F900EX CONFIGURATION DEVIATION LIST Part 0

Airplane PAGE 1 / 2
Flight Manual General Issue 3

CONFIGURATION DEVIATION LIST

This Configuration Deviation List must be attached to the DTM561 Airplane Flight Manual approved
by the DGAC on May 31, 1996.
The information contained herein supplements the information contained in sections 1 thru 5 and
annexes. For limitations, procedures and performance information not contained in this Configuration
Deviation List, consult sections 1 thru 5 and annexes.

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DTM561
Dassault Aviation - Genuine Documentation APPROVED
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Issue 3 General Flight Manual

LIST OF CDL REVISIONS

Revision Title Sub-sub-sections changes

and Date and
Approval reference Added Revised Removed

Original Original revision approved by EASA First Issue of all pages.

22-Jul-2011 under reference M5575 on
January 19, 2011.
Revision 1 Revision 1 approved by EASA under Part 0 Issue 2
09-Jan-2012 reference M5735 on January 09, ATA 27 Issue 2
2012.
ATA 32 Issue 2
ATA 52 Issue 2
Revision 2 Revision 2: The technical content of Part 0 Issue 3
16-Nov-2018 this document is approved under the ATA 23 Issue 2
authority of DOA EASA.21J.051
under reference M6069. ATA 56 Issue 2

LIST OF EFFECTIVE SECTIONS OF CONFIGURATION DEVIATION LIST

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Reference Issue Special applicability

Part 0 Issue 3
Part 1 Issue 1
ATA 21 Issue 1
ATA 23 Issue 2
ATA 25 Issue 1
ATA 27 Issue 2
ATA 32 Issue 2
ATA 33 Issue 1
ATA 34 Issue 1
ATA 34A Issue 1 US registered A/C
ATA 38 Issue 1
ATA 52 Issue 2
ATA 53 Issue 1
ATA 56 Issue 2

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Flight Manual Preamble Issue 1

PREAMBLE

INTRODUCTION
The following is applicable for authorized certificate holders operating under authorities operating
requirements. The operating requirements and the airworthiness standards require that all equipment
installed on an airplane must be operative.
PURPOSE
This Configuration Deviation List (CDL) contains additional approved limitations for operation of
airplane with certain secondary airframe and engine parts missing or damaged as listed herein. The
approved limitations in Section 1 are applicable except as amended herein. All EASA approved
limitations 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 the
bottom of each page:
- Name of the Aircraft,

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- Title of the document: Airplane Flight Manual,
- Page numbering system,
- Section issue number,
- Identification number of document: DTM561,
- 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 index
corresponding 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. Revised
parts are indicated with revision marks. This modified section is published through a new CDL
revision. The previous table of version of sections list all effective sections and give information about
issue 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 the
configuration of the airplane as originally manufactured. Secondary airframe parts changed or added
during completion or while the airplane is in operation should be addressed by supplementary
revisions to the list.
DEFINITION
The numbering and designation of systems in CDL item list is based in ATA specification No 100. The
parts within each ATA chapter are identified by functional description and when necessary, by part
numbers, or Illustrated Part Catalog index.

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Issue 1 Preamble Flight Manual

Multiple items
Unless otherwise specified herein, combination of missing or damaged items in different ATA
chapters is not authorized. Unless otherwise specified herein, combination of missing or damaged
items in a same ATA chapter is authorized. The performance penalties are cumulative. The decision
of the pilot in command of the flight, to have allowed missing or damaged 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 following
this event until it again complies with the limitations of the item list. This does not preclude the
issuance of a ferry permit to allow the airplane to be flown to a point where the necessary repairs or
replacements can be made.
Categorization (Rectification intervals)
- All users of a CDL approved under Authority must effect repairs of missing or damaged items, at or
prior to the rectification times established by the following designators, unless authorized by the
Authority:

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.
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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.
E Items in this category shall be rectified within 90 calendar days excluding the day
of discovery. This category allows to plan the repair at the next , or possibly the
second next, Basic Inspection per AMM 05-00/00.
F Items in this category shall be rectified within 300 calendar days excluding the
day of discovery. This category allows to plan the repair at the next , or possibly
the second next, A or A+ Inspection per AMM 05-00/00.
* Items in this category shall be rectified per the rectification interval of the relevant
MMEL item as indicated in Column 5.

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

Number installed / number required
The number of items installed is found in Column 3.
The minimum number of items required for dispatch is found in Column 4.
When the "Number required for dispatch" is equal to the "Number installed", the damaged item must
not be removed despite of the damage.
The dash "-" in Column 3 or Column 4 indicates a variable number of items.
ACTION REQUIRED
Maintenance LOG
The operator shall list in the airplane logbook an appropriate notation covering the missing or
damaged part(s) on each flight.

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Flight Manual Preamble Issue 1

Damage inspection
The operator shall make a thorough check of the airplane to ascertain that other areas have not been
damaged 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 a
conspicuous location in the cockpit.
The pilot shall be notified of each operation with a missing or damaged part(s) by listing the missing
or damaged part(s) in the flight or dispatch release.
Performance and flight planning
The effects of the missing parts are to be accounted for, as applicable, for maximum weight
determination during each phase of flight, i.e. take-off, landing and en route.
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 on the
pilot's instrument panel in the clear view of the pilot.

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3- Take-off performance penalties are applicable to the lowest of the maximum take-
off weight limited by structural limitation and the maximum take-off weight as limited
by available field length, obstacle clearance and climb performance requirements.
4- Landing performance penalties are applicable to the lowest of the maximum landing
weight limited by structural limitation and the maximum landing weight as limited by
available landing field length and approach and landing climb gradients
requirements.
5- En-route performance penalties are applicable to operations that are limited by one
or two engine(s) inoperative en-route climb performance.

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Flight Manual Air conditioning Issue 1

21 - AIR CONDITIONING
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

Note:
Combination of the following items is not
authorized, unless specified.
The unfixed part of a damaged seal must be cut.

1 - Main entrance door

1-1 Door seal on structure C 1 0 May be missing or damaged provided the flight is not

DASSAULT AVIATION Proprietary Data

pressurized:
- Perform the flight to a maximum altitude of 8,000 ft
AMSL, or to the minimum safe altitude taking into
account oxygen supply requirements.
Note:
Risk of water ingress and damage to interior in
case of rainy conditions.
Increased internal noise to be expected.

1-2 Brushes F 2 0 May be missing or damaged.

1-3 Seals on door C 2 0 May be missing or damaged.

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Issue 1 Air conditioning Flight Manual

21 - AIR CONDITIONING
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

Note:
Combination of the following items is not
authorized, unless specified.
The unfixed part of a damaged seal must be cut.

2 - Baggage compartment
door
2-1 Door seal C 1 0 May be missing or damaged provided the flight is not
pressurized:
DASSAULT AVIATION Proprietary Data

- Perform the flight to a maximum altitude of 8,000 ft

AMSL, or to the minimum safe altitude taking into
account oxygen supply requirements.
Note:
Risk of water ingress and damage to interior in
case of rainy conditions.
Increased internal noise to be expected.
2-2 Brushes F 2 0 May be missing or damaged.

3 - Emergency exit door seal C 1 0 May be damaged provided that the remaining parts of
the seal are sufficient to prevent any mechanical play
of the door and that the flight is not pressurized:
- Perform the flight to a maximum altitude of 8,000 ft
AMSL, or to the minimum safe altitude taking into
account oxygen supply requirements.
Note:
Risk of water ingress and damage to interior in
case of rainy conditions.
Increased internal noise to be expected.

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Flight Manual Communications Issue 2

23 - COMMUNICATIONS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions
1 - Static dischargers E - 14 May be missing or damaged provided only one is
affected from each:
- Wingtip,
- Aileron,
- Horizontal stabilizer side (including elevator),
- Vertical stabilizer (including rudder).
Note:
The static discharger under the aft fuselage may
be missing but not damaged.
Compliance may be achieved by moving

DASSAULT AVIATION Proprietary Data

undamaged dischargers to replace the
missing/damaged ones as necessary.

2 - Radio communication * - - May be damaged provided there is no damage at the

VHF antennas antenna interface with the fuselage.
Relevant VHF system is considered inoperative, then
refer to MMEL for dispatch decision.

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Issue 2 Communications Flight Manual
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Flight Manual Equipment / Furnishing Issue 1

25 – EQUIPMENT / FURNISHING
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions
INSULATION SETS Note: may be combined with any other CDL item.

1 - Frame 4 to 11 E 1 - - Under floor: unlimited missing pad quantity.

set - Cabin area: at worst three pads missing allowed
to limit impact on comfort and water condensation
prone to damage the decor panels.
- Any unattached pad must be removed.
Note: cabin increased noise and temperature
imbalance should be expected.

DASSAULT AVIATION Proprietary Data

2 - Frame 11 to 19 E 1 - - Under floor: unlimited missing pad quantity.
set - Cabin area: at worst three pads missing allowed
to limit impact on comfort and water condensation
prone to damage the decor panels.
- Any unattached pad must be removed.
Note: cabin increased noise and temperature
imbalance should be expected.

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Flight Manual Flight controls Issue 2

27 - FLIGHT CONTROLS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

SEALING Note:
Combination of the following items is not
authorized, unless specified.
The unfixed part of a damaged seal must be
cut.

1 - Aileron seals

DASSAULT AVIATION Proprietary Data

1-1 Brush seals E 4 0 May be damaged or missing.

1-2 Rubber blade seals E 6 0 May be damaged or missing.

2 - Leading edges seals

2-1 Outboard leading E 20 0 Rubber blade seal and / or bead seal at the level of
edge seals actuator and hot air telescopic tube may be damaged
or missing provided flaps bead seal is found in good
condition.

2-2 Inboard slat seals E 4 0 Bead seals at lower part of the slats may be
damaged or missing provided flaps bead seal is
found in good condition.
Note: the long bead seal at upper part of inboard
leading edge structure may not be damaged.

3 - Flaps bead seal E 2 0 Bead seal at inboard rib may be damaged or

missing.

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Issue 2 Flight controls Flight Manual

27 - FLIGHT CONTROLS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

BONDING BRAID

4 - Airbrakes bonding braids C 6 2 Two bonding braids out of three may be broken or
(one bonding braid per missing, provided broken braids do not interfere with
airbrake) operation.
DASSAULT AVIATION Proprietary Data

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Flight Manual Landing gear Issue 2

32 - LANDING GEAR
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

DOORS (SEALING) Note:

Combination of the following items is not
authorized, unless specified.
The unfixed part of a damaged seal must be
cut.

1 - Main landing gear -

Main doors
(731AB/741AB) sealing

DASSAULT AVIATION Proprietary Data

1-1 Flat seal on doors F 2 0 Flat seal on main landing doors may be missing or
damaged.
1-2 Bead seals on F 16 0 Bead seals for main landing gear doors on structure
structure may be missing or damaged.

2 - Main landing gear -

Strut-linked doors
(732AB/742AB) sealing
2-1 Flat seal on doors F 2 0 Flat seal on main landing gear strut-linked doors
may be missing or damaged.
2-2 Bead seals on F 10 0 Bead seals for main landing gear strut-linked doors
structure on structure may be missing or damaged.
2-3 Brush seals on F 8 0 Brush seals for main landing gear strut-linked doors
structure on structure may be missing or damaged.

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Issue 2 Landing gear Flight Manual

32 - LANDING GEAR
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

DOORS (SEALING) Note:

(cont’d) Combination of the following items is not
authorized, unless specified.
The unfixed part of a damaged seal must be
cut.

3 - Nose landing gear -

Main doors (front)
(711AB/712AB) sealing
DASSAULT AVIATION Proprietary Data

3-1 Bead seals on doors F 2 0 Bead seal for nose landing gear on front doors may
or be missing or damaged.
4
3-2 Bead seals on F 4 0 Bead seal for nose landing gear front doors on
structure structure may be missing or damaged.

4 - Nose landing gear - F 3 0 Blade seal for nose landing gear rear doors on
Rear doors structure may be missing or damaged.
(713AB/714AB) sealing Note: allowance do not apply to rear transversal
seal as it protects wirings in the hinge area.

NOSE LANDING GEAR

5 - Towbar attachment F 2 0 May be missing or damaged provided scissors swivel

bushings freely.
Loose items or debris prone to detach during flight
are removed before flight.
Note:
Towing function is lost.
May be combined with any other CDL item.

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Flight Manual Landing gear Issue 2

32 - LANDING GEAR
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

BONDING BRAID

6 - Main landing gear - C 4 0 Bonding braids on main landing gear main doors
Main doors bonding braids may be broken or missing, provided broken braids do
not interfere with operation.

7 - Main landing gear - C 2 0 Bonding braids on main landing gear strut-linked

Strut-linked doors bonding doors may be broken or missing, provided broken

DASSAULT AVIATION Proprietary Data

braids braids do not interfere with operation.

8 - Main landing gear - C 6 0 Bonding braid on main landing gear leg may be
Leg bonding braids broken or missing, provided broken braids do not
interfere with operation.

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Issue 2 Landing gear Flight Manual
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Flight Manual Lights Issue 1

33 - LIGHTS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

Note: combination of the following items is not

authorized.

1 - Taxi light glass * 1 0 May be missing or damaged provided:

- “TAXI" CB is pulled off.
- Loose items or debris prone to detach during flight
are removed before flight.
- Taxi light is considered inoperative, then refer to
MMEL for dispatch decision.

DASSAULT AVIATION Proprietary Data

2 - Wing tip lights fairings E 2 0 May be missing or damaged provided:
- Loose items or debris prone to detach during flight
are removed before flight.

3 - Navigation lights lenses * 3 0* May be missing or damaged provided:

or - If one RH or LH position light lens is missing or
* Do not apply to LED type 5 damaged simultaneously with wing tip position
position lights. lights fairing, “NAV" CB must be pulled off. All
navigation lights are no more serviceable.
- If rear position light glass cover is missing or
damaged, “NAV" and “STROBE" CB's must be
pulled off. All navigation lights and all three white
anticollision lights are no more serviceable.
- Loose items or debris prone to detach during flight
are removed before flight.
- Relevant navigation lights and White Anticollision
Lights are considered inoperative, then refer to
MMEL for dispatch decision.

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Issue 1 Lights Flight Manual

33 - LIGHTS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

4 - Red ANTICOL lights glass * 2 - May be missing or damaged provided:

covers - If fin (or engine 2 air intake cowling) anti-collision
light glass cover is missing or damaged,
"ANTICOL FIN" CB must be pulled off. Fin (or
engine 2 air intake cowling) anti-collision light and
LH landing light are no more serviceable.
- If belly anti-collision light glass cover is missing or
damaged, "ANTICOL BELLY" CB must be pulled
off. Belly anti-collision light and RH landing light
are no more serviceable.
DASSAULT AVIATION Proprietary Data

- Loose items or debris prone to detach during flight

are removed before flight.
- Relevant red anti-collision lights and landing lights
are considered inoperative, then refer to MMEL
for dispatch decision.

5- White ANTICOL lights * 3 - May be missing or damaged provided:

glass covers - If RH or LH anti-collision light glass cover is
missing or damaged simultaneously with wing tip
position light fairing, "STROBE" CB must be
pulled off. All three strobe lights are no more
serviceable.
- If rear anti-collision light glass cover is missing or
damaged, "STROBE" and "NAV" CB's must be
pulled off. All three strobe lights and all navigation
lights are no more serviceable.
- Loose items or debris prone to detach during flight
are removed before flight.
- Relevant white anti-collision lights and navigation
lights are considered inoperative, then refer to
MMEL for dispatch decision.

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Flight Manual Lights Issue 1

33 - LIGHTS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

6 - Wing ice detection lights * 2 0 May be missing or damaged provided:

lenses - If LH wing ice detection light lens is missing or
damaged, “LH SLATS LIGHT" CB must be pulled
off. LH wing ice detection light is no more
serviceable.
- If RH wing ice detection light lens is missing or
damaged, “RH SLATS LIGHT" CB must be pulled
off. RH wing ice detection light is no more
serviceable.

DASSAULT AVIATION Proprietary Data

- Loose items or debris prone to detach during flight
are removed before flight.
- Relevant wing ice detection lights are considered
inoperative, then refer to MMEL for dispatch
decision.

7 - Exterior emergency * 2 0 May be missing or damaged provided:

lighting lights covers - Loose items or debris prone to detach during flight
are removed before flight.
- Relevant exterior emergency evacuation lights are
considered inoperative, then refer to MMEL for
dispatch decision.

8 - Pylon lights glass fairing * 1 0 May be missing or damaged provided:

or - Water ingress is prevented by installation of
2 speed resistant adhesive tape (ref 4605 or
equivalent).
- Loose items or debris prone to detach during flight
are removed before flight.
- Relevant baggage compartment light (exterior) is
considered inoperative, then refer to MMEL for
dispatch decision.

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Issue 1 Lights Flight Manual

33 - LIGHTS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

9 - Logo lights lenses * 2 0 May be missing or damaged provided:

(optional upper and lower) or - Water ingress is prevented by installation of
4 speed resistant adhesive tape (ref 4605 or
equivalent).
- Pull "UPPER LOGO LIGHT" CB and / or "LOWER
LOGO LIGHT" CB.
- Loose items or debris prone to detach during flight
are removed.
- Relevant logo lights are considered inoperative,
DASSAULT AVIATION Proprietary Data

then refer to MMEL for dispatch decision.

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Flight Manual Navigation Issue 1

34 - NAVIGATION
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

Note: combination of the following items is not

authorized.

1 - Radio navigation antennas When relevant, check there is no damage at the

antenna interface with the pressurized fuselage.
1-1 ATC antennas * - - May be damaged.
Relevant ATC transponder is considered inoperative,
then refer to MMEL for dispatch decision.

DASSAULT AVIATION Proprietary Data

1-2 VOR antennas * - - May be damaged.
Relevant VOR/ILS function is considered inoperative,
then refer to MMEL for dispatch decision.

1-3 DME antennas * - - May be damaged.

Relevant DME is considered inoperative, then refer
to MMEL for dispatch decision.

1-4 Radio-altimeter * - - May be damaged.

antennas Relevant radio-altimeter is considered inoperative,
then refer to MMEL for dispatch decision.

1-5 ADF antennas * - - May be damaged.

Relevant ADF is considered inoperative, then refer to
MMEL for dispatch decision.

2 - Pitot normal probes * 2 1 One pitot normal probe may be missing or damaged
provided there is no fuselage pressurization leakage.
Relevant Air Data Computer (ADC) is considered
inoperative, then refer to MMEL for dispatch
decision.

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Issue 1 Navigation Flight Manual

34 - NAVIGATION
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

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

without aircraft manufacturer authorization.
Note: if the airplane manufacturer authorizes
dispatch with skin deformations forward frame 5
(passenger door) and around Pitot, Static and
TAT / OAT probes, RVSM operations must not be
planned.
DASSAULT AVIATION Proprietary Data

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Flight Manual Navigation (US registered A/C) Issue 1

34 - NAVIGATION
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

Note: combination of the following items is not

authorized.

1 - Radio navigation antennas When relevant, check there is no damage at the

antenna interface with the pressurized fuselage.
1-1 ATC antennas * - - May be damaged.
Relevant ATC transponder is considered inoperative,
then refer to MMEL for dispatch decision.

DASSAULT AVIATION Proprietary Data

1-2 VOR antennas * - - May be damaged.
Relevant VOR/ILS function is considered inoperative,
then refer to MMEL for dispatch decision.

1-3 DME antennas * - - May be damaged.

Relevant DME is considered inoperative, then refer
to MMEL for dispatch decision.

1-4 Radio-altimeter * - - May be damaged.

antennas Relevant radio-altimeter is considered inoperative,
then refer to MMEL for dispatch decision.

1-5 ADF antennas * - - May be damaged.

Relevant ADF is considered inoperative, then refer to
MMEL for dispatch decision.

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

without aircraft manufacturer authorization.

US registered A/C
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Issue 1 Navigation (US registered A/C) Flight Manual
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US registered A/C
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Flight Manual Water waste Issue 1

38 – WATER WASTE
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

1 - Galley drain mast C 1 0 May be damaged provided:

- It is visually verified that there is no mounting
flange deformation introducing a risk of air
pressurization leakage.
- The forward cabin drains are not used (including
ice drawer if installed).
- The rear lavatory sink drain is not used.
- The drain heater circuit breaker is pulled.

DASSAULT AVIATION Proprietary Data

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Issue 1 Water waste Flight Manual
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Flight Manual Doors Issue 2

52 - DOORS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

DOORS MISSING Note: combination of the following items is not

authorized, unless specified.

1 - Forward toilet servicing E 1 0 May be missing provided:

door (124AB) - The proximity sensor connector (11MW) is
disconnected and firmly secured, in order to avoid
continuously lighting of "SERVICE DOOR"
caution light on ground.
- The socket connector (250P) is firmly capped.

DASSAULT AVIATION Proprietary Data

- Chains and bonding strip are removed.

2 - Pressure fueling panel E 1 0 May be missing.

door (194BR) Warning panel FUELING caution light remains
continuously on, apply MMEL item "FUELING
caution light" recommendations.
On ground, in order to avoid continuously lighting of
both fueling panel and fueling coupling lights, push
on (1 sec.) fueling panel door microswitch after
completing a refueling.

3 - External power receptacle E 1 0 May be missing.

door (311AR) In the external power receptacle, be ascertain to
return the EXT POWER / NORMAL switch to
NORMAL position after use.

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Issue 2 Doors Flight Manual

52 - DOORS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

DOORS MISSING Note: combination of the following items is not

(cont’d) authorized, unless specified.

4 - Oxygen inflation door E 1 0 May be missing provided:

(123AL) - Door and plug lanyards are removed and plug
torque checked.

E 1 0 May be missing provided:

- The recess is obstructed with speed resistant
DASSAULT AVIATION Proprietary Data

adhesive tape (ref.4605 or equivalent).

- The tape is renewed after 5 days of service.

5 - Hydraulic ground power

access doors

5-1 Hydraulic 1 E 1 0 May be missing provided chains are firmly secured.

ground power access door
(312AL)

5-2 Hydraulic 2 E 1 0 May be missing provided chains are firmly secured.

ground power access door
(311BR)

6 - Baggage compartment E 1 0 May be missing.

service door (193BL)

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 F900EX CONFIGURATION DEVIATION LIST ATA 52
Airplane PAGE 3 / 6
Flight Manual Doors Issue 2

52 - DOORS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

DOORS SEALING Note: combination of the following items is not

authorized, unless specified.

7 - Main entrance door, See chapter "21 - Air conditioning" of this CDL.
baggage compartment
door, and emergency exit
sealing.
8 - Emergency exit frangible C 1 0 May be missing or damaged provided loose items or

DASSAULT AVIATION Proprietary Data

cover debris prone to detach during flight are removed
before flight.
Note: risk of water ingress while A/C is parked in
humid or rainy conditions.

9 - Mechanic's servicing E 4 0 Seal on MSD may be missing or damaged.

compartment door sealing
(MSD)

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Issue 2 Doors Flight Manual

52 - DOORS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

MAIN ENTRANCE DOOR

STAIRWAY
10 - Handrail(s) F 1 0 May be missing or damaged provided:
(with or without second or - The door maneuver is not impaired (closing and
handrail option) 2 opening).
- The door is capable of being opened within
10 seconds measured from the time when the
unlocking sequence is begun to the time when the
door is fully opened.
DASSAULT AVIATION Proprietary Data

Note: in case of missing basic handrail the

folding step is maintained in stowed position by
an inner spring.

WARNING:

FOR USER SAFETY AND CONVENIENCE, THE

OPERATOR SHOULD PROVIDE ADEQUATE
GROUND DEVICES FOR COMPENSATING THE
UNAVAILABLE HANDRAIL AND FOLDING STEP.

Note: may be combined with any other CDL item.

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 F900EX CONFIGURATION DEVIATION LIST ATA 52
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Flight Manual Doors Issue 2

52 - DOORS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

MAIN ENTRANCE DOOR

STAIRWAY
(cont’d)
11 - Folding step attachment F 1 0 May be damaged provided:
- The folding step is correctly stowed during or
before the door closing, and do not impair
maneuver (closing or opening).
- The door is capable of being opened within
10 seconds measured from the time when the

DASSAULT AVIATION Proprietary Data

unlocking sequence is begun to the time when the
door is fully opened.

WARNING:

FOR USER SAFETY AND CONVENIENCE, THE

OPERATOR SHOULD PROVIDE ADEQUATE
GROUND DEVICES FOR COMPENSATING THE
POSSIBLY UNUSABLE FOLDING STEP.

Note: may be combined with any other CDL item.

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Issue 2 Doors Flight Manual

52 - DOORS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions

DOORS BONDING BRAID

12 - Main entrance door C 1 0 Bonding braid may be broken or missing, provided
bonding braid broken braid does not interfere with operation.
13 - Baggage compartment C 1 0 Bonding braid may be broken or missing, provided
door bonding braid broken braid does not interfere with operation.
14 - Mechanic servicing door C 1 0 Bonding braid may be broken or missing, provided
bonding braid broken braid does not interfere with operation.
Note: A/C without M2306 is not equipped with
DASSAULT AVIATION Proprietary Data

bonding braid.
15 - Main landing gear - See chapter “32 – Landing gear” of this CDL
Main doors bonding braids
16 - Main landing gear - See chapter “32 – Landing gear” of this CDL
Strut-linked doors bonding
braids

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 F900EX CONFIGURATION DEVIATION LIST ATA 53
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Flight Manual Fuselage Issue 1

53 - FUSELAGE
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions
1 - Nose cone lightning strips E 7 7 Limited damages permitted provided forecast stormy
conditions are avoided:
- Paint scaling,
- Black stains,
- Pitting,
- Missing metal dots (for two parts type nose
cones).

WARNING

DASSAULT AVIATION Proprietary Data

DISPATCH WITH A LIGHTNING STRIP TOTALLY
OR PARTIALLY MISSING IS NOT AUTHORIZED
WITHOUT AIRCRAFT MANUFACTURER
AUTHORIZATION.

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Issue 1 Fuselage Flight Manual
DASSAULT AVIATION Proprietary Data

INTENTIONALLY LEFT BLANK

DTM561
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 F900EX CONFIGURATION DEVIATION LIST ATA 56
Airplane PAGE 1 / 2
Flight Manual Windows Issue 2

56 - WINDOWS
1 - Item / Function
2 - Rectification interval
3 - Number installed
4 - Number required for dispatch
5 - Remarks or exceptions
1 - Sliding window sealing C 1 0 Bead seal may be missing or damaged provided the
flight is not pressurized:
- Perform the flight to a maximum altitude of
8,000 ft AMSL, or to the minimum safe altitude
taking into account oxygen supply requirements.

2 - Cockpit windows crack A 7 7 One ply per window may be cracked provided:
- Corresponding abnormal procedure is applied,
- Repairs are made within three flight days.

DASSAULT AVIATION Proprietary Data

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APPROVED
 ATA 56 CONFIGURATION DEVIATION LIST F900EX
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Issue 2 Windows Flight Manual
DASSAULT AVIATION Proprietary Data

INTENTIONALLY LEFT BLANK

DTM561
APPROVED