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EUROPEAN AVIATION SAFETY AGENCY

MASTER MINIMUM EQUIPMENT LIST

CESSNA CE-560XL

Citation Excel

REVISION: 1

23 October 2012

EUROPEAN AVIATION SAFETY AGENCY CITATION 560XL MASTER MINIMUM EQUIPMENT LIST 23 October 2012

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EUROPEAN AVIATION SAFETY AGENCY

MASTER MINIMUM EQUIPMENT LIST

CESSNA CITATION 560XL Revision 1

23 October 2012

This Master Minimum Equipment List (MMEL) is issued by the European Aviation Safety Agency (EASA) at the above revision and is recommended for approval as the basis of the preparation and

approval of individual operators' Minimum Equipment Lists (MELs) for aircraft of this type as certified by EASA and operated under the jurisdiction of EASA member states National Authorities.

MMEL Section Manager

For and on behalf of the EASA

Correspondence concerning this document should be addressed to the office listed below:

European Aviation Safety Agency

Postfach 10 12 53

50452 Koln

Germany

Attention: MMEL Section Manager, Experts Department

III


REVISION RECORD

REVISION No. ISSUE DATE INCORPORATED BY DATE

ORIGINAL 10-JAN-2009

1 23 October 2012

V


TABLE OF CONTENTS

I. APPROVAL SHEET III. REVISION RECORD V. TABLE OF CONTENTS

VII - VIII. LIST OF EFFECTIVE PAGES XI. – XII. PREAMBLE

XIII. – XVII. DEFINITIONS AND EXPLANATORY NOTES XVIII - XX. HILIGHTS OF REVISION

21 AIR CONDITIONING 22 AUTO FLIGHT 23 COMMUNICATIONS 24 ELECTRICAL POWER 25 EQUIPMENT/FURNISHINGS 26 FIRE PROTECTION 27 FLIGHT CONTROLS 28 FUEL 30 ICE AND RAIN PROTECTION 31 INDICATING & RECORD 33 LIGHTS 34 NAVIGATION 35 OXYGEN 38 WATER/WASTE 45 CENTRAL MAINTENANCE 46 INFORMATION SYSTEMS 49 AIRBORNE AUXILIARY POWER 52 DOORS 73 ENGINE FUEL CONTROL 76 ENGINE CONTROLS 77 ENGINE INDICATING 78 EXHAUST

VII


LIST OF EFFECTED PAGES

Page Title Revision Date

I. Approval Sheet 1

III. Revision Record 1

V. Table of Contents Original

VII. List of Effective Pages 1

VIII. List of Effective Pages (Continued) 1

IX. List of Effective Pages (Continued) 1

X. Preamble Original

XI. Preamble (Continued) Original

XII. Definitions and Explanatory Notes Original

XIII. Definitions and Explanatory Notes (Continued) Original

XIV. Definitions and Explanatory Notes (Continued) Original

XV Definitions and Explanatory Notes (Continued) Original

XVI. Definitions and Explanatory Notes (Continued) Original

XVIII. Highlights of Revision Original 1

XIX. Highlights of Revision Original (Continued) 1

XX. Highlights of Revision Original (Continued) 1 21-1 Air Conditioning 1 21-2 Air Conditioning (Continued) 1 21-3 Air Conditioning (Continued) 1 21-4 Air Conditioning (Continued) 1 21-5 Air Conditioning (Continued) 1 21-6 Air Conditioning (Continued) 1 22-1 Auto Flight 1 22-2 Auto Flight (Continued) 1 23-1 Communications 1 23-2 Communications (Continued) 1 23-3 Communications (Continued) 1 23-4 Communications (Continued) 1 23-5 Communications (Continued) 1 23-6 Communications (Continued) 1 24-1 Electrical Power 1 24-2 Electrical Power (Continued) 1 25-1 Equipment/Furnishings 1 25-2 Equipment/Furnishings (Continued) 1 25-3 Equipment/Furnishings (Continued) 1 25-4 Equipment/Furnishings (Continued) 1 25-5 Equipment/Furnishings (Continued) 1 25-6 Equipment/Furnishings (Continued) 1 26-1 Fire Protection Original 26-2 Fire Protection (Continued) 1

VIII


LIST OF EFFECTED PAGES (Continued) Page Title Revision Date

27-1 Flight Controls 1 27-2 Flight Controls (Continued) 1 28-1 Fuel 1 28-2 Fuel (Continued) 1 30-1 Ice and Rain Protection 1 30-2 Ice and Rain Protection (Continued) 1 30-3 Ice and Rain Protection (Continued) 1 30-4 Ice and Rain Protection (Continued) 1 31-1 Indicating & Record Original 31-2 Indicating & Record (Continued) 1 31-3 Indicating & Record (Continued) 1 31-4 Indicating & Record (Continued) 1 31-5 Indicating & Record (Continued) 1 31-6 Indicating & Record (Continued) 1 31-7 Indicating & Record (Continued) 1 31-8 Indicating & Record (Continued) 1 31-9 Indicating & Record (Continued) 1 31-10 Indicating & Record (Continued) 1 33-1 Lights 1 33-2 Lights (Continued) Original 33-3 Lights (Continued) Original 33-4 Lights (Continued) Original 34-1 Navigation (Continued) 1 34-2 Navigation (Continued) 1 34-3 Navigation (Continued) 1 34-4 Navigation (Continued) 1 34-5 Navigation (Continued) 1 34-6 Navigation (Continued) 1 34-7 Navigation (Continued) 1 34-8 Navigation (Continued) 1 34-9 Navigation (Continued) 1 34-10 Navigation (Continued) 1 34-11 Navigation (Continued) 1 34-12 Navigation (Continued) 1 34-13 Navigation (Continued) 1 34-14 Navigation (Continued) 1 34-15 Navigation (Continued) 1 34-16 Navigation (Continued) 1 35-1 Oxygen 1 35-2 Oxygen (Continued) 1

LIST OF EFFECTED PAGES (Continued)

IX


38-1 Water/Waste Original 38-2 Water/Waste (Continued) 1 45-1 Central Maintenance Original 45-2 Central Maintenance (Continued) 1 46-1 Information Systems 1 46-2 Information Systems (Continued) 1 49-1 Airborne Auxiliary Power Original 49-2 Airborne Auxiliary Power (Continued) 1 52-1 Doors 1 52-1 Doors (Continued) 1 73-1 Engine Fuel Control Original 73-2 Engine Fuel Control (Continued) 1 76-1 Engine Controls Original 76-2 Engine Controls (Continued) 1 77-1 Engine Indicating 1 77-2 Engine Indicating (Continued) 1 78-1 Exhaust Original 78-2 Exhaust (Continued) 1

X



XI


PREAMBLE

The following is applicable for operators under EASA or European operating regulations (EU-OPS). The regulations require that all equipment installed on an aircraft in compliance with the Airworthiness code and the operating requirements must be operative. However, the Regulations also permit the use 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. EASA Master Minimum Equipment List (MMEL) is developed by the Type Certificate Holder to improve aircraft utilisation and thereby provide more convenient and economic air transportation for the public. EASA MMEL includes those items of equipment related to airworthiness and operating requirements and other items of equipment which EASA 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's MELs, which take into consideration the operator's particular aircraft equipment configuration and operational conditions. 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 permits operation of the aircraft with inoperative equipment. Equipment not required by the operation being conducted and equipment in excess of the requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from Airworthiness Directives or any other Mandatory Requirement It is important to remember that all equipment related to the airworthiness and the operating requirements 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.

XII


PREAMBLE (Continued)

The MEL is intended to permit operation with inoperative items of equipment for a period of time until rectifications can be accomplished. It is important that rectifications 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 operator may be permitted, by their competent authority, a one-time extension of the applicable rectification intervals B, C or D for the same duration as that specified in their MEL. This extension policy has been taken into account during the development of this document. 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 the applicable regulations. The item is then either rectified or may be deferred per the MEL or other approval means acceptable to the competent Authority prior to further operation. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in a 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 the applicable regulations. 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. The exposure to additional failures during continued operation with inoperative systems or components must also be considered. Wherever possible account has been taken in this MMEL of multiple inoperative items. However, it is unlikely that all possible combinations of this nature have been accounted for. Therefore, when operating with multiple inoperative items, the inter-relationships between those items and the effect on aircraft operation and crew workload must be considered. Operators are to establish a controlled and sound rectification program including the parts, personnel, facilities, procedures and schedules to ensure timely rectification. This program should identify the actions required for Maintenance discrepancy messages. WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.

XIII


DEFINITIONS AND EXPLANATORY NOTES 1. In this list, the items of equipment are classified in systems according to the ATA 100

specification. Individual items within a given ATA classification are numbered sequentially.

2. “Item” (Column 1): The equipment, system, components or function as listed in Column 1. “(If installed)”: Indicates the listed item of equipment is not applicable to all models or configurations. It does not imply that the aeroplane may be operated in accordance with this MMEL with the item removed.

NOTE 1: Items annotated in UPPER CASE letters indicate the precise flight deck legend used.

3. “Rectification Intervals” (Column 2): Inoperative items or components, deferred in accordance with the MEL, must be rectified at or prior to the rectification intervals established by the following letter designators given in the “Rectification Interval” column (2) of the MMEL. Category A No standard interval is specified. However, items in this category shall be rectified in accordance with the conditions stated in the Remarks column (5) of the MMEL. Where a time period is specified it shall start at 00:01 on the calendar day following the day of discovery. Category B Items in this category shall be rectified within three (3) consecutive calendar days, excluding the day of discovery. For example, if it was recorded at 10 am on January 26th, the three day interval would begin at midnight on the 26th and end at midnight on the 29th. Category C Items in this category shall be rectified within ten (10) consecutive calendar days, excluding the day of discovery. For example, if it was recorded at 10 am on January 26th, the 10 day interval would begin at midnight on the 26th and end at midnight on February 5th. Category D Items in this category shall be rectified within one hundred and twenty (120) consecutive calendar days, excluding the day of discovery.

XIV


DEFINITIONS AND EXPLANATORY NOTES

4. “Number Installed” (Column 3): The number of the specified items normally installed in the aeroplane. This number identifies the aeroplane configuration considered in developing the MMEL.

5. “Number Required for Dispatch (Column 4): The minimum number of the specified items required for operation provided the conditions defined in Column 5 are met.

6. “Remarks or Exceptions” (Column 5): This column includes a statement prohibiting operation or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation and appropriate notes. A note in column 5 indicates additional information and references for crew and/or maintenance personnel consideration; they are not part of the provisos. Where references are stated in column 5 these are to identify certain inter-relationships between the subject item and other MMEL items, AFM material etc. These references are intended to assist, but not relieve, an operator of the responsibility for determining such inter-relationships as stated in the Preamble.

7. Dash (-): This symbol indicates a variable quantity when used in Columns 3 or 4.

8. Each inoperative item must be placarded to inform and remind the crew members and maintenance personnel of the equipment condition. To the extent practicable, placards should be located adjacent to the control or indicator for the item affected such that it is clear to the operating crew that it or its associated system is inoperative.

9. “Inoperative”: A system or item of equipment is deemed inoperative if it malfunctions such that it does not accomplish its intended purpose and/or is not consistently functioning within its designed operating limit(s) or tolerance(s).

10. “(O)”: The use of this symbol in Column 5 indicates that an appropriate operating procedure (or change to an existing procedure) must be established, published and utilized to maintain the required level of safety while operating under the terms of the (M) MEL. Normally, these procedures are accomplished by the flight crew. However, other personnel may be qualified and authorized to perform certain functions.

11. “(M)”: The use of this symbol in Column 5 indicates that an appropriate maintenance procedure must be established, published and utilized prior to the first flight undertaken following discovery of the defect and, if necessary, repeated at specified intervals during operation under the terms of the (M)MEL to maintain the required level of safety.

XV



Normally, these procedures are accomplished by maintenance personnel. However, other personnel may be qualified and authorised to perform certain functions.

Note: When an item is annotated (O)/(M), the “/” is defined as “and/or”, which shows that there may be different options available in respect of the MEL procedures.

12. “Visual Flight Rules (VFR)”: is as defined by National Authority Operating Requirements. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

13. “Icing Conditions”: An atmospheric condition that may cause ice to form on the aeroplane or in the engines.

14. “Visible Moisture”: An atmospheric environment containing water in any form that can be seen in natural or artificial light, i.e. clouds, fog, rain, sleet, hail, snow.

15. “Flight Hour”: The time from the moment an aeroplane leaves the surface of the earth until it touches it at the next point of landing.

16. “Flight”: For the purpose of a MEL, a flight is the period of time between the moment when an aeroplane begins to move by its own means, for the purpose of preparing for take-off, until the moment the aeroplane comes to a complete stop on its parking area, after the subsequent landing (and no subsequent take-off).

17. “Flight day”: A 24 hour period (from midnight to midnight) either UTC or local time as established by the operator, during which at least one flight is initiated for the affected aeroplane.

18. “Authority”: The competent regulatory authority according to the country of registry.

19. “Deleted”: When applied to an item number, indicates that the item was previously listed but is now required to be operative.

XVI



20. “Combustible (Material)”: refers to material which is capable of catching fire and burning. In particular: If a MEL item prohibits loading of combustible (or flammable or inflammable) material, no material may be loaded except the following:

1) Cargo handling equipment (unloaded, empty or with ballast);

2) Fly away kits (excluding e.g. cans of hydraulic fluid, cleaning solvents, batteries, capacitors, chemical generators, etc.); and

Note: If serviceable tires are included they should only be inflated to a minimum pressure that preserves their serviceability.

3) Inflight service material (return catering – only closed catering trolley/boxes, no newspapers, no alcohol or duty free goods).

21. “System”: System means the group of directly related components which together perform a specified function, for example “RPM Indication System” would include the RPM Indicator, tachometer generator, circuit breaker and associated circuitry.

22. “Dispatch”: The point at which an aeroplane first moves under its own power for the purpose of commencing a flight.

Note: The MMEL/MEL applies to all defects that occur up to the point of dispatch, and comes into effect again when the aeroplane next comes to rest at the end of its flight.

23. “Deactivated” and “Secured”: means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by the operator.

24. "Administrative control item": means an item listed by the operator in the MEL for tracking and informational purposes. It may be added to an operator's MEL by approval of the National Authority provided no relief is granted, or provided conditions and limitations are contained in an approved document (i.e. Structural Repair Manual, airworthiness directive, etc.). If relief other than that granted by an approved document is sought for an administrative control item, a request must be submitted to the National Authority. If the request results in review and approval by the OEB, the item becomes an MMEL item rather than an administrative control item.

25. "Excess Items": means those items that have been installed that are redundant to the requirements of the Operating Requirements

XVII



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

2. “Considered Inoperative”: as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used or operated until the original deferred item is repaired. Additional 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.

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

4. “MCTOM”: means the Maximum Certificated Takeoff Mass.

5. “MAPSC”: means the Maximum Approved Seating Configuration

XVIII


HIGHLIGHTS OF REVISION

Note: Updated entire document’s number scheme to reflect those changes made in 560XL FAA MMEL Revision 6.

Reformatted blank pages throughout the document.

21-10-05 Moved relief from chapter 33 and added relief for holder assembly.

21-21-04 Revised relief title. Relief was previously listed as Pilot Wemac.

21-21-05 Added new relief for cabin air outlet.

21-30-02 Revised relief.

21-30-02-03 Relief removed for manual control mode.

21-32-01 Clarified relief between pressurized and unpressurized relief.

21-32-02 Clarified relief between pressurized and unpressurized relief.

21-32-03 Revised Remarks and Exceptions, Deleted relief for Manual Mode.

21-33-02 Clarified relief between pressurized and unpressurized relief and added gravel operation restriction.

21-50-01 Removed unnecessary proviso item.

21-60-01 Removed unnecessary proviso item.

21-62-01 Revised proviso to remove requirement for AFM procedures be followed.

22-10-01 Removed note and incorporated into proviso. Removed A/-/0 relief.

22-10-02 Removed note and incorporated into proviso.


23-10-01 Deleted A/-/0 relief

23-10-01-04 Added relief for HF wire antenna.

23-20-03 Added note.

23-60-01 Added new relief for static wicks

24-21-01 Revised relief to add track engine operating time and maintenance schedule.

25-10-01 Revised title.

25-10-01-03 Combined recline and tilt function relief. Revised Remarks and Exceptions

25-10-01-06 Revised Remarks and Exceptions

25-10-02 Revised proviso and require alternate procedures be established.

XIX


HIGHLIGHTS OF REVISION (Continued)

25-10-05-01 Revised proviso for better definition.

25-10-07 Added relief for cockpit assist handle.

25-20-01 Revised title to include side facing seats. Added lumbar support and incorporated note 1 into proviso.

25-20-02 Added relief for refreshment center.

25-40-01 Revised relief combining separate relief items into one proviso.

25-60-01 Revised relief to reflect FAA MMEL

25-60-02 Revised relief to reflect FAA policy letter.

25-61-01 Revised title to include crew and passenger.

25-62-01 Revised relief to reflect FAA policy letter.

26-10-01 Revised proviso to remove unnecessary item.

27-20-01 Revised proviso to reflect FAA MMEL.


27-31-02 Added new relief for elevator trim position indicator tip.

27-51-01 Added new relief for flap position indictor tip.

27-60-01 Revised relief to include maximum airspeed restriction.

28-00-01 Removed locking dust cap relief.

28-40-01 Revised proviso adding three day restriction.

28-41-01 Removed relief for wing tank fuel quantity indicating system.

30-00-01 Revised proviso. 30-30-01 Revised relief to reflect FAA MMEL.

30-30-02 Relief removed for Standby pitot tube heater.

30-30-03 Revised relief to reflect FAA MMEL.

30-30-04 Revised relief to reflect FAA MMEL. 30-40-03 Added relief for surface seal protection system.

31-10-01 Added relief for autopilot mode controller AP button light. 31-10-02 Added new relief for autopilot mode controller YD engage light.

31-50-02 Removed relief for AP engage switch. 31-50-04-02 Removed relief for battery overtemp.

31-50-11 Removed relief for fuel quantity fault monitoring system.

31-50-12 Revised proviso. 31-50-16-01 Title revised to add failure to illuminate.

31-50-20 Removed relief for YD engage switch.

XX


HIGHLIGHTS OF REVISION (Continued)

33-10-01 Revised title and proviso. 33-20-01 Revised repair category and provisos.

33-20-03 Revised title and proviso.

33-40-01 Revised proviso requiring other operative lights and repairs made in three flight days.

33-40-10 Revised repair category, number installed, number required for dispatch, and proviso.

33-50-02 Relief moved to chapter 25.

33-50-03 Revised titles and added relief.

34-25-06-01 Revised proviso.

34-25-09 Revised proviso. 34-44-01 Added relief for runway awareness and advisory system.

34-44-02 Revised proviso from 5 further flights to 6.

34-45-01 Added relief for audio functions and airspace selection function. 35-00-01 Revised proviso.

35-00-02 Revised proviso.

35-00-03 Added relief for blowout Disc/Green label.

35-20-01 Reformatted relief for oxygen system, mask, and drop out panel. 46-00-01 Removed (M) procedures.

46-00-03 Relief removed. 46-00-04 Added relief.

49-20-01 Revised proviso.

49-50-01 Revised proviso. 52-10-01 Revised title.

52-10-02 Revised title. 52-10-04 Revised proviso.

52-10-06 Removed cabin door precatch relief. 73-30-01 Revised proviso to removed requirement for both fuel quantity indicating systems be

operative.

EUROPEAN AVIATION SAFETY AGENCY 23 October 2012 MASTER MINIMUM EQUIPMENT LIST

Cessna Citation 560XL Revision No: 1 Page: 21-1

(1) System & Sequence Numbers ATA 21 AIR CONDITIONING Item

(2) Rectification Interval (3) Number Installed (4) Number required for dispatch (5) Remarks or Exceptions

-21-01 Display Guidance Computer (DGC) Fan (IC FAN 1 or 2) (Units 5001 – 6000)

B 2 0 (O) May be inoperative provided operations are conducted per Aeroplane Flight Manual limitations and IC FAN 1 or 2 abnormal procedures.

-21-02 Display Unit (DU) Fan (DU 1, 2 or 3) Annunciator (Units 5501 – 6000)

B 3 0 (O) May be inoperative provided operations are conducted per Aeroplane Flight Manual limitations and IC FAN 1 or 2 abnormal procedures.

-21-03 Radome Fan (Units 5001 – 6000)

C 1 0 (O) May be inoperative provided operations are conducted per Aeroplane Flight Manual limitations and RADOME FAN abnormal procedures including a maximum ground operation time of 30 minutes with avionics on.

-21-04 Cockpit Air Outlet C - 0

-21-05 Cabin Air Outlet C - 0

- 21-06 Overhead Cabin Blower/Wemac Boost Fan (Units 5001-5500)

C 1 0

- 21-07 Cockpit Recirculation Fan C 1 0

-30-01 Emergency Pressurization System

C 1 0 (O) May be inoperative provided: a) Air cycle machine is operative, b) Both left and right bleed sources are

operative, and c) Aeroplane is operated at FL 250 or

below.





-30-02 Cabin Pressurization System C 1 0 (O)May be inoperative provided: a) Procedures for flight planning at

lower altitudes and supplemental oxygen use are established and used,

b) Cabin EMER DUMP is selected ON, c) Cabin altitude is set to 14,000 feet,

and d) Aeroplane is operated at 14,000 feet

MSL or below.

-01 Auto Schedule Control Mode C 1 0 May be inoperative provided: a) Cabin differential pressure gauge is

operative, b) Cabin altimeter is operative, c) Cabin rate indicator is operative, and d) Aircraft is operated at FL 410 or

below.

-02 Isobaric Control Mode C 1 0 May be inoperative provided: a) Cabin differential pressure gauge is

operative, b) Cabin altimeter is operative, c) Cabin rate indicator is operative, and d) Aeroplane is operated at FL 410 or

below.

-03 Manual Control Mode Deleted revision 1.





-32-01 Cabin Differential Pressure Gauge

-01 (Pressurized) C 1 0 (O) May be inoperative provided: a) Cabin altimeter is operative, b) Either auto schedule or isobaric

control mode is operative, and c) A chart is provided and used to

convert cabin and aeroplane altitude to differential pressure.

-02 (Unpressurized) C 1 0 (O) May be inoperative provided: a) Procedures for flight planning at




MSL or below.

-32-02 Cabin Altimeter

-01 (Pressurized) C 1 0 (O) May be inoperative provided: a) Cabin differential pressure gauge is

operative, and b) A chart is provided and used to

convert aeroplane altitude and differential pressure to cabin altitude.





MSL or below.





-32-03 Cabin Rate Indicator

-01 (Pressurized) C 1 0 May be inoperative provided: a) Cabin altimeter is operative, b) Cabin differential pressure gauge is

operative, and c) Either autoschedule or isobaric

control mode is operative.





MSL or below.

-33-01 Outflow Valve (Unpressurized)

C 2 0 (M) (O) May be inoperative provided: a) Procedures for flight planning at


b) At least one valve is removed, c) PRESS SOURCE selector remains

OFF, d) Cabin EMER DUMP is selected ON, e) Cabin altitude is set to 14,000 feet,

and f) Aeroplane is operated at 14,000 feet

MSL or below.





-33-02 Flow Control and Shutoff Valve

-01 (Unpressurised) C 2 0 (O) May be inoperative provided: a) Gravel operations are prohibited, b) Both flow control and shutoff valves

are verified CLOSED, c) Procedures for flight planning at


d) PRESS SOURCE selector remains OFF,

e) Cabin EMER DUMP is selected ON, f) Cabin altitude is set to 14,000 feet,

and g) Aeroplane is operated at 14,000 feet

MSL or below.

-02 (Pressurized) C 2 1 (O) One may be inoperative provided: a) Right side must be operative for

gravel operations, b) PRESS SOURCE selector remains

on the operative source, c) Failed flow control and shutoff valve

is CLOSED, and d) Aeroplane is operated at FL 250 or

below.





-50-01 Air Cycle Machine (Unpressurized)

C 1 0 (O) May be inoperative provided: a) Procedures for flight planning at


b) PRESS SOURCE selector remains OFF,

c) Cabin EMER DUMP is selected ON, d) Cabin altitude is set to 14,000 feet,

and e) Aeroplane is operated at 14,000 feet

MSL or below.

- 50-02 Freon/R134a Air Conditioning System (Units 5001 – 5500) (If Installed)

C 1 0 (M) May be inoperative provided Freon/R134a air conditioning system is deactivated.

-60-01 Cockpit/Cabin Air Temperature Control System (Unpressurized)

C 1 0 (O) May be inoperative provided: a) Procedures for flight planning at


b) Cabin PRESS SOURCE selector remains OFF,

c) Cabin EMER DUMP is selected ON, d) Cabin altitude is set to 14,000 feet,

and e) Aeroplane is operated at 14,000 feet

MSL or below.

-01 Automatic Mode C 2 0 May be inoperative provided the associated air temperature control system is operative in manual mode.

-02 Manual Mode C 2 0 May be inoperative provided the associated air temperature control system is operative in automatic mode.

-61-01 Cabin Temperature Remote Controller System

D 1 0





-62-01 Cabin Temperature Indicator

-01 Without Cabin Occupants C 1 0

-02 With Cabin Occupants C 1 0 (O) May be inoperative provided: a) Alternate means are established and

used to determine cabin temperature, and

b) Aeroplane is operated per Aeroplane Flight Manual COLD WEATHER OPERATIONS, Normal Procedures.

-62-02 Cockpit Temperature Indicator

C 1 0



(1) System & Sequence Numbers ATA 22 AUTOFLIGHT Item


-10-01 Autopilot B 1 0 (M) (O) One or more functions may be inoperative provided:

a) For the intended operations, any increase in crew workload caused by the inoperative functions has been considered,

b) Inoperative functions are deactivated as applicable,

c) Applicable operating minima do not require its use,

d) The navigation specifications of the route to be flown do not require their use, and

e) Aircraft is not operated RVSM.

-10-02 Yaw Damper B 1 0 (M) (O) May be inoperative provided: a) Yaw damper is deactivated, b) Autopilot is considered inoperative, c) Aircraft is not operated RVSM.

-10-03 Autopilot Disconnect Functions (Red, Yoke Mounted Quick Release Controls)

-01 C 2 1 One may be inoperative for pilot not flying provided:

a) Autopilot is not used below 1500 feet AGL, and

b) Approach minimums do not require use of the autopilot.

-02 B 2 0 (M) (O) May be inoperative provided: a) Autopilot is considered inoperative, b) Electric trim is considered

inoperative, c) Aircraft is not operated RVSM.



(1) System & Sequence Numbers ATA 22 AUTOFLIGHT Item


-10-04 Go-Around Button C 2 1

C 2 0 May be inoperative provided: a) Flight director is not used for takeoff

or during go-around, and b) Autopilot is disconnected for go-

around.

NOTE: FMS missed approach procedure must be activated via the FMS CDU.

-10-05 Autopilot/Flight Director Touch Control Steering (TCS or AP SYNC)

C 2 0



(1) System & Sequence Numbers

ATA 23 COMMUNICATIONS Item

(2) Rectification Interval (3) Number Installed (4) Number required for dispatch (5) Remarks or Exception

-00-01 VHF Communications System

C - 1 May be inoperative provided: a) COMM 1 is operative, and b) Aircraft is operated VFR over routes

navigated by reference to visual landmarks.

-00-02 Flight Phone System (If Installed)

D - 0

-01 Cockpit Handset D - 0

-02 Cabin Handset D - 0

-00-03 Radio Tuning Control on Cursor Control Panel (CCP) (Units 6001 and on)

C 2 0 May be inoperative provided direct tuning is operative on both cockpit display units (CDUs).

-00-04 SATCOM (If Installed)

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

-00-05 Radio Management Unit (RMU) (Units 5001 – 6000)

C 2 1 (O) One may be inoperative provided: a) Remaining RMU is operative, and b) Auxiliary com/nav control display unit

is verified operative.

-00-06 Cockpit Voice Recorder (CVR) (If installed)

A 1 0 One or more may be inoperative provided: a) The Aeroplane does not exceed 8

further consecutive flights with the cockpit voice recorder inoperative,

b) A maximum of 72 hours have elapsed since the cockpit voice recorder was found to be inoperative, and

c) Any flight data recorder required to be carried is operative.

NOTE: This alleviation is not applicable to combined CVR/FDRs.






-10-01 High Frequency (HF) Communication System (If Installed)

-01 D - - Any in excess of those required for the intended route, may be inoperative.

-02 C - 1 (O) Any in excess of one may be inoperative for flight on a route that requires two Long Range Communication Systems provided:

a) SATCOM air-ground communications with relevant Air Navigation Service Provider(s) is available over the route to be flown,

b) SATCOM voice function is operative, c) Prior to each flight, coordination with

the appropriate Air Navigation Service Provider(s) is established where INMARSAT codes, or equivalent, are not available whilst using SATCOM voice function, and

d) Alternate communication procedures are established and used.

NOTE1: SATCOM is to be used only as a backup to normal HF Communications, unless otherwise authorized by the appropriate ATS facilities.

NOTE 2: For all routes, consider the need for ACAS.

-03 A - 1 (O) Any in excess of one may be inoperative for a maximum of 3 calendar days, for flight on a route that requires two Long Range Communication Systems provided alternate communication procedures are established and used.

(Continued)






-10-01 High Frequency (HF) Communication System (If Installed) (Continued)

NOTE 1: When the route enters airspace for which an In Flight Blind Broadcast Procedure exists, select the appropriate I.F.B.F. VHF frequency and apply the procedure.

NOTE 2: For all routes, consider the need for ACAS.

-04 High Frequency (HF) Externally Mounted Wire Antenna (If installed)

C - 0 (M) May be inoperative or missing provided: a) Antenna and associated mounting

hardware are removed, and b) High Frequency (HF) communication

system is considered inoperative.

-20-01 Selective Call (SELCAL) Systems (If Installed)

-01 D - 0 May be inoperative provided procedures do not require its use.

-02 C - 0 (O) May be inoperative provided alternate procedures are established and used.

-20-02 Individual SELCAL (VHF/UHF/HF) Channel (If Installed)








-20-03 Datalink (AFIS/ACARS/UNILINK) (If Installed)


NOTE: Subscription based service status does not constitute inoperative equipment.


NOTE: Subscription based service status does not constitute inoperative equipment.

-40-01 Passenger Address (PA) System

-01 Passenger Configuration C 1 0 (O) May be inoperative provided alternate normal, abnormal, and emergency procedures, and/or operating restrictions are established.

NOTE: Any function that operates normally may be used.

-02 Cargo Configuration D 1 0 May be inoperative provided procedures do not require its use.

-40-02 Automatic Cabin Briefer (If Installed)

D 1 0 (O) May be inoperative provided cabin occupants are briefed by alternate means.

-50-01 Cockpit Overhead Communication Speaker

C 2 1 One may be inoperative provided: a) Affected speaker is not required for

procedures, and b) A headset is installed and used for

associated inoperative speaker including headset use during emergency procedures.






-50-02 Hand-Held Microphone C 2 0 May be inoperative provided associated headset/boom microphone is operative.

-50-03 Headset with Boom Microphones

D - - Any in excess of one headset (including boom microphone) for each required crew member on flight deck duty may be missing or inoperative.

-60-01 Static Wick

-01 Left Wing C 6 5 Wingtip static wick must be operative.

-02 Right Wing C 6 5 Wingtip static wick must be operative.

-03 Empennage Stinger C 1 0

-04 Airborne Flight Information system (AFIS) (If installed) installed)

C 1 0



(1) System & Sequence Numbers ATA 24 ELECTRICAL POWER Item


-00-01 Ground Power Dispatch Switch (If Installed)

C 1 0

-21-01 AC Bearing (AC BEARING, L or R annunciator illuminated)

A 2 1 (O) May be inoperative provided: a) Procedures for tracking engine

operating time on affected side are established and used, and

b) AC Alternator Bearing maintenance is accomplished within time limits required by AC BEARING L or R annunciator aeroplane flight manual procedure.

-31-01 Battery Temperature Indicator (If Installed)

C 1 0

-35-01 Engine Driven Generator A 2 1 (O) One may be inoperative provided: a) Aeroplane is equipped with an APU, b) APU is operative and used entire

flight, c) APU generator is verified operative

and is used entire flight, d) Aeroplane is operated at FL 300 or

below, and e) Repairs are made within 3 flight

days.

-35-02 Auxiliary Power Unit (APU) Generating System (If Installed)

C 1 0 May be inoperative provided APU generator switch remains off.

-40-01 External Power Receptacle C 1 0

-50-01 AC Cockpit Outlet (If Installed)





(1) System & Sequence Numbers ATA 24 ELECTRICAL POWER Item





(1) System & Sequence Numbers ATA 25 EQUIPMENT/FURNISHINGS Item


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

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

-00-02 Security System (Securaplane) (If Installed)

D 1 0

-10-01 Flight Crew Seat (per seat)

-01 Armrest

-01 Remain in Aeroplane C - 0 May be inoperative provided a) seat position is acceptable for crew,

and b) Armrest is stowed in retracted

position.

-02 Removed from Aeroplane C - 0 (M) May be inoperative provided seat position is acceptable to the flight crew member.

NOTE: If an inoperative armrest will hinder an emergency evacuation or any other flight duties is should be removed.

-02 Lumbar Support (If Installed) C 1 0

-03 Recline/Tilt Function B 1 0 (M) May be inoperative provided: a) Affected seat is secured or locked in

a fixed position, b) Affected seat is failed in a position

that permits normal visibility, c) Full flight control movement is

available, and d) Crewmember can reach all

necessary controls and equipment while restrained.

-04 Restraint Buckle Protective Padding (If installed)

C - 0 May be missing or inoperative.

(Continued)





-10-01 Flight Crew Seat (per seat) (Continued)

-05 Thigh Support (If installed)

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

-06 Vertical Adjustment B 1 0 (M) May be inoperative provided: e) Affected seat is secured or locked in

a fixed position, f) Affected seat is failed in a position

that permits normal visibility, g) Full flight control movement is

available, and h) Crewmember can reach all

necessary controls and equipment while restrained.

-10-02 Pilot or Copilot Eye Locator Reference Ball

C 3 0 (O) May be inoperative or missing provided alternate procedures are developed and used for eye position reference.

-10-03 Yoke Mounted Chart Holder (If Installed)

C 2 0

-10-04 Yoke Mounted Chart Holder Light (If Installed)

C 2 0

-10-05 Cockpit Flashlight and Holder Assembly (If Installed)

-01 Flashlight C 2 0 May be inoperative or missing provided each required member has an operative independent portable light readily available when seated at designated station.

-02 Holder Assembly C 2 0 May be inoperative provided associated flashlight is stowed by alternate means.

-10-06 Cockpit Sunvisor System and/or Attach Mechanism

D - 0 May be missing or inoperative provided pilot’s field of vision is not obstructed.

-10-07 Cockpit Assist Handle D - 0





-20-01 Passenger Seat (Including Side Facing Seats)

D - - May be inoperative provided: a) Seat does not block an

emergency exit, b) Seat does not restrict any cabin

occupant from access to the aisle,

c) Affected seat(s) are blocked and placarded "DO NOT OCCUPY", and

d) A seat with an inoperative seatbelt is considered inoperative.

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

-01 Armrest

-10 With Recline Mechanism D - - (M) May be inoperative or missing and seat occupied provided:

a) Armrest does not block an emergency exit,

b) Armrest does not restrict any passenger from access to the main Aeroplane aisle, and

c) If armrest is missing, seat is secured in the full upright position.

NOTE: Any damage to passenger seats and components must not be detrimental to passenger safety.

-20 Without Recline Mechanism D - - May be inoperative or missing and seat occupied provided:

a) Armrest does not block an emergency exit, and

b) Armrest does not restrict any passenger from access to the main Aeroplane aisle.

(Continued)





-20-01 Passenger Seat (Including Side Facing Seats) (Continued)

-02 Headrest C - - May be inoperative and seat occupied provided headrest is failed in placarded taxi, takeoff and landing position.

C - - May be missing or inoperative in other than placarded taxi, takeoff, and landing position provided affected seat is considered inoperative.

NOTE: Any damage to passenger seats and components must not be detrimental to passenger safety.

-03 Recline Mechanism C - - May be inoperative and seat occupied provided seat back is immovable in the upright position.

D - - (M) May be inoperative and seat occupied provided seat back is secured in full upright position.

-04 Floor Tracking Mechanism C - - May be inoperative and seat occupied provided

a) Seat base is failed immovable, b) Seat does not restrict any cabin

occupant from access to the main aircraft aisle,

c) Seat is positioned so it will not affect emergency egress.

-05 Seat Tracking and Swivel Mechanism

C - - May be inoperative and seat occupied provided seat is failed immovable in placarded taxi, takeoff and landing position.

-06 Lumbar Support (If installed)

D - -





-20-02 Refreshment Center

-01 Hot Liquid Storage System Heater

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

-40-01 Ashtray A - 1 Any in excess of one may be inoperative for three flight days.

-60-01 Emergency Vision Assurance System (EVAS) (If Installed)

D - 0 May be inoperative, missing, or removed if removal is directed by the EVAS Operator’s Guide provided procedures do not require its use.

-60-02 Emergency Medical Equipment

-01 Automatic External Defibrillator (AED) and/or Associated Equipment (If Installed)

D - 0 (O) May be incomplete, missing or inoperative provided AED is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit.

-02 Emergency Medical Kit (EMK) and/or Associated Equipment (If Installed)

D - 0 (O) May be incomplete, missing or inoperative provided EMK is resealed in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit.

-03 First Aid Kit (FAK) and/or Associated Equipment

D - 1 Any in excess of those required may be incomplete or missing.

-61-01 Life Jackets (Crew and Passenger) (If installed)

D - - Any in excess of the minimum required may be missing or inoperative provided:

a) Inoperative lifejacket is placarded inoperative, removed from the installed location and placed out of sight so it cannot be mistaken for a functional unit, and

b) Required distribution of serviceable lifejackets is maintained.





-62-01 Emergency Locator Transmitter (ELT)

-01 Survival ELT(S) (If installed)

D - - (M) Any in excess of those required may be missing or inoperative provided the inoperative equipment is placarded inoperative, removed from the installed location, and placed out of sight so it cannot be mistaken for a functional unit.

-02 Fixed ELTs (If installed)

D - - (M) Any in excess of those required by operating requirements may be missing or inoperative provided system is deactivated.

A - 0 May be inoperative provided repairs are made within 6 further flights or 25 flying hours, whichever occurs first.

-64-01 Life Raft (If Installed)

C - - Any in excess of those required may be missing or inoperative provided the inoperative equipment is placarded inoperative, removed from the installed location, and placed out of sight so it cannot be mistaken for a functional unit.



(1) System & Sequence Numbers ATA 26 FIRE PROTECTION Item


-10-01 APU Fire Detection System (If installed)

C 1 0 May be inoperative provided APU is considered inoperative

-11-01 Baggage Smoke Detector (If installed)

C - - Any in excess of those required by regulations may be inoperative.

-12-01 Lavatory Smoke Detector (If Installed)

C - - Any in excess of those required by regulations may be inoperative.

-22-01 Portable Fire Extinguisher D - - Any in excess of those required by regulations may be inoperative or missing provided:

a) Inoperative fire extinguisher is tagged inoperative, removed from the installed location and stored out of sight so it cannot be mistaken for a functional unit, and

b) Required distribution is maintained.



(1) System & Sequence Numbers ATA 26 FIRE PROTECTION Item





(1) System & Sequence Numbers ATA 27 FLIGHT CONTROLS Item


-20-01 Rudder Pedal Adjustment System

B 4 2 (M) (O) May be inoperative provided: a) Two pedal adjustments are not

inoperative at the same pilot station, b) Affected pedal is positioned in a

detent and adjustment mechanism is secured from movement,

c) Unaffected pedal is adjusted to match affected pedal, and

d) Pilot with affected pedal verifies full control movement and brake application is available while restrained, prior to each flight.

-31-01 Electric Trim B 1 0 (M) (O) May be inoperative provided: a) Electric trim system is deactivated, b) Autopilot is considered inoperative,

and c) Aeroplane is not operated RVSM.

-31-02 Elevator Trim Position Indicator Tip

C 1 0 (M) May be missing provided an alternate means of marking Indicator Tip is established and used.

-42-01 Horizontal Stabilizer Actuator A 1 0 (M) (O) May be inoperative provided: a) Horizontal stabilizer is in the

negative (–) 2 degree (takeoff) position,

b) STAB CONTROL circuit breaker is pulled and secured,

c) Airspeed is limited to 200 knots/.62 M or less,

d) Touch and go landings are not conducted,

e) Aeroplane is operated at FL 410 or below, and

f) Repairs are made within two flight days.

-51-01 Flap Position Indicator Tip C 1 0 (M) May be missing provided an alternate means of marking Indicator Tip is established and used.



(1) System & Sequence Numbers ATA 27 FLIGHT CONTROLS Item


-60-01 Speed Brake System B 1 0 (M) (O) May be inoperative provided: a) Speed brakes are secured stowed, b) Aeroplane is operated at 41,000 feet

MSL or below, c) Maximum airspeed for operation is

limited to Vmo/Mmo of 280 KIAS and .70 mach respectively, and

d) Steep approaches are not conducted.

-70-01 Control Lock System C 1 0 (O) May be inoperative in the unlocked position provided full flight control and throttle movement is available.



(1) System & Sequence Numbers ATA 28 FUEL Item


-00-01 Single Point Refueling System

C 1 0

-01 Locking Dust Cap Deleted revision 1.

-10-01 Over Wing Refueling Cap Lock (If installed)

D - 0

-40-01 Fuel Low Level Indicating System

A 2 1 (O) One may be inoperative provided: a) Procedures for monitoring fuel

quantity are established and used, and

b) Repairs are made within three flight days.

-41-01 Wing Tank Fuel Quantity Indicating System

Deleted revision 1.

-43-01 Fuel Temperature Indication C 2 1



(1) System & Sequence Numbers ATA 28 FUEL Item





(1) System & Sequence Numbers ATA 30 ICE AND RAIN PROTECTION Item


-00-01 Drain Mast Heater C - 0 (M) May be inoperative provided: a) Refreshment center drains and

lavatory basins are not used, b) Any remaining ice and/or fluid is

removed from the refreshment center,

c) Hot liquid overfill drain is placarded “DRAIN HEAT INOP, DO NOT USE”, and

d) A placard is placed on the instrument panel stating “Pilot Relief Tube INOP” and Pilot Relief Tube is not used.

-00-02 Rosemount Ram Air Temperature (RAT) Probe Heater (Units 5001 – 6000)

C 1 0 May be inoperative provided: a) Aeroplane is not operated in visible

moisture with ram air temperature of +10 degrees C or below, and

b) Aeroplane is not operated in known or forecast icing conditions.

-10-01 Wing Bleed Air Anti-Ice System Failed Off (No Flow)

C 2 1 (M) One may be inoperative provided: a) Aeroplane is not operated in visible



-10-02 Pneumatic Tail De-Ice System

C 1 0 May be inoperative provided: a) Aeroplane is not operated in visible







-20-01 Engine Anti-Ice System

-01 Anti-Ice Failed On (Flow)

C 2 0 (M) (O) May be inoperative provided: a) Takeoff and landing field

temperatures are not in excess of +10 degrees C, and

b) If only one system has failed, the operational system is also selected ON.

-02 Anti-Ice Failed Off (No Flow)

C 2 1 (M) One may be inoperative provided: a) Affected engine anti-ice is secured

for no flow, b) Aeroplane is not operated in visible


c) Aeroplane is not operated in known or forecast icing conditions.

-30-01 Pilot and Copilot Pitot Heater (Standby Excluded)

B 2 1 May be inoperative provided: a) Aeroplane is not operated in visible

moisture with ram air temperature of +10 degrees C or less in flight,

b) Aeroplane is not operated in known or forecast icing conditions,

c) Aeroplane is operated VFR only, and d) Aeroplane is not operated at night.

-30-02 Standby Pitot Tube Heater Deleted Revision 1.

-30-03 Pilot and Copilot Pitot Static Port Heater (Standby Excluded)

B 4 3 (O) One may be inoperative provided: a) Standby static port heater is verified

operative, b) Aeroplane is not operated in visible

moisture with ram air temperature of +10 degrees C or less in flight,

c) Aeroplane is not operated in known or forecast icing conditions,

d) Aeroplane is operated VFR only, and e) Aeroplane is not operated at night. f) Aeroplane is not operated RVSM.





-40-01 Rain Removal System (Forced Air)

C 1 0 May be inoperative provided Aeroplane is not operated in precipitation within 5 nautical miles of airport used for takeoff or intended landing.

-40-02 Windshield Anti-Ice System C 2 1 One may be inoperative provided: a) Aeroplane is not operated in visible

moisture with ram air temperature of +10 degrees C or less in flight, and


-40-03 Surface Seal Protection System

C 2 0 May be inoperative provided operations are not conducted in known or forecast precipitation within the arrival and departure areas.



(1) System & Sequence Numbers ATA 31 RECORD & INDICATING Item


-00-01 Quick Access Recorder (QAR) (If installed)

C 1 0 (M) (O) May be inoperative for Flight Data Monitoring (FDM) purposes provided approved alternate procedures, if appropriate to other programmes using associated data, are established and used.

-10-01 Autopilot Mode Controller AP Button Light (units 5001-6000)

B 1 0 (O) May be inoperative provided flight crew verifies AP ON indication is displayed on both PFDs when the autopilot is engaged.

-10-02 Autopilot Mode Controller YD Engage Light (units 5001-6000)

B 1 0 (O) May be inoperative provided flight crew verifies yaw damper is disconnected prior to every flight.

-20-01 Auxiliary Power Unit (APU) Hour Meter (If installed)

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

-20-02 Clock C - 0 May be inoperative provided an accurate timepiece is operative on the flight deck indicating the time in hours, minutes, and seconds.

NOTE: On the basis that the timepiece required does not need to be approved, an accurate pilot’s wristwatch which indicates hours, minutes, and seconds would be acceptable.

-20-03 MAX-VIZ EVS-1000 Enhanced Vision System (EVS) (If installed)

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

-20-04 Flight Hour Meter C 1 0 (O) May be inoperative provided flight time is tracked by alternate means.

-20-05 N1 Reminder (Mechanical or Electric) (Units 5001 – 6000)

D 1 0





-20-06 Throttle Detent Indicating Light/Indication (Units 5001 – 6000) (If Installed)

D 6 0

-30-01 Flight Data Recorder (FDR) System (If installed)

A - 0 One or more may be inoperative provided: a) The Aeroplane does not exceed 8

further consecutive flights with the flight data recorder inoperable,

b) Not more than 72 hours have elapsed since the flight data recorder was found to be inoperable, and

c) Any cockpit voice recorder required to be carried is operative.

NOTE1: The flight data recorder is considered to be inoperative when any of the following conditions exist:

a) Loss of the flight recording function is evident to the flight crew during the pre-flight check e.g. by means of a system status monitor, or

b) The need for maintenance has been identified by the system monitors, where available, with the setting of an indicator and the cause of that setting has not been determined, or

c) Analyses of recorded data or maintenance actions have shown that more than 5% of the total number of individual parameters (variable and discrete) required to be recorded for the particular Aeroplane, are not being recorded properly.

NOTE 2: Where improper recording affects 5% of the parameters or less, timely corrective action will need to be taken by the Aeroplane operator in accordance with approved maintenance procedures.





- 50-01 AIR DUCT O'HEAT, CKPT or CAB Annunciator (Units 5001 – 6000)

C 2 0 (O) May be inoperative (failure to illuminate) provided:

a) PRESS SOURCE selector switch remains OFF,

b) Cabin EMER DUMP is selected on, c) Cabin altitude is set to 14,000 feet,


MSL or below.

-50-02 AP ENGAGE Switch Annunciator (Units 5001 – 6000)

Moved to ATA 34

-50-03 APU Oil Service Light (If Installed)

C - 0 (M) (O) May be inoperative (failure to illuminate) provided:

a) APU oil level is verified prior to each flight, and

b) APU operating times are tracked.

-50-04 Battery Overtemp Indication

-01 BATT O'TEMP Annunciator (Units 5001 – 6000)

C 1 0 May be inoperative (failure to illuminate) provided Aeroplane is equipped with a lead-acid battery.

-02 BATTERY OVERTEMP Red CAS Message (Units 6001 and on)

Deleted Rev 1.

-50-05 Cabin Altitude Warning System Indication

-01 CAB ALT Annunciator (Units 5001 – 6000)

C 1 0 (O) May be inoperative (failure to illuminate) provided Aeroplane is operated at 14,000 feet MSL or below.

-02 CABIN ALTITUDE Red CAS Message (Units 6001 and on)

C 1 0 (O) May be inoperative (failure to illuminate) provided Aeroplane is operated at 14,000 feet MSL or below.





-50-06 Cabin Door Indication

-01 CABIN DOOR Annunciator (Units 5001 – 6000)

B 1 0 (O) May be inoperative (failure to illuminate or extinguish) provided:

a) Lock flags are visible in sight glass locations in the door,

b) Cabin door vent is verified closed with the cabin door shut,

c) Internal and external door handles are verified correctly stowed,

d) Passenger seat belt sign is on for duration of flight, and

e) Aeroplane is operated at FL 250 or below.

02 CABIN DOOR Amber CAS Message (Units 6001 and on)



b) Cabin door vent is verified closed, with the cabin door shut,

c) Internal and external door handles are verified correctly stowed,



03 Light System (6-Pack) B 1 0 (O) May be inoperative (failure to illuminate or extinguish) provided:


b) Internal and external door handles are verified correctly stowed,

c) Cabin door vent is verified closed with the cabin door shut,







-50-07 Cabin Door Seal Indication

-01 DOOR SEAL Annunciator System (Units 5001 – 6000)


a) Door seal inflation is verified prior to each flight, and

b) Aeroplane is operated at FL 250 or below.

-02 CABIN DOOR SEAL Amber CAS Message (Units 6001 and on)


a) Door seal inflation is verified prior to each flight, and

b) Aeroplane is operated at FL 250 or below.

-50-08 Emergency Pressurization Indication

-01 EMER PRESS Annunciator (Units 5001 – 6000)

C 1 0 (M) May be inoperative (failure to illuminate) provided the emergency pressurization system is verified operative.

-02 EMERGENCY PRESSURIZATION Amber CAS Message (Units 6001 and on)

C 1 0 (M) May be inoperative (failure to illuminate) provided the emergency pressurization system is verified operative.

-50-09 Engine Anti Ice Indication

-01 ENG ANTI-ICE, L or R Annunciator (Units 5001 – 6000)

B 2 1 One may be inoperative (failure to illuminate) provided:

a) Aeroplane is not operated in visible moisture with ram air temperature of +10 degrees C or below, and


(Continued)





-50-09 Engine Anti Ice Indication (Continued)

-02 ENG ANTI-ICE COLD, L - R Amber or White CAS Message (Units 6001 and on)

B 2 1 One may be inoperative (failure to illuminate) provided:



-50-10 Exterior Door Unlocked Indication

-01 ACC DOOR UNLOCKED, NOSE or TAIL Annunciator System (Units 5001 – 6000)

C 2 0 May be inoperative (failure to illuminate or extinguish) provided flight crew verifies by physical inspection the associated door is closed and latched before each departure.

-02 NOSE DOOR Amber CAS Message (Units 6001 and on)

C 1 0 May be inoperative (failure to illuminate or extinguish) provided flight crew verifies by physical inspection the door is closed and latched before each departure.

-03 TAILCONE ACC DOOR Amber CAS Message (Units 6001 and on)


-04 BATTERY DOOR Amber CAS Message (Units 6001 and on)


-05 AFT BAGGAGE DOOR Amber CAS Message (Units 6001 and on)






-50-11 Fuel Quantity Fault Monitoring System

-01 FUEL GAUGE, L or R Annunciator (Units 5001 – 6000)

Deleted Revision 1.

-02 FUEL GAUGE, L – R Amber CAS Message (Units 6001 and on)

Deleted Revision 1.

-50-12 Generator (DC) Indication

-01 GEN OFF, L or R Annunciator (Units 5001 – 6000)

C 2 1 (O) One may be inoperative (failure to illuminate) provided affected system is verified operative prior to flight.

-02 DC GENERATOR OFF L - R Amber CAS Message (Units 6001 and on)

C 2 1 (O) One may be inoperative (failure to illuminate) provided affected system is verified operative prior to flight.

-50-13 Hydraulic Flow Indication

-01 LO HYD FLOW, L or R Annunciator (Units 5001 – 6000)

C 2 1 (O) May be inoperative (failure to illuminate) provided hydraulic system operation is verified with only the affected side engine operating prior to each flight.

-02 HYDRAULIC FLOW LOW Amber CAS Message (Units 6001 and on)

C 2 1 (O) May be inoperative (failure to illuminate) provided hydraulic system operation is verified with only the affected side engine operating prior to each flight.

-50-14 Hydraulic Fluid Level Indication

-01 LO HYD LEVEL Annunciator (Units 5001 – 6000)

C 1 0 (O) May be inoperative (failure to illuminate) provided adequate fluid level is verified before each flight.

-02 HYDRAULIC FLUID LEVEL LOW Amber CAS Message (Units 6001 and on)

C 1 0 (O) May be inoperative (failure to illuminate) provided adequate fluid level is verified before each flight.





-50-15 Lavatory Door Indication

-01 LAV DOOR Annunciator System (Units 5001 – 6000)

B 1 0 (O) May be inoperative (failure to illuminate or extinguish) provided flight crew verifies that the lavatory door is latched open prior to every takeoff and landing.

-02 LAVATORY DOOR Amber CAS Message (Units 6001 and on)

B 1 0 (O) May be inoperative (failure to illuminate or extinguish) provided flight crew verifies that the lavatory door is latched open prior to every takeoff and landing.

-50-16 Master Warning/Caution Light System

-01 Master Warning Light (Failure to illuminate)

C 2 1

-02 Master Warning Reset Function

C 2 1

-03 Master Caution Light C 2 1

-04 Master Caution Reset Function

C 2 1

-50-17 Pitot/Static Heater Indication

-01 P/S HTR, L or R, or STBY P/S HTR Annunciators (Units 5001 – 6000)

B 3 1 (O) May be inoperative (failure to illuminate) provided:

a) Pitot/static heater systems are verified operative before each takeoff,

b) Aeroplane is not operated in visible moisture with ram air temperature of +10 degrees C or below, and


(Continued)





-50-17 Pitot/Static Heater Indication (Continued)

-02 PITOT/STATIC COLD L - R-STBY Amber or White CAS Message (Units 6001 and on)

B 2 1 (O) May be inoperative (failure to illuminate) provided:

a) Pitot/static heater systems are verified operative before each takeoff,

b) Aeroplane is not operated in visible moisture with ram air temperature of +10 degrees C or below, and


-50-18 TAWS Annunciator (PULL UP, TERRAIN, BELOW G/S) (Units 5001 – 5500)

B - 0 May be inoperative (failure to illuminate) provided affected aural warning is operative.

-50-19 Wing Anti-Ice Indication

-01 WING ANTI-ICE, L or R Annunciator (Units 5001 – 6000)

C 2 1 One may be inoperative (failure to illuminate) provided:



-02 WING ANTI-ICE COLD, L - R Amber or White CAS Message (Units 6001 and on)

C 2 1 One may be inoperative (failure to illuminate) provided:







-50-20 YD ENGAGE Switch Annunciator (Units 5001 – 6000)

Moved to ATA 34

-50-21 Flight Director Mode Selector Annunciator (Units 5001 – 6000)

C - 0 (O) May be inoperative provided flight crew verifies annunciation(s) displayed on the PFD is appropriate to function selected.



(1) System & Sequence Numbers ATA 33 LIGHTS Item


-10-01 Flight Deck Lighting System (Excluding Internally Lighted Annunciators and Buttons, and Standby Flight Instrument Lighting)

C - - Individual lights may be inoperative provided remaining lights are:

a) Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided,

b) Positioned so that direct rays are shielded from flight crewmembers eyes,

c) Lighting configuration and intensity is acceptable to the flight crew, and

d) Flight deck emergency (flood and aux panel) lighting is operative.

-10-02 Windshield Ice Detect Light

-01 C 2 1 (O) One may be inoperative provided alternate procedures are established and used.

-02 C 2 0 May be inoperative provided aeroplane is not operated at night.

-20-01 Cabin Interior Lighting System (Excludes Cabin Emergency Lighting System)

-01 C - 0 (O) Individual lights may be inoperative for night operation provided:

a) Sufficient lighting is operative for crew to perform required duties,

b) Cabin emergency lighting is verified operative, and

c) Sufficient lighting is operative for carrying cabin occupants at night.

-02 C - 0 (O) May be inoperative provided: a) Cabin emergency lighting verified

operative, and b) No cabin occupants are carried.





-20-02 Divider Accent Light

-01 Incandescent C - -

-02 LED C - -

-20-03 Cabin Signs (Fasten Seat Belt and No Smoking Signs) (Excludes Cabin Emergency Lighting System)

-01 C - - (O) May be inoperative provided alternate procedures for notifying cabin occupants are established and used.

-02 C - - (O) May be inoperative provided: a) Passenger Address System is

operative and can be clearly heard throughout the cabin during flight, and

b) Alternate procedures are established and used to notify passengers when seat belts must be fastened and smoking is prohibited as appropriate.

-03 C - 0 May be inoperative provided no passengers are carried.

-20-04 Exit Sign Lighting (Incandescent)

C - - Two light bulbs may be inoperative in each fixture.

-20-05 Light Source for Pyramid Exit Sign (LED) (Units 5501 and on)

C 16 14

-40-01 Anti-Collision Light System (Strobes)

C - - May be inoperative provided the Aeroplane is not operated at night.





-40-02 Fuselage Mounted Taxi/Landing Light

-01 C 2 0 May be inoperative provided the Aeroplane is not operated at night.

-02 C 2 1 50% of taxi lights may be inoperative for night operations.

-40-03 Ground Recognition Light (Flashing Beacon)

C 1 0 (O) May be inoperative for daylight operations provided all white anti-collision lights are operative.

NOTE: If the red beacon light is inoperative, alternative procedures must be developed and used when the aeroplane is on the ground with the engine(s) running.

-40-04 Logo Light C 2 0

-40-05 Navigation/Position Lights C 1 0 May be inoperative provided aeroplane is not operated at night.

-40-06 Pulse Light System (If Installed)

D 1 0

-40-07 Tail Cone Baggage Compartment Light

C 3 0

-40-08 Tail Cone Maintenance Compartment Light

C 1 0

-40-09 Toilet Service Light C - 0 (O) May be inoperative provided alternate procedures are established and used.

-40-10 Wing Illumination/Inspection Lights

-01 D - 0 One or more may be inoperative for daylight operations.

-02 C 2 1 One may be inoperative provided ground deicing procedures do not require its use.





-40-11 Wing Leading Edge Landing Light

-01 C - 0 All may be inoperative for daylight operations.

-02 B 2 1 One may be inoperative for night operations provided fuselage mounted taxi/landing light on associated side is operative.

-40-12 Wingtip Mounted Recognition Light

-01 C 2 0 May be inoperative provided aeroplane is not operated at night.

-02 C 2 1

-50-01 Exterior Emergency Light B 3 0 May be inoperative for daylight operations.

-50-02 Flight Deck Flashlight Moved to chapter 25.

-50-03 Floor Proximity Emergency Escape Path Marking System Light

-01 Left Forward Half incandescent bulbs (Emergency Lighting)

B - - Up to six bulbs (three pairs) may be inoperative provided no two adjacent pairs are inoperative.

-02 Left Forward Half LED (Emergency Lighting)

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

-03 Left Aft Half B - 0

(Continued)





-50-03 Floor Proximity Emergency Escape Path Marking System Light (Continued)

-04 Right Aft Half incandescent bulbs (Emergency Lighting)

B - - Up to six bulbs (three pairs) may be inoperative provided no two adjacent pairs are inoperative.

-05 Right Aft Half LED (Emergency Lighting)

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

-06 Right Forward Half B - 0

-50-04 LED Light Source for Emergency Exit (Escape Hatch) (If Installed)

C 20 17



(1) System & Sequence Numbers ATA 34 NAVIGATION Item


-00-01 Course Selector Knob B 2 1 One may be inoperative provided it is not required by procedures or regulations.

-00-02 Moving Map Display (If Installed)

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

-00-03 VHF Navigation System

-01 VOR C 2 0 May be inoperative provided: a) Procedures do not require its use,

and b) System is not required by

regulations.

-02 ILS

-10 Localizer C 2 0 May be inoperative provided: a) Procedures do not require its use, b) Associated glideslope is considered

inoperative, and c) System is not required by

regulations.

-20 Glideslope C 2 0 May be inoperative provided: a) Procedures do not require its use,

and b) System is not required by

regulations.

-18-01 Angle of Attack Gauge (Units 5001 – 5500)

C 1 0

-18-02 Angle of Attack Indexer C 1 0

-18-03 Angle of Attack Probe Heater B 1 0 May be inoperative provided: a) Aeroplane is not operated in visible

moisture with ram air temperature of +10 degrees C or below,

b) Aeroplane is not operated in known or forecast icing conditions, and

c) Aeroplane is not operated at night.





-20-01 Slip-Skid Indicator (Bezel mounted inclinometer) (Units 5001 – 5500)

B 3 1 Two may be inoperative provided each pilot has either a bezel mounted slip indicator or a PFD displayed slip indicator.

-23-01 Non-Stabilized Magnetic Compass (If Installed)

B 1 0 May be inoperative provided: a) Both AHRS heading information

sources are operative, and b) Standby HSI heading information is

operative.

-25-01 Display Controller – Honeywell

-01 Primary Flight Display (PFD) Controller (Units 5001 – 6000)

-10 Descent Height/Minimum Descent Altitude Select Knob (Units 5501 – 6000)


-15 Elapsed Time Function Switch (Units 5001 – 6000)

C 2 0

-20 FMS Source Selector Switch (Units 5001 – 6000)


-25 Ground Speed/Time to Go (GSPD/TTG) Switch (Units 5001 – 5500)

C 2 0

-30 Horizontal Indicator Mode Selector Switch (HSI) (Units 5001 – 6000)

C 2 0 NOTE: Weather radar requirements must be considered if ARC display modes are inoperative on both PFDs and the MFD is inoperative.

(Continued)





-25-01 Display Controller – Honeywell (Continued)

-01 Primary Flight Display (PFD) Controller (Units 5001 – 6000) (Continued)

-35 Preview Switch (Units 5501 – 6000)

C 2 0

-40 RA/BARO Switch (Units 5001 – 6000) (If Installed)

C 2 0 May be inoperative provided the setting required for intended approach is available.

-45 Radio Altitude Knob (Units 5001 – 5500)


-50 Single Cue/Cross Pointer (SC/CP) Switch (Units 5001 – 6000)

C 2 0

-55 "STANDARD" Barometer Pressure Switch (PUSH STD) (Units 5501 – 6000)

C 2 0

-60 VOR/Localizer Source Selector Switch (NAV) (Units 5001 – 6000)

C 2 - May be inoperative provided procedures do not require their use.

NOTE: Aeroplane powers up to the onside VOR/LOC source, and cannot be changed. If FMS selected, VOR/LOC cannot be reselected.

(Continued)






-01 Primary Flight Display (PFD) Controller (Units 5001 – 6000) (Continued)

-65 WX/TERR Switch (Units 5501 – 6000)

C 2 0 NOTE: Weather radar requirements must be considered if the WX/TERR switches are inoperative on both PFDs and the MFD is inoperative.

-70 Bearing Pointer Select Knob (Units 5001 – 6000)

C 4 0 May be inoperative provided required bearing pointers are available for procedures.

-02 Multi Function Display (MFD) Controller – Honeywell (Units 5001 – 6000)

-10 Checklist Function Button (NORM, EMER, RCL, PAG, SKP, ENT) (Units 5001 – 5500)

C 6 0

-20 Checklist Function Button (NORM, EMER, RCL, PAG, SKP, ESC) (Units 5501 – 6000)

C 6 0

-30 Data Set Knob (Units 5501 – 6000)

C 1 0 May be inoperative provided PFD settings for baro set and metric alt are set correctly for the intended flight.

-40 ET1/2 and ST1/2 Button (Units 5501 – 6000)

C 4 0

(Continued)






-02 Multi Function Display (MFD) Controller – Honeywell (Units 5001 – 6000)

-50 Joystick Controller (Units 5001 – 5500)

C 1 0

-55 Joystick Controller (Units 5501 – 6000)

C 1 0 May be inoperative provided PFD settings for baro set and metric alt are set correctly for the intended flight.

-60 MAP/PLAN SWITCH (Units 5001 – 6000)

C 1 0

-70 Range Selector (Units 5001 – 6000)

C 1 0

-80 Symbol Display Button (APT, VOR, DAT) (Units 5001 – 5500)

C 3 0

-90 WX SWITCH (Units 5001 – 5500)

C 1 0 May be inoperative provided at least one PFD HSI switch operates normally.

-95 WX SWITCH (Units 5501 – 6000)

C 1 0 May be inoperative provided at least one PFD WX/TERR operates normally.

-25-02 Multi-Function Display Unit (MFD) (Units 5001 – 6000)

C 1 0 (O) May be inoperative provided: a) Alternate procedures are established

and used, and b) All functions of the PFD controllers

are verified operative.





-25-03 Display Controller – Collins (Units 6001 and on)

-01 Display Control Panel (DCP) (Units 6001 and on)

B 2 1 (O) One may be inoperative provided a) Both cursor control panels (CCPs)

are operative, b) Affected primary flight display (PFD)

is controlled by CCP, and c) Copilot's multi function display (MFD)

is operative.

-02 Cursor Control Panel (CCP) (Units 6001 and on)

B 2 1 (O) One may be inoperative provided: a) Both display control panels (DCPs)

are operative, b) Affected primary flight display (PFD)

is controlled by DCP, and c) Copilot's multi function display (MFD)

is operative.

-25-04 Co-Pilot Multi Function Display (MFD) (Units 6001 and on)

C 1 0 (O) May be inoperative provided: a) Alternate procedures are established

and used, b) All functions of DCPs and CCP

controllers are verified operative, and c) Right REV switch is set to PFD.

-25-05 Flight Director System B 2 0 May be inoperative provided: a) Command bars remain out of view, b) Approach minimums do not require

use of flight director, c) Autopilot is considered inoperative,

and d) Aircraft is not flown RVSM.

-25-06 Flight Director Mode Select Panel Function (Units 6001 and on)

C - - Individual functions may be inoperative provided:

a) Procedures do not require its use, and

b) AP XFER is operative.

(Continued)





-25-06 Flight Director Mode Select Panel Function (Units 6001 and on) (Continued)

-01 AP (Autopilot) B 1 0 May be inoperative provided: a) Autopilot is considered inoperative,

and b) Aeroplane is not operated RVSM.

-02 YD (Yaw Damper) B 1 0 May be inoperative provided autopilot and yaw damper can be engaged via AP push button.

-25-07 GH-3000 Electronic Standby Instrument System Heading Information (Units 5001 – 6000) (If Installed)

B 1 0 (M) May be inoperative provided: a) Both AHRS heading information

sources are operative, and b) Aeroplane is equipped with an

operative magnetic compass.

-25-08 Standby HSI Heading Information (Units 5001 – 6000)

B 1 0 May be inoperative provided: a) Both AHRS heading information

sources are operative, and b) Aeroplane is equipped with an

operative magnetic compass.

25-09 Standby Flight Display (EHSI-4000) (Units 6001 and on)

B 1 0 (O) May be inoperative provided flight crew verifies prior to each flight that reversion of heading information to the GH-3000 has occurred appropriately.

-34-01 Marker Beacon Receiver System

C 2 0 May be inoperative provided: a) Approach procedures do not require

its use, and b) Not required by regulations.





-35-01 Heads-Up Display (HUD) (If Installed)

-01 C - 0 May be inoperative provided procedures do not require its use.


-42-01 Weather Radar System C 1 - May be inoperative provided the weather reports or forecast available to the commander indicate that cumulo-numbus clouds or other potentially hazardous weather conditions, which could be detected by the system when in working order, are unlikely to be encountered on the intended route.

-44-01 Ground Proximity Warning System (GPWS) (If installed)

A - 0 May be inoperative for a maximum of 6 flights or 25 flight hours or 2 calendar days, whichever occurs first.

-01 Modes 1 to 4 A - 0 May be inoperative for a maximum of 6 flights or 25 flight hours or 2 calendar days, whichever occurs first.

-02 Test Mode A - 0 May be inoperative for a maximum of 6 flights or 25 flight hours or 2 calendar days, whichever occurs first.

-03 Glideslope Deviation (Mode 5)

-10 B - 0 May be inoperative.

-20 C - 0 May be inoperative for day VMC only.

(Continued)





-44-01 Ground Proximity Warning System (GPWS) (If installed) (Continued)

-04 Terrain Awareness & Warning System (TAWS) (where required)

-10 A - 0 May be inoperative for a maximum of 10 calendar days provided the GPWS functions are operative.

-20 A - 0 May be inoperative for a maximum of 6 flights or 25 flight hours or 2 calendar days, whichever occurs first.

-05 Advisory Callouts C - 0 (O) May be inoperative provided alternate procedures are established and used.

NOTE: Check Flight Manual limitations for approach minima.

-06 Windshear Mode (Reactive)

D - 0 (O) May be inoperative provided alternate procedures are established and used.

NOTE: For some designs, these functions are dealt with by other systems.

-07 Runway Awareness and Advisory System (RAAS)

C 1 0





-44-02 Radio Altimeter System A 1 0 May be inoperative provided: a) Approach minimums or operating

procedures do not require its use, b) GPWS is considered inoperative, c) ACAS is considered inoperative, and d) Repairs or replacements are carried

out within 5 further flights or 25 flying hours or 2 calendar days, whichever occurs first.

NOTE 1: Landing gear warning system will function differently without radio altimeter input.

NOTE 2: Aeroplane 6001 and on, TOPI and LOPI operation will be affected.

-44-03 Altitude Alerting System B - 0 (O) May be inoperative provided an autopilot with an altitude hold is operative.

NOTE: One altitude alerting system is required to be operative for RVSM operations.

-45-01 Airborne Collision Avoidance System (ACAS)

-01 ACAS System A - 0 (M) (O) May be inoperative for a maximum of 10 calendar days provided the system is deactivated and secured.

-02 Combined TA and RA Dual Displays

C - 1 (O) May be inoperative on the non-flying pilot side provided:

a) TA and RA elements and audio functions are operative on flying pilot’s side, and

b) TA and RA display indications are visible to the non-flying pilot.

(Continued)





-45-01 Airborne Collision Avoidance System (ACAS) (Continued)

-03 Resolution Advisory (RA) Display System(s)

-10 C - 1 (O) One may be inoperative on the non-flying pilot side.

-20 C - 0 (O) One or more may be inoperative provided:

a) All Traffic Alert (TA) display elements and voice command audio functions are operative, and

b) TA only mode is selected by the crew.

-04 Traffic Alert (TA) Display System(s)

-10 C - 0 (O) One or more may be inoperative provided all installed RA display and audio functions are operative.

-20 C - 1 One may be inoperative on non-flying pilot side.

-05 Audio Functions B 1 0 May be inoperative provided ACAS is considered inoperative.

-06 Airspace Selection Function (If installed)

C - 0





-46-01 Lightning Detection System (If Installed)

C 1 - Any in excess of those required by regulations may be inoperative.

-51-01 Distance Measuring Equipment (DME) Systems

D - - Any in excess of those required by regulations may be inoperative.

-52-01 SSR Transponder

-01 Mode A/C Functions

-10 C - - Any in excess of those required for the route to be flown may be inoperative.

-20 A - 0 (O) May be inoperative for a maximum of 5 flights provided:

a) Permission is obtained from the Air Navigation Service Provider(s) along the route or any planned diversion, and

b) Flight is conducted under VFR over routes navigated by reference to visual landmarks.

NOTE: Mode C function is required to be operative for RVSM operations.

-02 Mode S Function

-10 D - 0 Any in excess of those required for the intended route, may be inoperative.

NOTE: A SSR transponder with an operative Mode S function is defined as a transponder which can provide, at least, Elementary Surveillance capability.

-20 C - 0 One or more may be inoperative provided permission is obtained from the Air Navigation Service Provider(s) when required for the intended route.

(Continued)





-52-01 SSR Transponder (Continued)

NOTE 1: An SSR transponder with an operative Mode S function is defined as a transponder which can provide, at least Elementary Surveillance capability.

NOTE 2: Altitude reporting provided by an SSR transponder Mode S function is required for ACAS operation.

NOTE 3: Altitude reporting provided by an SSR transponder Mode S function is required for flight into RVSM airspace.

-03 Enhanced Surveillance Functions (If installed)

-10 D - 0 One or more Downlinked Aeroplane Parameters (DAP’s), which provide Enhanced Surveillance, may be inoperative when not required for the intended route.

-20 C - 0 One or more Downlinked Aeroplane Parameters (DAP’s), which provide Enhanced Surveillance, may be inoperative when required for the intended route.

-55-01 Automatic Direction Finding (ADF) System

D - - Any in excess of those required by regulations may be inoperative.

-57-01 Global Positioning System (GPS/GNSS/SBAS)

C - - Any in excess of those required by operating requirements may be inoperative.

NOTE: Enhanced function of TAWS may not be available.





-60-01 Flight Management System (FMS)

C - - Any in excess of those required by regulations may be inoperative provided functions are not required by other procedures.

NOTE: Enhanced function of TAWS may not be available.

-01 Navigation Database (If installed) NOTE: Any out of date

Database is to be inoperative.

-10 C - - (O) May be out of currency provided: a) Current aeronautical information

(e.g. charts) is available for the entire route and for the aerodromes to be used, and

b) Navigation database information is disregarded.

-20 C - 1 Any in excess of one may be inoperative provided the operative database is:

a) Up to date for routes, departures, arrival and approach procedures that require the use of navigation Database for RNAV, and

b) This up to date Database is readily available to the flight crew member(s) responsible for navigation.

(Continued)





-60-01 Flight Management System (FMS) (Cont.)

-01 Navigation Database (If installed) installed) (Cont.)

-30 A - 0 (O) One or more may be out of date for a maximum of 10 calendar days provided:

a) Area Navigation (RNAV) departure, arrival and approach procedures do not depend on the data amended in the current database cycle,

b) Before each flight, current aeronautical information is used to verify database Navigation Fixes, coordinates, frequencies, status (as applicable) and suitability of Navigational Facilities required for the intended route, and

c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures, and which have been amended in the current database cycle, are manually tuned and identified.

(Continued)





-60-01 Flight Management System (FMS) (Cont.)

-01 Navigation Database (If installed) (Cont.)

-40 A - 0 (O) One or more may be out of date for a maximum of 10 calendar days provided:

a) Conventional (non-RNAV) departure, arrival and approach procedures, (when available), or ANSP assistance are used as an alternative to RNAV procedures which have been amended in the current database cycle,

b) Before each flight, current aeronautical information is used to verify the database Navigation Fixes, the coordinates, frequencies, status (as applicable) and suitability of Navigational Facilities required for the intended route, and

c) Radio navigation aids, which are required to be flown for departure, arrival and approach procedures and which have been amended in the current database cycle, are manually tuned and identified.

-02 Fuel Planning and Indicating Function

C - - May be inoperative provided fuel flow indicating systems are operative.



(1) System & Sequence Numbers ATA 35 OXYGEN Item


-00-01 Oxygen Tank Fill Port C - 0 (M) May be inoperative provided bottle is filled using alternate means, if service is required.

-00-02 Oxygen Servicing Panel Pressure Gauge

C - 0 (M) May be inoperative provided alternate procedures are used for servicing oxygen system.

-00-03 Blowout Disc/Green Label C 1 0 (O) May be missing or damaged provided oxygen pressure is verified prior to each flight.

-10-01 EROS Crew Oxygen Mask Tension Control System (If installed)

C - 0 (O) May be inoperative provided oxygen mask is verified operative prior to each flight.

-20-01 Passenger Oxygen System C 1 0 May be inoperative provided: a) Aeroplane is operated without cabin

occupants, and b) Crew oxygen system is operative.

-01 Mask B - 0 Individual oxygen masks or dispensers may be inoperative or missing provided associated seats are placarded “DO NOT OCCUPY”.

-02 Drop Out Panel B - 0 (M) Individual panels may be out of normal position provided:

a) Oxygen masks and drop out panel are removed, and

b) Associated seats are placarded “DO NOT OCCUPY”.



(1) System & Sequence Numbers ATA 35 OXYGEN Item


-30-01 Protective Breathing Equipment (PBE) (If installed)

D - - (M) (O) Any in excess of those required may be inoperative or missing provided:

a) Required distribution of operative unit is maintained throughout the Aeroplane,

b) The inoperative PBE and its location are placarded inoperative, removed from the Aeroplane or retained in an approved stowage or out of sight location so it cannot be mistaken for a functional unit, and

c) Procedures are established and used to alert crew members of inoperative or missing equipment.

NOTE: Some PBEs may be considered hazardous material if they are inoperative, and contain oxygen generators or compressed gas.

-30-02 Portable Oxygen Bottles C - - Any in excess of those required by regulations may be inoperative:

a) Required distribution of serviceable bottles is maintained throughout the Aeroplane, and

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



(1) System & Sequence Numbers ATA 38 WATER/WASTE Item


-00-01 Overboard Drain C - - (M) May be inoperative provided the system associated with the drain has been drained and deactivated.

-10-01 Potable Water Systems

-01 C - - (M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, and

b) Associated system components are verified not to have leaks.

NOTE: Any portion of the system operating normally may be used.

-02 C - - (M) May be inoperative provided: a) System is drained, and b) Procedures are established to

ensure system is not serviced.

-30-01 Lavatory Waste Systems C - - (M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, and

b) Associated system component is verified not to have leaks.

NOTE: Any portion of the system operating normally may be used.



(1) System & Sequence Numbers ATA 38 WATER/WASTE Item





(1) System & Sequence Numbers ATA 45 MAINTENANCE COMPUTER Item


-00-01 Maintenance Diagnostic Computer (MDC) System (Units 6001 and on)




(1) System & Sequence Numbers ATA 45 MAINTENANCE COMPUTER Item





(1) System & Sequence Numbers ATA 46 INFORMATION SYSTEMS Item


-00-01 Electronic Flight Bag (EFB) System (If installed)

-01 Class 3 EFBs Integrated Flight Information System (IFIS) (Units 6001 and on) Advanced File Graphics Server (Units 5501 – 6000)

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

NOTE: Any function, program or document which operates normally may be used.

-02 Data Connectivity (Class 2) (if installed)


-03 Power Connection (Class 1 & 2) (If installed)


-04 Mounting Device (Class 2) (If installed)

C - 0 (M) (O) May be inoperative provided: a) Associated EFB and hardware is

secured by an alternate means or removed from the aeroplane, and

b) Alternate procedures are established and used.

-00-02 Electronic Checklist System (If installed)

D - 0 May be inoperative provided equivalent checklist is available.

-00-03 Integrated Flight Information system (IFIS) (Units 6001 and on)

Deleted Revision 1.



(1) System & Sequence Numbers ATA 46 INFORMATION SYSTEMS Item


-00-04 Dedicated EFB Power Connection (does not include AC Cockpit Outlet) (If installed)





(1) System & Sequence Numbers ATA 49 AIBORNE AUXILIARY Item POWER


-20-01 Auxiliary Power Unit (APU) (If Installed)

C 1 0 (M) May be inoperative provided: a) APU is deactivated, and b) Procedures do not require its use.

-30-01 APU Fuel Shutoff Valve (If Installed)

C 1 0 (M) May be inoperative provided: a) Valve is verified closed, b) Valve is deactivated, and c) APU is considered inoperative.

-50-01 APU Bleed Air Valve (If Installed)

C 1 0 (O) May be inoperative provided: a) Valve is verified closed, and b) APU system BLEED AIR switch

remains off.



(1) System & Sequence Numbers ATA 49 AIBORNE AUXILIARY Item POWER





(1) System & Sequence Numbers ATA 52 DOORS Item


-00-01 Cockpit Divider Door/Curtain

-01 Divider Door C 2 0 May be inoperative provided door remains secured open.

-02 Curtain C 2 0 May be missing or inoperative provided curtain remains secured open.

-10-01 Cabin Door Primary Seal

-01 (Pressurized) C 1 0 (O) May be inoperative provided: a) Primary seal does not interfere with

door operation, b) Secondary door seal is verified

intact, and c) Aeroplane is operated at FL 250 or

below.

-02 (Unpressurized) C 1 0 (O) May be inoperative provided: a) Primary seal does not interfere with

door operation, b) Procedures for flight planning at


c) Cabin EMER DUMP is operative and selected to ON,

d) Cabin altitude is set to 14,000 feet, and

e) Aeroplane is operated at 14,000 feet MSL or below.

-10-02 Cabin Door Secondary Seal

-01 (Pressurized) C 1 0 (O) May be inoperative provided: a) Secondary seal does not interfere

with door operation, b) Primary door seal is verified

operative, and c) Aeroplane is operated at FL 250 or

below.

(Continued)





-10-02 Cabin Door Secondary Seal (Continued)

-02 (Unpressurized) C 1 0 (O) May be inoperative provided: a) Secondary seal does not interfere

with door operation, b) Procedures for flight planning at


c) Cabin EMER DUMP is operative and selected to ON,

d) Cabin altitude is set to 14,000 feet, and

e) Aeroplane is operated at 14,000 feet MSL or below.

-10-03 Cabin Door Acoustic Seal C 1 0

-10-04 Cabin Door Key Lock D 1 0 May be inoperative in the unlocked position.

-10-05 Cabin Vent Door C 1 0 (O) May be inoperative provided vent door is manually closed using appropriate AFM procedure prior to each flight.

-10-06 Cabin Door Precatch Deleted Revision 1.

-30-01 Baggage Compartment Door Key Lock

D 1 0 May be inoperative in the unlocked position.

-40-01 Left Nose Avionics Compartment Key Lock


-40-02 Right Nose Avionics Compartment Key Lock


-40-03 Tailcone Maintenance Access Door Key Lock


-42-01 Battery Compartment Door Key Lock for 560-5001 thru 5187, which do not have SB560XL-52-09 incorporated (If Installed)






-46-01 Single Point Refueling System Door Key Lock

-01 D 1 0 May be inoperative in the unlocked position.

-02 D 1 0 May be inoperative in the locked position provided over wing refueling cap locks are not failed in locked position.



(1) System & Sequence Numbers ATA 73 ENGINE FUEL & CONTROL Item


-30-01 Fuel Flow Indicating System A 2 1 One may be inoperative provided repairs are made within three flight days.



(1) System & Sequence Numbers ATA 73 ENGINE FUEL & CONTROL Item





(1) System & Sequence Numbers ATA 76 ENGINE CONTROLS Item


-00-01 Electronic Engine Control (EEC) (Units 5001 – 6000)

C 2 0 (O) May be inoperative provided a) Both EEC switches are set to

MANUAL to provide matched throttles and similar engine response,

b) Operations are conducted in accordance with AFM Supplement, and

c) Engine synchronizer system is considered inoperative.

NOTE: Units 6001 and on cannot dispatch with any ENGINE FAULT CAS Message illuminated.

-01-01 Engine Synchronizer System C 1 0 May be inoperative failed off.



(1) System & Sequence Numbers ATA 76 ENGINE CONTROLS Item





(1) System & Sequence Numbers ATA 77 ENGINE INDICATING Item


-14-01 N1 Indicators

-01 N1 Digital Display Indicator (Units 5001 – 6000)

B 2 1 One may be inoperative provided: a) Corresponding N1 tape display is

operative, b) All other engine indicators are

operative, and c) EEC auto mode with throttle detents

is operative.

-02 N1 Tape Display Indicator (Units 5001 – 6000)

B 2 1 One may be inoperative provided: a) Corresponding digital display is

operative, b) All other engine indicators are

operative, and c) EEC auto mode with throttle detents

is operative.

-32-01 Engine Vibration Monitor System

B 2 1 One may be inoperative provided no abnormal vibration exists.

NOTE: White ENG VIB annunciator/CAS message may be annunciated/displayed.



(1) System & Sequence Numbers ATA 77 ENGINE INDICATING Item





(1) System & Sequence Numbers ATA 78 ENGINE EXHAUST Item


-30-01 Thrust Reverser C 2 0 (M) May be inoperative provided thrust reverser(s) is secured in the forward thrust position.



(1) System & Sequence Numbers ATA 78 ENGINE EXHAUST Item

