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Revision: 3Date: 10/7/2010

DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

Dassault Aviation

DA-7X(Falcon 7X)

Bryan WatsonChairman, Flight Operations

Evaluation Board (FOEB)

Federal Aviation AdministrationFlight Standards Division

Aircraft Evaluation Group, SEA-AEG1601 Lind Ave. S.W.

Renton, Washington 98057-3356

Telephone: (425)-917-6600FAX: (425)-917-6638

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U.S. DEPARTMENT OF TRANSPORTATIONMASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATIONAIRCRAFT:

FALCON 7XREVISION NO.3

DATE: 10/7/2010PAGE NO.

ITABLE OF CONTENTS

SYSTEM NO. SYSTEM PAGE NO.

SYSTEM PAGE REVISION DATE

Table Of Contents I, II 3 10/7/2010

Highlights Of Change III to IV 3 10/7/2010

Definitions (Operator Responsibility) V 3 10/7/2010

Preamble (Operator Responsibility) VI 3 10/7/2010

21 - Air Conditioning 1 to 6 3 10/7/2010

22 Autoflight 1 to 2 3 10/7/2010

23 - Communications 1 to 7 3 10/7/2010

24 Electrical Power 1 3 10/7/2010

25 Equipment/Furnishings 1 to 10 3 10/7/2010

26 - Fire Protection 1 3 10/7/2010

27 - Flight Controls 1 to 14 3 10/7/2010

28 - Fuel 1 to 13 3 10/7/2010

29 - Hydraulic Power 1 3

10/7/2010

30 - Ice And Rain Protection 1 to 5 3 10/7/2010

31 Indicating/Recording Systems 1 to 3 3 10/7/2010

32 - Landing Gear 1 to 2 3 10/7/2010

33 - Lights 1 to 4 3 10/7/2010

34 - Navigation 1 to 18 3 10/7/2010

35 - Oxygen 1 to 2 3 10/7/2010

36 - Pneumatic 1 to 3 310/7/2010

38 Water/Waste 1 Original 5/10/2007

45 - Central Maintenance System 1 Original 5/10/2007

46 New Technology 1 1 11/9/2007

49 - Airborne Auxiliary Power 1 to 2 3 10/7/2010

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FALCON 7XREVISION NO.3

DATE: 10/7/2010PAGE NO.

IITABLE OF CONTENTS

SYSTEM NO. SYSTEM PAGE NO.

SYSTEM PAGE REVISION DATE

52 - Doors 1 to 3 Original 5/10/2007

73 Engine Fuel & Control 1 to 2 3 10/7/2010

74 - Ignition 1 Original 5/10/2007

77 Engine Indicating 1 Original 5/10/2007

78 Exhaust 1 1 11/9/2007

79 Engine Oil 1 3 10/7/2010

80 Starting 1 3 10/7/2010

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FALCON 7XREVISION: 3

DATE: 10/7/2010PAGE NO:

IIIHIGHLIGHTS OF CHANGE

System Page No. Rev. No. Current Date

EFFECTIVE ABOVE DATE, the Falcon 7X Master Minimum Equipment List has beenrevised.

Several all encompassing changes have been made in this revision:

1. The terms operable and verified reflect Policy Letter 25 definition guidance.Those items not specifically addressed in the highlights of change table below andidentified by change bars in the individual ATA sections reflect PL guidance only.

2. Log of Revisions and Control pages are incorporated into the Table of Contents.

3. Revision changes will be reflected for an entire ATA section vice by individual page.

4. The Definition section will reference the current Policy Letter vice reprinting the text.Operators are responsible for inclusion when developing individual MinimumEquipment Lists (MEL). Current Policy Letters may be found on the internet athttp://fsims.avs.faa.gov.

5. The Preamble section will reference the current Policy Letter vice printing the text.Operators are responsible for using the appropriate 14 CFR Part Preamble whendeveloping individual Minimum Equipment Lists (MEL). Current Policy Letters may

be found on the internet at http://fsims.avs.faa.gov.

EFFECTIVE ABOVE DATE, The Falcon 7X Master Minimum Equipment List has beenrevised. Please replace affected pages of the previous list with this revision for a completeup-to-date MMEL. Retain this sheet with your MMEL until the next revision is issued.

ATA 21 AIR CONDITIONINGItem 2, 3, 4, 5, 6, 8, 10 modified. Items 14, 15, 16, 17 added.

ATA 22 AUTOFLIGHTItems 2, 3, 6, 10 modified.

ATA 23 COMMUNICATIONSItems 1, 7, 8 modified.

ATA 24 ELECTRICAL POWERItem 4 modified.

ATA 25 EQUIPMENT / FURNISHINGSItems 1, 4, 13 modified
http://fsims.avs.faa.gov/http://fsims.avs.faa.gov/http://fsims.avs.faa.gov/http://fsims.avs.faa.gov/

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IVHIGHLIGHTS OF CHANGE

System Page No. Rev. No. Current Date

Item 2 reflects PL 56 for operations that do not require an observer seat

Item 3 reflects PL 79 change from C to D with provisos added

ATA 26 FIRE PROTECTIONItem 1 relief moved to 49-1 as intended in previous revisions

ATA 27 FLIGHT CONTROLSItems 1, 2, 3 ,4, 5, 6, 7, 8, 9 modified. Items 10, 11, 12, 13, 14 added

ATA 28 FUELItems 1, 2, 3, 4, 5, 8, 9, modified.

ATA 30 ICE AND RAIN PROTECTION

Items 1, 2, 3 modified.

ATA 31 INDICATING / RECORDING SYSTEMSItems 1, 5 modified.

ATA 32 LANDING GEARItem 4 modified. Item 5 added.

ATA 33 LIGHTSItems 4, 6, 7, 8, 9, 12, 14 modified.

ATA 34 NAVIGATION

Items 3, 6, 7, 8, 9, 10, 12, 17, 18, 19, 20 modified. Item 26 added.

ATA 35 OXYGENItem 2 modified.

ATA 36 PNEUMATICItem 8 added.

ATA 49 AIRBORNE AUXILIARY POWERItems 5 and 6 are DELETED with relief placed under 49-1 as intended in previousrevisionsItem 7 modified.

ATA 73 ENGINE FUEL AND CONTROLItem 1 modified.

ATA 79 OILItems 1, 2, 3, 4 modified.

ATA 80 STARTINGItem 1 modified.

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DATE: 10/7/2010PAGE:

VDEFINITIONS

Insert current Policy Letter 25 DEFINITIONS here.

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VIPREAMBLE

Insert current Policy Letter 34 or 36, as applicable, PREAMBLE here.

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DEPARTMENT OF TRANSPORTATIONMASTER MINIMUM EQUIPMENT LIST


FALCON 7XREVISION NO: 3


21-1

1. REPAIR CATEGORY2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

SYSTEMSEQUENCE &NUMBERS

4. REMARKS AND EXCEPTIONS21 AIR CONDITIONING

1. Cabin Pressure ControlSystem (CPCS)

1) Automatic Mode C 1 0 (O) May be inoperative provided:a) The flight is conducted in non-

pressurized configuration, andb) Destination airfield landing

elevation and current airfieldelevation are below 8,000 ft.

2) LOW Cabin AltitudeRate Mode

C 1 0

2. Cabin Ventilation ValveAutomatic ControllerChannels

B 2 1 (O) One may be inoperative provided:a) Cabin ventilation valve is

verified operative in manualmode, and

b) Baggage ventilation valve isverified operative in manualmode.

C 2 0 One or more may be inoperativeprovided automatic mode of cabinpressure control system is consideredinoperative (refer to item 21-1).

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21-2





3. Baggage VentilationValve AutomaticController Channels

C 2 1 (O) One may be inoperative provided:a) Cabin ventilation valve is

verified operative in manualmode, and

b) Baggage ventilation valve isverified operative in manualmode.

C 2 0 (O) One or more may be inoperative

provided:a) Both cabin ventilation valveautomatic controller channelsare operative,

b) Baggage ventilation valve isverified operative in manualmode,

c) Baggage ventilation valve is setto closed position before take-off, and

d) Flight level is limited to FL400.

4. PressurizationIndications (in ECSsynoptic)

C 3 0 (O) One or more may be inoperativeprovided the flight is conducted in non-pressurized configuration.

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21-3





5. Air ManagementModules (AMM)

1) AMM #1 C 1 0 May be inoperative provided:a) AMM #2 and AMM #3 are

operative,b) Engine #1 bleed air system is

considered inoperative (refer toitem 36-1),

c) Wing anti-icing control valve isconsidered inoperative (refer toitem 30-2),

d) S-Duct anti-icing control valveis considered inoperative (referto item 30-3), and

e) Brake heating system, ifinstalled, is consideredinoperative (refer to item 30-8).

|||||

2) AMM #2 A 1 0 May be inoperative for one flight

provided:

a) AMM #1 and AMM #3 areoperative,b) Engine #2 bleed air system is

considered inoperative (refer toitem 36-1),

c) Wing anti-icing control valve isconsidered inoperative (refer toitem 30-2),

d) S-Duct anti-icing control valveis considered inoperative (referto item 30-3), and

e) Cabin and cockpit manual

temperature controls areconsidered inoperative (refer toitems 21-8 and 21-10).

|||||

(Continued)

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21-4





5 Air ManagementModules(AMM)(Contd)

3) AMM #3 A 1 0 May be inoperative for one flightprovided:

a) AMM #1 and AMM #2 areoperative,

b) Engine #3 bleed air system

PRSOV is consideredinoperative (refer to item 36-1),c) Cabin and cockpit automatic

temperature controls areconsidered inoperative (refer toitems 21-8 and 21-10), and

d) Humidifier, if installed, is notused (refer to item 21-13).

|||

||

6. Cabin Zone

Temperature SensorsC 2 1 One may be inoperative.

C 2 0 Both may be inoperative provided cabinautomatic temperature control isconsidered inoperative (refer to item21-8).

7. Cockpit Zone

Temperature SensorC 1 0 May be inoperative provided cockpit

automatic temperature control isconsidered inoperative (refer to item21-10).

8. Cabin TemperatureControl

1) Automatic Mode C 1 0 (O) May be inoperative provided cabinmanual temperature control is verifiedoperative.

2) Manual Mode C 1 0 May be inoperative provided cabin

automatic temperature control isoperative.

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21-5





9. Remote TemperatureControl

C 1 0

10. Cockpit TemperatureControl

1) Automatic Mode C 1 0 (O) May be inoperative providedcockpit manual temperature control isverified operative.

2) Manual Mode C 1 0 May be inoperative provided cockpitautomatic temperature control isoperative.

11. Lounge Valves C 2 0 (M) May be inoperative provided:a) The lounge valves are secured

in open position, andb) Cabin temperature control

automatic mode is operative.

12. Crew Hot Air LH/RH

Distribution Control(Foot Warmer)

C 1 0

13.***

Humidifier (M-OPT0045)

D 1 0 (M) May be inoperative provided:a) HUMID pushbutton is set to

OFF position,b) Humidifier air valve is verified in

closed position,c) Humidifier is purged, andd) Humidifier water shut off valve

is verified in closed position.

14. Turbine By-Pass Valve(TBPV) C 1 0 (M) May be inoperative provided it issecured in closed position.

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21-6





15. Baggage CompartmentBasic LeakageDetector (A/C withM0566)

C 1 0 (O) May be inoperative provided:a) The LH and RH FCS zone

temperature sensors areoperative, and

b) ARINC Communicationbetween PCB Fan and MAU isverified operative.

16.

***

Baggage Compartment

Optional LeakageDetector (M-OPT0045 /M-OPT0182)(A/C with M0566)

D 1 0 (O) May be inoperative provided:

a) The LH and RH FCS zonetemperature sensors areoperative, and

b) ARINC Communicationbetween PCB Fan and MAU isverified operative.

17. ARINC Communication

Between PCB Fan andMAU (A/C with M0566)

C 1 0 (M) May be inoperative provided thediscrete overheat system is verifiedoperative.

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22-1




4. REMARKS AND EXCEPTIONS22 AUTOFLIGHT

1. Autopilot Function (AP) B 1 0 (O) May be inoperative provided:a) Approach and landing minima

do not require its use,b) Enroute operations do not

require its use, andc) Flight crew members are

limited to 5 flight hours perscheduled day.

2. Flight DirectorChannels(FD #1 and FD #2)

C 2 1 One may be inoperative providedapproach and landing minimums do notrequire its use.

|||

3. Flight Director (FD)

Upper ModesC - - (O) One or more may be inoperative

provided:a) Approach and landing minima

do not require use of theinoperative FD upper mode(s),and

b) Enroute operations do not

require use of the inoperativeFD upper mode(s).

Note 1: Any upper mode which isoperative may be used.

Note 2: This item includes associatedcontrols / readouts on guidancepanel.

4. Take-Off / Go-Around

(TOGA) ModeRESERVED

5. Touch Control Steering(TCS) Mode

C 1 0 May be inoperative.

Note: This item includes TCS switcheson side-sticks.

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22-2




4. REMARKS AND EXCEPTIONS22 AUTOFLIGHT

6. Autothrottle Function(AT)

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

||

7. Thrust Director (TD) C 1 0 May be inoperative.

Note: AT function is inoperative.

8. FD / TD Pushbuttons(on Guidance Panel)

C 2 0

9. AP Pushbutton (onGuidance Panel)

B 1 0 May be inoperative provided APfunction is considered inoperative (referto item 22-1).

10. AT Quick DisconnectSwitches (on ThrottleQuadrant Assembly)

C 2 1 One may be inoperative provided:a) AT pushbutton on guidance

panel is operative, andb) Autothrottle is not used below

1,500 feet AGL.

C 2 0 Both may be inoperative provided:

a) AT pushbutton on guidancepanel is operative, and

b) autothrottle is not used below10,000 feet AGL.

11. AT Pushbutton (on

Guidance Panel)C 1 0 May be inoperative provided AT

function is considered inoperative(refer to item 22-6).

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23-1




4. REMARKS AND EXCEPTIONS23 COMMUNICATIONS

1. VHF CommunicationSystems

D 3 - Any in excess of those required byFAR, and not powered by an EssentialBus or required for emergencyprocedures may be inoperative.

Note: VHF #1 communication systemmust be operative and tunable.

1) Tuning Means C 4 2 Any in excess of two may beinoperative provided there remains one

means to tune each VHF at each pilotsstation.

2. HF Communication

SystemsD 2 - Any in excess of those required by FAR

may be inoperative.

C 2 1 (O) May be inoperative whileconducting operations that require twoLong Range Communications Systems(LRCS) provided:

a) SATCOM Voice or Data Linkoperates normally,

b) Alternate procedures areestablished and used,

c) SATCOM coverage is availableover the intended route of flight,and

d) If Inmarsat coeds are notavailable while using SATCOMvoice, prior coordination withthe appropriate ATS facility isrequired.

Note: SATCOM is to be used only as abackup to normal HFcommunications unlessotherwise authorized by theappropriate ATS facilities

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23-2





3. Third Audio Panel(non-commercialoperators only)

D 1 0 May be inoperative.

Note: Air carriers use relief of chapter25, item 2.

4. Headsets D - - One headset (including boommicrophone) must be operative foreach required flight crew member onflight deck duty. Any in excess of those

required by regulations may beinoperative.

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23-3





5. Public Address System(PA)

1) PassengerConfiguration

B 1 0 (O) May be inoperative provided:a) Alternate, normal and emergency

procedures, and/or operatingrestrictions are established andused, and

b) Flight attendant alerting system

(audio and visual) operatesnormally.

Note: Since the Falcon 7X does notrequire a flight attendant, and hasno flight attendant alertingsystem, b) may be complied withby ensuring no closed door orother obstruction exists betweenthe cockpit and passenger cabin.

Note: Any station function(s) thatoperate normally may be used.

C 1 0 (O) May be inoperative provided:a) PA is not required by FAR, andb) Alternate, normal and emergency

procedures, and/or operatingrestrictions are established andused.


a) Lavatory Speakers C - 0 (O) May be inoperative providedalternate procedures are established

and used.

(Continued)

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23-4





5. Public Address System(PA)(Contd)

2) Cargo Configuration C 1 0 (O) May be inoperative providedalternate, normal and emergencyprocedures, and/or operatingrestrictions are established and used.

D 1 0 May be inoperative provided

procedures do not require its use.

a) Lavatory Speakers C - 0 (O) May be inoperative providedalternate procedures are establishedand used.

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

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23-5





6. Flight Crew InterphoneSystem

1) PassengerConfiguration

a) Flight Deck to Cabin /Cabin to Flight DeckFunctions

B - - (O) May be inoperative provided:Flight deck to cabin and cabin to

flight deck interphone functions

operate normally on at least fiftypercent of the cabin headsets,and

Alternate communicationsprocedures between the affectedflight attendants station(s) areestablished and used.


b) Flight Deck to GroundFunction

C - 0 (O) May be inoperative providedalternate procedures are establishedand used.


(Continued)

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23-6





6. Flight Crew InterphoneSystem (Contd)

2) Cargo Configuration

a) Flight Deck to Cabin /Cabin to Flight DeckFunctions

C - 0 (O) May be inoperative providedalternate, normal and emergencyprocedures, and/or operatingrestrictions are established and used.


b) Flight Deck to GroundFunction

C - 0 (O) May be inoperative providedalternate procedures are establishedand used.


7. Handheld Mikes C - - One or more may be inoperative or

missing provided associated headset(including boom microphone) isoperative.

8. Cockpit Loudspeakers C 2 0 One or more may be inoperativeprovided headsets are installed andused.

9.***

SATCOM C 1 0 May be inoperative provided alternateprocedures are established and used.

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

10.***

AFIS / SAT AFIS C 1 0 May be inoperative provided alternateprocedures are established and used.

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

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23-7





11.***

Selective Call Systems(SELCAL)

C - 0 May be inoperative provided alternateprocedures are established and used.


1) Channels C - 0 May be inoperative provided alternateprocedures are established and used.


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24-1




4. REMARKS AND EXCEPTIONS24 ELECTRICAL POWER

1. DC External PowerSystem

C 1 0 May be inoperative provided APUelectrical generation system isoperative.

2. Ram Air Turbine (RAT)Generator Heater

A 1 0 May be inoperative for one flight.

3. APU ElectricalGeneration System

C 1 0

4. Engine-DrivenGenerators

1) Generator RESERVED

2) Generator LineContactor (GLC)

A 3 2 (O) GLC #1 or #3 may be inoperativefor one flight provided:a) The associated GEN switch on

the overhead panel is set to OFFposition, and

b) The GLC is verified in open

position.

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25-1




4. REMARKS AND EXCEPTIONS25 EQUIPMENT /FURNISHINGS

1. Flight Crew Seats

1) Power Adjustments D 2 0 May be inoperative for each flight crewmember.

2) Manual Adjustments

a) Vertical and Recline

Adjustments

B 2 0 One or more may be inoperative

provided, for each flight crew member,the associated power control isoperative.

B 2 0 (M) One or more may be inoperativeprovided, for each flight crew member,the associated seat is secured orlocked in a position acceptable to theflight crew member.

b) Other Adjustments C - 0 One or more may be inoperativeprovided the associated seat is secured

in a position acceptable to the flightcrew member.

Note: If an inoperative armrest willhinder an emergency evacuationor any other flight deck duties itshould be removed.

Note: This includes lateral adjustments.

Note: Longitudinal Adjustments mustbe operative.

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25-2





2. Third Crew MemberSeat (includingassociated equipment)

A 1 0 May be inoperative provided:a) A passenger seat in the

passenger cabin is madeavailable to an FAA inspector forthe performance of officialduties, and

b) Repairs are made within twoflight days.

A 1 0 May be inoperative provided:a) Required minimum safety

equipment (safety belt andoxygen) is available,

b) Seat is acceptable to an FAAinspector for the performanceof official duties, and

c) Repairs are made within twoflight days.

Note1: These provisos are intended toprovide for occupancy of the

above seat by an FAAinspector when the minimumsafety equipment (oxygen andsafety belt) is functional andthe inspector determines theconditions to be acceptable.

Note 2: The pilot-in-command willdetermine if the minimumsafety equipment is functionalfor other persons authorized tooccupy any observer seat.

Note 3: When not occupied, theobserver seat must be stowedso as to not impede egressfrom the cockpit.

(Continued)

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25-3





Third Crew MemberSeat (includingassociated equipment)(cont)

||||

1)***

Additional ObserverSeat(s) (includingassociated equipment

D - 0 Note: The pilot-in-command willdetermine if the minimum safetyequipment is functional for the

purposes authorized to occupy any ob

|||

|2) Observer Seat Not

Required by FAR(including associatedequipment)

D - 0 Note: The pilot-in-command willdetermine if the minimum safetyequipment is functional for otherpersons authorized to occupy anyobserver seat(s).

|||||

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25-4





3. Passenger Seats D - - May be inoperative provided:a) Seat does not block an

Emergency Exit,b) Seat does not restrict any

passenger from access to themain aircraft aisle, and

c) The affected seat(s) are blockedand placarded "DO NOT

OCCUPY".Note 1: A seat with an inoperative seat

belt is considered inoperative.

Note 2: Inoperative seats do not affectthe required number of FlightAttendants.

Note 3: Affected seat(s) may includethe seat(s) behind and/oradjacent outboard seats.

|

1) Recline Mechanism D - - May be inoperative and seat occupied

provided seat back is immovable in fullup-right position.

|

D - - (M) May be inoperative and seat

occupied provided seat back issecured in the full upright position.

2) Underseat BaggageRestraining Bars

C - - (O) May be inoperative provided:a) Baggage is not stowed under

seat with inoperative restrainingbar,

b) Associated seat is placarded

"DO NOT STOW BAGGAGEUNDER THIS SEAT", and

c) Procedures are established toalert Cabin Crew of inoperativerestraining bar.

(Continued)

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25-5





3. Passenger Seats(Cont'd)

3) Armrest

a) Armrest with ReclineMechanism

D - - May be inoperative or missing and seatoccupied provided:

a) Armrestdoes not block an

Emergency Exit,b) Armrest does not restrict anypassenger from access to themain aircraft aisle, and

c) If armrest is missing, seat issecured in the full uprightposition.

|

|||

b) Armrest without

Recline MechanismD - - May be inoperative or missing and seat

occupied provided:a) Armrestdoes not block an

Emergency Exit, and

b) Armrest does not restrictany passenger from accessto the main aircraft aisle.

||||

|||

4. Flash Lights C - - One or more may be inoperative

provided each required crew memberassigned to affected position has anoperative flash light.

5. Protective Breathing

Equipment (PBE)Refer to ATA 35.

6. Life Rafts D - - Any in excess of those required by FARmay be inoperative.

7. Crash Axes D - - Any in excess of those required by FARmay be inoperative.

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25-6





8. Automatic ExternalDefibrillator (AED)and/or AssociatedEquipment

A - 0 (O) May be incomplete, missing orinoperative provided:

a) AED is resealed in a manner thatwill identify it as a unit that cannot be mistaken for a fullyserviceable unit, and

b) Repairs or replacements aremade within 3 flight cycles.

D - - Any in excess of those required by FARmay be incomplete, missing, orinoperative.

9. Emergency Medical Kit(EMK) and/orAssociated Equipment

A - 0 (O) May be incomplete, missing orinoperative provided:

a) EMK is resealed in a manner thatwill identify it as a unit that cannot be mistaken for a fullyserviceable unit, and

b) Repairs or replacements are

made within 3 flight cycles.


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25-7





10. First Aid Kit (FAK)and/or AssociatedEquipment

A - - (O) If more than one is required byFAR, only one of the required first aidkits may be incomplete, missing orinoperative provided:

a) FAK is resealed in a manner thatwill identify it as a unit that cannot be mistaken for a fullyserviceable unit, and

b) Repairs or replacements aremade within 3 flight cycles.


11. Emergency LocatorTransmitter (ELT)

Refer to ATA 31.

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25-8





12. Lifejackets D - - Any in excess of the minimum requiredmay be missing or inoperative,provided:

a) Inoperative lifejacket isplacarded inoperative, removedfrom the installed location andplaced out of sight so it cannotbe mistaken for a functional

unit, andb) Required distribution ofserviceable lifejackets ismaintained.

13. Exterior Lavatory DoorAshtrays

1) A/C with more than oneexterior lavatory doorashtray

A - - One may be missing provided it isreplaced within ten consecutivecalendar days.

2) A/C with only oneexterior lavatory doorashtray

A 1 0 May be missing provided it is replacedwithin three consecutive calendar days.

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25-9





14. PassengerConvenience / Non-Essential Equipment &Furnishings (NEF)Items

1)DELETED Rev 3

2)***

Non-EssentialEquipment &Furnishings (NEF)

- 0 May be inoperative, damaged ormissing provided that the item(s) isdeferred in accordance with theoperators NEF program. The NEFprogram, procedures and processesare outlined in the operators (insertname) Manual. (M) and (O)procedures, if required, must beavailable to the flight crew and includedin the operators appropriate document.

Note: Exterior lavatory door ash trays

are not NEF items.

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25-10





15. Cockpit ConvenienceItems

D - 0 Note 1: Prior to December 31, 2007,Items such as sunshades, cupholders, curtains,upholstery/trim, gogglestowage bags, side panelholders, and yoke clips may beinoperative or missing.

Note 2: After December 31, 2007, refer

to item 25-14.2.

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26-1




4. REMARKS AND EXCEPTIONS26 FIRE PROTECTION

1. APU Fire ProtectionSystem

Note: May be inoperative providedAPU is considered inoperative (referto item 49-1).

|

2. Engine Fire RepeaterSystems (red lights onthrottle levers)

C 3 0

3. Engine Decision Help

Systems (white LED onDISCH# pushbuttons)

C 3 0

4. Baggage CompartmentFire Protection System

C 1 0 (O) May be inoperative providedbaggage compartment remainsempty.

5. Rear Compartment FireProtection System

C 1 0 May be inoperative provided pre-cooler systems are operative.

6.***

Toilet Smoke Detector D - - Any in excess of those required byregulations may be inoperative.

7.***

Aft Lounge SmokeDetector

D 1 0 Any in excess of those required byregulations may be inoperative.

8. Hand FireExtinguishers

D - - Any in excess of those required byFAR may be inoperative or missingprovided:

a) The inoperative fire extinguisheris tagged inoperative, removedfrom the installed location, andplaced out of sight so it cannotbe mistaken for a functional unit,

andb) Required distribution is

maintained.

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4. REMARKS AND EXCEPTIONS27 FLIGHT CONTROLS

1. Main Flight ControlComputers (MFCC) /Secondary FlightControl Computers(SFCC)

C 6 5 (O) One may be inoperative provided:a) No other failure is reported from

the Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044, and

b) No amber "FCS: TEST FAIL"CAS message is displayed after

the FCS test.c) Steep approach landings are not

planned.

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2. Flight DataConcentrators (FDC)

1) A/C without M305 orSB 7X-018

C 5 4 (O) FDC #1, FDC #2, FDC #3, or FDC#4 may be inoperative provided:

a) No other failure is reported fromthe Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines as

described in Dassault documentDGT106044,

b) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test,

c) Crosswind at take-off or landingis limited to 15 kt,

d) Auto airbrake deployment isconsidered inoperative,

e) Landing distance is increased by12%, and

f) Steep approach landings are not

planned.

C 5 4 (O) FDC #5 may be inoperative

provided:a) No other failure is reported from

the Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044,

b) No amber "FCS: TEST FAIL"CAS message is displayed after

the FCS test, andc) Steep approach landings are not

planned.

(Continued)

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2. Flight DataConcentrators (FDC)(Cont'd)

2) A/C with M305 or SB

7X-018C 5 4 (O) FDC #1, FDC #2, FDC #3, or FDC

#4 may be inoperative provided:a) No other failure is reported

from the Primary Flight ControlSystem (PFCS) in any of the

other PFCS functional lines asdescribed in Dassaultdocument DGT106044,

b) No amber "FCS: TEST FAIL"CAS message is displayedafter the FCS test,

c) Crosswind at take-off orlanding is limited to 15 kt,

d) Airbrakes are manuallyextended at touch down, and

e) Landing distance is increasedby 12%.

C 5 4 (O) FDC #5 may be inoperative



b) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test.

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3. Actuator Control andMonitoring Units(ACMU)

C 4 3 (O) ACMU #1 or ACMU #2 may beinoperative provided:a) No other failure is reported from

the Primary Flight Control System(PFCS) in any of the other PFCSfunctional lines as described inDassault document DGT106044,and

b) No amber "FCS: TEST FAIL"

CAS message is displayed afterthe FCS test.

C 4 3 (O) ACMU #3 may be inoperativeprovided:

a) Selection and Monitoring #3(SELMON #3) is operative,

b) No other failure is reported fromthe Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault document

DGT106044, andc) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test.

|||||||||

||||

A 4 3 (O) ACMU #3 may be inoperative forone flight provided:

a) No other failure is reported fromthe Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault document

DGT106044, andb) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test.

(Continued)

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3. Actuator Control andMonitoring Units(ACMU) (Cont'd)

C 4 3 (O) ACMU #4 may be inoperativeprovided:

a) Selection and Monitoring #4(SELMON #4) is operative,

b) No other failure is reported from


c) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test.

|||||

||||||||

4. Maintenance andAvionics InterfaceComputers (MAIC)

C 4 3 (O) One may be inoperativeprovided:

a) No other failure is reported from

the Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044,

b) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test, and

c) Steep approach landings arenot planned.

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5. Front / Rear RackPower Supplies

1) RH Front Power #1 C 1 0 (O) May be inoperative provided:a) FDC #1 is considered

inoperative (refer to item 27-2),b) All other rack power supplies

except RH Rear Power #1 areoperative,

c) No other failure is reported fromthe Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044, and

d) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test.

2) RH Rear Power #1 C 1 0 (O) May be inoperative provided:a) All other rack power supplies

except RH Front Power #1 areoperative, andb) No other failure is reported from



(Continued)

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5. Front / Rear RackPower Supplies(Cont'd)

3) LH Front Power #2 C 1 0 (O) May be inoperative provided:a) FDC #2 is considered

inoperative (refer to item 27-2),b) All other rack power supplies

except LH Rear Power #2 are

operative,c) No other failure is reported

from the Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassaultdocument DGT106044, and

d) No amber "FCS: TEST FAIL"CAS message is displayedafter the FCS test.

|||||

||||||||||

4) LH Rear Power #2 C 1 0 (O) May be inoperative provided:

a) All other rack power suppliesexcept LH Front Power #2 areoperative,

b) No other failure is reportedfrom the Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassaultdocument DGT106044, and

c) No amber "FCS: TEST FAIL"CAS message is displayedafter the FCS test.

|

(Continued)

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5) LH Front Power #3 C 1 0 (O) May be inoperative provided:a) All other rack power supplies

are operative,b) No other failure is reported from

the Primary Flight Control

System (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044, and


6) LH Rear Power #3 A 1 0 (O) May be inoperative for one flightprovided:

a) All other rack power suppliesare operative,

b) No other failure is reported fromthe Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044, and


(Continued)

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7) LH Front Power #4 C 1 0 (O) May be inoperative provided:a) FDC #4 is considered

inoperative (refer to item 27-2),b) All other rack power supplies are

operative,

c) No other failure is reported fromthe Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044, and

d) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test.

|||||

|||||||||

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6. Sidestick Pitch / RollSensors

1) A/C without M305 or

SB 7X-018C 20 16 (O) Any in excess of sixteen may be

inoperative provided:a) The inoperative sidestick sensors

are in the same Primary FlightControl System (PFCS) functionalline,

b) No other failure is reported fromthe PFCS in any of the otherPFCS functional lines asdescribed in Dassault documentDGT106044,

c) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test, and

d) Steep approach landings are notplanned.


7X-018

C 20 16 (O) Any in excess of sixteen may be

inoperative provided:a) The inoperative sidestick sensors

are in the same Primary FlightControl System (PFCS) functionalline,

b) No other failure is reported fromthe PFCS in any of the otherPFCS functional lines asdescribed in Dassault documentDGT106044, and

c) No amber "FCS: TEST FAIL" CASmessage is displayed after the

FCS test.

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7. Primary Flight ControlSystem PermanentMagnet Alternator(PMA) Converters

C 2 1 (O) PMA #1 converter may beinoperative provided:a) FDC #1 is considered inoperative

(refer to item 27-2),b) No other failure is reported from

the Primary Flight Control System(PFCS) in any of the other PFCSfunctional lines as described inDassault document DGT106044,

andc) No amber "FCS: TEST FAIL"

CAS message is displayed afterthe FCS test.

C 2 1 (O) PMA #2 converter may beinoperative provided:a) FDC #2 is considered

inoperative (refer to item 27-2),b) No other failure is reported from

the Primary Flight ControlSystem (PFCS) in any of the

other PFCS functional lines asdescribed in Dassault documentDGT106044, and


|||||||

||||||

8. Back-Up Mode A 1 0 May be inoperative for one flightwithout passenger provided PrimaryFlight Control System operatedspoilers are operative.

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9. Rudder Pedal Sensors

1) A/C without M305 or

SB 7X-018C 4 3 (O) One may be inoperative


the Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines as

described in Dassault documentDGT106044,

b) No amber "FCS: TEST FAIL"CAS message is displayed afterthe FCS test, and

c) Steep approach landings arenot planned.


7X-018C 4 3 (O) One may be inoperative


the Primary Flight Control

System (PFCS) in any of theother PFCS functional lines asdescribed in Dassault documentDGT106044, and


Note: Back-Up mode dedicated pedal

sensors are not part of this item.

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10. Inboard Flap PositionSensors

1) Primary Flight ControlSystem (PFCS)Channels

C 4 3 (O) One may be inoperativeprovided:a) No other failure is reported from

the Primary Flight ControlSystem (PFCS) in any of theother PFCS functional lines as

described in Dassault documentDGT106044, and


c) Steep approach landings are notplanned.

Note: This item does not include theflap position sensors channelsdedicated to the Slat/Flap andAirbrake Unit.

11. LH Aileron FightingForce Compensation

C 1 0 (O) One may be inoperative providedno amber "FCS: TEST FAIL" CASmessage is displayed after the FCStest.

12. RH Aileron Fighting

Force CompensationC 1 0 (O) One may be inoperative provided

no amber "FCS: TEST FAIL" CASmessage is displayed after the FCStest.

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13. LH Elevator FightingForce Compensation

C 1 0 (O) One may be inoperative providedno amber "FCS: TEST FAIL" CASmessage is displayed after the FCStest.

14. RH Elevator Fighting

Force CompensationC 1 0 (O) One may be inoperative provided

no amber "FCS: TEST FAIL" CASmessage is displayed after the FCStest.

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4. REMARKS AND EXCEPTIONS28 FUEL

1. Fuel QuantityManagement Computer(FQMC) Channels

A 2 1 FQMC channel #1 may be inoperativeprovided:

a) APU oil tank gauging systemis considered inoperative (referto item 49-7), and

b) Repairs are made within threeconsecutive calendar days.

A 2 1 FQMC channel #2 may be inoperative

provided repairs are made withinthree consecutive calendar days.

2. Booster Pumps C 6 5 (M) One normal booster pump may be

inoperative provided the associatedstand-by booster pump is used.

Note: Dispatch with stand-by boosterpumps inoperative is notauthorized.

3. Fuel Crossfeed

Systems

1) X-BP 1-2 CrossfeedSystem

B 1 0 (M)(O) May be inoperative provided:a) The BP #2 transfer valve is

secured in open position,b) The BP #1 transfer valve is

secured in closed position,c) X-BP 2-3 crossfeed system is

operative,d) All booster pumps are

operative,

e) The back-up X-BP 1-3

crossfeed system is verifiedoperative,

f) The back-up X-TK 1-3 transfersystem is verified operative,and

g) The defuelling transfer valve issecured in closed position.

(Continued)

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3. Fuel CrossfeedSystems (Cont'd)

3) X-BP 1-3 CrossfeedSystems

C 2 1 (M)(O) Normal X-BP 1-3 crossfeedsystem may be inoperative provided:

a) The failed BP transfer valve issecured in closed position, and

b) The back-up X-BP 1-3crossfeed system is verified

operative. B 2 1 (M)(O) Back-up X-BP 1-3 crossfeed

system may be inoperative provided:a) Back-up X-BP 1-3 crossfeed

system and back-up X-TK 1-3crossfeed system are securedin normal flight configurationposition,

b) All booster pumps areoperative, and

c) The normal X-BP 1-3

crossfeed system is verifiedoperative.

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4. Fuel Transfer Systems

1) X-TK 1-2 TransferSystem

B 1 0 (M)(O) May be inoperative provided:a) The BP #2 transfer valve is

secured in open position,b) The BP #1 transfer valve is

secured in closed position,c) X-BP 2-3 crossfeed system is

operative,

d) All booster pumps areoperative,

e) The back-up X-BP 1-3crossfeed system is verifiedoperative,



2) X-TK 2-3 Transfer

System

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

a) The BP #2 transfer valve issecured in open position,

b) The BP #3 transfer valve issecured in closed position,

c) X-BP 1-2 crossfeed system isoperative,


e) The back-up X-BP 1-3crossfeed system is verifiedoperative,



(Continued)

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4. Fuel Transfer Systems(Cont'd)

3) X-TK 1-3 TransferSystems

C 2 1 (M)(O) Normal X-TK 1-3 transfersystem may be inoperative provided:

a) The failed BP transfer valve issecured in closed position,

b) The back-up X-TK 1-3 transfersystem is verified operative

andc) The defuelling transfer valve is

secured in closed position.

B 2 1 (M)(O) Back-up X-TK 1-3 transfer

system may be inoperative provided:a) Back-up X-BP 1-3 crossfeed

system and back-up X-TK 1-3crossfeed system are securedin normal flight configurationposition,

b) All booster pumps are

operative, andc) The normal X-TK 1-3 transfersystem is verified operative.

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5. Fuel Gauging Systems B 3 2 (O) One may be inoperative provided:a) Initial quantity in the

associated group tanks can bedetermined by an acceptablemeans before each departure,

b) Associated fuel flowmeter isoperative,

c) Associated fuel 1,000 lb levelsensor is operative,


e) Partial refueling mode is notused, and

f) Associated Fuel Remaining(FR) and Fuel Used (FU)indications operate normally.

Note: The fuel transfer systems areinhibited, except back-up X-TK1-3 transfer system.

1) LH Wing Outboard

Tank Gauges

C 2 1 One may be inoperative provided:

a) LH wing middle tank gaugesare operative,

b) LH wing inboard tank gaugesare operative, and

c) All booster pumps areoperative.


B 2 0 One or more may be inoperative

provided group #1 tanks fuel gaugingsystem is considered inoperative(refer to item 28-5).

(Continued)

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28-7





5. Fuel Gauging Systems(Cont'd)

2) LH Wing Middle TankGauges

C 3 2 One may be inoperative provided:a) LH wing outboard tank gauges

are operative,b) LH wing inboard tank gauges

are operative, andc) All booster pumps are

operative.Note: The fuel transfer systems are

inhibited, except back-up X-TK1-3 transfer system.

B 3 0 One or more may be inoperativeprovided group #1 tanks fuel gaugingsystem is considered inoperative(refer to item 28-5).

3) LH Wing Inboard Tank

GaugesC 2 1 One may be inoperative provided:

a) LH wing outboard tank gauges

are operative,b) LH wing middle tank gauges


operative.


Note: This item does not include thehigh level sensor fitted on theLH wing inboard tank forward

gauge.

(Continued)

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28-8







Note: This item does not include thehigh level sensor fitted on the

LH wing inboard tank forwardgauge.

4) Front Tank Gauges C 2 1 One may be inoperative provided:

a) Rear tank gauges areoperative, and

b) All booster pumps areoperative.


Note: This item does not include thehigh level sensor fitted on thefront tank forward gauge.


Note: This item does not include thehigh level sensor fitted on thefront tank forward gauge.

(Continued)

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5) Rear Tank Gauges C 3 2 One may be inoperative provided:a) Front tank gauges are

operative, andb) All booster pumps are

operative.

Note: The fuel transfer systems are


Note: This item does not include thefuel 1,000 lb level sensor fittedon the rear tank left gauge.


Note: This item does not include the

fuel 1,000 lb level sensor fittedon the rear tank left gauge.

6) RH Wing Outboard

Tank GaugesC 2 1 One may be inoperative provided:

a) RH wing middle tank gaugesare operative,

b) RH wing inboard tank gaugesare operative, and

c) All booster pumps areoperative.



(Continued)

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7) RH Wing Middle TankGauges

C 3 2 One may be inoperative provided:a) RH wing outboard tank gauges

are operative,b) RH wing inboard tank gauges


operative.Note: The fuel transfer systems are



8) RH Wing Inboard Tank

GaugesC 2 1 One may be inoperative provided:

a) RH wing outboard tank gauges

are operative,b) RH wing middle tank gauges


operative.


Note: This item does not include thehigh level sensor fitted on theRH wing inboard tank forward

gauge.

(Continued)

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28-11







Note: This item does not include thehigh level sensor fitted on the

RH wing inboard tank forwardgauge.

6. Fuel Flowmeters B 3 2 One may be inoperative provided:

a) Associated engine primaryparameters are operative, and

b) Associated fuel gaugingsystem is operative.

7. Fuel 1,000 lb LevelSensors

B 3 2 One may be inoperative provided:a) Associated fuel gauging

system is operative, and

b) Associated fuel flowmeter isoperative.

8. Fuel TemperatureProbes

C 2 1

C 2 0 (O) Both may be inoperative providedfuel temperature monitoring isperformed based on TAT indication.

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9. Pressure RefuelingSystem (Cont'd)

C 3 0 (M) One or more may be inoperativeprovided:

a) Gravity refueling is performed,b) X-TK 1-2 and X-TK 2-3 transfer

systems are operative, andc) Vent valves are secured in

closed position at the end of thegravity refueling sequence.

4) Pressurization Valves C 2 0 (M) Automatic operation of the

pressurization valves may beinoperative provided:

a) Pressurization valves aremanually set to open positionbefore starting the pressurerefueling sequence, and

b) Pressurization valves aremanually set to closed position

and secured at the end of thepressure refueling sequence.

C 2 0 (M) One or more may be inoperativeprovided:

a) Gravity refueling is performed,

b) X-TK 1-2 and X-TK 2-3 transfersystems are operative, and

c) Pressurization valves aresecured in closed position atthe end of the gravity refuelingsequence.

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4. REMARKS AND EXCEPTIONS30 ICE AND RAINPROTECTION

1. Multi-Function Probe(MFP) HeatingSystems

1) Primary HeatingSystems

B 4 3 (O)(M) One may be inoperativeprovided:

a) The inoperative MFP primaryheating system and associated

ADS are deactivated andsecured,

b) ADS associated with the non-heatable MFP is consideredinoperative (refer to item 34-9),

c) PF side is on the side-slipcompensated ADS,

d) Approach and landing minimaare limited to CAT 1operations,

e) Enroute operations do notrequire its use, and

f) Flight is not conducted intoknown or forecast icingconditions.

Note: In case of MFP #3 or MFP #4primary heating systeminoperative, air data parametersdisplayed on SFD are not side-slip compensated.

2) Secondary HeatingSystems

C 4 3 One may be inoperative.

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30-2





2. Wing Anti-Icing System

1) Wing Anti-Icing ControlValve

C 1 0 (O)(M) May be inoperative provided:a) Wing anti-icing control valve is

secured in closed position, andb) Flight is not conducted into

known or forecast icingconditions.

2) Skin TemperatureSensors

C 2 0 (O) One or more may be inoperativeprovided:

a) Wing anti-icing control valve isset to closed position,

b) Wing anti-icing system is notused, and

c) Flight is not conducted intoknown or forecast icingconditions.

3) Pressure Transducers C 2 0 (O) One or more may be inoperativeprovided:a) Wing anti-icing control valve is

set to closed position,b) Wing anti-icing system is not

used, andc) Flight is not conducted into


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3. S-Duct Anti-IcingSystem

1) S-Duct Anti-IcingControl Valve

C 1 0 (M)(O) May be inoperative provided:a) S-duct anti-icing control valve is

secured in closed position, andb) Flight is not conducted into

known or forecast icing

conditions.

2) Skin TemperatureSensors

C 2 0 (O) One or more may be inoperativeprovided:

a) S-duct anti-icing control valve isset to closed position,

b) S-duct anti-icing system is notused, and

c) Flight is not conducted intoknown or forecast icingconditions.

3) Pressure Transducers C 2 1

C 2 0 (O) Both may be inoperative provided:a) S-duct anti-icing control valve is

set to closed position,b) S-duct anti-icing system is not

used, andc) Flight is not conducted into


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4. Engine Inlet Anti-IcingSystems

Note: Only one engine inlet anti-icingsystem may be affected byinoperative equipment at anyone time.

1) Pressure RegulatingShut-Off Valves(PRSOV)

C 3 2 (M)(O) One may be inoperativeprovided:

a) Engine inlet PRSOV is verified

and secured in closed position,b) Associated pressure transducer

is operative, andc) Flight is not conducted into


2) Pressure Transducers C 3 2 (O) One may be inoperative provided:a) Associated engine inlet anti-

icing PRSOV is set to closedposition,

b) Associated engine inlet anti-

icing system is not used, andc) Flight is not conducted intoknown or forecast icingconditions.

5. Rain Repellent System C 1 0 (M) May be inoperative provided drycoat is verified to be efficient.

C 1 0 May be inoperative provided:a) Operations are not conducted in

known or forecast precipitationwithin the arrival and departure

areas, andb) When low visibility conditionsare known or forecast,approach or take-off minima donot require its use.

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6. Windshield De-IcingSystem

1) LH / RH Power SupplyModules

C 2 1 One may be inoperative provided:a) BACK UP power supply

module is operative, andb) The inoperative power supply

module is reverted to BACK

UP power supply module.

2) BACK UP PowerSupply Module

C 1 0 May be inoperative provided LH andRH power supply modules areoperative.

7. Ice Detection System D 1 0 (M) May be inoperative provided thefailed ice detector is deactivated.

8.***

Brake Heating System(M-OPT0011)

D 1 0 (M) May be inoperative providedbrake heating control valve is securedin closed position.

9. TAT Probe HeatingSystems

C 2 1 May be inoperative providedassociated TAT probe is consideredinoperative (refer to item 31-6).

10. Ram Air Turbine (RAT)Generator Heater

Refer to ATA 24.

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4. REMARKS AND EXCEPTIONS31 INDICATING /RECORDING

SYSTEMS

1. Combined Recorders(CVR/DFDR)

1) Flight Data Recorder

(FDR) SystemsC 2 - Any in excess of those required by

FAR may be inoperative.

A 2 0 May be inoperative provided:

a) At least one Cockpit VoiceRecorder (CVR) operatesnormally,

b) Airplane is not dispatched froma designated airport as listedin the operator's MEL unless:

1) The FDR failure occursafter pushback butprior to takeoff, or

2) The FDR repair wasattempted but was notsuccessful.

c) In those cases where repair isattempted but not successful,the aircraft may be dispatchedon a flight or series of flightsuntil the next designatedairport where repair must beaccomplished prior todispatch, and

d) Repairs are made within threeflight days.

a) FDR Recording

Parameters required byFAR (FDR #1)

A 1 - May be inoperative provided:

a) At least one Cockpit VoiceRecorder (CVR) operatesnormally, and

b) Repairs are made within threeflight days

(Continued)

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SYSTEMS

1. Flight Data Recorder(FDR) Systems(Cont'd)

b) FDR RecordingParameters notrequired by FAR (FDR

#2)

A 1 - May be inoperative provided:a) FDR #1 operates normally, andb) Repairs are made prior to the

completion of the next heavymaintenance visit.

c) For an operator otherthan a holder of an aircarrier or commercialoperator certificate

C 2 1 Any in excess of those required byFAR may be inoperative.

A 2 0 May be inoperative provided repairsare made in accordance withapplicable FARs.

2) Cockpit Voice Recorder(CVR) Systems C 2 - Any in excess of those required byFAR may be inoperative.

A 2 0 May be inoperative provided:a) FDR #1 operates normally, andb) Repairs are made within three

flight days.

a) For an operator otherthan a holder of an aircarrier or commercialoperator certificate

C 2 1 Any in excess of those required byFAR may be inoperative.

A 2 - May be inoperative provided repairsare made in accordance withapplicable FARs.

2. Enhanced GroundProximity WarningSystem (EGPWS)

Refer to ATA 34.

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SYSTEMS

3. Traffic Alert andCollision AvoidanceSystem (TCAS)

Refer to ATA 34.

4. Emergency LocatorTransmitter (ELT)

1) Survival Type ELTs D - - Any in excess of those required byFAR may be inoperative or missing.

2) Fixed ELTs A - 0 May be inoperative or missingprovided repairs are made within 90days.

D - - Any in excess of those required byFAR may be inoperative or missing.

5. Clock Indications D 2 - Any in excess of those required byFAR may be inoperative.

6. Total Air Temperature(TAT) Probes

C 2 1 One may be inoperative provided:Fuel temperature indication is

operative, andFlight is not conducted into known

or forecast icing conditions

7. Display Units (DU) Refer to ATA 34.

8.***

Quick Access Recorder(QAR)(M-OPT0020)

C 1 0

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4. REMARKS AND EXCEPTIONS32 LANDING GEAR

5. Weight-On-Wheel(WOW) System

1) Nose Landing Gear

WOW #1 (A/C withM1031 or SB 7X-065)

A 1 0 May be inoperative for 4 flightsprovided:

a) All other WOW proximityswitches are operative,

b) If available, Weather Radar isswitched ON at T/O as

applicable and switched OFF atlanding,

c) APU is verified not ON beforeTake-Off,

d) Airbrakes are manuallyextended at touchdown,

e) Landing distance is increased by12%, and

f) Electrical loads on synoptics areclosely monitored on ground.

2) RH Main Landing Gear

WOW #1 (A/C withM1031 or SB 7X-065)

A 1 0 (M) May be inoperative for 4 flights

provided:a) All other WOW proximity

switches are operative,b) Thrust reverser system is

secured in stowed position,c) Take-off on icy runways is not

authorized,d) Airbrakes are manually

extended at touchdown,e) Landing distance is increased by

12%, andf) Electrical loads on synoptics are

closely monitored on ground.

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4. REMARKS AND EXCEPTIONS33 LIGHTS

1. Cockpit Lighting C - - Individual lights may be inoperativeprovided remaining lights are:

a) Sufficient to clearly illuminate allrequired instruments, controls,and other devices for which it isprovided,

b) Position so that direct rays areshielded from flight crew

members eyes, andc) Lighting configuration and

intensity is acceptable to theflight crew.

2. Cabin Lighting - - Considered as Non-EssentialEquipment and Furnishings.Refer to ATA 25.

3. Baggage CompartmentLighting


C 2 0 May be inoperative provided baggagecompartment is empty.

4. Compartment Lighting C - 0 One or more may be inoperativeprovided sufficient natural lighting isavailable to perform the required duty.

C - 0 One or more may be inoperative

provided an alternate lighting is used.

Note: Compartment lighting includesnose cone light, rearcompartment lighting, refueling

panel lighting, water fillingcompartment lighting.

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5. Cabin Signs (FASTENSEAT BELT and NOSMOKING)

C - - (M)(O) No passenger seat,crewmember seat or lavatory may beoccupied from which a FASTENSEAT BELT /NO SMOKING sign isnot readily legible.

C - - (M)(O) FASTEN SEAT BELT /NOSMOKING signs may be inoperativeand the affected passenger seat(s),

cabin crew seat(s) or lavatories maybe occupied provided:

a) The Public Address (PA)system is operative and can beclearly heard throughout thecabin during the flight, and

b) A procedure is used to notifypassengers when the seat beltsmust be fastened, smoking isprohibited, and passengersshould return to cabin from thelavatory.

C - - May be inoperative providedpassengers are not carried.

6. Wing Ice DetectionLights


B 2 0 Both may be inoperative for nightoperations provided a flashlight isused to illuminate ice accretion onanother outside surface visible fromthe flight deck.

D 2 0 Both may be inoperative for daylight

operations.

7. Navigation Lights C 3 0 One or more may be inoperative fordaylight operations.

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8. Anti-Collision Lights

1) Red Anti-CollisionLights

C 2 1

C 2 0 Both may be inoperative for daylightoperations.

Note: Alternative procedures must bedeveloped and used when the

aircraft is on the ground with theengine(s) running.

9. Landing Lights B 2 1 One may be inoperative.

C 2 0 Both may be inoperative for daylightoperations.

1) Pulse Function C 1 0

10. Taxi Light C 1 0 May be inoperative provided landinglights are operative.

C 1 0 May be inoperative for daylightoperations.

11. Logo Lights D - 0

12. Ground Utility Lighting(LH and RH pylonlights)

C - 0 One or more may be inoperativeprovided sufficient natural lighting isavailable to perform the required duty.

C - 0 One or more may be inoperative

provided an alternate lighting is used.

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13. Cabin EmergencyLighting

1) Path Lighting B - - One light may be inoperative.

Note: This item does not include strip.

14. Exterior EmergencyLighting Systems

C 2 0 One or more may be inoperative fordaylight operations.

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4. REMARKS AND EXCEPTIONS34 NAVIGATION

1. Display Units (DU) B 4 3 Lower display unit may be inoperativeprovided:

a) Inoperative DU is switchedOFF,

b) AGM #1, AGM #2 and AGM#4 are operative,

c) Jeppesen electronic terminalcharts, if installed, are notused, and

d) Video system, if installed, isnot used.

Note: Pilots should review the "loss ofsecond DU" procedure prior totakeoff.

2. Advanced GraphicsModules (AGM)

A 4 3 AGM #1 or AGM #4 may beinoperative provided:

a) All display units are operative(no black display unit),

b) Associated DU knob on the

reversion panel is set to REVposition,

c) Jeppesen electronic terminalcharts, if installed, are notused,

d) Video system, if installed, isnot used, and

e) Repairs are made within threeflights.

Note: A red crossed display unitshould not be switched OFF.

(Continued)

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4. REMARKS AND EXCEPTIONS34 NAVIGATION

2. Advanced GraphicsModules (AGM)(Cont'd)

B 4 3AGM #2 may be inoperative provided:

a) All display units are operative(no black display unit),

b) Associated DU knob on thereversion panel is set to REV

position,c) Jeppesen electronic terminal

charts, if installed, are notused, and

d) Video system, if installed

Documents

da-7x rev 3