n680na mel

MINIMUM EQUIPMENT LIST

Millbrook Aviation

For Aircraft:CE-680 SovereignSerial: 680-0526

Registration: N680NA

1032 First Street BLD 112

New Windsor, NY, United States, 12553845.677.1237

Copyright © 2011 Maximum Manuals LLC. All rights reserved.Millbrook Aviation Minimum Equipment List is reserved for the sole use of Millbrook Aviation personnel, aboard Millbrook Aviation aircraft and by appropriate State Regulatory Agencies.No part of this manual may be reproduced or transmitted (by any means including but not limited to: electronic, photocopy, photograph) without the express written consent of Maximum Manuals LLC

Millbrook Aviation MINIMUM EQUIPMENT LISTAIRCRAFT:

CE-680 SovereignSERIAL NO:

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TABLE OF CONTENTS

SYSTEM NO. SYSTEM DESCRIPTION PAGE NO.

- - - Table of Contents I- - - Log of Revisions II- - - Control Page(s) III THRU VII- - - Definitions (PL 25 Rev 20 Dated 12/17/2012) VIII THRU XXI- - - Preamble (PL 34 Rev 4 Dated 08/15/1997) XXII THRU XXIII- - - Company Policies & Procedures XXIV21 Air Conditioning 21 -1 THRU 2322 Auto Flight 22 -1 THRU 2023 Communications 23 -1 THRU 2024 Electrical Power 24 -1 THRU 425 Equipment/ Furnishings 25 -1 THRU 1826 Fire Protection 26 -1 THRU 627 Flight Controls 27 -1, 2, 328 Fuel 28 -1 THRU 429 Hydraulic Power 29 -130 Ice And Rain Protection 30 -1 THRU 1031 Indicating/ Recording Systems 31 -1 THRU 2132 Landing Gear 32 -133 Lights 33 -1 THRU 1534 Navigation 34 -1 THRU 2735 Oxygen 35 -1 THRU 636 Pneumatic 36 -1 THRU 738 Water/waste 38 -1 THRU 445 Central Maintenance Systems 45 -146 Information Systems 46 -1, 249 Airborne Auxiliary Power 49 -1, 2, 352 Doors 52 -1 THRU 853 Fuselage 53 -155 Stabilizers 55 -173 Engine Fuel & Control 73 -176 Engine Controls 76 -177 Engine Indicating 77 -1, 278 Engine Exhaust 78 -1- - - M&O Procedures - APPENDIX 1 THRU 66- - - Special Appendix - Cabin Altitude vs. Cabin Pressure

Differential Conversion Chart---



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LOG OF REVISIONS

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FAA Approval Stamp/Signature



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DEFINITIONS (PL 25 REV 20 DATED 12/17/2012)

1. Accessible Lavatory Items.Under 14 CFR § 382.63, accessible lavatory items include: ability to enter lavatory and maneuver by means of on-board wheelchair. The lavatory shall provide door locks, accessible call buttons, grab bars, faucets, other controls, and dispensers. As an air carrier, you must maintain all aircraft accessibility features in proper working order, per 14 CFR § 382.71. The accessible lavatory requirement, in part, applies to aircraft with more than one isle in which lavatories are provided per § 382.63(a). Aircraft operators are not required to retrofit cabin interiors of existing aircraft to comply with the requirements of § 382.63.

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

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

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

B. Repair Category.See definition #24.



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C. Number Installed.This column depicts the number (quantity) of instrument and equipment items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., fleet configuration differences, cockpit lighting items, cabin lighting items, cargo restraint components) a number is not required and the "-" symbol is used.

D. Number Required for Dispatch.This column depicts the minimum number (quantity) of instrument and equipment items required for operation provided the conditions specified in the "Remarks or Exceptions" column are met. Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator.

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

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

G. Notes.Notes provide additional information for crewmember or maintenance consideration. Notes are used to identify applicable material, which is intended to assist with compliance, but do not relieve the aircraft operator of the responsibility for compliance with all applicable requirements. Additional notes may be amended, deleted, or added to the MEL by the aircraft operator, as appropriate. Notes are not a part of the provisos.



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

4. Airplane Flight Manual (AFM), Rotorcraft Flight Manual (RFM).The FAA-approved AFM/RFM 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 term "approved flight manual" can apply to either an AFM or an RFM. The FAA requires an approved flight manual for aircraft type certification.

5. As Required by 14 CFR.When the MMEL states, "As Required by 14 CFR," the listed instrument or equipment item is subject to certain provisions (restrictive or permissive) expressed in the 14 CFR operating rules. The number of items required by 14 CFR must be operative. When the listed item is not required by 14 CFR, it may be inoperative for the time specified by repair category. The term "14 CFR" has replaced "FAR" as the current reference to Federal Regulations pertaining to aviation. However, many, if not most, MMELs still contain the acronym "FAR"; therefore, this acronym is acceptable and retained in PL-025 and this definition.

6. 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.



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

8. Continuing Authorization - Single Extension.An aircraft operator who has the authorization to use an 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.

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

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

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

12. Deleted."Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft.



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

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

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

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

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

18. Inoperative.A system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) and/or tolerance(s).

19. Inoperative Components of an Inoperative System.Inoperative instrument and equipment items, which are components of a system that is inoperative, are usually considered components directly associated with and having no other function than to support that system (warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MMEL).



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20. Is Not Used.The phrase "Is Not Used" in the provisos, remarks or exceptions for an MMEL instrument or equipment item may specify that another item in the MMEL "is not used". In such cases, crewmembers must not activate, actuate, or otherwise utilize that item under normal operations. It is not necessary for aircraft operators to accomplish the (M) procedure(s) associated with the item. However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used. This informs crewmembers that an instrument or equipment item is not to be used under normal operations.

21. Nonessential Equipment and Furnishings (NEF).NEFs are those items installed on the aircraft as part of the original type certification (TC), STC, engineering order, 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.

22. Operative.An operative system and/or component will accomplish its intended purpose and is consistently functioning normally within its design operating limit(s) and tolerance(s). When an MMEL item specifies that an item of equipment must be operative, it does not mean that it's operational status must be verified; it's to be considered operative unless reported or known to be malfunctioning. When an 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.



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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).

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

24. 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.



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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.

25. 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.

26. Triple Asterisk (***).Indicates an item which is not required by regulation but which may have been installed on some models of aircraft covered by this MMEL. This item may be included on the aircraft operator's MEL after the approving office has determined that the item has been installed on one or more of the aircraft operator's aircraft. The symbol, however, must not be carried forward into the aircraft operator's MEL. It should be noted that neither this policy nor the use of this symbol provides authority to install or remove an item from an aircraft.

27. 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.

28. 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.

29. 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.



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30. (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.

31. (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.

32. Electronic Fault Alerting System.New generation aircraft display system fault indications to the flight crew by use of computerized display systems. Aircraft manufacturers incorporate individual design philosophies when determining the data that is represented. The following are customized definitions (specific to each manufacturer) to help determine the level of messages affecting the aircraft's dispatch status.

A. AIRBUS (A300-600, A310, A318/319/320/321, A330, A340, A380)



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Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system condition messages {WARNING (red), CAUTION (amber)}. On A318/319/320/321, A330 and A340, the ECAM STATUS page also provides MAINTENANCE STATUS messages. Any message that affects airplane dispatch is displayed at the WARNING or CAUTION level. For A318/319/320/321, MAINTENANCE STATUS messages may also affect airplane dispatch. System faults that result only in messages on the Central Maintenance System (CMS) (for A330, A340 and A380) or on the Centralized Fault Display System (CFDS) (for A318/319/320/321) do not affect airplane dispatch and do not require action other than as addressed within the aircraft operator's standard maintenance program.

B. BOEING (B-717, MD-10, MD-11)

These aircraft are equipped with an alerting function which is a subsystem within the Electronic Instrument System (EIS). The alerting function provides various levels of system condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and STATUS). Alerts that affect aircraft dispatch will include WARNING, CAUTION, STATUS or MAINTENANCE level. MAINTENANCE alerts are displayed on the status page of the EIS display panel under the maintenance heading. A MAINTENANCE alert on the EIS indicates the presence of a system fault which can be identified by the Central Fault Display System (CFDS) interrogation. The systems are designed to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be verified for dispatch purposes.

C. BOEING (747-400, 747-8, 757, 767, 777, 787)



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Boeing airplanes equipped with Engine Indicating and Crew Alerting Systems (EICAS) provide different priority levels of system messages (WARNING, CAUTION, ADVISORY, STATUS and MAINTENANCE). Any messages that affect airplane dispatch status will be displayed at a STATUS message level or higher. The absence of an EICAS STATUS or higher level (WARNING, CAUTION, ADVISORY) indicates that the system/component is operating within its approved operating limits or tolerances. System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an aircraft operator's standard maintenance program.

D. CANADAIR (CL-65, CL-604)

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

E. De-HAVILLAND (DASH 8 SERIES 400)

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



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F. EMBRAER (EMB-135/145, ERJ-170/190 Series)

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

G. FOKKER (FK-100)

Fokker aircraft are equipped with Multi Function Display System (MFDS) which provides electronic message referring to the different priority levels of system information (WARNING (red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any messages that affect aircraft dispatch will be at the WARNING, CAUTION or AWARENESS level. In these cases, the MEL must be verified for dispatch capability and maintenance may be required. System conditions that only require maintenance are not presented on the flight deck. These maintenance indications/messages may be presented on the Maintenance & Test Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by dedicated Built-In Test Evaluation (BITE) of systems.

H. GULFSTREAM G-IV, G-V, GV-SP,GIV-X, GVI



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

I. GULFSTREAM G-150, G-200

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

J. GULFSTREAM G280



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Gulfstream airplanes equipped with EICAS provide different priority levels of system messages: WARNING (red), CAUTION (amber), ADVISORY and MAINTENANCE (cyan or blue), and STATUS (white). Any WARNING or CAUTION message affects aeroplane dispatch status and requires that the Aeroplane Flight Manual or the MEL be used to determine dispatch capability. ADVISORY messages which indicate a system failure (e.g., FMS 1 fail) require that the Aeroplane Flight Manual or the MEL be used to determine dispatch capability. MAINTENANCE messages do not affect aeroplane dispatch status. They indicate the presence of a system fault which can be identified by Onboard Maintenance System (OMS) interrogation or by reference to the Aeroplane Flight Manual. STATUS messages do not affect the dispatch status. They indicate the status of a system.



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PAGE NO.XXII

PREAMBLE (PL 34 REV 4 DATED 08/15/1997)

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.



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PREAMBLE (PL 34 REV 4 DATED 08/15/1997)

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.



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COMPANY POLICIES & PROCEDURES

Millbrook Aviation Policies & Procedures

Refer to the Millbrook Aviation General Operations Manual (GOM) for the applicable company MEL and deferral procedures.

Millbrook Aviation MEL Format

All ATA's and Sub-ATA's from the Master MEL are represented and in the following format:

Specific ATA items which are a Header or Title for a set of Sub-ATA's that follow and also contain no values in columns 2 and 3 are identified in BOLD throughout the MEL.

Every ATA item will be shown in the same order as the MMEL.

When an ATA item has multiple deferral options or lines, each deferral will be listed as its own with the same ATA sequence number and item to which it applies. These will also be listed in consecutive order, although circumstances may occur where that item could be listed and then continued to the next page.

Maintenance & Operations Procedures

Each (M) or (O) Procedure can be found in the Appendix of this manual and is identified by ATA system sequence number and name. All procedures are listed in the same order as they are found within the MEL chapters.

All (M) and (O) procedures should be verified by maintenance and crew members that no conflict exists when multiple deferrals are being used.

All (M) and (O) procedures are listed in the same order as the ATA items within the MEL. Items with multiple deferral options will also be listed in the same order and contain their own header to identify with the ATA. For example: an ATA item may have two (C) deferral options listed. The (M) or (O) procedures for each ATA line will also be listed in the same order.



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1. SYSTEM, SEQUENCE NUMBERS & ITEM

21 . AIR CONDITIONING

REPAIR CATEGORY

2.NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4.REMARKS & EXCEPTIONS

20-01 Cabin Overhead Air Outlet

C 10 0 May be inoperative

20-02 Cockpit Overhead Air Outlet


20-03 Cockpit Warm Air Side Console Outlet


20-04 Cold Air Supply Valve (Units -0501 and on)


21-03 Cabin Recirculation Fan (Units -0001 thru -0500)

0 0 Not Installed

*All (M) & (O) Procedures are located in the Appendix of this manual.



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REPAIR CATEGORY

2.NUMBER INSTALLED



21-04 Cockpit Recirculation Fan


21-06 Glareshield Fan

C 2 1 One may be inoperative

21-09 Radio Cabinet Fan (MRC) (Per cabinet) (Units -0001 thru -0500)

0 0 Not Installed

30-01 Cabin Dump Function (Unpressurized)

C 1 0 (M) May be inoperative provided:

a) One outflow valve is removed, andb) Cabin pressurization system is considered inoperative (Refer to item 21-30-02).

30-02 Cabin Pressurization System




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2.NUMBER INSTALLED



30-02-00A (Unpressurized with cabin occupants) (Units -0001 thru -0500)

0 0 Not Installed

30-02-00A (Unpressurized with cabin occupants) (Units -0501 and on)

C 1 0 (O) May be inoperative provided:

a) PRESSURIZATION AUTO/MAN is selected to MANUAL,b) CABIN DUMP is selected to DUMP,c) Aircraft is operated at 13,500 feet cabin altitude or below, andd) Flight crew oxygen system is used above 10,0000 feet through 12,00 feet (MSL) for flights over 30 minutes duration, and over 12,000 at all times.

NOTE: CABIN ALTITUDE amber or red message mayappear at 8,000 feet cabin altitude and CABINALTITUDE aural warning may sound.

30-02-00B (Unpressurized without cabin occupants) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



30-02-00B (Unpressurized without cabin occupants) (Units -0501 and on)

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

a) PRESSURIZATION AUTO/MAN is selected to MANUAL,b) Emergency pressurization system is deactivated,c) CABIN DUMP is selected to DUMP,d) PASS OXY is selected OFF,e) No cabin occupants are carried,f) Aircraft is operated at FL250 or below, andd) Flight crew oxygen system is used above 10,0000 feet through 12,00 feet (MSL) for flights over 30 minutes duration, and over 12,000 at all times.

NOTE: CABIN ALTITUDE amber or red message mayappear at 8,000 feet cabin altitude and CABINALTITUDE aural warning may sound.




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REPAIR CATEGORY

2.NUMBER INSTALLED



30-03 Emergency Pressurization System (Failed closed)

30-03-00A (Units -0001 thru -0500)

0 0 Not Installed

30-03-00A (Units -0501 and on)

C 1 0 May be inoperative provided:

a) L ENG BLD AIR is selected OFF,b) R ENG BLD AIR is selected NORM,c) Aircraft is not operated in known, forecast, or AFM-defined icing conditions, andd) Aircraft is operated at FL250 or below.

NOTE: BLD SEL NOT NORM L message may appear.




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REPAIR CATEGORY

2.NUMBER INSTALLED



30-03-00B (Units -0501 and on)


a) Emergency pressurization system is deactivated,b) Air cycle machine is operative,c) Both left and right bleed sources are operative, andd) Aircraft is operated at FL250 or below.

31-01 Cabin Pressurization Control Panel

31-01-01 Manual Altitude Lever (CABIN ALT)

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




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REPAIR CATEGORY

2.NUMBER INSTALLED



31-01-02 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).

31-01-03 Altitude Selector ("A" Knob) (Units -0001 thru -0500)

0 0 Not Installed

31-01-04 Cabin Pressurization Mode Switch (NORM/ALT SEL) (Units -0001 thru -0500)

0 0 Not Installed

31-01-05 Cabin/Aircraft Altitude Selector Gauge (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



31-01-06 Cabin/Aircraft Altitude Selector Gauge Lighting (Units -0001 thru -0500)

0 0 Not Installed

31-02 Cabin Pressurization System Mode

31-02-01 Automatic Schedule Mode (NORM) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



31-02-01 Automatic Schedule Mode (Units -0501 and on)


a) Altitude select mode is operative,b) MODE is selected to ALTITUDE SELECT on GTC Cabin Pressure Page,c) Cabin differential pressure gauge/indication is operative,d) Cabin altitude gauge/indication is operative,e) Cabin vertical speed gauge/indication is operative,f) Emergency pressurization system is operative, andg) Aircraft is operated at FL410 or below.

31-02-02 Altitude Select Mode (ALT SEL) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



31-02-02 Altitude Select Mode (ALT SEL) (Units -0501 and on)


a) Automatic schedule mode is operative,b) MODE is selected to NORMAL on GTC Cabin Pressure Page,c) Cabin differential pressure gauge/indication is operative,d) Cabin altitude gauge/indication is operative,e) Cabin vertical speed gauge/indication is operative,f) Emergency pressurization system is operative, andg) Aircraft is operated at FL410 or below.

31-02-04 Any Mode (Excluding manual) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



31-02-04 Any Mode (Excluding manual) (Units -0501 and on)


a) PRESSURIZATION AUTO/MAN is selected to MANUAL, andb) Aircraft is operated using manual pressurization.

32-01 Cabin Altitude Gauge/Indication

32-01-00A (Pressurized)


a) Cabin pressurization system automatic schedule mode is operative,b) Cabin differential pressure gauge/indication is operative, andc) A chart is provided to convert differential pressure and aircraft altitude to cabin altitude.




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REPAIR CATEGORY

2.NUMBER INSTALLED



32-01-00B (Unpressurized)


32-01-01 Gauge Lighting (Units -0001 thru -0500)

0 0 Not Installed

32-02 Cabin Differential Pressure Gauge/Indication




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REPAIR CATEGORY

2.NUMBER INSTALLED





a) Cabin altitude gauge/indication is operative,b) Cabin pressurization system automatic schedule mode is operative, andc) A chart is provided to convert cabin and aircraft altitude to differential pressure.



32-03 Cabin Vertical Speed Gauge/Indication




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REPAIR CATEGORY

2.NUMBER INSTALLED





a) Cabin altitude gauge/indication is operative, andb) Cabin pressurization system automatic schedule mode is operative.




0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



33-01 Cabin Outflow Valve


a) One outflow valve is removed, andb) Cabin pressurization system is considered inoperative (Refer to item 21-30-02).

33-02 Pressure Regulating Valve (Mass Flow Control Valve)

33-02-00A (Pressurized) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



33-02-00A (Pressurized) (Units -0501 and on)

C 2 1 (M) One may be inoperative provided:

a) Affected mass flow control valve is secured for no flow,b) PRESS SOURCE SELECT is selected to operative source,c) BAG HEAT is selected OFF, andd) Aircraft is operated at FL410 or below (11 cabin occupants or less) or at FL390 or below (12 cabin occupants).

NOTE: PRESS SRC NOT NORM amber message mayappear.




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REPAIR CATEGORY

2.NUMBER INSTALLED



33-02-00B (Unpressurized) (Units -0501 and on)


a) Both mass flow control valves are secured for no flow,b) PRESS SOURCE SELECT is selected OFF,c) BAG HEAT is selected OFF,d) Cockpit and cabin temperature control systems are considered inoperative (Refer to item 21-60-01), ande) Cabin pressurization system is considered inoperative (Refer to item 21-30-02).


33-02-00B (Unpressurized) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



40-01 Baggage Heat System (Failed closed) (Units -0001 thru -0500)

0 0 Not Installed

40-01 Baggage Heat System (Failed closed) (Units -0501 and on)


a) Baggage heat valve is verified closed, andb) BAG HEAT is selected OFF.

50-01 Air Cycle Machine (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-01 Air Cycle Machine (Units -0501 and on)


a) PRESS SOURCE SELECT is selected OFF,b) APU BLEED AIR is selected OFF,c) Both mass flow valves are verified closed,d) Cockpit and cabin temperature control systems are considered inoperative (Refer to item 21-60-01),e) Cabin pressurization system is considered inoperative (Refer to item 21-30-02), andf) Aircraft is operated in accordance with AFM temperature limitations.





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REPAIR CATEGORY

2.NUMBER INSTALLED



60-01 Cockpit and Cabin Temperature Control System

60-01-00 (Unpressurized)


60-01-01 Automatic Mode


a) Associated temperature control system manual mode is used, andb) APU MAX COOL is selected OFF.

60-01-02 Manual Mode

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




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REPAIR CATEGORY

2.NUMBER INSTALLED



61-01 Cabin Temperature Remote Control (Units -0001 thru -0500)

0 0 Not Installed

61-01 Cabin Temperature Remote Control (Units -0501 and on)

D 1 0 May be inoperative provided CABIN CONTROL is not selected on GTC Temperature Page.

61-02 Temperature Control Panel (Units -0001 thru -0500)

0 0 Not Installed

61-02-01 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).




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REPAIR CATEGORY

2.NUMBER INSTALLED



61-02-02 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).

61-02-03 Temperature Display

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

62-01 Temperature Indication System

62-01-01A Cabin (With cabin occupants)

C 1 0 (O) May be inoperative provided alternate means are established and used to determine cabin temperature.




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REPAIR CATEGORY

2.NUMBER INSTALLED



62-01-01B Cabin (Without cabin occupants)


62-02 Cockpit


62-03 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), andb) Associated DUCT O'TEMP amber message is monitored during temperature adjustment.

70-01 Water Separator

C 1 0 May be inoperative provided Air Cycle Machine (ACM) is considered inoperative (Refer to item 21-50-01).




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22 . AUTO FLIGHT

REPAIR CATEGORY

2.NUMBER INSTALLED



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




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22 . AUTO FLIGHT

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-01 Left Control Wheel

B 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) 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, ande) Approach minimums do not require use of autopilot system.




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22 . AUTO FLIGHT

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-02 Right Control Wheel

B 1 0 May be inoperative provided:

a) Left control wheel button is operative,b) 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, andd) Approach minimums do not require use of autopilot system.

10-02 Autopilot Interrupt/Flight Director Sync Button (TCS) (Units -0001 thru -0500)

0 0 Not Installed




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22 . AUTO FLIGHT

REPAIR CATEGORY

2.NUMBER INSTALLED



10-02 Autopilot Interrupt/Flight Director Sync Button (CWS) (Units -0501 and on)


10-03 Autopilot System (Units -0001 thru -0500)

10-03-00A (Single channel failed)

C 2 1 (M) One may be inoperative provided associated autopilot channel is deactivated.




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10-03-00B (Both channels failed)

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, andd) Aircraft is not operated RVSM.

10-03 Autopilot System (Units -0501 and on)


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, andd) Aircraft is not operated RVSM.




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2.NUMBER INSTALLED



10-04 Takeoff/Go-Around Button (TOGA)

10-04-00A Takeoff/Go-Around Button (TOGA)

C 2 1 One may be inoperative.

10-04-00B Takeoff/Go-Around Button (TOGA)


a) Flight director is not used during takeoff or go-around,b) Autopilot system is disconnected for go-around, andc) Autopilot interrupt/flight director sync button is operative on pilot-flying side.

NOTE: FMS missed approach procedure must bemanually advanced.




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10-05 Yaw Damper (Units -0001 thru -0500)

0 0

10-05-00A (Single channel failed)


a) Associated yaw damper is deactivated, andb) Associated autopilot channel is considered inoperative (Refer to item 22-10-03-00A).

10-05-00B (Both channels failed)


a) Yaw dampers are deactivated, andb) Autopilot system is considered inoperative (Refer to item 22-10-03-00B).




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2.NUMBER INSTALLED



10-05 Yaw Damper (Units -0501 and on)


a) Yaw damper is deactivated, andb) Autopilot system is considered inoperative (Refer to item 22-10-03).

13-01 Flight Guidance Controller Annunciator (GP-400) (Failed to illuminate) (Units -0001 thru -0500)

13-01 Flight Guidance Controller Annunciator (GMC 7200) (Failed to illuminate) (Units -0501 and on)




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13-01-01 Altitude (ALT button)

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

13-01-03 Approach (APPR button)


13-01-04 Autopilot (AP button - A or B annunciation) (Units -0001 thru -0500)

0 0 Not Installed

13-01-04 Autopilot (AP button) (Units -0501 and on)


a) AP annunciation appears in PFD flight director mode box, andb) Associated AP FAIL white message does not appear.




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2.NUMBER INSTALLED



13-01-05 Back Course (BC button)


13-01-05 Back Course (B/C button)


13-01-06 IAS/Mach Change-over (C/O button) (Units -0001 thru -0500)

0 0 Not Installed

13-01-07 Coupled Side (PFD Button - left or right arrow) (Units -0001 thru -0500)

0 0 Not Installed




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2.NUMBER INSTALLED



13-01-07 Coupled Side (CPL Button - left or right arrow) (Units -0501 and on)

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

13-01-08 Flight Director (FD button) (Units -0001 thru -0500)

0 0 Not Installed

13-01-09 Flight Level Change (FLC button)


13-01-10 Half Bank (BANK button)

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




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2.NUMBER INSTALLED



13-01-11 Heading (HDG button)


13-01-12 Navigation (NAV button)


13-01-13 Vertical Navigation (VNAV button)


13-01-14 Vertical Speed (V/S button) (Units -0001 thru -0500)

0 0 Not Installed




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13-01-14 Vertical Speed (VS button) (Units -0501 and on)


13-01-15 Yaw Damper (YD button - A or B annunciation) (Units -0001 thru -0500)

0 0 Not Installed

13-01-15 Yaw Damper (YD button) (Units -0501 and on)

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

13-02 Flight Guidance Controller Function Control (GP-400) (Units -0001 thru -0500)

0 0




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13-02 Flight Guidance Controller Function Control (GMC 7200) (Units -0501 and on)

13-02-01 Altitude (ALT button)


a) Procedures do not require its use, andb) Aircraft is not operated RVSM.

13-02-02 Approach (APPR button)

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

13-02-03 Autopilot (AP button)

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




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2.NUMBER INSTALLED



13-02-04 Back Course (BC button) (Units -0001 thru -0500)

0 0 Not Installed

13-02-04 Back Course (B/C button) (Units -0501 and on)

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

13-02-05 IAS/Mach Change-over (C/O Button) (Units -0001 thru -0500)

0 0 Not Installed

13-02-06 Coupled Side (CPL button) (Units -0501 and on)

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

13-02-06 Coupled Side (PFD button) (Units -0001 thru -0500)

0 0 Not Installed

13-02-07 Course (CRS1 or CRS2 knob) (Units -0001 thru -0500)

0 0 Not Installed

13-02-07 Course (L CRS or R CRS knob) (Units -0501 and on)

B 2 1 One may be inoperative provided procedures do not require its use.




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2.NUMBER INSTALLED



13-02-08 Course Direct (CRS1 or CRS2 PUSH DCT) (Units -0001 thru -0500)

0 0 Not Installed

13-02-08 Course Direct (L CRS or R CRS PUSH DIR) (Units -0501 and on)


13-02-09 Flight Director (FD button)

B 2 1 One may be inoperative provided button is operative on pilot-flying side.

13-02-10 Flight Level Change (FLC button)


13-02-11 Half Bank (BANK Button)





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13-02-13 Heading Sync (HDG PUSH SYNC)


13-02-14 Navigation (NAV Button)

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

13-02-15 Pitch Wheel (Units -0001 thru -0500)

0 0 Not Installed

13-02-16 Vertical Navigation (VNAV button)


13-02-17 Vertical Speed (V/S button) (Units -0001 thru -0500)

0 0 Not Installed




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13-02-17 Vertical Speed (VS button) (Units -0501 and on)


13-02-18 Yaw Damper (YD Button)

C 1 0 NOTE 1: Yaw damper may be engaged by engagingautopilot.NOTE 2: Yaw damper may be disengaged bypressing autopilot disconnect button.

13-03 Pedestal Autopilot Pitch Wheel (Units -0001 thru -0500)

0 0 Not Installed

20-01 Mach Trim System

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




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2.NUMBER INSTALLED



30-01 Autothrottle System (Units -0501 and on)


a) Autothrottle system is deactivated, andb) Procedures do not require its use.

30-01-01A Throttle Disengage Button (A/T DISC)

B 2 1 One may be inoperative.

30-01-01B Throttle Disengage Button (A/T DISC)


a) Autothrottles are disengaged using throttle engage button, andb) Autothrottles are disengaged below 500 ft AGL.




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2.NUMBER INSTALLED



30-01-01C Throttle Disengage Button (A/T DISC)

C 2 0 May be inoperative provided autothrottle system is considered inoperative (Refer to item 22-30-01).

30-01-02A Throttle Engage Button (A/T)

C 2 0 May be inoperative provided autothrottle system is considered inoperative (Refer to item 22-30-01).

30-01-02B Throttle Engage Button (A/T)





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REPAIR CATEGORY

2.NUMBER INSTALLED



0-01 Flight Phone / SATCOM System

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

0-01-01 Cockpit Handset


0-01-02 Cabin Handset

D 1 0 May be inoperative

0-01-03 Antenna/Jack (For portable device)

D 1 0 May be inoperative.




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REPAIR CATEGORY

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10-01 High Frequency (HF) Communication System

10-01-00A (LRCS not required)

D 1 0 May be inoperative provided crew determines they do not require the use of an HF system.




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REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-00B (LRCS required)

C 1 1 (O) One may be inoperative while conducting operations that require two long-range communication systems (LRCS) provided:

a) SATCOM voice or data link operates normally,b) Alternate procedures are established and used,c) SATCOM coverage is available over intended route of flight, andd) If SATCOM Voice is to be used over the intended route of flight, SATCOM Voice short codes (INMARSAT) or direct dial commercial numbers (IRIDIUM) must be available, prior coordination with appropriate ATS (FIR) facility is required.

NOTE: SATCOM voice is to be used only as abackup to normal HF communications.




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2.NUMBER INSTALLED



12-01 Very High Frequency (VHF) Communication System

D 2 0 Two communication systems appropriate to the ground facilities to be used must be operative for the following:

a) IFR Operations, orb) Extended Over Water Operations.

One communication System appropriate to the ground facilities to be used must be operative for the following:

a) VFR, VFR Night, or VFR Over-the- Top conditions.b) Wherever Air traffic Control is being exercised.

NOTE 1: When operated under Part 91, andwithout passengers, the aircraft may berelocated from a place where repairs orreplacement cannot be made to a place wherethey can be made, if not more than one ofeach of the dual radio communication andnavigational equipment requirementsmalfunctions or becomes inoperative.NOTE 2: The appropriate system may beinoperative provided it is not powered by theEmergency AC Bus, Emergency DC Bus, BatteryBus, Battery Direct Bus, or the DC TransferBus and not required for emergencyprocedures.




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12-01-01 VHF Datalink (VDL) (Units -0501 and on)


12-01-02 Communications Management Function (CMF) (Units -0001 thru -0500)

0 0 Not Installed



20-01 Satellite Datalink Service

20-01-01 Radio

0 0 Not Installed




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20-01-02A Weather

0 0 Not Installed

20-01-02B Weather

0 0 Not Installed

20-01-03 Internet

0 0 Not Installed


0 0 Not Installed

20-02 Ground Avionics/Diagnostics Wi-Fi System (Units -0501 and on)

D 1 0 (M) May be inoperative provided system is deactivated.

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

20-03-00A Selective Call (SELCAL) (System or individual channel)





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20-03-00B Selective Call (SELCAL) (System or individual channel)

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

20-04 SMS Text Message System (Units -0501 and on)


40-01 Automatic Cabin Briefer


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


40-02-01 Nose Wheel Well Headset Jack





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REPAIR CATEGORY

2.NUMBER INSTALLED



40-02-02 Tailcone Headset Jack (On APU control panel)


40-03 Passenger Address (PA) System


40-04 Passenger Seat Belt / Safety Chime


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

50-01 Audio Panel (Per side) (Units -0001 thru -0500)

0 0




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-01-01 Microphone Selector (COM 1, COM 2, HF 1, HF 2, PAGE, CABIN Button)

C 1 - Individual selectors may be inoperative provided the associated communication system is not required for the intended flight, otherwise the deferral for the appropriate system must also be used.

NOTE: Reference 23-12-01 for COMM deferralrequirements and 23-10-01 for HF deferralrequirements.

50-01-02 Audio Selector / Volume Control (COM 1, COM 2, HF 1, HF 2, NAV 1, NAV 2, ADF 1, ADF 2, DME 1, DME 2, MLS 1, ML2 2, MKR)

C 1 - Individual selectors may be inoperative provided the associated communication system is not required for the intended flight, otherwise the deferral for the appropriate system must also be used.

NOTE: Reference 23-12-01 for COMM deferralrequirements and 23-10-01 for HF deferralrequirements.




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-01-03 Marker Beacon Mute (MUTE)


50-02 Cabin / Observer Intercom System


50-02-01 Switch / Headphone Jack Panel


50-02-02 Cockpit Audio Control Switch (CABIN INTERCOM) (Units -0001 thru -0500)

0 0 Not Installed

50-02-03 Refreshment Center Audio Panel (AV-850)





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REPAIR CATEGORY

2.NUMBER INSTALLED



50-03 Cockpit Overhead Communication Speaker


a) Affected speaker is not required for procedures, andb) A headset is used for associated inoperative speaker.

50-04 Cockpit Hand Microphone

50-04-00A Cockpit Hand Microphone

C 2 0 May be inoperative provided associated boom microphone is operative.

50-04-00B Cockpit Hand Microphone

D 2 2 Any in excessive the two required hand microphones may be inoperative.




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-04-01 Jack

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

50-04-02 Holder

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




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-05 Cockpit Headset and Boom Microphone

D 2 0 May be inoperative, except when required by 14 CFR, provided both pilot cockpit speakers are operative.

NOTE: 14 CFR requires one operative headsetfor:a) 14 CFR 91 overwater flights (more than 30 minutes or 100 nm from shore).b) 14 CFR 135 extended overwater (more than 50 nm from shore).c) 14 CFR 135 IFR.

50-05-01A Boom Microphone (For a holder of an Air Carrier or Commercial Operator Certficate)

A 2 0 May be inoperative provided:

a) Associated hand microphone is installed and operative, andb) Repairs are made within three flight days.




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-05-01B Boom Microphone (For an operator other than a holder of an Air Carrier or Commercial Operator Certificate)

0 0 Not Applicable

50-02 Headset Earphones / Headphones

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

50-03 Active Noise Reduction (ANR) Function

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

50-04 Powered Headset System (Units -0501 and on)

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




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-06 Cockpit Headset Audio System


a) Both cockpit overhead communication speakers are used, andb) Headset audio system is not required by 14 CFR or procedures.

NOTE: 14 CFR requires one operative headsetfor:a) 14 CFR 91 overwater flights (more than 30 minutes or 100 nm from shore).b) 14 CFR 135 extended overwater (more than 50 nm from shore).c) 14 CFR 135 IFR.

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




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2.NUMBER INSTALLED



50-07-01 Yoke Switch

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

50-07-02 Remote Glareshield Switch

0 0 Not Installed

60-01 Static Wick

60-01-01 Aileron (Each side)

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

60-01-02 Wing Tip Assembly (Each side) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



60-01-03 Winglet (Each side) (Units -0501 and on)


60-01-05 Elevator (Each side)


60-01-08 Rudder

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

70-01 Cockpit Voice Recorder (CVR)




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REPAIR CATEGORY

2.NUMBER INSTALLED



70-01-00A (Holder of an Air Carrier or Commercial Operator Certificate)


a) Any Flight Data Recorder (FDR) required to be installed is operative, andb) Repairs are made within three flight days.

70-01-00B (Operator other than a holder of an Air Carrier or Commercial Operator Certificate)

0 0 Not Applicable

70-01-01 Recorder Independent Power Supply (RIPS)





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REPAIR CATEGORY

2.NUMBER INSTALLED



70-01-02 Underwater Locator Device (ULD)

D 1 0 ULD is required equipment on the CVR when aircraft is operated with 6, or more, passenger seats. Inop ULD is subject to the same deferral as the CVR. The "D" deferral only applies to additional ULD devices that may be installed.

70-01-03A Datalink Recording

C 1 0 May be inoperative provided the aircraft is not required to have a CVR and FDR, and the datalink system was installed prior to April 6, 2012. Otherwise the "A" deferral must be used.

70-01-03B Datalink Recording

A 1 0 May be inoperative provided repairs are made within three flight days.




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REPAIR CATEGORY

2.NUMBER INSTALLED



70-02 Forward-facing Glareshield Camera

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



20-01 Engine AC Generating System

C 2 1 One may be inoperative provided affected windshield anti-ice system is considered inoperative (Refer to item 30-40-02).

30-01 APU DC Generating System (Units -0001 thru -0500)

0 0 Not Installed

30-01 APU DC Generating System (Units -0501 and on)

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

37-01 APU DC Amperage Gauge/Indication (Units -0001 thru -0500)

0 0 Not Installed




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0 0 Not Installed

37-01 APU DC Amperage Gauge/Indication (Units -0501 and on)

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

37-02 APU DC Voltage Gauge/Indication


40-01 External Power System


50-01 AC Cockpit Outlet

50-01-00A AC Cockpit Outlet





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REPAIR CATEGORY

2.NUMBER INSTALLED



50-01-00B AC Cockpit Outlet


60-01 DC Cockpit Outlet

60-01-00A DC Cockpit Outlet

0 0 Not Installed

60-01-00B DC Cockpit Outlet

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



60-03 Interior Disconnect


a) Interior power system is deactivated,b) Cabin emergency lighting is verified operative, andc) Passengers are briefed on disabled cabin electrical systems or are not carried.

NOTE: Items powered by interior bus areconsidered inoperative. This includes, but isnot limited to: Cabin interior lighting,cabin window shade system, galley appliances,galley drain, vanity drain, forward equipmentfan, aft equipment fan, cabin AC inverter,and cabin entertainment system.




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25 . EQUIPMENT/ FURNISHINGS

REPAIR CATEGORY

2.NUMBER INSTALLED



0-01 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.

10-01 Cockpit Assist Handle


10-02 Cockpit Curtain

0 0 Not Installed

10-02-01 Track

0 0 Not Installed

10-03 Cockpit Sunvisor System (Including attach mechanism)

0 0 Not Installed




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2.NUMBER INSTALLED



10-05 Flight Crew Seat (Per seat)

10-05-01A Armrest

C 2 0 May be inoperative provided affected armrest is stowed in retracted position.

10-05-01B Armrest

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

10-05-02 Lumbar Support





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2.NUMBER INSTALLED



10-05-03 Recline/Tilt Function

D 1 0 (M) (O) May be inoperative provided:

a) Affected seat is secured or failed in a position that permits normal visibilty,b) Full flight control movement is available, andc) Crewmember can reach all necessary controls and equipment while restrained.

10-05-04 Restraint Buckle Protective Padding

D 1 0 May be damaged or missing.

10-05-05 Thigh Support

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




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2.NUMBER INSTALLED



10-05-06 Vertical Adjustment

D 1 0 (M) (O) May be inoperative provided:

a) Affected seat is secured or failed in a position that permits pilot normal visibility,b) Full flight control movement is available, andc) Crewmember can reach all necessary controls and equipment while restrained.

10-05-06 Flight Deck Observer's Seat




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2.NUMBER INSTALLED



10-06-00A (Seat not required)

D 1 0 May be inoperative provided:

a) A forward observer's seat on the flight deck, or forward passenger seat with headset or speaker is provided for use by the Administrator while conducting en route inspections.b) Seat is correctly stowed.

NOTE: Pilot-in-command will determine ifminimum safety equipment is functional forother persons authorized to occupy anyobserver seat.




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DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



10-06-00B (Seat required)


a) A passenger seat in passenger cabin is made available to an inspector for performance of official duties,b) Seat is correctly stowed, andc) Repairs are made within two flight days.

10-07 Headset Hook

0 0 Not Installed

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.




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DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



10-09 Yoke-mounted Chart Holder


10-09-01 Light


20-03 Cabin Curtain

0 0 Not Installed

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

D 1 0 May be inoperative provided affected window shades are failed open or in a position that does not interfere with emergency procedures.




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



20-05 Non-essential Equipment and Furnishings (NEF)

- - 0 May be inoperative, damaged or missing provided that item(s) is deferred in accordance with operator’s NEF deferral program. NEF program procedures and processes are outlined in operator’s [manua]. (M) and (O) procedures, if required, must be available to flight crew and included in operator’s appropriate document.

NOTE: Exterior lavatory door ashtray is notconsidered an NEF item.

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


a) Seat does not block an emergency exit,b) Seat does not restrict any cabin occupant access to aisle,c) Affected seat(s) are blocked and placarded “DO NOT OCCUPY”.

NOTE: Affected seat(s) may include seats nearinoperative seat(s).




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



20-06-01 Armrest

D 18 0 May be inoperative or missing and seat occupied provided:

a) Armrest does not block an emergency exit, andb) Armrest does not restrict any cabin occupant from access to aisle.

20-06-02A Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking, swivel, and other positioning controls)

D 9 0 (M) May be inoperative and seat occupied provided seat is secured in taxi, takeoff and landing position.

20-06-02B Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking, swivel, and other positioning controls)

D 9 0 May be inoperative and seat occupied provided control is failed in taxi, takeoff and landing position.

20-06-02C Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking, swivel, and other positioning controls)

D 9 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).




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REPAIR CATEGORY

2.NUMBER INSTALLED



20-06-03 Seat Belt / Shoulder Harness

D 11 0 May be inoperative provided affected seat is placarded "DO NOT OCCUPY FOR TAXI, TAKEOFF, LANDING OR WHEN FASTEN SEAT BELT SIGN IS ILLUMINATED".

20-06-04 Seat Belt / Shoulder Harness Keeper


20-06-05 Lumbar Support


30-01 Refreshment Center Hot Liquid Storage System Heater

C 1 0 (M) May be inoperative provided system is deactivated.

30-02 Refreshement Center Microwave / Oven

D 1 0 (M) May be inoperative provided system is deactivated.




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



40-01 Exterior Lavatory Door Ashtray

A 1 0 May be inoperative in accordance with AD 74-08-09 in its most current revision.

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.

50-01-01 Anchor Plate

0 0 Not Installed

50-02 Cabin Storage Compartment




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-02-00A Cabin Storage Compartment


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, ande) Affected compartment is prominently placarded "DO NOT USE".




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-02-00B Cabin Storage Compartment


a) Affected door is removed,b) Affected compartment is not used for storage of any item, except those permanently affixed,c) Cabin occupants are briefed that affected compartment may not be used, andd) Affected compartment is prominently placarded “DO NOT USE”.

NOTE: Any permanently affixed emergencyequipment located in affected compartment isavailable for use.




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DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



50-02-01 Shelving

D 4 0 (O) May be inoperative provided:

a) Any permanently affixed emergency equipment located on affected shelf is relocated and available for use, andb) Cabin occupants are briefed on location of relocated equipment.

50-02-02 Key Lock

0 0 Not Installed

60-01 Cockpit Smoke Vision System (CSVS)

0 0 Not Installed

60-02 Crash Axe / Survival Tool

0 0 Not Installed




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



60-03 Emergency Medical Equipment

60-03-01 Automatic External Defibrillator (AED) (Includes associated equipment)

0 0 Not Installed

60-03-02 Emergency Medical Kit (EMK) (Includes associated equipment)

0 0 Not Installed

60-03-03 First Aid Kit (FAK) (Includes associated equipment)

D 1 1 May be incomplete, missing, or inoperative, provided at least one First aid kit(s) for treatment of injuries likely to occur in flight or in minor accidents is provided.




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



61-01 Life Preserver (Crew and passenger)

D 11 0 For extended over water flights:

a) An approved life preserver equipped with an approved survivor locator light for each occupant of the aircraft is required.b) The life preserver must be easily accessible to each seated occupant.c) Any seats where a life vest is unavailable should be placarded “Due not Occupy”.

62-01 Emergency Locator Transmitter (ELT)




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DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



62-01-01 Survival Type

D 1 0 May be inoperative or missing provided the unit is not part of the Life Raft required equipment.

62-01-02A Fixed, Automatic

A 1 0 (M) May be inoperative provided:

a) System is deactivated or removed, andb) Repairs are made within 90 calendar days.

62-01-02B Fixed, Automatic

D 1 0 (M) Any in excess of the one ELT required may be inoperative provided system is deactivated or removed.




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



64-01 Life Raft

D 1 0 For extended over water flights:

a) Enough approved life-rafts of a rated capacity and buoyancy to accommodate the occupants of the aircraft, as defined in FAR 135.167 & 25.1415.b) This requires enough life rafts to include the overflow capacity, whould one raft fail.




680-0526REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.26-1


26 . FIRE PROTECTION

REPAIR CATEGORY

2.NUMBER INSTALLED



11-01 Baggage Compartment Smoke Detection System (Units -0001 thru -0500)

0 0 Not Installed

11-01 Baggage Compartment Smoke Detection System (Units -0501 and on)


a) Baggage compartment remains empty (excluding ballast and/or fly away kits), andb) BAG HEAT is selected OFF.

NOTE: Operator's MEL should define whichitems are approved for inclusion in fly awaykits and which materials can be used asballast.NOTE 2: Acceptable items include: EngineInlet 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




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



12-01 APU Fire Detection System

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

13-01 Bleed Leak Detection System (Failed to pass preflight test)

13-01-01 Air Cycle Machine (ACM) (Unpressurized)


a) Air Cycle Machine (ACM) is considered inoperative (Refer to item 21-50-01), andb) APU is considered inoperative (Refer to item 49-20-01).




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



13-01-02 Horizontal Stabilizer


a) Both ANTI-ICE ENGINE/STAB switches are selected OFF,b) Both stabilizer anti-ice valves are verified closed, andc) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

13-01-03 Wing


a) Both ANTI-ICE ENGINE/STAB switches are selected OFF,b) Both ANTI-ICE WING switches are selected OFF,c) Both wing anti-ice valves are verified closed, andd) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



20-01 APU / Baggage Compartment Fire Extinguishing System (Units -0001 thru -0500)

0 0 Not Installed

20-01 APU / Baggage Compartment Fire Extinguishing System (Units -0501 and on)


a) APU is considered inoperative (Refer to item 49-20-01),b) Baggage compartment remains empty (excluding ballast and/or fly away kits), andc) BAG HEAT is selected OFF.

NOTE: Operator's MEL should define whichitems are approved for inclusion in fly awaykits and which materials can be used asballast. See Appendix.

20-02 Baggage Compartment Fire Extinguishing System (Nose MDR Bottle) (Units -0001 thru -0500)

0 0 Not Installed




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DATE:06/02/2014

PAGE NO.26-5



REPAIR CATEGORY

2.NUMBER INSTALLED



20-02 Baggage Compartment Fire Extinguishing System (Nose MDR Bottle) (Units -0501 and on)


a) Baggage compartment remains empty (excluding ballast and/or fly away kits), andb) BAG HEAT is selected OFF.

NOTE 1: If bottle is low or empty, aircraftweight and moment may need to be adjusted.NOTE: Operator's MEL should define whichitems are approved for inclusion in fly awaykits and which materials can be used asballast. See Appendix.




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REVISION:Original

DATE:06/02/2014

PAGE NO.26-6



REPAIR CATEGORY

2.NUMBER INSTALLED



22-01 Portable Fire Extinguisher

D 2 1 At least one hand fire extinguisher must be conveniently located on the flight deck for use by the flight crew, and per FAR 25, aircraft with more than 6 passenger seats, one portable fire extinguisher must be conveniently located in the cabin. Additional installations may be missing, or inoperative, provided:

a) The inoperative fire extinguisher is tagged inoperative, removed from the installed location, and placed out of sight so it can not be mistaken for a functional unit, andb) Required distribution is maintained.




680-0526REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.27-1


27 . FLIGHT CONTROLS

REPAIR CATEGORY

2.NUMBER INSTALLED



11-01 Aileron Trim Tab Position Indicator / Indication (Right-hand) (Units -0005, -0016, -0033, -0050 thru -0500 and Units -0001 thru -0004, -0006 thru -0015, -0017 thru -0032, -0034 thru -0049 incorporating SB680-27 02)

0 0 Not Installed

11-01-01 Trim Position Display Button (RH AILERON TRIM DISPLAY)

0 0 Not Installed




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REVISION:Original

DATE:06/02/2014

PAGE NO.27-2



REPAIR CATEGORY

2.NUMBER INSTALLED



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, andd) Crewmember seated at affected station verifies full control movement and brake application is available while restrained, prior to each flight.

20-01 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.




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REVISION:Original

DATE:06/02/2014

PAGE NO.27-3



REPAIR CATEGORY

2.NUMBER INSTALLED



50-01 Flap Handle Lighting(Units -0001 thru -0500)

0 0 Not Installed

70-02 Control / Gust Lock System(Failed unlocked)

C 1 0 (O) May be inoperative provided pilot verifies full flight control and throttle movement.




680-0526REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.28-1


28 . FUEL

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01 Over-wing Refueling Cap Lock

10-01-00A (Failed unlocked)


10-01-00B (Failed locked)

C 2 0 NOTE: If Single-Point Refueling door lock isalso failed in locked position or SPR systemis inoperative, refueling will not bepossible.

10-02 Single-point Refueling (SPR) System





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DATE:06/02/2014

PAGE NO.28-2


28 . FUEL

REPAIR CATEGORY

2.NUMBER INSTALLED



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 fuel quantity indicating systems are operative, andc) Repairs are made within three flight days.




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REVISION:Original

DATE:06/02/2014

PAGE NO.28-3


28 . FUEL

REPAIR CATEGORY

2.NUMBER INSTALLED



41-02 Fuel Quantity Indicating System(Wing tank)

A 2 1 (O) One 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 RH 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, andh) Repairs are made within three flight cycles.




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REVISION:Original

DATE:06/02/2014

PAGE NO.28-4


28 . FUEL

REPAIR CATEGORY

2.NUMBER INSTALLED



43-01 Fuel Temperature Indication

C 2 1 One may be inoperative provided aircraft is not operated in North Polar Area.




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REVISION:Original

DATE:06/02/2014

PAGE NO.29-1


29 . HYDRAULIC POWER

REPAIR CATEGORY

2.NUMBER INSTALLED



23-01 Auxiliary Hydraulic Pump


a) HYDRAULIC PUMP AUX is selected OFF,b) Aircraft is chocked prior to engine start and prior to engine shutdown following arrival, andc) Parking brake is set as soon as main hydraulic pressure is available.

NOTE: Parking brake is not intended forlong-term parking.




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REVISION:Original

DATE:06/02/2014

PAGE NO.30-1


30 . ICE AND RAIN PROTECTION

REPAIR CATEGORY

2.NUMBER INSTALLED



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


a) Wing/horizontal stabilizer crossover valve is operative,b) Affected valve is secured for no flow,c) Affected ANTI-ICE ENGINE/STAB switch is selected OFF, andd) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

10-04 Wing Bleed Air Anti-Ice System




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DATE:06/02/2014

PAGE NO.30-2



REPAIR CATEGORY

2.NUMBER INSTALLED



10-04-01 Inboard Leading Edge


a) Wing/horizontal stabilizer crossover valve is operative,b) Affected valve is secured for no flow,c) Both ANTI-ICE ENGINE/STAB switches are selected OFF, andd) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

10-04-02 Outboard Leading Edge


a) Affected valve is secured for no flow,b) Both ANTI-ICE WING switches are selected OFF, andc) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.




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REVISION:Original

DATE:06/02/2014

PAGE NO.30-3



REPAIR CATEGORY

2.NUMBER INSTALLED



10-06 Anti-Ice Crossover Valve (Wing / Horizontal Stabilizer) (Units -0001 thru -0500)

0 0 Not Installed

10-06 Anti-Ice Crossover Valve (Wing) (Units -0501 and on)


a) All ANTI ICE ENGINE/STAB and WING switches are selected OFF,b) WING XFLOW is selected OFF, andc) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

20-01 Engine Anti-Ice System


a) Affected valve is secured for no flow,b) Both ANTI-ICE ENGINE/STAB switches are selected OFF, andc) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.




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REVISION:Original

DATE:06/02/2014

PAGE NO.30-4



REPAIR CATEGORY

2.NUMBER INSTALLED



30-01 Angle of Attack (AOA) Heater

30-01-01 Case

C 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions.

30-01-02 Vane

C 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions.




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REVISION:Original

DATE:06/02/2014

PAGE NO.30-5



REPAIR CATEGORY

2.NUMBER INSTALLED



30-03 Pitot Tube Heater (Excluding Standby)

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) The operable pitot heater cockpit indication functions correctly, andd) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.




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REVISION:Original

DATE:06/02/2014

PAGE NO.30-6



REPAIR CATEGORY

2.NUMBER INSTALLED



30-04 Static Port Heater (Excluding Standby)


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, andd) Aircraft is not operated RVSM.

30-05 Temperature Probe Heater (RAT - Two per engine)


a) ENGINE CONTROL FAULT amber message does not appear, andb) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



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 or intended landing.

40-02 Windshield Electric Anti-Ice System


a) Affected windshield anti-ice system is deactivated,b) A means to clear the windshield of moisture is available, andc) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.




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REVISION:Original

DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



40-04 Windshield Rain Repellant

C 1 0 May be inoperative provided aircraft is not operated in precipitation within five nautical miles of airport used for takeoff or intended landing.

40-05 Frost Pane Defog System


70-01 Drain Heater




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REVISION:Original

DATE:06/02/2014

PAGE NO.30-9



REPAIR CATEGORY

2.NUMBER INSTALLED



70-01-01 Aft Vanity Basin


a) Drain heater is deactivated,b) All liquid is removed from basin,c) Basin is placarded "DRAIN HEAT INOP, DO NOT USE", andd) Refreshment center drain heater is considered inoperative (Refer to item 30-70-01-04).




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REVISION:Original

DATE:06/02/2014

PAGE NO.30-10



REPAIR CATEGORY

2.NUMBER INSTALLED



70-01-04 Refreshment Center Drain Heater


a) Drain heater is deactivated,b) Hot liquid storage tank remains empty,c) Hot liquid overfill drain is placarded "DRAIN HEAT INOP, DO NOT USE",d) Ice drawer drain valve remains closed, ande) Aft vanity basin drain heater is considered inoperative (Refer to item 30-70-01-01).




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REVISION:Original

DATE:06/02/2014

PAGE NO.31-1


31 . INDICATING/ RECORDING SYSTEMS

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01 APU Maintenance Panel

10-01-01 ADD OIL Light (Failed lamp test) (Units -0001 thru -0084 not incorporating SB680-49-05)

A 1 0 May be inoperative provided aircraft is operated in accordance with AFM normal limitations for amber ADD OIL light illuminates during preflight test.

10-01-02 LOW OIL Light (Amber) (Units -0001 thru -0084 incorporating SB680-49-05 and Units -0085 and on) (Failed lamp test)

A 1 0 May be inoperative provided aircraft is operated in accordance with AFM normal limitations for amber LOW OIL light illuminates during preflight test.

10-01-02 LOW OIL Light (Red) (Units -0001 thru -0084 not incorporating SB680-49-05) (Failed lamp test)


a) Amber ADD OIL light does not illuminate during preflight test, andb) APU oil level is visually verified.




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DATE:06/02/2014

PAGE NO.31-2



REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-03 APU Oil Test (LAMP TEST or PRE FLT)

C 2 0 May be inoperative provided APU oil level is visually verified.

10-01-04 Emergency Shutoff

C 1 0 May be inoperative provided a crewmember is present in cockpit during APU operation.

10-02 Panel Switch Lights (Failed to illuminate)

10-02-01 ADC Reversion (REVERSION ADC) (Units -0001 thru -0500)

0 0 Not Installed




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DATE:06/02/2014

PAGE NO.31-3



REPAIR CATEGORY

2.NUMBER INSTALLED



10-02-02 Anti-Collision Lights (ANTI-COLL - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-02 Anti-Collision Lights (ANTI-COLL - ON) (Units -0501 and on)

C 1 0 (O) May be inoperative provided anti-collision lights (strobes) are visually verified on prior to each flight.

10-02-03 Anti-Ice Crossflow (WING/STAB XFLOW - XFLOW / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-03 Anti-Ice Crossflow (WING XFLOW - XFLOW / OFF) (Units -0501 and on)


a) Switch functionality is verified operative, andb) A/I WING XFLOW OPEN white and amber messages are monitored.

10-02-04 APU Bleed Air (BLEED AIR - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed




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DATE:06/02/2014

PAGE NO.31-4



REPAIR CATEGORY

2.NUMBER INSTALLED



10-02-04 APU Bleed Air (APU BLEED AIR - ON / OFF) (Units -0501 and on)


a) Switch functionality is verified operative, andb) APU BLD VALVE OPEN amber message and APU BLD VALVE CLOSED white message are monitored.

10-02-05 APU Bleed Valve Open (BLEED VALVE OPEN) (Annunciator) (Units -0001 thru -0500)

0 0 Not Installed

10-02-06 APU Fire (APU FIRE PUSH) (Units -0001 thru -0500)

0 0 Not Installed

10-02-06 APU Fire (APU FIRE) (Units -0501 and on)

C 1 0 May be inoperative provided APU/baggage compartment fire extinguishing system is considered inoperative (Refer to item 26-20-01).




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DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



10-02-07 APU Generator (GENERATOR - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-08 APU Master (MASTER - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-09 APU Ready To Load (READY TO LOAD) (Annunciator only) (Units -0001 thru -0500)

0 0 Not Installed

10-02-10 APU Start (START) (Units -0001 thru -0500)

0 0 Not Installed

10-02-11 APU Stop (STOP) (Units -0001 thru -0500)

0 0 Not Installed




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DATE:06/02/2014

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REPAIR CATEGORY

2.NUMBER INSTALLED



10-02-12 APU Test (APU TEST) (Units -0001 thru -0500)

0 0 Not Installed

10-02-13 Attitude / Heading Reversion (REVERSION ATT/HDG) (Units -0001 thru -0500)

0 0 Not Installed

10-02-14 Auxiliary Hydraulic Pump (HYDRAULIC PUMP AUX - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-14 Auxiliary Hydraulic Pump (HYDRAULIC PUMP AUX - ON / OFF) (Units -0501 and on)


a) Switch functionality is verified operative, andb) HYD AUX PUMP ON white message is monitored.

10-02-15 Avionics Power (L / R AVN - ON / OFF)





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2.NUMBER INSTALLED



10-02-16 Baggage Fire (BAGGAGE FIRE PUSH) (Units -0001 thru -0500)

0 0 Not Installed

10-02-16 Baggage Fire (BAGGAGE FIRE) (Units -0501 and on)

C 1 0 May be inoperative provided APU/baggage compartment fire extinguishing system is considered inoperative (Refer to item 26-20-01).

10-02-17 Baggage Heat (BAGGAGE HEAT - OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-17 Baggage Heat (BAG HEAT - OFF) (Units -0501 and on)

C 1 0 May be inoperative provided baggage heat system is considered inoperative (Refer to item 21-40-01).

10-02-18 Cabin Recirculating Fan (RECIRC AIR CABIN - NORM / HI) (Units -0001 thru -0500)

0 0 Not Installed




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10-02-19 Cabin Temperature Remote Control (CABIN TEMP CONTROL - COCKPIT / CABIN) (Units -0001 thru -0500)

0 0 Not Installed

10-02-20 Cockpit Recirculating Fan (RECIRC AIR CKPT - NORM / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-21 Cockpit Speaker Mute (COCKPIT SPEAKERS - ON / MUTE) (Cyan light) (Units -0001 thru -0500)

0 0 Not Installed

10-02-22 Day / Night (DAY/NIGHT) (Units -0001 thru -0500)

0 0 Not Installed

10-02-23 Display Reversion (DISPLAY REV - NORM / REV) (Units -0501 and on)

C 2 0 (O) May be inoperative provided switch functionality is verified operative.




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2.NUMBER INSTALLED



10-02-24 EICAS (EICAS - LEFT / RIGHT) (Units -0001 thru -0500)

0 0 Not Installed

10-02-25 EICAS Power (EICAS - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-27 Engine / Stabilizer Anti-Ice (ENGINE/STAB - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-27 Engine / Stabilizer Anti-Ice (ENGINE/STAB - ON / OFF) (Units -0501 and on)


a) Switch functionality is verified operative, andb) ANTI-ICE ON ENG/STAB white message is monitored.

10-02-30 Engine Syncronizer (ENGINE SYNC - NORM / OFF) (Units -0001 thru -0500)

0 0 Not Installed




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10-02-31 External Power (EXT PWR - ON / AVAIL)

C 2 0 May be inoperative provided external power system is not utilized.

10-02-32 Fuel Boost (FUEL BOOST - NORM / ON) (Units -0001 thru -0500)

0 0 Not Installed

10-02-32 Fuel Boost (BOOST PUMP - NORM / ON) (Units -0501 and on)


a) Switch functionality is verified operative, andb) FUEL BST PUMP ON L-R white and amber messages are monitored.

10-02-33 Ground Recognition Light (GND RECOG - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed




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10-02-35 Interior Power (INTERIOR - NORM) (Units -0001 thru -0500)

0 0 Not Installed

10-02-35 Interior Power (INTERIOR - ON) (Units -0501 and on)


10-02-36 Landing Light (LDG - ON / OFF) (Cyan light) (Units -0001 thru -0500)

0 0 Not Installed

10-02-36 Landing Light (LDG - ON) (Cyan light) (Units -0501 and on)

C 2 0 May be inoperative provided landing lights are visually monitored.

10-02-37 Max Cool (MAX COOL - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-37 Max Cool (MAX COOL - OFF) (Units -0501 and on)


a) Switch functionality is verified operative, andb) MAX COOL – ON switch light is monitored.




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10-02-38 Navigation Light (NAV - ON / OFF) (Cyan light) (Units -0001 thru -0500)

0 0 Not Installed

10-02-40 Passenger Safety (PAX SAFETY - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-40 Passenger Safety (PAX SAFETY - ON) (Units -0501 and on)

C 1 0 May be inoperative provided passenger safety lights are visually monitored and passenger safety chime is aurally monitored.

10-02-41 Pitot / Static Anti-Ice (PITOT/STATIC - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-41 Pitot / Static Anti-Ice (PITOT/STATIC - ON / OFF) (Units -0501 and on)


a) Switch functionality is verified operative, andb) P/S COLD L-R-STBY white and amber messages are monitored.




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10-02-43 Pulse Light (PULSE - ON / OFF) (Cyan light) (Units -0001 thru -0500)

0 0 Not Installed

10-02-43 Pulse Light (PULSE - ON) (Cyan light) (Units -0501 and on)


10-02-45 Recognition Light (RECOG - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-45 Recognition Light (RECOG - ON) (Units -0501 and on)

C 1 0 May be inoperative provided recognition lights are visually monitored.

10-02-46 Seat Belt (SEAT BELTS - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed




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2.NUMBER INSTALLED



10-02-46 Seat Belt (SEAT BELTS - ON) (Units -0501 and on)

C 1 0 May be inoperative provided seat belt lights are visually monitored and seat belt chime is aurally monitored.

10-02-47 Secondary Baggage Fire (SEC BAG BOTTLE PUSH) (Units -0001 thru -0500)

0 0 Not Installed

10-02-47 Secondary Baggage Fire (SEC BAG BOTTLE) (Units -0501 and on)

C 1 0 May be inoperative provided baggage compartment fire extinguishing system is considered inoperative (Refer to item 26-20-02).

10-02-49 Tail Flood Light (TAIL FLOOD - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed




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10-02-49 Tail Flood Light (TAIL FLOOD - ON) (Units -0501 and on)


10-02-50 Taxi Light (TAXI - ON / OFF) (Cyan light) (Units -0001 thru -0500)

0 0 Not Installed

10-02-50 Taxi Light (TAXI - ON) (Units -0501 and on)


a) Taxi lights are visually monitored, andb) TAXI is selected OFF prior to takeoff.

10-02-52 Windshield Rain Fan (W/S FAN - ON / OFF)


10-02-53 Wing Anti-Ice (WING - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed




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10-02-53 Wing Anti-Ice (WING - ON / OFF) (Units -0501 and on)


a) Switch functionality is verified operative, andb) A/I WING COLD L-R white and amber messages are monitored.

10-02-54 Wing Inspection Light (WING INSP LTS - ON / OFF) (Units -0001 thru -0500)

0 0 Not Installed

10-02-54 Wing Inspection Light (WING INSP - ON) (Units -0501 and on)


a) Switch functionality is verified operative, andb) Wing inspection light is monitored.

20-01 APU Hour Meter

C 1 0 (O) May be inoperative provided APU operation time is tracked by alternate means.




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2.NUMBER INSTALLED



20-02 Clock

D 1 1 One required for dispatch. Any in excess of one may be inoperative.

20-04 Flight Hour Meter

C 1 0 (O) May be inoperative provided flight time is tracked by alternate means.

30-02 Engine Event Marker (Function or EVENT MARKER button)


30-03 Flight Data Recorder

30-03-00A Flight Data Recorder

C 1 0 May be inoperative provided recorder is not installed in an aircraft with a configuration of 10, or more, passenger seats.




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2.NUMBER INSTALLED



30-03-00B (Operator other than a holder of an Air Carrier or Commercial Operator Certificate)

0 0 Not Installed

30-03-00C (Holder of an Air Carrier or Commercial Operator Certificate)


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, orc) 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 repair must be accomplished prior to dispatch, ande) Repairs are made within three flight days.




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2.NUMBER INSTALLED



30-03-01A Flight Data Recorder (FDR) Parameters required by 14 CFR

0 0 Not Installed

30-03-01B Flight Data Recorder (FDR) Parameters not required by 14 CFR

0 0 Not Installed

30-03-02 Underwater Locator Device (ULD)

C 1 0 ULD is required equipment on the CVR when aircraft is operated with 6, or more, passenger seats. Inop ULD is subject to the same deferral as the CVR. The "D" deferral only applies to additional ULD devices that may be installed.

30-04 Quick Access Recorder (QAR)





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REPAIR CATEGORY

2.NUMBER INSTALLED



40-01 Audio Checklist


40-02 Electronic Checklist

D 1 0 May be inoperative, missing, or out of currency provided an approved checklist is available and used.

50-02 Cabin Altitude Warning System


50-03 Central Warning




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2.NUMBER INSTALLED



50-03-01 Master Warning Light (Failed to illuminate)


50-03-02 Master Warning Cancel / Reset Function


50-03-03 Master Caution Light (Failed to illuminate)


50-03-04 Master Caution Cancel / Reset Function


60-01 Cockpit Fold-down Monitor





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REPAIR CATEGORY

2.NUMBER INSTALLED



41-02 Tire Spin Down System (Units -0001 thru -0500)

0 0 Not Installed

44-01 Tire Pressure Monitoring System

D 1 0 NOTE: Any individual wheel sensors which areoperative may be used.




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REPAIR CATEGORY

2.NUMBER INSTALLED



10-01 Cockpit and Instrument Lighting (Excluding button lights, standby flight instrument lighting, internally lighted annunciators, and required placard lighting)

10-01-00A (Day)

C 6 0 May be inoperative provided aircraft is not operated at night.




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2.NUMBER INSTALLED



10-01-00B (Night)

C 6 - 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, andd) Lighting configuration and intensity is acceptable to flight crew.

10-02 Cockpit Flood Light (Units -0001 thru -0500)

0 0




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



10-02-00A (Single light failed)


10-02-00B (Both lights failed)

C 2 0 May be inoperative provided lighting configuration and intensity is acceptable to flight crew.

10-02 Cockpit Flood Light (LED string, 5 elements each) (Units -0501 and on)

C 16 - Individual strings may be inoperative provided lighting configuration and intensity is acceptable to flight crew.

10-03 Cockpit Map Light

10-03-00A (Single light failed)

C 2 1 One may be inoperative provided a cockpit flood light is operative.




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REPAIR CATEGORY

2.NUMBER INSTALLED



10-03-00B (Both lights failed)


a) A cockpit flood light is operative, andb) A flashlight is available to affected crewmember.

10-05 Windshield Ice Detection Light

10-05-00A Windshield Ice Detection Light


10-05-00B Windshield Ice Detection Light

C 2 1 (O) One may be inoperative provided alternate procedures are established and used to monitor ice accretion.




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



20-02 Cabin Interior Lighting (Excluding cabin emergency lighting)

20-02-00A Cabin Interior Lighting (Excluding cabin emergency lighting)

C 16 - (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, andc) Sufficient lighting is operative for carrying cabin occupants at night.

20-02-00B Cabin Interior Lighting (Excluding cabin emergency lighting)

D 16 - (O) May be inoperative provided:

a) Cabin emergency lighting is verified operative, andb) Aircraft is not operated at night or cabin occupants are not carried.

20-03 Entry Lights Timer

C 1 0 May be inoperative provided entry lights are selected OFF when aircraft is vacated.




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REPAIR CATEGORY

2.NUMBER INSTALLED



20-04 Lighted Passenger Information Sign (Excluding cabin exit signs)

20-04-00A (With cabin occupants)


a) Alternate procedures are established and used to notify cabin occupants, andb) Inop NO SMOKING Signs have a complement of NO SMOKING Placards installed in open view of the passengers within the cabin.

20-04-00B (Without cabin occupants)

C 4 0 May be inoperative provided no cabin occupants are carried.




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REPAIR CATEGORY

2.NUMBER INSTALLED



30-01 Aft Baggage Compartment Light


30-01-01 Door Proximity Switch (Failed to extinguish light)

C 1 0 May be inoperative provided BAGGAGE LIGHT switch is selected OFF prior to baggage door closure.

30-02 Tailcone Maintenance Light


40-01 Anti-Collision Light System (Strobe)


a) Position/navigation light system is operative,b) Ground recognition light is operative, andc) Repairs are made within three flight days.

40-01-01 LED Light Assembly (Per light) (LED element) (Units -0001 thru -0500)

0 0 Not Installed




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



40-01-01 LED Light Assembly (Per light) (LED element) (Units -0501 and on)

C 30 24 Up to six elements may be inoperative.

NOTE: Anti-collision light system is stillconsidered operative.

40-02 Ground Recognition Light (Beacon)


40-03 Landing Light

40-03-00A Landing Light


40-03-00B Landing Light

C 2 1 One may be inoperative provided a taxi light is operative.




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



40-03-01 Recognition Light Mode

C 1 0 (O) May be inoperative provided at least one landing light is verified operative for night operations.

40-03-02 Pulse Light Mode

D 1 0 (O) May be inoperative provided at least one landing light is verified operative for night operations.

40-04 Main Cabin Door Step Lights

40-04-00A (Select lights failed)

C 6 3 One may be inoperative on each step.




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



40-04-00B (All lights failed)

C 6 0 May be inoperative provided an alternate source of illumination is available.

40-05 Position / Navigation Light System


40-05-01 LED Wing Light (Per side) (Units -0001 thru -0500)

0 0 Not Installed

40-05-01-01A LED Wing Light (Left – red) (LED element) (Units -0501 and on)

C 14 7 Up to seven elements may be inoperative.

NOTE: Position / navigation light system isstill considered operative.

40-05-01-01B LED Wing Light (Right – green) (LED element) (Units -0501 and on)

C 12 6 Up to six elements may be inoperative.

NOTE: Position / navigation light system isstill considered operative.




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



40-06 Pylon Work Light


40-08 Tail Flood Light


40-09 Taxi Light

40-09-00A Taxi Light


40-09-00B Taxi Light

C 2 0 May be inoperative provided both landing lights are operative.

40-09-00C Taxi Light





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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



40-10 Wing Inspection Light

40-10-00A Wing Inspection Light


40-10-00B Wing Inspection Light

C 2 1 One may be inoperative provided ground deicing procedures do not require its use.

50-01 Cockpit Flashlight

C 2 1 Additional Flashlight installations may be inoperative provided there is one functioning flashlight equipped with at least 2 "D" Cells, or equivalent.




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



50-01-01 Holder

C 2 0 May be inoperative provided associated flashlight is stowed by alternate means.

50-02 Dropped-aisle Lighting System (LED)

50-02-01 Left Forward Half (Emergency Lighting)

C - - Up to four LED elements may be inoperative within any two-foot length.

NOTE: Dropped-aisle lighting system is stillconsidered operative.

50-02-02 Left Aft Half

C - 0 May be inoperative




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33 . LIGHTS

REPAIR CATEGORY

2.NUMBER INSTALLED



50-02-03 Right Aft Half (Emergency Lighting)

C - - Up to four LED elements may be inoperative within any two-foot length.

NOTE: Dropped-aisle lighting system is stillconsidered operative.

50-02-04 Right Forward Half

C - 0 May be inoperative

50-03 Emergency Lighting Battery (CBS 28) (Excluding Pack 1 UF004)


a) Main cabin door exit signs are verified operative,b) Left forward dropped-aisle lighting is verified operative,c) Exterior emergency lights are considered inoperative (Refer to item 33-50-04).d) No cabin occupants are carried, ande) Aircraft is not operated at night.




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REPAIR CATEGORY

2.NUMBER INSTALLED



50-04 Exterior Emergency Light

B 3 0 May be inoperative provided aircraft is not operated at night.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



16-01 Altitude Alerting System

A 2 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, andd) Repairs are made within three flight days.

16-01-01 Aural Alert


a) Visual alert operates normally, andb) Autopilot with altitude hold and capture operates normally.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



16-01-02 Visual Alert


a) Aural alert operates normally, andb) Autopilot with altitude hold and capture operates normally.

18-01 Angle of Attack (AOA) System

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).

18-01-01 Indexer


18-01-03 Stick Shaker

B 2 1 One may be inoperative provider stick shaker on pilot flying side is operative.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



22-01 AHRS Automatic Slaving System (Units -0001 thru -0500)

0 0 Not Installed

25-01 Cursor Control Device (CCD) (Units -0001 thru -0500)

0 0 Not Installed

25-01-01 Display Selection Key (Two inboard keys) (Per side)

C 2 1 One may be inoperative provided two inboard keys are operative on non-failed Cursor Control Device (CCD).

25-01-02 Display Selection Button (Outboard key) (Per side)

C 1 0 NOTE: PFD range in ARC mode cannot beadjusted on failed side.

25-01-03 Enter Button (Per side)


25-01-04 TCAS Button (Per side)

C 1 0 May be inoperative provided TCAS button is operative on opposite Cursor Control Device (CCD).




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



25-01-05 Trackball (Per side)

C 1 0 May be inoperative provided all controls are operative on opposite Cursor Control Device (CCD).

25-01-06 Concentric Control Knobs (Per side)

C 2 0 May be inoperative or knobs may be missing provided Cursor Control Device (CCD) is considered inoperative (Refer to item 34-25-01).

25-02 Display Unit (Copilot PFD – DU4) (Units -0001 thru -0500) (Effective following release of 68FM TC-R11-07, TC-R11-08 and 68CLEAP TC-R11-05)

0 0 Not Installed

25-03 Flight Director System




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



25-03-00A (Single side failed)

C 2 1 One side may be inoperative provided:

a) Command bars are not present on affected side, andb) Approach or departure procedures do not require its use.

25-03-00B (Both sides failed)


a) Command bars are not present,b) Approach or departure procedures do not require its use, andc) Autopilot system is considered inoperative (Refer to item 22-10-03).

25-04 Multi-Function Display (GMX-200) (Units -0001 thru -0500)

0 0 Not Installed




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



25-04-01 Database

A 1 0 May be out-of-date provided aircraft is operated in accordance with applicable AFM limitations.

25-05 Display Controller (DC-840) (Units -0001 thru -0500) (Per side)

0 0

25-05 Display Controller (GCU 275) (Units -0501 and on) (Per side)

25-05-01 Bearing Selector (BRG) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



25-05-02 Minimums Selector (RAD-BARO) (Units -0001 thru -0500)

0 0 Not Installed

25-05-03 Minimums Knob (Units -0001 thru -0500)

0 0 Not Installed

25-05-04 Navigation Source Selector (NAV-PREVIEW-FMS) (Units -0001 thru -0500)

0 0 Not Installed

25-05-05 Timer Control (ET) (Units -0001 thru -0500)

0 0 Not Installed

25-05-06 HSI Mode Selector (HSI) (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



25-05-07 Weather Radar / Terrain Selector (WX/TERR) (Units -0001 thru -0500)

0 0 Not Installed

25-05-08 Barometer Units Selector (IN-HPa) (Units -0001 thru -0500)

0 0 Not Installed

25-05-09 Barometer Standard (PUSH STD)


25-05-10 Radio Altimeter Test (PUSH RAD TEST) (Units -0001 thru -0500)

0 0 Not Installed

25-05-11 Range / Pan Control (Knob) (Units -0501 and on)

C 1 0 May be inoperative provided touchscreen controller left knob for associated display is operative.




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REPAIR CATEGORY

2.NUMBER INSTALLED



25-05-12 Clear (CLR) (Units -0501 and on)


25-05-13 Enter (ENT) (Units -0501 and on)


25-05-14 Cursor / Select (PFD / PUSH ENT) (Units -0501 and on)


25-05-15 Direct To (D>) (Units -0501 and on)


NOTE: Function may be selected on touchscreencontroller.

25-05-16 Flight Plan (FPL) (Units -0501 and on)






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REPAIR CATEGORY

2.NUMBER INSTALLED



25-05-17 Radio Control (COM/NAV) (Units -0501 and on)



25-05-18 Procedure (PROC) (Units -0501 and on)



25-06 Control Display Unit (Right MCDU) (Units -0001 thru -0500)

0 0 Not Installed

25-07 Touchscreen Controller (GTC) (Excluding MFD L) (Units -0501 and on)

C 3 2 (M) One may be inoperative provided controller is deactivated.

NOTE: Any functions or controls that operatenormally may be used.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



25-10 Synthetic Vision (Units -0501 and on)


31-01 Localizer System


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, andd) There is at least 1 operative ILS receiver for IFR operations.

32-01 Glideslope System


a) Procedures do not require its use, andb) There is at least 1 operative ILS receiver for IFR operations.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



34-01 Marker Beacon Receiver System


a) Published approach procedures do not require its use, andb) One marker beacon receiver providing visual and aural signals is available for IFR operations.

36-01 Reactive Windshear System (Includes TAWS windshear mode)





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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



42-01 Weather Radar System


a) Operations are conducted in day VFR conditions, orb) Operations are not conducted in IFR or night VFR conditions when current weather reports indicate that thunderstorms, or potentially hazardous weather conditions that can be detected with airborne weather radar equipment, may reasonably be expected along the route to be flown, orc) Passengers-carrying operations are not being conducted, ord) Aircraft is solely operated within the state of Alaska, within the state of Hawaii, or within the that part of Canada west of Longitude 130 degrees W, between Latitude 70 degrees N, and Latitude 53 degrees N, ore) During any training, test, or ferry flight.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



44-01 Radio Altimeter System

A 1 0 (M) May be inoperative provided:

a) Radio altimeter system is deactivated,b) Approach minimums or operating procedures do not require its use,c) Basic TAWS modes are considered inoperative (Refer to item 34-40-03),d) TCAS II is considered inoperative (Refer to item 34-45-01), ande) Repairs are made within two flight days.

NOTE 1: Landing gear warning system willfunction differently without radio altimeterinput. Landing gear warning may occur athigher altitudes above ground with flapsextended.NOTE 2: Landing Operations Phase Inhibit(LOPI) operation will be affected. LOPI willnot activate during approach or go-around.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



44-02 Surface Awareness System (Runway Awareness and Advisory System RAAS) (Units -0001 thru -0500)

0 0 Not Installed

44-02 Surface Awareness System (SurfaceWatch) (Units -0501 and on)


44-03 Terrain Awareness and Warning System (TAWS) (Including test mode) (Class A or B TAWS required)


a) Alternate procedures are established and used,b) RNP AR procedures are not conducted, andc) Repairs are made within two flight days.

44-03-01 Forward Looking Terrain Avoidance Function and Premature Descent Alert Function

B 2 0 (O) May be inoperative provided alternate procedures are established and used.

44-03-02 Excessive Rate of Descent (Mode 1) and Altitude Loss After Takeoff or Missed Approach (Mode 3)


a) Alternate procedures are established and used, andb) Repairs are made within two flight days.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



44-03-03A Voice Callouts (Mode 6) ("Five-Hundred")

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

44-03-03B Voice Callouts (Mode 6) (Other)


44-03-04A Excessive Closure Rate to Terrain (Mode 2) and Flight Into Terrain Not in Landing Configuration (Mode 4) (Class A TAWS required)


a) Alternate procedures are established and used, andb) Repairs are made within two flight days.

44-03-04B Excessive Closure Rate to Terrain (Mode 2) and Flight Into Terrain Not in Landing Configuration (Mode 4) (Class B TAWS required)

0 0 Not Installed




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



44-03-05 Excessive Downward Glideslope/Glidepath Deviation (Mode 5) (Class B TAWS required)

0 0 Not Installed

44-03-05A Excessive Downward Glideslope/Glidepath Deviation (Mode 5) (Class A TAWS required)

B 1 0 May be inoperative

44-03-05B Excessive Downward Glideslope/Glidepath Deviation (Mode 5) (Class A TAWS required)

C 1 1 May be inoperative provided affected glideslope or glidepath is not used.

44-03-06 Terrain Display (Class B TAWS required)

0 0 Not Installed

44-03-06A Terrain Display (Select display failed) (Class A TAWS required)





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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



44-03-06B Terrain Display (All displays failed) (Class A TAWS required)


44-03-07 Switch (Any excluding TAWS Test) (Class B TAWS required)

0 0 Not Installed

44-03-07A Switch (Flap Override, Terrain Inhibit, Terrain Display Inhibit) (Class A TAWS required)

0 0 Not Installed

44-03-07B Switch (Other excluding TAWS Test) (Class A TAWS required)

0 0 Not Installed




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



44-03-08 Annunciator / Indication (Class B TAWS required)

0 0 Not Installed

44-03-08A Annunciator / Indication (Terrain Inhibited) (Class A TAWS required)


44-03-08B Annunciator / Indication (Other) (Class A TAWS required)


45-01 Traffic Alert and Collision Avoidance System (TCAS II)

45-01-00A Traffic Alert and Collision Avoidance System (TCAS II)


a) System is deactivated, andb) Enroute or approach procedures do not require its use.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



45-01-00B Traffic Alert and Collision Avoidance System (TCAS II)


a) System is deactivated,b) System is not installed on an aircraft with 10, or more, passenger seats; otherwise the "B" deferral is to be used.c) Enroute or approach procedures do not require its use.

45-01-03 Combined Traffic Alert (TA) and Resolution Advisory (RA) Display System (TCAS II only)


a) Affected system is on pilot not flying side,b) TA and RA visual display is operative on pilot flying side, andc) TA and RA audio function is operative on pilot flying side.

45-01-04 Audio Function

B 1 0 May be inoperative provided enroute or approach procedures do not require use of TCAS.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



45-01-05 Airspace Selection Function

0 0 Not Installed

45-02 Traffic Collision Avoidance Device (TCAD)


46-01 Lightning Detection System

D 1 0 May be inoperative provided system is not installed to satisfy the requirements of CFR 135.173 for Thunderstorm Detection Equipment.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



51-01 Distance Measuring Equipment (DME)


a) Aircraft is below FL 240b) Not required for approach, or missed approachc) Operations below FL 240 do not require the use of a DMEd) A suitable RNAV is available.

Reference: CFR 91.205

52-01 ATC Transponder and Automatic Altitude Reporting System

52-01-00A (Select transponders failed)

0 0 Not Installed




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



52-01-00B (All transponders failed)

0 0 Not Installed

52-01-01 Elementary and Enhanced Downlink Aircraft Reportable Parameters (Not required by 14 CFR)

0 0 Not Installed

52-01-02 ADS-B Squitter Transmission (Units -0501 and on)

D 1 0 May be inoperative provided operations do not require their use.

52-03 Transponder Ident Button (XDPR IDENT)





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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



54-01 Very High Frequency Omni Range (VOR) System


a) Affected system is not on an emergency bus,b) Procedures do not require its use, andc) System is not required per the requirements outlined below -

Two navigation systems appropriate to the ground facilities to be used must be operative as follows:

a) When conducting operations under Instrument Flight Rules, orb) When conducting extended overwater operations

One navigation system appropriate to the ground facilities to be used must be operative as follows:

a) When conducting operations under VFR Over-the-Top, orb) When conducting operations under VFR at night, orc) When conducting IFR operations in Class B airspace.




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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



55-01 Automatic Direction Finder (ADF)

D 1 0 May be inoperative provided ADF is not being used in lieu of inoperative VOR equipment on the intended route.

57-01 Global Navigation Satellite System (GNSS) (Including SBAS)


a) System is not being used as one of the two Long-Range Navigation System required for extended over-water or RVSM operations.b) Operations do not require its use.

NOTE 1: Enhanced function of TAWS may not beavailable.NOTE 2: ADS-B output may not be available.

60-01 Data Loader





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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



60-02 Flight Management System (FMS)


a) System is not being used as one of the two Long-Range Navigation System required for extended over-water or RVSM operations.b) Operations do not require its use.

NOTE : Enhanced function of TAWS may not beavailable.

60-02-01 Fuel Planning Function


60-02-02 Takeoff and Landing Data (TOLD) Calculation Function or Database

D 1 0 Function may be inoperative or database may be not loaded.




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DATE:06/02/2014

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34 . NAVIGATION

REPAIR CATEGORY

2.NUMBER INSTALLED



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,c) Approach navigation radios are manually tunes and identified.




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DATE:06/02/2014

PAGE NO.35-1


35 . OXYGEN

REPAIR CATEGORY

2.NUMBER INSTALLED



0-01 Cockpit Oxygen Pressure Gauge / Indication (Aircraft with extended range oxygen system)


a) Associated oxygen bottle is considered inoperative (Refer to item 35-00-02), andb) Non-associated oxygen bottle is operative.

0-01-01 Gauge Lighting (Units -0001 thru -0500 with either oxygen system)

0 0 Not Installed

0-01-02 Low Pressure Light (Units -0001 thru -0500 with extended range oxygen system)

B 2 1 One may be inoperative provided associated cockpit oxygen pressure gauge / indication is operative and monitored.

0-02 Oxygen Bottle (Aircraft with extended range oxygen system)

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, andc) Oxygen duration is computed using only operative bottle.




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DATE:06/02/2014

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35 . OXYGEN

REPAIR CATEGORY

2.NUMBER INSTALLED



0-03 Oxygen System

0-03-01 Fill Port

C 1 0 (M) May be inoperative provided bottle is filled using alternate means, if service is required.

0-03-02 Servicing Panel Pressure Gauge

C 1 0 (M) May be inoperative provided bottle is filled using alternate means, if service is required.

0-03-03 Blowout Disk / Green Label

C 1 0 May be missing or damaged provided oxygen pressure is verified prior to each flight.




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35 . OXYGEN

REPAIR CATEGORY

2.NUMBER INSTALLED



20-01 Passenger Oxygen System

20-01-00A (With cabin occupants)


a) Cabin pressurization system is operative,b) Aircraft is able to decend within 4 minutes to a cabin pressure altitude of 13,000 feet at all points along route to be flown, andc) Aircraft is operated at FL250 or below.

20-01-00B (Without cabin occupants)


a) PASS OXY is selected OFF, andb) No cabin occupants are carried.




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DATE:06/02/2014

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35 . OXYGEN

REPAIR CATEGORY

2.NUMBER INSTALLED



20-01-00C (Unpressurized)

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

20-01-01 Mask

C 9 0 (M) Individual oxygen masks or dispensers may be inoperative or missing provided:

a) Affected mask pintle pin is installed, andb) Associated seat or lavatory is placarded "DO NOT OCCUPY".

20-01-02 Drop-out Panel (Units -0001 thru -0500)

0 0 Not Installed

20-01-02 Drop-out Panel (Decorative cover) (Units -0501 and on)

C 9 0 Individual panels may be missing.




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35 . OXYGEN

REPAIR CATEGORY

2.NUMBER INSTALLED



20-02 Therapeutic Oxygen System


30-01 Portable Oxygen System

D 9 0 May be inoperative provided portable oxygen bottle installation is not a requirement to comply with Part 25 Portable Breathing Equipment, and:

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, andb) Bottles not properly serviced are replaced, serviced, or removed at next available maintenance facility.




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35 . OXYGEN

REPAIR CATEGORY

2.NUMBER INSTALLED



30-02 Protective Breathing Equipment (PBE)

D 2 2 Per 14 CFR Part 25, fixed (stationary, or built in) protective breathing equipment must be installed for use by the flight crew, and one portable protective breathing equipment shall be located at, or near, the flight deck for use by the flight crew. Any equipment above these requirements installed on the aircraft may be inoperative or removed provided location placarding is removed or obscured.

NOTE: Equivalent “fixed” equipment may becrew oxygen masks and smoke goggles, whileequivalent “portable” equipment may beportable oxygen bottles and respiration mask(or similar, as specified in Part 25) withsmoke goggles, unused cabin oxygen masks &smoke goggles, or equipment manufactured toTSO-C116 (as amended).




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DATE:06/02/2014

PAGE NO.36-1


36 . PNEUMATIC

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01 Bleed Air Shutoff Valve

10-01-00A Left (Units -0001 thru -0500)

0 0 Not Installed




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PAGE NO.36-2


36 . PNEUMATIC

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-00A Left (Units -0501 and on)


a) Affected valve is secured for no flow,b) Emergency pressurization system is considered inoperative (Refer to item 21-30-03),c) L ENG BLD AIR is selected OFF,d) BAG HEAT is selected OFF,e) Aircraft is operated at FL250 or below, andf) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

NOTE: BLD SEL NOT NORM L amber message mayappear.

10-01-00B Right (Units -0001 thru -0500)

0 0 Not Installed




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36 . PNEUMATIC

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-00B Right (Units -0501 and on)


a) Affected valve is secured for no flow,b) R ENG BLD AIR is selected OFF,c) BAG HEAT is selected OFF,d) Aircraft is operated at FL300 or below, ande) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

NOTE: BLD SEL NOT NORM R amber message mayappear.

10-01-01A High-pressure (HP) (Units -0001 thru -0500)

0 0 Not Installed




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36 . PNEUMATIC

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-01A High-pressure (HP) (Units -0501 and on)


a) Affected valve is secured for no flow,b) Associated ENG BLD AIR knob is selected to LP,c) Aircraft is not operated in known, forecast, or AFM-defined icing conditions, andd) Aircraft is operated at FL410 or below (11 cabin occupants or less) or at FL390 or below (12 cabin occupants).

NOTE: BLD SEL NOT NORM L-R amber message mayappear.

10-01-01B High-pressure (HP) (Units -0001 thru -0500)

0 0 Not Installed




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36 . PNEUMATIC

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-01B High-pressure (HP) (Units -0501 and on)


a) Both valves are secured for no flow,b) Both ENG BLD AIR knobs are selected to LP,c) BAG HEAT is selected OFF,d) Aircraft is not operated in known, forecast, or AFM-defined icing conditions, ande) Aircraft is operated at FL410 or below.


10-02 Engine Bleed Air Precooler Temperature Control System




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36 . PNEUMATIC

REPAIR CATEGORY

2.NUMBER INSTALLED



10-02-00A Engine Bleed Air Precooler Temperature Control System

B 2 1 (M) One may be inoperative provided:

a) Precooler temperature control system is deactivated,b) Precooler bypass air butterfly valve is secured open,c) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

10-02-00B (Units -0001 thru -0500)

0 0 Not Installed




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36 . PNEUMATIC

REPAIR CATEGORY

2.NUMBER INSTALLED



10-02-00B (Units -0501 and on)


a) Associated ENG BLD AIR is selected OFF,b) Aircraft is operated at FL250 (left failed) / FL410 (right failed) or below, andc) Aircraft is not operated in known, forecast, or AFM-defined icing conditions.





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38 . WATER/WASTE

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01 Potable Water System


a) System is drained, andb) Procedures are established and used to ensure system is not serviced.

10-01-01 Individual Components

C 1 0 (M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, andb) Associated system components are verified not to have leaks.

NOTE: Any portion of system operatingnormally may be used.




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38 . WATER/WASTE

REPAIR CATEGORY

2.NUMBER INSTALLED



30-02 Lavatory External Service System

C 1 0 (M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, andb) Associated system components are verified not to have leaks.

30-02-01A Dump Cable

C 1 0 May be inoperative provided lavatory is not serviced or used.

30-02-01B Dump Cable

C 1 0 (M) May be inoperative provided lavatory is serviced by alternate means.




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38 . WATER/WASTE

REPAIR CATEGORY

2.NUMBER INSTALLED



30-02-08 Heater Gasket


a) Waste line is drained of all fluids,b) Heater gasket is deactivated,c) Refreshment center drain heater is considered inoperative (Refer to item 30-70-01-04), andd) Toilet is not serviced within four hours of landing or at surface temperatures below +10 C.

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, andb) Lavatory is placarded “DO NOT USE”.




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38 . WATER/WASTE

REPAIR CATEGORY

2.NUMBER INSTALLED



30-04 Overboard Drain (Excluding drain heater)

30-04-01 Refreshment Center

C 1 0 May be inoperative provided refreshment center drain heater is considered inoperative (Refer to item 30-70-01-04).

30-04-02 Aft Vanity

C 1 0 May be inoperative provided aft vanity drain heater is considered inoperative (Refer to item 30-70-01-01).




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REVISION:Original

DATE:06/02/2014

PAGE NO.45-1


45 . Central Maintenance Systems

REPAIR CATEGORY

2.NUMBER INSTALLED



0-01 Aircraft Recording System (AReS)


0-02 Central Maintenance System (CMC) (Units -0001 thru -0500)

0 0 Not Installed

0-02 Central Maintenance System (CDMS) (Units -0501 and on)





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DATE:06/02/2014

PAGE NO.46-1


46 . Information Systems

REPAIR CATEGORY

2.NUMBER INSTALLED



0-01 Electronic Flight Bag (EFB) System

0-01-00A Class 3 EFB

0 0 Not Installed

0-01-00B Class 3 EFB

0 0 Not Installed

0-01-01A Data Connectivity (Class 2)

0 0 Not Installed

0-01-01B Data Connectivity (Class 2)

0 0 Not Installed




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DATE:06/02/2014

PAGE NO.46-2


46 . Information Systems

REPAIR CATEGORY

2.NUMBER INSTALLED



0-01-02A Power Connection (Class 1 & 2)

0 0 Not Installed

0-01-02A Power Connection (Class 1 & 2)

0 0 Not Installed

0-01-03A Mounting Device (Class 2)

0 0 Not Installed

0-01-03B Mounting Device (Class 2)

0 0 Not Installed




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REVISION:Original

DATE:06/02/2014

PAGE NO.49-1


49 . Airborne Auxiliary Power

REPAIR CATEGORY

2.NUMBER INSTALLED



20-01 Auxiliary Power Unit (APU)


a) APU is deactivated, andb) Procedures do not require its use.

30-01 APU Fuel Shutoff Valve


a) APU fuel shutoff valve is verified closed, andb) APU is considered inoperative (Refer to item 49-20-01).

50-01 APU Bleed Air Heat Exchanger Fan (Units -0501 and on)

C 1 0 (M) May be inoperative provided heat exchanger fan is deactivated.

50-02 APU Bleed Air System (Units -0001 thru -0500)

0 0 Not Installed




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DATE:06/02/2014

PAGE NO.49-2



REPAIR CATEGORY

2.NUMBER INSTALLED



50-02 APU Bleed Air System (Units -0501 and on)


a) APU BLEED AIR is selected OFF, andb) APU bleed air valve is verified closed.

50-02-01 Max Cool Function (Units -0001 thru -0500)

0 0 Not Installed

50-02-01 Max Cool Function (Units -0501 and on)


a) MAX COOL is selected OFF, andb) APU bleed control valve is verified operative.

70-01 APU Exhaust Gas Temperature (EGT) Display (Units -0001 thru -0500)

0 0 Not Installed




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REPAIR CATEGORY

2.NUMBER INSTALLED



70-01 APU Exhaust Gas Temperature (EGT) Display (Units -0501 and on)


a) APU performed normal start and shutdown on prior use, andb) APU SYS FAIL amber message does not appear during APU start.

70-02 APU Speed (RPM%) Display (Units -0001 thru -0500)

0 0 Not Installed

70-02 APU Speed (RPM%) Display (Units -0501 and on)


a) APU performed normal start and shutdown on prior use, andb) APU SYS FAIL amber message does not appear during APU start.




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DATE:06/02/2014

PAGE NO.52-1


52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01 Main Cabin Door

10-01-01 Key Lock (Failed unlocked)


10-01-02 Precatch


a) Precatch is secured in retracted position,b) Alternate procedures for closing door are established and used.

10-01-03 Acoustic Seal

C 1 0 May be damaged provided seal does not interfere with door operation.




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52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



10-01-04 Primary Seal (Cabin unpressurized)

C 1 0 May be damaged provided:

a) Primary seal does not interfere with door operation, andb) Cabin pressurization system is considered inoperative (Refer to item 21-30-02).

10-01-07 Handrail

C 1 0 (O) May be inoperative or damaged provided:

a) Door operates and latches normally, andb) Alternate procedures are established and used for assisting passengers during entry and exit.

30-01 Aft Baggage Door




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52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



30-01-01A Key Lock (Failed unlocked)

D 1 0 May be inoperative provided door is verified closed and latched prior to each flight.

30-01-01B Key Lock (Failed locked)


a) Baggage compartment smoke detection system is operative,b) APU/baggage compartment fire extinguishing system is operative, andc) Contents and weight of baggage compartment is known.

30-01-02 Door Seal (Units -0001 thru -0500)

0 0 Not Installed




680-0526REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.52-4


52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



30-01-02 Door Seal (Units -0501 and on)

C 1 0 (O) May be damaged provided:

a) Baggage compartment is verified empty prior to each flight, andb) BAG HEAT is selected OFF.

30-01-04 Door Cable

B 2 1 One may be inoperative or missing provided:

a) Affected cable is removed, andb) Door steps are not used.

30-01-05 Gas Spring

C 1 0 (O) May be inoperative or missing provided precautions are taken when opening door.

40-01 Nose Access Door (Per side)




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DATE:06/02/2014

PAGE NO.52-5


52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



40-01-01 Key Lock (Failed unlocked)


42-01 Battery Access Door Key Lock (Failed unlocked)


46-01 Single-point Refueling (SPR) Access Door Key Lock

46-01-00A (Failed unlocked)





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52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



46-01-00B (Failed locked)

C 1 0 NOTE: If over-wing refueling cap locks arealso failed in locked position refueling willnot be possible.

48-01 Tail Cone Access Door Key Lock (Failed unlocked)


50-01 Cockpit Divider Door

C 2 0 (M) May be inoperative provided door is secured open.

50-02 Lavatory Door

C 2 0 (M) May be inoperative provided door is secured open.

70-01 Door Warning System




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DATE:06/02/2014

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52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



70-01-01 Aft Baggage

C 1 0 May be inoperative provided door is verified closed, latched, and locked prior to each flight.

70-01-02 Emergency Exit

C 1 0 May be inoperative provided hatch is verified closed and latched prior to each flight.

70-01-03 Tail Cone Access





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52 . DOORS

REPAIR CATEGORY

2.NUMBER INSTALLED



70-01-04 Lavatory

C 1 0 May be inoperative provided lavatory door is visually verified latched or secured open prior to each taxi, takeoff, or landing.

70-01-05 Nose Access





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53 . FUSELAGE

REPAIR CATEGORY

2.NUMBER INSTALLED



20-01 Vortex Generator (Stinger)

C 8 6 Two may be missing or damaged.

45-01 Life Raft Mooring Ring

D 1 0 May be inoperative or damaged provided life raft is not required by operating rule.

50-01 Radome Erosion Boot

0 0 Not Installed




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DATE:06/02/2014

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55 . STABILIZERS

REPAIR CATEGORY

2.NUMBER INSTALLED



34-01 Vortex Generator

34-01-01 Vertical Stabilizer

C 8 6 Two may be missing or damaged.

34-01-02 Horizontal Stabilizer Wiper Fairing

C 4 0 May be missing or damaged.

44-01 Vortex Generator (Rudder)

C 24 16 Eight may be missing or damaged.




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DATE:06/02/2014

PAGE NO.73-1


73 . ENGINE FUEL & CONTROL

REPAIR CATEGORY

2.NUMBER INSTALLED



33-01 Fuel Flow Indicating System

A 2 1 One may be inoperative provided:

a) Both fuel quantity indicating systems are operative, andb) Repairs are made within three flight days.




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DATE:06/02/2014

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76 . ENGINE CONTROLS

REPAIR CATEGORY

2.NUMBER INSTALLED



1-01 Engine Synchronizer System (Failed off) (Units -0001 thru -0500)

0 0 Not Installed




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77 . ENGINE INDICATING

REPAIR CATEGORY

2.NUMBER INSTALLED



14-01 Engine RPM Gauge / Indication (Units -0001 thru -0500)

0 0

14-01-01 Standby N1

A 2 1 One may be inoperative provided:

a) Standby N2 and standby ITT indicators are operative, andb) Repairs are made within three flight cycles.

14-01-02 Standby N2

C 2 1 One may be inoperative provided standby N1 and standby ITT indicators are operative.




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77 . ENGINE INDICATING

REPAIR CATEGORY

2.NUMBER INSTALLED



22-01 Engine ITT Gauge / Indication (Standby ITT) (Units -0001 thru -0500)

0 0 Not Installed




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DATE:06/02/2014

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78 . ENGINE EXHAUST

REPAIR CATEGORY

2.NUMBER INSTALLED



30-01 Thrust Reverser


a) Affected thrust reverser is deactivated and secured in forward thrust position, andb) Takeoffs on contaminated runways are prohibited.

NOTE: Flight crew should review AFMSingle-Engine Reversing procedure.


Millbrook AviationMINIMUM EQUIPMENT LIST APPENDIX MAINTENANCE &

OPERATIONS PROCEDURES

AIRCRAFT:CE-680 Sovereign

SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.1

ItemNo. Description Category No.Installed No. Req.Dispatch

21-30-01 Cabin Dump Function (Unpressurized)

C 1 0

MAINTENANCE (M)NOTE: This procedure expires upon release of 680 Maintenance Manual revision 20 at which time operators must refer to 680 Maintenance Manual Chapter 21, Dispatch Deviation.

Remove the Cabin Outflow Valve.(1) Remove the primary outflow valve or the secondary outflow valve. Refer to 680 Maintenance Manual Chapter 21, Aft Pressurization Components – Maintenance Practices. (2) Make sure that protective caps or plugs are installed on open tubes and electrical connectors.


21-30-02-00A

(Unpressurized with cabin occupants) (Units -0501 and on)

C 1 0

OPERATIONS (O)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.




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21-30-02-00B

(Unpressurized without cabin occupants) (Units -0501 and on)

C 1 0

MAINTENANCE (M)Pull and secure the EMER PRESSURE (HF040) circuit breaker on the copilot’s circuit breaker panel.

OPERATIONS (O)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.


21-30-03-00B (Units -0501 and on) C 1 0

MAINTENANCE (M)(Units -0001 thru -0500) Pull and secure the EMER PRESSURE (HF026) circuit breaker on the copilot’s circuit breaker panel.

(Units -0501 and on) Pull and secure the EMER PRESSURE (HF040) circuit breaker on the copilot’s circuit breaker panel.




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DATE:06/02/2014

PAGE NO.3


21-32-01-00A (Pressurized) C 1 0

OPERATIONS (O)Use the chart in Appendix A to convert differential pressure and aircraft altitude to cabin altitude.


21-32-02-00A (Pressurized) C 1 0

OPERATIONS (O)Use the chart in Appendix A to convert cabin and aircraft altitude to differential pressure.


21-33-01 Cabin Outflow Valve C 2 0


Remove the Cabin Outflow Valve.(1) Remove the primary outflow valve or the secondary outflow valve. Refer to 680 Maintenance Manual Chapter 21, Aft Pressurization Components – Maintenance Practices. (2) Make sure that protective caps or plugs are installed on open tubes and electrical connectors.




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DATE:06/02/2014

PAGE NO.4


21-33-02-00A (Pressurized) (Units -0501 and on)

C 2 1


Install a Blocking Plate on the Unserviceable Mass Flow Shutoff Valve (Refer to Figure 901).

NOTE: The blocking plate installation on the left and the right mass flow shutoff valves is typical.

(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 mass flow shutoff valve from the ozone converter (upstream of the valve). Refer to 680 Maintenance Manual Chapter 21, Compression - Maintenance Practices.(3) Install the blocking plate on the unserviceable mass flow shutoff valve, between the valve and the ozone converter.(4) Connect the unserviceable mass flow shutoff valve to the ozone converter. Refer to Refer to 680 Maintenance Manual Chapter 21, Compression - Maintenance Practices.




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DATE:06/02/2014

PAGE NO.5


21-33-02-00B (Unpressurized) (Units -0501 and on)

C 2 0


Install a Blocking Plate on the Left and the Right Mass Flow Shutoff Valves (Refer to Figure 901).

NOTE: The blocking plate installation on the left and the right mass flow shutoff valves is typical.

(1) Fabricate two 0.020 inch (0.51 mm) thick blocking plates from Type 301, 1/2-hard stainless steel of the applicable diameter.(2) Disconnect the left and the right mass flow shutoff valves from the left and the right ozone converters (upstream of the valves). Refer to 680 Maintenance Manual Chapter 21, Compression - Maintenance Practices.(3) Install the blocking plate on the left and right mass flow shutoff valves, between the valves and the ozone converters.(4) Connect the left and the right mass flow shutoff valves to the left and the right ozone converters. Refer to Refer to 680 Maintenance Manual Chapter 21, Compression - Maintenance Practices.




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DATE:06/02/2014

PAGE NO.6


21-40-01 Baggage Heat System (Failed closed) (Units -0501 and on)

C 1 0


Make sure that the Baggage Compartment Heat Shutoff Valve is Closed.

(1) Start the left and the right engines. Refer to the Model 680 Approved Airplane Flight Manual.(2) Push the BAG HEAT switch/light on the BAGGAGE panel on the pedestal to the OFF position.(3) Connect the nose and main landing gear simulator test sets to the nose and main landing gear. Refer to 680 Maintenance Manual Chapter 32, Landing Gear - Maintenance Practices.(4) Put the breakout boxes in the IN AIR mode.(5) 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 Test Procedures menu and select Ice Protection System.(d) Find the Baggage Heat Valve Position indication and make sure that the COMMAND/(6) Make sure that no warm air flows from the tailcone warm air ducts in the baggage compartment.

---<CONTINUED ON NEXT PAGE>---




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21-40-01 Baggage Heat System (Failed closed) (Units -0501 and on)

C 1 0

(7) Stop the left and the right engines. Refer to the Model 680 Approved Airplane Flight Manual.(8) Disconnect the nose and main landing gear simulator test sets from the nose and main landing gear. Refer to 680 Maintenance Manual Chapter 32, Landing Gear - Maintenance Practices.


21-50-01 Air Cycle Machine (Units -0501 and on)

C 1 0

OPERATIONS (O)1. Start the left and the right engines. Refer to the Model 680 Approved Airplane Flight Manual. The APU should remain OFF.2. Make sure that no warm air flows from the cabin warm air ducts or the overhead outlets with PRESS SOURCE SELECT selected OFF.


21-62-01-01A Cabin (With cabin occupants)

C 1 0

OPERATIONS (O)Make sure the cabin has been warmed to an acceptable temperature prior to flight. Refer to the Model 680 Approved Airplane Flight Manual. A portable temperature indicating device may be used to determine the temperature.




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DATE:06/02/2014

PAGE NO.8


22-10-01-01 Left Control Wheel B 1 0

OPERATIONS (O)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.


22-10-03-00A (Single channel failed) C 2 1

MAINTENANCE (M)Pull and secure the L AUTOPILOT (HC053) circuit breaker on the pilot’s circuit breaker panel or the R AUTOPILOT (HC056) circuit breaker on the copilot’s circuit breaker panel.


22-10-03-00B (Both channels failed) B 2 0

MAINTENANCE (M)Pull and secure the L AUTOPILOT (HC053) circuit breaker on the pilot’s circuit breaker panel and the R AUTOPILOT (HC056) circuit breaker on the copilot’s circuit breaker panel.


22-10-03 Autopilot System (Units -0501 and on)

B 1 0

MAINTENANCE (M)Pull and secure the AUTOPILOT (HC073) circuit breaker on the pilot’s circuit breaker panel.




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DATE:06/02/2014

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22-10-05-00A (Single channel failed) C 2 1

MAINTENANCE (M)Pull and secure the L YAW DAMP (HC052) circuit breaker on the pilot’s circuit breaker panel or the R YAW DAMP (HC057) circuit breaker on the copilot’s circuit breaker panel.


22-10-05-00B (Both channels failed) B 2 0

MAINTENANCE (M)Pull and secure the L YAW DAMP (HC052) circuit breaker on the pilot’s circuit breaker panel and the R YAW DAMP (HC057) circuit breaker on the copilot’s circuit breaker panel.


22-10-05 Yaw Damper (Units -0501 and on)

B 1 0

MAINTENANCE (M)Pull and secure the AUTOPILOT (HC073) circuit breaker on the pilot’s circuit breaker panel.


22-30-01 Autothrottle System (Units -0501 and on)

C 1 0

MAINTENANCE (M)Pull and secure the AUTO THROTTLE (HC072) circuit breaker on the pilot’s circuit breaker panel.




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DATE:06/02/2014

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23-10-01-00B (LRCS required) C 1 1

OPERATIONS (O)1. Prior to each flight, a crew member shall make sure that SATCOM Data Link and ACARS systems are operational for transmitting and receiving information from a ground station.2. Prior to each flight, a crew member shall review SATCOM system user’s guide/manual to ensure coverage exists for the intended route of flight.3. Prior to flight, a crew member shall coordinate with the appropriate ATC facility to advise of intended flight without INMARSAT codes, if codes are not available.


23-20-02 Ground Avionics/Diagnostics Wi-Fi System (Units -0501 and on)

D 1 0

MAINTENANCE (M)NOTE: It has been determined that deactivation of the system is not necessary. The maintenance procedure requirement will be removed at next revision of the MMEL. No action is needed.


23-20-03-00B Selective Call (SELCAL) (System or individual channel)

C 1 0

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.




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23-40-04 Passenger Seat Belt / Safety Chime

C 1 0

OPERATIONS (O)A crew member must use the PA system from the cockpit to make the appropriate announcements.


23-50-04-02 Holder D 2 0

OPERATIONS (O)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.


23-50-07-01 Yoke Switch B 2 1

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




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24-50-01-00A AC Cockpit Outlet C 2 0

OPERATIONS (O)1. If equipment utilizing the affected power source is battery operated, make sure that adequate battery life is available and backup batteries for intended operating times are available.2. Use alternate cockpit/cabin power source if power source is available and within close proximity.




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DATE:06/02/2014

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24-60-03 Interior Disconnect C 1 0

MAINTENANCE (M)Pull the LEFT INTERIOR FEED BUS (HZ001) fuse in the LH power junction box and the RIGHT INTERIOR FEED BUS (HZ002) fuse in the RH power junction box.

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.




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DATE:06/02/2014

PAGE NO.14


25-0-01 Required Documents Holder (Airworthiness Certificate, Registration,

etc)

D 1 0

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.


25-10-05-01B Armrest C 2 0

MAINTENANCE (M)Using the appropriate seat manual, remove and store the affected armrest(s).

NOTE: Refer to the appropriate Cessna Maintenance Manual and/or seat manual for information of the individual aircraft installation.




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DATE:06/02/2014

PAGE NO.15


25-10-05-03 Recline/Tilt Function D 1 0

MAINTENANCE (M)Using the appropriate seat manual, secure the seat in the desired position.


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


25-10-05-06 Vertical Adjustment D 1 0

MAINTENANCE (M)Using the appropriate seat manual, secure the seat in the desired position.


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




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DATE:06/02/2014

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25-10-08 Eye Reference Ball C 3 0

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.


25-20-06-02A

Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking,

swivel, and other positioning controls)

D 9 0

MAINTENANCE (M)Using the appropriate seat manual, secure the seat in the full upright position.

NOTE: Refer to the appropriate Cessna Maintenance Manual and/or Interiors Manual for information of the individual aircraft installation.




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DATE:06/02/2014

PAGE NO.17


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

C 1 0

MAINTENANCE (M)1. Access the appropriate junction box.2. Pull and secure the appropriate circuit breaker. NOTE: Refer to the appropriate Interiors Manual for information of the individual aircraft installation.


25-30-02 Refreshement Center Microwave / Oven

D 1 0

MAINTENANCE (M)1. Access the appropriate junction box.2. Pull and secure the appropriate circuit breaker. NOTE: Refer to the appropriate Interiors Manual for information of the individual aircraft installation.




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REVISION:Original

DATE:06/02/2014

PAGE NO.18


25-50-02-00A Cabin Storage Compartment C 28 0


Secure the Cabin Storage Compartment Door.(1) Put the cabin storage compartment door in the closed position. CAUTION: Do not use duct tape or other tapes that can contain substances known to cause damage to the furniture finish or leave residues.

(2) Carefully attach sufficient lengths of 3M vinyl tape (or equivalent) across the door opening at a 90-degree angle to make sure that the door does not open during airplane operation.


25-50-02-00B Cabin Storage Compartment C 28 0


Remove the Cabin Storage Compartment Door.(1) Remove the cabin storage compartment door. Refer to the Model 680 Interior Maintenance Manual and Illustrated Parts Catalog.




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DATE:06/02/2014

PAGE NO.19


25-50-02-01 Shelving D 4 0

OPERATIONS (O)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.


25-62-01-02A Fixed, Automatic A 1 0


Isolate the ELT Antenna.(1) Disconnect the ELT antenna coaxial connector adapter from the ELT antenna. Refer to 680 Maintenance Manual Emergency Locator Transmitter (ELT) - Maintenance Practices.(2) Put protective covers on the coaxial connector plug and jack.(3) Stow the coaxial cable.




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25-62-01-02B Fixed, Automatic D 1 0


Isolate the ELT Antenna.(1) Disconnect the ELT antenna coaxial connector adapter from the ELT antenna. Refer to 680 Maintenance Manual Emergency Locator Transmitter (ELT) - Maintenance Practices.(2) Put protective covers on the coaxial connector plug and jack.(3) Stow the coaxial cable.




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PAGE NO.21


26-13-01-02 Horizontal Stabilizer B 1 0


(Units -0001 thru -0500) Make Sure that the Horizontal Stabilizer Anti-Ice Pressure-Regulating Shutoff Valves are Closed. (1) Start the left and the right engines. Refer to the Model 680 Approved Airplane Flight Manual.(2) Make sure that the ENGINE/STAB L-R switch/lights on the right switch panel are in the OFF position.(3) Use the copilot's cursor control device (CCD) to access the Citation Diagnostic Maintenance System on the copilot's multifunction display (MFD). Refer to 680 Maintenance Manual Chapter 45, Citation Diagnostic Maintenance System (CDMS) - Maintenance Practices.(a) On the CDMS screen, select the MAINTENANCE page. NOTE: If the system was just started, it can take up to four minutes for the MAINTENANCE option to be highlighted as the system boots.

(b) Move the cursor to SOVEREIGN DIAGNOSTICS and push the cursor select button on the CCD.(c) Use the right top selector knob on the CCD to highlight the ATA Chapter 30 and push the cursor SELECT button.(d) Select the NC111 L ANTI-ICE PC BOARD display.





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(e) Make sure that the L STAB ANTI-ICE SOV shows CLOSE.(f) Select the NC108 L BLEED AIR MON PC BOARD display.(g) Make sure that the L TAIL LE A/I TEMP SENSOR 1 and 2 show approximately the ambient temperature.(h) Select the NF211 R ANTI-ICE PC BOARD display.(i) Make sure that the R STAB ANTI-ICE SOV shows CLOSE.(j) Select the NF208 R BLEED AIR MON PC BOARD display.(k) Make sure that the R TAIL LE A/I TEMP SENSOR 1 and 2 show approximately the ambient temperature.(4) Stop the left and the right engines. Refer to the Model 680 Approved Airplane Flight Manual. (Units -0501 and on)Make Sure that the Horizontal Stabilizer Anti-Ice Pressure-Regulating Shutoff Valves are Closed(1) Start the left and the right engines. Refer to the Model 680 Approved Airplane Flight Manual.(2) Make sure that the ENGINE/STAB L-R switch/lights on the right switch panel are 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 680 Maintenance Manual 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 Anti-Ice LH - NC111.(d) Scroll until you find the L Stab Anti-Ice SOV indication and make sure that the COMMAND/ STATUS shows Closed.





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(e) In the Live Data View, find the Bleed Air Monitor LH - NC108.(f) Scroll until you find the Tail RTD indications and make sure that they show approximately the ambient temperature.(g) In the Live Data View, find the Anti-Ice RH - NF211.(h) Scroll until you find the R Stab Anti-Ice SOV indication and make sure that the COMMAND/STATUS shows Closed.(i) In the Live Data View, find the Bleed Air Monitor RH - NF208.(j) Scroll until you find the Tail RTD indications and make sure that they show approximately the ambient temperature.(4) Stop the left and the right engines. Refer to the Model 680 Approved Airplane Flight Manual.




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DATE:06/02/2014

PAGE NO.24


27-20-01 Rudder Pedal Adjustment System

B 4 2


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. 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.




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PAGE NO.25


27-70-02 Control / Gust Lock System(Failed unlocked)

C 1 0

OPERATIONS (O)During the flight control check in the Before Taxi checklist, verify both throttles can be moved freely.




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DATE:06/02/2014

PAGE NO.26


28-41-01 Fuel Low Level Indicating System

A 2 1

OPERATIONS (O)1. Flight crew shall brief the loss of low fuel quantity warning system on the affected side.2. Flight crew shall monitor fuel balance during flight to make sure adequate fuel remains in both wing fuel tanks for planned mission.


28-41-02 Fuel Quantity Indicating System(Wing tank)

A 2 1

OPERATIONS (O)1. 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.2. 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. 3. 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. 4. 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.5. Re-engage the autopilot. Monitor the RETRIM L or R WING DOWN amber message.




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DATE:06/02/2014

PAGE NO.27


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

C 2 1


Install a Blocking Plate on the Unserviceable Horizontal Stabilizer Anti-Ice Pressure-Regulating Shutoff Valve (Refer to Figure 901).

NOTE: The blocking plate installation on the left and the right horizontal stabilizer anti-ice pressure-regulating shutoff valves is typical.

(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 bleed air tube upstream from the unserviceable horizontal stabilizer anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Horizontal Stabilizer Leading Edge Anti-Ice System - Maintenance Practices.(3) Install the blocking plate on the unserviceable horizontal stabilizer anti-ice pressure-regulating shutoff valve, between the valve and the bleed air tube.(4) Connect the bleed air tube to the unserviceable horizontal stabilizer anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Horizontal Stabilizer Leading Edge Anti-Ice System – Maintenance Practices.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.28


30-10-04-01 Inboard Leading Edge C 2 1


Install a Blocking Plate on the Unserviceable Wing Anti-Ice Pressure-Regulating Shutoff Valve (Refer to Figure 902).

NOTE: The blocking plate installation on the left and the right wing anti-ice pressure-regulating shutoff valves is typical.

(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 bleed air tube upstream from the unserviceable wing anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Wing Leading Edge Anti-Ice System - Maintenance Practices.(3) Install the blocking plate on the unserviceable wing anti-ice pressure-regulating shutoff valve, between the valve and the bleed air tube.(4) Connect the bleed air tube to the unserviceable wing anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Wing Leading Edge Anti-Ice System - Maintenance Practices.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.29


30-10-04-02 Outboard Leading Edge C 2 0


Install a Blocking Plate on the Unserviceable Outboard Wing Anti-Ice Pressure-Regulating Shutoff Valve (Refer to Figure 902).

NOTE: The blocking plate installation on the left and the right outboard wing anti-ice pressure-regulating shutoff valves is typical.

(5) Fabricate a 0.020 inch (0.51 mm) thick blocking plate from Type 301, 1/2-hard stainless steel of the applicable diameter.(6) Disconnect the bleed air tube upstream from the unserviceable outboard wing anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Wing Leading Edge Anti-Ice System - Maintenance Practices.(7) Install the blocking plate on the unserviceable outboard wing anti-ice pressure-regulating shutoff valve, between the valve and the bleed air tube.(8) Connect the bleed air tube to the unserviceable outboard wing anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Wing Leading Edge Anti-Ice System - Maintenance Practices.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.30


30-20-01 Engine Anti-Ice System C 2 1


Install a Blocking Plate on the Unserviceable Engine Air Inlet Anti-Ice Pressure-Regulating Shutoff Valve (Refer to Figure 903).

NOTE: The blocking plate installation on the left and the right engine air inlet anti-ice pressure-regulating shutoff valves is typical.

(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 bleed air tube upstream from the unserviceable engine air inlet anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Engine Air Inlet Anti-Ice - Maintenance Practices.(3) Install the blocking plate on the unserviceable engine air inlet anti-ice pressure-regulating shutoff valve, between the valve and the bleed air tube.(4) Connect the bleed air tube to the unserviceable engine air inlet anti-ice pressure-regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 30, Engine Air Inlet Anti-Ice - Maintenance Practices.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.31


30-40-02 Windshield Electric Anti-Ice System

C 2 1

MAINTENANCE (M)(Units -0001 thru -0500): Pull and secure the L WSHLD ANTI-ICE (HC003) circuit breaker on the pilot’s circuit breaker panel or the R WSHLD ANTI-ICE (HF010) circuit breaker on the copilot’s circuit breaker panel.

(Units -0501 and on): Pull and secure the L W/S ANTI-ICE (HC041) circuit breaker on the pilot’s circuit breaker panel or the R W/S ANTI-ICE (HF059) circuit breaker on the copilot’s circuit breaker panel.


30-70-01-01 Aft Vanity Basin C 1 0

MAINTENANCE (M)Pull and secure the DRAIN HEATERS (CB111V) circuit breaker on the aft interior junction box.


30-70-01-04 Refreshment Center Drain Heater

C 1 0

MAINTENANCE (M)Pull and secure the DRAIN HEATERS (CB111V) circuit breaker on the aft interior junction box.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.32


31-10-02-02 Anti-Collision Lights (ANTI-COLL - ON) (Units -0501 and on)

C 1 0

OPERATIONS (O)1. During the Cockpit/Cabin Inspection: Exterior Lights procedure, press the ANTI-COLL switch.2. Visually verify the anti-collision lights illuminate.3. Press the switch again, verify the lights extinguish.


31-10-02-03 Anti-Ice Crossflow (WING XFLOW - XFLOW / OFF) (Units -0501 and on)

C 2 0

OPERATIONS (O)1. During the Before Takeoff: Anti-Ice Systems procedure, press the WING XFLOW switch.2. Verify the A/I WING XFLOW OPEN white message appears.3. Press the switch again, verify the message(s) extinguishes.


31-10-02-04 APU Bleed Air (APU BLEED AIR - ON / OFF) (Units -0501 and on)

C 2 0

OPERATIONS (O)1. Following the Cockpit Preparation: APU start procedure, press the APU BLEED AIR switch.2. Verify the APU BLD VALVE CLOSE white message extinguishes.3. Press the switch again, verify the message appears.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.33


31-10-02-14

Auxiliary Hydraulic Pump (HYDRAULIC PUMP AUX - ON / OFF) (Units -0501 and

on)

C 2 0

OPERATIONS (O)1. During the Before Start procedure, press the HYDRAULIC PUMP AUX switch.2. Verify the AUX HYDRAULIC PUMP ON white message appears.3. Press the switch again, verify the message(s) extinguishes.


31-10-02-23 Display Reversion (DISPLAY REV - NORM / REV) (Units -0501 and on)

C 2 0

OPERATIONS (O)1. With avionics on, press the affected DISPLAY REV switch.2. Verify the associated PFD and MFD enter reversionary mode.3. Press the DISPLAY REV switch again.4. Verify the associated PFD and MFD return to normal mode.


31-10-02-27

Engine / Stabilizer Anti-Ice (ENGINE/STAB - ON / OFF) (Units -0501

and on)

C 4 0

OPERATIONS (O)1. During the Before Takeoff: Anti-Ice Systems procedure, press the affected ENGINE/STAB switch.2. Verify the associated ANTI-ICE ON ENG/STAB and/or A/I ENGINE COLD white messages appear.3. Press the switch again, verify the message(s) extinguishes.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.34


31-10-02-32 Fuel Boost (BOOST PUMP - NORM / ON) (Units -0501 and on)

C 4 0

OPERATIONS (O)1. Following engine start, press the affected BOOST PUMP button.2. Verify the associated FUEL BST PUMP ON L-R white message appears.3. Press the switch again.4. Verify the message extinguishes.


31-10-02-35 Interior Power (INTERIOR - ON) (Units -0501 and on)

C 1 0

OPERATIONS (O)1. With main DC power active, press the INTERIOR button.2. Verify the OFF annunciator illuminates.3. Verify items on the INTERIOR bus, such as downwash lighting, are inoperative.4. Press the INTERIOR button again.5. Verify the OFF annunciator extinguishes.6. Verify the same interior items are now operative.


31-10-02-37 Max Cool (MAX COOL - OFF) (Units -0501 and on)

C 1 0

OPERATIONS (O)1. Following the Cockpit Preparation: APU start procedure, press the MAX COOL switch.2. Verify the operative MAX COOL ON switch light illuminates.3. Press the switch again, verify the switch light extinguishes.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.35


31-10-02-41 Pitot / Static Anti-Ice (PITOT/STATIC - ON / OFF) (Units -0501 and on)

B 4 0

OPERATIONS (O)1. During the Cockpit/Cabin Inspection: Anti-Ice PITOT/STATIC check, press the affected PITOT/STATIC switch.2. Externally verify the associated pitot and static heaters are heating.3. Verify the associated P/S COLD L-R-STBY white message appears briefly and then extinguishes.


31-10-02-52 Windshield Rain Fan (W/S FAN - ON / OFF)

C 2 0

OPERATIONS (O)1. Following the Cockpit/Cabin Inspection: Batteries On procedure, press the W/S FAN switch.2. Audibly verify the nose compartment blower turns on.3. Press the switch again, verify the blower turns off.


31-10-02-53 Wing Anti-Ice (WING - ON / OFF) (Units -0501 and on)

C 4 0

OPERATIONS (O)1. During the Before Takeoff: Anti-Ice Systems procedure, press the affected WING switch and both ENGINE/STAB switches.2. Verify the ANTI-ICE ON ALL white messages appears and/or associated A/I WING COLD white message appears briefly.3. Press the switch again, verify the message(s) extinguishes.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.36


31-10-02-54 Wing Inspection Light (WING INSP - ON) (Units -0501 and on)

C 1 0

OPERATIONS (O)1. During the Cockpit/Cabin Inspection: Exterior Lights procedure, press the WING INSP switch.2. Visually verify the wing inspection lights illuminate.3. Press the switch again, verify the lights extinguish.


31-20-01 APU Hour Meter C 1 0

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").


31-20-04 Flight Hour Meter C 1 0

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").




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.37


33-10-05-00B Windshield Ice Detection Light

C 2 1

OPERATIONS (O)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.


33-20-02-00A Cabin Interior Lighting (Excluding cabin emergency lighting)

C 16 -



33-20-02-00B Cabin Interior Lighting (Excluding cabin emergency lighting)

D 16 -





SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.38


33-20-04-00A (With cabin occupants) C 4 0

OPERATIONS (O)A crew member will use the PA system or turn and face the cabin occupants to make appropriate announcements.


33-40-03-01 Recognition Light Mode C 1 0

OPERATIONS (O)During the Preliminary Exterior Inspection, verify at least one landing light is operative.


33-40-03-02 Pulse Light Mode D 1 0

OPERATIONS (O)During the Preliminary Exterior Inspection, verify at least one landing light is operative.


33-50-03 Emergency Lighting Battery (CBS 28) (Excluding Pack 1 UF004)

B 3 0

OPERATIONS (O)1. With both batteries off and no generators running, select EMER LTS to ON.2. Quickly verify the main cabin door EXIT signs and the left forward dropped aisle lighting are operative.3. Select EMER LTS to OFF.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.39


34-16-01 Altitude Alerting System A 2 0

OPERATIONS (O)1. Crew briefings must include a reminder that the Altitude Alerting System is inoperative.2. The flight crew will use aural callouts pertaining to approach target altitudes as assigned by ATC or depicted on approach charts.


34-25-07 Touchscreen Controller (GTC) (Excluding MFD L) (Units -0501 and on)

C 3 2

MAINTENANCE (M)Pull and secure the L PFD GTC (HC070) circuit breaker on the pilot’s circuit breaker panel, the R PFD GTC (HF069) circuit breaker on the copilot’s circuit breaker panel, or the MFD R GTC (HF068) circuit breaker on the copilot’s circuit breaker panel.


34-36-01 Reactive Windshear System (Includes TAWS windshear mode)

C 1 0

OPERATIONS (O)Crew briefings must include escape procedures for a windshear encounter and alternate methods used for monitoring for windshear encounters.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.40


34-44-01 Radio Altimeter System A 1 0

MAINTENANCE (M)(Units -0001 thru -0500): Pull and secure the RADIO ALTIMETER 1 (HC062) circuit breaker on the pilot’s circuit breaker panel.

(Units -0501 and on): Pull and secure the appropriate circuit breaker.


34-44-03 Terrain Awareness and Warning System (TAWS) (Including test mode) (Class A or

B TAWS required)

A 1 0

OPERATIONS (O)Crew briefings must include aural callouts through use of appropriate aircraft equipment to ensure obstacle and terrain clearance.


34-44-03-01 Forward Looking Terrain Avoidance Function and Premature Descent Alert

Function

B 2 0





SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.41


34-44-03-02

Excessive Rate of Descent (Mode 1) and Altitude Loss After Takeoff or Missed

Approach (Mode 3)

A 2 0



34-44-03-03A Voice Callouts (Mode 6) ("Five-Hundred")

B 1 0

OPERATIONS (O)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 Voice Callouts (Mode 6) (Other)

C 1 1

OPERATIONS (O)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.


34-44-03-04A

Excessive Closure Rate to Terrain (Mode 2) and Flight Into Terrain Not in Landing

Configuration (Mode 4) (Class A TAWS required)

A 2 0





SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.42


34-45-01-00A Traffic Alert and Collision Avoidance System (TCAS II)

B 1 0

MAINTENANCE (M)(Units -0001 thru -0500): Pull and secure the TCAS II (HC061) circuit breaker on the pilot’s circuit breaker panel.

(Units -0501 and on): Pull and secure the TCAS (HF053) circuit breaker on the pilot’s circuit breaker panel.


34-45-01-00B Traffic Alert and Collision Avoidance System (TCAS II)

C 1 0

MAINTENANCE (M)(Units -0001 thru -0500): Pull and secure the TCAS II (HC061) circuit breaker on the pilot’s circuit breaker panel.

(Units -0501 and on): Pull and secure the TCAS (HF053) circuit breaker on the pilot’s circuit breaker panel.


34-61-01 Navigation Database C 2 0

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.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.43


35-0-02 Oxygen Bottle (Aircraft with extended range oxygen system)

C 2 1


Close the Unserviceable or Empty Oxygen Cylinder Pressure Regulator (Refer to Figure 901).(1) Remove fuselage access panel 164BC to get access to the oxygen cylinder. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.(2) Remove and discard the safety wire from the pressure regulator.(3) Move the pressure regulator lever to the OFF position.(4) Safety the pressure regulator lever in the OFF position with safety wire. Refer to 680 Maintenance Manual Chapter 20, Safetying - Maintenance Practices.(5) Install fuselage access panel 164BC. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.(6) For Airplanes -0001 thru -0500, disconnect the SYSTEM PRESS LOW indicator light.(a) Disengage the OXYGEN circuit breaker on the pilot's circuit breaker panel.(b) Disengage the PANEL LIGHTS circuit breaker on the copilot's circuit breaker panel.(c) Remove the screws that attach the oxygen switch panel to the instrument panel.(d) Carefully move the oxygen switch panel from the instrument panel a sufficient distance to get access to the electrical wiring for the SYSTEM PRESS LOW indicator light (FI011 left, FI031 right).





SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.44


35-0-02 Oxygen Bottle (Aircraft with extended range oxygen system)

C 2 1

(e) Disconnect the electrical wiring from the SYSTEM PRESS LOW indicator light. Refer to the Model 680 Wiring Diagram Manual.(f) Put protective caps or covers on the electrical wiring.(g) Put the oxygen switch panel in its position on the instrument panel.(h) Install the screws that attach the oxygen switch panel to the instrument panel.(i) Engage the PANEL LIGHTS circuit breaker on the copilot's circuit breaker panel.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.45


35-0-03-01 Fill Port C 1 0


Do the Servicing of the Oxygen Cylinder at the Pressure Regulator (Refer to Figure 901).(1) Remove fuselage access panel 164BC to get access to the oxygen cylinder. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.(2) Remove and discard the safety wire from the pressure regulator.(3) Move the pressure regulator lever to the OFF position.(4) Disconnect the fill line assembly from the pressure regulator. Refer to 680 Maintenance Manual Chapter 35 Oxygen Cylinder and Pressure Regulator - Maintenance Practices.(a) 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.(6) Move the pressure regulator lever to the ON position.(7) Use the temperature and pressure tables given in 680 Maintenance Manual Chapter 12, Oxygen System - Servicing to fill the oxygen cylinder to the correct pressure.(8) Move the pressure regulator lever to the OFF position.(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 680 Maintenance Manual Chapter 35, Oxygen Cylinder and Pressure Regulator - Maintenance Practices.





SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.46


35-0-03-01 Fill Port C 1 0

(11) Move the pressure regulator lever to the ON position.(12) Safety the pressure regulator lever in the ON position with safety wire. Refer to 680 Maintenance Manual Chapter 20, Safetying - Maintenance Practices.(13) Install fuselage access panel 164BC. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.


35-0-03-02 Servicing Panel Pressure Gauge

C 1 0


Do the Servicing of the Oxygen System with the Cockpit Oxygen Pressure Gage.

NOTE: The use of the cockpit oxygen pressure gage is an alternative to the oxygen pressure gage at the oxygen servicing panel.

(1) Do the servicing of the oxygen system. Refer to 680 Maintenance Manual Chapter 12, Oxygen System - Servicing.(a) During the servicing, use a second person in the cockpit to monitor the cockpit oxygen pressure gage (Airplanes -0001 thru -0500) or display (Airplanes -0501 and On).




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.47


35-20-01-01 Mask C 9 0


Install the Passenger Oxygen Mask Pintle Pin.(1) If installed, remove the passenger oxygen mask. Refer to 680 Maintenance Manual Chapter 35, Passenger Oxygen System - Maintenance Practices.(2) Install the pintle pin.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.48


36-10-01-00A Left (Units -0501 and on) B 1 0


Install a Blocking Plate on the Bleed Air Shutoff Valve (Refer to Figure 901).

NOTE: The blocking plate installation on the left and the right bleed air shutoff valves is typical.

(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 bleed line casting assembly upstream from the unserviceable bleed air shutoff valve. Refer to 680 Maintenance Manual Chapter 36, Pneumatic Distribution - Maintenance Practices.(3) Install the blocking plate on the unserviceable bleed air shutoff valve, between the valve and the bleed line casting assembly.(4) Connect the bleed line casting assembly to the unserviceable bleed air shutoff valve. Refer to 680 Maintenance Manual Chapter 36, Pneumatic Distribution - Maintenance Practices.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.49


36-10-01-00B Right (Units -0501 and on) B 1 0


Install a Blocking Plate on the Bleed Air Shutoff Valve (Refer to Figure 901).


(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 bleed line casting assembly upstream from the unserviceable bleed air shutoff valve. Refer to 680 Maintenance Manual Chapter 36, Pneumatic Distribution - Maintenance Practices.(3) Install the blocking plate on the unserviceable bleed air shutoff valve, between the valve and the bleed line casting assembly.(4) Connect the bleed line casting assembly to the unserviceable bleed air shutoff valve. Refer to 680 Maintenance Manual Chapter 36, Pneumatic Distribution - Maintenance Practices.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.50


36-10-01-01A High-pressure (HP) (Units -0501 and on)

C 2 1


Install a Blocking Plate on the Unserviceable High-Pressure-Regulating Shutoff-Valve (Refer to Figure 901).


(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 bleed air tube upstream from the unserviceable high-pressure regulating shutoff valve. Refer to 680 Maintenance Manual Chapter 36, Pneumatic Distribution - Maintenance Practices.(3) Install the blocking plate on the unserviceable high-pressure regulating shutoff-valve, between the valve and the bleed air tube.(4) Connect the bleed air tube to the unserviceable high-pressure regulating shutoff-valve. Refer to 680 Maintenance Manual Chapter 36, Pneumatic Distribution - Maintenance Practices.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.51


36-10-02-00A Engine Bleed Air Precooler Temperature Control System

B 2 1


Secure the Precooler Temperature Control Valve in the Full Open Position.

NOTE: This procedure is typical for the left and the right precooler temperature control valves.

(1) Remove pylon access panel 411BB left, 412BB right to get access to the precooler temperature control valve. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.(2) Disconnect the electrical connector from the precooler temperature control actuator. Refer to 680 Maintenance Manual Chapter 36 Pneumatic Distribution - Maintenance Practices.(a) Put a protective cap on the electrical connector and stow it.(3) Disconnect the precooler temperature control actuator from the precooler temperature control valve. Refer to 680 Maintenance Manual Chapter 36, Pneumatic Distribution - Maintenance Practices. (4) Move the precooler temperature control valve lever to the full open position. NOTE: The open and closed positions are indicated on the valve body. The valve lever will be approximately 60 degrees to the flow direction in the full open position.

(5) Safety the lever in the full open position, through the bolt hole, to the precooler temperature control actuator bracket with safety wire. Refer to 680 Maintenance Manual Chapter 20, Safetying – Maintenance Practices.





SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.52


36-10-02-00A Engine Bleed Air Precooler Temperature Control System

B 2 1

(6) Install pylon access panel 411BB left, 412BB right. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.53


38-10-01 Potable Water System C 1 0


Drain the Aft Vanity Water System.(1) Drain the Aft Vanity Water System. Refer to the Model 680 Interior Maintenance Manual and Illustrated Parts Catalog.


38-10-01-01 Individual Components C 1 0

MAINTENANCE (M)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.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.54


38-30-02 Lavatory External Service System

C 1 0

MAINTENANCE (M)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 Dump Cable C 1 0


Do the Servicing of the Externally Serviceable Flush Toilet (Manual Operation of the Drain Valve).(1) Remove the upholstery adjacent to the externally serviceable flush toilet to get access to the drain valve.(2) Do the servicing of the externally serviceable flush toilet. Refer to 680 Maintenance Manual Chapter 12, Externally Serviceable Flush Toilet - Servicing.(a) During the servicing, use a second person inside the airplane to operate the drain valve manually, when necessary.(3) Install the upholstery.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.55


38-30-02-08 Heater Gasket C 1 0

MAINTENANCE (M)Pull and secure the appropriate circuit breaker in the aft interior junction box.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.56


49-20-01 Auxiliary Power Unit (APU) C 1 0

MAINTENANCE (M)(Units -0001 thru -0500): Pull and secure the APU MASTER (HF014) circuit breaker on the copilot’s circuit breaker panel.

(Units -0501 and on): Pull and secure the APU MASTER (HF041) circuit breaker on the copilot’s circuit breaker panel.




SERIAL NO:680-0526

REG.NO:N680NA

REVISION:Original

DATE:06/02/2014

PAGE NO.57


49-30-01 APU Fuel Shutoff Valve C 1 0


(Units -0001 thru -0500)Make Sure that the APU Fuel Shutoff Valve is Closed.(1) Remove fuselage fairing access panels 330ABC and 330CBC to get access to the APU. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.(2) Disconnect the fuel supply line from the APU.(3) Put a metal container below the disconnected fuel supply line.(4) Connect external electrical power to the airplane.(5) Push the EXT PWR switch/light on the left switch panel to the ON position.(6) Push the BUS TIE OPEN/CLOSED switch/light on the left switch panel to the CLOSED position.(7) Make sure that the MASTER switch/light on the APU SYSTEM switch panel is in the OFF position.(8) Use the copilot's cursor control device (CCD) to access the Citation Diagnostic Maintenance System on the copilot's multifunction display (MFD). Refer to 680 Maintenance Manual Chapter 45, Citation Diagnostic Maintenance System (CDMS) - Maintenance Practices.(a) On the CDMS screen, select the MAINTENANCE page. NOTE: If the system was just started, it can take up to four minutes for the MAINTENANCE option to be highlighted as the system boots.





SERIAL NO:680-0526

REG.NO:N680NA

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DATE:06/02/2014

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(b) Move the cursor to SOVEREIGN DIAGNOSTICS and push the cursor select button on the CCD.(c) Use the right top selector knob on the CCD to highlight the ATA Chapter 28 and push the cursor SELECT button.(d) Select the FUEL menu.(e) Make sure that the APU FUEL VLV shows CLOSED.(9) Push the FUEL BOOST NORM/ON R switch/light on the left switch panel to the ON position. (10) Make sure that no fuel flows from the disconnected fuel supply line at the APU.(11) Push the FUEL BOOST NORM/ON R switch/light on the left switch panel to the NORM position.(12) Push the BUS TIE OPEN/CLOSED switch/light on the left switch panel to the OPEN position.(13) Push the EXT PWR switch/light on the left switch panel to the AVAIL position.(14) Disconnect the external electrical power from the airplane.(15) Connect the fuel supply line to the APU.(16) Remove the metal container from below the APU.(17) Install fuselage fairing access panels 330ABC and 330CBC. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.

(Units -0501 and on)Make Sure that the APU Fuel Shutoff Valve is Closed.





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(1) Remove fuselage fairing access panels 330ABC and 330CBC to get access to the APU. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.(2) Disconnect the fuel supply line from the APU.(3) Put a metal container below the disconnected fuel supply line.(4) Connect external electrical power to the airplane.(5) Push the EXT PWR switch/light on the left switch panel to the ON position.(6) Push the BUS TIE switch/light on the left switch panel to the CLOSED position.(7) Make sure that the APU rotary switch on the pedestal switch panel is in the OFF position.(8) Use the pilot's right Garmin GTC 570 Touchscreen Controller to select Aircraft Systems from the Home page. Refer to 680 Maintenance Manual 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 - NZ107.(d) Scroll until you find the APU Fuel Vlv Cmd indication and make sure that the COMMAND/STATUS shows Closed.(9) Push the BOOST PUMP R switch/light on the pedestal switch panel to the ON position. (10) Make sure that no fuel flows from the disconnected fuel supply line at the APU.(11) Push the BOOST PUMP R switch/light on the pedestal switch panel to the NORM position.(12) Push the BUS TIE switch/light on the left switch panel to the OPEN position.





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(13) Push the EXT PWR switch/light on the left switch panel to the AVAIL position.(14) Disconnect the external electrical power from the airplane.(15) Connect the fuel supply line to the APU.(16) Remove the metal container from below the APU.Install fuselage fairing access panels 330ABC and 330CBC. Refer to 680 Maintenance Manual Chapter 6, Access Plates and Panels Identification - Description and Operation.


49-50-01 APU Bleed Air Heat Exchanger Fan (Units -0501 and on)

C 1 0

MAINTENANCE (M)Pull and secure the BLEED AIR HX FAN (HT236) circuit breaker in the LH power junction box.


49-50-02 APU Bleed Air System (Units -0501 and on)

C 1 0

OPERATIONS (O)1. Prior to engine start, start the APU.2. Verify no air flow exists from the overhead air outlets.




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DATE:06/02/2014

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49-50-02-01 Max Cool Function (Units -0501 and on)

C 1 0

OPERATIONS (O)(1) Prior to engine start, start the APU.(2) Select APU BLEED AIR to ON.(3) Verify air flow from the overhead air outlets.(4) Select APU BLEED AIR to OFF.(5) Verify the air flow ceases after a few seconds.




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52-10-01-02 Precatch C 1 0


Secure the Cabin Door Precatch.(1) Open the cabin door.(2) Move and hold the cabin door precatch in the retracted position.(3) 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.(4) Use a second person to close and latch the cabin door.(5) Make sure that there is no interference between the cabin door precatch and the exit path through the cabin door. OPERATIONS (O)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.




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52-10-01-07 Handrail C 1 0

OPERATIONS (O)1. Prior to entry and exit, occupants are briefed by a crew member not to utilize the handrail.2. Passengers may need assistance entering and exiting the aircraft.


52-30-01-02 Door Seal (Units -0501 and on)

C 1 0

OPERATIONS (O)Prior to each flight, a crew member must make sure the aft baggage compartment is empty.


52-30-01-05 Gas Spring C 1 0

OPERATIONS (O)1. The flight crew should brief any occupants or crewmembers who would need to access the aft baggage that the spring is inoperative.2. When opened, the door shall be held open or supported by another means which is secure enough to prevent the door from swinging in the wind.




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52-50-01 Cockpit Divider Door C 2 0


Secure the Cockpit Divider Door.(1) Put the cockpit divider door in the open position. CAUTION: Do not use duct tape or other tapes that can contain substances known to cause damage to the furniture finish or leave residues.

(2) Carefully attach sufficient lengths of 3M vinyl tape (or equivalent) across the door opening at a 90-degree angle to make sure that the door does not close during airplane operation.




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52-50-02 Lavatory Door C 2 0


Secure the lavatory Divider Door.(1) Put the lavatory divider door in the open position. CAUTION: Do not use duct tape or other tapes that can contain substances known to cause damage to the furniture finish or leave residues.

(2) Carefully attach sufficient lengths of 3M vinyl tape (or equivalent) across the door opening at a 90-degree angle to make sure that the door does not close during airplane operation.




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78-30-01 Thrust Reverser C 2 0


Secure the Left and/or the Right Thrust Reversers.(1) Do the Thrust Reverser Flight Lockout procedure for the left and/or the right thrust reversers. Refer to 680 Maintenance Manual Chapter 78, Thrust Reversers - Maintenance Practices.

CABIN ALTITUDE vs. CABIN PRESSURE DIFFERENTIAL CONVERSION (Cabin Pressure Differential Display or Cabin Altimeter Inoperative)

CABIN

ALT AIRCRAFT PRESSURE ALTITUDE × 1000'

CA

BIN

ALT

ITU

DE

x 10

00'

x 1000' 0 5 10 15 20 25 28 31 33 35 37 39 41 43 45 47 49 51

11.0 1.4 3.0 4.3 4.9 5.6 5.9 6.3 6.6 6.9 7.1 7.4 7.6 7.8 8.0 8.1 10.5 1.6 3.2 4.5 5.1 5.7 6.1 6.4 6.8 7.1 7.3 7.5 7.8 8.0 8.1 8.3 10.0 0.0 1.8 3.4 4.7 5.3 5.9 6.3 6.6 7.0 7.3 7.5 7.7 8.0 8.2 8.3 8.5 9.5 0.2 2.0 3.6 4.9 5.5 6.1 6.5 6.8 7.2 7.5 7.7 7.9 8.2 8.4 8.5 8.7 9.0 0.4 2.2 3.8 5.1 5.7 6.3 6.7 7.0 7.4 7.7 7.9 8.1 8.4 8.6 8.7 8.9 8.5 0.6 2.4 4.0 5.3 5.9 6.5 6.9 7.2 7.6 7.9 8.1 8.3 8.6 8.8 8.9 9.1 8.0 0.8 2.6 4.2 5.5 6.1 6.7 7.1 7.5 7.8 8.1 8.3 8.6 8.8 9.0 9.2 9.3 7.5 1.0 2.8 4.4 5.7 6.4 7.0 7.3 7.7 8.0 8.3 8.5 8.8 9.0 9.2 9.4 9.5 7.0 1.2 3.0 4.6 5.9 6.6 7.2 7.5 7.9 8.2 8.5 8.7 9.0 9.2 9.4 9.6 9.7 6.5 1.5 3.3 4.8 6.1 6.8 7.4 7.8 8.1 8.4 8.7 9.0 9.2 9.4 9.6 9.8 10.0 6.0 1.7 3.5 5.0 6.3 7.0 7.6 8.0 8.3 8.6 8.9 9.2 9.4 9.6 9.8 10.0 5.5 1.9 3.7 5.2 6.5 7.2 7.8 8.2 8.5 8.9 9.1 9.4 9.6 9.9 10.1 5.0 0.0 2.1 3.9 5.5 6.8 7.5 8.1 8.4 8.8 9.1 9.4 9.6 9.9 10.1 4.5 0.2 2.4 4.2 5.7 7.0 7.7 8.3 8.7 9.0 9.3 9.6 9.9 10.1 4.0 0.5 2.6 4.4 5.9 7.2 7.9 8.5 8.9 9.2 9.5 9.8 10.1 3.5 0.7 2.8 4.6 6.2 7.5 8.2 8.8 9.1 9.5 9.8 10.1 3.0 0.9 3.1 4.9 6.4 7.7 8.4 9.0 9.4 9.7 10.0 2.5 1.2 3.3 5.1 6.7 8.0 8.6 9.2 9.6 10.0 2.0 1.4 3.6 5.4 6.9 8.2 8.9 9.5 9.9 10.2 1.5 1.7 3.8 5.6 7.2 8.5 9.1 9.8 10.1 1.0 1.9 4.1 5.9 7.4 8.7 9.4 10.0 0.5 2.2 4.3 6.1 7.7 9.0 9.7 0.0 0.0 2.5 4.6 6.4 7.9 9.2 9.9 -0.5 0.3 2.7 4.9 6.7 8.2 9.5 10.2 -1.0 0.5 3.0 5.1 6.9 8.5 9.8 10.5



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PAGE NO.

SECTION TWO

CASMESSAGEORIENTED

MEL RELIEF



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PAGE NO.I

TABLE OF CONTENTS

SYSTEM NO. SYSTEM DESCRIPTION PAGE NO.

- - - Table of Contents I- - - Log of Revisions II- - - Control Page(s) III THRU VII- - - Section Two - Introduction VIII THRU X90 Cas Indication 90 -1 THRU 18- - - M&O Procedures - APPENDIX 1 THRU 1



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PAGE NO.II

LOG OF REVISIONS

REVISION DATE PAGE NUMBERS INITIALS

Original 06/02/2014 ALL



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PAGE NO.III

CONTROL PAGE(S)


Original 06/02/2014 3 11/28/2013

PAGENO.



REVISION DATE

I Original 06/02/2014

II Original 06/02/2014

III Original 06/02/2014

IV Original 06/02/2014

V Original 06/02/2014

VI Original 06/02/2014

VII Original 06/02/2014

VIII Original 06/02/2014

IX Original 06/02/2014

X Original 06/02/2014

90-1 Original 06/02/2014

90-2 Original 06/02/2014

90-3 Original 06/02/2014

90-4 Original 06/02/2014

90-5 Original 06/02/2014

90-6 Original 06/02/2014

90-7 Original 06/02/2014

90-8 Original 06/02/2014

90-9 Original 06/02/2014

90-10 Original 06/02/2014

90-11 Original 06/02/2014

90-12 Original 06/02/2014

90-13 Original 06/02/2014

90-14 Original 06/02/2014

90-15 Original 06/02/2014

90-16 Original 06/02/2014

90-17 Original 06/02/2014

90-18 Original 06/02/2014

M&O PROCEDURES

1 Original 06/02/2014




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PAGE NO.IV

CONTROL PAGE(S)


Original 06/02/2014 REV. NO. 3 11/28/2013




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PAGE NO.V

CONTROL PAGE(S)


Original 06/02/2014 REV. NO. 3 11/28/2013




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PAGE NO.VI

CONTROL PAGE(S)


Original 06/02/2014 REV. NO. 3 11/28/2013




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REVISION:Original

DATE:06/02/2014

PAGE NO.VII

CONTROL PAGE(S)


Original 06/02/2014 REV. NO. 3 11/28/2013




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REVISION:ORIGINAL

DATE:06/02/2014

PAGE NO.VIII

SECTION TWO - INTRODUCTION

Two section MMELs are authorized by FAA PL 119. Section Two of two-section MMELs may grant relief for failure indications presented as CAS messages on Engine Indicating and Crew Alerting Systems (EICAS), or Electronic Centralized Aircraft Monitoring (ECAM), rather than the traditional relief (Section One) for failed equipment. New technology self-diagnostic tests eliminate the need for failure isolation procedures by maintenance personnel for many CAS messages. By using (O) procedures, the crew can complete selected system/component deactivation/re-configuration from the cockpit for which the crew has been trained.

Section Two will only contain CAS message relief if the crew can act on the item. CAS message relief must ensure safe operation of aircraft. Flight Operations Evaluation Boards (FOEB) will use the normal FOEB processes for determining which CAS messages go into each section.

TWO-SECTION MMEL GUIDANCE:

Modern technology CAS MMELs shall be divided into two sections.

A. Section One. Items which either require maintenance actions (this may include some CAS messages), or caution/advisory information. Section One will continue to use the existing Line Replaceable Units (LRU) - oriented MMEL format and should address the following type of equipment failures:

1. Failures which are not annunciated to crew; and

2. Failures which are annunciated, but the failure indication by itself is not considered sufficient to determine the aircraft airworthiness status.

B. Section Two. Includes only items where flight members may act on CAS messages. MMEL items where CAS messages can be used to determine the aircraft airworthiness should be formatted as follows:



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PAGE NO.IX


1. It should have only two columns:

a. Column one should list the failure indications (messages) for which relief is given (if desired, the messages may be listed in alphabetical order with no ATA break down).

b. Column two should include the corresponding MMEL limitations and/or procedures. The format of this column should be in line with the format requirements of the "Remarks or Exceptions" column of the conventional "LRU oriented" MMEL.

Note: In many cases, CAS messages will not require maintenance to perform fault analysis.

Relief provisos for these CAS items are expected to be more restrictive in content and repair interval, as compared to Section One relief provisos.

2. Section Two CAS message relief items require flight crews to accomplish one or more steps to deactivate/re-configure the affected system prior to flight. The "(O)" indicates the need for these tasks.

Tasks include, but are not necessarily limited to the following duties:

a. Procedures accomplished using cockpit (or cabin) system controls;

b. Deactivation of affected systems (by pulling system breaker or use of remote electronic system isolation);

c. Visual confirmation of remote gauge indications, or valve positions as provided by integral external indicators; and

d. Visual inspection behind panels (internal or external).

1) These panels must be accessible without tools via quick-release latches and must clearly indicate their unlocked or unsafe state (red/green safe window; flush fit latches - candidates to be verified at FOEB).

2) The visual inspection of compartments accessed by the panels is within the normal crew duty requirements for which they have been trained; and

3) The crew may use an external ladder for visual inspection behind panels as long as this procedure is within the normal crew duty requirements for which they have been trained.



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REVISION:ORIGINAL

DATE:06/02/2014

PAGE NO.X


Special equipment such as maintenance stands and hydraulic lifts may not be used by the crew to perform visual inspections.

C. The following statement will be included on page 1 of Section Two in all two-section MMELs:

1. Section Two of the MMEL will list only Crew Alerting system (CAS) messages meeting the following requirements:

a. Equipment failure indications(s) that can be used to determine the airworthiness status of the airplane;

b. Messages that the crew can act upon from the cockpit with simple troubleshooting procedures without the assistance of a mechanic, and for which the crew has been trained.

c. Messages using the new self-diagnostic technology (virtual) actions for which the crew has been trained.

2. CAS message relief items not meeting these requirements will be listed in Section One of the MMEL.



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REVISION:Original

DATE:06/02/2014

PAGE NO.90-1

CAS Indication Dispatch Consideration

WHITE CAS INDICATIONS

AC BEARING L-R (Units -0501 and on)

Aircraft may be dispatched provided aircraft is operated in accordance with airplane flight manual AC BEARING L-R white message procedure.

ADS-B FAIL (Units -0501 and on)

Aircraft may be dispatched provided Automatic Dependent Surveillance-Broadcast (ADS-B) Squitter Transmission is considered inoperative.




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PAGE NO.90-2


AP FAIL (Units -0501 and on)

Aircraft may be dispatched provided autopilot system is considered inoperative.

AT FAIL (Units -0501 and on)

Aircraft may be dispatched provided autothrottle system is considered inoperative.

BAGGAGE HEAT FAIL (Units -0501 and on)

Aircraft may be dispatched provided baggage heat system is considered inoperative.

ENG DISPATCH LIM L-R (Units -0501 and on)

Aircraft may be dispatched provided aircraft is operated in accordance with airplane flight manual ENG DISPATCH LIM L-R white message procedure.




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REVISION:Original

DATE:06/02/2014

PAGE NO.90-3


FDR FAIL (Units -0501 and on)

Not applicable.

FIRE BTL LOW BAG-APU (Units -0501 and on)

Aircraft may be dispatched provided Auxiliary Power Unit (APU)/baggage compartment fire extinguishing system is considered inoperative.

FIRE BTL LOW BAGGAGE (Units -0501 and on)

Aircraft may be dispatched provided baggage compartment fire extinguishing system (nose MDR bottle) is considered inoperative.

OIL FLTR BYPASS L-R (Units -0501 and on)

Aircraft may be dispatched provided aircraft is operated in accordance with airplane flight manual OIL FLTR BYPASS L and/or R white message procedure.

OIL LEVEL LOW L-R (Units -0501 and on)

Aircraft may be dispatched provided aircraft is operated in accordance with airplane flight manual OIL LEVEL LOW L-R white message procedure.




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PAGE NO.90-4


TEMP FAULT CKT-CAB (Units -0501 and on)

Aircraft may be dispatched provided automatic temperature control system is considered inoperative.

TRANSPONDER FAIL 1/2 (Units -0501 and on)

Aircraft may be dispatched provided ATC transponder is considered inoperative.

YD FAIL (Units -0501 and on)

Aircraft may be dispatched provided yaw damper is considered inoperative.




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PAGE NO.90-5


CYAN CAS INDICATIONS

AC BEARING L-R (Units -0001 thru -0500)

Not applicable.

AP FAIL A-B (Units -0001 thru -0500)

Not applicable.

BAGGAGE HEAT FAIL (Units -0001 thru -0500)

Not applicable.

ENGINE DISPATCH LIMIT L-R (Units -0001 thru -0500)

Not applicable.




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REVISION:Original

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PAGE NO.90-6


FDR FAIL (Units -0001 thru -0500)

Not applicable.

FIRE BOTTLE LOW BAG-APU (Units -0001 thru -0500)

Not applicable.

FIRE BOTTLE LOW BAGGAGE (Units -0001 thru -0500)

Not applicable.

GROUND PROX FAIL (Units -0001 thru -0500)

Not applicable.

MAIN WHEEL SPINDOWN FAIL (Units -0001 thru -0500)

Not applicable.




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REVISION:Original

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PAGE NO.90-7


OIL FILTER BYPASS L-R (Units -0001 thru -0500)

Not applicable.

OIL LEVEL LOW L-R (Units -0001 thru -0500)

Not applicable.

RAAS FAIL (Units -0001 thru -0500)

Not applicable.

TERR FAIL (Units -0001 thru -0500)

Not applicable.

WINDSHEAR FAIL (Units -0001 thru -0500)

Not applicable.




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PAGE NO.90-8


YD FAIL A-B (Units -0001 thru -0500)

Not applicable.




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PAGE NO.90-9


AMBER CAS INDICATIONS

A/I RATE FAIL L-R (Units -0501 and on)

Aircraft may be dispatched provided all bleed air anti-ice systems are considered inoperative.

AOA HEAT FAIL L-R Aircraft may be dispatched provided Angle of Attack (AOA) vane heater is considered inoperative.

AP STAB TRIM INOP B Aircraft may be dispatched provided:

a) PRIMARY STAB TRIM FAIL amber message does not appear, andb) Autopilot system is considered inoperative.




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PAGE NO.90-10


APU FIRE DETECT FAIL (Units -0001 thru -0500)

Not applicable.

APU SYS FAIL (Units -0501 and on)

Aircraft may be dispatched provided aircraft is operated in accordance with airplane flight manual APU SYS FAIL amber message procedure or Auxiliary Power Unit (APU) is considered inoperative.

AT FAIL (Units -0501 and on)

Aircraft may be dispatched provided autothrottle system is considered inoperative.




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BAGGAGE DOOR OPEN Aircraft may be dispatched provided aft baggage door warning system is considered inoperative.

EMERGENCY EXIT OPEN Aircraft may be dispatched provided emergency exit door warning system is considered inoperative.

ENG ANTI-ICE COLD L-R (Units -0001 thru -0500)

Not applicable.

A/I ENGINE COLD L-R (Units -0501 and on)

Aircraft may be dispatched provided engine inlet anti-ice is considered inoperative.

FUEL LEVEL LOW L-R (when fuel quantity is known to be above threshold)

Aircraft may be dispatched provided Fuel Level Low Indicating System is considered inoperative.




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PAGE NO.90-12


GPS 1-2 INACTIVE (Units -0001 thru -0500)

Not applicable.

GROUND PROX FAIL (Units -0501 and on)

Aircraft may be dispatched provided Terrain Awareness and Warning System (TAWS) excessive descent rate mode, excessive terrain closure rate mode, altitude loss after takeoff mode, reduced required terrain clearance mode, and glideslope deviation mode are considered inoperative.

NOTE: Voice callouts may be inoperative.

HP VALVE FAIL L-R (Units -0001 thru -0500)

Not applicable.

HP VALVE CLOSED L-R (Units -0501 and on)

Aircraft may be dispatched provided High Pressure (HP) bleed valve is considered inoperative.




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PAGE NO.90-13


INBD WING A/I COLD L-R (Units -0001 thru -0500)

Not applicable.

A/I INB WNG COLD L-R (Units -0501 and on)

Aircraft may be dispatched provided inboard leading edge wing bleed air anti-ice system is considered inoperative.

LAVATORY DOOR Aircraft may be dispatched provided lavatory door warning system is considered inoperative.

MACH TRIM FAIL Aircraft may be dispatched provided mach trim system is considered inoperative.




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PAGE NO.90-14


NOSE DOOR OPEN L-R Aircraft may be dispatched provided nose access door warning system is considered inoperative.

O2 PRESS LOW R (Units -0501 and on)

Aircraft may be dispatched provided extended range oxygen bottle is considered inoperative.

PITOT/STATIC COLD L-R (when selected ON) (Units -0001 thru -0500)

Not applicable.

P/S COLD L-R (when selected ON) (Units -0501 and on)

Aircraft may be dispatched provided pilot or copilot static port heater is considered inoperative.




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PAGE NO.90-15


PITOT/STATIC COLD L-R (when selected ON) (Units -0001 thru -0500)

Not applicable.

P/S COLD L-R (when selected ON) (Units -0501 and on)

Aircraft may be dispatched provided pilot or copilot pitot heater is considered inoperative.

PRESSURIZATION FAULT (Units -0501 and on)

Aircraft may be dispatched provided cabin pressurization controller modes (excluding manual) are considered inoperative.

RAT HEAT FAIL L-R Aircraft may be dispatched provided Ram Air Temperature (RAT) probe heater is considered inoperative.

STAB ANTI-ICE COLD L-R (Units -0001 thru -0500)

Not applicable.




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A/I STAB COLD L-R (Units -0501 and on)

Aircraft may be dispatched provided horizontal stabilizer bleed air anti-ice system is considered inoperative.

TAILCONE DOOR OPEN Aircraft may be dispatched provided tail cone access door warning system is considered inoperative.

TCAS FAIL Aircraft may be dispatched provided traffic alert and collision avoidance system is considered inoperative.




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TERRAIN FAIL (Units -0501 and on)

Aircraft may be dispatched provided Terrain Awareness and Warning System (TAWS) forward looking terrain avoidance function and premature descent alert function are considered inoperative.

NOTE: Glideslope deviation mode and voice callouts may beinoperative.

TRANSPONDER FAIL 1-2 (Units -0501 and on)

Aircraft may be dispatched provided ATC transponder is considered inoperative.

WINDSHEAR FAIL (Units -0501 and on)

Aircraft may be dispatched provided Terrain Awareness and Warning System (TAWS) windshear mode is considered inoperative.




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WINDSHIELD HEAT INOP L-R (Units -0001 thru -0500)

Not applicable.

WSHLD HEAT INOP L-R (Units -0501 and on)

Aircraft may be dispatched provided windshield anti-ice system is considered inoperative.

WING ANTI-ICE COLD L-R (Units -0001 thru -0500)

Not applicable.

A/I WIND COLD L-R (Units -0501 and on)

Aircraft may be dispatched provided outboard leading edge wing bleed air anti-ice system is considered inoperative.


Millbrook AviationMINIMUM EQUIPMENT LIST APPENDIX MAINTENANCE & OPERATIONS

PROCEDURES


SERIAL NO:680-0526

REG.NO:N680NA

REVISION:pagenumber1pagenumber

DATE:date1date

PAGE NO.

1