f2000 - afm cdl rev02 complet - 20100712

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Part 0

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F2000Airplane

Flight Manual

CONFIGURATION DEVIATION LIST

General Issue 2

DTM537

EASA APPROVED


This Configuration Deviation List must be attached to the DTM537 Airplane Flight Manual approvedby the DGAC on November 30, 1994.

The information contained herein supplements the information contained in sections 1 thru 5 andannexes. For limitations, procedures and performance information not contained in this ConfigurationDeviation List, consult sections 1 thru 5 and annexes.


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Issue 2


General

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Flight Manual

DTM537

EASA APPROVED

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LIST OF CDL REVISIONS

Sub-sub-sections changesRevisionand Date

Titleand

Approval reference Added Revised Removed

Original

13-nov-2002

Approved by lingenieur des etudes etde lexploitation de laviation civileSylvie MORALES.

First Issue of all pages.

Revision 1

15-jun-2009

New page layout

Approved by EASA under referenceEASA.A.C.02096 dated June 15,2009.

Part 0 Issue 1

Part 1 Issue 1

ATA 21 Issue 1

ATA 23 Issue 1

ATA 25 Issue 1

ATA 27 Issue 1

ATA 32 Issue 1

ATA 33 Issue 1ATA 34 Issue 1

ATA 34A Issue 1

ATA 38 Issue 1

ATA 52 Issue 1

ATA 56 Issue 1

All pages

Revision 2

12-jul-2010

Miscellaneous corrections

Approved under DOAEASA.21.J.051 authority underchange reference M3346.

Part 0 Issue 2


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F2000Airplane

Flight Manual


General Issue 2

DTM537

EASA APPROVED

LIST OF EFFECTIVE SECTIONS OF CONFIGURATION DEVIATION LIST

New and modified Parts or ATA at revision 2 are indicated in bold character.

Reference Issue Special applicability

Part 0 Issue 2

Part 1 Issue 1

ATA 21 Issue 1

ATA 23 Issue 1

ATA 25 Issue 1

ATA 27 Issue 1

ATA 32 Issue 1

ATA 33 Issue 1

ATA 34 Issue 1

ATA 34A Issue 1 US registered A/C

ATA 38 Issue 1

ATA 52 Issue 1

ATA 56 Issue 1


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Issue 2


General

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INTENTIONALLY LEFT BLANK


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CONFIGURATION DEVIATION LIST Part 1

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F2000Airplane

Flight ManualPreamble Issue 1

DTM537

EASA APPROVED

PREAMBLE

INTRODUCTION

The following is applicable for authorized certificate holders operating under authoritiesoperating requirements. The operating requirements and the airworthiness standards requirethat all equipment installed on an airplane must be operative.

PURPOSE

This Configuration Deviation List (CDL) contains additional approved limitations for operation ofFalcon 2000 without certain secondary airframe and engine parts as listed herein. The approvedlimitations in Section 1 are applicable except as amended herein. All DGAC or EASA approvedlimitations must be followed when operating with a configuration deviation.

ORGANIZATION OF CDL

Pages identification

The identification of the pages of the CDL consists of the following data printed at the top and thebottom of each page:

- Name of the Aircraft,

- Title of the document: Airplane Flight Manual,

- Page numbering system,

- Section issue number,

- Identification number of document: DTM537,

- Notation: EASA APPROVED.

Page numbering system

The page numbering system consists of 2 elements:

- Number of the section (Part number or ATA number), possibly followed by an alphabetical indexcorresponding to a variant,

- Number of the page in the section always followed by total number of pages of the current section.

Amendment system

When a page is modified, the whole section is revised and its issue number is incremented. Revisedparts are indicated with revision marks. This modified section is published through a new CDLrevision. The following table of version of sections list all effective sections and give information aboutissue and applicability.

APPLICABILITY

This list does not include parts which do not affect the airworthiness of the airplane, such as galley

equipment, entertainment systems, passenger convenience items, etc., and is based on theconfiguration of the airplane as originally manufactured. Secondary airframe parts changed or addedduring completion or while the airplane is in operation should be addressed by supplementaryrevisions to the list.

DEFINITION

The numbering and designation of systems in CDL item list is based in ATA specification No 100. Theparts within each ATA chapter are identified by functional description and when necessary, by partnumbers, or Illustrated Part Catalog index.


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Part 1 CONFIGURATION DEVIATION LIST

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Issue 1 Preamble

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DTM537

EASA APPROVED

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Multiple items

Unless otherwise specified herein, combination of missing or damaged items in the different ATAchapters is not authorized. Unless otherwise specified herein, combination of missing or damageditems in a same ATA chapter is authorized. The performance penalties are cumulative. The decisionof the pilot in command of the flight, to have allowed missing parts corrected prior to flight, will take

precedence over the provisions contained in this publication.If an additional part is lost in flight, the airplane may not depart the airport at which it landed followingthis event until it again complies with the limitations of the item list. This does not preclude theissuance of a ferry permit to allow the airplane to be flown to a point where the necessary repairs orreplacements can be made.

Categorization (Rectification intervals)

- All users of a CDL approved under Authority must effect repairs of inoperative items, at or prior tothe rectification times established by the following letter designators, unless authorized by theAuthority:

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 CDL.

Where a time period is specified, it shall start at 00:01 on the calendar day

following the day of discovery.

B - Items in this category shall be rectified within three (3) consecutive calendar

days excluding the day of discovery.

C - Items in this category shall be rectified within ten (10) consecutive calendar

days excluding the day of discovery.

D - Items in this category shall be rectified within one hundred and twenty (120)

consecutive calendar days excluding the day of discovery.

- The letter designators are inserted in Column 2 Rectification interval.

ACTION REQUIRED

Maintenance LOG

The operator shall list in the airplane logbook an appropriate notation covering the missing part(s) oneach flight.

Damage inspection

The operator shall make a thorough check of the airplane to ascertain that other areas have not beendamaged or affected.

Placarding

The operator shall make a placard by duplicating the complete Configuration Deviation List (CDL)item from this publication and cut it to size to show only the subject item. Install this placard in aconspicuous location in the cockpit.

The pilot shall be notified of each operation with a missing part(s) by listing the missing part(s) in theflight or dispatch release.

If the missing part requires a reduction of VMO / MMO, an approved placard for the reducedVMO / MMO must be installed adjacent to the airspeed indicator and any additional restrictions mustbe placarded for the pilots easily see.

Performance and flight planning

When applicable, the effect of the missing parts will be included in the calculations for take-off,landing and cruise.


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CONFIGURATION DEVIATION LIST Part 1

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F2000Airplane

Flight ManualPreamble Issue 1

DTM537

EASA APPROVED

LIMITATIONS

1 - When the airplane is operated using this Configuration Deviation List, it

must be operated in accordance with the limitations specified in the Airplane

Flight Manual.

2 - The associated limitations must be listed on a placard affixed in the cockpit onthe pilot's instrument panel in the clear view of the pilot.

3 - Take-off performance penalties are applicable to take-off gross weights that

are limited by MTOW, landing field length, second segment climb, or take-off

flight path.

4 - Landing performance penalties are applicable to landing gross weights that

are limited by MLW, landing field length, landing climb, or approach climb.

5 - En-route performance penalties are applicable to operations that are limited by

one engine inoperative en-route climb performance.


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CONFIGURATION DEVIATION LIST ATA 21

PAGE 1 / 2

F2000Airplane

Flight ManualAir conditioning Issue 1

DTM537

EASA APPROVED

21 - AIR CONDITIONING

2 - Rectification interval

3 - Number installed

4 - Number required for dispatch

1 - Item / Function

5 - Remarks or exceptions

Note: combination of the following items is notauthorized, unless specified.

1 - Main entrance door seal C 1 0 May be damaged or missing provided the flight is notpressurized:

- Perform the flight to a maximum altitude of10,000 ft MSL, or to the minimum safe altitudetaking into account oxygen supply requirements.

2 - Baggage compartmentdoor seal

C 1 0 May be damaged or missing provided the flight is notpressurized:


3 - Emergency exit door seal C 1 0 May be damaged or missing provided the flight is notpressurized:


- Risk of water ingress and damage to interior incase of rainy conditions.


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ATA 21 CONFIGURATION DEVIATION LIST

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Issue 1 Air conditioning

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EASA APPROVED

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F2000Airplane

Flight ManualCommunications Issue 1

DTM537

EASA APPROVED

23 - COMMUNICATIONS




1 - Item / Function


1 - Static dischargers C - 14 May be damaged or missing provided only one isaffected from each:

- Aileron,

- Wing tip,

- Horizontal stabilizer.

2 - Radio communicationantennas damaged

- - VHF antennas: As required by Regulations.

3 - Nose cone lightning strips(80RD)

C 7 7 - No missing strip allowed, even partially,

- Limited damages permitted:

- Paint scaling,

- Black stains,

- Pitting,

- Missing metal dots(for two parts type nose cones).

- Avoid forecast stormy conditions.


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Issue 1 Communications

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Flight Manual

DTM537

EASA APPROVED

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F2000Airplane

Flight ManualEquipment / Furnishing Issue 1

DTM537

EASA APPROVED

25 EQUIPMENT / FURNISHING




1 - Item / Function

INSULATION SETS


1 - Frame 4 to 11 C 1set

- - Underfloor: unlimited missing pad quantity.

- Cabin area: max three pads missing allowed tolimit impact on comfort and water condensationprone to damage the dcor panels.

- Cabin increased noise and temperatureimbalance should be expected.

2 - Frame 11 to 19 C 1set

- - Underfloor: unlimited missing pad quantity.

- Cabin area: max three pads missing allowed tolimit impact on comfort and water condensationprone to damage the dcor panels.

- Cabin increased noise and temperatureimbalance should be expected.


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Issue 1 Equipment / Furnishing

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F2000Airplane

Flight ManualFlight controls Issue 1

DTM537

EASA APPROVED

27 - FLIGHT CONTROLS




1 - Item / Function


1 - Aileron: Brush seals C 4 0 Brush seals may be damaged or missing.

2 - Leading edges seals C 8 0 Rubber blade seal and / or bead seal at the level of

actuator and hot air telescopic tube may be damagedor missing provided flaps bead seal is found in goodcondition.

3 - Flaps bead seal C 2 0 Bead seal at inboard rib may be damaged ormissing.


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Issue 1 Flight controls

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Flight Manual

DTM537

EASA APPROVED

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F2000Airplane

Flight ManualLanding gear Issue 1

DTM537

EASA APPROVED

32 - LANDING GEAR




1 - Item / Function


DOORS (SEALING) Note: combination of the following items is notauthorized, unless specified.

1 - Main landing gear -

Main doors(731AB / 741AB) sealing

C

C

2

6

0

0

Flat seal on main landing doors may be damaged ormissing.

Bead seal for main landing gear doors on structuremay be damaged or missing.

2 - Main landing gear -

Strut-linked doors

(732AB / 742AB) sealing

C

C

2

5

0

0

Brush seals for main landing gear strut-linked doorson structure may be damaged or missing.

Bead seal for main landing gear strut-linked doors onstructure may be damaged or missing.

3 - Nose landing gear -

Main doors (front)(711AB / 712AB) sealing

C

C

4

2

0

0

Bead seal for nose landing gear front doors onstructure may be damaged or missing.

Bead seal for nose landing gear on front doors maybe damaged or missing.

4 - Nose landing gear -

Rear doors(713AB / 714AB) sealing

C 4 0 Blade seal for nose landing gear rear doors onstructure may be damaged or missing.


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Issue 1 Landing gear

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Flight Manual

DTM537

EASA APPROVED

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32 - LANDING GEAR




1 - Item / Function


NOSE LANDING GEAR

1 - Towbar attachmentbushings

C 2 0 May be damaged or missing provided scissors swivelfreely.

Towing function lost.


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F2000Airplane

Flight ManualLights Issue 1

DTM537

EASA APPROVED

33 - LIGHTS




1 - Item / Function


1 - Taxi light glass C 1 0 May be damaged or missing provided TAXI" CB ispulled off.

Loose items or debris prone to detach during flightmust be removed before flight.

2 - Wing tip lights fairings C 2 0 May be damaged or missing.


3 - Navigation lights lenses

* Do not apply to LED typeposition lights.

C 3 0* May be missing, see MMEL deviation.

If RH or LH position light lense is missingsimultaneously with wing tip position lights fairing,NAV" CB must be pulled off. All three navigationlights are no more serviceable.

If rear position light glass cover is missing, NAV"and STROBE" CB's must be pulled off. All threenavigation lights and all three strobe lights are nomore serviceable.



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Issue 1 Lights

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DTM537

EASA APPROVED

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33 - LIGHTS




1 - Item / Function


4 - Red ANTICOL lights glasscovers

2 - As required by Regulations.

If fin (or top fuselage) anti-collision light glass coveris missing, "ANTICOL FIN" CB must be pulled off.Fin (or top fuselage) anti-collision light is no moreserviceable.

If belly anti-collision light glass cover is missing,"ANTICOL BELLY" CB must be pulled off. Belly anti-collision light is no more serviceable.


5 - White ANTICOL lightsglass covers

3 - As required by Regulations.

If RH or LH anti-collision light glass cover is missingsimultaneously with wing tip position light fairing,"STROBE" CB must be pulled off. All three strobelights are no more serviceable.

If rear anti-collision light glass cover is missing,"STROBE" and "NAV" CB's must be pulled off. Allthree strobe lights and all three navigation lights areno more serviceable.



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F2000Airplane

Flight ManualLights Issue 1

DTM537

EASA APPROVED

33 - LIGHTS




1 - Item / Function


6 - Wing ice detection lightslenses

C 2 0 May be missing, see MMEL deviation.

If LH wing ice detection light lense is missing, LHEXT LIGHTS" CB must be pulled off. LH wing icedetection light and LH landing light are no moreserviceable.

If RH wing ice detection light lense is missing, RHEXT LIGHTS" CB must be pulled off. RH wing icedetection light and RH landing light are no moreserviceable.


7 - Exterior emergencylighting lights covers

C 2 0 May be missing or damaged, see MMEL deviation.


8 - Pylon lights glass fairing(30LS, 40LS)

C 2 0 May be missing or damaged, see MMEL deviation(baggage compartment exterior lights).



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F2000Airplane

Flight ManualNavigation Issue 1

DTM537

EASA APPROVED

34 - NAVIGATION




1 - Item / Function


1 - Radio navigation antennas

1.1 ATC antennas

1.2 VOR / DME antennas

1.3 Radio altimeterantennas

1.4 - ADF antennas

A

-

-

-

-

-

-

-

-

As required by Regulations, see MMEL deviations.


May be missing, see MMEL deviations.

As required by Regulations.

2 - Pitot normal probes A 2 1 One Pitot Normal probe may be missing or damaged.

Corresponding Air Data Computer is consideredinoperative, refer to MMEL ATA 34, Item:

8 - Air Data Computer (ADC).

3 - Skin deformations - - Dispatch with skin deformation is not authorizedwithout aircraft manufacturer authorization.

Note: If the airplane manufacturer authorizesdispatch with skin deformations forwardframe 5 (passenger door) and aroundPitot, Static and TAT / OAT probes, RVSMoperations must not be planned.


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Issue 1 Navigation

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CONFIGURATION DEVIATION LIST ATA 34A

PAGE 1 / 2

F2000Airplane

Flight ManualNavigation (US registered A/C) Issue 1

DTM537US Registered A/C

EASA APPROVED

34 - NAVIGATION




1 - Item / Function


1 - Radio navigation antennas

1.1 ATC antennas

1.2 VOR / DME antennas

1.3 Radio altimeterantennas

1.4 - ADF antennas

A

-

-

-

-

-

-

-

-



May be missing, see MMEL deviations.

As required by Regulations.

2 - Skin deformations - - Dispatch with skin deformation is not authorized

without aircraft manufacturer authorization.


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Issue 1 Navigation (US registered A/C)

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EASA APPROVED

US Registered A/C

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F2000Airplane

Flight ManualWater waste Issue 1

DTM537

EASA APPROVED

38 WATER WASTE




1 - Item / Function


1 - Galley drain mast (26MT) C 1 0 May be damaged provided the forward cabin drainsare not used (including ice drawer if installed).

Note: In case of major damage, pull the DRAINHEAT CB.

In that case the rear lavatory sink drainalso must not be used.


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Issue 1 Water waste

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F2000Airplane

Flight ManualDoors Issue 1

DTM537

EASA APPROVED

52 - DOORS




1 - Item / Function


DOORS MISSING Note: combination of the following items is notauthorized, unless specified.

1 - Forward toilet servicingdoor (124AB, optionM1235)

C 1 0 May be missing.In order to avoid continuously lighting of DOORSwarning light, disconnect and firmly secure theproximity sensor connector (11MW).

2 - Toilet service panel door(186AB)

C 1 0 May be missing.

3 - Pressure fueling paneldoor (186DR)


Warning panel FUELING caution light remains

continuously on, apply MMEL FUELING cautionlight" recommendations.

On ground, in order to avoid continuously lighting ofboth fueling panel and fueling coupling lights, pushon (1 sec.) fueling panel door microswitch aftercompleting a refueling.

4 - Refueling connector door(186CR) and its actuator


Warning panel FUELING caution light remainscontinuously on, apply MMEL item FUELINGcaution light" recommendations.

On ground, both fueling panel and fueling couplinglights remain on.


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Issue 1 Doors

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Flight Manual

DTM537

EASA APPROVED

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52 - DOORS




1 - Item / Function


DOORS MISSING Note: combination of the following items is notauthorized, unless specified.

5 - Potable water service

panel door (180BB)


6 - External power receptacledoor (314BR)


In the external power receptacle, be ascertain toreturn the GPU ON / OFF switch to OFF positionafter use.

7 - Ground air connector door(314CR)


8 - Oxygen inflation door

(123AL)

C 1 0 May be missing provided:

- Door and plug lanyards are removed and plugtorque checked.

Or

- The recess is obturated with speed resistantadhesive tape (ref.4605 or equivalent perSRM 51-003 procedure).


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F2000Airplane

Flight ManualDoors Issue 1

DTM537

EASA APPROVED

52 - DOORS




1 - Item / Function


DOORS SEALING Note: combination of the following items is notauthorized, unless specified.

1 - Main entrance door,baggage compartmentdoor, and emergency exitsealing.

See chapter "21 - Air conditioning" of this CDL.

2 - Forward servicing doorsealing (FSD)

C 3 0 One blade seal and two bead seals on FSD may bedamaged or missing.

3 - Forward servicing doorsealing (structure around

FSD)

C 4 0 Four blade seal on structure around FSD may bedamaged or missing.

4 - Aft servicing door sealing(ASD)

C 1 0 Blade seal on structure around ASD may bedamaged or missing.

5 - Emergency exit frangiblecover


Loose items or debris prone to detach during flightmust be removed.


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Issue 1 Doors

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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52 - DOORS




1 - Item / Function


MAIN ENTRANCE DOORSTAIRWAY

Note: combination of the following items is notauthorized, unless specified.

1 - Handrail C 1 0 May be missing or damaged provided the doormaneuver is not impaired (closing and opening).Check that door is capable of being opened within10 seconds measured from the time when theunlocking sequence is begun to the time when thedoor is fully opened.

Note: In case of missing handrail the foldingstep is maintained in stowed position byan inner spring.

Warning: For user safety and convenience, theOperator should provide adequate grounddevices for compensating the unavailablehandrail and folding step.

2 - Folding step attachment C 1 0 May be damaged provided the folding step iscorrectly stowed during or before the door closing,and do not impair maneuver.Check that door is capable of being opened within10 seconds measured from the time when theunlocking sequence is begun to the time when thedoor is fully opened.

Warning: For user safety and convenience, theOperator should provide adequate grounddevices for compensating the possiblyunusable folding step.


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F2000Airplane

Flight ManualWindows Issue 1

DTM537

EASA APPROVED

56 - WINDOWS




1 - Item / Function


1 - Sliding window sealing C 1 0 Bead seal may be damaged or missing provided theflight is not pressurized:

- Perform the flight to a maximum altitude of 10,000ft MSL, or to the minimum safe altitude taking intoaccount oxygen supply requirements.


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Issue 1 Windows

F2000Airplane

Flight Manual

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f2000 - afm cdl rev02 complet - 20100712

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