777 MEL - Korean Aircontents.koreanair.com/contents/Courses/SELIT/TechData...777 MEL Preamble Policy...

777 MEL Preamble Policy Section 1

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1-00-01-01 Policy

1. General

The Minimum Equipment List (MEL) for each aircraft type is prepared to comply with each respective FAA Approved Master MEL and FAA Approved Airplane Flight Manual (AFM). The authority to operate under the MEL is contained in KAL’s Operations Specifications D95

2. Regulatory Standards

A. Allowable Operation Standard: MEL

1) General

Modern transport aircraft is equipped with duplicated systems, components, instruments, electric communication facilities, structure, and important parts so that it may maintain its flight airworthiness and assure its reliability in spite of a malfunction of any parts. MEL is established for above reason. But MEL does not include items which are essentially required for the flight such as Wing, Rudder, Engine, Flap and Landing Gear and non-airworthiness related items like Cabin equipment, Cargo Loading Items, Minor airframe parts excluding major structure, etc.

2) Purpose

The purpose of the MEL is to dispatch the aircraft punctually within acceptable level of safety limit in operating the aircraft.

3) Creation and Revision

A) The MEL is created /revised in compliance with MMEL (Master MEL) which is approved by Airworthiness Authority of Manufacturer.

B) KAL MEL should be approved by the Korean Airworthiness Authority.

C) The MEL is complied with the KAL MEL of each aircraft type approved by the Korean Airworthiness Authority.

4) Application and Limitation


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A) When an abnormal condition covered by MEL occurs, the aircraft is applied per MEL by means of “Defer” referred to section 2. B. Classification and Policy for Defer.

B) Items or components which are not installed on the aircraft are not applied.

C) Items and contents which are not prescribed in this MEL follow the AFM or information from manufacturer

D) Optional item for operator’s convenience, affected items can be removed or block/deactivation or can be converted to the alternative way which does not affect airworthiness and safety.

B. Classification and Policy for Defer

1) Defer

“Defer” is used as a special term in Korean Air, which means to carry over the corrective action due to lack of parts, manpower, scheduled commitments, etc. Defect on the aircraft found on the base or at the station should be cleared before the flight. But if the defect doesn’t affect the airworthiness or the flight, the correction can be deferred. The defect will be corrected as an unscheduled maintenance.

2) Defer conditions are as follows:

A) Malfunction included in MEL Items For inoperative items covered by Minimum Equipment List (MEL), Flight Requirements of this policy is applied.

B) Malfunction included NEF (Nonessential Equipment & Furnishings) Items For inoperative items covered by NEF Program, the defer method and procedure are described in KALMOI I31503 NEF List and the policies are in MPPM PF-01-04 NEF Program. • Defects of non-airworthy items like cargo loading/unloading,

passenger convenience items, or Flight Crew/Flight Attendant Rest Area Convenience Items etc.

C) Malfunction has the allowable limits in Maintenance Manual or Maintenance Program. • Defects like fuel or hydraulic leaking, tire worn, window crack,

etc, are within Maintenance Manual limits. • Defects in aircraft structure/sub-structure are within manual

(AMM, Structural Repair Manual, etc.) limits or necessary


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actions for the defects are performed according to the recommendation of manufacturer/vendor

3) Defer Procedure

A) Deferred defects should be recorded on the flight log at the airport where the defects occurred.

B) If correction is available, it should be done immediately.

C) Defects affected by MEL should be corrected within the time limit excluding the calendar day the malfunction was recorded in the aircraft maintenance log and/or record.

D) Deferred defects and corrective actions should be recorded on the proper form besides the logbook. And the condition of the defect should be watched till the defect is totally cleared.

E) Detail procedure are described in ‘MPPM PF-01-02 Defer’

4) Scope of Repair Interval

A) Corrective actions for defects should be accomplished as soon as personnel, facility, equipment, property and time is secured. If it is impossible to correct defects, it can be defer. And in that case, it should be corrected by the time when is referred in Repair Interval designated as category.(Refer to page 1-00-01-03.3, Definition No.22 Repair Interval)

B) The above limit days are regarded as the term from midnight of the deferred date to midnight of the expired date. (Refer to page 1-00-01-03.3, Definition No.22 Repair Interval)

C) If the expire date falls on any day during schedule maintenance, it can be extended until the schedule maintenance are completed.

D) The certificate holder is authorized to use a continuing authorization to approve extensions to the maximum repair interval for category B and C items as specified in the approved MEL, provided those extensions are reported to the Korean Airworthiness Authority as soon as all their terminating actions are fully completed.

E) Detail procedures are described in 'MPPM PF-01-02 Defer'.

5) Decision to Defer


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A) Before door close: Captain, dispatcher, and the responsible maintenance personnel must exchange views with one and another regarding applicable defects. If the malfunction range may be satisfied in accordance with applicable standards, and acceptance level of safety is assured, the departure is released. The responsible maintenance personnel should provide information and explain about corrective action to captain or dispatcher if necessary.

B) After door close: The flight crew may defer as required by the designated MEL items. The aircraft may continue on a planned journey to a base where maintenance will repair or re-defer.

Crew Defer procedureThe procedure that the flight crew may apply when malfunction occurs between closing of the doors and increase of thrust for takeoff, and indicated by ‘Crew Defer’ in the ‘After Door Close’ column of the MEL.

Note) Flight crew must return to ramp when ‘Return To Gate’ is marked in the ‘After Door Close’ column of the MEL.

• If Crew Defer Procedure is applied by flight crew, accomplish the (O) procedure in the MEL before takeoff.

• The "INOPERATIVE" tabs located at the bottom of cockpit Aircraft Placard (KAL-MA-435A) must be torn off and placed on inoperative instruments, switches and lights.

• The flight crew notify the contents of Defer to MC with available communications (ACARS, SATCOM, etc.) after carrying out Crew Defer.

• If the flight is continued after applying the Crew Defer Procedure, the flight crew shall record the fact of carrying out the Crew Defer procedure based on MEL in the flight & maintenance log as the following before the flight duty ends.

‘Crew Defer’ designation was selected by cross-organizational team compromised of Operations Engineering, Flight


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Operations, Line Maintenance and Maintenance Engineering, and required as follows:

• Flight crew’s agreement. • Procedures does not require specialized knowledge or skill,

test equipment, tools, or disconnecting electrical or mechanical components.


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6) Action of the responsible maintenance personnel In case that the aircraft may be dispatched in accordance with this chapter, the responsible maintenance personnel should perform the following items.

A) Isolation of malfunction and placard The appropriate action should be performed to the defected part and other system or part related with defect should be ensured. Then, inoperative states or limited items about inoperative equipments must be placarded so that crew may not make the error of operation .

B) Record or Report The responsible maintenance personnel should record the necessary items in the flight log. Thereafter it shall be informed to captain or dispatcher by him, and informed from each station to another station of applicable route including main base. However if defect occurs after DOOR CLOSE for departure and it is satisfied with MEL, it could be recorded on aircraft flight log at arrival station.

7) Ferry Flight: Refer to Operations Specifications D084

3. Aircraft Configurations

This document uses specific terminology to define the various aircraft configurations: “Passenger” is any aircraft configured to carry only passengers on the main deck.

777 MEL Preamble Introduction Section 1

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1-00-01-02 Introduction

1. Document Content and Organization

The MEL is divided into three sections as follows:

Section 0 - Front Material This section provides Control Page, Record of Revision and List of Effective Pages.

Section 1 - Preamble This section provides Policy, Introduction, Definition, Required Systems or Equipments List and EICAS.

Section 2 – Minimum Equipment List Items For ease of use, page numbering uses the MEL item number as follows:

2-XX-XX-XX.X

2. Allowable Operation Standard Requirements

A. Standard about each item must be arranged according to aircraft model in case of aircraft’s departure.

B. Contents per item of MEL are as follows.

XX-XX ITEM NAME XX-XX-XXXX-XX-XXA SUB-ITEM NAME

Interval Installed Required Procedure After Door Close

(Colum1) (Colum2) (Colum3) (Colum4) (Colum5)

(REMARKS OR EXCEPTIONS)

PLACARD

MAINTENANCE (M) and/or OPERATIONS (O)

MAINTENANCE NOTE and/or OPERATIONS NOTE

1stROW

2ndROW

3rdROW

4thROW

Page Number MEL Item Number MEL Section Number

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1) 1st Row : Item number and name included sub-items

2) 2nd Row : This Row consists of 5 Columns

A) Column 1: "Interval" It indicates category A,B,C and D that means the period of defer. The limitation of correction for the deferred item is as followings. Refer to 1-00-01-03 Definition No. 22 Repair Intervals.

B) Column 2 : " Installed " Refer to 1-00-01-03 Definition No.1 System Definitions.

C) Column 3 : "Required" Refer to 1-00-01-03 Definition No.1 System Definitions.

D) Column 4: "Procedure" Refer to definition No.15,16 for more details. Special marks to be used in this MEL are as follows. � (O) : Refer to 1-00-01-03 Definition No.16 (O) symbol. � (M) : Refer to 1-00-01-03 Definition No.15 (M) symbol. � - : Refer to 1-00-01-03 Definition No.5 “-” symbol.

E) Column 5: "After Door Close" Refer to 1-00-01-03 Definition No.1 System Definitions.

3) 3rd Row : REMARKS OR EXCEPTIONS - Refer to 1-00-01-03 Definition No.1 System Definitions.

4) 4th Row : This row includes MAINTENANCE (M) and/or OPERATIONS (O), and MAINTENANCE NOTE and/or OPERATIONS NOTE

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Preamble Definition Section 1

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1-00-01-03 Definition 1. Accessible Lavatory Items. Accessible lavatory items include: ability to enter

lavatory and maneuver by means of on-board wheelchair. The lavatory shall provide accessible door locks, call buttons, grab bars, faucets, other controls, and dispensers. As an air carrier, you must maintain all aircraft accessibility features in proper working order.

2. Administrative Control Item (ACI). An ACI is listed by the aircraft operator in the MEL for tracking and informational purposes. As an example, ACI may be used to track ETOPS accomplishment of required APU cold-soak, or in-flight verification starts. An ACI may be added to an aircraft operator’s MEL by approval of the POI provided no relief is granted, or provided conditions and limitations are contained in an approved document (e.g., Structural Repair Manual (SRM) or Airworthiness Directive (AD)). If relief other than that granted by an approved document is sought for an ACI, 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 ACI

3. ATA System Page. The ATA system page is divided into four (4) columns and contains: item and repair category; number installed; number required for dispatch; and remarks or exceptions. Standard ATA categories are used. Items are numbered sequentially.

A. Item. This column depicts the equipment, system, component, or function listed in the “Item” column.

B. Repair Category. See definition #24. C. Number Installed. This column depicts the number (quantity) of

instrument and equipment items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MEL. Should the number be a variable (e.g., fleet configuration differences, cockpit lighting items, cabin lighting items, cargo restraint components) a number is not required and the “-” symbol is used.

D. Number Required for Dispatch. This column depicts the minimum number (quantity) of instrument and equipment items required for operation provided the conditions specified in the “Remarks or Exceptions” column are met. 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.

E. Remarks or Exceptions. This column may include a statement(s) either prohibiting or permitting operation with a specific number of instrument and equipment items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

F. Provisos. Provisos are indicated by a number or a lower case letter in

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“Remarks or Exceptions”. Provisos are conditions or limitations that must be complied with for operation with the listed instrument or equipment item inoperative.

G. Notes. Notes provide 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 aircraft operator of the responsibility for compliance with all applicable requirements. Additional notes may be amended, deleted, or added to the MEL by the aircraft operator, as appropriate. Notes are not a part of the provisos.

H. Vertical Bar (change bar). A vertical bar Indicates a change, addition, or deletion in the adjacent text for the current revision of that page only. All change bars applicable to the previous revision of the MMEL are removed prior to the release of the next revision.

4. The approved flight manual for the specific aircraft is listed on the applicable Type Certificate Data Sheet (TCDS). The approved flight manual is the source document for operational limitations and performance parameters for an aircraft. The term “approved flight manual” can apply to an AFM.

5. Reserved 6. Reserved 7. Considered Inoperative. The phrase, “Considered Inoperative”, as used in

the provisos, means that an instrument and equipment item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item will not be used or operated until the original deferred item is repaired. Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MEL provisions, including any (M) and (O) procedures and observing the repair category.

8. Continuing Authorization – Single Extension. An aircraft operator who has the authorization to use an approved MEL may also have the authority to use a continuing authorization to approve a single (one-time) extension to the repair interval for category B or C items in accordance with Operations Specification D095. Continuing Authorization – Single Extension is not authorized for repair category A and D items.

9. Dash (-). Indicates a variable number (quantity) of the instrument and equipment items may be installed or required for dispatch. This is common when a fleet MEL is used since aircraft of the same make and model may have differing numbers of specific instrument and/or equipment items installed.

10. Day of Discovery. This is the calendar-day an equipment/instrument malfunction was recorded in the aircraft maintenance record/logbook. This day is excluded from the calendar-days or flight-days specified in the MEL for the repair interval of an inoperative instrument and/or equipment item. This provision is applicable to all MEL items; i.e., categories A, B, C, and D.

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11. Deactivated and/or Secured. When the MEL refers to an instrument and/or equipment item as deactivated and/or secured, the specified component must be put into an acceptable condition for safe flight. An acceptable method of deactivating and/or securing will be established by the aircraft operator.

12. Deleted. "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.

13. Extended Range Operations (ER). ER refers to extended range operations (ETOPS) of an airplane with operational approval to conduct ETOPS in accordance with the applicable regulations.

14. Excess Items. Excess items are those instrument and equipment items that have been installed that are redundant to the requirements.

15. Flight Day. A flight-day is a 24-hour period (from midnight to midnight) either universal coordinated time (UTC) or local time, as established by the aircraft operator, during which at least one flight is initiated for the affected aircraft.

16. Heavy Maintenance Visit (HMV). HMV is a scheduled C-check/D-check or airworthiness maintenance program inspection where the aircraft is scheduled to be out of service for 4 or more days.

17. Icing Conditions. An atmospheric environment that may cause ice to form on the aircraft (structural) or in the engine(s) (induction).

18. Inoperative. 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) and/or tolerance(s).

19. Inoperative Components of an Inoperative System. Inoperative instrument and equipment items, which are components of a system that 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 MEL).

20. Is Not Used. The phrase “Is Not Used” in the provisos, remarks or exceptions for an MEL instrument or equipment item may specify that another item in the MEL “is not used”. In such cases, crewmembers must not activate, actuate, or otherwise utilize that item under normal operations. It is not necessary for aircraft operators to accomplish the (M) procedure(s) 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. This informs crewmembers that an instrument or equipment item is not to be used under normal operations.

21. Nonessential Equipment and Furnishings (NEF). NEFs are those items installed on the aircraft as part of the original type certification (TC), STC, or other form of alteration that have no effect on the safe operation of flight and

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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. NEF items are not instrument and equipment items already identified in the MEL or CDL of the applicable aircraft. They do not include instrument and equipment items that are functionally required to meet the certification rule or for compliance with any operational rule.

22. Operative. An operative system and/or component will accomplish its intended purpose and is consistently functioning normally within its design operating limit(s) and tolerance(s). When an MEL item specifies that an item of equipment must be operative, it does not mean that it’s operational status must be verified; it’s to be considered operative unless reported or known to be malfunctioning. When an MEL item specifies that an item of equipment must be verified operative, it means that it must be checked and confirmed operative at the interval(s) specified for that MEL item. When an MEL item specifies that an item of equipment must be verified but no interval is specified, verification is required only at the time of deferral. Other terminology sometimes used interchangeably with “operative” within the MEL is “operates normally”, "fully operative", and "considered operative”.

23. Placarding. Each inoperative instrument or equipment item must be placarded to inform and remind the crewmembers and maintenance personnel of the item condition. To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified (i.e. AFM), placard wording and location will be determined by the aircraft operator.

24. "Day Operation" means an any flight conducted from the point of take off to that of landing between 30 minutes before sunrise and 30 minutes after sunset.

25. Extended Overwater Operation: Any flight conducted over 50 nautical mile distance from the nearest coast.

26. "Approach minimums" is the requirement for CAT-II/III operations. Required number of system(s) or equipment(s) for dispatch is listed in 0-4 CAT-II/III Operation Equipment List.

27. "Over-the-top" means above the layer of clouds or other obscuring phenomena forming the ceiling, under VFR when it is not being operated on an IFR flight plan.

28. Area Navigation (RNAV) is defined as a method of navigation which permits aircraft operation on desired flight path within the coverage of ground navigation facilities or within the capability of self-contained navigation aids, or a combination of these. a. B-RNAV Operation Procedures

Basic Area Navigation (B-RNAV) is a navigation performance which is a required track-keeping accuracy of ± 5NM for at least 95% of flight time in European airspace.

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b. P-RNAV Operation Procedures in Europe Precision Area Navigation (P-RNAV) is a navigation performance requirement for RNAV instrument flight procedure in designated European terminal airspace. It requires aircraft conformance to a track-keeping accuracy of ± 1NM for at least 95% of flight time.

29. RNP-X : It requires aircraft performance to a track-keeping accuracy of ± X NM (1 : terminal, 4 or 10 : oceanic) for at least 95% of flight time. On-board performance monitoring and alerting are required.

30. RNP AR approach is defined as an RNP approach procedure that requires a lateral TSE(Total System Error) as low as +/- 0.1 NM on any segment of the approach procedure and also require that a specific vertical accuracy be maintained.

31. North Polar Region: the area north of 78 degree north. 32. Cross Polar Routes general

The current cross polar routes established between North America and Asia consists of 4 routes that is polar 1,2,3,4. of above 4 KAL use Polar 3 and Polar 4.these two routes locates Canadian ACA and Russia Magadan OCA airspace. Polar 3 route pass up to 85N while polar 4 passes south of 80N.

33. "Once each flight day" means that these items are required to be checked at least once each flight day. This check need not be performed prior to the first flight of the day, but at least once each flight day.

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777 MEL

Preamble Enroute Operations Requirements Section 1

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1-00-01-04 Required Systems or Equipments List for : This section provides the systems or equipments required to perform specific operations. 1. CAT-II/III Operation

Listed System(s) or equipment(s) must comply requirements to perform applicable CAT-II/III operation.

MEL Item No.

Required Equipment or

System

No. Installed

CAT-II

CAT-IIIa

CAT-IIIb

POM

System CAT-II

CAT-IIIa

CAT-IIIb

22-11-01 Autopilot Flight

Director Computer (AFDC)

3 2 2 3 AFDC 2 2 3

Autopilot 2 2 3

22-11-02 Autopilot Backdrive Actuator Systems

2 1 1 2

Autopilot Backdrive Actuator System

1 1 2

22-11-06-01 MCP - A/P Engage Switches 2 1 1 1

Autopilot Engage Switch

1 1 1

22-11-06-08 MCP - APP Switch 1 1 1 1 APP Switch 1 1 1

22-11-08

Control Wheel Autopilot Disconnect Switches

2 2 2 2 Autopilot

Disconnect Switch

2 2 2

22-11-09 Takeoff/Go-Around (TO/GA) Switches

2 1 1 2 TO/GA Switch 1 1 2

22-11-10 Flight Director Systems 2 2 2 2

Flight Director Display 2 2 2

22-11-06-04 MCP - F/D Switches 2 2 2 2

22-31-01 Autothrottle System 1 0 1 1

Autothrottle System and disconnect

warning

0 1 1

22-11-06-02 MCP - Autothrottle Arm Switches (A/T ARM L,R)

2 0 2 2

22-11-06-03 MCP - A/T Engage Switch 1 0 1 1

22-31-02 Autothrottle Servo Motors 2 0 2 2

22-31-03 Autothrottle Disconnect Switches

2 0 2 (a) 2 (a) Autothrottle Disconnect

Switch 0 2 2

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MEL Item No.


System

No. Installed

CAT-II

CAT-IIIa

CAT-IIIb

POM

System CAT-II

CAT-IIIa

CAT-IIIb

30-41-01

Flight Deck Forward Window Primary Heater Systems

2 1 (b) 1 (b) 1 (b) Window Heat on Window FWD+No2

3 3 3

30-42-01 30-42-01-02

Windshield Wipers (- High Speed Function)

2 2 2 2 Windshield wipers (High) 2 2 2

31-51-05

Warning Electronic System (WES) - Autopilot Disconnect Warning Function

1 1 1 1 Autopilot

Disconnect Warning

1 1 1

32-42-01 Normal Antiskid Valve 12 10 12 12

Anti-skid 0 1 1

32-42-02 Antiskid Wheelspeed Transducer

12 10 12 12

32-42-04

Autobrake System (Including Autobrake Solenoid Valve)

1 0 1 1

Autobrake or ADIRU

Groundspeed Indications

0 1 1

34-21-03-01 ADIRU Faults 1 0 (c) 0 (c) 1 ADIRU 1 1 1

34-21-04-01 Right Pitot Air Data Module 1

2 2

1

ADM's Pitot and Static 2 2 3

34-21-04-02 Left Pitot Air Data Module 1 1

34-21-04-03 Center Pitot Air Data Module 1 1

34-21-05-01 Right Static Air Data Module 1

2 2

1

34-21-05-02 Left Static Air Data Module 1 1

34-21-05-03 Center Static Air Data Module 1 1

34-31-01 Instrument Landing System (ILS)

3 2 2 3 ILS receiver 2 2 3

34-32-01 Marker Beacon System 1 1 1 1

Marker Beacon

Indications or Equivalent

2 (e) 2 (e) 2 (e)

34-33-01 Radio Altimeter System 3 2 2 3 Radio

Altimeter 2 2 3

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MEL Item No.


System

No. Installed

CAT-II

CAT-IIIa

CAT-IIIb

POM

System CAT-II

CAT-IIIa

CAT-IIIb

22-11-07 Automatic Landing System (Autoland) 1 1 1 1

Additional Maintenance Requirement for CAT-II/III Operation

22-11-07-01 Triple Channel Autoland (LAND 3) 1 0 0 1

27-02-03 Primary Flight Computer (PFC) Channels

3 2 2 3

27-02-04 PFCS Interface 1 0 0 0 (d) 30-31-01-01 Right Pitot Heater 1

0 0

1 30-31-01-02 Left Pitot Heater 1 1

30-31-01-03 Center Pitot Heater 1 1

34-21-07 SAARU 1 0 0 1

34-31-02 Glide Slope Antenna Switching 3 2 2 3

34-31-03 Localizer Antenna Switching 3 2 2 3

PFDs (Independent) 2 2 2

NDs 2 2 2 AFDS FMA /

Autoland Status

Annunciation

2/2 2/2 2/2

Minimum Display (RADIO)

2 2 2

Nose wheel Steering 0 1 1

ILS Deviation 2 2 2 Normal Flight

Controls Required

Required

Required

Hydraulic Systems 2 2 3

ENG operating 1 1 2

(a) One may be inoperative provide both A/T ARM switches operate normally. (b) L/H Forward and Both No.2(L/H and R/H) window heaters must be operative. (c) Cat-II operation is available with ADIRU status message displayed but ADIRU must

be operative. (d) Refer to applicable MEL operation note.

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(e) Appropriate marker beacon information, or equivalent, must be displayed to each pilot for outer, middle and inner markers. The appropriate equivalent information, such as a precision or surveillance radar fix, a designated NDB, VOR, DME fix, or a published minimum Glide slope interception Altitude fix, may be used as a substitute for the outer marker beacon information.

Note: “Approach minimums” is requirement for CAT-II/III operation. Required number of system(s) or equipment(s) for dispatch is listed in CAT-II/III Operation Equipment List.

2. RNAV or RNP Operation

RNAV/RNP Requirement

Minimum Aircraft RNAV System Requirement Remark

FMS IRS VOR DME GPS NAV DB

ENROUTE RNAV 5 1 1 2

or 1 1 1 1 or 1 1 1

RNAV 2 1 1 1 1 or 1 1 2 1 or 1 1 1 1 1

OCEANIC ENROUTE

RNP 4 1 1 2 ADS/ CPDLC required

RNP 10 1* 1 1 1 *Refer FOM

10.3.3 or 1* 1 2 or 1* 1 1

TERMINAL RNAV 1 or 2 1 1 1 1

or 1 1 2 1 or 1 1 1 1 1 RNP 1 1 1 1 1 or 1 1 2 0(a) 1

APPROACH RNP 0.3 2 1 1 1 2 1

or 2 1 2 2 1

(a) If required SID / STAR charts in JPSN clearly specify it, DME/DME or DME/DME/IRU may be usable for the RNP 1

777 MEL PREAMBLE EICAS Messages Section 1

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1-00-02-00 EICAS Message - Table of Contents

EICAS Message - Introduction ............................................. 1-00-02-01 EICAS Message - Cross Reference List .............................. 1-00-02-02

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777 MEL Introduction EICAS Messages Section 1

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1-00-02-01 EICAS Message - Introduction

Introduction - EICAS Messages Cross Reference List A Cross Reference List of Engine Indication and Crew Alerting System (EICAS) messages and corresponding MEL items is provided in this section. The Cross Reference List is intended to assist operators in quickly identifying the proper MEL item to consult for possible dispatch relief. All EICAS messages at Status level or higher are listed by message text in alphabetic order. A description of the information provided in each column of the Cross Reference List follows.

Message Text This column alphabetically lists each message exactly as they would appear on EICAS.

Level The appropriate EICAS message level is listed: Warning, Caution, Advisory, Memo, Comm, or Status.

MEL Item This column lists the appropriate MEL item(s) to consult for possible dispatch relief with the associated message displayed. EICAS messages that do not have a specific MEL item to allow dispatch are listed with one of the following cross references:

N/A Not Applicable: There is no MEL item listed because the message does not indicate a system failure.

None There is no MEL item for the failure condition indicated by this message. NO DISPATCH


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EICAS Messages EICAS is the primary means of displaying airplane system information to the flight crew. EICAS consolidates engine and subsystem indications and provides a centrally located crew alerting function. EICAS displays System Alerts (Warning, Caution, and Advisory), Communication Alerts, Memo messages, and Status messages.

Warning A non-normal operational or system condition displayed in red text accompanied by annunciation of the master warning lights and an aural tone. Immediate crew awareness and corrective action is required.

Caution A non-normal operational or system condition displayed in amber text accompanied by annunciation of the master caution lights and an aural tone. Immediate crew awareness is required and corrective action may be required.

Advisory A non-normal operational or system condition displayed in amber text without other visual or aural annunciations. Routine crew awareness is required and corrective action may be required.

Comm A reminder of normal incoming flight crew communications displayed in white text.

Memo A reminder of a normal condition in white text that indicates the current state of certain manually and automatically configured airplane systems.

Status A system condition which affects airplane dispatch, displayed in white text on the MFD status page. Status messages are checked prior to engine start and the condition should be corrected or dispatched per the operator’s MEL. There are no inflight crew procedures associated with Status messages.


1-00-02-01.3 27 JUN 2011

Maintenance Level Messages Maintenance level messages are not included in the Cross Reference List, since they do not affect the airworthiness release of the airplane. Maintenance level messages are provided by EICAS and the Central Maintenance Computing System (CMCS) as follows:

Scheduled Maintenance Task (SMT): These are a special category of EICAS messages that are uniquely associated with a Certification Maintenance Requirement (CMR) or a Scheduled Maintenance Task (SMT). They are displayed on a special MFD maintenance page. SMT messages are checked as a result of a specified maintenance task defined by the CMR or maintenance program requirement, which also defines a specific time interval when corrective maintenance action is required. There is no requirement to check SMT messages prior to each flight. SMT messages are not included in the Cross Reference List.

Central Maintenance Computing System (CMCS) Messages: The Central Maintenance Computing Function of the Onboard Maintenance System processes BITE fault reports into maintenance messages. These are nonessential messages that are displayed on the Maintenance Access Terminal (MAT). Maintenance messages are not displayed on EICAS and they are not used to determine the airworthiness of the airplane. They provide diagnostic information useful in troubleshooting or maintenance planning. There are two general types of CMCS maintenance messages: correlated and uncorrelated. Correlated messages are associated with a specific EICAS message or other flight deck effect. Each fault indicated by an EICAS message has at least one correlated maintenance message to assist the maintenance personnel in determining the root cause of the fault indicated on EICAS. Uncorrelated messages do not have a corresponding flight deck effect. Some uncorrelated messages, known as Maintenance Memos, provide information regarding the condition of a redundant component or system that is installed to enhance departure reliability, but is not required for certification. Maintenance Memos provide airline maintenance departments the ability to monitor system degradation and plan appropriate action before annunciation of an EICAS message which affects the airworthiness release of the airplane. CMCS maintenance messages are not included in the Cross Reference List.


1-00-02-01.4 27 JUN 2011

Considerations for Dispatch with Displayed EICAS and CMCS MessagesAny monitored faults that affect airplane dispatchability will be displayed on EICAS as a Status or Alert level (Warning, Caution, Advisory) message, with a corresponding correlated maintenance message. System faults displayed at Status level or Alert level should be resolved by MEL compliance or maintenance action prior to engine start. After engine start, EICAS Alert messages are the primary means of alerting the crew to non-normal conditions or improper configuration. Display of any Alert message requires accomplishment of the appropriate non-normal procedure by the crew. Upon completion of the procedure and prior to takeoff, the operator’s MEL should be consulted to determine if relief is available for continued operation with system faults displayed at the Alert level (Warning, Caution, Advisory).

Any system faults that result only in a SMT message or a CMCS maintenance message do not require MEL consideration or maintenance action prior to dispatch. They are addressed within an operator’s standard maintenance program.

Considerations for Dispatch Using Synoptic Displays Airplane system faults and/or ARINC 629 communication faults may result in missing information on synoptic displays. Missing data may include any synoptic display element such as flow bars, pump or valve symbols, and digital indications. Display elements may be absent from one, two, or all three Multi-Function Displays. Missing information on a specific synoptic page caused by an ARINC 629 communication fault is not indicative of a fault in the system associated with that synoptic page. Decisions regarding dispatch should be based on EICAS Status or Alert level messages and/or other flight deck effects.

777 MEL

PREAMBLE EICAS Messages Section 1

1-00-02-02.1 23 OCT 2013

1-00-02-02 EICAS Message - Cross Reference List

- L (Message Level) : W (Warning), C (Caution), A (Advisory), M (Memo), S (Status), COM (Comm), N (Nuisance)

- A/D/C(After Door Close) : RTG(Return to gate), CD(Crew Defer) - During engine start and prior to take-off, it is not necessary to check status

messages as any message having an adverse effect on safe continuation of the flight, and requiring crew attention, will appear as an EICAS alert message (warning, caution, or advisory). But Particular MEL items can be only distinguishable by checking with the combination of EICAS alert and status messages. So the EICAS status message may be required to be checked when identifying which MEL item is applicable.

Message L Condition MEL Item A/D/C

A/P DISC WARN SYS S

Warning Electronic System (WES) Autopilot Disconnect Warning Function 31-51-05 RTG

Warning Electronic System (WES) Autopilot Disconnect Warning Function

- WES Autopilot Interfaces31-51-05-01 RTG

ACTUATOR PRESS SNSR S Actuator Pressure Sensors 27-02-05 CD

ADF L S ADF Systems 34-57-01 CDADF R S ADF Systems 34-57-01 CD

ADIRU S

Air Data Inertial Reference Unit (ADIRU)- ADIRU Faults- Ground Nav (Navigational Facility) Available

34-21-03-01A RTG

Air Data Inertial Reference Unit (ADIRU)- ADIRU Faults- Ground Nav (Navigational Facility) Not Available

34-21-03-01B RTG

ADIRU ALIGN MODE M N/A

ADS-B OUT L AATC Transponder/Automatic Altitude Reporting

Systems- ADS-B Squitter Transmissions

34-53-01-02 CD

ADS-B OUT L S ADS-B OUT L 34-53-01-02 CD

ADS-B OUT R AATC Transponder/Automatic Altitude Reporting

Systems- ADS-B Squitter Transmissions

34-53-01-02 CD

ADS-B OUT R S ADS-B OUT R 34-53-01-02 CD

AFDC CAFDC LAFDC R

S Autopilot Flight Director Computers (AFDC)– One Inoperative 22-11-01A RTG

S Autopilot Flight Director Computers (AFDC)– Two Inoperative 22-11-01B RTG

S Autopilot Flight Director Computers (AFDC)– All Inoperative 22-11-01C RTG

AFT CGO A/C EXH SOV S ACAC Exhaust Shutoff Valve 21-28-04 RTG

777 MEL


1-00-02-02.2 23 OCT 2013

AILERON ACTUATOR SAileron Power Control Units (PCUs)- Passenger (300ER or -200/-300 equivalent SBs

incorporated)27-11-03-01 RTG

AIMS S No Dispatch

AIMS CABINET BUS S Airplane Information Management System (AIMS)- AIMS-II Cabinet Bus 31-41-03-01 CD

AIR/GROUND L S Air/Ground System - Weight on Wheels- Left System Inoperative 32-09-01A RTG

AIR/GROUND R S Air/Ground System - Weight on Wheels- Right System Inoperative 32-09-01B RTG

AIR/OIL VLV CLOSED L S No DispatchAIR/OIL VLV CLOSED R S No DispatchAIR DATA SYS C No DispatchAIRSPEED LOW C N/AALTITUDE ALERT C N/AALTITUDE ALERT SYS S Altitude Alerting System 34-16-01 RTG

ALTITUDE CALLOUTS AGround Proximity Warning System (GPWS)GPWS FunctionAdvisory Callouts (Mode 6)

34-46-01-01-03 CD

ALTN ATTITUDE A N/A

ALTN GEAR EXTEND SLanding Gear Alternate Extend System 32-35-01 RTGLanding Gear Alternate Extend System- Alternate Extend Hydraulic Pressure Switch 32-35-01-01 RTG

ALTN PITCH TRIM LEV S Alternate Pitch Trim Position Switches 27-41-02 CD

ALTN VENT SYS A

Status Msg : LAV-GALLEY SOVLavatory/Galley Ventilation Shutoff Valve 21-26-07 RTG

Status Msg : AVS FANAlternate Ventilation System Fan 21-26-08 RTG

Status Msg : AVS FWD SOVAlternate Ventilation System Shutoff Valves 21-26-09 RTG

Status Msg : AVS SWITCHAlternate Ventilation System ALTN VENT Switch 21-26-10 CD

ANTI-ICE ENG LANTI-ICE ENG RANTI-ICE LEAK ENG LANTI-ICE LEAK ENG RANTI-ICE LOSS ENG LANTI-ICE LOSS ENG R

AACCAA

Engine Anti-Ice Systems(Valve is locked closed) 30-21-01 RTG

Engine Anti-Ice Systems- PW- OAT 38 Degrees C or Below, With Deactivation Kit

Installed

30-21-01-01A RTG

Engine Anti-Ice Systems- PW- OAT 38 Degrees C or Below, Without Deactivation Kit

Installed

30-21-01-01B RTG

Engine Anti-Ice Systems- PW- OAT Above 38 Degrees C, With Deactivation Kit

Installed

30-21-01-01C RTG

777 MEL


1-00-02-02.3 23 OCT 2013

Engine Anti-Ice Systems- PW- OAT Above 38 Degrees C, Without Deactivation Kit

Installed

30-21-01-01D RTG

Engine Anti-Ice Systems- GE- OAT 38 Degrees C or Below, With Deactivation Kit

Installed

30-21-01-02A RTG

Engine Anti-Ice Systems- GE- OAT 38 Degrees C or Below, Without Deactivation

Kit Installed

30-21-01-02B RTG

Engine Anti-Ice Systems- GE- OAT Above 38 Degrees C, With Deactivation Kit

Installed

30-21-01-02C RTG

Engine Anti-Ice Systems- GE- OAT Above 38 Degrees C, Without Deactivation Kit

Installed

30-21-01-02D RTG

ANTI-ICE ON A N/A

ANTI-ICE WING AWing Anti-Ice Systems 30-11-01 RTGWing Anti-Ice Control (Card and Switch) 30-11-02 RTG

ANTISKID A No Dispatch RTGANTISKID S No Dispatch RTGANTISKID ALTN VALVE S Alternate Antiskid Valves 32-42-03 RTG

ANTISKID NORM VLV LANTISKID NORM VLV R

SS

Normal Antiskid Valves- Deactivation Tool Used 32-42-01A RTG

Normal Antiskid Valves - Brake Line Capped 32-42-01B RTG

ANTISKID XDCR LANTISKID XDCR R

SS Antiskid Wheel speed Transducers 32-42-02 RTG

AOA VANE LAOA VANE R

SS Angle of Attack (AOA) Vane Systems 34-21-06 CD

APU S Auxiliary Power Unit (APU) 49-11-01 CDAPU AIR STARTER S APU Air Turbine Starter 49-43-01 CD

APU BATTERYAPU BATTERY OVHT

SS

APU Battery- APU Required 24-31-01A RTG

APU Battery- APU Not Required 24-31-01B CD

APU Battery- APU Not Required, Battery Removed 24-31-01C RTG

APU BLEED AIR S APU Bleed Air System 49-52-01 CDAPU CONTROL S APU Controller 49-61-01 CDAPU COOLDOWN M N/A

APU DOOR S

APU Air Inlet Door Actuation System- Procedures Do Not Require APU 49-15-01A RTG

APU Air Inlet Door Actuation System- APU Required 49-15-01B RTG

777 MEL


1-00-02-02.4 23 OCT 2013

APU Air Inlet Door Actuation System- APU Air Inlet Door Actuator Position Indication

Switch49-15-01-01 RTG

APU LIMIT C Auxiliary Power Unit (APU) 49-11-01 CD

APU OIL QTY S

APU OIL QTY Indication- APU Required 49-94-01A RTG

APU OIL QTY Indication- Procedures Do Not Require APU 49-94-01B CD

APU REMOTE SHUTDOWN S Auxiliary Power Unit (APU) 49-11-01 CD

APU RUNNING M N/AAPU SHUTDOWN A Auxiliary Power Unit (APU) 49-11-01 CD

APU START SYS S

APU Starting System (Includes Electric Starter)- APU Required 49-42-01A RTG

APU Starting System (Includes Electric Starter)- Procedures Do Not Require APU 49-42-01B CD

ARINC 629 DATA BUS S No DispatchASCP CONTROLLER S No Dispatch

ASCP PRIMARY CTRL LASCP PRIMARY CTRL R

SS

Air Supply and Cabin Pressure Controllers (ASCPC)- Primary (Digital) Controllers 36-00-01 -01 RTG

ATC COMM MESSAGE N/A

ATC COMM S

Flight Deck Communications System (Data Link)- SATCOM Voice Inoperative 23-27-02A CD

Flight Deck Communications System (Data Link)- SATCOM Voice Operative 23-27-02B CD

Flight Deck Communications System (Data Link)- Procedures Do Not Require Use 23-27-02C CD

ATC DATALINK LOST A N/AAUTO SPEEDBRAKE A Automatic Speedbrake Function 27-62-01 RTGAUTO SPEEDBRAKE S Automatic Speedbrake Function 27-62-01 RTG

AUTOBRAKEAUTOBRAKE

AS

Autobrake System (Including Autobrake SolenoidValve)- Solenoid Verified Closed

32-42-04A RTG

Autobrake System (Including Autobrake SolenoidValve)

- Control Module Deactivated32-42-04B RTG

AUTOBRAKE 1 M N/AAUTOBRAKE 2 M N/AAUTOBRAKE 3 M N/AAUTOBRAKE 4 M N/AAUTOBRAKE MAX M N/AAUTOBRAKE RTO M N/A

AUTOBRAKE SOL VALVE S


- Solenoid Verified Closed32-42-04A RTG


- Control Module Deactivated32-42-04B RTG

777 MEL


1-00-02-02.5 23 OCT 2013

AUTOPILOT C

Autopilot Flight Director Computers (AFDC)- One Inoperative 22-11-01A RTG

Autopilot Flight Director Computers (AFDC)- Two Inoperative 22-11-01B RTG

Autopilot Flight Director Computers (AFDC)- All Inoperative 22-11-01C RTG

AUTOPILOT BACKDRV LAUTOPILOT BACKDRV R

SS

Autopilot Backdrive Actuator Systems- One Inoperative 22-11-02A RTG

Autopilot Backdrive Actuator Systems- Both Inoperative 22-11-02B RTG

AUTOPILOT DISC W

Autopilot Flight Director Computers (AFDC)- One Inoperative 22-11-01A RTG

Autopilot Flight Director Computers (AFDC)- Two Inoperative 22-11-01B RTG

Autopilot Flight Director Computers (AFDC)- All Inoperative 22-11-01C RTG

AUTOTHROTTLE DISC C Autothrottle System 22-31-01 CD

AUTOTHROTTLE LAUTOTHROTTLE RAUTOTHROTTLE SERVO LAUTOTHROTTLE SERVO R

AASS

Autothrottle Servo Motors- One Inoperative 22-31-02A RTG

Autothrottle Servo Motors- Both Inoperative 22-31-02B RTG

AUTOTHROTTLE SYS S Autothrottle System 22-31-01 CDAVS AFT SOV S Alternate Ventilation System Shutoff Valve 21-26-09 RTGAVS FAN S Alternate Ventilation System Fan 21-26-08 RTGAVS FWD SOV S Alternate Ventilation System Shutoff Valve 21-26-09 RTGAVS SWITCH S Alternate Ventilation System ALTN VENT Switch 21-26-10 CD


BANK ANGLE PROTECT S Bank Angle Protection- KAL All 27-02-01-02 CD

BARO SET DISAGREE A N/A

BAT CHARGER APU S

APU Battery Charger- APU Required 24-31-02A RTG

APU Battery Charger- APU Not Required 24-31-02B RTG

BAT CHARGER MAIN S No DispatchBBAND XMIT ON M N/ABLEED FAMV LBLEED FAMV R

SS Fan Air Modulation Valves (FAMV) 36-11-05 RTG

BLEED HPSOV LBLEED HPSOV R

SS

High Pressure Shutoff Valves (HPSOV)- 777-200ER- Associated Engine Bleed Used

36-11-02-02A RTG

High Pressure Shutoff Valves (HPSOV)- 777-200ER- Associated Engine Bleed Not Used

36-11-02-02B RTG

High Pressure Shutoff Valves (HPSOV)- 777-300- Associated Engine Bleed Used

36-11-02-04A RTG

777 MEL


1-00-02-02.6 23 OCT 2013

High Pressure Shutoff Valves (HPSOV)- 777-300- Associated Engine Bleed Not Used

36-11-02-04B RTG


36-11-02-05A RTG


36-11-02-05B RTG

High Pressure Shutoff Valves (HPSOV)- 777F- Associated Engine Bleed Used

36-11-02-06A RTG

High Pressure Shutoff Valves (HPSOV)- 777F- Associated Engine Bleed Not Used

36-11-02-06B RTG

BLEED ISLN CLOSED C A

Center Isolation System (Valve and/or Indication)- Valve Locked Closed 36-12-02A RTG

Center Isolation System (Valve and/or Indication)- Valve Locked Open 36-12-02B RTG

BLEED ISLN CLOSED LBLEED ISLN CLOSED R

AA

Left and Right Isolation Systems (Valve and/orIndication)

- Valve Locked Closed36-12-01A RTG


- Valve Locked Open36-12-01B RTG

BLEED ISLN OPEN C A



BLEED ISLN OPEN LBLEED ISLN OPEN R

AA





BLEED ISLN VALVE C S



BLEED ISLN VALVE LBLEED ISLN VALVE R

SS





BLEED LEAK BODY C No DispatchBLEED LEAK L C No DispatchBLEED LEAK R C No DispatchBLEED LEAK STRUT L C No DispatchBLEED LEAK STRUT R C No DispatchBLEED LOOP 1 BODY S Body Duct Leak Detector Loops 26-18-02 CD

777 MEL


1-00-02-02.7 23 OCT 2013

BLEED LOOP 1 STRUT LBLEED LOOP 1 STRUT R

SS Strut Overheat Detector Loops 26-18-03 CD

BLEED LOOP 1 WING LBLEED LOOP 1 WING R

SS Wing Duct Leak Detector Loops 26-18-01 CD

BLEED LOOP 2 BODY S Body Duct Leak Detector Loops 26-18-02 CDBLEED LOOP 2 STRUT LBLEED LOOP 2 STRUT R

SS Strut Overheat Detector Loops 26-18-03 CD

BLEED LOOP 2 WING LBLEED LOOP 2 WING R

SS Wing Duct Leak Detector Loops 26-18-01 CD

BLEED LOSS BODY A No DispatchBLEED LOSS BODY L A No DispatchBLEED LOSS BODY R A No DispatchBLEED LOSS WING L A No DispatchBLEED LOSS WING R A No Dispatch

BLEED OFF APU A

APU Bleed Air Shutoff System (Valve and/orIndications) 36-12-03 RTG

APU Bleed Air Shutoff System- Valve Indications- APU Not Required

36-12-03-01A RTG

APU Bleed Air Shutoff System- Valve Indications- APU Bleed Not Required

36-12-03-01B RTG

BLEED OFF ENG LBLEED OFF ENG R

AA

Pressure Regulating and Shutoff Systems (PRSOV,PRSOVC)

- 777-200ER36-11-01-02 RTG


- 777-30036-11-01-04 RTG


- 777-300ER36-11-01-05 RTG


- 777F

36-11-01-06 RTG


36-11-02-02A RTG


36-11-02-02B RTG

High Pressure Shutoff Valves (HPSOV)- 777-300- Associated Engine Bleed Used

36-11-02-04A RTG

High Pressure Shutoff Valves (HPSOV)- 777-300- Associated Engine Bleed Not Used

36-11-02-04B RTG


36-11-02-05A RTG

777 MEL


1-00-02-02.8 23 OCT 2013


36-11-02-05B RTG

High Pressure Shutoff Valves (HPSOV)- 777F- Associated Engine Bleed Used

36-11-02-06A RTG

High Pressure Shutoff Valves (HPSOV)- 777F- Associated Engine Bleed Not Used

36-11-02-06B RTG

BLEED PRESS SENSOR LBLEED PRESS SENSOR R

SS Intermediate Pressure Sensing Systems 36-21-02 CD

BLEED PRSOV LBLEED PRSOV R

SS


- 777-200ER36-11-01-02 RTG


- 777-30036-11-01-04 RTG


- 777-300ER36-11-01-05 RTG


- 777F

36-11-01-06 RTG

BLEED TEMP SENSOR LBLEED TEMP SENSOR R

SS

Manifold Temperature Sensing Systems- 777-200ER- Associated Engine Bleed Used

36-22-01-02A RTG

Manifold Temperature Sensing Systems- 777-200ER- Associated Engine Bleed Not Used

36-22-01-02B RTG

Manifold Temperature Sensing Systems- 777-300- Associated Engine Bleed Used

36-22-01-04A RTG

Manifold Temperature Sensing Systems- 777-300- Associated Engine Bleed Not Used

36-22-01-04B RTG

Manifold Temperature Sensing Systems- 777-300ER- Associated Engine Bleed Used

36-22-01-05A RTG

Manifold Temperature Sensing Systems- 777-300ER- Associated Engine Bleed Not Used

36-22-01-05B RTG

Manifold Temperature Sensing Systems- 777F- Associated Engine Bleed Used

36-22-01-06A RTG

Manifold Temperature Sensing Systems- 777F- Associated Engine Bleed Not Used

36-22-01-06B RTG

BLEED VALVE APU S

APU Bleed Air Shutoff System (Valve and/orIndications) 36-12-03 RTG

APU Bleed Air Shutoff System (Valve and/orIndications)

- Valve Indications- APU Not Required

36-12-03-01A RTG

777 MEL


1-00-02-02.9 23 OCT 2013

APU Bleed Air Shutoff System (Valve and/orIndications)

- Valve Indications- APU Bleed Not Required

36-12-03-01B RTG

BOTTLE 1 DISCH ENG A No DispatchBOTTLE 1 ENG S No Dispatch

BOTTLE 1A CARGOBOTTLE 1B CARGOBOTTLE 2A CARGO

SSS

Lower Cargo Compartment Fire Extinguisher Bottles- Without LLAR Installed 26-23-01-01 RTG

Lower Cargo Compartment Fire Extinguisher Bottles- With LLAR Installed 26-23-01-02 RTG

BOTTLE 2B CARGOBOTTLE 2C CARGOBOTTLE 2D CARGOBOTTLE 2E CARGOBOTTLE 2F CARGO

SSSSS

Lower Cargo Compartment Fire Extinguisher Bottles- Metered Bottles 26-23-01-03 RTG

BOTTLE 2 DISCH ENG A No DispatchBOTTLE 2 ENG S No DispatchBOTTLE APU S APU Fire Extinguisher System 26-22-01 CDBOTTLE CREW REST LWR S Lower Lobe Attendant Rest (LLAR) Fire Extinguisher

Bottle 26-25-01 RTG

BOTTLE DISCH APU A APU Fire Extinguisher System 26-22-01 CD

BOTTLE DISCH CARGO A Lower Cargo Compartment Fire Extinguisher Bottles

26-23-01-0126-23-01-0226-23-01-0326-23-01-04

RTG

BRAKE SOURCE A N/ABRAKE TEMP A N/ABRAKE TEMP SYS S Brake Temperature Monitor System (BTMS) 32-46-01 CD

Message L Condition MEL Item A/D/CCABIN ALERT COMM MESSAGE N/A

CABIN ALT AUTO LCABIN ALT AUTO R

SS

Auto Cabin Pressure Controls (L and R)- Passenger- Manual Control Operates on Both Outflow Valves

21-31-01-01A RTG

Auto Cabin Pressure Controls (L and R)- Passenger- One Outflow Valve Deactivated/Manual Control

Operates on Other Valve

21-31-01-01B RTG

Auto Cabin Pressure Controls (L and R)- 777F 21-31-01-02 RTG

Auto Cabin Pressure Controls (L and R)- All 21-31-01-03 RTG

CABIN ALTITUDE W No Dispatch

CABIN ALTITUDE AUTO C

Auto Cabin Pressure Controls (L and R)- Passenger- Manual Control Operates on Both Outflow Valves

21-31-01-01A RTG

Auto Cabin Pressure Controls (L and R)- Passenger- One Outflow Valve Deactivated/Manual Control

Operates on Other Valve

21-31-01-01B RTG

777 MEL


1-00-02-02.10 23 OCT 2013

Auto Cabin Pressure Controls (L and R)- 777F 21-31-01-02 RTG

Auto Cabin Pressure Controls (L and R)- All 21-31-01-03 RTG

Outflow Valves (FWD and AFT)- Passenger 21-31-03-02 RTG

Outflow Valves (FWD and AFT)- 777F 21-31-03-03 RTG

Outflow Valves (FWD and AFT)- All 21-31-03-04 RTG

CABIN CALL COMM MESSAGE N/A

CABIN INTERPHONE S

Cabin Interphone Systems (Passenger)- Flight Deck to Cabin, Cabin to Flight Deck, Functions 23-42-01-01 CD

Cabin Interphone Systems (Passenger)- Cabin to Cabin Functions 23-42-01-02 CD

Cabin Interphone Systems (Passenger)- Flight Deck/Cabin to Crew Rest, Crew Rest to Flight

Deck/Cabin, Functions23-42-01-03 CD

Cabin Interphone Systems (Passenger)- Cabin Interphone Controller Modes 23-42-01-04 RTG

CABIN READY COMM MESSAGE N/A

CABIN TEMP CTRL LCABIN TEMP CTRL R

SS

Cabin Temperature Controllers (CTC)- Passenger 21-61-01-03 RTG

Cabin Temperature Controllers (CTC)- 777F- AVS Operative

21-61-01-05A RTG

Cabin Temperature Controllers (CTC)- 777F- AVS Inoperative

21-61-01-05B RTG

Cabin Temperature Controllers (CTC)- All 21-61-01-06 RTG

CABIN TEMPERATURE A N/A

CARGO A/C LWR AFT A

ACAC Flow Regulating Valve 21-28-03 RTGACAC Exhaust Shutoff Valve 21-28-04 RTGCabin Temperature Controllers (CTC)- 777F- AVS Operative

21-61-01-05A RTG


21-61-01-05B RTG


ACAC Duct Temperature Sensing System- 777F 21-61-09 RTG

Status Msg : CGO TMP SNSRS LWR AFTACAC Cargo Compartment Temperature Sensing

System- 777F

21-61-10 CD

ACAC Cargo Zone Trim Air Modulation Valve- 777F 21-61-11 RTG

777 MEL


1-00-02-02.11 23 OCT 2013

ACAC Cargo Temperature Control- 777F 21-61-12 RTG

Trim Air Control Systems- 777F- One Inoperative

21-62-01-02-02 RTG

Trim Air Pressure Regulating/Shutoff Valves(PRSOVs)

- 777F- One Inoperative

21-62-02-02-02 RTG

CARGO A/C LWR FWD A

FCAC Flow Regulating Valve 21-28-03 RTGCabin Temperature Controllers (CTC)- 777F- AVS Operative

21-61-01-05A RTG


21-61-01-05B RTG


FCAC Duct Temperature Sensing System- 777F 21-61-05-02 RTG

Status Msg : CGO TMP SNSRS LWR FWDFCAC Cargo Compartment Temperature Sensing

System- 777F

21-61-06-02 CD

FCAC Cargo Zone Trim Air Modulation Valve- 777F 21-61-07-01 RTG

FCAC Cargo Temperature Control- 777F 21-61-08-01 RTG


21-62-01-02-02 RTG

Trim Air Pressure Regulating/Shutoff Valves(PRSOVs)

- 777F- One Inoperative

21-62-02-02-02 RTG

CARGO A/C SELECT FWD S FCAC Cargo Temperature Control

- 777F 21-61-08-01 RTG

CARGO CALL COMM MESSAGE N/A

CARGO EXH FAN FWD S

Forward Cargo Air Conditioning(FCAC) Exhaust Fan- FCAC Used 21-26-05A RTG

Forward Cargo Air Conditioning(FCAC) Exhaust Fan- FCAC Not Used 21-26-05B RTG

CARGO HEAT AFT A

Status Msg : ECS CARD L or REnvironmental Control System Miscellaneous Cards (ECSMC)- Passenger

21-00-01-01 RTG

Environmental Control System Miscellaneous Cards (ECSMC)- 777F

21-00-01-02 RTG

Status Msg : CARGO HEAT VALVE AFTAft Cargo Heat Valves 21-44-01 RTG

777 MEL


1-00-02-02.12 23 OCT 2013

Status Msg : CARGO TEMP SNSR AFTAft Cargo Compartment Temperature Sensor 21-44-02 CD

CARGO HEAT BULK

Note : This message is not applicable to 777F airplanes. Disregard the message when it comes on 777F airplanes. It will be corrected in the future.

A

Status Msg : ECS CARD L or REnvironmental Control System Miscellaneous Cards (ECSMC)- Passenger

21-00-01-01 RTG

Status Msg : CARGO HEAT VLV BULKBulk Cargo Heat Valves (Passenger) 21-44-03 RTG

Status Msg : CARGO TEMP SNSR BULKBulk Cargo Compartment Temperature Sensor(Passenger)

21-44-04 CD

CARGO HEAT VALVE AFT S Aft Cargo Heat Valves 21-44-01 RTG

CARGO HEAT VALVE FWD S Forward Cargo Heat Valve 21-27-07 RTG

CARGO HEAT VLV BULK S Bulk Cargo Heat Valves (Passenger) 21-44-03 RTG

CARGO SQUIB TEST SFire Extinguishing Squib Test System 26-21-02 RTGFire Extinguishing Squib Test System- Cargo Squib Test System 26-21-02-01 RTG

CARGO TEMP SNSR AFT S Aft Cargo Compartment Temperature Sensor 21-44-02 CDCARGO TEMP SNSR BULK S Bulk Cargo Compartment Temperature

Sensor(Passenger) 21-44-04 CD

CARGO TRIM VALVE FWD S FCAC Cargo Zone Trim Air Modulation Valve

- 777F 21-61-07-01 RTG

CARGO VENT FAN BULK S

Chiller Boost Fan 21-26-02 RTGBulk Cargo Ventilation Fan- With Chiller Exhaust System Installed 21-26-03-01 RTG

Bulk Cargo Ventilation Fan- Without Chiller Exhaust System Installed 21-26-03-02 RTG

CDU C S Control Display Units (CDU)- Center CDU 34-61-03-01 CD

CDU LCDU R

SS

Control Display Units (CDU)- Other than Center CDU 34-61-03-02 RTG

CGO A/C FRV LWR AFT S ACAC Flow Regulating Valve 21-28-03 RTGCGO A/C FRV LWR FWD S FCAC Flow Regulating Valve 21-28-02 RTG

CGO A/C SEL LWR AFT S ACAC Cargo Temperature Control- 777F 21-61-12 RTG

CGO A/C SEL MAIN AFTCGO A/C SEL MAIN FWD

SS

ACAC Cargo Temperature Control- 777F 21-61-16 RTG

CGO DCT SNSR LWR AFT S ACAC Duct Temperature Sensing System

- 777F 21-61-09 RTG

CGO DCT SNSR LWRFWD S FCAC Duct Temperature Sensing System

- 777F 21-61-05-02 RTG

CGO DCT SNSR M/D AFTCGO DCT SNSR M/D FWD

SS

MDAC Duct Temperature Sensing System-777F 21-61-13 RTG

CGO TMP SNSRS LWRAFT S

ACAC Cargo Compartment Temperature Sensing System

- 777F21-61-10 RTG

777 MEL


1-00-02-02.13 23 OCT 2013

CGO TMP SNSRS LWR FWD S

FCAC Cargo Compartment Temperature Sensing System

- 777F21-61-06-02 CD

CGO TMP SNSR M/D AFTCGO TMP SNSR M/D FWD

SS

MDAC Cargo Compartment Temperature Sensing System

-777F21-61-14 CD

CGO TRM VLV LWR AFT S ACAC Cargo Zone Trim Air Modulation Valve- 777F 21-61-11 RTG

CGO TRM VLV MAIN AFTCGO TRM VLV MAIN FWD

SS

MDAC Cargo Zone Trim Air Modulation Valve- 777F 21-61-15 RTG

CHECKLIST SYS SElectronic Checklist (ECL) System 31-61-07 RTGElectronic Checklist (ECL) System- ECL Closed Loop Switch Indications 31-61-07-01 CD

CMPRSR TEMP SENSOR LCMPRSR TEMP SENSOR R

SS Compressor Discharge Temperature Sensors 21-52-03 RTG

COMM COMM MESSAGE N/ACOMM BUSY COMM MESSAGE N/ACON IGNITION ON L M N/ACON IGNITION ON L+R M N/ACON IGNITION ON R M N/ACOND TEMP SENSOR LCOND TEMP SENSOR R

SS Condenser Inlet Temperature Control Systems 21-52-07 RTG

CONFIG DOORS W N/ACONFIG FLAPS W N/ACONFIG GEAR W N/ACONFIG GEAR STEERING W N/ACONFIG PARKING BRAKE W N/ACONFIG RUDDER W N/ACONFIG SPOILERS W N/ACONFIG STABILIZER W N/ACONFIG W SYS A No DispatchCONFIG W SYS S No DispatchCONTROL COLUMN XDCR S Control Column Position Transducers 27-31-01 CDCONTROL WHEEL XDCR S Control Wheel Position Transducers 27-11-02 CDCPCS AIR/GND S No DispatchCPCS REMOTE SENSOR S Remote Cabin Pressure Sensor 21-31-04 CD

CREW OXYGEN LOW A

Crew Oxygen System- Crew Oxygen Pressure Indication System 35-11-01-01 RTG

Crew Oxygen System- Crew Oxygen Solenoid Bleed Valve 35-11-01-02 RTG

CREW REST CALL COMM MESSAGE N/A

CREW REST SQUIB TEST S

Fire Extinguishing Squib Test System- Lower Lobe Attendant Rest (LLAR) Squib Test System- Squib Continuity Verified

26-21-02-02A RTG

777 MEL


1-00-02-02.14 23 OCT 2013

Fire Extinguishing Squib Test System- Lower Lobe Attendant Rest (LLAR) Squib Test System- Squib Continuity Not Verified

26-21-02-02B RTG

CSD CAN BUS SCargo Smoke Detection (CSD) System Controller (777F)CSD Controller Area Network Bus

26-16-04-03 CD

CSD CONTROLLER CH ACSD CONTROLLER CH B S

Cargo Smoke Detection (CSD) System Controller (777F)CSD Controller Channels

26-16-04-02 CD

CSD POWER BUS SCargo Smoke Detection (CSD) System Controller (777F)- CSD Controller Power Bus

26-16-04-01 CD

CURSOR CONTROL LCURSOR CONTROL R

SS

Cursor Control Devices (CCD)- One Inoperative 31-61-02A CD

Cursor Control Devices (CCD)Both Inoperative 31-61-02-B CD

CSD ZONE 1 CARGO AFTCSD ZONE 2 CARGO AFTCSD ZONE 3 CARGO AFT

S

Lower Cargo Compartment Smoke Detection Systems- 777F (AFT) 26-16-02-02 RTG

Lower Cargo Compartment Smoke Detection Systems- 777F (AFT) 26-16-02-02-02 RTG

CSD ZONE 1 CARGO FWDCSD ZONE 2 CARGO FWDCSD ZONE 3 CARGO FWD

S

Lower Cargo Compartment Smoke Detection Systems- 777F (FWD) 26-16-02-01 RTG

Lower Cargo Compartment Smoke Detection Systems- 777F (FWD) 26-16-02-01-02 RTG

CSD ZONE 1 MAINCSD ZONE 2 MAINCSD ZONE 3 MAINCSD ZONE 4 MAINCSD ZONE 5 MAINCSD ZONE 6 MAINCSD ZONE 7 MAINCSD ZONE 8 MAIN

S

Main Deck Cargo Compartment Smoke Detection Systems- 777F

26-16-03 RTG

Main Deck Cargo Compartment Smoke Detection Systems- 777F- Detector Zone

26-16-03-02 RTG


DATA COMM MGMT S

Data Communication Management SystemSATCOM Voice Inoperative 23-27-01A CD

Data Communication Management SystemSATCOM Voice Operative 23-27-01B CD

Data Communication Management SystemAutomatic Dependent Surveillance - Contract (ADS-C)Function

23-27-01-01 CD

DATALINK AVAIL COMM MESSAGE N/ADATALINK LOST A N/A

DATALINK SYS A

Data Communication Management System- SATCOM Voice Inoperative 23-27-01A CD

Data Communication Management System- SATCOM Voice Operative 23-27-01B CD

Data Communication Management System- Automatic Dependent Surveillance - Contract(ADS-C) Function

23-27-01-01 CD

777 MEL


1-00-02-02.15 23 OCT 2013

DET CHAN 1 C/R LWRDET CHAN 2 C/R LWR S

Lower Lobe Attendant Rest (LLAR) Smoke DetectionSystem- Remote Smoke Detector Channels

26-14-01-01 CD

DET CHAN 1 CARGO AFTDET CHAN 2 CARGO AFT S

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger)- Lower Cargo Compartment Smoke Detector Channels

26-16-01-01 CD

DET CHAN 1 CARGO FWDDET CHAN 2 CARGO FWD S

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger)- Lower Cargo Compartment Smoke Detector Channels

26-16-01-01 CD

DET FAN 1 CARGO AFTDET FAN 1 CARGO FWDDET FAN 2 CARGO AFTDET FAN 2 CARGO FWD

SLower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger)- Lower Cargo Compartment Smoke Detector Fans

26-16-01-02 CD

DET CHAN 1 E/E SMOKEDET CHAN 2 E/E SMOKE S E/E Cooling Smoke Detector Channels 26-19-01 CD

DET FIRE APU A

Status Msg : FIRE CARD APUAPU Fire Detection System- APU Not Used

26-15-01A CD

Status Msg : FIRE CARD APUAPU Fire Detection System- APU Used On Ground

26-15-01B RTG

Status Msg : FIRE LOOP 1 APUFIRE LOOP 2 APU

APU Fire Detection System- APU Fire Detector Loops

26-15-01-01 CD

DET FIRE CARGO AFTDET FIRE CARGO FWD

AA

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger) 26-16-01 RTG

Lower Cargo Compartment Smoke Detection Systems (777F)- Forward

26-16-02-01 RTG

Lower Cargo Compartment Smoke Detection Systems (777F)- Aft

26-16-02-02 RTG

DET FIRE ENG L A No DispatchDET FIRE ENG R A No Dispatch

DET FIRE CARGO MAIN A Main Deck Cargo Compartment Smoke DetectionSystems (777F) 26-16-03 RTG

DET FIRE WHEEL WELLDET FIRE WHEEL WELL

AS

Wheel Well Fire Detection System- BTMS Operative 26-17-01A CD

Wheel Well Fire Detection System- BTMS Inoperative 26-17-01B RTG

DET HTR CARGO AFTDET HTR CARGO FWD

SS

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger)- Lower Cargo Compartment Smoke Detector Heaters- Humid Cargo Not Carried

26-16-01-04A CD

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger)- Lower Cargo Compartment Smoke Detector Heaters- Humid Cargo Carried

26-16-01-04B CD

777 MEL


1-00-02-02.16 23 OCT 2013

DET OVERHEAT ENG LDET OVERHEAT ENG R

AA Engine Overheat Circuits 26-11-02 CD

DET SMOKE C/R LWR S Lower Lobe Attendant Rest (LLAR) Smoke DetectionSystem 26-14-01 RTG

DET SMOKE E/E EXH S Equipment Cooling Smoke Detectors (777F)- Exhaust Smoke Detector 26-19-02-02 RTG

DET SMOKE E/E SUPPLY S Equipment Cooling Smoke Detectors (777F)- Supply Smoke Detector 26-19-02-01 CD

DET TURB OVHT ENG L S No DispatchDET TURB OVHT ENG R S No Dispatch

DET ZONE 1 CARGO AFTDET ZONE 1 CARGO FWDDET ZONE 2 CARGO AFTDET ZONE 2 CARGO FWDDET ZONE 3 CARGO AFTDET ZONE 3 CARGO FWDDET ZONE 4 CARGO AFTDET ZONE 4 CARGO FWD

S

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger)- Lower Cargo Compartment Smoke Detector Zones

26-16-01-03 RTG

Lower Cargo Compartment Smoke Detection Systems- 777F (FWD)- Detector

26-16-02-01-01 RTG

Lower Cargo Compartment Smoke Detection Systems- 777F (AFT)- Detector

26-16-02-02-01 RTG

DET ZONE 1 MAINDET ZONE 2 MAINDET ZONE 3 MAINDET ZONE 4 MAINDET ZONE 5 MAINDET ZONE 6 MAINDET ZONE 7 MAINDET ZONE 8 MAIN

SMain Deck Cargo Compartment Smoke Detection Systems (777F)- Detector

26-16-03-01 RTG

DETECTOR IFES SMOKE S In-Flight Entertainment System (IFES) EquipmentCooling Smoke Detector 21-27-11 RTG

DISPLAY INTERCABINET S No DispatchDISPLAY INTERFACE S No DispatchDISPLAY PROCESSING S No DispatchDISPLAY RESOURCES S No DispatchDISPLAY SELECT PNL A Display Select Panel (DSP) 31-61-04 CDDME LDME R

SS Distance Measuring Equipment (DME) 34-55-01 CD

DOOR AFT CARGO A Door Indication Systems 52-71-01 RTGDOOR AFT CARGO C Door Indication Systems 52-71-01 RTGDOOR AFT CARGO ARMED S No DispatchDOOR AFT CARGO IND S Door Indication Systems 52-71-01 RTGDOOR BULK CARGO A Door Indication Systems 52-71-01 RTGDOOR E/E ACCESS A Door Indication Systems 52-71-01 RTGDOOR ENTRY 1L A Door Indication Systems 52-71-01 RTGDOOR ENTRY 1R A Door Indication Systems 52-71-01 RTGDOOR ENTRY 2L A Door Indication Systems 52-71-01 RTGDOOR ENTRY 2R A Door Indication Systems 52-71-01 RTGDOOR ENTRY 3L A Door Indication Systems 52-71-01 RTGDOOR ENTRY 3R A Door Indication Systems 52-71-01 RTG

777 MEL


1-00-02-02.17 23 OCT 2013

DOOR ENTRY 4L A Door Indication Systems 52-71-01 RTGDOOR ENTRY 4R A Door Indication Systems 52-71-01 RTGDOOR ENTRY 5L A Door Indication Systems 52-71-01 RTGDOOR ENTRY 5R A Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 1L S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 1R S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 2L S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 2R S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 3L S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 3R S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 4L S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 4R S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 5L S Door Indication Systems 52-71-01 RTGDOOR ENTRY IND 5R S Door Indication Systems 52-71-01 RTG

DOOR FLIGHT LOCK 1L S

Main Entry Door Flight Lock Systems- Passenger 52-11-05-01 RTG

Main Entry Door Flight Lock Systems- 777F 52-11-05-02 RTG

DOOR FLIGHT LOCK 1R S

Main Entry Door Flight Lock Systems- Passenger 52-11-05-01 RTG

Main Entry Door Flight Lock Systems- 777F 52-11-05-02 RTG

DOOR FLIGHT LOCK 2L S Main Entry Door Flight Lock Systems- Passenger 52-11-05-01 RTG

DOOR FLIGHT LOCK 2R S Main Entry Door Flight Lock Systems- Passenger 52-11-05-01 RTG







DOOR FWD ACCESS A Door Indication Systems 52-71-01 RTGDOOR FWD CARGO C Door Indication Systems 52-71-01 RTGDOOR FWD CARGO IND S Door Indication Systems 52-71-01 RTGDOOR MAIN CARGO IND S Door Indication Systems 52-71-01 RTGDOOR MAIN DECKCARGO C Door Indication Systems 52-71-01 RTG

DOOR WING SLIDE L A Door Indication Systems 52-71-01 RTGDOOR WING SLIDE L S Door Indication Systems 52-71-01 RTGDOOR WING SLIDE LK L S Door Indication Systems 52-71-01 RTG

777 MEL


1-00-02-02.18 23 OCT 2013

DOOR WING SLIDE LK R S Door Indication Systems 52-71-01 RTGDOOR WING SLIDE R A Door Indication Systems 52-71-01 RTGDOOR WING SLIDE R S Door Indication Systems 52-71-01 RTGDOORS A Door Indication Systems 52-71-01 RTGDOORS AUTO M N/ADOORS AUTO/MANUAL M N/ADOORS MANUAL M N/ADUCT PRESS DET E4 S Equipment Cooling Duct Pressure Sensors 21-27-12 CDDUCT PRESS DET E5 S Equipment Cooling Duct Pressure Sensors 21-27-12 CDDUCT PRESS DET F/D S Equipment Cooling Duct Pressure Sensors 21-27-12 CDDUCT PRESS DET VSCF S Equipment Cooling Duct Pressure Sensors 21-27-12 CDDUCT SENS EQUIP COOL S Equipment Cooling Duct Temperature Sensing System

-777F 21-61-17-02 RTG


EAI CARD LEAI CARD R

SS



Installed

30-21-01-01A RTG


Installed

30-21-01-01C RTG


Installed

30-21-01-02A RTG


Installed

30-21-01-02C RTG

EAI LOOPS FANCASE LEAI LOOPS FANCASE R

SS

Engine Fan Case Overheat Detection Systems- PW & GE 26-18-04-01 RTG

EAI PRESS SENSOR LEAI PRESS SENSOR R

SS



Installed

30-21-01-01A RTG


Installed

30-21-01-01C RTG


Installed

30-21-01-02A RTG

777 MEL


1-00-02-02.19 23 OCT 2013


Installed

30-21-01-02C RTG

EAI VALVE LEAI VALVE R

SS



Installed

30-21-01-01A RTG

Engine Anti-Ice Systems- PW- OAT 38 Degrees C or Below, Without Deactivation

Kit Installed

30-21-01-01B RTG


Installed

30-21-01-01C RTG

Engine Anti-Ice Systems- PW- OAT Above 38 Degrees C, Without Deactivation Kit

Installed

30-21-01-01D RTG


Installed

30-21-01-02A RTG

Engine Anti-Ice Systems- GE- OAT 38 Degrees C or Below, Without Deactivation

Kit Installed

30-21-01-02B RTG


Installed

30-21-01-02C RTG

Engine Anti-Ice Systems- GE- OAT Above 38 Degrees C, Without Deactivation Kit

Installed

30-21-01-02D RTG

ECON COOL VALVE LECON COOL VALVE R

SS

Economy Cooling Valves (ECV)- One Valve Inoperative 21-52-02A RTG

Economy Cooling Valves (ECV)- One or Both Valves Inoperative Deactivated Closed 21-52-02B RTG

ECS CARD LECS CARD R

SS

Environmental Control System Miscellaneous Cards (ECSMC)- Passenger

21-00-01-01 RTG

Environmental Control System Miscellaneous Cards (ECSMC)

- 777F21-00-01-02 RTG

EFIS CONTROL PNL LEFIS CONTROL PNL LEFIS CONTROL PNL REFIS CONTROL PNL R

ASAS

EFIS Control Panels 31-61-08 CD

ELEC AC BUS L C No DispatchELEC AC BUS R C No Dispatch

777 MEL


1-00-02-02.20 23 OCT 2013

ELEC BACKUP GEN LELEC BACKUP GEN LELEC BACKUP GEN RELEC BACKUP GEN RELEC BACKUP SYSELEC BACKUP SYS

ASASAS

Backup Electrical Power System (Backup Generators, Converter and CCBs)- Generator Installed

24-25-01A CD

Backup Electrical Power System (Backup Generators, Converter and CCBs)- Generator Removed

24-25-01B RTG

ELEC BATTERY BUS S No DispatchELEC BATTERY OFF A N/AELEC BUS ISLN L A No DispatchELEC BUS ISLN R A No DispatchELEC CABIN/UTIL OFF A N/AELEC IFE/SEATS OFF A N/AELEC DC BUS L S No DispatchELEC DC BUS R S No DispatchELEC GEN DRIVE L A Engine Driven Generator Systems (IDG, GCB) 24-11-01 RTGELEC GEN DRIVE R A Engine Driven Generator Systems (IDG, GCB) 24-11-01 RTG

ELEC GEN OFF APU A APU Driven Generator System (Generator, AGCU, APB) 24-21-01 CD

ELEC GEN OFF L A Engine Driven Generator Systems (IDG, GCB) 24-11-01 RTGELEC GEN OFF R A Engine Driven Generator Systems (IDG, GCB) 24-11-01 RTGELEC GEN SYS L S Engine Driven Generator Systems (IDG, GCB) 24-11-01 RTGELEC GEN SYS R S Engine Driven Generator Systems (IDG, GCB) 24-11-01 RTG

ELEC GND HDLG BUSELEC GND HDLG BUS

AS

Relays – AC- Ground Handling 24-22-01-01 RTG

Relays – AC- Ground Service Select 24-22-01-02 RTG

Relays – AC- Ground Service Transfer 24-22-01-03 RTG

ELEC HOT BATTERY BUS S No Dispatch

ELEC STANDBY BUS S No DispatchELEC STANDBY SYS A No DispatchELEC STANDBY SYS S No DispatchELEC TRU C1 S No DispatchELEC TRU C2 S No DispatchELEC TRU L S No DispatchELEC TRU R S No Dispatch

ELMS P110 CHANNEL S Electrical Load Management System (ELMS) PowerManagement Channels 24-09-01 RTG

ELMS P110 PANEL S No Dispatch




777 MEL


1-00-02-02.21 23 OCT 2013


ELT ON A

Emergency Locator Transmitter (ELT)- Survival Type ELTs 25-63-03 CD

Emergency Locator Transmitter (ELT)- Fixed ELTs- Inoperative

23-24-02A RTG

Emergency Locator Transmitter (ELT)- Fixed ELTs- Missing

23-24-02B RTG

EMER LIGHTS A N/AENG ANTI-ICE AIR L A No DispatchENG ANTI-ICE AIR R A No DispatchENG AUTOSTART LENG AUTOSTART R

CC

Autostart System- Crew Defer with maintenance consulting 80-11-02 CD

ENG AUTOSTART OFF A N/AENG CCC VALVE L S Core Compartment Cooling Valves (GE) 75-23-02 RTGENG CCC VALVE R S Core Compartment Cooling Valves (GE) 75-23-02 RTGENG CONTROL L A No DispatchENG CONTROL L S No DispatchENG CONTROL R A No DispatchENG CONTROL R S No DispatchENG DMS L S No DispatchENG DMS R S No DispatchENG EEC C1 L S EEC C1 Faults 73-21-04 CDENG EEC C1 R S EEC C1 Faults 73-21-04 CD

ENG EEC MODE LENG EEC MODE LENG EEC MODE RENG EEC MODE R

ASAS

Engine PT2 Probe Heater Systems (PW) 30-34-01 CDElectronic Engine Controls (EEC) Normal Mode- PW 73-21-02-01 CD

Electronic Engine Controls (EEC) Normal Mode- GE 73-21-02-02 CD

ENG EEC OVHT L S No DispatchENG EEC OVHT R S No DispatchENG FAIL L C No DispatchENG FAIL R C No DispatchENG FUEL FILT SNSR L(GE) S Engine Fuel Filter Bypass Warning Systems

- GE 73-34-01-02 RTG

ENG FUEL FILT SNSR R(GE) S Engine Fuel Filter Bypass Warning Systems

- GE 73-34-01-02 RTG

ENG FUEL FILTER L(PW)ENG FUEL FILTER L(PW)ENG FUEL FILTER R(PW)ENG FUEL FILTER R(PW)

ASAS

Engine Fuel Filter Bypass Warning Systems- PW 73-34-01-01 RTG

ENG FUEL FILTER L (GE) A No DispatchENG FUEL FILTER L (GE) S No Dispatch

777 MEL


1-00-02-02.22 23 OCT 2013

ENG FUEL FILTER R (GE) A No DispatchENG FUEL FILTER R (GE) S No Dispatch

ENG FUEL VALVE L AEngine Fuel Shutoff Valve Indication Systems 73-21-06 RTG(Nuisance) EICAS Status Messages- System(s) Used 31-61-05A RTG

ENG FUEL VALVE L S Engine Fuel Shutoff Valve Indication Systems 73-21-06 RTG

ENG FUEL VALVE R AEngine Fuel Shutoff Valve Indication Systems 73-21-06 RTG(Nuisance) EICAS Status Messages- System(s) Used 31-61-05A RTG

ENG FUEL VALVE R S Engine Fuel Shutoff Valve Indication Systems 73-21-06 RTGENG HPTACC VALVE L S No DispatchENG HPTACC VALVE R S No DispatchENG IDLE DISAGREE A Engine Idle Selection Systems 73-21-01 CD

ENG IGNITOR L1ENG IGNITOR L2ENG IGNITOR R1ENG IGNITOR R2

S

Ignition Systems- EAI System Operative 74-00-01A CD

Ignition Systems- EAI System Inoperative 74-00-01B CD

ENG L START EGT S No DispatchENG LIMIT PROT L C N/AENG LIMIT PROT R C N/AENG LPC ANTI-ICE LENG LPC ANTI-ICE RENG LPC AI VALVE LENG LPC AI VALVE R

AASS

Low Pressure Compressor (LPC) Anti-Ice (AI) Valve(GE90-115B) 75-10-01 RTG

ENG LPTACC VALVE LENG LPTACC VALVE R

SS

Turbine Case Cooling Air Flow Systems- LPT Systems (GE) 75-24-01-03 RTG

ENG OIL FILT SNSR LENG OIL FILT SNSR R

SS

Engine Oil Filter Bypass Warning Systems- PW 79-35-01-01 RTG

Engine Oil Filter Bypass Warning Systems- GE 79-35-01-02 CD

ENG OIL FILTER L A No DispatchENG OIL FILTER L S No DispatchENG OIL FILTER R A No DispatchENG OIL FILTER R S No DispatchENG OIL PRESS L C N/AENG OIL PRESS R C N/AENG OIL TEMP L A N/AENG OIL TEMP R A N/AENG OPU L S No DispatchENG OPU R S No DispatchENG OVERSPEED GOV L S No DispatchENG OVERSPEED GOV R S No DispatchENG R START EGT S No DispatchENG REV LIMITED LENG REV LIMITED R

AA

Thrust Reversers- 200ER/-300 78-31-01-01 RTG

777 MEL


1-00-02-02.23 23 OCT 2013

- All (Except -300ER/777F)

Reverse Thrust Lever Interlocks- 200ER/-300 78-34-01-01 CD

ENG REV LIMITED LENG REV LIMITED R- 300ER/777F

AA

Thrust Reversers-300ER/777F 78-31-01-02 RTG

Reverse Thrust Lever Interlocks- 300ER/777F- Interlock Retracted

78-34-01-02B CD

ENG REVERSER LENG REVERSER LENG REVERSER RENG REVERSER R

ASAS

Thrust Reversers- 200ER/-300 78-31-01-01 RTG

Thrust Reversers-300ER/777F 78-31-01-02 RTG

ENG REVERSER SNSR LENG REVERSER SNSR R

SS Reverser Proximity Sensors 78-36-01 RTG

ENG RPM LIMITED L A N/AENG RPM LIMITED R A N/AENG SHUTDOWN C N/AENG SHUTDOWN L C N/AENG SHUTDOWN R C N/AENG START BLEED L S No DispatchENG START BLEED R S No DispatchENG START VALVE LENG START VALVE LENG START VALVE RENG START VALVE R

ASAS

Engine Start Valves 80-11-01 CD

ENG STARTER CUTOUT LENG STARTER CUTOUT R

CC

Engine Start Valves 80-11-01 CDStart Selector Holding/Cutout Systems 80-11-03 CD

ENG TCMA LENG TCMA R

SS

Engine Thrust Control Malfunction Accommodation (TCMA) Functions (GE90-100 Series) 73-21-07 CD

ENG THRUST L C No DispatchENG THRUST R C No DispatchENG VIB MONITOR LENG VIB MONITOR R

SS Engine Vibration Monitor Systems 77-31-01

77-31-01 CD

ENG/APU SQUIB TEST S Fire Extinguishing Squib Test System 26-21-02 RTGEQUIP 3 WAY VALVE S Equipment Cooling Three-Way Valve 21-27-15-02 RTGEQUIP COOL A/C FLOW S Flight Deck Equipment Cooling System 21-27-16 RTGEQUIP COOLING A No DispatchEQUIP COOLING CTRL LEQUIP COOLING CTRL R

SS Equipment Cooling Controllers 21-27-08 CD

EQUIP COOLING FAN LEQUIP COOLING FAN R

SS Equipment Cooling Supply Fans 21-27-02

21-27-02 RTG

EQUIP COOLING OVRD A No DispatchEQUIP DIVERT VALVE S Equipment Cooling Divert Valve 21-27-13 RTG

EQUIP FLOW DET S

Equipment Cooling Low Flow Sensors- Passenger 21-27-04-01 RTG

Equipment Cooling Low Flow Sensors- 777F- Main Equipment Center Low Flow Sensor

21-27-04-02-01 RTG

777 MEL


1-00-02-02.24 23 OCT 2013

Equipment Cooling Low Flow Sensors- 777F- Flight Deck Low Flow Sensor

21-27-04-02-02 RTG

EQUIP INBOARD VALVE S Equipment Cooling Inboard Valve 21-27-14-02 RTGEQUIP VENT FAN S Equipment Cooling Vent Fan 21-27-05 RTG

EQUIP VENT VALVE S

Equipment Cooling Vent Valve- Passenger 21-27-06-01 RTG

Equipment Cooling Vent Valve- 777F 21-27-06-02 RTG

EXH REST UPR AFT S Overhead Flight Attendant Rest Exhaust Valves- Overhead Flight Attendant Rest (OFAR) (-300ER) 21-29-05-02 RTG

Message L Condition MEL Item A/D/CF/OIL VALVE CLOSED LF/OIL VALVE CLOSED R

SS Engine Fuel/Oil Cooler Bypass Valves (PW) 79-21-02 CD

F/OIL VALVE OPEN L S No DispatchF/OIL VALVE OPEN R S No DispatchFIRE APU W No Dispatch

FIRE CARD APU S

APU Fire Detection System- APU Not Used 26-15-01A CD

APU Fire Detection System- APU Used On Ground 26-15-01B RTG

FIRE CARD ENG L S No DispatchFIRE CARD ENG R S No DispatchFIRE CARGO AFT W No DispatchFIRE CARGO FWD W No DispatchFIRE CARGO MAIN DECK W No Dispatch

FIRE ENG L W No DispatchFIRE ENG R W No DispatchFIRE LOOP 1 APUFIRE LOOP 2 APU S APU Fire Detection System

- APU Fire Detector Loops 26-15-01-01 CD

FIRE LOOP 1 ENG LFIRE LOOP 1 ENG RFIRE LOOP 2 ENG LFIRE LOOP 2 ENG R

SSSS

Engine Fire Detector Loops- PW & GE 26-11-01 CD

FIRE TEST FAIL W

Engine Overheat Circuits 26-11-02 CDAPU Fire Detection System- APU Not Used 26-15-01A CD

APU Fire Detection System- APU Used On Ground 26-15-01B RTG

APU Fire Detection System- APU Fire Detector Loops 26-15-01-01 CD

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (Passenger) 26-16-01 RTG

Lower Cargo Compartment Smoke Detection Systems (Forward and Aft) (777F) 26-16-02 RTG

777 MEL


1-00-02-02.25 23 OCT 2013

Wheel Well Fire Detection System- BTMS Operative 26-17-01A CD

Wheel Well Fire Detection System- BTMS Inoperative 26-17-01B RTG

FIRE TEST IN PROG W N/AFIRE TEST PASS W N/AFIRE WHEEL WELL W No DispatchFLAP/SLAT CONTROL C No DispatchFLAP/SLAT CONTROL 1FLAP/SLAT CONTROL 2

SS Flap/Slat Control Lanes 27-03-01 RTG

FLAP/SLAT SKEW SNSRS S Flap/Slat Skew Sensors 27-59-01 RTG

FLAPERON ACTUATOR SFlaperon Power Control Units (PCUs)- Passenger (300ER or -200/-300 equivalent SBs incorporated, refer to NOTE below)

27-11-04-01 RTG

FLAPS DRIVE C No DispatchFLAPS PRIMARY FAIL C No DispatchFLAPS SECONDARY FAIL S Flap Secondary Control 27-03-02 RTGFLIGHT CONTROL MODE C No DispatchFLIGHT CONTROL SYS S No DispatchFLIGHT CONTROLS C No DispatchFLIGHT DECK A/C FRV S Flight Deck Flow Regulating Valve 21-51-04 RTG

FLOW VALVE CARGO AFTFLOW VALVE CARGO FWD

S

S

Lower Cargo Compartment Fire Extinguisher FlowValves (Forward or Aft)- One Inoperative

26-23-02A RTG

Lower Cargo Compartment Fire Extinguisher FlowValves (Forward or Aft)- Both Inoperative

26-23-02B RTG

FLT CONTROL VALVE A Flight Control Hydraulic Shutoff Valve Systems 27-02-06 RTG

FLT DECK FLOW DET S

Equipment Cooling Low Flow Sensors- Passenger 21-27-04-01 RTG

Equipment Cooling Low Flow Sensors- 777F- Main Equipment Center Low Flow Sensor

21-27-04-02-01 RTG

Equipment Cooling Low Flow Sensors- 777F- Flight Deck Low Flow Sensor

21-27-04-02-02 RTG

FLT INST BUS CAPT S No DispatchFLT INST BUS F/O S No DispatchFLT RECORDER SYS S Flight Data Recorder (FDR) System 31-31-01 CDFMC A Flight Management Computing Systems (FMCS) 34-61-01 RTGFMC COMM MESSAGE N/AFMC S Flight Management Computing Systems (FMCS) 34-61-01 RTGFMC L A Flight Management Computing Systems (FMCS) 34-61-01 RTGFMC L S Flight Management Computing Systems (FMCS) 34-61-01 RTGFMC MESSAGE A N/AFMC R A Flight Management Computing Systems (FMCS) 34-61-01 RTGFMC R S Flight Management Computing Systems (FMCS) 34-61-01 RTG

777 MEL


1-00-02-02.26 23 OCT 2013

FMC RUNWAY DISAGREE C N/AFUEL AUTO JETTISON C Fuel Jettison System 28-31-01 RTGFUEL CROSSFEED AFT A

Crossfeed Valves 28-22-03 RTGFUEL CROSSFEED AFT SFUEL CROSSFEED FWD AFUEL CROSSFEED FWD SFUEL DIAGREE A N/AFUEL FLOW ENG L A N/A RTGFUEL FLOW ENG R A N/A RTGFUEL IMBALANCE A N/AFUEL IN CENTER A N/AFUEL ISLN VALVE APU S APU Fuel Isolation Valve 28-25-03 RTG

FUEL JETT NOZZLE LFUEL JETT NOZZLE LFUEL JETT NOZZLE RFUEL JETT NOZZLE R

ASAS

Fuel Jettison Nozzle Valves- One Inoperative 28-31-04A RTG

Fuel Jettison Nozzle Valves- Both Inoperative 28-31-04B RTG

FUEL JETT PUMP L SMain Tanks Jettison Pumps 28-31-03 RTGFUEL JETT PUMP R S

FUEL JETTISON MAIN AFUEL JETTISON SYS C Fuel Jettison System 28-31-01 RTGFUEL JETTISON SYS S Fuel Jettison System 28-31-01 RTGFUEL LOW CENTER A N/AFUEL PRESS ENG L C No DispatchFUEL PRESS ENG L+R A N/AFUEL PRESS ENG R C No DispatchFUEL PUMP APU S APU DC Fuel Pump 28-25-01 RTG

FUEL PUMP CENTER LFUEL PUMP CENTER LFUEL PUMP CENTER RFUEL PUMP CENTER R

ASAS

Center Tank Fuel Override/Jettison Pumps- One Pump Inoperative 28-22-02A RTG

Center Tank Fuel Override/Jettison Pumps- Both Pumps Inoperative 28-22-02B RTG

FUEL PUMP L AFT A

Main Tank Fuel Pumps 28-22-01 RTG

FUEL PUMP L AFT SFUEL PUMP L FWD AFUEL PUMP L FWD SFUEL PUMP R AFT AFUEL PUMP R AFT SFUEL PUMP R FWD AFUEL PUMP R FWD SFUEL QTY CHANNEL S Fuel Quantity Processor Input/Output (I/O) Channels 28-41-02 CD

FUEL QTY INDICATION S

Fuel Quantity Indications (Flight Deck)- Center Tank 28-41-01-01 RTG

Fuel Quantity Indications (Flight Deck)- Main Tanks 28-41-01-02 RTG

FUEL QTY LOW C N/AFUEL SCAVENGE SYS A Fuel Scavenge Systems 28-22-04 RTG

777 MEL


1-00-02-02.27 23 OCT 2013

FUEL SOV BATTERY S Fuel Shutoff Valve Battery 28-22-06 CD

FUEL SPAR VALVE L SNo Dispatch

(Nuisance) EICAS Status Messages- System(s) Used 31-61-05A RTG

FUEL SPAR VALVE R SNo Dispatch


FUEL TEMP INDICATION S Fuel Temperature Indicating System 28-43-01 CDFUEL TEMP LOW A N/AFUEL VALVE APU A

APU Fuel Shutoff Valve 28-25-02 RTGFUEL VALVE APU S

Message L Condition MEL Item A/D/CG/S ANTENNA C S

Glideslope Antenna Switching 34-31-02 CDG/S ANTENNA L S

G/S ANTENNA R S

GEAR CONTROL S Landing Gear Selector Valve Electrical Control Circuits 32-31-02 RTGGEAR DISAGREE C No DispatchGEAR DOOR A No Dispatch

GEAR INDICATION SYS S

Landing Gear Position Indication Systems 32-61-01 RTGLanding Gear Position Indication Systems- Truck Tilt Sensors 32-61-01-01 RTG

Landing Gear Position Indication Systems- Nose Gear Not Compressed Sensors- PSEU 2 Sensor Inoperative

32-61-01-02A RTG

Landing Gear Position Indication Systems- Nose Gear Not Compressed Sensors- PSEU 1 Sensor Inoperative

32-61-02B RTG

GND PROX SYS

For Crew Defer, Contact the MCC to obtain the determination of the MEL item to be applied.

A

Ground Proximity Warning System (GPWS)- GPWS Function 34-46-01-01 CD

Ground Proximity Warning System (GPWS)- Terrain Awareness Function- Terrain Display Functions- Both Inoperative

34-46-01-03-01B CD

GND PROX SYS S

Ground Proximity Warning System (GPWS)- GPWS Function 34-46-01-01 CD

Ground Proximity Warning System (GPWS)- Terrain Awareness Function- Terrain Display Functions- Both Inoperative

34-46-01-03-01B CD

GPS A

Status Msg : GPS L and GPS RGlobal Positioning Systems- Both Inoperative

34-58-01A RTG

Status Msg : GPS L or GPS RGlobal Positioning Systems- One Inoperative

34-58-01B CD

GPS LGPS R

SS

Global Positioning Systems- Both Inoperative 34-58-01A RTG

777 MEL


1-00-02-02.28 23 OCT 2013

Global Positioning Systems- One Inoperative 34-58-01B CD

GROUND CALL COMM MESSAGE N/A

GROUND TEST ENABLE S

Electronic Engine Controls (EEC) Normal Mode- PW 73-21-02-01 CD

Electronic Engine Controls (EEC) Normal Mode- GE 73-21-02-02 CD

Message L Condition MEL Item A/D/CHEAT PITOT CHEAT PITOT C

AS

Pitot Probe Heater Systems- Center Pitot Heater 30-31-01-03 RTG

HEAT PITOT LHEAT PITOT L

AS

Pitot Probe Heater Systems- Left Pitot Heater 30-31-01-02 RTG

HEAT PITOT L+C+R A No DispatchHEAT PITOT RHEAT PITOT R

AS

Pitot Probe Heater Systems- Right Pitot Heater 30-31-01-01 RTG

HEAT TAT S Total Air Temperature (TAT) Probe Heater System- Single TAT System 30-33-01-01 CD

HF DATALINK OFF M N/AHYD AUTO CONTROL C A No DispatchHYD AUTO CONTROL LHYD AUTO CONTROL R

AA Hydraulic Interface Module (HYDIM) Cards 29-11-05 RTG

HYD ISLN VALVE S Center Hydraulic Isolation System 29-11-06 RTG

HYD OVERHEAT DEM C1HYD OVERHEAT DEM C2

AA

Center System Demand Air Driven Pumps (ADP)- Remaining ADP Heater/Auto Operative 29-11-03A RTG

Center System Demand Air Driven Pumps (ADP)- Remaining ADP Heater/Auto Inoperative 29-11-03B RTG

Center System Demand Air Driven Pumps (ADP)- One Auto Function Inoperative, Other ADP Operates Normally

29-11-03-01A RTG

Center System Demand Air Driven Pumps (ADP)- ADP Auto Function- One Auto Function Inoperative, Other ADP

Inoperative

29-11-03-01B RTG

Center System Demand Air Driven Pumps (ADP)- ADP Auto Function- Both Auto Function Inoperative

29-11-03-01C RTG

HYD OVERHEAT DEM L A No DispatchHYD OVERHEAT DEM R A No Dispatch

HYD OVERHEAT PRI C1 A Center System Primary Alternating Current MotorPumps (ACMP) 29-11-02 RTG

HYD OVERHEAT PRI C2 A Center System Primary Alternating Current MotorPumps (ACMP) 29-11-02 RTG

HYD OVERHEAT PRI L A No DispatchHYD OVERHEAT PRI R A No Dispatch

HYD PRESS DEM C1HYD PRESS DEM C2 A



777 MEL


1-00-02-02.29 23 OCT 2013

Center System Demand Air Driven Pumps (ADP)- One Auto Function Inoperative, Other ADP Operates

Normally29-11-03-01A RTG


Inoperative

29-11-03-01B RTG


29-11-03-01C RTG

Demand Pump Selectors- Center System AUTO Position- After Set Switch ON then message disappear

29-11-04-01 CD

Demand Pump Selectors- ON Position- After Set Switch AUTO then message disappear

29-11-04-03 CD

HYD PRESS DEM LHYD PRESS DEM R

AA

Demand Pump Selectors- Left & Right System AUTO Position- After Set Switch ON then message disappear

29-11-04-02 CD

Demand Pump Selectors- ON Position- After Set Switch AUTO then message disappear

29-11-04-03 CD

Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PRESS IND DEM C1HYD PRESS IND DEM C2

SS

Pump Pressure Indication Systems- Center System- Pump Operative

29-31-02-02A RTG

Pump Pressure Indication Systems- Center System- Pump Inoperative

29-31-02-02B CD

HYD PRESS IND DEM L S Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PRESS IND DEM R S Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PRESS IND PRI C1HYD PRESS IND PRI C2

SS


29-31-02-02A RTG


29-31-02-02B CD

HYD PRESS IND PRI L S Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PRESS IND PRI R S Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PRESS PRI C1HYD PRESS PRI C2

AA

Center System Primary Alternating Current MotorPumps (ACMP) 29-11-02 RTG


29-31-02-02A RTG


29-31-02-02B CD

777 MEL


1-00-02-02.30 23 OCT 2013

HYD PRESS PRI L A Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PRESS PRI R A Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PRESS SYS C C No DispatchHYD PRESS SYS L C No DispatchHYD PRESS SYS L+C C No DispatchHYD PRESS SYS L+C+R C No DispatchHYD PRESS SYS L+R C No DispatchHYD PRESS SYS R C No DispatchHYD PRESS SYS R+C C No Dispatch

HYD PUMP DEM C1HYD PUMP DEM C2

SS



Center System Demand Air Driven Pumps (ADP)- One Auto Function Inoperative, Other ADP Operates

Normally29-11-03-01A RTG


Inoperative

29-11-03-01B RTG


29-11-03-01C RTG

Demand Pump Selectors- Center System AUTO Position 29-11-04-01 CD

Demand Pump Selectors- ON Position 29-11-04-03 CD

HYD PUMP DEM LHYD PUMP DEM R

SS

Demand Pump Selectors- Left & Right System AUTO Position 29-11-04-02 CD

Demand Pump Selectors- ON Position 29-11-04-03 CD

Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PUMP PRI C1 S Center System Primary Alternating Current MotorPumps (ACMP) 29-11-02 RTG

HYD PUMP PRI C2 S Center System Primary Alternating Current MotorPumps (ACMP) 29-11-02 RTG

HYD PUMP PRI L S Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD PUMP PRI R S Pump Pressure Indication Systems- Left & Right Systems 29-31-02-01 RTG

HYD QTY LOW C A No DispatchHYD QTY LOW L A No DispatchHYD QTY LOW L+C C No DispatchHYD QTY LOW L+C+R C No DispatchHYD QTY LOW L+R C No Dispatch

777 MEL


1-00-02-02.31 23 OCT 2013

HYD QTY LOW R A No DispatchHYD QTY LOW R+C C No Dispatch

HYD RSVR PRESS C SNo Dispatch


HYD RSVR PRESS L SNo Dispatch


HYD RSVR PRESS R SNo Dispatch


HYD SYS PRESS SNSR C SHydraulic System Pressure Transducers

29-31-0129-31-0129-31-01

CDHYD SYS PRESS SNSR L SHYD SYS PRESS SNSR R S

HYD TEMP IND DEM C1HYD TEMP IND DEM C2

SS

Pump Temperature Indications- Center System- Pump Operative

29-32-01-02A RTG

Pump Temperature Indications- Center System- Pump Inoperative

29-32-01-02B CD

HYD TEMP IND DEM LHYD TEMP IND DEM R

SS

Pump Temperature Indications- Left & Right Systems 29-32-01-01 RTG

HYD TEMP IND PRI C1HYD TEMP IND PRI C2

SS

Pump Temperature Indications- Center System- Pump Operative

29-32-01-02A RTG

Pump Temperature Indications- Center System- Pump Inoperative

29-32-01-02B CD

HYD TEMP IND PRI LHYD TEMP IND PRI R

SS

Pump Temperature Indications- Left & Right Systems 29-32-01-01 RTG

HYDIM CARD HCLHYDIM CARD HCRHYDIM CARD HLHYDIM CARD HR

SSSS

Hydraulic Interface Module (HYDIM) Cards 29-11-05 RTG

Message L Condition MEL Item A/D/CICE DETECTOR L S

Ice Detectors 30-81-01 CDICE DETECTOR R SICE DETECTORS AICING ENG C N/AICING WING A N/AIDG VALVE CLOSED L S

Engine Driven Generator Systems (IDG, GCB) 24-11-01 RTGIDG VALVE CLOSED R S

IFES COOLING FAN S In-Flight Entertainment System (IFES) EquipmentCooling Fan 21-27-10 RTG

ILS ANTENNA C Status Msg : ILS L or C or RInstrument Landing System (ILS) 34-31-01 CD

777 MEL


1-00-02-02.32 23 OCT 2013

Status Msg : G/S ANTENNA L or C or RGlideslope Antenna Switching 34-31-02 CD

Status Msg : LOC ANTENNA L or C or RLocalizer Antenna Switching 34-31-03 CD

ILS C S Instrument Landing System (ILS) 34-31-01CDILS L S Instrument Landing System (ILS) 34-31-01

ILS R S Instrument Landing System (ILS) 34-31-01INSUFFICIENT FUEL A N/A RTG


JETT ISLN VALVE L SCenter Tank Jettison Isolation Valves-200ER, -300, -300ER, 777F- Fuel Jettison System Deactivated

28-31-02-02A RTG

JETT ISLN VALVE R SCenter Tank Jettison Isolation Valves-200ER, -300, -300ER, 777F- Main Tank Jettison Operative

28-31-02-02B RTG

Message L Condition MEL Item A/D/CL GEAR DOOR SENSOR S Landing Gear Door Position Sensors 32-61-02 RTGL GEAR UPLOCK SENSOR S Landing Gear Uplock Position Sensors 32-61-03 RTG

LANDING ALTITUDE A N/ALAV-GALLEY FAN L S Lavatory/Galley Ventilation Fans 21-26-01 RTGLAV-GALLEY FAN R S Lavatory/Galley Ventilation Fans 21-26-01 RTGLAV-GALLEY SOV S Lavatory/Galley Ventilation Shutoff Valve 21-26-07 RTGLOC ANTENNA C S Localizer Antenna Switching 34-31-03 CDLOC ANTENNA L S Localizer Antenna Switching 34-31-03 CDLOC ANTENNA R S Localizer Antenna Switching 34-31-03 CDLSCF ASG CARD LLSCF ASG CARD R

SS

Systems Cardfile ARINC Signal Gateway (ASG) Cards- Left Systems Cardfile ASG Cards 31-09-01-01 CD

LSCF PWR SUPPLY 1LSCF PWR SUPPLY 2

SS

Systems Cardfile Power Supplies- Left Systems Cardfile (LSCF) Power Supplies 31-09-02-01 RTG

Message L Condition MEL Item A/D/CMAIN BATTERY S No DispatchMAIN BATTERY DISCH A No DispatchMAIN BATTERY OVHT S No Dispatch

MAIN DECK A/C A

Status Msg : MAIN DECK FWD SOV 1 or 2Main Deck Cargo Shutoff Valves- Forward Shutoff Valves 1 and 2

21-40-01-01 RTG

Status Msg : MAIN DECK AFT SOV 1 or 2Main Deck Cargo Shutoff Valves- Aft Shutoff Valves 1 and 2

21-40-01-02 RTG

Status Msg : MAIN DECK FWD or AFT SOV 3Main Deck Cargo Shutoff Valves- Forward and Aft Shutoff Valves 3

21-40-01-03 RTG

777 MEL


1-00-02-02.33 23 OCT 2013

Status Msg : CGO DCT SNSR M/D FWD or AFTMDAC Duct Temperature Sensing System 21-61-13 RTG

Status Msg : CGO TMP SNSR M/D FWD or AFTMDAC Cargo Compartment Temperature SensingSystem

21-61-14 CD

Status Msg : CGO TRM VLV MAIN FWD or AFTMDAC Cargo Zone Trim Air Modulation Valves 21-61-15 RTG

Status Msg : CGO A/C SEL MAIN FWD or AFTMDAC Cargo Temperature Controls 21-61-16 CD

Status Msg : TRIM AIR L or RTrim Air Control Systems- 777F

21-62-01-02-02 RTG

Status Msg : TRIM AIR PRSOV L or RTrim Air Pressure Regulating/Shutoff Valves(PRSOVs)- 777F

21-62-02-02-02 RTG

MAIN DECK AFT SOV 1 S Main Deck Cargo Shutoff Valves- Aft Shutoff Valves 1 and 2 21-40-01-02 RTG

MAIN DECK AFT SOV 2 S Main Deck Cargo Shutoff Valves- Aft Shutoff Valves 1 and 2 21-40-01-02 RTG

MAIN DECK AFT SOV 3 S Main Deck Cargo Shutoff Valves- Forward and Aft Shutoff Valves 3 21-40-01-03 RTG

MAIN DECK FWD SOV 1 S Main Deck Cargo Shutoff Valves- Forward Shutoff Valves 1 and 2 21-40-01-01 RTG

MAIN DECK FWD SOV 2 S Main Deck Cargo Shutoff Valves- Forward Shutoff Valves 1 and 2 21-40-01-01 RTG

MAIN DECK FWD SOV 3 S Main Deck Cargo Shutoff Valves- Forward and Aft Shutoff Valves 3 21-40-01-03 RTG

MAIN DK ALERT S Main Deck Alert System 33-37-02 CDMAIN GEAR BRACE L C No DispatchMAIN GEAR BRACE R C No DispatchMAIN GEAR STEERING A Main Gear Steering System (Including Indication) 32-53-01 RTGMAIN GEAR STEERING S Main Gear Steering System (Including Indication) 32-53-01 RTGMAN PRESS SENSOR L S Manifold Pressure/Flow Sensing Systems 36-21-01 CDMAN PRESS SENSOR R S Manifold Pressure/Flow Sensing Systems 36-21-01 CDMANIFOLD SENSOR L S Manifold Pressure/Flow Sensing Systems 36-21-01 CDMANIFOLD SENSOR R S Manifold Pressure/Flow Sensing Systems 36-21-01 CDMODE CTRL PANEL LANE S Autopilot Mode Control Panel Lanes 22-11-03 CD

Message L Condition MEL Item A/D/CNACELLE VENT VALVE L S

Nacelle Zone Ventilation Valves (PW) 75-23-01 RTGNACELLE VENT VALVE R SNAV ADIRU INERTIAL C No DispatchNAV AIR DATA SYS A No DispatchNAV UNABLE RNP C N/ANAV UNABLE RNP A N/A

777 MEL


1-00-02-02.34 23 OCT 2013

NITROGEN GEN PERF S Nitrogen Generation System (NGS)- Nitrogen Generation Performance 47-11-01-01 CD

NITROGEN GEN SYS S Nitrogen Generation System (NGS) 47-11-01 RTG

NO AUTOLANDNO AUTOLAND

AC

Automatic Landing System (Autoland) 22-11-07 CDAutomatic Landing System (Autoland)- Triple Channel Autoland (LAND 3) 22-11-07-01 CD

NO AUTOLAND S Automatic Landing System (Autoland) 22-11-07 CDNO ELECTRONICS ON M N/A

NO LAND 3 A Automatic Landing System (Autoland)- Triple Channel Autoland (LAND 3) 22-11-07-01 CD

NO LAND 3 C Automatic Landing System (Autoland)- Triple Channel Autoland (LAND 3) 22-11-07-01 CD

NO LAND 3 S Automatic Landing System (Autoland)- Triple Channel Autoland (LAND 3) 22-11-07-01 CD

NO SMOKING ON M N/ANOSE GEAR DOOR SNSR S Landing Gear Door Position Sensors 32-61-02 RTGNOSE GEAR PRESS XDCR S Nose Gear Pressure Transducer 27-48-04 CDNOSE GEAR UP SENSOR S Landing Gear Uplock Position Sensors 32-61-03 RTG

Message L Condition MEL Item A/D/COIL PRESS SENSORS L S No DispatchOIL PRESS SENSORS R S No DispatchOIL QTY SENSOR L S

Engine Oil Quantity Indicating Systems 79-31-01 RTGOIL QTY SENSOR R SOIL TEMP SENSORS L S No DispatchOIL TEMP SENSORS R S No DispatchOPBC L S

Overhead Panel Bus Controllers (OPBC) 23-93-01 RTGOPBC R S

OPIC LA1OPIC LA2OPIC RA1OPIC RA2

SSSS

Overhead Panel Interface Cards (OPIC)- Both ADPs(HYD Demand Pump C1, C2) is Operative 23-93-02A CD

Overhead Panel Interface Cards (OPIC)- One ADP(HYD Demand Pump C1 or C2) Inoperative 23-93-02B CD

OUTFLOW VALVE AFTOUTFLOW VALVE AFTOUTFLOW VALVE FWDOUTFLOW VALVE FWD

ASAS

Outflow Valves (FWD and AFT)- Passenger 21-31-03-02 RTG

Outflow Valves (FWD and AFT)- 777F 21-31-03-03 RTG

Outflow Valves (FWD and AFT)- All 21-31-03-04 RTG

OVERHEAT CIRCUIT L1 S

Engine Overheat Circuits 26-11-02 CDOVERHEAT CIRCUIT L2 SOVERHEAT CIRCUIT R1 SOVERHEAT CIRCUIT R2 SOVERHEAT ENG L C No DispatchOVERHEAT ENG R C No DispatchOVERSPEED W N/AOVERSPEED SYS S No Dispatch

777 MEL


1-00-02-02.35 23 OCT 2013

OVERSPEED VFE S No DispatchOVERSPEED VMO/MMO S No DispatchOVRD VALVE MOTOR L S

Equipment Cooling Override Valve Motors 21-27-03 RTGOVRD VALVE MOTOR R S

Message L Condition MEL Item A/D/CPACK ACM L S

Air Cycle Machines (ACM) 21-52-01 RTGPACK ACM R S

PACK FCV LPACK FCV R

SS

Pack Flow Control/Shutoff Valves (FCVs)- Upper FCVs 21-51-02-01 RTG

Pack Flow Control/Shutoff Valves (FCVs)- Lower FCVs 21-51-02-02 RTG

PACK FCV LWR L S Pack Flow Control/Shutoff Valves (FCVs)- Lower FCVs 21-51-02-02 RTG

PACK FCV LWR R S Pack Flow Control/Shutoff Valves (FCVs)- Lower FCVs 21-51-02-02 RTG

PACK FCV UPR L S Pack Flow Control/Shutoff Valves (FCVs)- Upper FCVs 21-51-02-01 RTG

PACK FCV UPR R S Pack Flow Control/Shutoff Valves (FCVs)- Upper FCVs 21-51-02-01 RTG

PACK LPACK L

AS

Air Conditioning Packs- Passenger 21-51-01-03 RTG

Air Conditioning Packs- 777F 21-51-01-05 RTG

Air Conditioning Packs- All 21-51-01-06 RTG

PACK L + R C




PACK MODE LPACK MODE R

AA

Air Cycle Machines (ACM) 21-52-01 RTGEconomy Cooling Valves (ECV)- One Valve Inoperative 21-52-02A RTG

Economy Cooling Valves (ECV)- Both Valves Inoperative Deactivated Closed 21-52-02B RTG

Condenser Inlet Temperature Control Systems 21-52-07 RTGPACK OUT TEMP SNSR L S

Pack Discharge Temperature Sensors 21-52-04 RTGPACK OUT TEMP SNSR R S

PACK RPACK R

AS




PARKING BRAKE SET M N/APASS OXYGEN C S Passenger Oxygen System 35-21-01 RTG

777 MEL


1-00-02-02.36 23 OCT 2013

PASS OXYGEN L SPASS OXYGEN LOW APASS OXYGEN ON A N/APASS OXYGEN R S Passenger Oxygen System 35-21-01 RTGPASS SIGNS ON M N/A

PASSENGER ADDRESS S

Passenger Address System (Passenger) 23-31-01 CDPassenger Address System (Passenger)- Passenger Address Controller Mode 23-31-01-01 CD

Passenger Address System (Passenger)- Lavatory Speakers 23-31-01-02 CD

Passenger Address System (Passenger)- Cabin Speakers- Inoperative Speakers Not Adjacent

23-31-01-03A CD

Passenger Address System (Passenger)- Cabin Speakers- Inoperative Speakers Adjacent

23-31-01-03B RTG

Passenger Address System (Passenger)- Ambient Noise Sensor (ANS) System 23-31-01-04 CD

Passenger Address System (Passenger)- Prerecorded Passenger Announcement System 23-31-01-05 CD

PDCU L SPanel Data Concentrator Units (PDCU) 23-93-03 CD

PDCU R SPFC CHANNEL S Primary Flight Computer (PFC) Channels 27-02-03 RTGPFC CONTROL LANES S Primary Flight Computer (PFC) Lanes 27-02-02 CDPFCS INTERFACE S PFCS Interface 27-02-04 RTGPILOT RESPONSE A N/APILOT RESPONSE C N/APILOT RESPONSE W N/APITCH DOWN AUTHORITY C No DispatchPITCH UP AUTHORITY C No Dispatch

PITOT ADM C S Pitot Air Data Modules (Primary - ARINC 629)- Center Pitot Air Data Module 34-21-04-03 RTG

PITOT ADM L S Pitot Air Data Modules (Primary - ARINC 629)- Left Pitot Air Data Module 34-21-04-02 RTG

PITOT ADM R S Pitot Air Data Modules (Primary - ARINC 629)- Right Pitot Air Data Module 34-21-04-01 RTG

PRI FLIGHT COMPUTERS C No DispatchPRINTER COMM MESSAGE N/APSEU 1 S No DispatchPSEU 2 S No Dispatch

PSEU 1 CHANNELPSEU 2 CHANNEL

SS

Proximity Sensor Electronic Unit (PSEU) Channels- One Inoperative 32-08-01A CD

Proximity Sensor Electronic Unit (PSEU) Channels- Two Inoperative - PSEU 1 On Left System Bus, PSEU 2 On Right System Bus

32-08-01B RTG

Proximity Sensor Electronic Unit (PSEU) ChannelsTwo Inoperative - PSEU 1 On Right System Bus,PSEU 2 On Left System Bus

32-08-01C RTG

777 MEL


1-00-02-02.37 23 OCT 2013

Proximity Sensor Electronic Unit (PSEU) Channels- Two Inoperative - Gear Down Dispatch 32-08-01D RTG

PVD BOTH ON M N/APVD CAPT ON M N/APVD F/O ON M N/A

Message L Condition MEL Item A/D/CR GEAR DOOR SENSOR S Landing Gear Door Position Sensors 32-61-02 RTGR GEAR UPLOCK SENSOR S Landing Gear Uplock Position Sensors 32-61-03 RTGRADIO ALT CRADIO ALT MONITOR C S

Radio Altimeter Systems 34-33-01 CDRADIO ALT LRADIO ALT MONITOR L S

RADIO ALT RRADIO ALT MONITOR R S

RADIO TRANSMIT A N/A

RAM AIR EXIT DOOR LRAM AIR EXIT DOOR R

SS

Ram Air Exhaust Door Systems(HL7743 & Subsequent)- -200ER/-300ER- Pack(s) May Be Used

21-52-06-01A RTG

Ram Air Exhaust Door Systems(HL7743 & Subsequent)- 777F- Pack(s) Is Not Used

21-52-06-02A RTG

Ram Air Exhaust Door Systems(HL7743 & Subsequent)- -200ER/-300ER- Pack(s) Is Not Used

21-52-06-01B RTG

Ram Air Exhaust Door Systems(HL7743 & Subsequent)- 777F- Pack(s) Is Not Used

21-52-06-02B RTG

RAM AIR INLET DOOR LRAM AIR INLET DOOR R

SS

Ram Air Inlet Door Systems- Pack(s) May Be Used 21-52-05A RTG

Ram Air Inlet Door Systems- Pack(s) Is Not Used 21-52-05B RTG

RAT DEPLOY INOP S No DispatchRAT GEN HEAT S RAT Heater System 29-21-01-01 RTGRAT UNLOCKED A No Dispatch

RECIRC FAN S Recirculation Fans (Upper, Lower)- Passenger 21-25-01-01 RTG

RECIRC FAN S Recirculation Fans (Lower)- 777F 21-25-01-02 RTG

RECIRC FANS OFF M N/AREMOTE LIGHT SENSOR S Remote Light Sensor (RLS) System 31-61-03 CDRESERVE BRAKES/STRG A Center Hydraulic Isolation System 29-11-06 RTG

REVERSER INTERLOCK LREVERSER INTERLOCK R

SS

Reverse Thrust Lever Interlocks- 200ER/-300 78-34-01-01 CD

777 MEL


1-00-02-02.38 23 OCT 2013

Reverse Thrust Lever Interlocks- 300ER/777F- Interlock Released

78-34-01-02A CD

Reverse Thrust Lever Interlocks- 300ER/777F- Interlock Retracted

78-34-01-02B CD

RSCF ASG CARD LRSCF ASG CARD R

SS

Systems Cardfile ARINC Signal Gateway (ASG) Cards- Right Systems Cardfile ASG Cards 31-09-01-02 CD

RSCF PWR SUPPLY 1 SSystems Cardfile Power Supplies- Right Systems Cardfile (RSCF) Power Supplies- Power Supply 1 Inoperative

31-09-02-02B RTG

RSCF PWR SUPPLY 2 SSystems Cardfile Power Supplies- Right Systems Cardfile (RSCF) Power Supplies- Power Supply 2 Inoperative

31-09-02-02A RTG

RUNWAY OVRD A N/ARUNWAY POS A N/A


SAARU S

Secondary Attitude Air Data Reference Unit (SAARU)- Without Integrated Standby Flight Display (ISFD)Installed

34-21-07-01 RTG

Secondary Attitude Air Data Reference Unit (SAARU)- With Integrated Standby Flight Display (ISFD)Installed

34-21-07-02 CD

SATCOM ASatellite Communication (SATCOM) Systems 23-15-01 CDSatellite Communication (SATCOM) Systems- SATCOM Voice Systems 23-15-01-01 CD

SATCOM COOLING FAN LSATCOM COOLING FAN R

SS

SATCOM Backup Cooling Fans- Both Lavatory/Galley Vent Fans Operational 21-27-09A RTG

SATCOM Backup Cooling Fans- Lavatory/Galley Fan(s) Inoperative 21-27-09A RTG

SATCOM DATALINK A Satellite Communication (SATCOM) Systems- SATCOM Data Link 23-15-01-02A CD

SATCOM DATALINK OFF M N/A

SATCOM HI GAIN S Satellite Communication (SATCOM) Systems- SATCOM Voice Systems 23-15-01-01 CD

SATCOM MESSAGE COMM MESSAGE N/ASATCOM MESSAGE COMM MESSAGE N/A

SATCOM SYSTEMSATCOM VOICE

SA

Satellite Communication (SATCOM) Systems 23-15-01 CDSatellite Communication (SATCOM) Systems- SATCOM Voice Systems 23-15-01-01 CD

SATVOICE AVAIL COMM MESSAGE N/ASATVOICE LOST A N/ASEATBELTS ON M N/ASELCAL COMM MESSAGE N/ASEMI LEVER GEAR S

Semi-Lever Gear (SLG) System (-300ER) 32-30-02 RTGSEMI LEVER GEAR LOCK S

777 MEL


1-00-02-02.39 23 OCT 2013

SEMI LEVER GEAR SYS SSGL SOURCE AIR DATA A No DispatchSGL SOURCE DISPLAYS C No DispatchSGL SOURCE RAD ALT A No DispatchSINGLE SOURCE F/D A 22-11-10SINGLE SOURCE ILS C Instrument Landing System (ILS) 34-31-01 CDSLATS DRIVE C No DispatchSLATS PRIMARY FAIL C No DispatchSLATS SECONDARY FAIL S Slat Secondary Control 27-03-03 RTG

SMOKE COMP UPR DR 1 C N/ASMOKE COMP UPR DR 2 C N/ASMOKE COMP UPR DR 3 C N/ASMOKE COMP UPR DR 4 C N/ASMOKE COMP UPR DR 5 C N/ASMOKE CREW REST F/D C N/ASMOKE CREW REST LWR C N/ASMOKE CREW REST MAIN C N/ASMOKE EQUIP COOLING C N/ASMOKE LAV/COMPT A N/ASMOKE LAVATORY A N/ASMOKE LAVATORY C N/ASMOKE REST UPR DR 1 C N/ASMOKE REST UPR DR 2 C N/ASMOKE REST UPR DR 3 C N/ASMOKE REST UPR DR 4 C N/ASMOKE REST UPR DR 5 C N/ASOV CREW REST LWR S Lower Lobe Attendant Rest (LLAR) Shutoff Valve 21-29-01 RTG

SOV REST UPR AFT S Overhead Flight Attendant Rest Supply Shutoff Valves- Overhead Flight Attendant Rest (OFAR) (-300ER) 21-29-04-02 RTG

SPEEDBRAKE ARMED M N/ASPEEDBRAKE EXTENDED C N/ASPEEDBRAKE LEV XDCR S Speedbrake Lever Position Transducers 27-61-01 CD

SPOILER ACTUATOR S

Spoiler Power control Units (PCUs)- Passenger 27-61-03-01 RTG

Spoiler Power control Units (PCUs)- 777F 27-61-03-02 RTG

SPOILERS A

Spoiler Power control Units (PCUs)- Passenger 27-61-03-01 RTG

Spoiler Power control Units (PCUs)- 777F 27-61-03-02 RTG

STAB AUTO SHUTDOWN S No Dispatch

STAB GREENBAND ANose Gear Pressure Switch 27-48-03 CDNose Gear Pressure Transducer 27-48-04 CD

STAB POSITION XDCR S Stabilizer Position Transducer Modules 27-48-02 CD

777 MEL


1-00-02-02.40 23 OCT 2013

STAB RATE VALVE S Stabilizer Trim Rate Solenoid Valves 27-41-03 CDSTABILIZER W No DispatchSTABILIZER C A No DispatchSTABILIZER CUTOUT A N/ASTABILIZER R A No Dispatch

STALL W SYS LSTALL W SYS R

SS

Stall Warning Systems 27-32-01 CDStall Warning Systems- Stick Shakers 27-32-01-01 CD

STANDBY INVERTER S No Dispatch

STATIC ADM C S Static Air Data Modules (Primary - ARINC 629)- Center Static Air Data Module 34-21-05-03 RTG

STATIC ADM L S Static Air Data Modules (Primary - ARINC 629)- Left Static Air Data Module 34-21-05-02 RTG

STATIC ADM R S Static Air Data Modules (Primary - ARINC 629)- Right Static Air Data Module 34-21-05-01 RTG

SUPRNMRY CALL COMM MESSAGE N/ASUPRNMRY DUCT

SENSOR S Supernumerary Duct Temperature Sensing System- 777F 21-61-19 RTG

SUPRNMRY OXYGEN LOW S Supernumerary Seats/Crew Rest/Lavatory GaseousOxygen System (777F) 35-21-06 RTG

SUPRNMRY OXYGEN ON A N/A

SUPRNMRY OXYGEN C SSupernumerary Seats/Crew Rest/Lavatory GaseousOxygen System (777F)- Center Circuit

35-21-06-02 RTG

SUPRNMRY OXYGEN L SSupernumerary Seats/Crew Rest/Lavatory GaseousOxygen System (777F)- Left Circuit

35-21-06-01 RTG

SUPRNMRY OXYGEN R SSupernumerary Seats/Crew Rest/Lavatory GaseousOxygen System (777F)- Right Circuit

35-21-06-03 RTG

SUPRNMRY SIGNS ON M N/A

SUPRNMRY TRIM VALVE S Supernumerary Zone Trim Air Modulation Valve- 777F 21-61-20 RTG

Message L Condition MEL Item A/D/CTAIL SKID A Tail Strike Detector Channels 32-72-01 CDTAIL SKID S Tail Strike Detector Channels 32-72-01 CDTAIL STRIKE C No DispatchTAIL STRIKE CHAN 1 S Tail Strike Detector Channels 32-71-01 CDTAIL STRIKE CHAN 2 S Tail Strike Detector Channels 32-71-01 CDTAT S No DispatchTCAS A Traffic Collision and Avoidance System (TCAS) 34-45-01 RTGTCAS S 34-45-01TCAS OFF A N/ATCAS RA CAPTAIN A Traffic Collision and Avoidance System (TCAS) 34-45-01 RTG

777 MEL


1-00-02-02.41 23 OCT 2013

TCAS RA F/OFor Crew Defer, Contact the MCC to obtain the determination of the MEL item to be applied.

A Traffic Collision and Avoidance System (TCAS)- Resolution Advisory (RA) Display Systems- One Inoperative

34-45-01-01A CD

Traffic Collision and Avoidance System (TCAS)- Resolution Advisory (RA) Display Systems- Both Inoperative

34-45-01-01B CD

TERR OVRD A N/A

TERR POS AStatus Msg : TERR SYSGround Proximity Warning System (GPWS)- Terrain Awareness Function

34-46-01-03 CD

TERR SYS S Ground Proximity Warning System (GPWS)- Terrain Awareness Function 34-46-01-03 CD

THERAPEUTIC OXY ON M N/ATHRUST ASYM COMP A

Thrust Asymmetry Compensation (TAC) Function 27-02-08 CDTHRUST ASYM COMP STIRE PRESSTIRE PRESSTIRE PRESS SYS

ASS

Tire Pressure Indication System (TPIS)- Required By Procedures 32-49-01A CD

TRANSPONDER LTRANSPONDER LTRANSPONDER RTRANSPONDER R

AAAA

ATC Transponder/Automatic Altitude ReportingSystems- One Inoperative

34-53-01A CD

ATC Transponder/Automatic Altitude ReportingSystems- Both Inoperative

34-53-01B RTG

ATC Transponder/Automatic Altitude ReportingSystems- Elementary and Enhanced Downlink AircraftReportable Parameters Not Required By Regulations

34-53-01-01 RTG

ATC Transponder/Automatic Altitude ReportingSystems- ADS-B Squitter Transmissions

34-53-01-02 RTG

TRIM AIR LTRIM AIR R

AA

Status Msg : TRIM AIR L or RTrim Air Control Systems- Passenger- One Inoperative- Only TRIM AIR L or TRIM AIR R EICAS Advisory Message display, flight crew may apply to Crew Defer procedure.

21-62-01-01A CD

Status Msg : TRIM AIR L and RTrim Air Control Systems- Passenger- Both Inoperative

21-62-01-01B RTG

Status Msg : TRIM AIR L or RTrim Air Control Systems- 777F- One Inoperative

21-62-01-02-02 RTG

Status Msg : TRIM AIR PRSOV L or RTrim Air Pressure Regulating/Shutoff Valves(PRSOVs)- Passenger- One Inoperative

21-62-02-01A RTG

777 MEL


1-00-02-02.42 23 OCT 2013

Status Msg : TRIM AIR PRSOV L and RTrim Air Pressure Regulating/Shutoff Valves(PRSOVs)- Passenger- Both Inoperative

21-62-02-01B RTG

Status Msg : TRIM AIR PRSOV L or RTrim Air Pressure Regulating/Shutoff Valves(PRSOVs)- 777F- One Inoperative

21-62-02-02-02 RTG

TRIM AIR LTRIM AIR R

SS

Trim Air Control Systems- Passenger- One Inoperative

21-62-01-01A CD

Trim Air Control Systems- Passenger- Both Inoperative

21-62-01-01B RTG


21-62-01-02-02 CD

TRIM AIR PRSOV LTRIM AIR PRSOV R

SS

Trim Air Pressure Regulating/Shutoff Valves(PRSOVs)- Passenger- One Inoperative

21-62-02-01A RTG

Trim Air Pressure Regulating/Shutoff Valves(PRSOVs)- Passenger- Both Inoperative

21-62-02-01B RTG

Trim Air Pressure Regulating/Shutoff Valves(PRSOVs)- 777F- One Inoperative

21-62-02-02-02 RTG

TRIM VLV EQUIP COOL S Equipment Cooling Trim Air Modulation Valve-777F 21-61-18-02 RTG

TURB CASE COOL HPT L S Turbine Case Cooling Air Flow Systems- HPT Systems (PW) 75-24-01-01 RTG

TURB CASE COOL HPT R S Turbine Case Cooling Air Flow Systems- HPT Systems (PW) 75-24-01-01 RTG

TURB CASE COOL LPT L S Turbine Case Cooling Air Flow Systems- LPT Systems (PW) 75-24-01-02 RTG

TURB CASE COOL LPT R S Turbine Case Cooling Air Flow Systems- LPT Systems (PW) 75-24-01-02 RTG

TURB COOLING AIR LTURB COOLING AIR R

SS

Turbine Cooling Air Systems (PW)- One Inoperative 75-24-02A RTG

Turbine Cooling Air Systems (PW)- Both Inoperative 75-24-02B RTG


VHF DATALINK A VHF Communications Systems- VHF Data Link 23-12-01-01 CD

VHF DATALINK OFF M N/AVMO GEAR DOWN M N/AVOR L S Marker Beacon System 34-32-01 CD

777 MEL


1-00-02-02.43 23 OCT 2013

VOR Navigation Systems 34-51-01 CDVOR R S VOR Navigation Systems 34-51-01 CDVSCF VALVE CLOSED L S No DispatchVSCF VALVE CLOSED R S No Dispatch

Message L Condition MEL Item A/D/CWAI CARD S Wing Anti-Ice Control (Card and Switch) 30-11-02 RTGWAI PRESS SENSOR L S Wing Anti-Ice Systems 30-11-01 RTGWAI PRESS SENSOR R S Wing Anti-Ice Systems 30-11-01 RTGWAI VALVE L S Wing Anti-Ice Systems 30-11-01 RTGWAI VALVE R S Wing Anti-Ice Systems 30-11-01 RTGW SPEAKER L S Aural Warning Speaker Systems 31-51-03 CDW SPEAKER R S Aural Warning Speaker Systems 31-51-03 CD

WEU CHANNEL L1WEU CHANNEL L2WEU CHANNEL R1WEU CHANNEL R2

SSSS

Warning Electronics System (WES) Channels- Passenger- Channel Not Deactivated

31-51-04-01A CD

Warning Electronics System (WES) Channels- 777F- Channel Not Deactivated

31-51-04-02A CD

Warning Electronics System (WES) Channels- Passenger- Channel Deactivated

31-51-04-01B RTG

Warning Electronics System (WES) Channels- 777F- Channel Deactivated

31-51-04-02B RTG

WINDOW FLT DECK L A Flight Deck Window Indication Systems (Side - No. 2) 56-11-01 CDWINDOW FLT DECK R A Flight Deck Window Indication Systems (Side - No. 2) 56-11-01 CDWINDOW HEAT A No DispatchWINDOW HEAT BACKUP L S No DispatchWINDOW HEAT BACKUP R S No DispatchWINDOW HEAT L FWD A Flight Deck Forward Window Primary Heater Systems 30-41-01 CDWINDOW HEAT L FWD S Flight Deck Forward Window Primary Heater Systems 30-41-01 CDWINDOW HEAT L SIDE A Flight Deck Side (No. 2) Window Heater Systems 30-41-02 CDWINDOW HEAT L SIDE S Flight Deck Side (No. 2) Window Heater Systems 30-41-02 CDWINDOW HEAT R FWD A Flight Deck Forward Window Primary Heater Systems 30-41-01 CDWINDOW HEAT R FWD S Flight Deck Forward Window Primary Heater Systems 30-41-01 CDWINDOW HEAT R SIDE A Flight Deck Side (No. 2) Window Heater Systems 30-41-02 CDWINDOW HEAT R SIDE S Flight Deck Side (No. 2) Window Heater Systems 30-41-02 CDWINDOWS A Flight Deck Window Indication Systems (Side - No. 2) 56-11-01 CD

WINDSHEAR PRED S

Weather Radar System- Predictive Windshear Function- Reactive Windshear Operative

34-43-01-01A CD

Weather Radar System- Predictive Windshear Function- Reactive Windshear Inoperative

34-43-01-01B CD

777 MEL


1-00-02-02.44 23 OCT 2013

WINDSHEAR REAC S

Ground Proximity Warning System (GPWS)- Windshear Alert Mode Function (Reactive) (Mode 7)- Predictive Windshear Operative

34-46-01-02A CD

Ground Proximity Warning System (GPWS)- Windshear Alert Mode Function (Reactive) (Mode 7)- Predictive Windshear Inoperative

34-46-01-02B CD

WINDSHEAR SYSFor Crew Defer, Contact the MCC to obtain the determination of the MEL item to be applied.

A

Weather Radar System- Predictive Windshear Function- Reactive Windshear Operative

34-43-01-01A CD

Weather Radar System- Predictive Windshear Function- Reactive Windshear Inoperative

34-43-01-01B CD

Ground Proximity Warning System (GPWS)- Windshear Alert Mode Function (Reactive) (Mode 7)- Predictive Windshear Operative

34-46-01-02A CD

Ground Proximity Warning System (GPWS)- Windshear Alert Mode Function (Reactive) (Mode 7)- Predictive Windshear Inoperative

34-46-01-02B CD

WXR SYS S

Weather Radar System- Reactive Windshear Operative 34-43-01A RTG

Weather Radar System- Reactive Windshear Inoperative 34-43-01B RTG

Weather Radar System- One Operative- Crew Defer with maintenance consulting

34-43-01C CD

Weather Radar System- Predictive Windshear Function- Reactive Windshear Operative- Crew Defer with maintenance consulting

34-43-01-01A CD

Weather Radar System- Predictive Windshear Function- Reactive Windshear Inoperative- Crew Defer with maintenance consulting

34-43-01-01B CD

Weather Radar System- Auto Tilt Function 34-43-01-02 CD

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