...26 Fire Protection 26-1 27 Flight Controls 27-1 28 Fuel 28-1 29 Hydraulic Power 29-1 30 Ice and...

Millbrook Aviation Minimum Equipment List Aircraft: CE-750 (Citation X) Revision No: Original Date: 01-16-15

Page I

CE-750 N17XR S/N 750-0251 TABLE of CONTENTS

System ATA NO. System Title Page --- Table of Contents I --- Revision Record III --- Revision Highlights III --- Control Pages V --- Definitions IX --- Preamble XIII --- Procedures XV 21 Air Conditioning 21-1

22 Auto Flight 22-1

23 Communications 23-1

24 Electrical Power 24-1

25 Equipment and Furnishings 25-1

26 Fire Protection 26-1

27 Flight Controls 27-1

28 Fuel 28-1

29 Hydraulic Power 29-1

30 Ice and Rain Protection 30-1

31 Indicating and Recording Systems 31-1

33 Lights 33-1

34 Navigation 34-1

35 Oxygen 35-1

36 Pneumatic 36-1

38 Water / Waste 38-1

46 New Technology 46-1

49 APU 49-1

52 Doors 52-1


Page II

53 Fuselage 53-1

55 Stabilizers 55-1

71 Powerplant 71-1

73 Engine Fuel and Control 73-1

76 Engine Controls 76-1

77 Engine Indicating 77-1

78 Engine Exhaust 78-1

79 Engine Oil 79-1

80 Starting 80-1

--- MEL Index IND-1


Page III

REVISION RECORD

REVISION LOG

REVISION # REVISION DATE AFFECTED PAGES INITIALS

Original 01-16-15 All --- --- --- --- --- --- --- ---

REVISION HIGHLIGHTS

REVISION # REVISION DATE HIGHLIGHTS

Original 01-16-15 All --- --- --- --- --- --- --- ---


Page IV

Intentionally Left Blank


This manual is applicable to Millbrook Aviation CE-750 series aircraft, N17XR S/N 750-251 and is no less restrictive than the FAA approved CE-750 MMEL R6, dated 06/24/2014.

Page V

CONTROL PAGE Page Rev # Date I Original 01-16-15 II Original 01-16-15 III Original 01-16-15 IV Original 01-16-15 V Original 01-16-15 VI Original 01-16-15 VII Original 01-16-15 VIII Original 01-16-15 IX Original 01-16-15 X Original 01-16-15 XI Original 01-16-15 XII Original 01-16-15 XIII Original 01-16-15 XIV Original 01-16-15 XV Original 01-16-15 XVI Original 01-16-15

ATA 21 Air Conditioning 21-1 Original 01-16-15 21-2 Original 01-16-15 21-3 Original 01-16-15 21-4 Original 01-16-15 21-5 Original 01-16-15 21-6 Original 01-16-15 21-7 Original 01-16-15 21-8 Original 01-16-15 21-9 Original 01-16-15 21-10 Original 01-16-15 21-11 Original 01-16-15 21-12 Original 01-16-15 21-13 Original 01-16-15 21-14 Original 01-16-15 21-15 Original 01-16-15 21-16 Original 01-16-15 21-17 Original 01-16-15

Page Rev # Date 21-18 Original 01-16-15 21-19 Original 01-16-15 21-20 Original 01-16-15 21-21 Original 01-16-15 21-22 Original 01-16-15 21-23 Original 01-16-15 21-24 Original 01-16-15 21-25 Original 01-16-15 21-26 Original 01-16-15

ATA 22 Auto Flight 22-1 Original 01-16-15 22-2 Original 01-16-15 22-3 Original 01-16-15 22-4 Original 01-16-15 22-5 Original 01-16-15 22-6 Original 01-16-15 22-7 Original 01-16-15 22-8 Original 01-16-15 22-9 Original 01-16-15 22-10 Original 01-16-15 22-11 Original 01-16-15 22-12 Original 01-16-15

ATA 23 Communications 23-1 Original 01-16-15 23-2 Original 01-16-15 23-3 Original 01-16-15 23-4 Original 01-16-15 23-5 Original 01-16-15 23-6 Original 01-16-15 23-7 Original 01-16-15 23-8 Original 01-16-15 23-9 Original 01-16-15 23-10 Original 01-16-15 23-11 Original 01-16-15

Page Rev # Date 23-12 Original 01-16-15 23-13 Original 01-16-15 23-14 Original 01-16-15 23-15 Original 01-16-15 23-16 Original 01-16-15 23-17 Original 01-16-15 23-18 Original 01-16-15

ATA 24 Electrical Power 24-1 Original 01-16-15 24-2 Original 01-16-15 24-3 Original 01-16-15 24-4 Original 01-16-15 24-5 Original 01-16-15 24-6 Original 01-16-15 24-7 Original 01-16-15 24-8 Original 01-16-15 24-9 Original 01-16-15 24-10 Original 01-16-15 24-11 Original 01-16-15 24-12 Original 01-16-15

ATA 25 Equipment and Furnishings

25-1 Original 01-16-15 25-2 Original 01-16-15 25-3 Original 01-16-15 25-4 Original 01-16-15 25-5 Original 01-16-15 25-6 Original 01-16-15 25-7 Original 01-16-15 25-8 Original 01-16-15 25-9 Original 01-16-15 25-10 Original 01-16-15 25-11 Original 01-16-15 25-12 Original 01-16-15

FAA APPROVED D.O. IDENTIFIER FSDO # NAME EFFECTIVE

DATE SIGNATURE



Page VI

Page Rev # Date 25-13 Original 01-16-15 25-14 Original 01-16-15 25-15 Original 01-16-15 25-16 Original 01-16-15 25-17 Original 01-16-15 25-18 Original 01-16-15 25-19 Original 01-16-15 25-20 Original 01-16-15 25-21 Original 01-16-15 25-22 Original 01-16-15

ATA 26 Fire Protection 26-1 Original 01-16-15 26-2 Original 01-16-15 26-3 Original 01-16-15 26-4 Original 01-16-15 26-5 Original 01-16-15 26-6 Original 01-16-15

ATA 27 Flight Controls 27-1 Original 01-16-15 27-2 Original 01-16-15 27-3 Original 01-16-15 27-4 Original 01-16-15 27-5 Original 01-16-15 27-6 Original 01-16-15 27-7 Original 01-16-15 27-8 Original 01-16-15 27-9 Original 01-16-15 27-10 Original 01-16-15

ATA 28 Fuel 28-1 Original 01-16-15 28-2 Original 01-16-15 28-3 Original 01-16-15 28-4 Original 01-16-15 28-5 Original 01-16-15 28-6 Original 01-16-15

Page Rev # Date 28-7 Original 01-16-15 28-8 Original 01-16-15

ATA 29 Hydraulic Power 29-1 Original 01-16-15 29-2 Original 01-16-15

ATA 30 Ice and Rain Protection

30-1 Original 01-16-15 30-2 Original 01-16-15 30-3 Original 01-16-15 30-4 Original 01-16-15 30-5 Original 01-16-15 30-6 Original 01-16-15 30-7 Original 01-16-15 30-8 Original 01-16-15 30-9 Original 01-16-15 30-10 Original 01-16-15 30-11 Original 01-16-15 30-12 Original 01-16-15 30-13 Original 01-16-15 30-14 Original 01-16-15 30-15 Original 01-16-15 30-16 Original 01-16-15 30-17 Original 01-16-15 30-18 Original 01-16-15 30-19 Original 01-16-15 30-20 Original 01-16-15

ATA 31 Indicating and Recording Systems

31-1 Original 01-16-15 31-2 Original 01-16-15 31-3 Original 01-16-15 31-4 Original 01-16-15 31-5 Original 01-16-15 31-6 Original 01-16-15 31-7 Original 01-16-15

Page Rev # Date 31-8 Original 01-16-15 31-9 Original 01-16-15 31-10 Original 01-16-15

ATA 33 Lights 33-1 Original 01-16-15 33-2 Original 01-16-15 33-3 Original 01-16-15 33-4 Original 01-16-15 33-5 Original 01-16-15 33-6 Original 01-16-15 33-7 Original 01-16-15 33-8 Original 01-16-15 33-9 Original 01-16-15 33-10 Original 01-16-15 33-11 Original 01-16-15 33-12 Original 01-16-15 33-13 Original 01-16-15 33-14 Original 01-16-15 33-15 Original 01-16-15 33-16 Original 01-16-15 33-17 Original 01-16-15 33-18 Original 01-16-15 33-19 Original 01-16-15 33-20 Original 01-16-15

ATA 34 Navigation 34-1 Original 01-16-15 34-2 Original 01-16-15 34-3 Original 01-16-15 34-4 Original 01-16-15 34-5 Original 01-16-15 34-6 Original 01-16-15 34-7 Original 01-16-15 34-8 Original 01-16-15 34-9 Original 01-16-15 34-10 Original 01-16-15


DATE SIGNATURE



Page VII

Page Rev # Date 34-11 Original 01-16-15 34-12 Original 01-16-15 34-13 Original 01-16-15 34-14 Original 01-16-15 34-15 Original 01-16-15 34-16 Original 01-16-15 34-17 Original 01-16-15 34-18 Original 01-16-15 34-19 Original 01-16-15 34-20 Original 01-16-15 34-21 Original 01-16-15 34-22 Original 01-16-15 34-23 Original 01-16-15 34-24 Original 01-16-15 34-25 Original 01-16-15 34-26 Original 01-16-15 34-27 Original 01-16-15 34-28 Original 01-16-15 34-29 Original 01-16-15 34-30 Original 01-16-15 34-31 Original 01-16-15 34-32 Original 01-16-15 34-33 Original 01-16-15 34-34 Original 01-16-15 34-35 Original 01-16-15 34-36 Original 01-16-15

ATA 35 Oxygen 35-1 Original 01-16-15 35-2 Original 01-16-15 35-3 Original 01-16-15 35-4 Original 01-16-15 35-5 Original 01-16-15 35-6 Original 01-16-15 35-7 Original 01-16-15 35-8 Original 01-16-15

Page Rev # Date 35-9 Original 01-16-15 35-10 Original 01-16-15

ATA 36 Pneumatic 36-1 Original 01-16-15 36-2 Original 01-16-15

ATA 38 Water/Waste 38-1 Original 01-16-15 38-2 Original 01-16-15 38-3 Original 01-16-15 38-4 Original 01-16-15 38-5 Original 01-16-15 38-6 Original 01-16-15

ATA 46 New Technology 46-1 Original 01-16-15 46-2 Original 01-16-15

ATA 49 APU 49-1 Original 01-16-15 49-2 Original 01-16-15 49-3 Original 01-16-15 49-4 Original 01-16-15 49-5 Original 01-16-15 49-6 Original 01-16-15

ATA 52 Doors 52-1 Original 01-16-15 52-2 Original 01-16-15 52-3 Original 01-16-15 52-4 Original 01-16-15 52-5 Original 01-16-15 52-6 Original 01-16-15 52-7 Original 01-16-15 52-8 Original 01-16-15 52-9 Original 01-16-15 52-10 Original 01-16-15 52-11 Original 01-16-15 52-12 Original 01-16-15

Page Rev # Date ATA 53 Fuselage

53-1 Original 01-16-15 53-2 Original 01-16-15 53-3 Original 01-16-15 53-4 Original 01-16-15

ATA 55 Stabilizers 55-1 Original 01-16-15 55-2 Original 01-16-15

ATA 71 Powerplant 71-1 Original 01-16-15 71-2 Original 01-16-15

ATA 73 Engine Fuel and Control

73-1 Original 01-16-15 73-2 Original 01-16-15 73-3 Original 01-16-15 73-4 Original 01-16-15

ATA 76 Engine Controls 76-1 Original 01-16-15 76-2 Original 01-16-15

ATA 77 Engine Indicating 77-1 Original 01-16-15 77-2 Original 01-16-15 77-3 Original 01-16-15 77-4 Original 01-16-15

ATA 78 Engine Exhaust 78-1 Original 01-16-15 78-2 Original 01-16-15

ATA 79 Engine Oil 79-1 Original 01-16-15 79-2 Original 01-16-15 79-3 Original 01-16-15 79-4 Original 01-16-15

ATA 80 Starting 80-1 Original 01-16-15 80-2 Original 01-16-15


DATE SIGNATURE



Page VIII

Page Rev # Date MEL Index

IND-1 Original 01-16-15 IND-2 Original 01-16-15 IND-3 Original 01-16-15 IND-4 Original 01-16-15 IND-5 Original 01-16-15 IND-6 Original 01-16-15


DATE SIGNATURE


Page IX

Definitions

1. 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.

2. ATA System Page. The ATA system page is divided into six (6) columns (A thru F) 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. Item is the sequence number.

B. Name/Description. Name/Description depicts the equipment, system, component, or function.

C. Repair Category. Repair Category describes the time interval to repair MEL items.

D. 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.

E. 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.

F. 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.

G. Provisos. Provisos are indicated by a number or a lower case letter in “Remarks or Exceptions”. Provisos are conditions or limitations that must be complied with for operation with the listed instrument or equipment item inoperative.

H. 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.

I. 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 MEL are removed prior to the release of the next revision.

3. Airplane Flight Manual (AFM). The FAA approved AFM is the document approved by the responsible FAA Aircraft Certification Office (ACO) during type certification. 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 FAA requires an approved flight manual for aircraft type certification.

4. Code of Federal Regulations (CFR) and Federal Aviation Regulations (FAR). CFR, the current term, and FAR both refer to the applicable portions of the Federal Aviation Act and Code of Federal Regulations.


Page X

5. 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.

6. Continuing Authorization – Single Extension. An aircraft operator who has the authorization to use an FAA 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.

7. 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.

8. 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.

9. 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.

10. Flight Day. A flight day is a 24 hour period (from midnight to midnight) local time, during which at least one flight is initiated for the affected aircraft.

11. 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.

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

13. 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).

14. 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).

15. 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.

16. Nonessential Equipment and Furnishings (NEF). NEFs are those items installed on the aircraft as part of the original type certification, STC, or other form of alteration that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules. They are those items that, if inoperative, damaged, or missing, have no effect on the aircraft’s ability to be operated safely under all operational conditions. 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.


Page XI

17. 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 MMEL item specifies that an item of equipment must be operative, it does not mean that its operational status must be verified; it’s to be considered operative unless reported or known to be malfunctioning. When an MMEL 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 MMEL item. When an MMEL 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 MMEL is “operates normally”, "fully operative", and "considered operative”. The aircraft operator's MEL may incorporate standardized terminology of the aircraft operator’s choice to specify that an item of equipment must be operative, provided the aircraft operator's MEL definitions indicate that the selected "operative" terminology means that the required item of equipment will accomplish its intended purpose and is consistently functioning normally within its design operating limit(s) and tolerance(s).

18. 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. The MEL Sticker Location column below each MEL item depicts where the placard should be placed.

19. Repair Category. All users of an MEL approved under parts 91K, 121, 125, 129, 135 and 142 must effect repairs of inoperative instrument and equipment items, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators:

A. Repair Category A. This category item must be repaired within the time interval specified in the “Remarks or Exceptions” column of the aircraft operator’s approved MEL. For time intervals specified in “calendar days” or “flight days”, the day the malfunction was recorded in the aircraft maintenance record/logbook is excluded. For all other time intervals (i.e., flights, flight legs, cycles, hors, etc.), repair tracking begins at the point when the malfunction is deferred in accordance with the operator’s approved MEL.

B. Repair Category B. This category item must be repaired within 3 consecutive calendar days (72 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 3 day interval would begin at midnight the 26th and end at midnight the 29th.

C. Repair Category C. This category item must be repaired within 10 consecutive calendar days (240 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

D. Repair Category D. This category item must be repaired within 120 consecutive calendar days (2880 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook.

20. Takeoff. Takeoff is the act of beginning a flight in which an aircraft is accelerated from a state of rest to that of flight. For the purposes of MEL relief, this translates to the point at which the pilot physically begins to apply power to initiate the takeoff from the runway or takeoff surface.Visible Moisture. An atmospheric environment containing water, in any form, that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

21. Visual Flight Rules (VFR). VFR is as defined in 14 CFR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

22. Visual Meteorological Conditions (VMC). VMC means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules.


Page XII

23. (M). This symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally, these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment, should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the aircraft operator. Appropriate procedures are required to be produced as part of the aircraft operator’s manual or MEL.

24. (O). This symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally, these procedures are accomplished by the flightcrew; however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the aircraft operator. Appropriate procedures are required to be produced as a part of the aircraft operator’s manual or MEL.


Page XIII

Preamble

(Effective 6/14/89)

The following is applicable for authorized certificate holders operating under Title 14 Code of Federal Regulations (14 CFR) Parts 121, 125, 129, 135: 14 CFR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety.

A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which take into consideration the operator's particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment. Equipment not required by the operation being conducted and equipment in excess of 14 CFR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.

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

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

The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by 14 CFR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative. When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by 14 CFR. Such documentation is required prior to operation with any item of equipment inoperative.

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered. Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

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


Page XIV



Page XV

Procedures

General

The following are general procedures to be used any time a maintenance (M) or operations (O) procedures are to be accomplished by an authorized person. An authorized person is defined as a person qualified in accordance with applicable Federal Aviation Regulations who has been given responsibility by appropriate company management personnel to perform these procedures.

Circuit Breaker Disengagement, Safetying & Fuse Removal

This Describes the requirements when authorized personnel disengage circuit breakers (CB) and the maintenance procedure for safetying CBs in the off position and/or fuse removal. Aircraft may continue in service provided authorized personnel comply with the following procedures and/or restrictions:

1. Push button type CBs are locked in the off position by slipping a CB lockout device over the push button shaft or by tying off with a plastic bundle tie.

2. Fuses are inspected and replaced, or removed as necessary.

3. The discrepancy is recorded and deferred in accordance with the company MEL Procedures, Reference General Operations Manual Section Flight Procedures, page 67.

Placarding Procedures

This describes the requirements when authorized personnel placard an item as required by the MEL. Aircraft may continue in service provided authorized personnel comply with the following procedures and/or restrictions:

Placards must be placed on or adjacent to an inoperative switch, instrument or component as soon as practical. When an item is found to be inoperative, it is to be written up at the end of that flight. Unless authorized personnel correct the discrepancy, the item shall be deferred, if permitted by the MEL, and placarded.

The person installing the placard shall attach or place a self-adhesive inoperative placard immediately adjacent to the defective instrument, control, switch, or device. If a self-adhesive inoperative placard is not available, a piece of paper with inoperative written on it shall be taped in place. After installing the placard it is necessary to clearly record the malfunctioning equipment status in the aircraft's maintenance record in accordance with the companies MEL Procedures.

Crew Operating Procedures

Items marked with a (O) require operating procedures to be performed normally by flightcrew personnel. The following procedures and/or restrictions apply any time an operating procedure is performed and must be complied with before the specific operating procedures outlined in the following pages of the MEL are accomplished. Aircraft may continue in service provided flightcrew personnel comply with the following:

1. It is determined that the item is deferrable according to the MEL.

2. It is determined that the discrepancy will not affect the safety of the flight.

3. It is determined that required alternate equipment is operative.

4. The PIC will brief the SIC on the procedure to be used during the flight.

5. The PIC will brief the FA on the procedure to be used during the flight.


Page XVI

Maintenance Procedures

Items marked with an (M) require maintenance procedures to be performed by authorized personnel. The following procedures and/or restrictions apply at any time a maintenance procedure is performed and must be complied with before the specific maintenance procedures outlined in the following pages of the MEL are accomplished. Aircraft may continue in service provided authorized personnel comply with the following:

1. It is determined that the item is deferrable according to the MEL.

2. It is determined that the discrepancy will not affect the safety of the flight.

3. It is determined that required alternate equipment is operative.

4. Authorized personnel should utilize the procedures in the Manufacturer's Maintenance Manuals and Technical Publications any time the maintenance is being performed.

Stowing Electrical Connectors

Whenever a procedure calls for disconnecting or unplugging an electrical wire or cannon plug, the following procedures shall be accomplished:

1. For Electrical Wiring:

A. Assure the electrical wire(s) will not arc or short and if necessary, wrap wire ends in a non-conductible material.

B. Place end of the wire(s) in a plastic bag and tie-wrap.

OR

C. Secure the wire(s) to a suitable nearby stationary object.

2. For Cannon Plug:

A. Place cannon plug in plastic bag and tie-wrap.

OR

B. Secure the cannon plug to a suitable nearby stationary object.

NOTE: Fuel lines, hydraulic lines, control cables, etc. are not suitable objects for securing electrical wires or cannon plugs. Protection against chafing, battery acids, fluids, personnel and cargo, high temperatures, and protection in wheel wells and landing gear areas must be assured.

Flight Crew Deferral Procedures:

Flight Crew Deferral Item column found in each MEL item indicates whether or not Flight Crews may accomplish the deferral process. For items with a “YES”, Flight Crews have been qualified and authorized to perform all procedures associated with the MEL item. Normally, (M) Maintenance procedures are accomplished by maintenance personnel; however, if the “Flight Crew Deferral Item” column indicates “YES”, after coordinating with Maintenance Control, Flight Crews may perform (M) Maintenance procedures. For MEL items with a “NO” in the Flight Crew Deferral Item column, then Maintenance will be required to defer the item. At any time, the Flight Crew may request Maintenance to defer any MEL item.


Page 21-1

Chapter 21 Air Conditioning Page Number

21-20-01 Cabin Overhead Air Outlet ........................................................................................................ 21-2

21-20-02 Cockpit Overhead Air Outlet ..................................................................................................... 21-3

21-21-02 Baggage Compartment Warm Air Fan ..................................................................................... 21-4

21-21-03 Cabin Recirculation Fan ............................................................................................................ 21-5

21-21-06 Glareshield Fan ......................................................................................................................... 21-6

21-21-08 Nose Avionics Cooling Fan ....................................................................................................... 21-7

21-30-01 Cabin Dump Function ............................................................................................................... 21-8

21-30-02 Cabin Pressurization System .................................................................................................... 21-9

21-30-04 Baggage Compartment Pressurization System ...................................................................... 21-11

21-31-01 Cabin Pressurization Control Panel ........................................................................................ 21-12

21-31-02 Cabin Pressurization System Mode ........................................................................................ 21-13

21-32-01 Cabin Altitude Gauge/Indication ............................................................................................. 21-14

21-32-02 Cabin Differential Pressure Gauge/Indication......................................................................... 21-16

21-32-03 Cabin Vertical Speed Gauge/Indication .................................................................................. 21-17

21-33-01 Cabin Outflow Valve ............................................................................................................... 21-18

21-33-04 PAC Isolation Valve ................................................................................................................ 21-19

21-50-04 Pressurization Air Conditioning (PAC) System ....................................................................... 21-20

21-60-01 Cockpit and Cabin Temperature Control System ................................................................... 21-22

21-61-01 Cabin Temperature Remote Control ....................................................................................... 21-23

21-61-02 Temperature Control Panel..................................................................................................... 21-24

21-62-01 Temperature Indication System .............................................................................................. 21-25

21-70-01 Water Separator ...................................................................................................................... 21-26

ATA 21 – Air Conditioning


Page 21-2

21-20-01 Cabin Overhead Air Outlet Repair Category Number Installed

Name/Description Number Required For Dispatch

Item Remarks Or Exceptions -20-01 Cabin Overhead

Air Outlet C 10 0 May be inoperative.

Item MEL Sticker Location Flight Crew Deferral Item

21-20-01 Near The Environmental Control Panel YES



Page 21-3

21-20-02 Cockpit Overhead Air Outlet Repair Category Number Installed


Item Remarks Or Exceptions -20-02 Cockpit Overhead

Air Outlet (Units -0001 thru -0500)

C 2 0 May be inoperative.


21-20-02 Near The Cockpit Air Outlet YES



Page 21-4

21-21-02 Baggage Compartment Warm Air Fan Repair Category Number Installed


Item Remarks Or Exceptions -21-02 Baggage

Compartment Warm Air Fan






Page 21-5

21-21-03 Cabin Recirculation Fan Repair Category Number Installed


Item Remarks Or Exceptions -21-03 Cabin

Recirculation Fan (WEMAC Boost) (Units -0001 thru -0500)



21-21-03 Near The Cabin Recirculation Fan Switch YES



Page 21-6

21-21-06 Glareshield Fan Repair Category Number Installed


Item Remarks Or Exceptions -21-06 Glareshield Fan C 2 1 May be inoperative.


21-21-06 Near The Associated Glareshield Fan YES



Page 21-7

21-21-08 Nose Avionics Cooling Fan Repair Category Number Installed


Item Remarks Or Exceptions -21-08 Nose Avionics

Cooling Fan (Ref Des MN304) (Units -0001 thru -0500)






Page 21-8

21-30-01 Cabin Dump Function Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Cabin Dump

Function (Unpressurized)

C 1 0 (M) May be inoperative provided: a) One outflow valve is removed, and b) Cabin pressurization system is considered inoperative (Refer

to item 21-30-02).


21-30-01 Near The CABIN DUMP Switch Cover NO Maintenance (M)

Remove the Cabin Outflow Valve.

1. Remove the primary outflow valve or the secondary outflow valve. Refer to Primary Outflow Valve - Removal/Installation or Secondary Outflow Valve - Removal/Installation.

2. Make sure that protective caps or plugs are installed on open tubes and electrical connectors.



Page 21-9

21-30-02 Cabin Pressurization System Repair Category Number Installed


Item Remarks Or Exceptions -00A Cabin

Pressurization System (Unpressurized with cabin occupants) (Units -0001 thru -0500)

C 1 0 (O) May be inoperative provided: a) Baggage compartment remains empty (excluding ballast and/or

fly away kits), b) PRESSURIZATION NORM/MANUAL switch is selected to

MANUAL, c) CABIN DUMP is selected ON, d) ISO VLV CLOSE is selected ON, e) Aircraft is operated at 13,500 feet cabin altitude or below, and f) Flight crew oxygen system is used as required by 14 CFR.

NOTE: CABIN ALTITUDE amber message may appear at 8,500 feet cabin altitude. CABIN ALTITUDE red message may appear at 10,000 feet cabin altitude.

NOTE: Acceptable items for inclusion in fly away kit include: Engine Inlet and Exhaust Covers, Aircraft Tow Bar, Thrust Reverser, Stow Locks, Cargo Net, Jack Pad Adapters, Main Landing Gear Jacking Adapters, Nonflammable ballast material for aircraft balancing.

-00B Cabin Pressurization System (Unpressurized without cabin occupants) (Units -0001 thru -0500)

C 1 0 (O) May be inoperative provided: a) Baggage compartment remains empty (excluding ballast and/or

fly away kits), b) PRESSURIZATION NORM/MANUAL switch is selected to

MANUAL, c) CABIN DUMP is selected ON, d) ISO VLV CLOSE is selected ON, e) PASS OXY is selected OFF, f) No cabin occupants are carried, g) Aircraft is operated at FL250 or below, and h) Flight crew oxygen system is used as required by 14 CFR.

NOTE: CABIN ALTITUDE amber message may appear at 8,500 feet cabin altitude. CABIN ALTITUDE red message may appear at 10,000 feet cabin altitude.



21-30-02-00A 21-30-02-00B

Near The Environmental Control Panel YES

(Continued)



Page 21-10

Operations (O)

21-30-02--00A

1. Flight planning must consider the fuel burn and range associated with flight at lower altitudes.

2. Minimum enroute altitudes must be taken into account for the planned route.

3. Passengers must be briefed prior to each flight that cabin pressurization will be unavailable. Any medical complications or concerns must be considered in determination of the enroute altitude.

4. Portable or therapeutic oxygen may be used as needed for passenger comfort.

5. Cabin pressure must be monitored throughout the flight.

6. Ensure the following:

A. Baggage compartment remains empty (excluding ballast and/or fly away kits).

B. PRESSURIZATION NORM/MANUAL switch is selected to MANUAL.

C. CABIN DUMP is selected ON.

D. ISO VLV CLOSE is selected ON.

E. Aircraft is operated at 13,500 feet cabin altitude or below.

F. Flight crew oxygen system is used as required by 14 CFR.


21-30-02-00B

1. Flight planning must consider the fuel burn and range associated with flight at lower altitudes.

2. Minimum enroute altitudes must be taken into account for the planned route.

3. Cabin pressure must be monitored throughout the flight.


A. Baggage compartment remains empty (excluding ballast and/or fly away kits),

B. PRESSURIZATION NORM/MANUAL switch is selected to MANUAL,

C. CABIN DUMP is selected ON,

D. ISO VLV CLOSE is selected ON,

E. PASS OXY is selected OFF,

F. No cabin occupants are carried,

G. Aircraft is operated at FL250 or below, and

H. Flight crew oxygen system is used as required by 14 CFR.




Page 21-11

21-30-04 Baggage Compartment Pressurization System Repair Category Number Installed



Compartment Pressurization System (Excludes aft baggage door seal) (Units -0001 thru -0500)

C 1 0 May be missing or inoperative provided: a) ISO VLV CLOSE is selected ON, b) Aircraft is operated in accordance with AFM baggage

pressurization system limitations, and c) Aircraft is operated at FL410 or below.

NOTE: BAGGAGE ALTITUDE amber message may appear if baggage altitude exceeds 13,000 feet.


21-30-04 Near The ISOL VALVE Knob YES



Page 21-12

21-31-01 Cabin Pressurization Control Panel Repair Category Number Installed


Item Remarks Or Exceptions -01 Manual Altitude

Lever (CABIN ALT)

C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02).

-02 Manual Rate Selector (RATE)

C 1 0 May be inoperative or knob missing provided cabin pressurization system is considered inoperative (Refer to item 21-30-02).

-03 Altitude Selector ("A" Knob) (Units -0001 thru -0500)

C 1 0 May be inoperative or knob missing provided cabin pressurization system altitude select mode is considered inoperative (Refer to item 21-31-02-02).

-04 Cabin Pressurization Mode Switch (NORM/ALT SEL) (Units -0001 thru -0500)

C 1 0 May be inoperative provided non-selected mode is considered inoperative (Refer to item 21-31-02).

-05 Cabin/Aircraft Altitude Selector Gauge (Units -0001 thru -0500)

C 1 0 May be inoperative or knob missing provided cabin pressurization system altitude select mode is considered inoperative (Refer to item 21-31-02-02).

-06 Cabin/Aircraft Altitude Selector Gauge Lighting (Units -0001 thru -0500)

C 1 0 May be inoperative provided flight crew determines adequate natural or artificial lighting exists to read gauge.


21-31-01-01 thru

21-31-01-06




Page 21-13

21-31-02 Cabin Pressurization System Mode Repair Category Number Installed


Item Remarks Or Exceptions -01 Automatic

Schedule Mode (NORM) (Units -0001 thru -0500)

C 1 0 May be inoperative provided: a) Altitude select mode is operative, b) PRESSURIZATION NORM / ALT SEL switch is selected to

ALT SEL, c) Cabin differential pressure gauge/indication is operative, d) Cabin altitude gauge/indication is operative, e) Cabin vertical speed gauge/indication is operative, and f) Aircraft is operated at FL410 or below.

-02 Altitude Select Mode (ALT SEL) (Units -0001 thru -0500)

C 1 0 May be inoperative provided: a) Automatic schedule mode is operative, b) PRESSURIZATION NORM / ALT SEL switch is selected to

NORM, c) Cabin differential pressure gauge/indication is operative, d) Cabin altitude gauge/indication is operative, e) Cabin vertical speed gauge/indication is operative, and f) Aircraft is operated at FL410 or below.

-04 Any Mode (Excluding manual) (Units -0001 thru -0500)

C 2 0 May be inoperative provided: a) Autopilot system is operative, b) PRESSURIZATION NORM/MANUAL switch is selected to

MANUAL, and c) Aircraft is operated using manual pressurization.


21-31-02-01 21-31-02-02 21-31-02-04




Page 21-14

21-32-01 Cabin Altitude Gauge/Indication Repair Category Number Installed


Item Remarks Or Exceptions -00A Cabin Altitude

Gauge/Indication (Pressurized)

C 1 0 (O) May be inoperative provided: a) Cabin pressurization system automatic schedule mode is

operative and used, b) Cabin differential pressure gauge/indication is operative, and c) A chart is provided to convert differential pressure and aircraft

altitude to cabin altitude.

-00B Cabin Altitude Gauge/Indication (Unpressurized)


-01 Cabin Altitude Gauge/Indication (Gauge Lighting) (Units -0001 thru -0500)



21-32-01-00A 21-32-01-00B 21-32-01-01

Near The Associated Indication YES

Operations (O)

21-31-01-00A

1. Ensure there are no current logbook entries or deferrals related to the following:

• Cabin pressurization system automatic schedule mode

• Cabin differential pressure gauge/indication

2. Use the chart on the next page to convert differential pressure and aircraft altitude to cabin altitude.

(Continued)



Page 21-15



Page 21-16

21-32-02 Cabin Differential Pressure Gauge/Indication Repair Category Number Installed


Item Remarks Or Exceptions -00A Cabin Differential

Pressure Gauge/Indication (Pressurized)

C 1 0 (O) May be inoperative provided: a) Cabin pressurization system automatic schedule mode is

operative and used, b) Cabin altitude gauge/indication is operative, and c) A chart is provided to convert cabin and aircraft altitude to

differential pressure.

-00B Cabin Differential Pressure Gauge/Indication (Unpressurized)



21-32-02-00A 21-32-02-00B


Operations (O)

21-32-02-00A


• Cabin pressurization system automatic schedule mode

• Cabin altitude gauge/indication

2. Use the chart on previous page to convert cabin and aircraft altitude to differential pressure.



Page 21-17

21-32-03 Cabin Vertical Speed Gauge/Indication Repair Category Number Installed


Item Remarks Or Exceptions -00A Cabin Vertical

Speed Gauge/Indication (Pressurized)

C 1 0 May be inoperative provided: a) Cabin pressurization system automatic schedule mode is

operative and used, and b) Cabin altitude gauge/indication is operative.

-00B Cabin Vertical Speed Gauge/Indication (Unpressurized)


-01 Cabin Vertical Speed Gauge/Indication (Gauge Lighting) (Units -0001 thru -0500)



21-32-03-00A 21-32-03-00B 21-32-03-01




Page 21-18

21-33-01 Cabin Outflow Valve Repair Category Number Installed


Item Remarks Or Exceptions -33-01 Cabin Outflow

Valve C 2 0 (M) May be inoperative provided:

a) One outflow valve is removed, and b) Cabin pressurization system is considered inoperative (Refer

to item 21-30-02).


21-33-01 Near The Pressurization Controller NO Maintenance (M)

Remove the Cabin Outflow Valve.

1. Remove the primary outflow valve or the secondary outflow valve. Refer to Primary Outflow Valve - Removal/Installation or Secondary Outflow Valve - Removal/Installation.

2. Make sure that protective caps or plugs are installed on open tubes and electrical connectors.



Page 21-19

21-33-04 PAC Isolation Valve Repair Category Number Installed


Item Remarks Or Exceptions -33-04 PAC Isolation

Valve C 1 0 (O) May be inoperative provided:

a) Isolation valve is verified closed, b) Both PACs are operative, and c) APU bleed air system is operative.

NOTE: Cross bleed start is not available.


21-33-04 Near The ISOL VALVE Switch YES Operations (O)


• Either PAC

• APU bleed air system

2. Using AFM Normal Procedures, start the APU.

3. Position the APU BLEED AIR switch to ON.

4. Make sure the ISOL VALVE switch is in the CLSD position.

5. Place the CKPT PAC selector to ON.

6. Place one Cockpit Floor Vent valve to NORM.

7. Verify no airflow is present from the same valve.



Page 21-20

21-50-04 Pressurization Air Conditioning (PAC) System Repair Category Number Installed


Item Remarks Or Exceptions -00A Pressurization Air

Conditioning (PAC) System (Pressurized) (Units -0001 thru -0500)

C 2 1 One may be inoperative provided: a) Affected PAC is selected OFF, b) APU BLEED AIR is not selected to MAX COOL, and c) Aircraft is operated at FL410 or below.

-00B Pressurization Air Conditioning (PAC) System (Unpressurized)


-01A Pressurization Air Conditioning (PAC) System (Bi-Level Flow Control Valve)

C 2 1 (M) One may be inoperative provided: a) Affected valve is secured closed, and b) Aircraft is operated at FL410 or below.

-01B Pressurization Air Conditioning (PAC) System (Bi-Level Flow Control Valve) (Units -0001 thru -0500)

C 2 1 One may be inoperative provided: a) Associated ENG BLD AIR is selected OFF, b) ISOL VALVE is selected to CLSD, c) Opposite PAC is not selected to HIGH, d) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions, and e) Aircraft is operated at FL410 or below.


21-50-04-00A 21-50-04-00B 21-50-04-01B

Near The Pressurization Control Panel YES

21-50-04-01A Near The Pressurization Control Panel NO Maintenance (M)

21-50-04-01A

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Air Conditioning - General. For the supplier publication part number and manufacturer data, refer to the Introduction - Supplier Publication List.

Special Consumables

0.020 inch (0.51 mm) Thick Type 301, 1/2-Hard Stainless Steel.

Reference Material

Bi-Level Flow Control Valve - Removal/Installation.

(Continued)



Page 21-21

Setup

1. Fabricate a 0.020 inch (0.51 mm) thick blocking plate from Type 301, 1/2-hard stainless steel of the applicable diameter.

2. Disconnect the unserviceable bi-level flow control valve from the bleed air tube (upstream of the valve). Refer to Bi-Level Flow Control Valve - Removal/Installation.

3. Install a Blocking Plate on the Unserviceable Bi-Level Flow Control Valve (Refer to Figure 901).

NOTE: The blocking plate installation on the left and the right bi-level flow control valves is typical.

A. Install the blocking plate on the unserviceable bi-level flow control valve, between the valve and the bleed air tube.

B. Connect the unserviceable bi-level flow control valve to the bleed air tube. Refer to Bi-Level Flow Control Valve - Removal/Installation.



Page 21-22

21-60-01 Cockpit and Cabin Temperature Control System Repair Category Number Installed


Item Remarks Or Exceptions -60-01 Cockpit and

Cabin Temperature Control System (Amber TEMP FAULT CKT-CAB)


-01 Cockpit and Cabin Temperature Control System (Automatic Mode) (Units -0001 thru -0500)

C 2 0 May be inoperative provided: a) Associated temperature control system manual mode is used,

and b) APU BLEED AIR is not selected to MAX COOL.

-02 Cockpit and Cabin Temperature Control System (Manual Mode)

C 2 0 May be inoperative provided associated temperature control system automatic mode is used.


21-60-01 21-60-01-01 21-60-01-02

Near The Pressurization Control Panel YES



Page 21-23

21-61-01 Cabin Temperature Remote Control Repair Category Number Installed


Item Remarks Or Exceptions -61-01 Cabin

Temperature Remote Control (Units -0001 thru -0500)

D 1 0 May be inoperative provided CABIN TEMP CTL is selected to NRM.


21-61-01 Near The Pressurization Control Panel YES



Page 21-24

21-61-02 Temperature Control Panel Repair Category Number Installed


Item Remarks Or Exceptions -61-02 Temperature

Control Panel (Units -0001 thru -0500)

C 1 0 May be inoperative provided cockpit and cabin temperature control system automatic modes are considered inoperative (Refer to item 21-60-01-01).

-01 Temperature Control Panel (Temperature Selector)

C 2 1 One may be inoperative or knob missing provided affected temperature control system (automatic and manual) is considered inoperative (Refer to item 21-60-01).

-02 Temperature Control Panel (Temperature Display Selector)

C 1 0 May be inoperative or knob missing provided all temperature indication systems are considered inoperative (Refer to item 21-62-01).

-03 Temperature Control Panel (Temperature Display)

C 1 0 May be inoperative provided all temperature indication systems are considered inoperative (Refer to item 21-62-01).


21-61-02 thru

21-61-02-03

Near The Temperature Control Panel YES



Page 21-25

21-62-01 Temperature Indication System Repair Category Number Installed


Item Remarks Or Exceptions -01 Temperature

Indication System (Cabin) (Units -0001 thru -0500)


-02 Temperature Indication System (Cockpit)


-03 Temperature Indication System (Supply Duct)

C 2 1 One may be inoperative provided: a) Associated air temperature control system automatic mode is

considered inoperative (Refer to item 21-60-01-01), and b) Associated DUCT O'TEMP amber message is monitored

during temperature adjustment.


21-62-01-01 21-62-01-02 21-62-01-03

Near The Temperature Indication System YES



Page 21-26

21-70-01 Water Separator Repair Category Number Installed


Item Remarks Or Exceptions -70-01 Water Separator C 2 1 May be inoperative provided affected PAC is considered

inoperative (Refer to item 21-50-04).





Page 22-1

Chapter 22 Autoflight Page Number

22-10-01 Autopilot Disconnect Button (AP/TRIM/NWS DISC) (Failed deselected)................................. 22-2

22-10-02 Autopilot Interrupt/Flight Director Sync Button ......................................................................... 22-3

22-10-03 Autopilot System (Units -0001 thru -0500) ............................................................................... 22-4

22-10-04 Takeoff/Go-Around Button (GA) ............................................................................................... 22-5

22-10-05 Yaw Damper ............................................................................................................................. 22-6

22-13-03 Flight Guidance Controller Annunciator (Failed to illuminate) (GC-810) .................................. 22-7

22-13-04 Flight Guidance Controller Function Control (GC-810) ............................................................ 22-9

22-13-05 Pedestal Autopilot Pitch Wheel (Units -0001 thru -0500) ....................................................... 22-11

22-20-01 Mach Trim System .................................................................................................................. 22-12

ATA 22 – Auto Flight


Page 22-2

22-10-01 Autopilot Disconnect Button (AP/TRIM/NWS DISC) (Failed deselected) Repair Category Number Installed


Item Remarks Or Exceptions -00A Autopilot Disconnect

Button (Left Control Wheel)

C 1 0 (O) May be inoperative provided: a) Right control wheel button is operative, b) Alternate procedures for disconnecting nose wheel steering

during ground operations are established and used, c) A pilot remains seated in right seat with seat belt fastened

during all autopilot operations, d) Autopilot system is not used below AFM cruise minimum

use height, and e) Approach minimums do not require use of autopilot system.

-00B Autopilot Disconnect Button (Right Control Wheel)

C 1 0 May be inoperative provided: a) Left control wheel button is operative, b) A pilot remains seated in left seat with seat belt fastened

during all autopilot operations, c) Autopilot system is not used below AFM cruise minimum

use height, and d) Approach minimums do not require use of autopilot system.


22-10-01-00A 22-10-01-00B

Near FGC Controller YES

Operations (O)

22-10-01-00A

1. Ensure there are no current logbook entries or deferrals related to the Right control wheel button.

2. The flight crew must brief that during all aircraft ground movements (including takeoff and landing), the copilot will have control of the AP/TRIM/NWS DISC function so that, in the event of a system malfunction, the copilot will activate the disconnect and the pilot will maintain directional control of the aircraft using a combination of tiller wheel steering, differential braking and thrust.


A. Autopilot system is not used below AFM cruise minimum use height

B. Approach minimums do not require use of autopilot system



Page 22-3

22-10-02 Autopilot Interrupt/Flight Director Sync Button Repair Category Number Installed


Item Remarks Or Exceptions -10-02 Autopilot

Interrupt/Flight Director Sync Button (TCS) (Units -0001 thru -0500)



22-10-02 Near FGC Controller YES



Page 22-4

22-10-03 Autopilot System (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -00A Autopilot System

(Single channel failed) (Units -0001 thru -0500)

C 2 1 One may be inoperative provided operative autopilot channel is selected.

-00B Autopilot System (Both channels failed) (Units -0001 thru -0500)

B 2 0 (M) May be inoperative provided: a) Autopilot system is deactivated, b) Enroute procedures and approach minimums do not require

use of autopilot system, c) Cabin pressurization system is not operated in manual

mode, and d) Aircraft is not operated RVSM.

NOTE: A PRIMARY STAB TRIM FAIL may result if autopilot system is deactivated before flight guidance system self test is completed.

RVSM Operations Not Authorized


22-10-03-00A 22-10-03-00B


Maintenance (M)

22-10-03-00B

Pull and secure the AP A (HF043) and AP B (HF062) circuit breaker on the copilot’s circuit breaker panel.



Page 22-5

22-10-04 Takeoff/Go-Around Button (GA) Repair Category Number Installed


Item Remarks Or Exceptions -00A Takeoff/Go-Around

Button (GA) (Single button failed)

C 2 1 One may be inoperative.

-00B Takeoff/Go-Around Button (GA) (Both buttons failed)

C 2 0 May be inoperative provided: a) Flight director is not used during takeoff or go-around, b) Autopilot system is disconnected for go-around, and c) Autopilot interrupt/flight director sync button is operative on

pilot flying side.

NOTE: FMS missed approach procedure must be manually advanced.


22-10-04-00A 22-10-04-00B




Page 22-6

22-10-05 Yaw Damper Repair Category Number Installed


Item Remarks Or Exceptions -10-05 Yaw Damper

(Lower Rudder) (Units -0001 thru -0500) (Cyan YD FAIL LOWER A or B message)

B 2 1 One may be inoperative provided aircraft is operated in accordance with AFM YD FAIL LOWER A or B cyan message procedure.





Page 22-7

22-13-03 Flight Guidance Controller Annunciator (Failed to illuminate) (GC-810) Repair Category Number Installed


Item Remarks Or Exceptions -01 Flight Guidance

Controller Annunciator (Altitude) (ALT button)

C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box.

-03 Flight Guidance Controller Annunciator (Approach) (APP button) (Units -0001 thru -0500)


-04 Flight Guidance Controller Annunciator (Autopilot) (AP button - A or B annunciation) (Units -0001 thru -0500)

C 2 0 May be inoperative provided AP annunciation appears in PFD flight director mode box.

-05 Flight Guidance Controller Annunciator (Back Course) (BC button) (Units -0001 thru -0500)


-06 Flight Guidance Controller Annunciator (IAS/Mach Change-over) (C/O button) (Units -0001 thru -0500)

D 1 0 May be inoperative.

-07 Flight Guidance Controller Annunciator (Coupled Side) (PFD SEL Button - left or right arrow) (Units -0001 thru -0500)

C 2 0 May be inoperative provided associated green coupled arrow appears in PFD flight director mode box.

(Continued)



Page 22-8

22-13-03 Flight Guidance Controller Annunciator (Failed to illuminate) (GC-810) (Continued)

Repair Category Number Installed



Controller Annunciator (Flight Level Change) (FLC button)


-10 Flight Guidance Controller Annunciator (Half Bank) (BANK button)

C 1 0 May be inoperative provided green bank limit arc appears on PFD attitude display.

-11 Flight Guidance Controller Annunciator (Heading) (HDG button)


-12 Flight Guidance Controller Annunciator (Navigation) (NAV button)


-13 Flight Guidance Controller Annunciator (Vertical Navigation) (VNAV button)


-14 Flight Guidance Controller Annunciator (Vertical Speed) (VS button)


-15 Flight Guidance Controller Annunciator (Yaw Damper) (YD button - A or B annunciation) (Units -0001 thru -0500)

B 2 0 May be inoperative provided yaw damper is considered inoperative (Refer to item 22-10-05).


22-13-03-01 thru

22-13-03-15




Page 22-9

22-13-04 Flight Guidance Controller Function Control (GC-810) Repair Category Number Installed



Controller Function Control (Altitude) (ALT button)

B 1 0 May be inoperative provided: a) Procedures do not require its use, and b) Aircraft is not operated RVSM.


-02 Flight Guidance Controller Function Control (Approach) (APR button) (Units -0001 thru -0500)

B 1 0 May be inoperative provided procedures do not require its use.

-03 Flight Guidance Controller Function Control (Autopilot) (AP button)

B 1 0 May be inoperative provided autopilot system is considered inoperative (Refer to item 22-10-03).


-04 Flight Guidance Controller Function Control (Back Course) (BC button) (Units -0001 thru -0500)

C 1 0 May be inoperative provided procedures do not require its use.

-05 Flight Guidance Controller Function Control (IAS/Mach Change-over) (C/O Button) (Units -0001 thru -0500)


-06 Flight Guidance Controller Function Control (Coupled Side) (PFD SEL button) (Units -0001 thru -0500)

C 1 0 May be inoperative provided arrow points to pilot flying side.

(Continued)



Page 22-10

22-13-04 Flight Guidance Controller Function Control (GC-810) (Continued) Repair Category Number Installed



Controller Function Control (Flight Level Change) (FLC button)


-11 Flight Guidance Controller Function Control (Half Bank) (BANK Button)


-14 Flight Guidance Controller Function Control (Navigation) (NAV Button)

B 1 0 May be inoperative provided procedures do not require its use.

-15 Flight Guidance Controller Function Control (Pitch Wheel) (Units -0001 thru -0500)

C 1 0 (O) May be inoperative provided pedestal pitch wheel is verified operative.

-16 Flight Guidance Controller Function Control (Vertical Navigation) (VNAV button)


-17 Flight Guidance Controller Function Control (Vertical Speed) (VS button)



22-13-04-01 thru

22-13-04-17

Near The Flight Guidance Controller Annunciator

YES

Operations (O)

22-13-04-15

Make sure the flight director pitch can be adjusted when in an appropriate mode, such as PITCH or V/S using the pitch wheel on the pedestal.



Page 22-11

22-13-05 Pedestal Autopilot Pitch Wheel (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -13-05 Pedestal Autopilot

Pitch Wheel (Units -0001 thru -0500)

C 1 0 (O) May be inoperative provided flight guidance panel pitch wheel is verified operative.


22-13-05 Near FGC Controller YES Operations (O)

Make sure the flight director pitch can be adjusted when in an appropriate mode, such as PITCH or V/S using the pitch wheel on the flight guidance panel.



Page 22-12

22-20-01 Mach Trim System Repair Category Number Installed


Item Remarks Or Exceptions -20-01 Mach Trim System

(Units -0001 thru -0500) (Amber MACH TRIM OFF message)

C 1 0 May be inoperative provided aircraft is operated in accordance with AFM MACH TRIM OFF amber message procedure.





Page 23-1

Chapter 23 Communications Page Number

23-00-01 Flight Phone / SATCOM System .............................................................................................. 23-2

23-10-01 High Frequency (HF) Communication System ......................................................................... 23-3

23-12-01 Very High Frequency (VHF) Communication System .............................................................. 23-4

23-20-01 Satellite Datalink Service .......................................................................................................... 23-5

23-20-03 Selective Call (SELCAL) (System or individual channel) ......................................................... 23-6

23-40-01 Automatic Cabin Briefer ............................................................................................................ 23-7

23-40-02 Crewmember Interphone System (Flight deck to ground) ........................................................ 23-8

23-40-03 Passenger Address (PA) System ............................................................................................. 23-9

23-40-04 Passenger Seat Belt / Safety Chime ...................................................................................... 23-10

23-50-03 Cockpit Overhead Communication Speaker .......................................................................... 23-11

23-50-04 Cockpit Hand Microphone ...................................................................................................... 23-12

23-50-05 Cockpit Headset and Boom Microphone ................................................................................ 23-13

23-50-06 Cockpit Headset Audio System .............................................................................................. 23-14

23-50-07 Push-to-talk (PTT) Switch (Failed deselected) ....................................................................... 23-15

23-50-08 Radio Management Unit (RMU) ............................................................................................. 23-16

23-60-01 Static Wick .............................................................................................................................. 23-17

23-70-01 Cockpit Voice Recorder (CVR) (Cyan CVR FAIL message) .................................................. 23-18

ATA 23 – Communications


Page 23-2

23-00-01 Flight Phone / SATCOM System Repair Category Number Installed


Item Remarks Or Exceptions -00-01 Flight Phone /

SATCOM System D 1 0 May be inoperative provided procedures do not require its use.

-01 Flight Phone / SATCOM System (Cockpit Handset)

D 1 0 May be inoperative provided procedures do not require its use.

-02 Flight Phone / SATCOM System (Cabin Handset)



23-00-01 23-00-01-02 23-00-01-03

Near The Associated Handset YES



Page 23-3

23-10-01 High Frequency (HF) Communication System Repair Category Number Installed


Item Remarks Or Exceptions -00A High Frequency

(HF) Communication System (Dual LRCS not required)

D 1 0 May be inoperative unless the route of flight requires the use of HF radios.


23-10-01-00A Near The HF Controller YES



Page 23-4

23-12-01 Very High Frequency (VHF) Communication System Repair Category Number Installed


Item Remarks Or Exceptions -12-01 Very High

Frequency (VHF) Communication System

D 2 1 May be inoperative provided: a) Affected system is not on an emergency bus, and b) Procedures do not require its use.

NOTE 1: Number 2 required for Extended overwater or IFR operations.

NOTE 2: Number 1 VHF must be operative due to powered by emergency bus.


23-12-01 Near The COMM Panel YES



Page 23-5

23-20-01 Satellite Datalink Service Repair Category Number Installed


Item Remarks Or Exceptions -01 Satellite Datalink

Service (Radio)


-02A Satellite Datalink Service (Weather)


NOTE: Any function(s) that operate normally may be used.

-02B Satellite Datalink Service (Weather)

C 1 0 (O) May be inoperative provided alternate procedures are established and used.

-03 Satellite Datalink Service (Internet)



23-20-01-01 thru

23-20-01-03

Near The MFD YES

Operations (O)

23-20-01-02B

Crew shall use other available means to obtain weather information such as HIWAS or FLIGHTWATCH as well as radar.



Page 23-6

23-20-03 Selective Call (SELCAL) (System or individual channel) Repair Category Number Installed


Item Remarks Or Exceptions -00B Selective Call

(SELCAL) (System or individual channel) (SELCAL required)



23-20-03-00B Near The SELCAL Panel YES Operations (O)

1. Flight crew must advise ATC of inoperative SELCAL, as appropriate.

2. Flight crew will monitor the appropriate radios at all times in the absence of SELCAL. Consideration should be given to the effect of increased fatigue due to this requirement and the possibility of having only one crew member monitor the radios via headset (especially HF) if required for the given flight.



Page 23-7

23-40-01 Automatic Cabin Briefer Repair Category Number Installed


Item Remarks Or Exceptions -40-01 Automatic Cabin

Briefer D 1 0


23-40-01 Near the Cabin Briefer YES



Page 23-8

23-40-02 Crewmember Interphone System (Flight deck to ground) Repair Category Number Installed


Item Remarks Or Exceptions -40-02 Crewmember

Interphone System (Flight deck to ground)


-01 Nose Wheel Well Headset Jack


-02 Tailcone Headset Jack



23-40-02 23-40-02-01 23-40-02-02

Near Both Audio Panels YES



Page 23-9

23-40-03 Passenger Address (PA) System Repair Category Number Installed


Item Remarks Or Exceptions -40-03 Passenger Address

(PA) System D 1 0 May be inoperative.


23-40-03 Near The PA Switch YES



Page 23-10

23-40-04 Passenger Seat Belt / Safety Chime Repair Category Number Installed


Item Remarks Or Exceptions -40-04 Passenger Seat Belt

/ Safety Chime C 1 0 (O) May be inoperative provided:

a) Passenger address system is operative, and b) Cabin occupants are briefed by alternate means.


23-40-04 Near The SEAT BELT LTS / PASS SAFETY Switch

YES

Operations (O)

1. Ensure there are no current logbook entries or deferrals related to the Passenger address system.

2. A crew member must use the PA system from the cockpit to make the appropriate announcements.



Page 23-11

23-50-03 Cockpit Overhead Communication Speaker Repair Category Number Installed


Item Remarks Or Exceptions -50-03 Cockpit Overhead

Communication Speaker

C 2 1 One may be inoperative provided: a) Affected speaker is not required for procedures, and b) A headset is used for associated inoperative speaker.


23-50-03 Near The Affected Speaker YES



Page 23-12

23-50-04 Cockpit Hand Microphone Repair Category Number Installed


Item Remarks Or Exceptions -00B Cockpit Hand

Microphone C 2 0 May be inoperative provided associated boom microphone is

operative.

-01 Cockpit Hand Microphone (Jack)

C 2 0 May be inoperative provided associated hand microphone is considered inoperative (Refer to item 23-50-04).

-02 Cockpit Hand Microphone (Holder)

D 2 0 (O) May be inoperative provided associated hand microphone is secured by alternate means.


23-50-04-00B 23-50-04-01 23-50-04-02

Near The Affected Hand Microphone YES

Operations (O)

23-50-04-02

Prior to flight, a crew member must ensure that the hand micro phone is secured in a manner that will not interfere with aircraft operations. One method is to utilize adhesive hook and loop (Velcro) strips on the pedestal.



Page 23-13

23-50-05 Cockpit Headset and Boom Microphone Repair Category Number Installed


Item Remarks Or Exceptions -01A Boom Microphone

(For a holder of an Air Carrier or Commercial Operator Certificate)

A 2 0 May be inoperative provided: a) Associated hand microphone is installed and operative, and b) Repairs are made within three flight days.

-02 Headset Earphones / Headphones

C 2 1 May be inoperative provided associated cockpit overhead communication speaker is operative.

-03 Active Noise Reduction (ANR) Function

D 2 0 May be inoperative provided normal audio function of headset is operative.

-04 Powered Headset System (Units -0001 thru -0500)

D 2 0 May be inoperative provided non-powered headset jack is operative or headset is not used.


23-50-05-01A thru

23-50-05-04

Near The Associated Audio Panel YES



Page 23-14

23-50-06 Cockpit Headset Audio System Repair Category Number Installed


Item Remarks Or Exceptions -50-06 Cockpit Headset

Audio System C 2 0 May be inoperative provided:

a) Both cockpit overhead communication speakers are used, and

b) Headset audio system is not required by 14 CFR or procedures.


23-50-06 Near The Captains Instrument Panel YES



Page 23-15

23-50-07 Push-to-talk (PTT) Switch (Failed deselected) Repair Category Number Installed


Item Remarks Or Exceptions -01 Push-to-talk (PTT)

Switch (Failed deselected) (Yoke Switch)

B 2 1 (O) One may be inoperative provided alternate procedures are established and used for transmitting.

-03 Remote Pedestal Switch (Units -0001 thru -0500)

C 1 0


23-50-07-01 Near The Associated RMU YES

23-50-07-03 Adjacent to the Switch YES Operations (O)

Prior to flight, the crew member with the operative switch will be assigned all radio transmissions.



Page 23-16

23-50-08 Radio Management Unit (RMU) Repair Category Number Installed


Item Remarks Or Exceptions -50-08 Radio Management

Unit (RMU) (Units -0001 thru -0500)

C 2 1 (O) One may be inoperative provided: a) Standby radio control unit is verified operative, and b) COM 1 is verified operative.


23-50-08 Near The Associated RMU YES Operations (O)

1. Prior to each flight the flight crew shall discuss the new radio tuning procedures using only the standby radio control unit and the operative RMU.

2. Prior to each flight, a crew member shall check for proper transmission and reception using the standby radio control unit and RMU by tuning in at least one COM channel and one navigation aid.



Page 23-17

23-60-01 Static Wick Repair Category Number Installed


Item Remarks Or Exceptions -60-01 Static Wick NOTE: May include mounting base provided no damage

exists to attaching structure.

-03 Winglet (Each side) (Units -0001 thru -0500)

C 2 1 One may be damaged or missing provided outermost wick is installed and not damaged.

-04 Wing Trailing Edge (Each side)

C 2 1 One may be damaged or missing provided outermost wick is installed and not damaged.

NOTE: Wing trailing edge is area between aileron and wing tip assembly.

-05 Elevator (Each side)

C 3 1 Two may be damaged or missing provided outermost wick is installed and not damaged.

-06 Horizontal Stabilizer Trailing Edge (Each side)

- 1 1 NOTE: This static wick is required. Relief should not be taken under another installation area.


23-60-01 thru

23-60-01-06

Near The Captains Instrument Panel YES



Page 23-18

23-70-01 Cockpit Voice Recorder (CVR) (Cyan CVR FAIL message) Repair Category Number Installed


Item Remarks Or Exceptions -00A Cockpit Voice

Recorder (CVR) (Cyan CVR FAIL message) (Holder of an Air Carrier or Commercial Operator Certificate)

A 1 0 May be inoperative provided: a) Any Flight Data Recorder (FDR) required to be installed is

operative, and b) Repairs are made within three flight days.

NOTE: FDR not installed.

-02 Underwater Locator Device (ULD)

D 1 0 May be inoperative provided device is not required by 14 CFR.

NOTE: ULD not required for 14 CFR part 135 operations.

-03A Datalink Recording C 1 0 May be inoperative provided CPDLC operations are not conducted..


23-70-01-00A 23-70-01-02

23-70-01-03A

Near The CVR Panel YES



Page 24-1

Chapter 24 Electrical Power Page Number

24-20-01 Engine AC Generating System ................................................................................................. 24-2

24-30-01 APU DC Generating System .................................................................................................... 24-3

24-37-01 APU DC Amperage Gauge/Indication ...................................................................................... 24-4

24-37-02 APU DC Voltage Gauge/Indication ........................................................................................... 24-5

24-40-01 External Power System ............................................................................................................ 24-6

24-50-01 AC Cockpit Outlet ..................................................................................................................... 24-7

24-60-01 DC Cockpit Outlet ..................................................................................................................... 24-8

24-60-02 Ground Dispatch Power System............................................................................................... 24-9

24-60-03 Interior Disconnect .................................................................................................................. 24-10

ATA 24 – Electrical Power


Page 24-2

24-20-01 Engine AC Generating System Repair Category Number Installed


Item Remarks Or Exceptions -20-01 Engine AC

Generating System C 2 1 One may be inoperative provided affected windshield electric

anti-ice system is considered inoperative (Refer to item 30-40-02).


24-20-01 Near The AC Power Switch YES



Page 24-3

24-30-01 APU DC Generating System Repair Category Number Installed


Item Remarks Or Exceptions -30-01 APU DC Generating

System (Units -0001 thru -0500)

C 1 0 May be inoperative provided APU SYSTEM GENERATOR is selected OFF.

NOTE: APU GEN OFF cyan message may appear.


24-30-01 Near The GENERATOR Switch YES



Page 24-4

24-37-01 APU DC Amperage Gauge/Indication Repair Category Number Installed


Item Remarks Or Exceptions -37-01 APU DC Amperage

Gauge/Indication (Units -0001 thru -0500)

C 1 0 May be inoperative provided APU SYSTEM GENERATOR is selected OFF.

NOTE: APU GEN OFF cyan message may appear.


24-37-01 Near The APU DC Amperage Gauge/Indication

YES



Page 24-5

24-37-02 APU DC Voltage Gauge/Indication Repair Category Number Installed


Item Remarks Or Exceptions -37-02 APU DC Voltage

Gauge/Indication C 1 0 May be inoperative.


24-37-02 Near The APU DC Voltage Gauge/Indication YES



Page 24-6

24-40-01 External Power System Repair Category Number Installed


Item Remarks Or Exceptions -40-01 External Power

System D 1 0 May be inoperative.





Page 24-7

24-50-01 AC Cockpit Outlet Repair Category Number Installed


Item Remarks Or Exceptions -50-01 AC Cockpit Outlet D 2 0 May be inoperative provided procedures do not require its use.


24-50-01 Near The Associated Outlet YES



Page 24-8

24-60-01 DC Cockpit Outlet Repair Category Number Installed


Item Remarks Or Exceptions -60-01 DC Cockpit Outlet D 2 0 May be inoperative provided procedures do not require its use.


24-60-01 Near The DC Cockpit Outlet YES



Page 24-9

24-60-02 Ground Dispatch Power System Repair Category Number Installed


Item Remarks Or Exceptions -60-02 Ground Dispatch

Power System C 1 0 May be inoperative.





Page 24-10

24-60-03 Interior Disconnect Repair Category Number Installed


Item Remarks Or Exceptions -60-03 Interior Disconnect C 1 0 (M)(O) May be inoperative provided:

a) Interior power system is deactivated, b) Cabin emergency lighting is verified operative, and c) Passengers are briefed on disabled cabin electrical

systems or are not carried.

NOTE: Items powered by interior bus are considered inoperative. This includes, but is not limited to: Cabin interior lighting, cabin window shade system, galley appliances, galley drain, vanity drain, forward equipment fan, aft equipment fan, cabin AC inverter, and cabin entertainment system.


24-60-03 Near The Captains Instrument Panel NO Maintenance (M)

Interior Disconnect (INTERIOR Switch/Light) Inoperative

Tools and Equipment

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Electrical Power - General. For the supplier publication part number and manufacturer data, refer to the Introduction - Supplier Publication List.

Special Consumables

• Protective Caps or Covers.

Reference Material

• Chapter 6, Airplane Dimensions and Areas - Description and Operation

• Chapter 6, Access Plates and Panels Identification - Description and Operation

• Battery - Maintenance Practices

• External Electrical Power - Maintenance Practices.

Setup

1. Remove the electrical power from the airplane. Refer to Chapter 24, External Electrical Power - Maintenance Practices.

2. Disconnect the battery. Refer to Battery - Maintenance Practices.

3. Open the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

4. Remove aft baggage compartment panel 312ATC to get access to the DC power junction box (JBox).

(Continued)



Page 24-11

5. Refer to Chapter 6, Access Plates and Panels Identification - Description and Operation.

6. Remove the left and the right J-Box covers to get access to the left and the right interior power fuse limiters (HZ167 left, HZ268 right).

Disconnect Interior Electrical Power at the J-Box (Refer to Figure 901).

1. Remove the nuts, lock washers, washers, and electrical terminals from the left (HZ167) and the right (HZ268) fuse limiter studs.

2. Put protective caps or covers on the electrical terminals.

3. Stow the electrical wires away from other J-Box electrical components.

4. Install the washers, lock washers, and nuts on the left (HZ167) and the right (HZ268) fuse limiter studs.

Closeout

1. Install the left and the right J-Box covers to the J-Box.

2. Install aft baggage compartment panel 312ATC. Refer to Chapter 6, Access Plates and Panels Identification - Description and Operation.

3. Close the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

4. Connect the battery. Refer to Battery - Maintenance Practices.

(Continued)



Page 24-12

Operations (O)

1. With both batteries off and no generators running, select EMER LTS to ON.

2. Quickly verify the EXIT signs and the dropped aisle lighting near the main cabin door are operative.

3. Select EMER LTS to OFF.

4. Ensure passengers are briefed on disabled cabin electrical systems.



Page 25-1

Chapter 25 Equipment / Furnishings Page Number

25-00-01 Required Documents Holder (Airworthiness Certificate, Registration, etc ............................... 25-2

25-10-01 Cockpit Assist Handle ............................................................................................................... 25-3

25-10-03 Cockpit Sunvisor System (Including attach mechanism) ......................................................... 25-4

25-10-05 Flight Crew Seat (Per seat) ...................................................................................................... 25-5

25-10-07 Headset Hook ........................................................................................................................... 25-7

25-10-08 Eye Reference Ball ................................................................................................................... 25-8

25-10-09 Yoke-mounted Chart Holder ..................................................................................................... 25-9

25-20-04 Electric Cabin Window Shade (Individual shades or entire system) ...................................... 25-10

25-20-05 Non-essential Equipment and Furnishings (NEF) .................................................................. 25-11

25-20-06 Passenger Seat (Including side-facing seats, folding seats and couches) (Per seat) .......... 25-12

25-30-01 Refreshment Center Hot Liquid Storage System Heater ....................................................... 25-14

25-40-01 Exterior Lavatory Door Ashtray ............................................................................................... 25-15

25-50-01 Baggage Restraint System ..................................................................................................... 25-16

25-50-02 Cabin Storage Compartment .................................................................................................. 25-18

25-60-03 Emergency Medical Equipment .............................................................................................. 25-19

25-61-01 Life Preserver (Crew and passenger) ..................................................................................... 25-20

25-62-01 Emergency Locator Transmitter (ELT) ................................................................................... 25-21

25-64-01 Life Raft ................................................................................................................................... 25-22

ATA 25 – Equipment and Furnishings


Page 25-2

25-00-01 Required Documents Holder (Airworthiness Certificate, Registration, etc Repair Category Number Installed


Item Remarks Or Exceptions -00-01 Required

Documents Holder (Airworthiness Certificate, Registration, etc)

D 1 0 (O) May be inoperative or missing provided an alternate means of securing and displaying documents is used.


25-00-01 Near The Holder YES Operations (O)

Place the required documents in a clear plastic bag and display them in a manner that is visible to the appropriate authorities, crew members and passengers.



Page 25-3

25-10-01 Cockpit Assist Handle Repair Category Number Installed


Item Remarks Or Exceptions -10-01 Cockpit Assist

Handle D 1 0 May be inoperative.


25-10-01 Near The Cockpit Assist Handle YES



Page 25-4

25-10-03 Cockpit Sunvisor System (Including attach mechanism) Repair Category Number Installed


Item Remarks Or Exceptions -10-03 Cockpit Sunvisor

System (Including attach mechanism)

D 2 0 May be missing, or inoperative provided crewmember's field of vision is not obstructed.


25-10-03 Near The Associated Instrument Panel YES



Page 25-5

25-10-05 Flight Crew Seat (Per seat) Repair Category Number Installed


Item Remarks Or Exceptions -01A Flight Crew Seat

(Armrest) C 2 0 May be inoperative provided affected armrest is stowed in

retracted position.

-01B Flight Crew Seat (Armrest)

C 2 0 (M) May be missing, or inoperative provided affected armrest is removed.

-02 Flight Crew Seat (Lumbar Support


-03 Flight Crew Seat (Recline/Tilt Function)

C 1 0 (M)(O) May be inoperative provided: a) Affected seat is secured or failed in a position that permits

normal visibility, b) Full flight control movement is available, and c) Crewmember can reach all necessary controls and

equipment while restrained.

-04 Flight Crew Seat (Restraint Buckle Protective Padding)

D 1 0 May be damaged or missing.

-05 Flight Crew Seat (Thigh Support)

D 1 0 May be inoperative provided full flight control movement is available.

-06 Flight Crew Seat (Vertical Adjustment)

C 1 0 (M)(O) May be inoperative provided: a) Affected seat is secured or failed in a position that permits

normal visibility, b) Full flight control movement is available, and c) Crewmember can reach all necessary controls and

equipment while restrained.


25-10-05-01A 25-10-05-02 25-10-05-04 25-10-05-05

Near The Associated Instrument Panel YES

25-10-05-01B 25-10-05-03 25-10-05-06

Near The Associated Instrument Panel NO

Maintenance (M)

25-10-05-01B, 25-10-05-03, 25-10-05-06

Secure the flight crew seat in an acceptable position. Refer to the Model 750 Interior Maintenance Manual and Illustrated Parts Catalog.

NOTE: The Model 750 Interior Maintenance Manual and Illustrated Parts Catalog contains additional supplier data about the flight crew seats, including the supplier publication.

(Continued)



Page 25-6

Operations (O)

25-10-05-03, 25-10-05-05

1. Prior to flight, a crew member shall occupy the affected seat and fasten the restraining system.

2. Make sure full flight control movement and brake application are available.

3. Make sure all necessary controls and equipment can be reached.



Page 25-7

25-10-07 Headset Hook Repair Category Number Installed


Item Remarks Or Exceptions -10-07 Headset Hook D 2 0 May be inoperative.


25-10-07 Near The Associated Headset Hook YES



Page 25-8

25-10-08 Eye Reference Ball Repair Category Number Installed


Item Remarks Or Exceptions -10-08 Eye Reference Ball C 3 0 (O) May be inoperative or missing provided alternate

procedures are established and used for eye position reference.


25-10-08 Near The Locator YES Operations (O)

1. Prior to flight, a crew member shall occupy the affected seat and fasten the restraining system to ensure the following conditions are met:

A. Make sure full flight control movement and brake application.

B. Make sure access to all necessary controls and equipment.

2. Position the affected seat(s) so the pilot align the eyeball locator bracket so that the following sight picture with the bracket is achieved:

A. Eyeball locator base is flat.

B. The flange opposite to the affected seat is aligned for a straight edge.



Page 25-9

25-10-09 Yoke-mounted Chart Holder Repair Category Number Installed


Item Remarks Or Exceptions -10-09 Yoke-mounted Chart

Holder D 2 0 May be inoperative.

-01 Yoke-mounted Chart Holder (Light)



25-10-09 25-10-09-01

Near The Chart Holder YES



Page 25-10

25-20-04 Electric Cabin Window Shade (Individual shades or entire system) Repair Category Number Installed


Item Remarks Or Exceptions -20-04 Electric Cabin

Window Shade (Individual shades or entire system)

D 12 0 May be inoperative provided affected window shades are failed open or in a position that does not interfere with emergency procedures.





Page 25-11

25-20-05 Non-essential Equipment and Furnishings (NEF) Repair Category Number Installed


Item Remarks Or Exceptions -20-05 Non-essential

Equipment and Furnishings (NEF)

- - 0 item(s) is deferred in accordance with the operator’s NEF deferral program. The NEF program, procedures and processes are outlined in the operators NEF Program Manual. (M) and (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document.

NOTE: Exterior lavatory door ashtray is not considered an NEF item.


25-20-05 N/A YES



Page 25-12

25-20-06 Passenger Seat (Including side-facing seats, folding seats and couches) (Per seat)



Item Remarks Or Exceptions -20-06 Passenger Seat

(Including side-facing seats, folding seats and couches) (Per seat)

D 9 0 May be inoperative provided: a) Seat does not block an emergency exit, b) Seat does not restrict any cabin occupant access to aisle,

and c) Affected seat(s) are blocked and placarded “DO NOT

OCCUPY”.

NOTE: Affected seat(s) may include seats near inoperative seat(s).

-01 Armrest D 16 0 May be missing, or inoperative with seat occupied provided: a) Armrest does not block an emergency exit, and b) Armrest does not restrict any cabin occupant from access

to aisle.

-02A Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking, swivel, and other positioning controls)

D 44 0 (M) May be inoperative with seat occupied provided seat is secured in taxi, takeoff and landing position.

-02B Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking, swivel, and other positioning controls)

D 44 0 May be inoperative with seat occupied provided control is failed in taxi, takeoff and landing position.

-02C Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking, swivel, and other positioning controls)

D 44 0 May be missing or inoperative in other than taxi, takeoff, and landing position provided affected seat is considered inoperative (Refer to item 25-20-06).


25-20-06 thru

25-20-06-02C


25-20-06-02A Near The Captains Instrument Panel NO

(Continued)



Page 25-13

Maintenance (M)

25-20-06-02A

Secure the passenger seat in the taxi/takeoff/landing position. Refer to the Model 750 Cabin Equipment Operation Manual.



Page 25-14

25-30-01 Refreshment Center Hot Liquid Storage System Heater Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Refreshment Center

Hot Liquid Storage System Heater

C 2 0 (M) May be inoperative provided system is deactivated.


25-30-01 Near The Captains Instrument Panel YES Maintenance (M)

Pull and secure the UPPER HOT TANK (CB3F) and the LOWER HOT TANK (CB4F) Circuit Breakers located in the Refreshment Center.



Page 25-15

25-40-01 Exterior Lavatory Door Ashtray Repair Category Number Installed


Item Remarks Or Exceptions 40-01 Exterior Lavatory

Door Ashtray A 1 0 May be missing provided it is replaced within 10 consecutive

calendar days.


25-40-01 Near The Captains Instrument Panel YES NOTE: Relief is written per AD 74-08-09R3 and AMOC.



Page 25-16

25-50-01 Baggage Restraint System Repair Category Number Installed


Item Remarks Or Exceptions -50-01 Baggage Restraint

System D 1 0 Individual components may be inoperative or missing

provided baggage is secured by alternate means or not carried.

-01A Baggage Restraint System (Anchor Plate)

C 1 0 Individual anchor plates may be inoperative provided: a) No visible damage exists, and b) Baggage is secured using remaining anchor plates or not

carried.

-01B Baggage Restraint System (Anchor Plate)

C 26 0 (M) Individual anchor plates may be damaged provided: a) Attaching structure is inspected for damage, and b) Baggage is secured using remaining anchor plates or not

carried.


25-50-01 25-50-01-01A 25-50-01-01B

Near The Captains Instrument Panel NO

Maintenance (M)

25-50-01-01B

Tools and Equipment

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Equipment and Furnishings - General. For the supplier publication part number and manufacturer data, refer to the Introduction - Supplier Publication List.

Reference Material


• Chapter 6, Access Plates and Panels Identification - Description and Operation.

Setup

1. Open the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

2. Remove upholstery panels as necessary to get access to the tailcone baggage compartment floor.

3. Remove aft baggage compartment panels as necessary to get access to the baggage anchor plates and structure. Refer to Chapter 6, Access Plates and Panels Identification – Description and Operation.

4. Do an Inspection of the Baggage Anchor Plates and Structure.

5. Examine the baggage anchor plates and structure for damage, corrosion, cracks, loose fasteners, correct installation, or failure.

6. Identify the unserviceable baggage anchor plates that must not be used.

(Continued)



Page 25-17

Closeout

1. Install aft baggage compartment panels. Refer to Chapter 6, Access Plates and Panels Identification - Description and Operation.

2. Install upholstery panels as necessary.

3. Close the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.



Page 25-18

25-50-02 Cabin Storage Compartment Repair Category Number Installed


Item Remarks Or Exceptions -00A Cabin Storage

Compartment C 24 0 (M) May be inoperative provided:

a) Compartment does not contain any aircraft system protection devices,

b) Any emergency equipment located in affected compartment is considered inoperative,

c) Affected compartment is not used for storage of any item except for those permanently affixed,

d) Procedures are established and used to secure compartment closed, and

e) Affected compartment is prominently placarded "DO NOT USE".

-00B Cabin Storage Compartment

C 24 0 (M) May be inoperative provided: a) Affected door is removed, b) Affected compartment is not used for storage of any item,

including those permanently affixed, c) Cabin occupants are briefed that affected compartment

may not be used, and d) Affected compartment is prominently placarded "DO NOT

USE".

-01 Cabin Storage Compartment (Shelving)

D 14 0 (O) May be inoperative provided: a) Any permanently affixed emergency equipment located

on affected shelf is relocated and available for use, and b) Cabin occupants are briefed on location of relocated

equipment.


25-50-02-01 Near The Captains Instrument Panel YES

25-50-02-00A 25-50-02-00B


Maintenance (M)

25-50-02-00A, 25-50-02-00B

Remove the cabin storage compartment door. Refer to the Model 750 Interior Maintenance Manual and Illustrated Parts Catalog.

Operations (O)

25-50-02-01

1. Make sure all equipment located on affected shelf has been relocated and is available for use.

2. Brief cabin occupants on location of relocated equipment.



Page 25-19

25-60-03 Emergency Medical Equipment Repair Category Number Installed


Item Remarks Or Exceptions -60-03 First Aid Kit (FAK)

(Includes associated equipment)

1 1 MUST BE INSTALLED.

NOTE: Seal may be broken provided First Aid Kit contains minimum quantities of all required items.


25-60-03 N/A N/A



Page 25-20

25-61-01 Life Preserver (Crew and passenger) Repair Category Number Installed


Item Remarks Or Exceptions -61-01 Life Preserver

(Crew and passenger)

D 11 0 May be missing, or inoperative provided affected preserver is placarded "INOPERATIVE" or removed.

An operative life vest must be available for each occupant of the aircraft when operated beyond 50 nautical miles from the nearest shore,

OR

An operative life vest equipped with an approved survivor locator light must be available for each occupant of the aircraft when operated beyond 30 minutes flying time or 100 nautical miles from the nearest shore.





Page 25-21

25-62-01 Emergency Locator Transmitter (ELT) Repair Category Number Installed


Item Remarks Or Exceptions -01 Emergency Locator

Transmitter (ELT ) (Survival Type ELTs)

D 1 0 Except for Extended Overwater Operations, may be inoperative or missing.

-02A Emergency Locator Transmitter (ELT) (Fixed, Automatic)

A 1 0 (M) May be inoperative provided: a) System is deactivated or removed, and b) Repairs are made within 90 calendar days.


25-62-01-01 Near The Captains Instrument Panel YES

25-62-01-02A Near The Captains Instrument Panel NO Maintenance (M)

25-62-01-02A

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Equipment and Furnishings - General. For the supplier publication part number and manufacturer data, refer to the Introduction - Supplier Publication List.

Tools and Equipment

Protective Covers.

Reference Material

Artex 406-N Emergency Locator Transmitter (ELT) Antenna - Removal/Installation.

Isolate the ELT Antenna.

1. Disconnect the ELT antenna coaxial connector adapter from the ELT antenna. Refer to Artex 406-N Emergency Locator Transmitter (ELT) Antenna - Removal/Installation.

2. Put protective covers on the coaxial connector plug and jack.

3. Stow the coaxial cable.



Page 25-22

25-64-01 Life Raft Repair Category Number Installed


Item Remarks Or Exceptions -64-01 Life Rafts D 1 0 Except for Extended Overwater Operations, may be missing,

or inoperative provided affected raft is placarded "INOPERATIVE" or removed.





Page 26-1

Chapter 26 Fire Protection Page Number

26-11-01 Baggage Compartment Smoke Detection System ................................................................... 26-2

26-12-01 APU Fire Detection System ...................................................................................................... 26-3

26-20-03 APU Fire Extinguishing System (Cyan or White FIRE BOTTLE LOW APU message) ............ 26-4

26-22-01 Portable Fire Extinguisher ........................................................................................................ 26-5

ATA 26 – Fire Protection


Page 26-2

26-11-01 Baggage Compartment Smoke Detection System Repair Category Number Installed



Compartment Smoke Detection System (Units -0001 thru -0500)

C 1 0 May be inoperative provided: a) Baggage compartment remains empty (excluding ballast

and/or fly away kits), b) ISO VLV CLOSE is selected ON, and c) Aircraft is operated at FL410 or below.

NOTE 1: BAGGAGE ALTITUDE amber message may appear if baggage altitude exceeds 13,000 feet.

NOTE 2: Operator's MEL should define which items are approved for inclusion in fly away kits and which materials can be used as ballast.





Page 26-3

26-12-01 APU Fire Detection System Repair Category Number Installed


Item Remarks Or Exceptions -12-01 APU Fire Detection

System (Amber APU FIRE DETECT FAIL or FIRE DETECT FAIL A message)

C 1 0 May be inoperative provided APU is considered inoperative (Refer to item 49-20-01).


26-12-01 Near The APU Control Panel YES



Page 26-4

26-20-03 APU Fire Extinguishing System (Cyan or White FIRE BOTTLE LOW APU message)



Item Remarks Or Exceptions -20-03 APU Fire

Extinguishing System (Cyan or White FIRE BOTTLE LOW APU message)

C 1 0 May be inoperative provided APU is considered inoperative (Refer to item 49-20-01).


26-20-03 Near The APU Control Panel YES



Page 26-5

26-22-01 Portable Fire Extinguisher Repair Category Number Installed


Item Remarks Or Exceptions -22-01 Portable Fire

Extinguisher D 2 1 May be inoperative or missing provided:

a) Inoperative fire extinguisher is placarded "INOPERATIVE", removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit, and

b) Required distribution is maintained.

NOTE: One Fire Extinguisher is required on the flight deck





Page 26-6




Page 27-1

Chapter 27 Flight Controls Page Number

27-10-02 Aileron Position Indication ........................................................................................................ 27-2

27-11-01 Aileron Trim Tab Position Indicator / Indication ........................................................................ 27-3

27-20-01 Rudder Pedal Adjustment System ............................................................................................ 27-4

27-20-02 Rudder Position Indication (Lower rudder) ............................................................................... 27-6

27-30-01 Elevator Position Indication ...................................................................................................... 27-7

27-40-01 Horizontal Stabilizer Control Wheel Switch (Fails to arm or drive stabilizer)............................ 27-8

27-60-02 Speed Brake / Roll Spoiler Position Indication (EICAS synoptic wing) .................................... 27-9

27-81-01 Slat Position Indication (EICAS synoptic wing) ...................................................................... 27-10

ATA 27 – Flight Controls


Page 27-2

27-10-02 Aileron Position Indication Repair Category Number Installed


Item Remarks Or Exceptions -10-02 Aileron Position

Indication B 2 1 (O) One may be inoperative provided aileron control is visually

verified prior to each flight.


27-10-02 Near The Aileron Position Indication YES Operations (O)

During the flight control check in the Cockpit Preparation checklist, visually verify movement of both ailerons rather than referencing the EICAS display.



Page 27-3

27-11-01 Aileron Trim Tab Position Indicator / Indication Repair Category Number Installed


Item Remarks Or Exceptions -02 Indicator Cover

(Units -0001 thru -0182 incorporating SB750-27-41 and units -0183 thru -0500)

D 1 0 May be missing, or damaged provided aileron / rudder trim indicator is readable.


27-11-01-02 Near The Aileron Trim Tab Position Indicator / Indication

YES



Page 27-4

27-20-01 Rudder Pedal Adjustment System Repair Category Number Installed


Item Remarks Or Exceptions -20-01 Rudder Pedal

Adjustment System B 4 2 (M)(O) Two may be inoperative provided:

a) Two pedal adjustments are not inoperative at same pilot station,

b) Affected pedal is positioned in a detent and adjustment mechanism is secured from movement,

c) Unaffected pedal is adjusted to match affected pedal, and d) Crewmember seated at affected station verifies full control

movement and brake application is available while restrained, prior to each flight.


27-20-01 Near The Associated Instrument Panel NO Maintenance (M)

Match the Position and Secure the Rudder Pedals (Refer to Figure 901).

1. Set and secure the rudder pedal with the unserviceable adjustment mechanism in a detent position.

2. Set and secure the rudder pedal with the serviceable adjustment mechanism in the same detent position.

3. Operate the rudder pedals through their full range of motion to make sure that there is full rudder control movement and brake application.

(Continued)



Page 27-5

Operations (O)

1. Prior to flight, a crew member shall occupy the affected seat and fasten the restraining system.

2. Make sure full flight control movement and brake application are available.



Page 27-6

27-20-02 Rudder Position Indication (Lower rudder) Repair Category Number Installed


Item Remarks Or Exceptions -20-02 Rudder Position

Indication (Lower rudder)

A 1 0 (O) May be inoperative provided: a) Rudder control is visually verified prior to each flight, and b) Repairs are made within three flight cycles.


27-20-02 Near The Rudder Position Indication YES Operations (O)

During the flight control check in the Cockpit Preparation checklist, visually verify movement of the lower rudder rather than referencing the EICAS display.



Page 27-7

27-30-01 Elevator Position Indication Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Elevator Position

Indication B 2 1 (O) One may be inoperative provided elevator control is

visually verified prior to each flight.


27-30-01 Near The Elevator Position Indication YES Operations (O)

During the flight control check in the Cockpit Preparation checklist, visually verify movement of both elevators rather than referencing the EICAS display.



Page 27-8

27-40-01 Horizontal Stabilizer Control Wheel Switch (Fails to arm or drive stabilizer) Repair Category Number Installed


Item Remarks Or Exceptions -40-01 Horizontal Stabilizer

Control Wheel Switch (Fails to arm or drive stabilizer)

B 2 1 One switch pair may be inoperative provided switch pair is operative at pilot flying station.


27-40-01 Near The Horizontal Stabilizer Control Wheel Switch

YES



Page 27-9

27-60-02 Speed Brake / Roll Spoiler Position Indication (EICAS synoptic wing) Repair Category Number Installed


Item Remarks Or Exceptions -60-02 Speed Brake / Roll

Spoiler Position Indication (EICAS synoptic wing)

C 10 0 (O) Individual indications may be inoperative provided: a) Speedbrake / roll spoiler system is verified operative prior

to each flight, and b) NO TAKEOFF speedbrake warning is verified operative

prior to each flight.


27-60-02 Near The Speed Brake / Roll Spoiler Position Indication

YES

Operations (O)

1. A flight crew member must be placed in a position in front of the aircraft “exterior” where all speedbrakes and spoilers can be seen. Another flight crew member must be seated in the cockpit.

2. Using AFM Normal Procedures, start the engines. Verify both hydraulic systems are operating.

3. Roll the control wheel slowly to one direction.

4. (Exterior) Visually verify the corresponding roll spoiler panels extend and retract appropriately. Repeat for the other direction.

5. Extend the speed brake handle to 50%.

6. (Exterior) Visually verify all speed brake panels partially extend to approximately 20 degrees.

7. Verify the SPEED BRAKES white message appears.

8. Retract the speed brake handle.

9. (Exterior) Visually verify all panels retract.

10. Verify the SPEED BRAKE white message extinguishes.



Page 27-10

27-81-01 Slat Position Indication (EICAS synoptic wing) Repair Category Number Installed


Item Remarks Or Exceptions -81-01 Slat Position

Indication (EICAS synoptic wing)

C 2 0 (O) Individual indications may be inoperative provided: a) Slat system is verified operative prior to each flight, and b) NO TAKEOFF slat warning is verified operative prior to

each flight.


27-81-01 Near The Slat Position Indication YES Operations (O)

1. A flight crew member must be placed in a position in front of the aircraft “exterior” where both slats can be seen. Another flight crew member must be seated in the cockpit.

2. Using AFM Normal Procedures, start the engines. Verify both hydraulic systems are operating.

3. Set the SLAT/FLAP handle to any position excluding UP.

4. (Exterior) Visually verify both slats deploy symmetrically.

5. Verify the SLATS ASYMMETRY and SLATS FAIL amber messages do not appear.

6. Set the SLAP/FLAP handle to UP.

7. (Exterior) Visually verify both slats retract symmetrically.



Page 28-1

Chapter 28 Fuel Page Number

28-10-01 Over-wing Refueling Cap Lock ................................................................................................. 28-2

28-10-02 Single-point Refueling (SPR) System ....................................................................................... 28-3

28-24-01 Center to Wing Fuel Transfer System ...................................................................................... 28-4

28-41-01 Fuel Low Level Indicating System ............................................................................................ 28-5

28-41-02 Fuel Quantity Indicating System ............................................................................................... 28-6

28-43-01 Fuel Temperature Indication (Tank) ......................................................................................... 28-8

ATA 28 – Fuel


Page 28-2

28-10-01 Over-wing Refueling Cap Lock Repair Category Number Installed


Item Remarks Or Exceptions -00A Over-wing Refueling

Cap Lock (Failed unlocked)


-00B Over-wing Refueling Cap Lock (Failed locked)

C 2 0 NOTE: If Single-Point Refueling door lock is also failed in locked position or SPR system is inoperative, refueling will not be possible.


28-10-01-00A 28-10-01-00B

Near The Fuel Panel YES

ATA 28 – Fuel


Page 28-3

28-10-02 Single-point Refueling (SPR) System Repair Category Number Installed


Item Remarks Or Exceptions -10-02 Single-point

Refueling (SPR) System



28-10-02 Near The Fuel Panel YES

ATA 28 – Fuel


Page 28-4

28-24-01 Center to Wing Fuel Transfer System Repair Category Number Installed


Item Remarks Or Exceptions -04-01 Center to Wing Fuel

Transfer System (Units -0001 thru -0500)

B 2 1 One may be inoperative provided: a) Less than 300 pounds of center tank fuel is on-board, and b) Associated CTR WING XFER switch is selected OFF.


28-04-01 Near The CTR WING XFER Switch YES

ATA 28 – Fuel


Page 28-5

28-41-01 Fuel Low Level Indicating System Repair Category Number Installed


Item Remarks Or Exceptions -41-01 Fuel Low Level

Indicating System A 2 1 (O) One may be inoperative provided:

a) Procedures for monitoring fuel quantity are established and used,

b) Both wing fuel quantity indicating systems are operative, and

c) Repairs are made within three flight days.


28-41-01 Near The EICAS Display YES Operations (O)

1. Ensure there are no current logbook entries or deferrals related to either wing fuel quantity indicating systems.

2. Flight crew shall brief the loss of low fuel quantity warning system on the affected side.

3. Flight crew shall monitor fuel balance during flight to make sure adequate fuel remains in both wing fuel tanks for planned mission.

ATA 28 – Fuel


Page 28-6

28-41-02 Fuel Quantity Indicating System Repair Category Number Installed


Item Remarks Or Exceptions -01 Wing Tank A 2 1 (O) One indication may be inoperative provided:

a) Both fuel low level indicating systems and both fuel flow indicating systems are operative,

b) Fuel required for route to be flown is increased by 10%, c) Flight is restricted to a maximum of three hours, remaining

within one hour of a suitable airport at all points along route, d) Both fuel tanks are fueled over-wing to a known, balanced

quantity, e) APU use is limited to thirty cumulative minutes if LH

indicator is inoperative, f) Fuel use is tracked, g) If autopilot is used, it is disconnected every twenty minutes

to detect possible lateral fuel imbalance, monitor trim required and RETRIM L-R WING DOWN amber message, and

h) Repairs are made within three flight cycles.

-02 Center Tank (Units -0001 thru -0500)

B 1 0 (O) May be inoperative provided: a) Fuel required for route to be flown is increased by 10%, b) Center tank is fueled to a known quantity, c) Center to wing fuel transfer system is operative, d) Both wing tank fuel quantity indicating systems are

operative, e) Both CTR WING XFER switches are selected to NORM or

OFF depending on center tank fuel quantity, and f) Fuel use is tracked.


28-41-02-01 28-41-02-02

Near The Fuel Tank Display YES

Operations (O)

28-41-02-01


• Either fuel low level indicating systems

• Either fuel flow indicating systems

2. During preflight planning, increase the fuel required for the route to be flown by 10%. Also plan the route so that the flight will last no longer than three hours while remaining within one hour of a suitable airport at all points.

3. To achieve a known quantity in the affected tank, the tank may be emptied using Single-Point defueling then fueled to a known quantity. It may be completely fueled, or fuel may be transferred out of the tank until it is empty.

4. To track fuel use, operators may use a fuel log or develop their own procedure. This can include matched fuel flow techniques, use of the FMS fuel quantity system or other means.

(Continued)

ATA 28 – Fuel


Page 28-7

5. During flight, disconnect the autopilot every twenty minutes. Make sure a crew member has control of the aircraft prior to disconnecting the autopilot. Check for any abnormal roll tendencies. Check for roll trim required.

6. Re-engage the autopilot. Monitor the RETRIM L or R WING DOWN amber message.

7. Ensure APU use is limited to thirty cumulative minutes if LH indicator is inoperative.

28-41-02-02


• Center to wing fuel transfer system

• Either wing tank fuel quantity indicating systems

2. During preflight planning, increase the fuel required for the route to be flown by 10%.

3. To achieve a known quantity in the center tank, the tank may be emptied using Single-Point defueling then fueled to a known quantity. It may be completely fueled, or fuel may be transferred out of the tank until it is empty.

4. To track fuel use, operators may use a fuel log or develop their own procedure. This can include matched fuel flow techniques, use of the FMS fuel quantity system or other means.

5. Ensure both CTR WING XFER switches are selected to NORM or OFF depending on center tank fuel quantity.

ATA 28 – Fuel


Page 28-8

28-43-01 Fuel Temperature Indication (Tank) Repair Category Number Installed


Item Remarks Or Exceptions -43-01 Fuel Temperature

Indication (Tank)

C 2 1 One may be inoperative provided indications are not required for operations in North Polar Area.


28-43-01 Near The Fuel Temperature Indication YES

ATA 28 – Fuel


Page 29-1

Chapter 29 Hydraulic Power Page Number

29-30-01 Hydraulic Reservoir Quantity Indication (EICAS) ..................................................................... 29-2

ATA 29 – Hydraulic Power


Page 29-2

29-30-01 Hydraulic Reservoir Quantity Indication (EICAS) Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Hydraulic Reservoir

Quantity Indication (EICAS)

B 2 1 (M) One may be inoperative provided: a) Quantity in associated reservoir is verified adequate on

reservoir sight gauge prior to every flight, and b) Associated hydraulic pressure indication is monitored.


29-30-01 Near The EICAS Display Unit NO Maintenance (M)

Setup

1. Remove the applicable pylon access panel to get access to the hydraulic reservoir. Refer to Chapter 6, Access Plates and Panels Identification - Description and Operation.

2. For the left hydraulic reservoir, remove pylon access panel 411CB.

3. For the right hydraulic reservoir, remove pylon access panel 412CB.

Examine the Affected Hydraulic Reservoir.

Make sure that the hydraulic fluid quantity in the affected hydraulic reservoir is sufficient. Refer to the placard installed on the reservoir.

Closeout

1. Install the applicable pylon access panel. Refer to Chapter 6, Access Plates and Panels Identification - Description and Operation.

2. For the left hydraulic reservoir, install pylon access panel 411CB.

3. For the right hydraulic reservoir, install pylon access panel 412CB.

ATA 29 – Hydraulic Power


Page 30-1

Chapter 30 Ice and Rain Protection Page Number

30-10-01 Bleed Air Anti-Ice Resistive Temperature Device (RTD) .......................................................... 30-2

30-10-02 Horizontal Stabilizer Bleed Air Anti-Ice System (Failed open) ................................................. 30-3

30-10-03 Leading Edge Slat Bleed Air Anti-Ice System .......................................................................... 30-6

30-10-04 Wing Bleed Air Anti-Ice System (Inboard Leading Edge) ......................................................... 30-8

30-10-05 Wing Root Cuff Electric Anti-Ice System .................................................................................. 30-9

30-20-01 Engine Anti-Ice System .......................................................................................................... 30-10

30-30-03 Pitot Tube Heater (Excluding Standby) (Amber PITOT HTR FAIL L or R message) ............ 30-12

30-30-04 Static Port Heater (Excluding Standby) (Amber STATIC HT FAIL L or R message) ............ 30-13

30-30-05 Temperature Probe Heater (RAT) (Amber RAT HEAT FAIL L or R message) ..................... 30-14

30-40-01 Rain Removal System (Fan) ................................................................................................... 30-15

30-40-02 Windshield Electric Anti-Ice System ....................................................................................... 30-16

30-40-04 Windshield Rain Repellant ...................................................................................................... 30-17

30-40-05 Frost Pane Defog System ....................................................................................................... 30-18

30-70-01 Drain Heater (Refreshment center and aft vanity basin) ........................................................ 30-19

ATA 30 – Ice and Rain Protection


Page 30-2

30-10-01 Bleed Air Anti-Ice Resistive Temperature Device (RTD) Repair Category Number Installed


Item Remarks Or Exceptions -10-01 Bleed Air Anti-Ice

Resistive Temperature Device (RTD) (All except TH001, TH002, TH003, TH004, TL017, TL019, TL021, TR018, TR020, TR022, TT017, TT018, TT019, TT020, and TT021) (Units -0001 thru -0500)

C 44 29 May be inoperative provided: a) All ANTI-ICE ENGINE, STABILIZER, and SLAT

switches are selected OFF, and b) Aircraft is not operated in known, forecast, or AFM-

defined icing conditions.


30-10-01 Near The ANTI-ICE Panel YES



Page 30-3

30-10-02 Horizontal Stabilizer Bleed Air Anti-Ice System (Failed open) Repair Category Number Installed


Item Remarks Or Exceptions -10-02 Horizontal Stabilizer

Bleed Air Anti-Ice System (Failed open) (Units -0001 thru -0500)

C 2 1 (M) One may be inoperative provided: a) Affected valve is secured for no flow, b) Affected ANTI-ICE STABILIZER switch is selected OFF,

and c) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions.


30-10-02 Near The ANTI-ICE Panel NO Maintenance (M)

Setup


2. Disconnect the unserviceable horizontal stabilizer shutoff valve (VT033 left, VT022 right) from the anti-icing tube (upstreamof the valve). Refer to Horizontal Stabilizer Shutoff Valve - Removal/Installation.

Install a Blocking Plate on the Unserviceable Horizontal Stabilizer Shutoff Valve (Refer to Figure 903).

NOTE: The blocking plate installation on the left and the right horizontal stabilizer shutoff valves is opposite.

1. Install the blocking plate on the unserviceable horizontal stabilizer shutoff valve, between the valve and the anti-icing tube.

2. Connect the unserviceable horizontal stabilizer shutoff valve to the anti-icing tube. Refer to Horizontal Stabilizer Shutoff Valve - Removal/Installation.

(Continued)



Page 30-4

(Continued)



Page 30-5



Page 30-6

30-10-03 Leading Edge Slat Bleed Air Anti-Ice System Repair Category Number Installed


Item Remarks Or Exceptions -10-03 Leading Edge Slat

Bleed Air Anti-Ice System (Units -0001 thru -0500)

C 2 0 (M) May be inoperative provided: a) Both slat valves are secured for no flow, b) ANTI-ICE SLAT switch is selected OFF, and, c) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions.



Setup


2. Disconnect the left (VL001) and the right (VR002) wing leading edge shutoff valves from the anti-icing tubes (upstream of the valves). Refer to Wing Leading Edge Shutoff Valve - Removal/Installation.

Install Blocking Plates on the Left and the Right Wing Leading Edge Shutoff Valves (Refer to Figure 902).

NOTE: The blocking plate installation on the left and the right wing leading edge shutoff valves is opposite.

1. Install the blocking plates on the left and the right wing leading edge shutoff valves, between the valves and the anti-icing tubes.

2. Connect the left and the right wing leading edge shutoff valves to the anti-icing tubes. Refer to Wing Leading Edge Shutoff Valve - Removal/Installation.

(Continued)



Page 30-7



Page 30-8

30-10-04 Wing Bleed Air Anti-Ice System (Inboard Leading Edge) Repair Category Number Installed


Item Remarks Or Exceptions -10-04 Wing Bleed Air Anti-

Ice System (Inboard Leading Edge) (Units -0001 thru -0500)

A 2 0 (M) May be inoperative provided: a) Both wing valves are secured for no flow, b) Both ANTI-ICE ENGINE switches are selected OFF, c) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions, and d) Repairs are made within three flight days.



Setup


2. Disconnect the left (VT009) and the right (VT008) wing anti-icing engine shutoff valves from the tube assemblies (upstream of the valves). Refer to Wing Anti-Icing Engine Shutoff Valve -Removal/Installation.

Install Blocking Plates on the Left and the Right Wing Anti-Icing Engine Shutoff Valves (Refer to Figure 901).

NOTE: The blocking plate installation on the left and the right wing anti-icing engine shutoff valves is typical.

1. Install the blocking plates on the left and the right wing anti-icing engine shutoff valves, between the valves and the tube assemblies.

2. Connect the left and the right wing anti-icing engine shutoff valves to the tube assemblies. Refer to Wing Anti-Icing Engine Shutoff Valve - Removal/Installation.



Page 30-9

30-10-05 Wing Root Cuff Electric Anti-Ice System Repair Category Number Installed


Item Remarks Or Exceptions -10-05 Wing Root Cuff

Electric Anti-Ice System

A 2 0 (M) May be inoperative provided: a) Affected wing cuff is deactivated, b) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions, and c) Repairs are made within three flight days.



Pull and secure the following associated circuit breaker:

Item Circuit Breaker Location Wing Root Cuff Electric Anti-Ice System (Left) Inoperative

L FAIRING HEAT (HZ158) Left DC Power J-Box

Wing Root Cuff Electric Anti-Ice System (Right) Inoperative

R FAIRING HEAT (HZ258) Right DC Power J-Box



Page 30-10

30-20-01 Engine Anti-Ice System Repair Category Number Installed


Item Remarks Or Exceptions -20-01 Engine Anti-Ice


A 2 1 (M) One may be inoperative provided: a) Affected valve is secured for no flow, b) Affected ANTI-ICE ENGINE switch is selected OFF, c) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions, and d) Repairs are made within three flight days.



Setup


2. Disconnect the unserviceable engine air inlet shutoff valve (VD001 left, VD002 right) from the bleed air tube (upstream of the valve). Refer to Engine Air Inlet Shutoff Valve -Removal/Installation.

Install a Blocking Plate on the Unserviceable Engine Air Inlet Shutoff Valve (Refer to Figure 904).

NOTE: The blocking plate installation on the left and the right engine air inlet shutoff valves is typical.

1. Install the blocking plate on the unserviceable engine air inlet shutoff valve, between the valve and the bleed air tube.

2. Connect the unserviceable engine air inlet shutoff valve to the bleed air tube. Refer to Engine Air Inlet Shutoff Valve - Removal/Installation.

(Continued)



Page 30-11



Page 30-12

30-30-03 Pitot Tube Heater (Excluding Standby) (Amber PITOT HTR FAIL L or R message)



Item Remarks Or Exceptions -30-03 Pitot Tube Heater

(Excluding Standby) (Amber PITOT HTR FAIL L or R message)

B 2 1 One may be inoperative provided: a) Aircraft is not operated at night, b) Aircraft is not operated in Instrument Meteorological

Conditions (IMC), c) Pitot heater is not required by 14 CFR, and d) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions.





Page 30-13

30-30-04 Static Port Heater (Excluding Standby) (Amber STATIC HT FAIL L or R message)



Item Remarks Or Exceptions -30-04 Static Port Heater

(Excluding Standby) (Amber STATIC HT FAIL L or R message)

B 4 3 One may be inoperative provided: a) Aircraft is not operated at night, b) Aircraft is not operated in Instrument Meteorological

Conditions (IMC), c) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions, and d) Aircraft is not operated RVSM.





Page 30-14

30-30-05 Temperature Probe Heater (RAT) (Amber RAT HEAT FAIL L or R message)



Item Remarks Or Exceptions -30-05 Temperature Probe

Heater (RAT) (Amber RAT HEAT FAIL L or R message)

B 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions.





Page 30-15

30-40-01 Rain Removal System (Fan) Repair Category Number Installed


Item Remarks Or Exceptions -40-01 Rain Removal

System (Fan)

C 1 0 May be inoperative provided aircraft is not operated in precipitation within five nautical miles of airport used for takeoff, intended landing or any alternates required by 14 CFR.





Page 30-16

30-40-02 Windshield Electric Anti-Ice System Repair Category Number Installed


Item Remarks Or Exceptions -40-02 Windshield Electric

Anti-Ice System (Units -0001 thru -0500)

C 2 1 (M) One may be inoperative provided: a) Affected windshield anti-ice system is deactivated, b) Affected ANTI-ICE WINDSHIELD switch is selected OFF, c) A means to clear windshield of moisture is readily available,

and d) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions.


30-40-02 Near The ANTI-ICE Panel YES Maintenance (M)

Pull and secure the LH W/S (HC008) or RH W/S (HC027) circuit breaker on the pilot’s circuit breaker panel.



Page 30-17

30-40-04 Windshield Rain Repellant Repair Category Number Installed


Item Remarks Or Exceptions -40-04 Windshield Rain

Repellant C 1 0 May be missing provided aircraft is not operated in

precipitation within five nautical miles of airport used for takeoff, intended landing or any alternates required by 14 CFR.





Page 30-18

30-40-05 Frost Pane Defog System Repair Category Number Installed


Item Remarks Or Exceptions -40-05 Frost Pane Defog

System C 2 0 May be inoperative.





Page 30-19

30-70-01 Drain Heater (Refreshment center and aft vanity basin) Repair Category Number Installed


Item Remarks Or Exceptions -70-01 Drain Heater

(Refreshment center and aft vanity basin)

C 2 0 (M) May be inoperative provided: a) Drain heaters are deactivated, and b) Refreshment center and aft vanity basin overboard drains

are considered inoperative (Refer to item 38-30-04).


30-70-01 Near The ANTI-ICE Panel YES Maintenance (M)

Pull and secure the DRAIN HEATERS (HW2026) circuit breaker located Interior J-Box.



Page 30-20




Page 31-1

Chapter 31 Indicating / Recording Systems Page Number

31-10-01 APU Maintenance Panel ........................................................................................................... 31-2

31-20-01 APU Hour Meter........................................................................................................................ 31-3

31-20-02 Clock ......................................................................................................................................... 31-4

31-20-04 Flight Hour Meter ...................................................................................................................... 31-5

31-30-02 Engine Event Marker (Function or EVENT MARKER button) .................................................. 31-6

31-30-03 Flight Data Recorder (Cyan or White FDR FAIL message) ..................................................... 31-7

31-50-03 Central Warning ........................................................................................................................ 31-8

31-60-01 Cockpit Fold-down Monitor ....................................................................................................... 31-9

ATA 30 – Indicating and Recording Systems


Page 31-2

31-10-01 APU Maintenance Panel Repair Category Number Installed


Item Remarks Or Exceptions -04 Emergency Shutoff C 1 0 May be inoperative.


31-10-01-04 Near The APU Maintenance Panel YES



Page 31-3

31-20-01 APU Hour Meter Repair Category Number Installed


Item Remarks Or Exceptions -20-01 APU Hour Meter C 1 0 (O) May be inoperative provided APU operation time is

tracked by alternate means.


31-20-01 Near The APU Hour Meter YES Operations (O)

1. Log elapsed time of APU in aircraft logbook after each flight. This includes ground operation times during any maintenance performed when the aircraft is not intended to fly.

2. Once the APU hour meter is repaired, place a placard next to the hour meter showing the additional time accumulated while inoperative (e.g. “+ 14.2 hours”).



Page 31-4

31-20-02 Clock Repair Category Number Installed


Item Remarks Or Exceptions -20-02 Clock D 2 1 May be inoperative.


31-20-02 Near The Associated Clock YES



Page 31-5

31-20-04 Flight Hour Meter Repair Category Number Installed


Item Remarks Or Exceptions -20-04 Flight Hour Meter C 1 0 (O) May be inoperative provided flight time is tracked by

alternate means.


31-20-04 Near The Flight Hour Meter YES

Operations (O)

1. Record Zulu time of takeoff and landing.

2. Log elapsed time in aircraft logbook after each flight.

3. Once the flight hour meter is repaired, place a placard next to the hour meter showing the additional time accumulated while inoperative (e.g. “+ 14.2 hours”).



Page 31-6

31-30-02 Engine Event Marker (Function or EVENT MARKER button) Repair Category Number Installed


Item Remarks Or Exceptions -30-02 Engine Event

Marker (Function or EVENT MARKER button)



31-30-02 Near The Engine Event Marker YES



Page 31-7

31-30-03 Flight Data Recorder (Cyan or White FDR FAIL message) Repair Category Number Installed


Item Remarks Or Exceptions -00C Flight Data Recorder

(Cyan or White FDR FAIL message) (Holder of an Air Carrier or Commercial Operator Certificate)

A 1 0 May be inoperative provided: a) Aircraft is not dispatched from an airport where repairs

can be made unless, b) Flight Data Recorder (FDR) failure occurs after

dispatch but prior to takeoff, or c) Flight Data Recorder (FDR) repair was attempted but

not successful, d) In those cases where repair is attempted but not

successful, aircraft may be dispatched on a flight or series of flights until arriving at next airport where repairs can be made at which the repair must be accomplished prior to dispatch, and

e) Repairs are made within three flight days.

-01A Flight Data Recorder (FDR) Parameters required by 14 CFR

A 88 85 Up to three (3) recording parameters may be inoperative provided: a) Cockpit Voice Recorder (CVR) operates normally, and b) Repairs are made within 20 calendar days.

-01B Flight Data Recorder (FDR) Parameters not required by 14 CFR

A 65 0 May be inoperative provided repairs are made prior to completion of next scheduled inspection / check of FDR.

-02 Underwater Locator Device (ULD)

D 1 0 May be inoperative provided device is not required by 14 CFR.

NOTE: ULD not required for 14 CFR part 135 operations.


31-30-03-00C thru

31-30-03-02

Near The FDR Panel YES



Page 31-8

31-50-03 Central Warning Repair Category Number Installed


Item Remarks Or Exceptions -01 Master Warning

Light (Failed to illuminate)


-02 Master Warning Cancel / Reset Function


-03 Master Caution Light (Failed to illuminate)


-04 Master Caution Cancel / Reset Function



31-50-03-01 thru

31-50-03-04

Near The Associated Light YES



Page 31-9

31-60-01 Cockpit Fold-down Monitor Repair Category Number Installed


Item Remarks Or Exceptions -60-01 Cockpit Fold-down

Monitor D 1 0 May be inoperative.


31-60-01 Near The Cockpit Fold-down Monitor YES



Page 31-10




Page 33-1

Chapter 33 Lights Page Number

33-10-01 Cockpit and Instrument Lighting (Excluding button lights, standby flight instrument lighting, internally lighted annunciators, and required placard lighting) ................................................. 33-2

33-10-02 Cockpit Flood Light (Units -0001 thru -0500) ............................................................................ 33-3

33-10-05 Windshield Ice Detection Light ................................................................................................. 33-4

33-20-02 Cabin Interior Lighting (Excluding cabin emergency lighting) .................................................. 33-5

33-20-04 Lighted Passenger Information Sign (Excluding cabin exit signs) ............................................ 33-6

33-30-01 Aft Baggage Compartment Light .............................................................................................. 33-7

33-30-03 Single-point Refueling Panel Light ........................................................................................... 33-8

33-30-04 Tailcone Maintenance Light ...................................................................................................... 33-9

33-40-01 Anti-Collision Light System (Wing strobe) .............................................................................. 33-10

33-40-02 Ground Recognition Light (Beacon) ....................................................................................... 33-11

33-40-03 Landing Light .......................................................................................................................... 33-12

33-40-05 Position / Navigation Light System ......................................................................................... 33-13

33-40-06 Pylon Work Light ..................................................................................................................... 33-14

33-40-08 Tail Flood Light ....................................................................................................................... 33-15

33-40-09 Taxi Light ................................................................................................................................ 33-16

33-40-10 Wing Inspection Light ............................................................................................................. 33-17

33-50-01 Cockpit Flashlight ................................................................................................................... 33-18

33-50-02 Dropped-aisle Lighting System (LED) .................................................................................... 33-19

33-50-04 Exterior Emergency Light ....................................................................................................... 33-20

ATA 33 – Lights


Page 33-2

33-10-01 Cockpit and Instrument Lighting (Excluding button lights, standby flight instrument lighting, internally lighted annunciators, and required placard lighting)



Item Remarks Or Exceptions -00A Cockpit and

Instrument Lighting (Day)

C 1 0 May be inoperative provided aircraft is not operated at night.

-00B Cockpit and Instrument Lighting (Night)

C 1 0 Individual lights may be inoperative provided: a) Cockpit emergency lighting is operative, b) Remaining lights are sufficient to clearly illuminate all

required instruments, controls, and other devices for which it is provided,

c) Remaining lights are positioned so that direct rays are shielded from crewmembers' eyes, and

d) Lighting configuration and intensity is acceptable to flight crew.


33-10-01-00A 33-10-01-00B

Near The Associated Control YES

ATA 33 – Lights


Page 33-3

33-10-02 Cockpit Flood Light (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -00A Cockpit Flood Light

(Single light failed) C 2 1 One may be inoperative.

-00B Cockpit Flood Light (Both lights failed)

C 2 0 May be inoperative provided lighting configuration and intensity is acceptable to flight crew.


33-10-02-00A 33-10-02-00B


ATA 33 – Lights


Page 33-4

33-10-05 Windshield Ice Detection Light Repair Category Number Installed


Item Remarks Or Exceptions -00A Windshield Ice

Detection Light (Single light failed)

C 2 1 (O) One may be inoperative provided alternate procedures are established and used to monitor ice accretion.

-00B Windshield Ice Detection Light (Both lights failed)



33-10-05-00A 33-10-05-00B

Near The Associated Light YES

Operations (O)

33-10-05-00A

The flight crew member with the operative light must be assigned responsibility for monitoring the windshield for ice accumulation and alerted the other flight crew member.

ATA 33 – Lights


Page 33-5

33-20-02 Cabin Interior Lighting (Excluding cabin emergency lighting) Repair Category Number Installed


Item Remarks Or Exceptions -00A Cabin Interior

Lighting (Excluding cabin emergency lighting)

C 1 0 (O) Individual lights may be inoperative provided: a) Sufficient lighting is operative for crew to perform required

duties, b) Cabin emergency lighting is verified operative, and c) Sufficient lighting is operative for carrying cabin occupants

at night.

-00B Cabin Interior Lighting (Excluding cabin emergency lighting)

D 1 0 (O) May be inoperative provided: a) Cabin emergency lighting is verified operative, and b) Aircraft is not operated at night or cabin occupants are not

carried.


33-20-02-00A 33-20-02-00B


Operations (O)

33-20-02-00A





A. Sufficient lighting is operative for crew to perform required duties.

B. Sufficient lighting is operative for carrying cabin occupants at night.

33-20-02-00B




4. Ensure Aircraft is not operated at night or cabin occupants are not carried.

ATA 33 – Lights


Page 33-6

33-20-04 Lighted Passenger Information Sign (Excluding cabin exit signs) Repair Category Number Installed


Item Remarks Or Exceptions -00A Lighted Passenger

Information Sign (With cabin occupants)

C 4 0 (O) May be inoperative provided alternate procedures are established and used to notify cabin occupants.

-00B Lighted Passenger Information Sign (Without cabin occupants)

C 4 0 May be inoperative provided no cabin occupants are carried.


33-20-04-00A 33-20-04-00B

Near The Light Control YES

Operations (O)

33-20-04-00A

A crew member will use the PA system or turn and face the cabin occupants to make appropriate announcements.

ATA 33 – Lights


Page 33-7

33-30-01 Aft Baggage Compartment Light Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Aft Baggage

Compartment Light C 3 0 May be inoperative.


33-30-01 Near The Light Control YES

ATA 33 – Lights


Page 33-8

33-30-03 Single-point Refueling Panel Light Repair Category Number Installed


Item Remarks Or Exceptions -30-03 Single-point

Refueling Panel Light



33-30-03 Near The Light Control YES

ATA 33 – Lights


Page 33-9

33-30-04 Tailcone Maintenance Light Repair Category Number Installed


Item Remarks Or Exceptions -30-04 Tailcone

Maintenance Light C 2 0 May be inoperative.

-01 Tailcone Maintenance Light (Door Proximity Switch) (Failed to extinguish light)

C 1 0 May be inoperative provided TAILCONE LIGHT switch is selected OFF prior to tailcone access door closure.


33-30-04 33-30-04-01

Near The Light Switch YES

ATA 33 – Lights


Page 33-10

33-40-01 Anti-Collision Light System (Wing strobe) Repair Category Number Installed


Item Remarks Or Exceptions -00A Anti-Collision Light

System (Wing strobe)

C 1 0 May be inoperative provided system is not required by 14 CFR.

-00B Anti-Collision Light System (Wing strobe)

A 1 0 May be inoperative provided: a) Position / navigation light system is operative, b) Ground recognition light is operative, and c) Repairs are made within three flight days.


33-40-01-00A 33-40-01-00B

Near The Anti-Collision Light Switch YES

ATA 33 – Lights


Page 33-11

33-40-02 Ground Recognition Light (Beacon) Repair Category Number Installed


Item Remarks Or Exceptions -40-02 Ground Recognition

Light (Beacon)

C 2 0 NOTE: Position / navigation or anti-collision lights may be used on ground to alert nearby aircraft or personnel when engines are running or prior to start.


33-40-02 Near The Associated Switch YES

ATA 33 – Lights


Page 33-12

33-40-03 Landing Light Repair Category Number Installed


Item Remarks Or Exceptions -00A Landing Light

(Single light failed) C 2 1 One may be inoperative provided a taxi light is operative.

-00C Landing Light (Both lights failed, day)


-01 Landing Light (Recognition Light Mode)

C 1 0 (O) May be inoperative provided at least one landing light is verified operative for night operations.

-02 Landing Light (Pulse Light Mode)

D 1 0 (O) May be inoperative provided at least one landing light is verified operative for night operations.


33-40-03-00A thru

33-40-03-02

Near The Associated Switch YES

Operations (O)

33-40-03-01

During the Preliminary Exterior Inspection, verify at least one landing light is operative.

33-40-03-02

During the Preliminary Exterior Inspection, verify at least one landing light is operative.

ATA 33 – Lights


Page 33-13

33-40-05 Position / Navigation Light System Repair Category Number Installed


Item Remarks Or Exceptions -40-05 Position / Navigation

Light System C 1 0 May be inoperative provided aircraft is not operated at

night.

-01 LED Wing Light (Per side) (Units -0001 thru -0500 Winglet-equipped aircraft and Units -0501 and on)

C 2 1 One light assembly may be inoperative.

NOTE: Position / navigation light system is still considered operative.


33-40-05 33-40-05-01

Near The NAV LIGHTS Switch YES

ATA 33 – Lights


Page 33-14

33-40-06 Pylon Work Light Repair Category Number Installed


Item Remarks Or Exceptions -40-06 Pylon Work Light D 2 0 May be inoperative.



ATA 33 – Lights


Page 33-15

33-40-08 Tail Flood Light Repair Category Number Installed


Item Remarks Or Exceptions -40-08 Tail Flood Light D 2 0 May be inoperative.



ATA 33 – Lights


Page 33-16

33-40-09 Taxi Light Repair Category Number Installed


Item Remarks Or Exceptions -00A Taxi Light

(Single light failed) C 2 1 One may be inoperative.

-00B Taxi Light (Both lights failed, night)

C 2 0 May be inoperative provided both landing lights are operative.

-00C Taxi Light (Both lights failed, day)


-01 Taxi Light (Wingtip Downwash Light)



33-40-09-00A thru

33-40-09-01

Near The Associated Switch YES

ATA 33 – Lights


Page 33-17

33-40-10 Wing Inspection Light Repair Category Number Installed


Item Remarks Or Exceptions -00A Wing Inspection

Light (Single light failed)

C 2 1 One may be inoperative provided ground deicing procedures do not require its use.

-00B Wing Inspection Light (Both lights failed)

C 2 0 May be inoperative provided: a) Aircraft is not operated at night in known, forecast, or AFM-

defined icing conditions, and b) Ground deicing procedures do not require its use.


33-40-10-00A 33-40-10-00B

Near The WING INSP Light Switch YES

ATA 33 – Lights


Page 33-18

33-50-01 Cockpit Flashlight Repair Category Number Installed


Item Remarks Or Exceptions -50-01 Cockpit Flashlight C 2 0 May be inoperative or missing provided crewmember assigned

to associated seat has a flashlight with at least two “D” cells, or the equivalent, that is in good working order.

-01 Cockpit Flashlight (Holder)

C 2 0 May be inoperative provided associated flashlight is stowed by alternate means.


33-50-01 33-50-01-01

Near The Associated Holder YES

ATA 33 – Lights


Page 33-19

33-50-02 Dropped-aisle Lighting System (LED) Repair Category Number Installed


Item Remarks Or Exceptions -01 Dropped-aisle

Lighting System (LED) (Left Forward Half) (Emergency Lighting)

C 40 - Up to four LED elements may be inoperative within any two-foot length.

NOTE: Dropped-aisle lighting system is still considered operative.

-02 Dropped-aisle Lighting System (LED) (Left Aft Half)


-03 Dropped-aisle Lighting System (LED) (Right Aft Half) (Emergency Lighting)

C 10 6 Up to four LED elements may be inoperative within any two-foot length.

NOTE: Dropped-aisle lighting system is still considered operative.

-04 Dropped-aisle Lighting System (LED) (Right Forward Half)



33-50-02-01 thru

33-50-02-04

Near The Light Control YES

ATA 33 – Lights


Page 33-20

33-50-04 Exterior Emergency Light Repair Category Number Installed


Item Remarks Or Exceptions -50-04 Exterior Emergency

Light B 2 0 May be inoperative provided aircraft is not operated at night.


33-50-04 Near The EMERG LT Switch YES

ATA 33 – Lights


Page 34-1

Chapter 34 Navigation Page Number

34-16-01 Altitude Alerting System ............................................................................................................ 34-3

34-18-01 Angle of Attack (AOA) System .................................................................................................. 34-4

34-18-02 Angle of Attack (AOA) Heater ................................................................................................... 34-5

34-22-02 Standby Horizontal Situation Indicator (Heading information only) .......................................... 34-6

34-23-01 Non-stabilized Magnetic Compass (Units -0001 thru -0500) .................................................... 34-7

34-24-01 Mechanical Slip / Skid Indicator (PFD bezel) ........................................................................... 34-8

34-25-02 Display Unit (Center - DU3) ...................................................................................................... 34-9

34-25-03 Flight Director System ............................................................................................................ 34-10

34-25-05 Display Controller ................................................................................................................... 34-11

34-25-08 MFD Controller (Included on DC-840) (Units -0001 thru -0500) ............................................ 34-12

34-25-11 Course / Heading Panel Function Control (RI-871) (Units -0001 thru -0500) ........................ 34-13

34-25-13 Source Controller (SC-840) (Units -0001 thru -0500) ............................................................. 34-15

34-25-14 Display Unit Bezel Controller (BL-870 or BL-871) (Units -0001 thru -0500) .......................... 34-16

34-31-01 Localizer System .................................................................................................................... 34-17

34-32-01 Glideslope System .................................................................................................................. 34-18

34-34-01 Marker Beacon Receiver System ........................................................................................... 34-19

34-36-01 Reactive Windshear System ................................................................................................... 34-20

34-41-01 Inertial Reference System (IRS) ............................................................................................. 34-21

34-42-01 Weather Radar System .......................................................................................................... 34-22

34-44-01 Radio Altimeter System .......................................................................................................... 34-23

34-44-03 Terrain Awareness and Warning System (TAWS) ................................................................. 34-24

34-44-03 Terrain Awareness and Warning System (TAWS) (Continued) ............................................. 34-25

34-45-01 Traffic Alert and Collision Avoidance System (TCAS I or TCAS II) (Amber TCAS FAIL message) 34-27

34-51-01 Distance Measuring Equipment (DME) .................................................................................. 34-29

34-52-01 ATC Transponder and Automatic Altitude Reporting System ................................................ 34-30

34-54-01 Very High Frequency Omni Range (VOR) System ................................................................ 34-31

ATA 34 – Navigation


Page 34-2

34-55-01 Automatic Direction Finder (ADF) ........................................................................................... 34-32

34-57-01 Global Navigation Satellite System ........................................................................................ 34-33

34-60-01 Data Loader ............................................................................................................................ 34-34

34-60-02 Flight Management System (FMS) ......................................................................................... 34-35

34-61-01 Navigation Database .............................................................................................................. 34-36



Page 34-3

34-16-01 Altitude Alerting System Repair Category Number Installed


Item Remarks Or Exceptions -16-01 Altitude Alerting

System A 1 0 (O) May be inoperative provided:

a) Autopilot with altitude hold and capture operates normally, b) Aircraft does not depart from an airport where repair or

replacement can be made, c) Aircraft is not operated RVSM, and d) Repairs are made within three flight days.


-01 Altitude Alerting System (Aural Alert)

C 1 0 May be inoperative provided: a) Visual alert operates normally, and b) Autopilot with altitude hold and capture operates normally.

-02 Altitude Alerting System (Visual Alert)

C 1 0 May be inoperative provided: a) Aural alert operates normally, and b) Autopilot with altitude hold and capture operates normally.


34-16-01 34-16-01-01 34-16-01-02

Near The Remote Instrument Controller YES

Operations (O)

34-16-01

1. Ensure there are no current logbook entries or deferrals related to the altitude hold and capture modes of the Autopilot.

2. Crew briefings must include a reminder that the Altitude Alerting System is inoperative.

3. The flight crew will use aural callouts pertaining to approach target altitudes as assigned by ATC or depicted on approach charts.


A. Aircraft does not depart from an airport where repair or replacement can be made

B. Aircraft is not operated RVSM



Page 34-4

34-18-01 Angle of Attack (AOA) System Repair Category Number Installed


Item Remarks Or Exceptions -18-01 Angle of Attack

(AOA) System (Amber AOA PROBE FAIL L or R or STALL WARN L or R message)

B 2 1 One may be inoperative on pilot not flying side provided affected stick shaker is considered inoperative (Refer to item 34-18-01-03).

-01 Angle of Attack (AOA) System (Indexer)


-02 Angle of Attack (AOA) System (Indicator) (Units -0001 thru -0500)

C 1 0 May be inoperative provided both stick shakers are verified operative.

-03 Angle of Attack (AOA) System (Stick Shaker) (Amber AOA PROBE FAIL L or R or STALL WARN L or R message)

B 2 1 One may be inoperative provider stick shaker on pilot flying side is operative.


34-18-01 thru

34-18-01-03

Near The Associated Message or System YES



Page 34-5

34-18-02 Angle of Attack (AOA) Heater Repair Category Number Installed


Item Remarks Or Exceptions -01 Angle of Attack

(AOA) Heater (Probe) (Units -0001 thru -0500) (Amber AOA HEAT FAIL L or R message)

C 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions.

-02 Angle of Attack (AOA) Heater (Case)

C 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions.


34-18-02-01 34-18-02-02

Near The ANTI-ICE Panel YES



Page 34-6

34-22-02 Standby Horizontal Situation Indicator (Heading information only) Repair Category Number Installed


Item Remarks Or Exceptions -22-02 Standby Horizontal

Situation Indicator (Heading information only) (Units -0001 thru -0500)

B 1 0 May be inoperative provided: a) Dual heading information sources are operative, and b) Magnetic compass is operative.


34-22-02 Near The Standby HSI YES



Page 34-7

34-23-01 Non-stabilized Magnetic Compass (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -00A Non-stabilized

Magnetic Compass (Day, VMC)

B 1 0 May be inoperative provided: a) Any combination of two gyro, AHRS or INS-stabilized

compass systems are operative, and b) Aircraft is not operated at night or in Instrument

Meteorological Conditions (IMC).

-00B Non-stabilized Magnetic Compass (Day, VMC)

B 1 0 May be inoperative provided: a) Any combination of two gyro, AHRS or INS-stabilized

compass systems are operative, b) Aircraft is operated with dual independent navigation

capability, and c) Aircraft is operated under positive radar control by ATC on

enroute portion of flight.

-00C Non-stabilized Magnetic Compass (Day, VMC)

B 1 0 May be inoperative provided any combination of three gyro, AHRS or INS-stabilized compass systems are operative.

-01 Non-stabilized Magnetic Compass (Internal Lighting)

C 1 0 May be inoperative provided flight crew determines adequate natural or artificial lighting exists to read compass.


34-23-01-00A thru

34-23-01-01

Near The Non-Stabilized Magnetic Compass YES



Page 34-8

34-24-01 Mechanical Slip / Skid Indicator (PFD bezel) Repair Category Number Installed


Item Remarks Or Exceptions -24-01 Mechanical Slip /

Skid Indicator (PFD bezel) (Units -0001 thru -0500)

B 2 1 May be inoperative on pilot not flying side.


34-24-01 Near The Mechanical Slip / Skid Indicator YES



Page 34-9

34-25-02 Display Unit (Center - DU3) Repair Category Number Installed


Item Remarks Or Exceptions -25-02 Display Unit

(Center - DU3) (Units -0001 thru -0500) (Amber CHECK DU 3 message)

C 1 0 May be inoperative provided: a) Affected display unit is installed in center position, and b) EICAS DSPLY is selected L or R, as desired.


34-25-02 Near The Center - DU3 YES



Page 34-10

34-25-03 Flight Director System Repair Category Number Installed


Item Remarks Or Exceptions -25-03 Flight Director

System (Units -0001 thru -0500) (Cyan FGC A or B FAIL or Amber FD FAIL message)

C 2 1 One may be inoperative provided flight director reverts or is selected to operative channel.

-00A Flight Director System (Single side failed)

C 2 1 One side may be inoperative provided: a) Command bars are not present on affected side, and b) Approach or departure procedures do not require its use.

-00B Flight Director System (Both sides failed)

B 2 0 May be inoperative provided: a) Command bars are not present, b) Approach or departure procedures do not require its use,

and c) Autopilot system is considered inoperative (Refer to item

22-10-03).



34-25-03 34-25-03-00A 34-25-03-00B

Near The Flight Director Panel YES



Page 34-11

34-25-05 Display Controller Repair Category Number Installed


Item Remarks Or Exceptions -05 Display Controller

(Timer Control) (ET) (Per side) (Units -0001 thru -0500)


-06 Display Controller (HSI Mode Selector) (PFD HSI) (Per side) (Units -0001 thru -0500)

C 1 0 May be inoperative provided current horizontal situation indicator display on PFD is acceptable to flight crew.

-07 Display Controller (Weather Radar / Terrain Selector) (PFD WX) (Per side) (Units -0001 thru -0500)



34-25-05-05 34-25-05-06 34-25-05-07

Near The Display Controller YES



Page 34-12

34-25-08 MFD Controller (Included on DC-840) (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -01 MFD Controller

(Checklist Control) (NORM, ABN, EMER, RCL, PAG, SKP, ENT) (Per side)

C 7 0 NOTE: Any functions or controls that operate normally may be used.

-03 MFD Controller (Map Mode Control) (MFD MAP) (Per side)


-05 MFD Controller (Weather / Terrain Selector) (MFD WX) (Per side)

C 1 0 May be inoperative provided weather radar is displayed on PFD when required.

-07 MFD Controller (Joystick) (Per side)


-09 MFD Controller (Traffic Control) (TCAS) (Per side)

C 1 0 May be inoperative provided button on opposite controller is operative.

-10 MFD Controller (Aircraft System Control) (ACFT SYS) (Per side)



34-25-08-01 thru

34-25-08-10

Near The MFD Controller YES



Page 34-13

34-25-11 Course / Heading Panel Function Control (RI-871) (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -01 Course / Heading

Panel Function Control (Course)

B 2 1 One may be inoperative provided procedures do not require its use.

-02 Course / Heading Panel Function Control (Course Direct) (CRS PUSH DIR)


-03 Course / Heading Panel Function Control (Heading Sync) (HDG PUSH SYNC)



34-25-11-01 34-25-11-02 34-25-11-03

Near The Course / Heading Panel Function Control

YES



Page 34-14

34-25-12 Electric Standby Instrument System Repair Category Number Installed


Item Remarks Or Exceptions -25-12 Electric Standby

Instrument System (GH-3000) (Heading information only) (Units -0001 thru -0500)

B 1 0 May be inoperative provided: a) Dual heading information sources are operative, and b) Magnetic compass is operative.


34-25-12 Adjacent To The Electric Standby Instrument YES



Page 34-15

34-25-13 Source Controller (SC-840) (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -01 Source Controller

(Bearing Selector) (BRG) (Per side)

C 2 1 One may be inoperative provided procedures do not require its use.

-02 Source Controller (Navigation Source Selector) (NAV-PREV-FMS) (Per side)

C 3 0 May be inoperative provided: a) Button is operative on pilot flying side, and b) Flight director/autopilot is coupled to pilot flying side.


34-25-13-01 34-25-13-02

Near The Source Controller YES



Page 34-16

34-25-14 Display Unit Bezel Controller (BL-870 or BL-871) (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -01 Display Unit Bezel

Controller (Barometer Standard) (STD) (Per side)


-02 Display Unit Bezel Controller (MFD Range Control (Knob) (Per side)

C 1 0 May be inoperative provided current map range is acceptable to the flight crew.

-03 Display Unit Bezel Controller (Minimums Selector) (MINIMUMS) (Per side)

C 1 0 May be inoperative or knob may be missing provided procedures do not require its use.

-04 Display Unit Bezel Controller (Minimums Mode Selector) (RA/BARO) (Per side)



34-25-14-01 thru

34-25-14-04

Near The Display Unit Bezel Controller YES



Page 34-17

34-31-01 Localizer System Repair Category Number Installed


Item Remarks Or Exceptions -31-01 Localizer System C 2 1 Number 2 may be inoperative provided:

a) Affected system is not on an emergency bus, b) Associated glideslope is considered inoperative (Refer to

item 34-32-01). c) Procedures do not require its use, and d) Localizer is not required for the approach to be flown.


34-31-01 Near The Nav Panel YES



Page 34-18

34-32-01 Glideslope System Repair Category Number Installed


Item Remarks Or Exceptions -32-01 Glideslope System C 2 0 May be inoperative provided:

a) Procedures do not require its use, and b) Glideslope is not required for the approach to be flown.





Page 34-19

34-34-01 Marker Beacon Receiver System Repair Category Number Installed


Item Remarks Or Exceptions -34-01 Marker Beacon

Receiver System C 2 0 May be inoperative provided:

a) Procedures do not require its use, and b) Marker Beacon is not required for the approach to be flown.


34-34-01 Near The NAV Control Panel YES



Page 34-20

34-36-01 Reactive Windshear System Repair Category Number Installed


Item Remarks Or Exceptions -36-01 Reactive Windshear

System (Includes TAWS windshear mode) (Amber WINDSHEAR FAIL message)



34-36-01 Near The WINDSHEAR FAIL Message YES Operations (O)

Crew briefings must include escape procedures for a windshear encounter and alternate methods used for monitoring for windshear encounters.



Page 34-21

34-41-01 Inertial Reference System (IRS) Repair Category Number Installed


Item Remarks Or Exceptions -41-01 Inertial Reference

System (IRS) (Units -0016, -0067 and On and Units -0001 thru -0015, -0017 thru -0066 incorporating SB750-34-57)

C 2 0 (O) May be inoperative provided: a) Other navigation systems as required by 14 CFR are

operative, b) Affected IRS mode is selected to ATT, c) IRS 1 and 2 are verified capable of providing correct bank,

pitch, and magnetic heading indications to associated PFD, and

d) Aircraft is operated using applicable AFM limitations.


34-41-01 Near The NAV Control Panel YES Operations (O)

1. While on the ground, not moving, select the mode controller to ATT on the IRS controller.

2. Verify the attitude indication on the associated PFD shows the correct bank and pitch.

3. Set the magnetic heading to the correct direction.

4. Ensure aircraft is operated using applicable AFM limitations.

NOTE: Heading drift can occur while in the attitude mode, magnetic heading should be updated periodically using the best available sources.



Page 34-22

34-42-01 Weather Radar System Repair Category Number Installed


Item Remarks Or Exceptions -42-01 Weather Radar

System C 1 0 Do not operate the aircraft in IFR or night VFR conditions

when current weather reports indicate that thunderstorms, or other potentially hazardous weather conditions that can be detected with airborne weather radar, may reasonably be expected along the route to be flown.

-01 Radar Control Panel (Units -0001 thru -0500) (Aircraft with two control panels)



34-42-01 34-42-01-01

Near The Weather Radar Control YES



Page 34-23

34-44-01 Radio Altimeter System Repair Category Number Installed


Item Remarks Or Exceptions -00B Radio Altimeter

System (TAWS or TCAS II required) (Units -0001 thru -0500)

A 1 0 (M) May be inoperative provided: a) Radio altimeter is deactivated, b) Approach minimums or operating procedures do not require

its use, c) Basic TAWS modes are considered inoperative (Refer to

item 34-44-03), d) TCAS II is considered inoperative (Refer to item 34-45-01), e) Autothrottle system, if installed, is considered inoperative,

and f) Repairs are made within two flight days.

NOTE 1: Landing gear warning system will function differently without radio altimeter input. Landing gear warning may occur at higher altitudes above ground with flaps extended.

NOTE 2: Landing Operations Phase Inhibit (LOPI) operation will be affected. LOPI may not activate during approach or go-around.


34-44-01-00B Near The Radio Altimeter YES Maintenance (M)

Pull and secure the RADIO ALTIMETER (HZ150) Circuit Breaker located in the Left DC Power J-Box.



Page 34-24

34-44-03 Terrain Awareness and Warning System (TAWS) Repair Category Number Installed


Item Remarks Or Exceptions -44-03 Terrain Awareness

and Warning System (TAWS) (Including test mode) (Class A or B TAWS required) (Amber TERRAIN FAIL, TERR FAIL, GROUND PROX FAIL, or GPWS FAIL message)

A 1 0 (O) May be inoperative provided: a) Alternate procedures are established and used, b) RNP AR procedures are not conducted, and c) Repairs are made within two flight days.

-01 Forward Looking Terrain Avoidance Function and Premature Descent Alert Function (Amber TERRAIN FAIL or TERR FAIL message)

B 2 0 (O) May be inoperative provided alternate procedures are established and used.

-02 Excessive Rate of Descent (Mode 1) and Altitude Loss After Takeoff or Missed Approach (Mode 3) (Amber GROUND PROX FAIL or GPWS FAIL message)

A 2 0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within two flight days.

-03A Voice Callouts (Mode 6) ("Five-Hundred") (Amber GROUND PROX FAIL or GPWS FAIL message)

B 1 0 (O) May be inoperative provided alternate procedures are established and used.

(Continued)



Page 34-25

34-44-03 Terrain Awareness and Warning System (TAWS) (Continued) Repair Category Number Installed


Item Remarks Or Exceptions -03B Voice Callouts

(Mode 6) (Other) (Amber GROUND PROX FAIL or GPWS FAIL message)


-04B Excessive Closure Rate to Terrain (Mode 2) and Flight Into Terrain Not in Landing Configuration (Mode 4) (Class B TAWS required) (Amber GROUND PROX FAIL or GPWS FAIL message)


-05 Excessive Downward Glideslope/Glidepath Deviation (Mode 5) (Class B TAWS required) (Amber GROUND PROX FAIL or GPWS FAIL message)


-06 Terrain Display (Class B TAWS required)


-07 Switch (Any excluding TAWS Test) (Units -0001 thru -0500) (Class B TAWS required)


-08A Annunciator / Indication (Class B TAWS required)


(Continued)



Page 34-26


34-44-03 thru

34-44-03-08A

Near The GPWS Light YES

Operations (O)

34-44-03

1. Crew briefings must include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance.

2. Ensure RNP AR procedures are not conducted.

34-44-03-01

Crew briefings must include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance.

34-44-03-02

Crew briefings must include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance.

34-44-03-03A

Crew briefings must include aural callouts during approach through the use of appropriate aircraft equipment to ensure obstacle and terrain clearance. Briefing must include a procedure for a crew member to call out 500 feet above airport elevation.

34-44-03-03B

Crew briefings must include aural callouts during approach through the use of appropriate aircraft equipment to ensure obstacle and terrain clearance. Briefing must include MDA or DH and a procedure for a crew member to call out 500 feet above airport elevation, plus any other agreed upon by the flight crew.



Page 34-27

34-45-01 Traffic Alert and Collision Avoidance System (TCAS I or TCAS II) (Amber TCAS FAIL message)



Item Remarks Or Exceptions -00B Traffic Alert and

Collision Avoidance System (TCAS required)

B 1 0 (M) May be inoperative provided: a) System is deactivated, and b) Enroute or approach procedures do not require its use.

-01 Traffic Advisory (TA) Display (TCAS II only)

C 2 0 (O) May be inoperative provided: a) Resolution Advisory (RA) display and audio function are

operative, and b) Enroute or approach procedures do not require use of

TCAS.

-02A Resolution Advisory (RA) Display (TCAS II only)

C 2 1 One may be inoperative on pilot not flying side.

-02B Resolution Advisory (RA) Display (TCAS II only)

C 2 0 (O) May be inoperative provided: a) Traffic Advisory (TA) display and audio funciton are

operative, b) TA-only mode is selected on TCAS controller or menu, and c) Enroute or approach procedures do not require use of

TCAS.

-03A Traffic Advisory (TA) and Resolution Advisory (RA) Displays Failed (TCAS II only)

C 2 1 One side may be inoperative provided: a) Traffic Advisory (TA) and Resolution Advisory (RA) displays

are operative on pilot flying side, and b) Audio function is operative.

-04 Audio Function B 1 0 May be inoperative provided enroute or approach procedures do not require use of TCAS.

-05 Airspace Selection Function (Above / below)



34-45-01-00B thru

34-45-01-05

Near The TCAS Indication YES

Maintenance (M)

34-45-01-00B

Pull and secure the TCAS (HF056) circuit breaker on the copilot’s circuit breaker panel.

(Continued)



Page 34-28

Operations (O)

34-45-01-01

1. Prior to takeoff, perform the TCAS self-test. Make sure the RA display appears on both PFDs and the aural alerts sound.

2. Ensure enroute or approach procedures do not require use of TCAS.

34-45-01-02B

Prior to takeoff, perform the TCAS self-test. Make sure the TA display appears on the appropriate displays and the aural alerts sound.



Page 34-29

34-51-01 Distance Measuring Equipment (DME) Repair Category Number Installed


Item Remarks Or Exceptions -01 Distance Measuring

Equipment (DME) System


-02 Distance Measuring Equipment (DME) System

D 2 0 May be inoperative provided GPS operates normally.

-03 Distance Measuring Equipment (DME) System

D 2 0 May be inoperative for flight below FL 240, or for flight above FL 240 if navigation is not dependent on use of VOR.


34-51-01-01 34-51-01-02 34-51-01-03

Near The PFD Bezel YES



Page 34-30

34-52-01 ATC Transponder and Automatic Altitude Reporting System Repair Category Number Installed


Item Remarks Or Exceptions -00A ATC Transponder

and Automatic Altitude Reporting System (Individual transponder failed) (White TRANSPONDER FAIL 1 or 2 message)


-00B ATC Transponder and Automatic Altitude Reporting System (All transponders failed) (Amber TRANSPONDER FAIL 1 and 2)

B 2 0 May be inoperative provided: a) Operations do not require its use, b) Prior to flight, approval is obtained from ATC facilities

having jurisdiction over planned route of flight, c) TCAS, if installed, is considered inoperative (Refer to item

34-45-01), and d) Aircraft is not operated RVSM.


-01 ATC Transponder and Automatic Altitude Reporting System (Elementary and Enhanced Downlink Aircraft Reportable Parameters) (Not required by 14 CFR)

A 2 0 May be inoperative provided: a) Operations do not require their use, and b) Repairs are made prior to completion of next scheduled

inspection/check of transponder.


34-52-01-00A thru

34-52-01-01

Near The ATC Panel YES



Page 34-31

34-54-01 Very High Frequency Omni Range (VOR) System Repair Category Number Installed


Item Remarks Or Exceptions -54-01 Very High

Frequency Omni Range (VOR) System

C 2 1 Number 2 may be inoperative provided: a) Affected system is not on an emergency bus, b) Procedures do not require its use, and c) System is not required for the route to be flown.





Page 34-32

34-55-01 Automatic Direction Finder (ADF) Repair Category Number Installed


Item Remarks Or Exceptions -55-01 Automatic Direction

Finder (ADF) D 1 0 May be inoperative provided operations do not require its use.


34-55-01 Near The ADF Control Panel YES



Page 34-33

34-57-01 Global Navigation Satellite System Repair Category Number Installed


Item Remarks Or Exceptions -57-01 Global Navigation

Satellite System (GNSS) (Including SBAS)

C 2 0 May be inoperative provided: a) System is not required for the route to be flown, and b) Operations do not require its use.

NOTE: Enhanced function of TAWS may not be available.

NOTE: ADS-B output may not be available.

-01 Antenna/Jack (For portable device)



34-57-01 34-57-01-01

Near The NAV Panel YES



Page 34-34

34-60-01 Data Loader Repair Category Number Installed


Item Remarks Or Exceptions -60-01 Data Loader C 1 0 May be inoperative.


34-60-01 Near The Data Loader YES



Page 34-35

34-60-02 Flight Management System (FMS) Repair Category Number Installed


Item Remarks Or Exceptions -60-02 Flight Management

System (FMS) C 2 0 May be inoperative provided:

a) System is not required for the route to be flown, and b) Operations do not require its use.

NOTE: Enhanced function of TAWS may not be available.

-01 Fuel Planning Function



34-60-02 34-60-02-01

Near The Associated CDU YES



Page 34-36

34-61-01 Navigation Database Repair Category Number Installed


Item Remarks Or Exceptions -61-01 Navigation

Database C 2 0 (O) May be out of currency provided:

a) Current aeronautical charts are used to verify navigation fixes prior to each flight,

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

c) Approach navigation radios are manually tuned and identified.


34-61-01 Near The FMC CDU YES Operations (O)

The navigation database can only be used for enroute and terminal navigation when out of currency. Before using the FMS to navigate to a facility, verify the status, identifier, frequency and lat/long position with an alternate, current source of information. Refer to the applicable Airplane Flight Manual supplement for additional information.



Page 35-1

Chapter 35 Oxygen Page Number

35-00-01 Cockpit Oxygen Pressure Gauge / Indication ........................................................................... 35-2

35-00-02 Oxygen Bottle ........................................................................................................................... 35-3

35-00-03 Oxygen System......................................................................................................................... 35-5

35-20-01 Passenger Oxygen System ...................................................................................................... 35-7

35-20-02 Therapeutic Oxygen System .................................................................................................... 35-8

35-30-01 Portable Oxygen System .......................................................................................................... 35-9

35-30-02 Protective Breathing Equipment (PBE) .................................................................................. 35-10

ATA 35 – Oxygen


Page 35-2

35-00-01 Cockpit Oxygen Pressure Gauge / Indication Repair Category Number Installed


Item Remarks Or Exceptions -00-01 Cockpit Oxygen

Pressure Gauge / Indication (Units -0001 thru -0500 Extended range oxygen system-equipped aircraft and Units -0501 and on)

C 2 1 One may be inoperative provided: a) Associated oxygen bottle is considered inoperative (Refer

to item 35-00-03), and b) Non-associated oxygen bottle is operative.

-01 Gauge Lighting (Units -0001 thru -0500)



35-00-01 35-00-01-01

Near The Cockpit Oxygen Pressure Gauge YES

ATA 35 – Oxygen


Page 35-3

35-00-02 Oxygen Bottle Repair Category Number Installed


Item Remarks Or Exceptions -00-02 Oxygen Bottle

(Units -0001 thru -0500 Extended range oxygen system-equipped aircraft and Units -0501 and on)

C 2 1 (M) One may be inoperative or empty provided: a) Affected bottle regulator is closed, b) Non-affected cockpit oxygen pressure indication/gauge is

operative, and c) Oxygen duration is computed using only operative bottle.


35-00-02 Near The Associated Cockpit Gauge NO Maintenance (M)

Reference Material


• Chapter 20, Safetying - Maintenance Practices.

Setup

• For the left oxygen bottle assembly, open the left nose compartment door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

• For the right oxygen bottle assembly, open the right nose compartment door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

Close the Unserviceable or Empty Oxygen Bottle Assembly Pressure Regulator (Refer to Figure 901).

1. Remove and discard the safety wire from the pressure regulator.

2. Move the pressure regulator lever to the OFF position.

3. Safety the pressure regulator lever in the OFF position with safety wire. Refer to Chapter 20, Safetying - Maintenance Practices.

Closeout

Close the applicable nose compartment door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

(Continued)

ATA 35 – Oxygen


Page 35-4

ATA 35 – Oxygen


Page 35-5

35-00-03 Oxygen System Repair Category Number Installed


Item Remarks Or Exceptions -01 Oxygen System

(Fill Port) C 1 0 (M) May be inoperative provided bottle is filled using alternate

means, if service is required.

-02 Oxygen System (Servicing Panel Pressure Gauge)

C 1 0 (M) May be inoperative provided bottle is filled using alternate means, if service is required.

-03 Oxygen System (Blowout Disk / Green Label)

C 1 0 May be missing or damaged provided oxygen pressure is verified prior to each flight.


35-00-03-01 35-00-03-02

Near The Oxygen Servicing Panel Pressure Gauge

NO

35-00-03-03 Near The Oxygen Servicing Panel Pressure Gauge

YES

Maintenance (M)

35-00-03-01

Reference Material


• Chapter 12, Oxygen System - Servicing

• Chapter 20, Safetying - Maintenance Practices

• Oxygen Bottle Assembly - Removal/Installation.

Setup

• For the left oxygen bottle assembly, open the left nose compartment door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

• For the right oxygen bottle assembly, open the right nose compartment door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

Do the Servicing of the Oxygen Cylinder at the Pressure Regulator (Refer to Figure 901).

1. Remove and discard the safety wire from the pressure regulator.


3. Disconnect the fill line assembly from the pressure regulator. Refer to Oxygen Bottle Assembly - Removal/Installation.

4. Use dry nitrogen air to purge the oxygen from the fill line assembly.

5. Connect the oxygen service cart directly to the pressure regulator, at the fill port.

(Continued)

ATA 35 – Oxygen


Page 35-6

6. Move the pressure regulator lever to the ON position.

7. Use the temperature and pressure tables given in Chapter 12, Oxygen System - Servicing to fill the oxygen cylinder to the correct pressure.


9. Disconnect the oxygen service cart from the fill port on the pressure regulator.

10. Connect the fill line assembly to the pressure regulator. Refer to Oxygen Bottle Assembly -

11. Removal/Installation.

12. Move the pressure regulator lever to the ON position.

13. Safety the pressure regulator lever in the ON position with safety wire. Refer to Chapter 20, Safetying - Maintenance Practices.

Closeout

Close the applicable nose compartment door. Refer to Chapter 6, Airplane Dimensions and Areas - Description and Operation.

35-00-03-02

Reference Material

Chapter 12, Oxygen System - Servicing.

Do the Servicing of the Oxygen System with the Cockpit Oxygen Pressure Display.

NOTE: The use of the cockpit oxygen pressure display is an alternative to the oxygen pressure gage at the oxygen servicing panel.

Do the servicing of the oxygen system. Refer to Chapter 12, Oxygen System - Servicing. During the servicing, use a second person in the cockpit to monitor the cockpit oxygen pressure display.

ATA 35 – Oxygen


Page 35-7

35-20-01 Passenger Oxygen System Repair Category Number Installed


Item Remarks Or Exceptions -00A Passenger Oxygen

System (With cabin occupants)

B 1 0 May be inoperative provided: a) Cabin pressurization system is operative, b) Aircraft is able to descend within four minutes to a cabin

pressure altitude of 13,000 feet at all points along route to be flown, and

c) Aircraft is operated at FL250 or below.

-00B Passenger Oxygen System (Without cabin occupants)

C 1 0 May be inoperative provided: a) PASS OXY is selected OFF, and b) No cabin occupants are carried.

-00C Passenger Oxygen System (Cabin unpressurized)


-01 Passenger Oxygen System (Mask)

C 10 0 (M) Individual oxygen masks or dispensers may be inoperative or missing provided: a) Affected mask pintle pin is installed, and b) Associated seat or lavatory is placarded "DO NOT

OCCUPY".

-02 Passenger Oxygen System (Drop-out Panel) (Units -0001 thru -0500)

C 7 0 (M) Individual panels may be out of normal position provided: a) Affected oxygen mask and drop-out panel are removed, b) Affected mask pintle pin is installed, and c) Associated seat or lavatory is placarded "DO NOT

OCCUPY".


35-20-01-01 35-20-01-02


35-20-01-00A 35-20-01-00B 35-20-01-00C


Maintenance (M)

35-20-01-01, 35-20-01-02

Install the pintle pin (release pin) in the unserviceable or missing passenger oxygen canister.

Refer to Passenger Oxygen Mask - Maintenance Practices.

ATA 35 – Oxygen


Page 35-8

35-20-02 Therapeutic Oxygen System Repair Category Number Installed


Item Remarks Or Exceptions -20-02 Therapeutic Oxygen

System D 1 0 May be inoperative.



ATA 35 – Oxygen


Page 35-9

35-30-01 Portable Oxygen System Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Portable Oxygen

System D 1 0 May be inoperative provided:

a) Inoperative oxygen bottle is placarded "INOPERATIVE", removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit, and

b) Bottles not properly serviced are replaced, serviced, or removed at next available maintenance facility.



ATA 35 – Oxygen


Page 35-10

35-30-02 Protective Breathing Equipment (PBE) Repair Category Number Installed


Item Remarks Or Exceptions -30-02 Protective Breathing

Equipment (PBE) D 1 0 May be inoperative or missing provided location placarding is

removed or obscured.



ATA 35 – Oxygen


Page 36-1

Chapter 36 Pneumatic Page Number

36-10-03 Precooler Door System ............................................................................................................. 36-2

ATA 36 – Pneumatic


Page 36-2

36-10-03 Precooler Door System Repair Category Number Installed


Item Remarks Or Exceptions -10-03 Precooler Door

System C 2 0 (M) May be inoperative provided:

a) Affected door is secured in open position, b) Affected door system is deactivated, and c) Aircraft is not operated in known, forecast, or AFM-defined

icing conditions.


36-10-03 Near The Associated PAC Switch NO Maintenance (M)

Reference Material

• Chapter 20, Safetying - Maintenance Practices

• Ram Air Door Actuator - Removal/Installation.

Setup

1. Disconnect the unserviceable ram air door actuator (UT033 left, UT034 right) from the pylon doors mechanical linkage. Refer to Ram Air Door Actuator - Removal/Installation.

NOTE: When the actuator is disconnected from the mechanical linkage, the spring in the linkage will move the ram air doors to the full open position.

2. Disconnect the electrical connector (PT104 left, PT112 right) from the ram air door actuator.

3. Put a protective cap on the electrical connector and stow it.

Secure the Precooler Doors in the Full Open Position.

NOTE: This procedure is typical for the left and the right precooler doors.

Safety the upper and lower precooler doors to adjacent structure in the full open position with wire. Refer to Chapter 20, Safetying - Maintenance Practices.

ATA 36 – Pneumatic


Page 38-1

Chapter 38 Water / Waste Page Number

38-10-01 Potable Water System .............................................................................................................. 38-2

38-30-02 Lavatory External Service System ............................................................................................ 38-3

38-30-03 Lavatory Waste System ............................................................................................................ 38-5

38-30-04 Overboard Drain (Excluding drain heater) ................................................................................ 38-6

ATA 38 – Water and Waste


Page 38-2

38-10-01 Potable Water System Repair Category Number Installed


Item Remarks Or Exceptions -10-01 Potable Water

System C 2 0 (M) May be inoperative provided:

a) System is drained, and b) Procedures are established and used to ensure system is

not serviced.

-01 Potable Water System (Individual Components)

C 2 0 (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have

leaks.

NOTE: Any portion of system operating normally may be used.


38-10-01 38-10-01-01

Near The EICAS Panel NO

Maintenance (M)

38-10-01-00

Drain the vanity water supply system. Refer to Chapter 12, Vanity Water Supply - Servicing.

38-10-01-01

1. Deactivate the associated components. Refer to the appropriate Interior Maintenance Manual.

2. Verify no leaks are found. If leaks are found, system must be drained and all leaked fluid cleaned, system must not be re-serviced, and weight and Balance with missing fluid must be computed and provided to the flight crew for flight planning purposes.



Page 38-3

38-30-02 Lavatory External Service System Repair Category Number Installed


Item Remarks Or Exceptions -30-02 Lavatory External

Service System C 1 0 (M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have

leaks.

-01A Lavatory External Service System (Dump Cable)

C 1 0 May be inoperative provided lavatory is not serviced or used.

-01B Lavatory External Service System (Dump Cable)

C 1 0 (M) May be inoperative provided lavatory is serviced by alternate means.

-04 Lavatory External Service System (System Precharge Annunciator) (Green PRECHARGE)

C 1 0 (O) May be inoperative provided alternate procedures are established and used for filling toilet.

-08 Lavatory External Service System) (Heater Gasket

C 1 0 (M) May be inoperative provided: a) Waste line is drained of all fluids, b) Heater gasket is deactivated, c) Drain heaters are considered inoperative (Refer to item 30-

70-04), and d) Toilet is not serviced within four hours of landing or at

surface temperatures below +10 C.

-09 Lavatory External Service System (System Overfill Annunciator) (Red OVERFILL)

C 1 0 (O) May be inoperative provided alternate procedures are established and used for filling toilet.


38-30-02 38-30-02-01B 38-30-02-08

Near The EICAS Panel NO

38-30-02-01A 38-30-02-04 38-30-02-09

Near The EICAS Panel YES

(Continued)



Page 38-4

Maintenance (M)

38-30-02

1. Deactivate the associated components. Refer to the appropriate Interior or Airframe Maintenance Manual.

2. Verify no leaks are found. If leaks are found, system must be drained and all leaked fluid cleaned, system must not be re-serviced, and weight and Balance with missing fluid must be computed and provided to the flight crew for flight planning purposes.

38-30-02-01B, 38-30-02-08

Reference Material

Chapter 12, Toilet - Servicing

Model 750 Interior Maintenance Manual and Illustrated Parts Catalog.

Setup

1. Remove the upholstery adjacent to the externally serviceable flush toilet to get access to the drain valve. Refer to the Model 750 Interior Maintenance Manual and Illustrated Parts Catalog.

2. Do the Servicing of the Externally Serviceable Flush Toilet (Manual Operation of the Drain Valve).

A. Do the servicing of the externally serviceable flush toilet. Refer to Chapter 12, Toilet - Servicing.

B. During the servicing, use a second person inside the airplane to operate the drain valve manually, when necessary.

Closeout

Install the upholstery. Refer to the Model 750 Interior Maintenance Manual and Illustrated Parts Catalog.

Operations (O)

38-30-02-04

During lavatory servicing, use a second person inside the airplane to monitor the fluid quantity.

38-30-02-09

During lavatory servicing, use a second person inside the airplane to monitor the fluid quantity.



Page 38-5

38-30-03 Lavatory Waste System Repair Category Number Installed


Item Remarks Or Exceptions -30-03 Lavatory Waste

System C 1 0 Individual components may be inoperative provided:

a) Cabin occupants are briefed prior to each flight that lavatory is inoperative and unusable, and

b) Lavatory is placarded "DO NOT USE".


38-30-03 Near The EICAS Panel YES



Page 38-6

38-30-04 Overboard Drain (Excluding drain heater) Repair Category Number Installed


Item Remarks Or Exceptions -01 Overboard Drain

(Aft Vanity Basin) C 1 0 (O) May be damaged or obstructed provided:

a) All liquid is removed from basin, and b) Basin is placarded “DO NOT USE”.

-02 Overboard Drain (Refreshment Center)

C 1 0 (O) May be damaged or obstructed provided: a) All liquid is removed from refreshment center hot liquid

storage and drip pan, b) Refreshment center hot liquid storage and drip pan are

placarded “DO NOT USE”, and c) Ice drawer drain valve remains closed.


38-30-04-01 38-30-04-02

Near The EICAS Panel YES

Operations (O)

38-30-04-01

1. Remove all liquid from the basin by allowing it to drain while on the ground or using other means such as towels or wet vac.

2. Ensure Basin is placarded “DO NOT USE”.

38-30-04-02

1. Remove all liquid from the drip pan by allowing it to drain while on the ground or using other means such as towels or wet vac.

2. Empty the hot liquid storage tanks.

3. Ensure Refreshment center hot liquid storage and drip pan are placarded “DO NOT USE”.



Page 46-1

Chapter 46 Information Systems Page Number

46-00-01 Electronic Flight Bag (EFB) System ......................................................................................... 46-2

ATA 46 – New Technology


Page 46-2

46-00-01 Electronic Flight Bag (EFB) System Repair Category Number Installed


Item Remarks Or Exceptions -02B Power Connection

(Class 1 & 2) C 2 0 (O) May be inoperative provided alternate procedures are

established and used.


46-00-01-02B Near The Associated Instrument Panel YES Operations (O)

1. Prior to each takeoff, a crew member will ensure that the battery installed in EFB and back up battery has sufficient charge for intended usage during flight.

2. If sufficient battery charge cannot be determined, appropriate and current navigational publications for route of flight and alternates must be carried onboard.

ATA 46 – New Technology


Page 49-1

Chapter 49 APU Page Number

49-20-01 Auxiliary Power Unit (APU) ....................................................................................................... 49-2

49-30-01 APU Fuel Shutoff Valve ............................................................................................................ 49-3

49-50-02 APU Bleed Air System .............................................................................................................. 49-5

ATA 49 – APU


Page 49-2

49-20-01 Auxiliary Power Unit (APU) Repair Category Number Installed


Item Remarks Or Exceptions -20-01 Auxiliary Power Unit

(APU) (Amber APU SYS FAIL or APU FAIL message)

C 1 0 (M) May be inoperative provided: a) APU is deactivated, and b) Procedures do not require its use.


49-20-01 Near The APU Panel YES Maintenance (M)

Pull and secure the APU MASTER (HF096) circuit breaker on the copilot’s circuit breaker panel.

ATA 49 – APU


Page 49-3

49-30-01 APU Fuel Shutoff Valve Repair Category Number Installed


Item Remarks Or Exceptions -30-01 APU Fuel Shutoff

Valve C 1 0 (M) May be inoperative provided:

a) APU fuel shutoff valve is verified closed, and b) APU is considered inoperative (Refer to item 49-20-01).


49-30-01 Near The APU Panel NO Maintenance (M)

Auxiliary Power Unit (APU) Fuel Shutoff Valve Inoperative

Tools and Equipment

NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Auxiliary Power Unit - General. For the supplier publication part number and manufacturer data, refer to the Introduction - Supplier Publication List.

Tools and Equipment

Metal Container.

Reference Material

• Chapter 24, External Electrical Power - Maintenance Practices

• Chapter 45, Central Maintenance System - Description and Operation

• Auxiliary Power Unit Fuel Distribution Tube - Removal/Installation.

Setup

1. Disconnect the APU fuel distribution tube at the APU. Refer to Auxiliary Power Unit Fuel Distribution Tube - Removal/Installation.

2. Put a metal container below the disconnected fuel distribution tube.

Make Sure that the APU Fuel Shutoff Valve is Closed.

1. Connect external electrical power to the airplane. Refer to Chapter 24, External Electrical Power - Maintenance Practices.

2. Make sure that the APU rotary switch on the pedestal switch panel is in the OFF position.

3. Use the pilot's right Garmin GTC 570 Touchscreen Controller to select Aircraft Systems from the Home page. Refer to Chapter 45, Central Maintenance System - Description and Operation.

A. Select the Maintenance page.

B. Select the OEM Diagnostics page.

C. In the Live Data View, find the PCB menu and select Fuel Control LH - NZ102.

D. Scroll until you find the APU Fuel Vlv Cmd indication and make sure that the COMMAND/STATUS shows Closed.

(Continued)

ATA 49 – APU


Page 49-4

4. Push the BOOST PUMP R switch/light on the pedestal switch panel to the ON position.

5. Make sure that no fuel flows from the disconnected fuel distribution tube at the APU.

6. Push the BOOST PUMP R switch/light on the pedestal switch panel to the NORM position.

Closeout

1. Disconnect the external electrical power from the airplane. Refer to Chapter 24, External Electrical Power - Maintenance Practices.

2. Connect the APU fuel distribution tube to the APU. Refer to Auxiliary Power Unit Fuel Distribution Tube - Removal/Installation.

3. Remove the metal container.

ATA 49 – APU


Page 49-5

49-50-02 APU Bleed Air System Repair Category Number Installed


Item Remarks Or Exceptions -50-02 APU Bleed Air


C 1 0 (O) May be inoperative provided: a) APU SYSTEM BLEED AIR is selected OFF, and b) APU bleed air valve is verified closed.

-01 APU Bleed Air System (Max Cool Function) (Units -0001 thru -0500)

C 1 0 (O) May be inoperative provided: a) APU SYSTEM BLEED AIR is not selected to MAX COOL,

and b) Max cool valve is verified closed.


49-50-02 49-50-02-01

Near The APU Panel YES

Operations (O)

49-50-02-00

1. Ensure the APU SYSTEM BLEED AIR is selected OFF.

2. Prior to engine start, start the APU.

3. Verify no air flow exists from the overhead air outlets.

49-50-02-01

1. Prior to engine start, start the APU.

2. Select APU SYSTEM BLEED AIR to ON.

3. Make sure the ISOL VALVE selector is in the CLSD position (white line vertical).

4. Select CKPT PAC to ON.

5. Place one Cockpit Floor Vent valve to NORM.

6. Verify no airflow is present from the same valve.

7. Ensure the APU SYSTEM BLEED AIR is not selected to MAX COOL

ATA 49 – APU


Page 49-6


ATA 49 – APU


Page 52-1

Chapter 52 Doors Page Number

52-10-01 Main Cabin Door ....................................................................................................................... 52-2

52-30-01 Aft Baggage Door ..................................................................................................................... 52-4

52-30-03 Ski Tube Door ........................................................................................................................... 52-5

52-40-01 Nose Access Door (Per side) ................................................................................................... 52-6

52-46-01 Single-point Refueling (SPR) Access Door Key Lock .............................................................. 52-7

52-48-01 Tail Cone Access Door Key Lock (Failed unlocked) ................................................................ 52-8

52-50-01 Cockpit Divider Door ................................................................................................................. 52-9

52-50-02 Lavatory Door ......................................................................................................................... 52-10

52-70-01 Door Warning System ............................................................................................................. 52-11

ATA 52 – Doors


Page 52-2

52-10-01 Main Cabin Door Repair Category Number Installed


Item Remarks Or Exceptions -01 Main Cabin Door

(Key Lock) (Failed unlocked)


-02 Main Cabin Door (Precatch)

C 1 0 (M)(O) May be inoperative provided: a) Main cabin door warning system is operative, b) Precatch is secured in retracted position, and c) Alternate procedures for closing door are established and

used.

-03 Main Cabin Door (Acoustic Seal)

C 1 0 May be damaged provided seal does not interfere with door operation.

-04A Main Cabin Door (Primary Seal) (Cabin pressurized) (Amber CABIN DOOR SEAL message)

C 1 0 May be inoperative provided: a) Primary seal does not interfere with door operation, b) Secondary door seal is verified intact, and c) Aircraft is operated at FL250 or below.

-04B Main Cabin Door (Primary Seal (Cabin) unpressurized) (Amber CABIN DOOR SEAL message)

C 1 0 May be inoperative provided: a) Primary seal does not interfere with door operation, and b) Cabin pressurization system is considered inoperative

(Refer to item 21-30-02).

-05A Main Cabin Door (Secondary Seal) (Cabin pressurized)

C 1 0 May be damaged provided: a) Primary door seal is operative, b) Secondary seal does not interfere with door operation, and c) Aircraft is operated at FL250 or below.

-05B Main Cabin Door (Secondary Seal) (Cabin unpressurized)

C 1 0 May be damaged provided: a) Secondary seal does not interfere with door operation, and b) Cabin pressurization system is considered inoperative

(Refer to item 21-30-02).

-06 Main Cabin Door (Vent Door)

C 1 0 May be inoperative provided aircraft is operated in accordance with AFM CBN VENT DOOR OPEN amber message procedure.

-07 Main Cabin Door (Handrail)

C 1 0 (O) May be inoperative or damaged provided: a) Door operates and latches normally, and b) Alternate procedures are established and used for assisting

passengers during entry and exit.

(Continued)

ATA 52 – Doors


Page 52-3


52-10-01-01 thru

52-10-01-07


52-10-01-02 Near The Captains Instrument Panel NO Maintenance (M)

52-10-01-02

Setup

Open the cabin door.

Secure the Cabin Door Precatch.

1. Move and hold the cabin door precatch in the retracted position.

2. Carefully attach sufficient lengths of 3M vinyl tape (or equivalent) across the cabin door precatch to make sure that it stays in the retracted position.

3. Use a second person to close and latch the cabin door.

4. Make sure that there is no interference between the cabin door precatch and the exit path through the cabin door.

Operations (O)

52-10-01-02

1. Ensure there are no current logbook entries or deferrals related to the Main cabin door warning system.

2. After boarding aircraft and raising the cabin door, either have a crew member or ground crew hold the door closed while the second crew member latches the door.

52-10-01-07

1. Ensure Door and latches operates normally.

2. Prior to entry and exit, occupants are briefed by a crew member not to utilize the handrail.

3. Passengers may need assistance entering and exiting the aircraft.

ATA 52 – Doors


Page 52-4

52-30-01 Aft Baggage Door Repair Category Number Installed


Item Remarks Or Exceptions -01 Aft Baggage Door


D 1 0 May be inoperative provided door is verified closed and latched prior to each flight.

NOTE: Aircraft equipped with JAA baggage door must consider aft baggage door seal inoperative.

-02 Aft Baggage Door (Door Seal) (Units -0001 thru -0500) (Amber BAGGAGE DOOR SEAL message)

C 1 0 May be missing or inoperative provided: a) ISO VLV CLOSE is selected ON, b) Aircraft is operated in accordance with AFM baggage

pressurization system limitations, and c) Aircraft is operated at FL410 or below.

NOTE: BAGGAGE ALTITUDE amber message may appear if baggage altitude exceeds 13,000 feet.

-03 Aft Baggage Door (Ladder)

D 2 0 (O) May be inoperative provided: a) Ladder is removed, or stowed so it does not interfere with

door operation, b) No visible damage exists to surrounding structure, c) Ladder is placarded "DO NOT USE", and d) Alternate means of accessing baggage compartment are

established and used.


52-30-01-01 52-30-01-02 52-30-01-03


Operations (O)

52-30-01-03


A. Ladder is removed, or stowed so it does not interfere with door operation.

B. No visible damage exists to surrounding structure.

C. Ladder is placarded "DO NOT USE".

2. Use an acceptable method to access the baggage area if needed. One method could be to use a step ladder.

ATA 52 – Doors


Page 52-5

52-30-03 Ski Tube Door Repair Category Number Installed


Item Remarks Or Exceptions -30-03 Ski Tube Door

(Units -0080 and on) D 1 0 May be inoperative or missing provided baggage in ski tube is

secured.



ATA 52 – Doors


Page 52-6

52-40-01 Nose Access Door (Per side) Repair Category Number Installed


Item Remarks Or Exceptions -01 Nose Access Door



-02 Nose Access Door (Gas Spring)

D 1 0 May be inoperative or removed.

NOTE: Precautions should be taken when opening door(s).


52-40-01-01 52-40-01-02


ATA 52 – Doors


Page 52-7

52-46-01 Single-point Refueling (SPR) Access Door Key Lock Repair Category Number Installed


Item Remarks Or Exceptions -00A Single-point

Refueling (SPR) Access Door Key Lock (Failed unlocked)


-00B Refueling (SPR) Access Door Key Lock (Failed locked)

C 1 0 NOTE: If over-wing refueling cap locks are also failed in locked position, refueling will not be possible.


52-46-01-00A 52-46-01-00B


ATA 52 – Doors


Page 52-8

52-48-01 Tail Cone Access Door Key Lock (Failed unlocked) Repair Category Number Installed


Item Remarks Or Exceptions -48-01 Tail Cone Access

Door Key Lock (Failed unlocked)




ATA 52 – Doors


Page 52-9

52-50-01 Cockpit Divider Door Repair Category Number Installed


Item Remarks Or Exceptions -50-01 Cockpit Divider Door C 2 0 (M) May be inoperative provided door is secured open.


52-50-01 Adjacent To The Captains Instrument Panel NO Maintenance (M)

Secure the affected door in the open position. One method is to use adhesive tape, taking care not to damage the finish of the interior furnishings.

ATA 52 – Doors


Page 52-10

52-50-02 Lavatory Door Repair Category Number Installed


Item Remarks Or Exceptions -50-02 Lavatory Door C 1 0 (M) May be inoperative provided door is secured open.


52-50-02 Near The Captains Instrument Panel NO Maintenance (M)

Refer to 750 Maintenance Manual Chapter 25, Equipment/Furnishings - Dispatch Deviation.

ATA 52 – Doors


Page 52-11

52-70-01 Door Warning System Repair Category Number Installed


Item Remarks Or Exceptions -01 Door Warning

System (Aft Baggage) (Amber BAGGAGE DOOR OPEN message)

C 1 0 May be inoperative provided door is verified closed, latched, and locked prior to each flight.

-02 Door Warning System (Emergency Exit (Amber) EMERGENCY EXIT OPEN or ESCAPE HATCH OPEN message)

C 1 0 May be inoperative provided hatch is verified closed and latched prior to each flight.

-03 Door Warning System (Tail Cone Access) (Amber TAILCONE DOOR OPEN message)


-04 Door Warning System (Lavatory)

C 1 0 May be inoperative provided lavatory door is visually verified latched or secured open prior to each taxi, takeoff, or landing.

-05 Door Warning System (Nose Access) (Amber NOSE DOOR OPEN L-R message)


-07 Door Warning System (Main Cabin) (Amber CABIN DOOR OPEN message)

B 1 0 (O) May be inoperative provided: a) Main cabin door precatch is operative, b) Lock flags are visible in all door sight glass locations, c) Cabin vent door is verified closed with cabin door closed

and latched, d) Seat(s) immediately adjacent to or across from door are

blocked and placarded “DO NOT OCCUPY”, and e) Aircraft is operated at FL250 or below.

(Continued)

ATA 52 – Doors


Page 52-12

52-70-01 Door Warning System (Continued) Repair Category Number Installed


Item Remarks Or Exceptions -08 Door Warning

System (Single-point Refueling) (SPR) (Amber FUEL DOOR OPEN message)

C 1 0 May be inoperative provided door is verified closed and latched prior to each flight.

-09 Door Warning System (Toilet External Service) (Amber TOILET DOOR OPEN message)

C 1 0 May be inoperative provided door is verified closed and latched prior to each flight.


52-70-01-01 thru

52-70-01-09


Operations (O)

52-70-01-07

1. Once the aircraft has been boarded, a crew member must close and latch cabin door.

2. Verify all green door pin flags are visible.

3. Locate and unscrew cabin vent door access cover on aft side of cabin door steps.

4. Depress cabin vent door lever to ensure vent door is CLOSED.

5. Replace vent door cover.

6. Verify interior door handle is correctly stowed.


A. Main cabin door precatch is operative.

B. Seat(s) immediately adjacent to or across from door are blocked and placarded “DO NOT OCCUPY”.

C. Aircraft is operated at FL250 or below.

ATA 52 – Doors


Page 53-1

Chapter 53 Fuselage Page Number

53-45-01 Life Raft Mooring Ring .............................................................................................................. 53-2

53-50-01 Radome Erosion Boot ............................................................................................................... 53-3

ATA 53 – Fuselage


Page 53-2

53-45-01 Life Raft Mooring Ring Repair Category Number Installed


Item Remarks Or Exceptions -45-01 Life Raft Mooring

Ring D 1 0 Except for Extended Overwater Operations, may be

inoperative or damaged.



ATA 53 – Fuselage


Page 53-3

53-50-01 Radome Erosion Boot Repair Category Number Installed


Item Remarks Or Exceptions -50-01 Radome Erosion

Boot D 1 0 May be damaged or missing provided any remaining sections

of boot are removed.



ATA 53 – Fuselage


Page 53-4


ATA 53 – Fuselage


Page 55-1

Chapter 55 Stabilizers Page Number

55-34-01 Bullet Fairing Erosion Boot ....................................................................................................... 55-2

ATA 55 – Stabilizers


Page 55-2

55-34-01 Bullet Fairing Erosion Boot Repair Category Number Installed


Item Remarks Or Exceptions -34-01 Bullet Fairing

Erosion Boot D 1 0 May be damaged or missing provided any remaining sections

of boot are removed.



ATA 55 – Stabilizers


Page 71-1

Chapter 71 Powerplant Page Number

71-20-01 Active Engine Mount System .................................................................................................... 71-2

ATA 71 – Powerplant


Page 71-2

71-20-01 Active Engine Mount System Repair Category Number Installed


Item Remarks Or Exceptions -20-01 Active Engine Mount

System D 1 0 (M) May be inoperative provided system is deactivated.


71-20-01 Near The Captains Instrument Panel YES Maintenance (M)

Pull and secure the ACT NOISE CTRL (HK048) circuit breaker in the RH main power junction box.

ATA 71 – Powerplant


Page 73-1

Chapter 73 Engine Fuel & Control Page Number

73-10-01 Engine Fuel Filter ...................................................................................................................... 73-2

73-33-01 Fuel Flow Indicating System ..................................................................................................... 73-4

ATA 73 – Engine Fuel and Control


Page 73-2

73-10-01 Engine Fuel Filter Repair Category Number Installed


Item Remarks Or Exceptions -10-01 Engine Fuel Filter

(Impending bypass indication only) (Amber FUEL FLTR BYPASS L or R message)

A 2 1 (M) Aircraft may be dispatched with one impending bypass indication provided: a) Fuel filter full bypass pin is visually verified not extended

prior to each flight, and b) Repairs are made within ten flight hours.


73-10-01 Near The EICAS Display NO Maintenance (M)

1. Open the lower engine cowl to get access to the affected mechanical engine fuel filter actual bypass indicator.

2. Examine the Affected Mechanical Engine Fuel Filter Actual Bypass Indicator (Refer to Figure 901).

3. Make sure that the mechanical engine fuel filter actual bypass indicator (pin) is not extended.

(Continued)



Page 73-3



Page 73-4

73-33-01 Fuel Flow Indicating System Repair Category Number Installed


Item Remarks Or Exceptions -33-01 Fuel Flow Indicating

System A 2 1 One may be inoperative provided:

a) All fuel quantity indicating systems are operative, and b) Repairs are made within three flight days.


73-33-01 Near The EICAS Display YES



Page 76-1

Chapter 76 Engine Controls Page Number

76-01-01 Engine Synchronizer System (Failed off) (Units -0001 thru -0500) .......................................... 76-2

ATA 76 – Engine Controls


Page 76-2

76-01-01 Engine Synchronizer System (Failed off) (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -01-01 Engine Synchronizer

System (Failed off) (Units -0001 thru -0500)



76-01-01 Near The Engine Synchronizer Switch YES

ATA 76 – Engine Controls


Page 77-1

Chapter 77 Engine Indicating Page Number

77-14-01 Engine RPM Gauge / Indication (Units -0001 thru -0500) ........................................................ 77-2

77-22-01 Engine ITT Gauge / Indication (Standby ITT) ........................................................................... 77-3

77-32-01 Engine Vibration Monitor System (N1 or N2) ........................................................................... 77-4

ATA 77 – Engine Indicating


Page 77-2

77-14-01 Engine RPM Gauge / Indication (Units -0001 thru -0500) Repair Category Number Installed


Item Remarks Or Exceptions -01 Engine RPM Gauge

/ Indication (Standby N1)

A 2 1 One may be inoperative provided: a) Standby N2 and standby ITT indicators are operative, and b) Repairs are made within three flight cycles.

-02 Engine RPM Gauge / Indication (Standby N2)

C 2 1 One may be inoperative provided standby N1 and standby ITT indicators are operative.


77-14-01-01 77-14-01-02

Near The EICAS Pane YES



Page 77-3

77-22-01 Engine ITT Gauge / Indication (Standby ITT) Repair Category Number Installed


Item Remarks Or Exceptions -22-01 Engine ITT Gauge /

Indication (Standby ITT) (Units -0001 thru -0500)

C 2 1 One may be inoperative provided standby N1 and standby N2 indicators are operative.


77-22-01 Near The EICAS Pane YES



Page 77-4

77-32-01 Engine Vibration Monitor System (N1 or N2) Repair Category Number Installed


Item Remarks Or Exceptions -32-01 Engine Vibration

Monitor System (N1 or N2)

C 4 2 One system may be inoperative on each engine provided no abnormal vibration exists.


77-32-01 Near The EICAS Pane YES



Page 78-1

Chapter 78 Engine Exhaust Page Number

78-30-01 Thrust Reverser ........................................................................................................................ 78-2

ATA 78 – Engine Exhaust


Page 78-2

78-30-01 Thrust Reverser Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Thrust Reverser C 2 0 (M) May be inoperative provided affected thrust reverser is

deactivated and secured in forward thrust position.

NOTE: Flight crew should review AFM THRUST REVERSERS limitations.


78-30-01 Near The Thrust Reverser Handle NO Maintenance (M)

Disable the unserviceable thrust reverser. Refer to Stowed Thrust Reverser Provision -Maintenance Practices.

ATA 78 – Engine Exhaust


Page 79-1

Chapter 79 Engine Oil Page Number

79-20-01 Engine Oil Filter (Impending bypass indication only) ............................................................... 79-2

79-30-01 Engine Chip Detector ................................................................................................................ 79-3

79-32-02 Oil Level Sensor........................................................................................................................ 79-4

ATA 79 – Engine Oil


Page 79-2

79-20-01 Engine Oil Filter (Impending bypass indication only) Repair Category Number Installed


Item Remarks Or Exceptions -20-01 Engine Oil Filter

(Impending bypass indication only) (Units -0001 thru -0500) (Cyan OIL FILTER BYPASS L or R message)

A 2 1 Aircraft may be dispatched with one impending bypass indication provided aircraft is operated in accordance with AFM OIL FILTER BYPASS L or R cyan message procedure.





Page 79-3

79-30-01 Engine Chip Detector Repair Category Number Installed


Item Remarks Or Exceptions -30-01 Engine Chip

Detector C 2 1 (M) One may be inoperative provided a visual check of

affected chip detector before each flight reveals no anomalies.


79-30-01 Near The EICAS Panel NO Maintenance (M)

Using the appropriate engine maintenance manual, visually inspect the affected chip detector prior to each takeoff.



Page 79-4

79-32-02 Oil Level Sensor Repair Category Number Installed


Item Remarks Or Exceptions -32-02 Oil Level Sensor C 2 1 One may be inoperative provided oil level is checked visually

prior to each flight.





Page 80-1

Chapter 80 Starting Page Number

80-12-01 Engine Start Valve .................................................................................................................... 80-2

ATA 80 – Starting


Page 80-2

80-12-01 Engine Start Valve Repair Category Number Installed


Item Remarks Or Exceptions -12-01 Engine Start Valve C 2 1 (M) One may be inoperative provided:

a) Alternate starting procedures are established and used, and b) Affected start valve is verified closed after engine start.

NOTE: In-flight restart of affected engine will be limited to wind-milling restarts.


80-12-01 Near The Start Switch NO Maintenance (M)

WARNING: Exercise caution when working around couplings and valves. Bleed air lines and couplings may be extremely hot. Serious burns can result from direct physical contact.

1. Verify normal start pressure (greater than 30 PSI) is available.

2. Using a socket, turn the hex fitting at the bottom of the affected engine start valve to the OPEN index mark.

3. Start the affected engine.

4. After engine start, turn the hex fitting back to the CLOSED index mark.

5. Verify no START VALVE OPEN amber message exists.

ATA 80 – Starting


Page IND-1

A

AC Cockpit Outlet ........................................................................................................................................ 24-7

Aft Baggage Compartment Light ................................................................................................................. 33-7

Aft Baggage Door ........................................................................................................................................ 52-4

Aileron Position Indication ........................................................................................................................... 27-2

Aileron Trim Tab Position Indicator / Indication .......................................................................................... 27-3

Altitude Alerting System .............................................................................................................................. 34-3

Angle of Attack (AOA) Heater ..................................................................................................................... 34-5

Angle of Attack (AOA) System .................................................................................................................... 34-4

Anti-Collision Light System (Wing strobe) ................................................................................................. 33-10

APU Bleed Air System ................................................................................................................................ 49-5

APU DC Amperage Gauge/Indication ......................................................................................................... 24-4

APU DC Generating System ....................................................................................................................... 24-3

APU DC Voltage Gauge/Indication ............................................................................................................. 24-5

APU Fire Detection System ........................................................................................................................ 26-3

APU Fire Extinguishing System .................................................................................................................. 26-4

APU Fuel Shutoff Valve .............................................................................................................................. 49-3

APU Hour Meter .......................................................................................................................................... 31-3

APU Maintenance Panel ............................................................................................................................. 31-2

ATC Transponder and Automatic Altitude Reporting System ................................................................... 34-30

Automatic Cabin Briefer .............................................................................................................................. 23-7

Automatic Direction Finder (ADF) ............................................................................................................. 34-32

Autopilot Disconnect Button (AP/TRIM/NWS DISC) (Failed deselected) ................................................... 22-2

Autopilot Interrupt/Flight Director Sync Button ............................................................................................ 22-3

Autopilot System ......................................................................................................................................... 22-4

Auxiliary Power Unit (APU) ......................................................................................................................... 49-2

B

Baggage Compartment Pressurization System ........................................................................................ 21-11

Baggage Compartment Smoke Detection System ..................................................................................... 26-2

Baggage Compartment Warm Air Fan ........................................................................................................ 21-4

Baggage Restraint System ....................................................................................................................... 25-16

Bleed Air Anti-Ice Resistive Temperature Device (RTD) ............................................................................ 30-2

C

Cabin Altitude Gauge/Indication ............................................................................................................... 21-14

Cabin Differential Pressure Gauge/Indication ........................................................................................... 21-16

Cabin Dump Function ................................................................................................................................. 21-8

MEL Index


Page IND-2

Cabin Interior Lighting ................................................................................................................................. 33-5

Cabin Outflow Valve .................................................................................................................................. 21-18

Cabin Overhead Air Outlet .......................................................................................................................... 21-2

Cabin Pressurization Control Panel .......................................................................................................... 21-12

Cabin Pressurization System ...................................................................................................................... 21-9

Cabin Pressurization System Mode .......................................................................................................... 21-13

Cabin Recirculation Fan .............................................................................................................................. 21-5

Cabin Storage Compartment .................................................................................................................... 25-18

Cabin Temperature Remote Control ......................................................................................................... 21-23

Cabin Vertical Speed Gauge/Indication .................................................................................................... 21-17

Center to Wing Fuel Transfer System ......................................................................................................... 28-4

Central Warning .......................................................................................................................................... 31-8

Clock ........................................................................................................................................................... 31-4

Cockpit and Cabin Temperature Control System ..................................................................................... 21-22

Cockpit and Instrument Lighting ................................................................................................................. 33-2

Cockpit Assist Handle ................................................................................................................................. 25-3

Cockpit Divider Door ................................................................................................................................... 52-9

Cockpit Flashlight ...................................................................................................................................... 33-18

Cockpit Flood Light ..................................................................................................................................... 33-3

Cockpit Fold-down Monitor ......................................................................................................................... 31-9

Cockpit Hand Microphone ......................................................................................................................... 23-12

Cockpit Headset and Boom Microphone .................................................................................................. 23-13

Cockpit Headset Audio System ................................................................................................................ 23-14

Cockpit Overhead Air Outlet ....................................................................................................................... 21-3

Cockpit Overhead Communication Speaker ............................................................................................. 23-11

Cockpit Oxygen Pressure Gauge / Indication ............................................................................................. 35-2

Cockpit Sunvisor System (Including attach mechanism) ............................................................................ 25-4

Cockpit Voice Recorder (CVR) (Cyan CVR FAIL message) .................................................................... 23-18

Course / Heading Panel Function Control (RI-871) .................................................................................. 34-13

Crewmember Interphone System (Flight deck to ground) .......................................................................... 23-8

D

Data Loader .............................................................................................................................................. 34-34

DC Cockpit Outlet ....................................................................................................................................... 24-8

Display Controller ...................................................................................................................................... 34-11

Display Unit (Center - DU3) ........................................................................................................................ 34-9

Display Unit Bezel Controller (BL-870 or BL-871) .................................................................................... 34-16

Distance Measuring Equipment (DME) ..................................................................................................... 34-29

MEL Index


Page IND-3

Door Warning System ............................................................................................................................... 52-11

Drain Heater (Refreshment center and aft vanity basin) .......................................................................... 30-19

Dropped-aisle Lighting System (LED) ....................................................................................................... 33-19

E

Electric Cabin Window Shade (Individual shades or entire system) ........................................................ 25-10

Elevator Position Indication ......................................................................................................................... 27-7

Emergency Locator Transmitter (ELT) ...................................................................................................... 25-21

Emergency Medical Equipment ................................................................................................................ 25-19

Engine AC Generating System ................................................................................................................... 24-2

Engine Anti-Ice System ............................................................................................................................. 30-10

Engine Chip Detector .................................................................................................................................. 79-3

Engine Event Marker (Function or EVENT MARKER button) .................................................................... 31-6

Engine Fuel Filter ........................................................................................................................................ 73-2

Engine Oil Filter (Impending bypass indication only) .................................................................................. 79-2

Engine Synchronizer System (Failed off) .................................................................................................... 76-2

Exterior Emergency Light .......................................................................................................................... 33-20

Exterior Lavatory Door Ashtray ................................................................................................................. 25-15

External Power System ............................................................................................................................... 24-6

Eye Reference Ball ..................................................................................................................................... 25-8

F

Flight Crew Seat (Per seat) ......................................................................................................................... 25-5

Flight Data Recorder (Cyan or White FDR FAIL message) ........................................................................ 31-7

Flight Director System ............................................................................................................................... 34-10

Flight Guidance Controller Annunciator (Failed to illuminate) .................................................................... 22-7

Flight Guidance Controller Function Control ............................................................................................... 22-9

Flight Hour Meter ........................................................................................................................................ 31-5

Flight Management System (FMS) ........................................................................................................... 34-35

Flight Phone / SATCOM System ................................................................................................................ 23-2

Frost Pane Defog System ......................................................................................................................... 30-18

Fuel Flow Indicating System ....................................................................................................................... 73-4

Fuel Low Level Indicating System .............................................................................................................. 28-5

Fuel Quantity Indicating System ................................................................................................................. 28-6

Fuel Temperature Indication (Tank) ............................................................................................................ 28-8

G

Glareshield Fan ........................................................................................................................................... 21-6

Glideslope System .................................................................................................................................... 34-18

Global Navigation Satellite System ........................................................................................................... 34-33

MEL Index


Page IND-4

Ground Dispatch Power System ................................................................................................................. 24-9

Ground Recognition Light (Beacon) .......................................................................................................... 33-11

H

Headset Hook ............................................................................................................................................. 25-7

High Frequency (HF) Communication System ........................................................................................... 23-3

Horizontal Stabilizer Bleed Air Anti-Ice System (Failed open) .................................................................... 30-3

I Inertial Reference System (IRS) ............................................................................................................... 34-21

Interior Disconnect .................................................................................................................................... 24-10

L

Landing Light ............................................................................................................................................. 33-12

Lavatory Door ............................................................................................................................................ 52-10

Lavatory External Service System .............................................................................................................. 38-3

Lavatory Waste System .............................................................................................................................. 38-5

Leading Edge Slat Bleed Air Anti-Ice System ............................................................................................. 30-6

Life Preserver (Crew and passenger) ....................................................................................................... 25-20

Life Raft ..................................................................................................................................................... 25-22

Life Rafts ................................................................................................................................................... 25-22

Lighted Passenger Information Sign (Excluding cabin exit signs) .............................................................. 33-6

Localizer System ....................................................................................................................................... 34-17

M

Mach Trim System .................................................................................................................................... 22-12

Main Cabin Door ......................................................................................................................................... 52-2

Marker Beacon Receiver System ............................................................................................................. 34-19

Mechanical Slip / Skid Indicator (PFD bezel) .............................................................................................. 34-8

MFD Controller (Included on DC-840) ...................................................................................................... 34-12

N

Navigation Database ................................................................................................................................. 34-36

Non-essential Equipment and Furnishings (NEF) .................................................................................... 25-11

Non-stabilized Magnetic Compass ............................................................................................................. 34-7

Nose Access Door (Per side) ...................................................................................................................... 52-6

Nose Avionics Cooling Fan ......................................................................................................................... 21-7

O

Oil Level Sensor .......................................................................................................................................... 79-4

orizontal Stabilizer Control Wheel Switch (Fails to arm or drive stabilizer) ................................................ 27-8

Overboard Drain (Excluding drain heater) .................................................................................................. 38-6

MEL Index


Page IND-5

Over-wing Refueling Cap Lock ................................................................................................................... 28-2

Oxygen Bottle .............................................................................................................................................. 35-3

Oxygen System ........................................................................................................................................... 35-5

P

PAC Isolation Valve .................................................................................................................................. 21-19

Passenger Address (PA) System ............................................................................................................... 23-9

Passenger Oxygen System......................................................................................................................... 35-7

Passenger Seat (Including side-facing seats, folding seats and couches) (Per seat) .............................. 25-12

Passenger Seat Belt / Safety Chime ......................................................................................................... 23-10

Pedestal Autopilot Pitch Wheel ................................................................................................................. 22-11

Pitot Tube Heater (Excluding Standby) (Amber PITOT HTR FAIL L or R message) ............................... 30-12

Portable Fire Extinguisher ........................................................................................................................... 26-5

Portable Oxygen System ............................................................................................................................ 35-9

Position / Navigation Light System ........................................................................................................... 33-13

Potable Water System ................................................................................................................................ 38-2

Pressurization Air Conditioning (PAC) System ......................................................................................... 21-20

Protective Breathing Equipment (PBE) ..................................................................................................... 35-10

R

Radio Altimeter System ............................................................................................................................. 34-23

Radio Management Unit (RMU) ................................................................................................................ 23-16

Rain Removal System (Fan) ..................................................................................................................... 30-15

Reactive Windshear System ..................................................................................................................... 34-20

Refreshment Center Hot Liquid Storage System Heater .......................................................................... 25-14

Required Documents Holder (Airworthiness Certificate, Registration, etc ................................................. 25-2

Rudder Pedal Adjustment System .............................................................................................................. 27-4

Rudder Position Indication (Lower rudder) ................................................................................................. 27-6

S

Satellite Datalink Service ............................................................................................................................ 23-5

Selective Call (SELCAL) (System or individual channel) ............................................................................ 23-6

Single-point Refueling (SPR) Access Door Key Lock ................................................................................. 52-7

Single-point Refueling (SPR) System ......................................................................................................... 28-3

Single-point Refueling Panel Light .............................................................................................................. 33-8

Ski Tube Door ............................................................................................................................................. 52-5

Slat Position Indication (EICAS synoptic wing) ......................................................................................... 27-10

Source Controller (SC-840)....................................................................................................................... 34-15

Speed Brake / Roll Spoiler Position Indication (EICAS synoptic wing) ...................................................... 27-9

Standby Horizontal Situation Indicator (Heading information only) ............................................................ 34-6

MEL Index


Page IND-6

Static Port Heater (Excluding Standby) (Amber STATIC HT FAIL L or R message) ............................... 30-13

Static Wick................................................................................................................................................. 23-17

T

Tail Cone Access Door Key Lock (Failed unlocked) ................................................................................... 52-8

Tail Flood Light .......................................................................................................................................... 33-15

Tailcone Maintenance Light ........................................................................................................................ 33-9

Takeoff/Go-Around Button (GA) ................................................................................................................. 22-5

Taxi Light ................................................................................................................................................... 33-16

Temperature Control Panel ....................................................................................................................... 21-24

Temperature Indication System ................................................................................................................ 21-25

Temperature Probe Heater (RAT) (Amber RAT HEAT FAIL L or R message) ........................................ 30-14

Terrain Awareness and Warning System (TAWS) ................................................................................... 34-24

Therapeutic Oxygen System ....................................................................................................................... 35-8

Thrust Reverser .......................................................................................................................................... 78-2

Traffic Alert and Collision Avoidance System (TCAS I or TCAS II) (Amber TCAS FAIL message) ......... 34-27

V

Very High Frequency (VHF) Communication System ................................................................................ 23-4

Very High Frequency Omni Range (VOR) System ................................................................................... 34-31

W

Water Separator ........................................................................................................................................ 21-26

Weather Radar System ............................................................................................................................. 34-22

Windshield Electric Anti-Ice System ......................................................................................................... 30-16

Windshield Ice Detection Light .................................................................................................................... 33-4

Windshield Rain Repellant ........................................................................................................................ 30-17

Wing Bleed Air Anti-Ice System (Inboard Leading Edge) ........................................................................... 30-8

Wing Inspection Light ................................................................................................................................ 33-17

Wing Root Cuff Electric Anti-Ice System ..................................................................................................... 30-9

Y

Yaw Damper ............................................................................................................................................... 22-6

Yoke-mounted Chart Holder ....................................................................................................................... 25-9

MEL Index


Page IND-7


MEL Index

Date post:	11-Apr-2020
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