ¦        are operative.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Autopilot Engage    C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦ *** Indication System     ¦    ¦    ¦ autopilot system is also made       ¦ ¦

¦                           ¦    ¦    ¦ inoperative.                        ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 23-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Communication       C ¦ -  ¦ -  ¦ As required by FAR and no relief    ¦ ¦

¦     Systems (VHF, HF,     ¦    ¦    ¦ may be provided to an inoperative   ¦ ¦

¦     UHF)                  ¦    ¦    ¦ system or component if powered by   ¦ ¦

¦                           ¦    ¦    ¦ an emergency bus or equivalent and  ¦ ¦

¦                           ¦    ¦    ¦ required to accomplish an emergency ¦ ¦

¦                           ¦    ¦    ¦ procedure.                          ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Cockpit to Cockpit    ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Interphone System     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Cockpit Cabin         ¦    ¦    ¦                                       ¦

¦ *** Interphone Systems    ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦      1) Passenger       C ¦ -  ¦ 0  ¦ May be inoperative provided paging  ¦ ¦

¦         Configuration     ¦    ¦    ¦ (PA) system is operative on         ¦ ¦

¦                           ¦    ¦    ¦ passenger carrying flights.         ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦      2) Cargo           C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦         Configuration     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Passenger Address     ¦    ¦    ¦                                       ¦

¦     System                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦         Configuration     ¦    ¦    ¦     a) Alternate, normal and        ¦ ¦

¦                           ¦    ¦    ¦        emergency procedures and/or  ¦ ¦

¦                           ¦    ¦    ¦        operating restrictions are   ¦ ¦

¦                           ¦    ¦    ¦        established and used, and    ¦ ¦

¦                           ¦    ¦    ¦     b) Flight Deck/Cabin Interphone ¦ ¦

¦                           ¦    ¦    ¦        system operates normally.    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ ***  2) Cargo           D ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦         Configuration     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Cabin to Cabin      C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ *** Interphone System     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 23-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Prerecorded         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦ *** Passenger             ¦    ¦    ¦ alternate procedures are            ¦ ¦

¦     Announcement          ¦    ¦    ¦ established and used.               ¦ ¦

¦     Systems               ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Hand Held           C ¦ -  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦     Microphones           ¦    ¦    ¦     a) Each cockpit crewmember uses ¦ ¦

¦                           ¦    ¦    ¦        a boom microphone, and       ¦ ¦

¦                           ¦    ¦    ¦     b) Each (Control Wheel) Press-  ¦ ¦

¦                           ¦    ¦    ¦        to-Talk Switch is operative. ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 23-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  Boom Microphones      ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦ Cockpit Voice Recorder    ¦    ¦    ¦                                     ¦ ¦

¦ and Flight Data           ¦    ¦    ¦                                     ¦ ¦

¦ Recorder Installed        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦      1) Cockpit Voice   A ¦ -  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦         Recorder          ¦    ¦    ¦     a) Flight Data Recorder         ¦ ¦

¦         Equipped To       ¦    ¦    ¦        operates normally, and       ¦ ¦

¦         Record Boom       ¦    ¦    ¦     b) Repairs are made within      ¦ ¦

¦         Microphone per    ¦    ¦    ¦        three flight days.           ¦ ¦

¦         FAR 121.139(e),   ¦    ¦    ¦                                     ¦ ¦

¦         135.151(d) or     ¦    ¦    ¦                                     ¦ ¦

¦         125.227(e)        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦ ***  2) Cockpit Voice   D ¦ -  ¦ 0  ¦                                     ¦ ¦

¦         Recorder Not      ¦    ¦    ¦                                     ¦ ¦

¦         Equipped To       ¦    ¦    ¦                                     ¦ ¦

¦         Record Boom       ¦    ¦    ¦                                     ¦ ¦

¦         Microphone        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦ Cockpit Voice Recorder    ¦    ¦    ¦                                     ¦ ¦

¦ and NO Flight Data        ¦    ¦    ¦                                     ¦ ¦

¦ Recorder Installed        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦      1) Cockpit Voice   A ¦ -  ¦ 0  ¦ May be inoperative provided repairs ¦ ¦

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

¦         Equipped To       ¦    ¦    ¦                                     ¦ ¦

¦         Record Boom       ¦    ¦    ¦                                     ¦ ¦

¦         Microphone per    ¦    ¦    ¦                                     ¦ ¦

¦         FAR 121.139(e),   ¦    ¦    ¦                                     ¦ ¦

¦         135.151(d) or     ¦    ¦    ¦                                     ¦ ¦

¦         125.227(e)        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦ ***  2) Cockpit Voice   D ¦ -  ¦ 0  ¦                                     ¦ ¦

¦         Recorder Not      ¦    ¦    ¦                                     ¦ ¦

¦         Equipped To       ¦    ¦    ¦                                     ¦ ¦

¦         Record Boom       ¦    ¦    ¦                                     ¦ ¦

¦         Microphone        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 23-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  Selective Call      C ¦ -  ¦ 0  ¦ May be inoperative provided         ¦ ¦

¦ *** Systems (SEL/CAL)     ¦    ¦    ¦ procedures do not require its use.  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 Emergency Locator   C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦ *** Transmitters (ELT)    ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 Flitephone System   C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -12 Cockpit Speakers    C ¦ 2  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦                           ¦    ¦    ¦     a) Affected speaker is not      ¦ ¦

¦                           ¦    ¦    ¦        required for aural warnings, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     b) An operative headset is      ¦ ¦

¦                           ¦    ¦    ¦        provided for each person on  ¦ ¦

¦                           ¦    ¦    ¦        cockpit duty.                ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -13  Cockpit Voice        ¦    ¦    ¦                                     ¦ ¦

¦ ***  Recorder (CVR)       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        Flight Data      A ¦ 1  ¦ 0  ¦ (M)May be inoperative provided      ¦ ¦

¦        Recorder (FDR)     ¦    ¦    ¦ flight Data Recorder (FDR) is       ¦ ¦

¦        installed          ¦    ¦    ¦ operative.                          ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        NO Flight Data   A ¦ 1  ¦ 0  ¦ (M)May be inoperative provided      ¦ ¦

¦        Recorder (FDR)     ¦    ¦    ¦ repairs are made within three       ¦ ¦

¦        installed          ¦    ¦    ¦ flight days.                        ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 24-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Batteries           B ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦                           ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Aircraft is operated during  ¦ ¦

¦                           ¦    ¦    ¦        day VMC,                     ¦ ¦

¦                           ¦    ¦    ¦     b) There are no other           ¦ ¦

¦                           ¦    ¦    ¦        electrical power source      ¦ ¦

¦                           ¦    ¦    ¦        failures,                    ¦ ¦

¦                           ¦    ¦    ¦     c) Associated battery cables    ¦ ¦

¦                           ¦    ¦    ¦        are disconnected and         ¦ ¦

¦                           ¦    ¦    ¦        secured, and                 ¦ ¦

¦                           ¦    ¦    ¦     d) Associated battery           ¦ ¦

¦                           ¦    ¦    ¦        disconnect switch is pushed. ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  DC Generators       B ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦                           ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Generator drive shaft is     ¦ ¦

¦                           ¦    ¦    ¦        removed and generator is     ¦ ¦

¦                           ¦    ¦    ¦        reinstalled,                 ¦ ¦

¦                           ¦    ¦    ¦     b) Associated electrical cables ¦ ¦

¦                           ¦    ¦    ¦        are secured, and             ¦ ¦

¦                           ¦    ¦    ¦     c) APU Generator is operative.  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Alternators         B ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦                           ¦    ¦    ¦ provided:                           ¦ ¦

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

¦                           ¦    ¦    ¦        known of forecast icing      ¦ ¦

¦                           ¦    ¦    ¦        conditions,                  ¦ ¦

¦                           ¦    ¦    ¦     b) Alternator drive shaft is    ¦ ¦

¦                           ¦    ¦    ¦        removed and alternator is    ¦ ¦

¦                           ¦    ¦    ¦        reinstalled, and             ¦ ¦

¦                           ¦    ¦    ¦     c) Associated electrical cables ¦ ¦

¦                           ¦    ¦    ¦        are secured.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Main Inverters      C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦                           ¦    ¦    ¦ provided remaining inverter is      ¦ ¦

¦                           ¦    ¦    ¦ verified to power AC buses.         ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  E Inverter            ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 24-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  AC Voltmeter          ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Engine Generator      ¦    ¦    ¦                                     ¦ ¦

¦     D.C. Volt/Amp meter   ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦      1) Voltmeters      C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative          ¦ ¦

¦                           ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Associated Engine Generator  ¦ ¦

¦                           ¦    ¦    ¦        DC Ammeter is operative,     ¦ ¦

¦                           ¦    ¦    ¦     b) DC Bus Voltmeter is          ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     c) Associated Generator Off     ¦ ¦

¦                           ¦    ¦    ¦        Warning Light is operative.  ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦      2) Ammeters        C ¦ 2  ¦ 1  ¦ One may be inoperative provided     ¦ ¦

¦                           ¦    ¦    ¦ associated Engine Generator DC      ¦ ¦

¦                           ¦    ¦    ¦ voltmeter is operative.             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  DC Bus Voltmeter      ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  APU Generator       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided APU  ¦ ¦

¦     Ammeter               ¦    ¦    ¦ Generator is not used.              ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 APU Generator       C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  ¦ ¦

¦                           ¦    ¦    ¦     a) Both DC Generators are       ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     b) APU generator belt is        ¦ ¦

¦                           ¦    ¦    ¦        removed, and                 ¦ ¦

¦                           ¦    ¦    ¦     c) Associated electrical cables ¦ ¦

¦                           ¦    ¦    ¦        are secured.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 "C" Inverter        D ¦ 1  ¦ 0  ¦ (M)                                 ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -12 Frequency Meter     C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ *** System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 24-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -13 Alternator/Overheat C ¦ 2  ¦ 1  ¦ (O)(M)One may be inoperative        ¦ ¦

¦     Warning Systems       ¦    ¦    ¦ provided:                           ¦ ¦

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

¦                           ¦    ¦    ¦        known or forecast icing      ¦ ¦

¦                           ¦    ¦    ¦        conditions,                  ¦ ¦

¦                           ¦    ¦    ¦     b) Associated Alternator drive  ¦ ¦

¦                           ¦    ¦    ¦        shaft is removed and         ¦ ¦

¦                           ¦    ¦    ¦        alternator is reinstalled,   ¦ ¦

¦                           ¦    ¦    ¦     c) Associated electrical cables ¦ ¦

¦                           ¦    ¦    ¦        are secured, and             ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -14 Battery Temperature   ¦    ¦    ¦                                     ¦ ¦

¦ *** Monitor Systems       ¦    ¦    ¦                                     ¦ ¦

¦     (Indicator &          ¦    ¦    ¦                                     ¦ ¦

¦     Caution Light)        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦     Nicad Batteries     C ¦ -  ¦ -  ¦ (M)(O)One may be inoperative        ¦ ¦

¦     Installed             ¦    ¦    ¦ provided associated Battery is      ¦ ¦

¦                           ¦    ¦    ¦ electrically disconnected and       ¦ ¦

¦                           ¦    ¦    ¦ secured.                            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -15 DC Generator        C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦     Overheat Warning      ¦    ¦    ¦ provided:                           ¦ ¦

¦     Lights                ¦    ¦    ¦     a) Affected Generator drive     ¦ ¦

¦                           ¦    ¦    ¦        shaft is removed and         ¦ ¦

¦                           ¦    ¦    ¦        generator is reinstalled,    ¦ ¦

¦                           ¦    ¦    ¦     b) Associated electrical cables ¦ ¦

¦                           ¦    ¦    ¦        are secured, and             ¦ ¦

¦                           ¦    ¦    ¦     c) APU Generator is operative.  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 24-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -16 Battery Monitor       ¦    ¦    ¦                                     ¦ ¦

¦ *** System Ammeters       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦     Nicad Batteries     C ¦ 2  ¦ 0  ¦ Both may be inoperative provided:   ¦ ¦

¦     Installed             ¦    ¦    ¦     a) Essential D.C. Voltmeter is  ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     b) Associated Battery Fail      ¦ ¦

¦                           ¦    ¦    ¦        Lights are operative, and    ¦ ¦

¦                           ¦    ¦    ¦     c) Battery Disconnect Lights    ¦ ¦

¦                           ¦    ¦    ¦        are operative.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -17 Generator Off       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided: ¦ ¦

¦     Lights                ¦    ¦    ¦     a) Associated Engine Generator  ¦ ¦

¦                           ¦    ¦    ¦        D.C. Voltmeter is operative, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     b) Associated Engine Generator  ¦ ¦

¦                           ¦    ¦    ¦        D.C. Ammeter is operative.   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -18 Alternator Off      C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided  ¦ ¦

¦     Lights                ¦    ¦    ¦ Engine Driven Alternator A.C.       ¦ ¦

¦                           ¦    ¦    ¦ Voltmeter is operative.             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -19 External Power      C ¦ 1  ¦ 0  ¦ (M)                                 ¦ ¦

¦     System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 25-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Crash Axe           B ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  First Aid Kits      D ¦ -  ¦ -  ¦ Any in excess or those required by  ¦ ¦

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

¦                           ¦    ¦    ¦ provided required distribution is   ¦ ¦

¦                           ¦    ¦    ¦ maintained.                         ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Hand Fire             ¦    ¦    ¦ Moved to Chapter 26, Rev. 5.        ¦ ¦

¦     Extinguisher          ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Overwater Equipment C ¦ -  ¦ -  ¦ As required by FARs.                ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Passenger Seats     C ¦ -  ¦ 0  ¦ (M)May be inoperative provided the  ¦ ¦

¦                           ¦    ¦    ¦ following are accomplished using an ¦ ¦

¦                           ¦    ¦    ¦ approved maintenance procedure:     ¦ ¦

¦                           ¦    ¦    ¦     a) Appropriately secure or stow ¦ ¦

¦                           ¦    ¦    ¦        affected seat so that it     ¦ ¦

¦                           ¦    ¦    ¦        does not block egress to an  ¦ ¦

¦                           ¦    ¦    ¦        aisle or exit, and           ¦ ¦

¦                           ¦    ¦    ¦     b) Ensure that affected Seat is ¦ ¦

¦                           ¦    ¦    ¦        blocked and placarded "DO    ¦ ¦

¦                           ¦    ¦    ¦        NOT OCCUPY".                 ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦                           ¦    ¦    ¦          seatbelt is considered to  ¦ ¦

¦                           ¦    ¦    ¦          be inoperative.            ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦                           ¦    ¦    ¦          recline mechanism is       ¦ ¦

¦                           ¦    ¦    ¦          considered inoperative if  ¦ ¦

¦                           ¦    ¦    ¦          the seat cannot be secured ¦ ¦

¦                           ¦    ¦    ¦          in the upright position.   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Crewmember Shoulder B ¦ -  ¦ -  ¦ Any in excess of those required for ¦ ¦

¦     Harnesses             ¦    ¦    ¦ flight deck crew members (including ¦ ¦

¦                           ¦    ¦    ¦ official observer in observer seat) ¦ ¦

¦                           ¦    ¦    ¦ may be inoperative.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 25-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Observer Seat(s)      ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        1) Primary       A ¦ -  ¦ -  ¦ May be inoperative provided:        ¦ ¦

¦           Observer Seat   ¦    ¦    ¦     a) A passenger seat in          ¦ ¦

¦           (including      ¦    ¦    ¦        passenger cabin is available ¦ ¦

¦           associated      ¦    ¦    ¦        to an FAA inspector for      ¦ ¦

¦           equipment)      ¦    ¦    ¦        performance of official      ¦ ¦

¦                           ¦    ¦    ¦        duties, and                  ¦ ¦

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

¦                           ¦    ¦    ¦        flight days.                 ¦ ¦

¦                           ¦    ¦    ¦          OR                         ¦ ¦

¦                         A ¦    ¦    ¦     c) The secondary observer's     ¦ ¦

¦                           ¦    ¦    ¦        seat is available to the FAA ¦ ¦

¦                           ¦    ¦    ¦        inspector for the            ¦ ¦

¦                           ¦    ¦    ¦        performance of official      ¦ ¦

¦                           ¦    ¦    ¦        duties, and                  ¦ ¦

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

¦                           ¦    ¦    ¦        flight days.                 ¦ ¦

¦                           ¦    ¦    ¦          OR                         ¦ ¦

¦                         A ¦    ¦    ¦     e) The primary 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      ¦ ¦

¦                           ¦    ¦    ¦     f) Repairs are made within two  ¦ ¦

¦                           ¦    ¦    ¦        flight days.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦       (continued)                   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 25-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Observer Seat(s)      ¦    ¦    ¦                                     ¦ ¦

¦     (cont'd)              ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦           Observer Seat   ¦    ¦    ¦          intended to provide for    ¦ ¦

¦           (including      ¦    ¦    ¦          occupancy of the above     ¦ ¦

¦           associated      ¦    ¦    ¦          seats by an FAA inspector  ¦ ¦

¦           equipment)      ¦    ¦    ¦          when the minimum safety    ¦ ¦

¦           (cont'd.)       ¦    ¦    ¦          equipment (oxygen and      ¦ ¦

¦                           ¦    ¦    ¦          safety belt) is functional ¦ ¦

¦                           ¦    ¦    ¦          and the inspector          ¦ ¦

¦                           ¦    ¦    ¦          determines the conditions  ¦ ¦

¦                           ¦    ¦    ¦          to be acceptable.          ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦                           ¦    ¦    ¦          determine if the minimum   ¦ ¦

¦                           ¦    ¦    ¦          safety equipment is        ¦ ¦

¦                           ¦    ¦    ¦          functional for other       ¦ ¦

¦                           ¦    ¦    ¦          persons authorized to      ¦ ¦

¦                           ¦    ¦    ¦          occupy any observer        ¦ ¦

¦                           ¦    ¦    ¦          seat(s).                   ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        2) Additional    D ¦ -  ¦ 0  ¦ May be inoperative.                 ¦ ¦

¦ ***       Observer        ¦    ¦    ¦                                     ¦ ¦

¦           Seat(s)         ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  "Fasten Seat Belt   C ¦ -  ¦ -  ¦ One or more signs or placards may   ¦ ¦

¦     While Seated" sign    ¦    ¦    ¦ be illegible or missing provided a  ¦ ¦

¦     or placards           ¦    ¦    ¦ legible sign or placard is readable ¦ ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 25-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  Passenger             ¦ -  ¦ 0  ¦ Passenger convenience items, as     ¦ ¦

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

¦                           ¦    ¦    ¦ related to passenger convenience,   ¦ ¦

¦                           ¦    ¦    ¦ comfort or entertainment such as,   ¦ ¦

¦                           ¦    ¦    ¦ but not limited to, galley          ¦ ¦

¦                           ¦    ¦    ¦ equipment, movie equipment, ash     ¦ ¦

¦                           ¦    ¦    ¦ trays, stereo equipment, overhead   ¦ ¦

¦                           ¦    ¦    ¦ reading lamps, etc.  Items          ¦ ¦

¦                           ¦    ¦    ¦ addressed elsewhere in this         ¦ ¦

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

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

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

¦                           ¦    ¦    ¦ appropriate document.               ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦ NOTE:  LAVATORY DOOR ASHTRAYS ARE   ¦ ¦

¦                           ¦    ¦    ¦ NOT CONSIDERED CONVENIENCE ITEMS.   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 Megaphones          B ¦ -  ¦ 0  ¦ Any in excess of those required by  ¦ ¦

¦ ***                       ¦    ¦    ¦ FAR may be inoperative or missing   ¦ ¦

¦                           ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Inoperative megaphone is     ¦ ¦

¦                           ¦    ¦    ¦        removed from passenger       ¦ ¦

¦                           ¦    ¦    ¦        cabin, and                   ¦ ¦

¦                           ¦    ¦    ¦     b) Required distribution is     ¦ ¦

¦                           ¦    ¦    ¦        maintained.                  ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦                           ¦    ¦    ¦        operations.                  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 Flotation Devices   C ¦ -  ¦ -  ¦ Any in excess of those required by  ¦ ¦

¦                           ¦    ¦    ¦ FAR may be inoperative.             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 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   ¦ ¦

¦     System                ¦    ¦    ¦ APU is not used.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Fire Extinguishing    ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     System Engines        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  APU Fire            C ¦ -  ¦ -  ¦ (O)May be inoperative provided APU  ¦ ¦

¦     Extinguishing         ¦    ¦    ¦ is not used.                        ¦ ¦

¦     System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Rear Baggage        C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦ *** Compartment Smoke     ¦    ¦    ¦ cabin to baggage compartment door   ¦ ¦

¦     Detector Systems      ¦    ¦    ¦ remains OPEN.                       ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Passenger           C ¦ -  ¦ 0  ¦ (O)May be inoperative provided door ¦ ¦

¦ *** Compartment Closet    ¦    ¦    ¦ remains OPEN for visual check from  ¦ ¦

¦     Smoke Detector        ¦    ¦    ¦ crew stations.                      ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Entranceway Baggage C ¦ -  ¦ -  ¦ (O)May be inoperative provided      ¦ ¦

¦ *** Compartment Smoke     ¦    ¦    ¦ doors remain OPEN for visual check  ¦ ¦

¦     Detector              ¦    ¦    ¦ from crew stations.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Portable Fire       D ¦ -  ¦ -  ¦ Any in excess of those required by  ¦ ¦

¦     Extinguishers         ¦    ¦    ¦ 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    ¦ ¦

¦                           ¦    ¦    ¦        can not be mistaken for a    ¦ ¦

¦                           ¦    ¦    ¦        functional unit, and         ¦ ¦

¦                           ¦    ¦    ¦     b) Required distribution is     ¦ ¦

¦                           ¦    ¦    ¦        maintained.                  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 26-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  Lavatory Fire         ¦    ¦    ¦                                     ¦ ¦

¦ *** Extinguisher          ¦    ¦    ¦                                     ¦ ¦

¦     Systems               ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        1) Passenger     C ¦  - ¦ -  ¦ (M)(O)May be inoperative in each    ¦ ¦

¦           Configuration   ¦    ¦    ¦ lavatory provided:                  ¦ ¦

¦                           ¦    ¦    ¦     a) Lavatory Smoke Detector      ¦ ¦

¦                           ¦    ¦    ¦        System operates normally.    ¦ ¦

¦                           ¦    ¦    ¦          OR                         ¦ ¦

¦                           ¦    ¦    ¦     b) Lavatory waste receptacle is ¦ ¦

¦                           ¦    ¦    ¦        empty,                       ¦ ¦

¦                           ¦    ¦    ¦     c) Lavatory door is locked      ¦ ¦

¦                           ¦    ¦    ¦        CLOSED and placarded,        ¦ ¦

¦                           ¦    ¦    ¦        "INOPERATIVE-DO NOT ENTER",  ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

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

¦                           ¦    ¦    ¦        purpose.                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦ NOTE:  These provisos are not       ¦ ¦

¦                           ¦    ¦    ¦        intended to prohibit         ¦ ¦

¦                           ¦    ¦    ¦        lavatory inspections by      ¦ ¦

¦                           ¦    ¦    ¦        crewmembers.                 ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦           Configuration   ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 26-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  Lavatory Smoke        ¦    ¦    ¦                                     ¦ ¦

¦ *** Detection Systems     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦      1) Passenger       C ¦ -  ¦ -  ¦ (M)(O)May be inoperative in each    ¦ ¦

¦         Configuration     ¦    ¦    ¦ lavatory provided:                  ¦ ¦

¦                           ¦    ¦    ¦     a) Lavatory Fire Extinguisher   ¦ ¦

¦                           ¦    ¦    ¦        System operates normally.    ¦ ¦

¦                           ¦    ¦    ¦          OR                         ¦ ¦

¦                           ¦    ¦    ¦     b) Lavatory waste receptacle is ¦ ¦

¦                           ¦    ¦    ¦        empty,                       ¦ ¦

¦                           ¦    ¦    ¦     c) Lavatory door is locked      ¦ ¦

¦                           ¦    ¦    ¦        CLOSED and placarded,        ¦ ¦

¦                           ¦    ¦    ¦        "INOPERATIVE-DO NOT ENTER",  ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

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

¦                           ¦    ¦    ¦        purpose.                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦     NOTE: These provisos are not    ¦ ¦

¦                           ¦    ¦    ¦           intended to prohibit      ¦ ¦

¦                           ¦    ¦    ¦           lavatory inspections by   ¦ ¦

¦                           ¦    ¦    ¦           crewmembers.              ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦        Configuration      ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 Galley Fire         C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ *** Extinguishing         ¦    ¦    ¦                                     ¦ ¦

¦     Systems               ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 Galley Smoke        C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ *** Detection Systems     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -12 Flame Detectors     C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 27-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Stall Warning         ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Flap Position         ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Indicator             ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Trim Tab Indicators C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦ *** (Electric)            ¦    ¦    ¦ electric trim or electronic flight  ¦ ¦

¦                           ¦    ¦    ¦ control systems are considered      ¦ ¦

¦                           ¦    ¦    ¦ inoperative.                        ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 28-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Fuel Quantity       C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦     Indicators            ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Both tanks are completely    ¦ ¦

¦                           ¦    ¦    ¦        filled using overwing        ¦ ¦

¦                           ¦    ¦    ¦        refueling,                   ¦ ¦

¦                           ¦    ¦    ¦     b) Both fuel flow meters are    ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     c) Circuit breaker of the       ¦ ¦

¦                           ¦    ¦    ¦        inoperative system is pulled ¦ ¦

¦                           ¦    ¦    ¦        and collared,                ¦ ¦

¦                           ¦    ¦    ¦     d) After takeoff, power is set  ¦ ¦

¦                           ¦    ¦    ¦        by matching TGT indications  ¦ ¦

¦                           ¦    ¦    ¦        on both engines, and         ¦ ¦

¦                           ¦    ¦    ¦     e) Flight crew maintains a log  ¦ ¦

¦                           ¦    ¦    ¦        of fuel burned.              ¦ ¦

¦                           ¦    ¦    ¦         OR                          ¦ ¦

¦                         C ¦    ¦    ¦     f) Affected tank is defueled    ¦ ¦

¦                           ¦    ¦    ¦        before each refueling,       ¦ ¦

¦                           ¦    ¦    ¦     g) Affected tank is fueled with ¦ ¦

¦                           ¦    ¦    ¦        a known quantity of fuel,    ¦ ¦

¦                           ¦    ¦    ¦     h) Both fuel flow meters are    ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     i) Circuit breaker of the       ¦ ¦

¦                           ¦    ¦    ¦        inoperative system is pulled ¦ ¦

¦                           ¦    ¦    ¦        and collared,                ¦ ¦

¦                           ¦    ¦    ¦     j) After takeoff, power is set  ¦ ¦

¦                           ¦    ¦    ¦        by matching TGT indications  ¦ ¦

¦                           ¦    ¦    ¦        on both engines, and         ¦ ¦

¦                           ¦    ¦    ¦     k) Flight crew maintains a log  ¦ ¦

¦                           ¦    ¦    ¦        of fuel burned.              ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Fuel Crossfeed        ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Valve                 ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 28-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Fuel Filter Heat    C ¦ 2  ¦ 0  ¦ (M)(O)Both may be inoperative       ¦ ¦

¦     Systems               ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Anti-icing additives are     ¦ ¦

¦                           ¦    ¦    ¦        added to fuel,               ¦ ¦

¦                           ¦    ¦    ¦     b) Hot Air Gate Valve remains   ¦ ¦

¦                           ¦    ¦    ¦        CLOSED, and                  ¦ ¦

¦                           ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations and Procedures.  ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     d) Aircraft is operated with    ¦ ¦

¦                           ¦    ¦    ¦        fuel temperatures above +10  ¦ ¦

¦                           ¦    ¦    ¦        degrees C.                   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Fuel Boost Pumps    C ¦ 4  ¦ 3  ¦ (O)One may be inoperative provided: ¦ ¦

¦                           ¦    ¦    ¦     a) Fuel Intertank Valve is      ¦ ¦

¦                           ¦    ¦    ¦        installed and operative, and ¦ ¦

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

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Procedures.                  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Low Fuel Quantity   C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦     Warning Systems       ¦    ¦    ¦ provided both Fuel Quantity         ¦ ¦

¦                           ¦    ¦    ¦ Indicators are operative.           ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦                           ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Both Fuel Quantity           ¦ ¦

¦                           ¦    ¦    ¦        Indicators are operative,    ¦ ¦

¦                           ¦    ¦    ¦     b) All Fuel Boost Pumps are     ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     c) Fuel Crossfeed Valve is      ¦ ¦

¦                           ¦    ¦    ¦        OPENED when either wing tank ¦ ¦

¦                           ¦    ¦    ¦        contains 2000 pounds or less ¦ ¦

¦                           ¦    ¦    ¦        fuel.                        ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 28-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Fuel Intertank      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦ *** Valve                 ¦    ¦    ¦     a) All Fuel Boost Pumps are     ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     b) All Fuel Quantity Indicators ¦ ¦

¦                           ¦    ¦    ¦        are operative.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Single Point        C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided      ¦ ¦

¦ *** Refueling System      ¦    ¦    ¦ procedures are established to       ¦ ¦

¦                           ¦    ¦    ¦ deactivate single point refueling   ¦ ¦

¦                           ¦    ¦    ¦ system.                             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  Fuel Temperature    C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative          ¦ ¦

¦ *** Indication Systems    ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Fuel Filter Heat System is   ¦ ¦

¦                           ¦    ¦    ¦        operative for affected       ¦ ¦

¦                           ¦    ¦    ¦        engine.                      ¦ ¦

¦                           ¦    ¦    ¦     b) OAT Indicator is operative,  ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     c) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations and Procedures.  ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     d) Aircraft is operated at      ¦ ¦

¦                           ¦    ¦    ¦        outside air temperatures     ¦ ¦

¦                           ¦    ¦    ¦        above +10 degrees C.         ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 29-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Hydraulic Pumps       ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     (engine driven)       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Auxiliary Pump        ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Normal Hydraulic      ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Pressure Gauge        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Auxiliary Hydraulic C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦     Pressure Gauge        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Brake Accumulator   C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦     Pressure Gauge        ¦    ¦    ¦                                     ¦ ¦

¦     (Nose Wheelwell)      ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 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 and          C ¦ 2  ¦ 0  ¦ (M)(O)Both may be inoperative       ¦ ¦

¦     Propeller Deicing     ¦    ¦    ¦ provided aircraft is not operated   ¦ ¦

¦     Systems               ¦    ¦    ¦ into known or forecast icing        ¦ ¦

¦                           ¦    ¦    ¦ conditions.                         ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Pitot Heaters       B ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦                           ¦    ¦    ¦ provided aircraft is not operated   ¦ ¦

¦                           ¦    ¦    ¦ in visible moisture or known or     ¦ ¦

¦                           ¦    ¦    ¦ forecast icing conditions.          ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Windshield Wiper    C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative provided ¦ ¦

¦     Systems               ¦    ¦    ¦ aircraft is not operated in         ¦ ¦

¦                           ¦    ¦    ¦ precipitation within 5 NM of the    ¦ ¦

¦                           ¦    ¦    ¦ airport of takeoff or intended      ¦ ¦

¦                           ¦    ¦    ¦ landing.                            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Airfoil Deicing     C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided   ¦ ¦

¦     System (Wing &        ¦    ¦    ¦ aircraft is not operated into known ¦ ¦

¦     Empennage)            ¦    ¦    ¦ or forecast icing conditions.       ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Windshield Heat     B ¦ 2  ¦ 0  ¦ (O)(M)Both may be inoperative       ¦ ¦

¦     Systems               ¦    ¦    ¦ provided:                           ¦ ¦

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

¦                           ¦    ¦    ¦        known or forecast icing      ¦ ¦

¦                           ¦    ¦    ¦        conditions, and              ¦ ¦

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

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  DV Window Heat      C ¦ 2  ¦ 0  ¦ (M)(O)Both may be inoperative       ¦ ¦

¦     Systems               ¦    ¦    ¦ provided:                           ¦ ¦

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

¦                           ¦    ¦    ¦        known or forecast icing      ¦ ¦

¦                           ¦    ¦    ¦        conditions, and              ¦ ¦

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

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 30-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Side Window Heat    C ¦ 2  ¦ 0  ¦                                     ¦ ¦

¦ *** Systems               ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  Pneumatic Boots     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Pressure Gauge        ¦    ¦    ¦     a) Suction Gauge is operative,  ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     b) Suction Gauge is verified to ¦ ¦

¦                           ¦    ¦    ¦        have normal indications      ¦ ¦

¦                           ¦    ¦    ¦        before takeoff.              ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  Pitot Heat Light    B ¦ 2  ¦ 0  ¦ (M)(O)Both may be inoperative       ¦ ¦

¦     Systems               ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) All other elements of the    ¦ ¦

¦                           ¦    ¦    ¦        pitot heat system are        ¦ ¦

¦                           ¦    ¦    ¦        checked and operate          ¦ ¦

¦                           ¦    ¦    ¦        normally, and                ¦ ¦

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

¦                           ¦    ¦    ¦        known or forecast icing      ¦ ¦

¦                           ¦    ¦    ¦        conditions.                  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 Ice Detection       C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ *** Systems               ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 Pneumatic Boots     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Suction Gauge         ¦    ¦    ¦     a) Aircraft is not operated in  ¦ ¦

¦                           ¦    ¦    ¦        known or forecast icing      ¦ ¦

¦                           ¦    ¦    ¦        conditions,                  ¦ ¦

¦                           ¦    ¦    ¦     b) Aircraft is operated in an   ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     c) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 ft.             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 31-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦

¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Clock               C ¦ -  ¦ 1  ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

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

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

¦     System                ¦    ¦    ¦        System is operative, and     ¦ ¦

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

¦                           ¦    ¦    ¦        three flight days.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Cockpit Voice         ¦    ¦    ¦ Moved to Chapter 23, Rev. 5.        ¦ ¦

¦     Recorder (CVR)        ¦    ¦    ¦                                     ¦ ¦

¦     System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 32-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Anti-Skid Systems     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦                           ¦    ¦    ¦ aircraft is operated in accordance  ¦ ¦

¦                           ¦    ¦    ¦ with AFM Limitations.               ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦ ***  2) Electrical      C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided   ¦ ¦

¦                           ¦    ¦    ¦ aircraft is operated in accordance  ¦ ¦

¦                           ¦    ¦    ¦ with AFM Limitations.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Landing Gear          ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Position Indicator    ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Park Brake            ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Anti-Skid           C ¦ -  ¦ 0  ¦ (M)(O)May be inoperative provided:  ¦ ¦

¦ *** Indication Systems    ¦    ¦    ¦     a) Anti-skid System is          ¦ ¦

¦     (Electronic Anti-     ¦    ¦    ¦        electrically disabled, and   ¦ ¦

¦     Skid)                 ¦    ¦    ¦     b) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 33-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Cockpit/Flight      C ¦ -  ¦ -  ¦ Individual lights may be            ¦ ¦

¦     Deck/Flight           ¦    ¦    ¦ inoperative provided remaining      ¦ ¦

¦     Compartment and       ¦    ¦    ¦ lights are:                         ¦ ¦

¦     Instrument Lighting   ¦    ¦    ¦     a) Sufficient to clearly        ¦ ¦

¦     Systems (Excluding    ¦    ¦    ¦        illuminate all required      ¦ ¦

¦     EFIS)                 ¦    ¦    ¦        instruments, controls and    ¦ ¦

¦                           ¦    ¦    ¦        other devices for which it   ¦ ¦

¦                           ¦    ¦    ¦        is provided,                 ¦ ¦

¦                           ¦    ¦    ¦     b) Positioned so that direct    ¦ ¦

¦                           ¦    ¦    ¦        rays are shielded from       ¦ ¦

¦                           ¦    ¦    ¦        flight crewmembers' eyes,    ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     c) Lighting configuration and   ¦ ¦

¦                           ¦    ¦    ¦        intensity is acceptable to   ¦ ¦

¦                           ¦    ¦    ¦        the flight crew.             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Passenger Cabin     C ¦ -  ¦ -  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Interior              ¦    ¦    ¦     a) Sufficient lighting is       ¦ ¦

¦     Illumination          ¦    ¦    ¦        operative for crew to        ¦ ¦

¦     Systems               ¦    ¦    ¦        perform required duties, and ¦ ¦

¦                           ¦    ¦    ¦     b) Lighting configuration at    ¦ ¦

¦                           ¦    ¦    ¦        dispatch is acceptable to    ¦ ¦

¦                           ¦    ¦    ¦        flight crew.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Passenger Notice    B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦     System (No Smoking/   ¦    ¦    ¦ procedures are established and used ¦ ¦

¦     Fasten Seat Belts)    ¦    ¦    ¦ for notifying the passengers when   ¦ ¦

¦                           ¦    ¦    ¦ seat belts should be fastened and   ¦ ¦

¦                           ¦    ¦    ¦ smoking is prohibited.              ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Exterior Emergency  B ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦     Lights                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 33-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Landing Light       C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦     Systems               ¦    ¦    ¦ provided Taxi Lights are operative. ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦                           ¦    ¦    ¦ provided airplane is not operated   ¦ ¦

¦                           ¦    ¦    ¦ at night.                           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Taxi Lights         C ¦ 2  ¦ 0  ¦ (M)                                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Position Light      C ¦ -  ¦ -  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Bulbs                 ¦    ¦    ¦     a) One light bulb is operative  ¦ ¦

¦                           ¦    ¦    ¦        at each position.            ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

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

¦                           ¦    ¦    ¦        night.                       ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  Beacons             C ¦ 3  ¦ 0  ¦ (O)All may be inoperative provided  ¦ ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦ -9  Strobe "Anti-       B ¦ 3  ¦ 0  ¦ (O)All may be inoperative provided: ¦ ¦

¦ *** Collision) Lights     ¦    ¦    ¦     a) Aircraft is not operated at  ¦ ¦

¦                           ¦    ¦    ¦        night.                       ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                           ¦    ¦    ¦     b) All Beacons are operative.   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 33-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 Wing Inspection     C ¦ 4  ¦ 0  ¦ All may be inoperative provided:    ¦ ¦

¦     Lights                ¦    ¦    ¦     a) Portable lamp/light of       ¦ ¦

¦                           ¦    ¦    ¦        adequate capacity for wing   ¦ ¦

¦                           ¦    ¦    ¦        and/or control surface       ¦ ¦

¦                           ¦    ¦    ¦        inspection is available for  ¦ ¦

¦                           ¦    ¦    ¦        night operation in icing     ¦ ¦

¦                           ¦    ¦    ¦        conditions.                  ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦ ________________________C ¦    ¦    ¦     b) Aircraft is not operated     ¦ ¦

¦                           ¦    ¦    ¦        into known or forecast icing ¦ ¦

¦                           ¦    ¦    ¦        conditions.                  ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                           ¦    ¦    ¦     c) Aircraft is not operated at  ¦ ¦

¦                           ¦    ¦    ¦        night.                       ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 Interior Emergency    ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦     Lighting              ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -12 Master Warning        ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦     System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 33-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -13 Floor Proximity     C ¦ -  ¦ 0  ¦ Individual lights may be            ¦ ¦

¦ *** Emergency Escape      ¦    ¦    ¦ inoperative provided it is verified ¦ ¦

¦     Path Marking System   ¦    ¦    ¦ that the FAA approved Minimum       ¦ ¦

¦     Lights                ¦    ¦    ¦ acceptable lighting levels          ¦ ¦

¦                           ¦    ¦    ¦ specified in one of the following   ¦ ¦

¦                           ¦    ¦    ¦ documents are complied with:        ¦ ¦

¦                           ¦    ¦    ¦     a) FAA Engineering Approval     ¦ ¦

¦                           ¦    ¦    ¦        Letter.                      ¦ ¦

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

¦                           ¦    ¦    ¦        Type Design Holder.          ¦ ¦

¦                           ¦    ¦    ¦     c) Limitations and conditions   ¦ ¦

¦                           ¦    ¦    ¦        section of the applicable    ¦ ¦

¦                           ¦    ¦    ¦        Supplemental Type            ¦ ¦

¦                           ¦    ¦    ¦        Certificate (STC).           ¦ ¦

¦                           ¦    ¦    ¦     d) An FAA approved report       ¦ ¦

¦                           ¦    ¦    ¦        incorporated in the Master   ¦ ¦

¦                           ¦    ¦    ¦        Drawing List for the         ¦ ¦

¦                           ¦    ¦    ¦        Applicable STC.              ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -14 Logo Lights System  C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -15 Recognition Lights  C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ *** System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 34-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Airspeed Indicator    ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Attitude Indicator    ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Turn and Slip       B ¦ 2  ¦ 1  ¦ Turn function may be inoperative    ¦ ¦

¦     Indicator             ¦    ¦    ¦ provided Standby Attitude Indicator ¦ ¦

¦                           ¦    ¦    ¦ (Third Gyro Horizon) is installed   ¦ ¦

¦                           ¦    ¦    ¦ and operative.                      ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Directional Gyro      ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Compass System        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Altimeter             ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Rate-of-Climb       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided  ¦ ¦

¦     Indicators            ¦    ¦    ¦ aircraft is operated during day VMC ¦ ¦

¦                           ¦    ¦    ¦ conditions.                         ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Outside Air           ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Temperature           ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  Magnetic Compass    C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided both ¦ ¦

¦     (Standby)             ¦    ¦    ¦ directional gyro compass systems    ¦ ¦

¦                           ¦    ¦    ¦ are operative and slaved in the Mag ¦ ¦

¦                           ¦    ¦    ¦ position.                           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  MACH/Airspeed         ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Warning System        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -10 Radio Navigation      ¦    ¦    ¦ Item Deleted and moved to separate  ¦ ¦

¦     Equipment, DME, VOR   ¦    ¦    ¦ items within this ATA Chapter, Rev. ¦ ¦

¦     Radar, ADF,           ¦    ¦    ¦ 5.                                  ¦ ¦

¦     Transponder, ILS      ¦    ¦    ¦                                     ¦ ¦

¦     Marker Beacon         ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 34-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -11 Ground Proximity      ¦    ¦    ¦                                     ¦ ¦

¦     Warning System        ¦    ¦    ¦                                     ¦ ¦

¦     (GPWS)                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        1) Terrain       A ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦           Avoidance       ¦    ¦    ¦     a) Alternate procedures are     ¦ ¦

¦           Modes 1-4       ¦    ¦    ¦        established and used, and    ¦ ¦

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

¦                           ¦    ¦    ¦        flight days.                 ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        2) Test Mode     A ¦ 1  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦                           ¦    ¦    ¦     a) GPWS is considered           ¦ ¦

¦                           ¦    ¦    ¦        inoperative, and             ¦ ¦

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

¦                           ¦    ¦    ¦        flight days.                 ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        3) Glideslope    B ¦ 2  ¦ 0  ¦                                     ¦ ¦

¦           Deviation       ¦    ¦    ¦                                     ¦ ¦

¦           (Mode 5)        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦ ***    4) Advisory      C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦           Callouts        ¦    ¦    ¦ alternate procedures are            ¦ ¦

¦                           ¦    ¦    ¦ established and used.               ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

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

¦           Mode            ¦    ¦    ¦ alternate procedures are            ¦ ¦

¦                           ¦    ¦    ¦ established and used.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -12 Radar Altimeter     C ¦ -  ¦ -  ¦ (O)All may be inoperative provided: ¦ ¦

¦     Systems               ¦    ¦    ¦     a) Landing weather minimums or  ¦ ¦

¦                           ¦    ¦    ¦        operating procedures do not  ¦ ¦

¦                           ¦    ¦    ¦        require its use, and         ¦ ¦

¦                           ¦    ¦    ¦     b) Other systems affected       ¦ ¦

¦                           ¦    ¦    ¦        (GPWS, FD, AP, etc.) are     ¦ ¦

¦                           ¦    ¦    ¦        considered.                  ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -13 Flight Director     C ¦ -  ¦ 0  ¦ May be inoperative provided         ¦ ¦

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

¦                           ¦    ¦    ¦ its use.                            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 34-3     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -14 Area Navigation     D ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦ *** Systems               ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -15 Horizontal          C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided: ¦ ¦

¦ *** Situation             ¦    ¦    ¦     a) Aircraft is operated day VMC ¦ ¦

¦     Indicators (HSI)      ¦    ¦    ¦        only, and                    ¦ ¦

¦                           ¦    ¦    ¦     b) Compass heading indication   ¦ ¦

¦                           ¦    ¦    ¦        is available on each pilot's ¦ ¦

¦                           ¦    ¦    ¦        instrument panel.            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -16 Standby Attitude    B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Indicator (Third      ¦    ¦    ¦     a) EFIS is not installed, and   ¦ ¦

¦     Gyro Horizon)         ¦    ¦    ¦     b) Aircraft is operated day VMC ¦ ¦

¦                           ¦    ¦    ¦        only.                        ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦ *** 1) Glideslope/      C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦        Localizer          ¦    ¦    ¦                                     ¦ ¦

¦        Indicator          ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -17 Weather Radar       C ¦ 1  ¦ 0  ¦ As required by FAR.                 ¦ ¦

¦     System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -18 VOR/ILS Navigation  C ¦ -  ¦ -  ¦ As required by FAR and no relief    ¦ ¦

¦     Systems               ¦    ¦    ¦ may be provided to an inoperative   ¦ ¦

¦                           ¦    ¦    ¦ system or component if powered by   ¦ ¦

¦                           ¦    ¦    ¦ an emergency bus or equivalent and  ¦ ¦

¦                           ¦    ¦    ¦ required to accomplish an emergency ¦ ¦

¦                           ¦    ¦    ¦ procedure.                          ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -19 Marker Beacon       C ¦ -  ¦ -  ¦ May be inoperative provided         ¦ ¦

¦     Systems               ¦    ¦    ¦ approach procedures do not require  ¦ ¦

¦                           ¦    ¦    ¦ its use.                            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -20 Automatic Direction C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦     Finding Systems       ¦    ¦    ¦                                     ¦ ¦

¦     (ADF)                 ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 34-4     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -21 ATC Transponders    C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦     and Automatic         ¦    ¦    ¦                                     ¦ ¦

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

¦     Systems               ¦    ¦    ¦ FAR may be inoperative.             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -22 Distance Measuring  C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦     Equipment (DME)       ¦    ¦    ¦                                     ¦ ¦

¦     Systems               ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -23 Long Range          C ¦ -  ¦ 0  ¦ As required by FAR.                 ¦ ¦

¦ *** Navigation Systems    ¦    ¦    ¦                                     ¦ ¦

¦     (INS, IRS, OMEGA,     ¦    ¦    ¦                                     ¦ ¦

¦     LORAN, GPS, VLF,      ¦    ¦    ¦                                     ¦ ¦

¦     and OSS)              ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -24 Attitude Reference  C ¦ -  ¦ 2  ¦ May be inoperative provided         ¦ ¦

¦ *** Systems (Vertical     ¦    ¦    ¦ independent Primary Attitude        ¦ ¦

¦     Gyros, AHRS, IRS)     ¦    ¦    ¦ information is available on each    ¦ ¦

¦     (Excludes Standby     ¦    ¦    ¦ pilot's panel.                      ¦ ¦

¦     Attitude Indicator)   ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -25 Angle of Attack     C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ *** Indicator             ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -26 Comparator Monitor  C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦ *** System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 34-5     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -27 Electronic Flight     ¦    ¦    ¦                                     ¦ ¦

¦ *** Instrument System     ¦    ¦    ¦                                     ¦ ¦

¦     (EFIS)                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦     1) Multifunction    C ¦ 1  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦        Display Unit       ¦    ¦    ¦     a) Weather radar information    ¦ ¦

¦                           ¦    ¦    ¦        can be displayed at each     ¦ ¦

¦                           ¦    ¦    ¦        pilot station or weather     ¦ ¦

¦                           ¦    ¦    ¦        radar is considered          ¦ ¦

¦                           ¦    ¦    ¦        inoperative, and             ¦ ¦

¦                           ¦    ¦    ¦     b) Procedures do not require    ¦ ¦

¦                           ¦    ¦    ¦        its use.                     ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦     2) Symbol           C ¦ -  ¦ 2  ¦ One may be inoperative provided     ¦ ¦

¦        Generators         ¦    ¦    ¦ EFIS displays at pilot's and        ¦ ¦

¦                           ¦    ¦    ¦ copilot's stations are operative    ¦ ¦

¦                           ¦    ¦    ¦ from independent Symbol Generators. ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -28 Inertial Sensor     C ¦ 1  ¦ 0  ¦ May be inoperative provided at      ¦ ¦

¦ *** Display Unit (ISDU)   ¦    ¦    ¦ least one Flight Management System  ¦ ¦

¦                           ¦    ¦    ¦ is operative.                       ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -29 Microwave Landing   C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦ *** Systems (MLS)         ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -30 Navigation Data     C ¦ -  ¦ 0  ¦ May be inoperative provided         ¦ ¦

¦ *** Storage Systems       ¦    ¦    ¦ aircraft is operated in accordance  ¦ ¦

¦                           ¦    ¦    ¦ with AFM Limitations.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -31 Stormscopes         C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 34-6     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -32 Traffic Alert         ¦    ¦    ¦                                     ¦ ¦

¦ *** Collision 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)May be inoperative on the non-   ¦ ¦

¦           and RA          ¦    ¦    ¦ flying pilot side provided:         ¦ ¦

¦ ***       Dual Displays   ¦    ¦    ¦     a) TA and RA elements and audio ¦ ¦

¦                           ¦    ¦    ¦        functions are operative on   ¦ ¦

¦                           ¦    ¦    ¦        flying pilot side, and       ¦ ¦

¦                           ¦    ¦    ¦     b) TA and RA display            ¦ ¦

¦                           ¦    ¦    ¦        indications are visible to   ¦ ¦

¦                           ¦    ¦    ¦        the non-flying pilot.        ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦        3) Resolution    C ¦ 2  ¦ 1  ¦ (O)One may be inoperative on non-   ¦ ¦

¦           Advisory (RA)   ¦    ¦    ¦ 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          ¦    ¦    ¦ installed RA display and audio      ¦ ¦

¦                           ¦    ¦    ¦ functions are operative.            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -33 Vertical Navigation C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ *** System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -34 Voice Advisory      C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ *** System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 34-7     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -35 Voice Terrain       C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ *** Advisory (VTA)        ¦    ¦    ¦                                     ¦ ¦

¦     System (not part of   ¦    ¦    ¦                                     ¦ ¦

¦     Ground Proximity      ¦    ¦    ¦                                     ¦ ¦

¦     Warning System)       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -36 Windshear Detection C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦ *** and Guidance          ¦    ¦    ¦ alternate procedures are            ¦ ¦

¦     Systems               ¦    ¦    ¦ established and used.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -37 Fuel Management     C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ *** System                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -38 Altitude Alerting   A ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

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

¦                           ¦    ¦    ¦        is operative, and            ¦ ¦

¦                           ¦    ¦    ¦     b) Operators are limited to not ¦ ¦

¦                           ¦    ¦    ¦        more than three flight days  ¦ ¦

¦                           ¦    ¦    ¦        before repairs are made.     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -39 Lightning Sensor    C ¦ -  ¦ 0  ¦                                     ¦ ¦

¦ *** Systems (LSS)         ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 35-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 35  OXYGEN                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Oxygen System and   C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦

¦     Supply                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Cabin Oxygen System C ¦ 1  ¦ 0  ¦ May be inoperative provided:        ¦ ¦

¦ *** ON Warning System     ¦    ¦    ¦     a) Cabin Altitude Indicator is  ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     b) Cabin Differential Pressure  ¦ ¦

¦                           ¦    ¦    ¦        Indicator is operative, and  ¦ ¦

¦                           ¦    ¦    ¦     c) Cabin Pressure Warning       ¦ ¦

¦                           ¦    ¦    ¦        System is operative.         ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     d) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

¦                           ¦    ¦    ¦     e) Aircraft is operated at or   ¦ ¦

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Portable Oxygen     B ¦ -  ¦ -  ¦ Any in excess of those required by  ¦ ¦

¦ *** Dispensing Units      ¦    ¦    ¦ FAR may be inoperative or missing   ¦ ¦

¦     (Bottles and Mask)    ¦    ¦    ¦ provided required distribution is   ¦ ¦

¦                           ¦    ¦    ¦ maintained throughout the aircraft. ¦ ¦

¦                           ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦ NOTE:  Any bottle not properly      ¦ ¦

¦                           ¦    ¦    ¦        serviced is considered       ¦ ¦

¦                           ¦    ¦    ¦        inoperative and should be    ¦ ¦

¦                           ¦    ¦    ¦        removed.                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Oxygen Service      C ¦ 1  ¦ 0  ¦ (M)(O)                              ¦ ¦

¦ *** Panel Gauge           ¦    ¦    ¦                                     ¦ ¦

¦     (External)            ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Protective          B ¦ -  ¦ -  ¦ Any in excess of those required by  ¦ ¦

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

¦     (PBE)                 ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 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)(O)May be inoperative provided:  ¦ ¦

¦     Unit                  ¦    ¦    ¦     a) Both DC Generators are       ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     b) Both DC Generator Overheat   ¦ ¦

¦                           ¦    ¦    ¦        Warning Lights are           ¦ ¦

¦                           ¦    ¦    ¦        operative,                   ¦ ¦

¦                           ¦    ¦    ¦     c) Procedures do not require    ¦ ¦

¦                           ¦    ¦    ¦        its use for electrical power ¦ ¦

¦                           ¦    ¦    ¦        or as an air source, and     ¦ ¦

¦                           ¦    ¦    ¦     d) Aircraft is operated in      ¦ ¦

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  APU Air Load Valve  C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  ¦ ¦

¦                           ¦    ¦    ¦     a) Procedures do not require    ¦ ¦

¦                           ¦    ¦    ¦        its use as an air source,    ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

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

¦                           ¦    ¦    ¦        accordance with AFM          ¦ ¦

¦                           ¦    ¦    ¦        Limitations.                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  APU RPM Indicator   C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  APU EGT Indicator   C ¦ 1  ¦ 0  ¦                                     ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  APU Oil Pressure    C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided   ¦ ¦

¦     Indicator Light       ¦    ¦    ¦ APU is considered inoperative.      ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  APU Operating RPM   C ¦ 1  ¦ 0  ¦ (O)                                 ¦ ¦

¦     Indicator Light       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 49-2     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 49  AIRBORNE AUXILIARY    ¦    ¦    ¦                                       ¦

¦     POWER                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  APU Generator Off   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     Indicator Light       ¦    ¦    ¦     a) APU Generator Ammeter is     ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     b) APU Operating RPM Indicator  ¦ ¦

¦                           ¦    ¦    ¦        Light is operative           ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦    ¦    ¦     c) APU Generator Ammeter is     ¦ ¦

¦                           ¦    ¦    ¦        operative, and               ¦ ¦

¦                           ¦    ¦    ¦     d) APU RPM Indicator is         ¦ ¦

¦                           ¦    ¦    ¦        operative.                   ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -8  APU Start Indicator C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided APU  ¦ ¦

¦     Light                 ¦    ¦    ¦ is considered inoperative.          ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -9  APU External Fire   C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided   ¦ ¦

¦ *** Warning Alarm (Fire   ¦    ¦    ¦ APU operation is monitored in       ¦ ¦

¦     Warning Bell)         ¦    ¦    ¦ cockpit.                            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 52-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 52  DOORS                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Door Warning Light  C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     ¦ ¦

¦     System                ¦    ¦    ¦     a) A crewmember verifies by     ¦ ¦

¦                           ¦    ¦    ¦        visual inspection before     ¦ ¦

¦                           ¦    ¦    ¦        each departure that the      ¦ ¦

¦                           ¦    ¦    ¦        associated doors are CLOSED  ¦ ¦

¦                           ¦    ¦    ¦        and LOCKED, and              ¦ ¦

¦                           ¦    ¦    ¦     b) Locking pin is removed from  ¦ ¦

¦                           ¦    ¦    ¦        the baggage door lock handle ¦ ¦

¦                           ¦    ¦    ¦        before each departure.       ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Door Inflatable     C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative          ¦ ¦

¦     Seal Systems          ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) Flight is conducted in an    ¦ ¦

¦                           ¦    ¦    ¦        unpressurized configuration, ¦ ¦

¦                           ¦    ¦    ¦        and                          ¦ ¦

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

¦                           ¦    ¦    ¦        below 10,000 feet.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Cargo Door Warning  C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided a    ¦ ¦

¦ *** Light System          ¦    ¦    ¦ crewmember verifies by visual       ¦ ¦

¦                           ¦    ¦    ¦ inspection before each departure    ¦ ¦

¦                           ¦    ¦    ¦ that the cargo door is CLOSED and   ¦ ¦

¦                           ¦    ¦    ¦ LOCKED.                             ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Cargo Door          C ¦ 1  ¦ 0  ¦ (O)(M)May be inoperative provided:  ¦ ¦

¦ *** Operating System      ¦    ¦    ¦     a) Door is not used, and        ¦ ¦

¦                           ¦    ¦    ¦     b) A crewmember verifies by     ¦ ¦

¦                           ¦    ¦    ¦        visual inspection before     ¦ ¦

¦                           ¦    ¦    ¦        each departure that the      ¦ ¦

¦                           ¦    ¦    ¦        cargo door is CLOSED and     ¦ ¦

¦                           ¦    ¦    ¦        LOCKED.                      ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 61-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 61  PROPELLERS            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Below Flight Fine     ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦     Pitch Lock Lights     ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Flight Fine Pitch   B ¦ 2  ¦ 1  ¦ (O)                                 ¦ ¦

¦     Lock Lights           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Cruise Lockout        ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦     Lights                ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Cruise Pitch Lights B ¦ 2  ¦ 1  ¦ (O)                                 ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Auto Feathering       ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦     System                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Propeller           C ¦ 1  ¦ 0  ¦ (M)(O)                              ¦ ¦

¦     Synchronizer System   ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -7  Propeller Brake     C ¦ 1  ¦ 0  ¦ (M)(O)                              ¦ ¦

¦ ***                       ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 73-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 73  ENGINE FUEL & CONTROL ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Fuel Flowmeters     B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided  ¦ ¦

¦                           ¦    ¦    ¦ both Fuel Quantity Indicators are   ¦ ¦

¦                           ¦    ¦    ¦ operative.                          ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Fuel Trim           C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided: ¦ ¦

¦     Indicators            ¦    ¦    ¦     a) Both trim actuators are set  ¦ ¦

¦                           ¦    ¦    ¦        simultaneously utilizing     ¦ ¦

¦                           ¦    ¦    ¦        operative indicator starting ¦ ¦

¦                           ¦    ¦    ¦        at 0% trim for engine        ¦ ¦

¦                           ¦    ¦    ¦        starting and takeoff, and    ¦ ¦

¦                           ¦    ¦    ¦     b) TGT indicator is used for    ¦ ¦

¦                           ¦    ¦    ¦        setting trim in flight.      ¦ ¦

¦                           ¦    ¦    ¦           OR                        ¦ ¦

¦                         C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative provided ¦ ¦

¦                           ¦    ¦    ¦ takeoff and landing operations are  ¦ ¦

¦                           ¦    ¦    ¦ confined to ambient air             ¦ ¦

¦                           ¦    ¦    ¦ temperatures below I.S.A.           ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Fuel Trimmer          ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦     Actuator              ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Fuel Low Pressure   C ¦ 4  ¦ 2  ¦ (O)Two may be inoperative provided: ¦ ¦

¦     Warning Lights        ¦    ¦    ¦     a) One is operative on each     ¦ ¦

¦                           ¦    ¦    ¦        engine, and                  ¦ ¦

¦                           ¦    ¦    ¦     b) Fuel Crossfeed Valve is      ¦ ¦

¦                           ¦    ¦    ¦        OPEN.                        ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Fuel Used           C ¦ 2  ¦ 0  ¦ (O)Both may be inoperative provided ¦ ¦

¦ *** Indicators            ¦    ¦    ¦ both Fuel Quantity Indicators are   ¦ ¦

¦                           ¦    ¦    ¦ operative.                          ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -6  Fuel Trim Computer  D ¦ 1  ¦ 0  ¦ (O) May be inoperative provided AFM ¦ ¦

¦                           ¦    ¦    ¦ fuel trimmer/datum charts are       ¦ ¦

¦                           ¦    ¦    ¦ available in cockpit.               ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 77-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Tachometers           ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  TGT Indicators        ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Torque Pressure       ¦    ¦    ¦ DELETED, Rev. 3.                    ¦ ¦

¦     Indicator             ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Engine Turbine      C ¦ 2  ¦ 0  ¦                                     ¦ ¦

¦ *** Vibration             ¦    ¦    ¦                                     ¦ ¦

¦     Indicators (TVI)      ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -5  Engine Synchroscope C ¦ 1  ¦ 0  ¦ (M)                                 ¦ ¦

¦ *** Indicator             ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 79-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 79  ENGINE OIL            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Oil Temperature       ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Indicator             ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Oil Pressure          ¦    ¦    ¦ DELETED, Rev. 5.                    ¦ ¦

¦     Indicator             ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Oil Low Pressure    C ¦ 2  ¦ 1  ¦                                     ¦ ¦

¦     Warning Lights        ¦    ¦    ¦                                     ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 80-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 80  STARTING              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Starter Engaged     C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦

¦ *** Lights                ¦    ¦    ¦ Engine Selector Switch is switched  ¦ ¦

¦                           ¦    ¦    ¦ to OFF when engine has reached      ¦ ¦

¦                           ¦    ¦    ¦ self-sustaining speed.              ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦                  G-159                   ¦ DATE: 12/27/1995      ¦ 82-1     ¦

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

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

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

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

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

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

¦ 82  WATER INJECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -1  Water/Methanol      C ¦ 2  ¦ 0  ¦ (O)One or both systems may be       ¦ ¦

¦     Injection Systems     ¦    ¦    ¦ inoperative provided performance    ¦ ¦

¦                           ¦    ¦    ¦ requirements are met with dry       ¦ ¦

¦                           ¦    ¦    ¦ power.                              ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -2  Water Methanol      C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative        ¦ ¦

¦     Pumps                 ¦    ¦    ¦ provided:                           ¦ ¦

¦                           ¦    ¦    ¦     a) An adequate water-methanol   ¦ ¦

¦                           ¦    ¦    ¦        supply, as determined from   ¦ ¦

¦                           ¦    ¦    ¦        AFM, is in the tank with the ¦ ¦

¦                           ¦    ¦    ¦        operative pump, and          ¦ ¦

¦                           ¦    ¦    ¦     b) Associated Water Methanol    ¦ ¦

¦                           ¦    ¦    ¦        Low Pressure Warning Light   ¦ ¦

¦                           ¦    ¦    ¦        is operative.                ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -3  Water Methanol Low  C ¦ 2  ¦ 1  ¦                                     ¦ ¦

¦     Pressure Warning      ¦    ¦    ¦                                       ¦

¦     Lights                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ -4  Water Methanol      C ¦ 2  ¦ 0  ¦ (M)(O)One or both may be            ¦ ¦

¦     Quantity Indicators   ¦    ¦    ¦ inoperative provided Water methanol ¦ ¦

¦                           ¦    ¦    ¦ quantity in tank with the           ¦ ¦

¦                           ¦    ¦    ¦ inoperative Indicator is checked    ¦ ¦

¦                           ¦    ¦    ¦ with a dipstick before each wet     ¦ ¦

¦                           ¦    ¦    ¦ takeoff.                            ¦ ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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