Revision:

ORIGINAL

 

Date: 08/31/2009

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON, D.C.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

AIRBUS   A-380-800

 

 

 

 

 

 

 

 

 

 

 

James H Kling, Chairman

 

 

Flight Operations Evaluation Board

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Federal Aviation Administration

 

 

Flight Standards Division

 

 

Aircraft Evaluation Group, SEA-AEG

 

 

1601 Lind Ave. S.W.

 

 

Renton Washington 98057-3356

 

 

 

 

 

 

 

 

Telephone:

(425)-917-6600

 

FAX:

(425)-917-6638

 

 

 

 

 

 

 

 

                FEDERAL AVIATION ADMINISTRATION         Page: I

                                                       Revision: ORIGINAL

                 MASTER MINIMUM EQUIPMENT LIST          Date: 08/31/2009

 

                             A-380

 

                       Table of Contents

 

SYSTEM                             PAGES             REVISION       DATE

                                                    

Table of Contents                  I                 ORIGINAL     08/31/2009

Highlights of Change               II                   

Definitions                        III THRU XI          13        09/11/2006

Preamble                           XII, XIII            2        06/14/1989

21  Air Conditioning               21-1 THRU 19      ORIGINAL     08/31/2009

22  Auto Flight                    22-1 THRU 7       ORIGINAL     08/31/2009

23  Communications                 23-1 THRU 4       ORIGINAL     08/31/2009

24  Electrical                     24-1 THRU 7       ORIGINAL     08/31/2009

25  Equipment/Furnishings          25-1 THRU 18      ORIGINAL     08/31/2009

26  Fire and Smoke Protection      26-1 THRU 15      ORIGINAL     08/31/2009

27  Flight Controls                27-1 THRU 9       ORIGINAL     08/31/2009

28  Fuel                           28-1 THRU 23      ORIGINAL     08/31/2009

29  Hydraulic                      29-1 THRU 5       ORIGINAL     08/31/2009

30  Ice and Rain Protection        30-1 THRU 9       ORIGINAL     08/31/2009

31  Indicating/Recording           31-1 THRU 7       ORIGINAL     08/31/2009

32  Landing Gear                   32-1 THRU 9       ORIGINAL     08/31/2009

33  Lights                         33-1 THRU 9       ORIGINAL     08/31/2009

34  Navigation                     34-1 THRU 9       ORIGINAL     08/31/2009

35  Oxygen                         35-1 THRU 5       ORIGINAL     08/31/2009

36  Pneumatic                      36-1 THRU 6       ORIGINAL     08/31/2009

38  Water/Waste                    38-1, 2           ORIGINAL     08/31/2009

42  Avionics Network               42-1              ORIGINAL     08/31/2009

44  Cabin Systems                  44-1 THRU 7       ORIGINAL     08/31/2009

45  Maintenance                    45-1              ORIGINAL     08/31/2009

46  Information Systems            46-1, 2, 3        ORIGINAL     08/31/2009

49  Auxiliary Power Unit           49-1, 2           ORIGINAL     08/31/2009

50  Cargo Compartments             50-1, 2, 3        ORIGINAL     08/31/2009

52  Doors                          52-1 THRU 9       ORIGINAL     08/31/2009

56  Windows                        56-1              ORIGINAL     08/31/2009

73  Engine Control and Fuel        73-1, 2, 3        ORIGINAL     08/31/2009

74  Ignition                       74-1              ORIGINAL     08/31/2009

75  Engine Cooling                 75-1              ORIGINAL     08/31/2009

77  Engine Indicating              77-1, 2           ORIGINAL     08/31/2009

78  Engine Reversers               78-1, 2           ORIGINAL     08/31/2009

79  Engine Oil                     79-1, 2           ORIGINAL     08/31/2009

80  Engine Start                   80-1              ORIGINAL     08/31/2009

 

 

                FEDERAL AVIATION ADMINISTRATION         Page: II

                                                       Revision: ORIGINAL   MASTER MINIMUM EQUIPMENT LIST         Date: 08/31/2009

 

                             A-380

 

                     Highlights of Change

 

EFFECTIVE ABOVE DATE, the Airbus A-380 Master Minimum Equipment List is issued as an original.

 

 

 

 

 

 

 

 

 

                FEDERAL AVIATION ADMINISTRATION         Page: III

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          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.   Repair interval categories (A, B, C, and D) are listed on right side of column 1. Repair intervals are described in definition 22.

 

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 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

 

                FEDERAL AVIATION ADMINISTRATION         Page: IV

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 

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.  .  As used in MMELs, "ER" refers to Extended Operations (ETOPS) of an airplane with operational approval to conduct ETOPS in accordance with the applicable regulations.

 

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 (structural) or in the engine(s) (induction).

 

11.  Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for 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

 

                FEDERAL AVIATION ADMINISTRATION         Page: VI

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 

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 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.  For time intervals specified in "flight days," the day the malfunction was recorded in the aircraft maintenance record/logbook is excluded.  For all other time intervals (flights, flight legs, cycles,

 

                FEDERAL AVIATION ADMINISTRATION         Page: VI

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 

hours, etc), repair tracking begins at the point when the malfunction is deferred in accordance with 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 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.

 

An operator who has the authorization to use an MEL also has the authority to approve extensions to the maximum repair interval for category B and C items provided the responsible Flight Standards District Office (FSDO) is notified within 24 hours of the MEL extension.  The operator is not authorized to extend A and D items in the MEL. Misuse of the MEL extension authority may result in the operators OpSpecs/Mspecs being amended by removing the authority for the operator to use the MEL extension authority and/or use an MEL.

 

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 (747-400, 757, 767, 777, 787)

 

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.

 

                FEDERAL AVIATION ADMINISTRATION         Page: VII

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 

System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program.

 

b.  BOEING  (B-717, MD-10, MD-11)

 

These 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-318/319/320/321, 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-318/319/320/321, A-330, and A-340 also provide MAINTENANCE status messages.

 

Any message that affects airplane dispatchability will normally be at the WARNING, CAUTION or STATUS level. MAINTENANCE messages (A-318/319/320/321, 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-318/319/320/321) or CMS (A-330/A-340) interrogation. The systems are designed to be fault tolerant.  For A-318/319/320/321, MAINTENENACE status (Class II) do not affect dispatch but are listed in the MMEL.  Dispatch is allowed without specific conditions except for: 
 
-          BLUE RSVR MAINTENANCE status: If applicable, and 
-          AIR BLEED MAINTENANCE status: As applicable. 
 
For the A-330 and A-340, MAINTENANCE status messages do not affect dispatch.
 
d.    FOKKER  (FK-100)
 
Fokker aircraft are equipped with Multi Function Display System (MFDS) which provides electronic message referring to the different priority 
 

                FEDERAL AVIATION ADMINISTRATION         Page: VIII

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 
levels of system information (WARNING (red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any messages that affect 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.

 

e. CANADAIR  (CL-65, CL-604)

 
Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAS) provide four classes of messages (WARNING, CAUTION, ADVISORY, and STATUS). Any message that affects aircraft dispatch will be at the WARNING, CAUTION, or STATUS level.
 
System conditions that only require maintenance are not visible to the flight crew. These maintenance indications/messages are only activated by maintenance personnel using the Maintenance Diagnostics Computer.

 

f.     EMBRAER  (EMB-135/145, ERJ-170 Series)

 

The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew Alerting System (EICAS) that provides three different message levels: WARNING, CAUTION, and ADVISORY. The ERJ-170/190 Series add STATUS messages.  Failures that effect dispatchability are presented to the flight crew at one of these levels.  Other failures may be presented only to the maintenance personnel on the Multi Function Display (MFD) maintenance pages or through the download of the Central Maintenance Computer (CMC).  System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator's standard maintenance program.

 

g.     GULFSTREAM (G-IV, G-V, GV-SP,GIV-X, G-150 and G-200)

 

Gulfstream airplanes equipped with EICAS provide different priority levels of system messages: WARNING (red), CAUTION (amber), ADVISORY, STATUS and MAINTENANCE (cyan or blue).  Any WARNING or CAUTION message affects airplane dispatch status and requires that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  STATUS messages  which indicate a system failure (e.g., FMS 1 fail) require that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  MAINTENANCE  messages do not affect airplane dispatch status. They indicate the presence of a system fault which can be identified by Maintenance Data Acquisition Unit (MDAU on the G-V) interrogation, Central Maintenance Computer (CMC on the GV-SP/GIV-X) interrogation or by reference to the Airplane Flight Manual. .

 

                FEDERAL AVIATION ADMINISTRATION         Page: IX

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 

Gulfstream mid-cabin airplanes (G-150, G-200) equipped with EICAS provide different priority levels of system messages: WARNING (red), CAUTION (amber), ADVISORY (green), and STATUS (white).  The Airplane Flight Manual prohibits take off with any WARNING message displayed.  CAUTION, ADVISORY and STATUS messages may affect airplane dispatch status and requires the Airplane Flight Manual or the MEL be used to determine dispatch capability.  The airplane may dispatch with CAUTION, ADVISORY and STATUS messages that indicate proper system operation and are not illuminated due to a system failure (i.e. FUEL STBY PUMP ON when the pump is selected ON, GND A/B OUT with LAND selected on the ground, or APU GEN OFF with the switch OFF).  MAINTENANCE and MAINTENANCE DATA STATUS messages do not affect airplane dispatch status.  They indicate the presence of a system fault which can be retrieved from the Maintenance Diagnostics Computer.  In all cases, the Airplane Flight Manual must be referenced and procedures compiled with for the displayed message prior to applying MEL dispatch relief.

 

h.    De-HAVILLAND  (DASH 8 SERIES 400)
 
Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all cautions and warnings. Advisory messages are displayed by the Electronic Indication System (EIS) or individual advisory lights supplied in the cockpit.
 
"Class 1 failures" are failures that prevent continued operation of a specific Line Replacement Unit or channel and are annunciated via advisory messages: caution, warning or advisory lights in the flight compartment. Dispatch with such posted failures are to be in accordance with the MMEL. 
 
"Class 2 failures" are failures which do not prevent continued system function. These faults will not be annunciated to the flight crew and the absence of the higher level alert (warning,  caution, advisory) indicates that the system/component is operating within its approved operating limits or tolerances.  Such faults would be evident during maintenance interrogation performed during maintenance activities. Class 2 faults do not affect dispatch and will be listed in the Fault Isolation Manual (FIM). Class 2 faults will be left to the discretion of the operators when these faults are to be rectified.

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.

 

                FEDERAL AVIATION ADMINISTRATION         Page: X

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 

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 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."

 

28.  “Considered Inoperative”, as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used or operated until the original deferred item is repaired. Additional actins include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repair category.

 

29. “Is not used” in the provisos, remarks or exceptions for an MMEL item may specify that another item relieved in the MMEL “is not used.” In such cases, crewmembers should not activate, actuate, or otherwise utilize that component or system under normal operations. It is not necessary for the operators to accomplish the (M) procedures associated with the item. However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crewmembers that a component or system is not used under normal operations.

 

30.  Nonessential equipment and furnishings (NEF) are those items installed on the aircraft as part of the original type certification, supplemental type certificate, or other form of alteration that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules.  They are those items that if inoperative, damaged or missing have no effect on the aircraft’s ability to be operated safely under all operational conditions.  These nonessential items may be installed in areas including, but not limited to, the passenger compartment, flight deck area, service areas, cargo areas, crew rest areas, lavatories, and galley areas.  NEF items are not items already identified in the MEL or CDL of the applicable aircraft.  They do not include items that are functionally required to meet the certification rule or for compliance

 

                FEDERAL AVIATION ADMINISTRATION         Page: XI

                                                       Revision: 13

                 MASTER MINIMUM EQUIPMENT LIST          Date: 09/11/2006

 

                             A-380

 

                          Definitions

 

with any operational rule.  Operator’s NEF process shall not provide for deferral of items within serviceable limits identified in the manufacturer’s maintenance manual or operator’s approved maintenance program such as wear limits, fuel/hydraulic leak rates, oil consumption, etc.  Cosmetic items that are fully serviceable but worn or soiled may be deferred under an operator’s NEF process.

 

 

                FEDERAL AVIATION ADMINISTRATION         Page: XII

                                                       Revision: 2

                 MASTER MINIMUM EQUIPMENT LIST          Date: 06/14/1989

 

                             A-380

 

                           Preamble

 

The following is applicable for authorized certificate holders operating under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The FAR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety. A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which take into consideration the operator's particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment.

 

Equipment not required by the operation being conducted and equipment in excess of FAR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.

 

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained.

 

                FEDERAL AVIATION ADMINISTRATION         Page: XIII

                                                       Revision: 2

                 MASTER MINIMUM EQUIPMENT LIST          Date: 06/14/1989

 

                             A-380

 

                           Preamble

 

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment.

 

The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative.

 

When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by FAR. Such documentation is required prior to operation with any item of equipment inoperative.

 

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered.

 

Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

 

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-1

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

01-01  PACK Pb-Sw FAULT Light

C

2

0

 

 

 

 

 

 

 

 

 

 

01-02  PACK Pb-Sw OFF Light

C

2

0

 

 

 

 

 

 

 

 

 

 

01-03  HOT AIR Pb-Sw FAULT Light

C

2

0

 

 

 

 

 

 

 

 

 

 

01-04  HOT AIR Pb-Sw OFF Light

C

2

0

 

 

 

 

 

 

 

 

 

 

01-05  CABIN AIR EXTRACT Pb-Sw OVRD Light

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

02-01  CABIN ALT MODE Pb-Sw MAN Light

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

02-02  CABIN V/S MODE Pb-Sw MAN Light

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

02-03  DITCHING Pb-Sw ON Light

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

02-04  CABIN ALT TRGT Selector

C

1

0

 

 

 

 

 

 

 

 

 

 

02-05  CABIN V/S TRGT Selector

C

1

0

 

 

 

 

 

 

 

 

 

 

03-01  BULK Cargo ISOL VALVES Pb-Sw FAULT Light

C

1

0

 

 

 

 

 

 

 

 

 

 

03-02  BULK Cargo ISOL VALVES Pb-Sw OFF Light

C

1

0

 

 

 

 

 

 

 

 

 

 

03-03  BULK Cargo HEATER Pb-Sw FAULT Light

C

1

0

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-2

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

03-04  BULK Cargo HEATER Pb-Sw OFF Light

C

1

0

 

 

 

 

 

 

 

 

 

 

03-05  AFT Cargo ISOL

***    VALVES Pb-Sw FAULT Light

C

1

0

 

 

 

 

 

 

 

 

 

 

03-06  AFT Cargo ISOL

***    VALVES Pb-Sw OFF Light

C

1

0

 

 

 

 

 

 

 

 

 

 

03-07  FWD Cargo ISOL

***    VALVES Pb-Sw FAULT Light

C

1

0

 

 

 

 

 

 

 

 

 

 

03-08  FWD Cargo ISOL

***    VALVES Pb-Sw OFF Light

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

04-01  CAB FANS Pb-Sw OFF Light

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

04-02  VENT EXTRACT Pb-Sw FAULT Light

C

1

0

 

 

 

 

 

 

 

 

 

 

04-03  VENT EXTRACT Pb-Sw OVRD Light

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

04-04  COOLG Pb-Sw FAULT Light

C

1

0

 

 

 

 

 

 

 

 

 

 

04-05  COOLG Pb-Sw OFF Light

C

1

0

 

 

 

 

 

 

 

 

 

 

21-01  Primary Cabin Fan

C

4

3

(O)One may be inoperative.

 

 

 

 

 

 

 

 

 

 

C

4

2

(O)Two may be inoperative provided both packs are operative.

 

 

 

 

 

 

 

 

 

21-02  Secondary Cabin Fans

C

-

-

(O)One or two may be inoperative.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-3

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

21-03  Forward Ventilation Controller Channel

C

2

1

(O)One may be inoperative.

 

 

 

 

 

 

 

 

 

21-04  Aft Ventilation Controller Channel

C

2

1

(O)One may be inoperative.

 

 

 

 

 

 

 

 

 

21-05  Forward Ventilation Control Redundancy Function

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

21-06  Aft Ventilation Control Redundancy Function

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

21-07  Lavatories and Galleys Extraction

C

1

0

(O)May be inoperative on ground provided one lavatories and galleys air extraction isolation valve is checked operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

(M)(O)May be inoperative on ground provided one lavatories and galleys air extraction isolation valve is deactivated in open position.

 

 

 

 

 

 

 

 

 

25-01  Pack Bay Ventilation

C

2

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

25-02  THS Bay Ventilation

C

1

0

(M)May be inoperative provided the absence of fuel leak in the THS bay is checked before each flight.

 

 

 

 

 

 

 

 

 

26-01  Avionics Ventilation Blowing Fan

C

2

1

(O)One may be inoperative provided the associated backup mode is checked operative.

 

 

 

 

 

 

 

 

 

 

C

2

1

(M)(O)One may be inoperative provided:

a)    Associated backup valve is deactivated open, and

b)    Associated backup mode is checked operative.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-4

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

26-02  Avionics Ventilation Filter

C

2

1

(M)(O)One may be clogged provided:

a)    Associated blowing fan is deactivated,

b)    Associated backup mode is checked operative, and

c)    The opposite blowing fan is operative.

 

 

 

 

 

 

 

 

 

 

C

2

1

(M)(O)One may be clogged provided:

a)    Associated blowing fan is deactivated,

b)    Associated backup valve is deactivated open,

c)    Associated backup mode is checked operative, and

d)    The opposite blowing fan is operative.

 

 

 

 

 

 

 

 

 

 

B

2

0

(M)(O)Both may be clogged provided:

a)    One filter is removed and the associated blowing fan is checked operative,

b)    The opposite blowing fan is deactivated, and

c)    The backup mode is checked operative

 

 

 

 

 

 

 

 

 

 

B

2

0

(M)(O)Both may be clogged provided:

a)    One filter is removed and the associated blowing fan is checked operative,

b)    The opposite blowing fan and backup valve are deactivated, and

c)    The backup mode is checked operative

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-5

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

26-03  Avionics Cooling Effect Detector

C

2

0

(M)May be inoperative provided:

a)    Associated cooling effect detector is deactivated,

b)    Associated blowing fan is checked operative before each flight

c)    Associated ventilation air flow is checked through the avionics racks before each flight, and

d)    Associated air filter is checked operative.

 

 

 

 

 

 

 

 

 

26-04  Avionics Extraction Auto Mode

C

1

0

(O)May be inoperative provided:

a)    The EXTRACT pb-sw is set to OVRD, and

b)    The overboard valve is indicated green partially open on ECAM COND page.

 

 

 

 

 

 

 

 

 

 

C

1

0

(M)(O)May be inoperative provided:

a)    The EXTRACT pb-sw is set to OVRD, and

b)    The overboard valve is deactivated partially open.

 

 

 

 

 

 

 

 

 

26-05  Avionics Overboard Valve Control on Ground

C

1

0

(O)May be inoperative provided the caution VENT AVNCS EXTRACT FAULT is not displayed on ECAM EWD after engine start.

 

 

 

 

 

 

 

 

 

27-01  Lower Deck Cabin

***    Crew Rest Compartment Ventilation

D

1

0

May be inoperative provided the lower deck cabin crew rest compartment is locked closed and placarded inoperative.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-6

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

27-02  Lower Deck Cabin

***    Crew Rest Compartment Isolation

D

1

0

(M)May be inoperative provided:

a)    Both isolation valves are deactivated in closed position, and

b)    The lower deck cabin crew rest compartment is locked closed and placarded inoperative.

 

 

 

 

 

 

 

 

 

28-01  BULK Cargo Ventilation

C

1

0

(O)May be inoperative provided the BULK VALVES pb-sw is set to OFF.

 

 

 

 

 

 

 

 

 

28-02  BULK Cargo Isolation

C

1

0

(O)May be inoperative provided procedures are established and used to ensure the aft and bulk cargo compartments remain empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits.

 

NOTE: Operator MELs must define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast.

 

 

 

 

 

 

 

 

 

 

C

1

0

(M)(O)May be inoperative provided the affected isolation valve is deactivated in closed position.

 

 

 

 

 

 

 

 

 

28-03  Aft Cargo

***    Ventilation

D

1

0

(O)May be inoperative provided the AFT ISOL VALVES pb-sw is set to OFF.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-7

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

28-04  Aft Cargo Isolation

***

D

1

0

(O)May be inoperative provided procedures are established and used to ensure the aft and bulk cargo compartments remain empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits.

 

NOTE: Operator MELs must define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast.

 

 

 

 

 

 

 

 

 

 

D

1

0

(M)(O)May be inoperative provided the affected isolation valve is deactivated in closed position.

 

 

 

 

 

 

 

 

 

28-05  Forward Cargo

***    Ventilation

D

1

0

(O)May be inoperative provided the FWD ISOL VALVES pb-sw is set to OFF.

 

 

 

 

 

 

 

 

 

28-06  Forward Cargo

***    Isolation

D

1

0

(O)May be inoperative provided procedures are established and used to ensure the forward cargo compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs), and/or Fly Away Kits.

 

NOTE: Operator MELs must define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast.

 

 

 

 

 

 

 

 

 

 

D

1

0

(M)(O)May be inoperative provided the affected isolation valve is deactivated in closed position.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-8

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

29-01  IFE Bay Ventilation

***

D

1

0

(O)May be inoperative provided the IFEC pb-sw is set to OFF.

 

 

 

 

 

 

 

 

 

29-02  IFE Bay Isolation

***

C

1

0

(M)May be inoperative provided:

a)    The IFE backup valve is deactivated in closed position, and

b)    The IFE bay ventilation is operative.

 

 

 

 

 

 

 

 

 

 

D

1

0

(M)(O)May be inoperative provided:

a)    The IFE backup valve is deactivated in closed position, and

b)    The IFEC pb-sw is set to OFF.

 

 

 

 

 

 

 

 

 

30-01  Cabin Altitude Manual Control

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

30-02  Cabin Vertical Speed Manual Control

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

30-03  Outflow Valve Automatic Control

C

4

2

(O)One or two may be inoperative.

 

 

 

 

 

 

 

 

 

 

C

4

1

(O)Three may be inoperative provided the caution CAB PRESS MAN CTL FAULT is not displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

30-04  Outflow Valve Automatic Control Redundancy Function

C

1

0

 

 

 

 

 

 

 

 

 

 

30-05  Outflow Valve

C

4

3

(O)One may be inoperative provided it is indicated closed on ECAM CAB PRESS page.

 

 

 

 

 

 

 

 

 

 

C

4

3

(M)One may be inoperative provided it is deactivated in closed position.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-9

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

30-06  Negative Relief Valves

C

2

1

One may be inoperative in closed position.

 

 

 

 

 

 

 

 

 

30-07  Cabin Pressure Landing Elevation

C

1

0

(O)May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

 

50-01  Pack

C

2

1

(O)One may be inoperative provided:

a)    Associated PACK pb-sw is set to OFF,

b)    Both associated pack valves are checked closed on ECAM BLEED page, and

c)    A check is made before each flight that, for the remaining pack, none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

C

2

1

(M)(O)One may be inoperative provided:

a)    Associated PACK pb-sw is set to OFF,

b)    Both associated pack valves are deactivated and secured in closed position, and

c)    A check is made before each flight that, for the remaining pack, none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O)Both may be inoperative provided:

a)    The flight is not pressurized,

b)    Both PACK pb-sw are set to OFF, and

c)    Both pack 1 and both pack 2 valves are deactivated and secured in closed position

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-10

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

50-02  Pack 1 Valve

C

2

1

(O)One may be inoperative provided it is indicated amber closed on ECAM BLEED page.

 

 

 

 

 

 

 

 

 

 

C

2

1

(M)(O)One may be inoperative provided it is deactivated and secured in closed position.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O)Both may be inoperative provided:

a)    The PACK 1 pb-sw is set to OFF,

b)    Both pack 1 valves are deactivated and secured in closed position, and

c)    A check is made before each flight that, for the pack 2, none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

50-03  Pack 2 Valve

C

2

1

(O)One may be inoperative provided it is indicated amber closed on ECAM BLEED page.

 

 

 

 

 

 

 

 

 

 

C

2

1

(M)(O)One may be inoperative provided it is deactivated and secured in closed position.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O)Both may be inoperative provided:

a)    The PACK 2 pb-sw is set to OFF,

b)    Both pack 2 valves are deactivated and secured in closed position, and

c)    A check is made before each flight that, for the pack 1, none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-11

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

50-04  Pack 1 Flow Sensor

C

2

1

(M)(O)One may be inoperative provided it is deactivated.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O)Both may be inoperative provided:

a)    They are deactivated, and

b)    A check is made before each flight that, for the pack 2, none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

50-05  Pack 2 Flow Sensor

C

2

1

(M)(O)One may be inoperative provided it is deactivated.

 

 

 

 

 

 

 

 

 

 

C

2

0

(M)(O)Both may be inoperative provided:

a)    They are deactivated, and

b)    A check is made before each flight that, for the pack 1, none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-12

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

50-06  Pack Temperature Regulation

C

2

1

(O)One pack may operate with degraded temperature regulation provided a check is made before each flight that, for the remaining pack, none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

C

2

1

(O)One pack may operate with degraded temperature regulation provided:

a)    Associated PACK pb-sw is set to OFF when flying at or below FL 290, and

b)    A check is made before each flight that, for the remaining pack , none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

50-07  Pack 1+2 Temperature Regulation Redundancy Function

C

1

0

(O)May be inoperative provided a check is made before each flight that none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-13

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

50-08  Pack Altitude Valve

C

2

1

(O)One may be inoperative provided:

a)    Associated PACK pb-sw is set to OFF when flying at or below FL 290, and

b)    A check is made before each flight that, for the remaining pack , none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

A

2

0

(M)May be inoperative for 50 consecutive calendar days provided the associated pack altitude valve is deactivated in closed position.

 

 

 

 

 

 

 

 

 

50-09  Pack Turbine Bypass Valve

A

4

2

(M)One on each pack may be inoperative for 50 consecutive calendar days provided the associated turbine bypass valve is deactivated and secured in closed position.

 

 

 

 

 

 

 

 

 

 

C

4

2

(O)One or both on the same pack may be inoperative provided:

a)    Associated PACK pb-sw is set to OFF when flying at or below FL 290, and

b)    A check is made before each flight that, for the remaining pack , none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-14

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

50-10  Pack Turbine Isolation Valve

C

2

1

(M)(O)One may be inoperative provided:

a)    Associated valve is deactivated in required position as described in the Aircraft Maintenance Manual, and

b)    A check is made before each flight that, for the remaining pack , none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

C

2

1

One may be inoperative provided the associated pack is considered inoperative.

 

 

 

 

 

 

 

 

 

50-11  Pack Ram Air Inlet Door Actuation

C

2

1

(M)(O)One may be inoperative provided:

a)    Associated ram air inlet door is deactivated and secured in open position, and

b)    A check is made before each flight that, for the remaining pack , none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

C

2

1

One may be inoperative provided the associated pack is considered inoperative.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-15

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

50-12  Pack Ram Air Outlet Door Actuation

C

4

0

(M)(O)May be inoperative provided the associated ram air outlet door is deactivated and secured in open position

 

 

 

 

 

 

 

 

 

 

C

4

0

May be inoperative provided the associated pack is considered inoperative.

 

 

 

 

 

 

 

 

 

50-13  Pack 1 Controller Channel

C

2

1

(M)(O)One may be inoperative provided the associated ram air outlet door is deactivated and secured in open position

 

 

 

 

 

 

 

 

 

 

C

2

0

May be inoperative provided pack 1 is considered inoperative.

 

 

 

 

 

 

 

 

 

50-14  Pack 2 Controller Channel

C

2

1

(M)(O)One may be inoperative provided the associated ram air outlet door is deactivated and secured in open position

 

 

 

 

 

 

 

 

 

 

C

2

0

May be inoperative provided pack 2 is considered inoperative.

 

 

 

 

 

 

 

 

 

 

50-15  Pack 1 Control Redundancy Function

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

50-16  Pack 2 Control Redundancy Function

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

50-17  Pack Airflow Selection

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-16

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

59-01  Supplemental Cooling System

C

2

0

(O)May operate with degraded cooling performance.

 

 

 

 

 

 

 

 

 

 

D

2

1

(M)(O)One may be inoperative provided it is deactivated.

 

 

 

 

 

 

 

 

 

 

D

2

0

Both may be inoperative provided the COOLG pb-sw is set to OFF.

 

 

 

 

 

 

 

 

 

59-02  Supplemental Cooling System Overheat Protection

D

2

0

(M)(O)May be inoperative provided the affected supplemental cooling system is deactivated.

 

 

 

 

 

 

 

 

 

60-01  Cabin Temperature Controller Channel

C

2

1

 

 

 

 

 

 

 

 

 

 

60-02  Cabin Temperature Control Redundancy Function

C

1

0

 

 

 

 

 

 

 

 

 

 

60-03  Cabin Temperature Control

C

1

1

(O)May operate in degraded mode.

 

 

 

 

 

 

 

 

 

60-04  Hot Air Valve

C

2

0

(O)May be inoperative provided the closure of both associated pack valves is checked operative on ECAM BLEED page.

 

 

 

 

 

 

 

 

 

60-05  Cabin/Cockpit
Trim Air Valve

C

16

0

(O)May be inoperative provided the closure of all pack valves is checked operative on ECAM BLEED page.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-17

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

60-06  Hot Air System

C

1

0

(M)(O)May be inoperative provided:

a)    Both trim air shut off valves are deactivated in closed position,

b)    Both hot air valves are deactivated in closed position,

c)    Both HOT AIR pb-sw are set to OFF,

d)    Both pack 1 valves are deactivated and secured in closed position,

e)    PACK 1 pb-sw is set to OFF, and

f)    A check is made before each flight that, for pack 2 , none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

C

1

0

(M)(O)May be inoperative provided:

a)    Both trim air shut off valves are deactivated in closed position,

b)    Both hot air valves are deactivated in closed position,

c)    Both HOT AIR pb-sw are set to OFF,

d)    Both pack 2 valves are deactivated and secured in closed position,

e)    PACK 2 pb-sw is set to OFF, and

f)    A check is made before each flight that, for pack 1 , none of the cautions listed in the operational procedure are displayed on ECAM EWD.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-18

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

60-07  Lower Deck Crew

***    Rest Trim Air Valve

D

1

0

(M)May be inoperative provided:

a)    It is deactivated in closed position, and

b)    The lower deck crew rest compartment is locked closed and placarded inoperative.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O)May be inoperative provided:

a)    The closure of both hot air valves is checked operative on ECAM COND page, and

b)    The lower deck crew rest compartment is locked closed and placarded inoperative.

 

 

 

 

 

 

 

 

 

60-08  Cabin Temperature Selection on FAP

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

60-09  Cabin Temperature Selection on AIR Overhead Panel

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

60-10  Cockpit Temperature Selection

C

1

0

May be inoperative provided cockpit temperature selection is suitable to flight crew.

 

 

 

 

 

 

 

 

 

60-11  Bulk Cargo Heater

C

1

0

(O)May be inoperative provided the BULK HEATER pb-sw is set to OFF.

 

 

 

 

 

 

 

 

 

60-12  Aft Cargo

***    Temperature Regulation

D

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

60-13  Aft Cargo

***    Trim Air Valve

D

1

0

(M)(O)May be inoperative provided it is deactivated in closed position

 

 

 

 

 

 

 

 

 

 

C

1

0

(O)May be inoperative provided the closure of both hot air valves is checked operative on ECAM COND page.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

21-19

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

21  AIR CONDITIONING

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

60-14  Aft Cargo Hot Air

***    System

C

1

0

(M)(O)May be inoperative provided:

a)    The aft cargo trim air valve is deactivated in closed position,

b)    The trim air shut off valve 2 is deactivated in closed position, and

c)    The hot air valve 1 is deactivated in closed position.

 

 

 

 

 

 

 

 

 

60-15  Forward Cargo

***    Temperature Regulation

D

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

60-16  Forward Cargo

***    Trim Air Valve

D

2

0

(M)(O)May be inoperative provided both forward Cargo trim air valves are deactivated in closed position

 

 

 

 

 

 

 

 

 

 

C

2

0

(O)May be inoperative provided the closure of both hot air valves is checked operative on ECAM COND page.

 

 

 

 

 

 

 

 

 

60-17  Forward Cargo Hot

***    Air System

C

1

0

(M)(O)May be inoperative provided:

a)    Both forward cargo trim air valves are deactivated in closed position,

b)    The trim air shut off valve 1 is deactivated in closed position, and

c)    The hot air valve 1 is deactivated in closed position.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

22-1

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

22  AUTO FLIGHT

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

10-01  Autopilot System

C

2

1

(O)One may be inoperative provided approach minimums do not require its use.

 

 

 

 

 

 

 

 

 

 

B

2

0

(O)May be inoperative provided:

a)    Approach minimums do not require their use,

b)    Enroute operations do not require their use, and

c)    Number of flight segments and segment duration is acceptable to flight crew.

 

 

 

 

 

 

 

 

 

10-02  Flight Director System

C

2

0

(O)May be inoperative provided operations or procedures do not require their use.

 

 

 

 

 

 

 

 

 

10-03  AUTOLAND Light

C

2

0

(O)May be inoperative provided approach minimums do not require use of autoland.

 

 

 

 

 

 

 

 

 

10-04  Automatic Roll Out Function

C

1

0

(O)May be inoperative provided approach minimums do not require its use.

 

 

 

 

 

 

 

 

 

10-05  Sidestick AP Locking Device

C

2

1

(O)One may be inoperative unlocked provided:

a)    The rudder pedals AP locking device is operative, and

b)    No autoland is performed.

 

 

 

 

 

 

 

 

 

 

C

2

0

(O)Both may be inoperative unlocked provided AP is not used.

 

 

 

 

 

 

 

 

 

10-06  Rudder Pedals AP Locking Device

C

1

0

(O)May be inoperative unlocked provided:

a)    Both sidestick AP locking devices are operative, and

b)    No autoland is performed.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O)May be inoperative unlocked provided AP is not used.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

22-2

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

22  AUTO FLIGHT

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

10-07  CAT 3 Dual Approach Capability

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

10-08  CAT 2 Approach Capability

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

30-01  Autothrust

C

4

0

(O)May be inoperative on all engines provided:

a)    Thrust lever position sensors are checked operative, and

b)    Approach minimums do not require use of autothrust.

 

 

 

 

 

 

 

 

 

30-02  Autothrust Instinctive Disconnect Pb

C

2

1

(O)One may be inoperative provided the other autothrust instinctive disconnect pb is checked operative.

 

 

 

 

 

 

 

 

 

 

B

2

0

(O)Both may be inoperative provided  autothrust disconnection is checked operative when thrust levers are set to idle.

 

 

 

 

 

 

 

 

 

70-01  Flight Management Computer

C

3

2

FMC-B or FMC-C may be inoperative.

 

 

 

 

 

 

 

 

 

 

C

3

2

FMC-A may be inoperative provided both ISIS are operative.

 

 

 

 

 

 

 

 

 

 

A

3

1

(O)Two may be inoperative provided:

a)    Both ISIS are operative,

b)    The FM selector is operative,

c)    Operations do not require its use, and

d)    Repairs are made within three flight legs.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

22-3

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

22  AUTO FLIGHT

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

70-02  FM Selector

C

1

0

(O)May be inoperative provided:

a)    All FMCs are operative, and

b)    Procedures do not require its use.

 

 

 

 

 

 

 

 

 

 

B

1

0

(O)May be inoperative provided:

a)    Two FMCs are operative,

b)    Both ISIS are operative, and

c)    Procedures do not require its use.

 

 

 

 

 

 

 

 

 

70-03  FM Navigation Database

C

-

-

(O)May be out of currency provided:

a)    Current Aeronautical Charts are used to verify Navigation Fixes prior to dispatch,

b)    Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and

c)    Approach Navigation Radios are manually tuned and identified.

 

 

 

 

 

 

 

 

 

80-01  AFS Control Panel

A

1

0

(O)May be inoperative for three flights provided one TCAS is operative.

 

 

 

 

 

 

 

 

 

80-02  AFS Control Panel and CAPT MFD FCU Backup

A

2

0

(O)Both may be inoperative for three flights provided:

a)    The F/O EFIS control panel is operative,

b)    The F/O MFD FCU backup is operative, and

c)    One TCAS is operative.

 

 

 

 

 

 

 

 

 

80-03  AFS Control Panel and F/O MFD FCU Backup

A

2

0

(O)Both may be inoperative for three flights provided:

a)    The CAPT EFIS control panel is operative,

b)    The CAPT MFD FCU backup is operative, and

c)    One TCAS is operative.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

22-4

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

22  AUTO FLIGHT

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

 

 

 

 

 

 

 

80-04  AFS Control Panel AP Pb

C

2

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

80-05  AFS Control Panel A/THR Pb

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

80-06  AFS Control Panel FD Pb

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

80-07  AFS Control Panel LOC Pb

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

80-08  AFS Control Panel ALT Pb

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

80-09  AFS Control Panel APPR Pb

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

80-10  AFS Control Panel Speed Selection Knob

B

1

0

(O)May be inoperative provided one MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

80-11  AFS Control Panel Heading/Track Selection Knob

B

1

0

(O)May be inoperative provided one MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

80-12  AFS Control Panel Altitude Selection Knob

A

1

0

(O)May be inoperative for three flights provided

a)    One MFD FCU backup is operative, and

b)    One TCAS is operative.

 

 

 

 

 

 

 

 

 

80-13  AFS Control Panel V/S FPA Selection Knob

C

1

0

(O)May be inoperative provided one MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided operations do not require its use.

 

 

 

 

 

 

 

 

 

80-14  AFS Control Panel Selection Window

C

4

0

(O)All may be inoperative.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

22-5

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

22  AUTO FLIGHT

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

80-15  AFS Control Panel HDG-V/S/TRK-FPA Pb

C

1

0

(O)May be inoperative provided one MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided the

HDG-V/S selection is operative.

 

 

 

 

 

 

 

 

 

80-16  AFS Control Panel MACH/SPD Pb

C

1

0

(O)May be inoperative provided one MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided the SPD selection is operative.

 

 

 

 

 

 

 

 

 

80-17  AFS Control Panel METER Pb

C

1

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

80-18  AFS Control Panel TRUE/MAG Pb

C

1

0

(O)May be inoperative provided one MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided the MAG selection is operative.

 

 

 

 

 

 

 

 

 

80-19  AFS Control Panel Pb Light

C

7

0

 

 

 

 

 

 

 

 

 

 

80-20  MFD FCU Backup

C

2

1

 

 

 

 

 

 

 

 

 

 

 

C

2

0

Both may be inoperative provided the AFS control panel is operative.

 

 

 

 

 

 

 

 

 

81-01  EFIS Control Panel

C

2

1

(O)One may be inoperative provided the associated MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

 

B

2

0

(O)Both may be inoperative provided both MFD FCU backups are operative.

 

 

 

 

 

 

 

 

 

81-02  EFIS Control Panel Barometric Reference Display Window

C

2

0

(O)May be inoperative.

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

                                       MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

REVISION NO :

ORIGINAL

PAGE:

 

 

A-380

DATE:

08/31/2009

22-6

 

 

SYSTEM &                  1.
SEQUENCE           ITEM

NUMBER

2.   NUMBER INSTALLED

 

 

 

3.   NUMBER REQUIRED FOR DISPATCH

 

 

 

 

 

 

22  AUTO FLIGHT

 

 

 

4.    REMARKS OR EXCEPTIONS

 

 

 

 

 

 

 

81-03  EFIS Control Panel Barometric Reference Selector Outer Ring

       (in Hg/hPa)

C

2

0

(O)May be inoperative provided the associated MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

 

C

2

0

(O)May be inoperative provided the required barometric reference unit for the intended flight is available on both EFIS control panels.

 

 

 

 

 

 

 

 

 

81-04  EFIS Control Panel Barometric Reference Selector Inner Knob

C

2

1

(O)One may be inoperative provided the associated MFD FCU backup is operative.

 

 

 

 

 

 

 

 

 

 

B

2

0

(O)Both may be inoperative provided both MFD FCU backups are operative.

 

 

 

 

 

 

 

 

 

81-05  EFIS Control Panel V V Pb