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FALCON 2000EX 

MAINTENANCE MANUAL 

CHAPTER 5-40

AIRWORTHINESS LIMITATIONS 

REVISION 9 - FEBRUARY 2013 

DGT 113877 - PUB 657/684/454

09004000806a01a8 - VALIDATED - Certification Repository 
F2000EX 

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INFORMATION TO OPERATORS 

Please find enclosed Revision No. 9 of Chapter 5-40. 

Modifications and corrections contained in this revision are : 

the introduction of the F2000LXS and F2000S Aircraft. 

the introduction of the CP013 (ATA 27 and 36) 

the introduction of the CP014 (ATA 32) 
F2000EX 

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This document is divided into 6 paragraphs: 

A. History of revision 

B. General 

C. Corrosion Prevention Control Program 

D. Notes 

E. Airframe components with limited service life 

F. Mandatory maintenance operations 
F2000EX 

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A. HISTORY OF REVISION 

Approved by EASA 

Date of approval: 

- Original edition: 

June 17, 2004 (for S/N 6 and >=28) and 

April 24, 2003 (for S/N 1 to 5 and 7 to 27) 

- Revision 1 DGT 685: February 20, 2006 

- Revision 2 DGT 685: 

EASA approved under EASA A.A. 01179 on June 8, 2006 (for S/N 6 and >=28) and 

EASA approved under EASA A.C. 04543 on October 25, 2006 (for S/N 1 to 5 and 7 

to 27) 

- Revision 3 DGT 113877 supersedes DGT 685 § 5-40: EASA approved under 

EASA.A.C.09412 on August 15, 2008 

-Revision 4 DGT 113877 approved under of the authority of DOA nr. EASA.21J.051 

(R5001) which incorporates CP 001 and CP 002: 

CP 001, EASA approved under EASA.A.C.11570 on January 26, 2009 

CP 002, EASA approved under EASA.A.C.04822 on April 23, 2009 

- Revision 5 DGT 113877 

This revision 5 is the compilation of the following EASA changes proposal, with no further 

technical changes: 

CP 003, EASA approved under EASA 10029544 on March 31, 2010 

CP 007, EASA approved under EASA 10029959 on May 06, 2010 

The technical content of this revision is approved under DOA EASA.21J.051 authority by 

reference R5017. This approval means that the revision has been prepared exclusively with 

already EASA approved data and is released under DOA procedures. 

Effective date of this revision: September 29, 2010. 

- Revision 6 DGT 113877 

This revision 6 is the compilation of the following EASA changes proposal, with no further 

technical changes: 

CP 004, EASA approved under change reference M3391 

CP 009, EASA approved under change reference M3551 

The technical content of this revision is approved under DOA EASA.21J.051 authority by 

reference R5020. This approval means that the revision has been prepared exclusively with 

already EASA approved data and is released under DOA procedures. 

Effective date of this revision: November 07, 2011. 

- Revision 7 DGT 113877 

This revision 7 is the compilation of the following EASA changes proposal, with no further 

technical changes: 

CP 005, EASA approved under change reference M3337 

CP 008, EASA approved under change reference M3339 

The technical content of this revision is approved under DOA EASA.21J.051 authority by 

reference R5032. This approval means that the revision has been prepared exclusively with 

already EASA approved data and is released under DOA procedures. 
F2000EX 

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Effective date of this revision: March 28, 2012. 

- Revision 8 DGT 113877 

This complete revision 8 is the renumbering of tasks, the presentation of the chapter, the 

introduction of the Corrosion Prevention Control Program. 

The technical content of this revision is approved under DOA EASA.21J.051 authority by 

reference R5037. This approval means that the revision has been prepared exclusively with 

already EASA approved data and is released under DOA procedures. 

Effective date of this revision: September 21, 2012 

- Revision 9 DGT 113877 

This complete revision 9 is the compilation of the following EASA changes proposal:

CP 013, EASA approved under change reference M5000 

CP 014, EASA approved under change reference M3605 

The introduction of the new Aircraft F2000LXS and F2000S. 

The technical content of this revision is approved under DOA EASA.21J.051 authority by 

reference R5053. This approval means that the revision has been prepared exclusively with 

already EASA approved data and is released under DOA procedures. 

Effective date of this revision: Mai 03, 2013. 
F2000EX 

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B. GENERAL

This document is applicable to : 

-FALCON 2000EX S/N 1 to 5 and 7 to 27, 

-FALCON 2000EX EASy versions S/N 6 and 28 to 604 including : 

 -FALCON 2000EX with M1691 (F2000EX EASy), 

 -FALCON 2000EX with M2846 (F2000LX), 

-FALCON 2000EX with M5000 (F2000LXS) S/N 263-600, 

-FALCON 2000EX with M3000 (F2000DX) S/N 601-604, 

-FALCON 2000EX with M5001 (F2000S) S/N>= 701. 

For aircraft equipped with Winglets (Modification M2846 (F2000LX, F2000LXS, F2000S)) 

the validity of this chapter 05-40 is limited to 5000 flights. Fatigue calculations will raise this 

limit. New limits and associated inspections will be integrated in a future revision of chapter 

05-40. 

This section contains instructions pertaining to Airworthiness (refer to JAR 25-1529 

Appendix H, paragraph H25-4 and at change 13). These instructions apply to components and 

systems designed and approved by DASSAULT AVIATION and included in the aircraft type 

design. 

This section contains instructions pertaining to Airworthiness of aircraft and Safe Life 

limitations until the Design Service Goal (20,000 flights/30,000 flying hours). 

The tasks and intervals specified are mandatory and cannot be changed, escalated, or deleted 

without the concurrence of the responsible Aircraft Certification Office. 

With respect to the Airworthiness of the aircraft, this section is subject to approval by the 

European Aviation Safety Agency (E.A.S.A.). 

For U.S. Registered aircraft, the Airworthiness Limitations section specifies maintenance 

required under part 43 and part 91 of the Federal Aviation Regulations, unless an alternative 

program has been F.A.A. approved. 

Evaluations and reasons for Airworthiness Limitations do not take into account the influence 

of modifications not approved by DASSAULT AVIATION such as STC, PMA (Part 

Manufacturer Approval), etc. 

1. Definition of a Standard Aircraft

This program is defined for a "STANDARD AIRCRAFT" as defined below. 

For non-standard aircraft, this program needs to be adapted with Instructions for Continued 

Airworthiness developed to cover the non-standard features (STC, repairs, operating 

conditions, ...). 
F2000EX 

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1.1. Standard Aircraft Primary structure must be entirely identical to DASSAULT 

AVIATION type design: 

Condition of the primary structure of a standard aircraft has to correspond to definition at 

aircraft delivery: 

- which can be supplemented by the DASSAULT AVIATION Service Bulletins 

incorporated on aircraft, 

- which must have incorporated the applicable mandatory Service Bulletins. 

 An aircraft cannot be considered as a standard aircraft if its primary structure has been 

changed by an STC or repaired through a definition not reviewed by DASSAULT 

AVIATION in the frame of the applicability of these instructions. 

1.2. Aircraft operations should be close to the fatigue load spectrum defined during type 

certification. This spectrum corresponds to public or private transport defined by 

short, middle and long distance flights. 

When type of mission listed hereafter are performed on a regular basis, the aircraft can not 

be considered as a Standard Aircraft. 

- Low altitude search and rescue flights. 

- Target towing and transport of under wing stores. 

- Scientific research. 

- Cargo transport. 

- Flight training. 

- Others types of operation than normal passengers transport. 

1.3. Maintenance must have been performed in accordance with either: 

- Maintenance Manual and Structural Repair Manual (formerly Maintenance and Repair 

Instructions) recommended by DASSAULT AVIATION, 

or 

- Approved maintenance procedures. 

2. Important

These instructions must mandatorily be complied with by the operators. 

Failure to comply with these instructions will lead to the immediate suspension of the 

Airworthiness Certificate. 

The mandatory nature of these instructions does not in any way reduce the importance of the 

other tasks listed in the Recommended Maintenance Program which must be performed in 

agreement with the national Airworthiness Authorities. 

The mandatory maintenance operations time limits given in section 5-40 correspond to results 

obtained from computations. 

In order to help operators planning maintenance program and to reduce grounding time due to 

scheduled maintenance, these mandatory maintenance operations are also listed in sections 5-

10 or 5-20 but with time limits corresponding to aircraft inspections (A, B, C, etc.).
F2000EX 

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The time base to be taken into account for equipment is defined in section 5-20-00 and the 

date of origin to be taken into account for aircraft maintenance operation is defined in section 

5-10-00. 

An operation required in section 5-40 may not necessarily have to be performed, provided it 

was previously performed during an inspection required in sections 5-10 or 5-20. 

3. Updating of 5-40 Sections

When a new maintenance operation is added due to a revision of Chapter 5-40, this operation 

must be performed when the time at which it is scheduled falls due, unless othervise 

specified. 

When the aircraft inspection have two limits (i.e., 7500 landings or 12 years), the due time 

will be which ever is reached the first.

4. List of units

The units and their equivalent abbreviations used in this document are listed hereafter: 

- LDG: Landings 

- Y: Years 

- M: Months 

- FH: Flight Hour 

- FC: Flight Cycle 

The definitions of landing, flight hour and flight cycle are in Chapter 5 section 5-00-00 § 

Structural Maintenance. 
F2000EX 

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“DASSAULT AVIATION Proprietary Data”

C. CORROSION PREVENTION CONTROL PROGRAM

NOTE: Refer to chapter 05-15 for definitions of Level 1, 2 and 3 corrosion. 

A CPCP is a systematic approach for controlling corrosion in the airplane's primary structure. 

It is a program of maintenance tasks designed to control an aircraft structure to Corrosion 

level 1 or better (Chapter 05-15 and EASA AMC 20-20 provide further details). 

During the whole life of the aircraft, the operator is required to maintain the aircraft structure 

to level 1 of corrosion or better on Principal Structural Element (PSE, Ref. to list in SRM 

number 51-00-02 RPI). 

In order to control the aircraft structure to corrosion level 1 or better on PSEs, the operator 

should implement a CPCP as per Chapter 05-15 (baseline) and to comply and conform to the 

aircraft maintenance manual tasks listed in Chapter 5.10 and 5.20. 

This baseline CPCP should be adapted by the operator to take into account "non standard" 

features of his aircraft, if any. In this case, the operator can find some guidelines in Chapter 

05-15. 

DASSAULT AVIATION is responsible for monitoring the effectiveness of the Baseline 

Program and the pertinence of the inspection threshold and, if necessary, to define changes 

based on analysis of the operators reported findings. Consequently, operators are mandated to 

report any finding affecting a PSE to DASSAULT AVIATION when corrosion level 2 or 3 is 

found. This will allow DASSAULT AVIATION to justify periodicity changes and to publish 

updates of the baseline CPCP. 

NOTE: Reporting of Level 1 corrosion that is recurrent in the same location or nil finding is 

also of interest to DASSAULT AVIATION and should be reported to assist in understanding 

the aging of the fleet and the possible need for escalation or alleviation of maintenance 

program. 
F2000EX 

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D. NOTES

The following notes are the notes used in this document: 

NOTE (1): Reserved 

NOTE (2): Reserved 

NOTE (3): Reserved 

NOTE (4): Reserved 

NOTE (5): Operations covered by zonal inspection 55-00-00-210-802- TSK and 57-00-00-

210-801- TSK scheduled every 2 Y 

NOTE (6): For A/C which exceeded 1400 FH and which did not carry out the inspection yet, 

inspection to be done within 400 FH from effective date of revision 7. 
F2000EX 

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E. AIRFRAME COMPONENTS WITH LIMITED SERVICE LIFE 

The components with limited service life are listed in the tabular form as follows: 

Column 1: Component Functional Index (CFI): Index that allows search throughout 

the maintenance documentation, and for electrical components it is also the electrical 

index. 

Column 2: Part Numbers (P/N): The task is applicable only to the listed P/Ns. Note: A 

P/N in the list may not be applicable to your aircraft. Refer to the IPC for this 

information. 

Column 3: Limited service life: threshold at which the task has to be performed. 

Column 4: Remark: Note or comment related to the procedure/operation or its 

interval. The numbered notes are listed in § Notes 

Column 5: Scheduled maintenance task number, may be either: 

o A task number (12 digits), in accordance with the AMM tasks numbering 

system. In this case, the whole task (all operations of the task) must be 

performed at the required interval. 

o An operation number (14 digits), the first 12 digits being the AMM tasks 

number. In this case, only the operation codes listed have to be performed at 

the required interval. 

 Column 6: Task title: Description of the task or the operation in accordance with the 

AMM. 
FALCON 2000EX 

CHAPTER 5-40

32 : LANDING GEAR

Scheduled

maintenance

task number

Limited Title / Operation

service life

Component

Functional

Index

P/N Remark

5GA - LH MLG leg P/N D23733000-X 32-11-00-960-801-01 REPLACEMENT OF THE MLG LEGS (DISCARD OF LIFE LIMITED 

PARTS) - LH MLG LEG (5GA)

20000 LDG

10GA - RH MLG leg P/N D23734000-X 32-11-00-960-801-02 REPLACEMENT OF THE MLG LEGS (DISCARD OF LIFE LIMITED 

PARTS) - RH MLG LEG (10GA)

20000 LDG

P/N D23732000 or

P/N D23732000-X

5GB - NLG leg 32-21-00-960-801-01 REPLACEMENT OF THE NLG LEG (DISCARD OF LIFE LIMITED 

PARTS) - NLG LEG (5GB)

20000 LDG

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F. MANDATORY MAINTENANCE OPERATIONS 

The mandatory maintenance operations to be performed are listed in the tabular form as 

follows: 

Column 1: Scheduled maintenance task number, may be either: 

o A task number (12 digits), in accordance with the AMM tasks numbering 

system. In this case, the whole task (all operations of the task) must be 

performed at the required interval. 

o An operation number (14 digits), the first 12 digits being the AMM tasks 

number. In this case, only the operation codes listed have to be performed at 

the required interval. 

o The previous numbering (5 digits), if existing, is indicated under the new 

AMTOSS number, as it may be called in some old documents. 

 Column 2: Origin : The origin of these mandatory maintenance operations can be 

o Operations resulting from fatigue tests and damage tolerance calculations –

identified by "FD”: Fatigue and Damage.

o Operations resulting from the certification maintenance requirements - 

identified by "CMR". 

o Operations resulting from aircraft utilization identified by "RetEx": Return of 

Experience.

o Operations resulting from Airworthiness limitation identified by “ALI”.

Column 3: Task title: Description of the task or the operation in accordance with the 

AMM. 

Column 4: First inspection: Threshold at which the task has to be performed. 

Column 5: Interval: Interval at which the task is to be repeated. 

Column 6: Remark: Note, comment or effectivity related to the procedure/operation or 

its interval. The numbered notes are listed in § Notes 
FALCON 2000EX 

CHAPTER 5-40

21 : AIR CONDITIONING

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

21-315

21-32-00-710-803 CMR OPERATIONAL TEST OF THE "CABIN" WARNING LIGHT 440 FH 440 FH [F2000EX]

21-314

21-32-06-200-801-03 INSPECTION / CHECK OF THE ELECTROPNEUMATIC AND PNEUMATIC 1640 FH

VALVES - CHECK OF OVERPRESSURE TIGHTNESS OF 

ELECTROPNEUMATIC VALVE (70HP)

CMR 1640 FH

21-314

21-32-06-200-801-04 INSPECTION / CHECK OF THE ELECTROPNEUMATIC AND PNEUMATIC 1640 FH

VALVES - CHECK OF OVERPRESSURE TIGHTNESS OF PNEUMATIC 

VALVE (80HP)

CMR 1640 FH

21-314

21-32-06-200-801-05 INSPECTION / CHECK OF THE ELECTROPNEUMATIC AND PNEUMATIC 7500 FH

VALVES - CHECK OF OVERPRESSURE RELIEF VALVE VACUUM 

SUPPLY LINES (975HP) AND (976HP)

CMR 7500 FH

21-32-06-720-801-01 FUNCTIONAL TEST OF THE ELECTROPNEUMATIC AND PNEUMATIC 7500 FH

VALVES - ELECTROPNEUMATIC VALVE (70HP)

CMR 7500 FH

21-32-06-720-801-02 FUNCTIONAL TEST OF THE ELECTROPNEUMATIC AND PNEUMATIC 7500 FH

VALVES - PNEUMATIC VALVE (80HP)

CMR 7500 FH

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Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

22 : AUTO FLIGHT

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

22-112

22-13-01-350-801 CMR RESTORATION OF THE YAW DAMPER ACTUATOR (OVERHAUL) 3000 FH 3000 FH [F2000EX]

P/N 822-1794-001

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Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

23 : COMMUNICATIONS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

23-110

23-11-17-710-801 CMR OPERATIONAL TEST OF THE "VHF 1 EMERG" RADIO TUNING SWITCH 1640 FH 1640 FH [F2000EX EASy versions and F2000S]

23-503

23-50-00-710-802 CMR OPERATIONAL TEST OF THE "BKUP" AUDIO BUTTON 1640 FH 1640 FH [F2000EX EASy versions and F2000S]

23-503

23-50-00-710-802 CMR OPERATIONAL TEST OF THE "BKUP" AUDIO BUTTON 1640 FH 1640 FH [F2000EX EASy versions and F2000S]

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FALCON 2000EX 

CHAPTER 5-40

24 : ELECTRICAL POWER

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

24-304

24-30-00-710-801 CMR OPERATIONAL TEST OF THE VOLTAGE MONITORING CIRCUITS 1800 FH 1800 FH See note (6)

24-313

24-30-00-710-803-01 CHECK OF THE CURRENT PROTECTION OF BATTERIES 1 AND 2 AND 7500 FH

OF ESS/MD BUSES INTERCONNECTION - CHECK OF CURRENT 

PROTECTION CIRCUIT BATTERY 1 (150PC)

CMR 7500 FH [F2000EX EASy versions and F2000S]

24-313

24-30-00-710-803-02 CHECK OF THE CURRENT PROTECTION OF BATTERIES 1 AND 2 AND 7500 FH

OF ESS/MD BUSES INTERCONNECTION - CHECK OF CURRENT 

PROTECTION CIRCUIT BATTERY 2 (50PC)

CMR 7500 FH [F2000EX EASy versions and F2000S]

24-313

24-30-00-710-803-03 CHECK OF THE CURRENT PROTECTION OF BATTERIES 1 AND 2 AND 7500 FH

OF ESS/MD BUSES INTERCONNECTION - CHECK OF ESS/MD BUSES 

INTERCONNECTION CONTACTOR (14PC2)

CMR 7500 FH [F2000EX EASy versions and F2000S]

24-313

24-30-00-710-803-04 CHECK OF THE CURRENT PROTECTION OF BATTERIES 1 AND 2 AND 30000 FH

OF ESS/MD BUSES INTERCONNECTION - CHECK OF CURRENT 

PROTECTION CIRCUIT FOR ESS/MD BUSES INTERCONNECTION 

CONTACTOR (14PC2)

CMR 30000 FH [F2000EX EASy versions and F2000S]

24-332

24-30-00-710-804 CMR CHECK OF "LH ISOL" AND "RH ISOL" DISCONNECTION 1800 FH 1800 FH [F2000EX EASy versions and F2000S]

See note (6)

24-337

24-30-00-710-805 CMR CHECK OF "LH ISOL" AND "RH ISOL" LOGIC IN FLIGHT CONDITION 15000 FH 15000 FH [F2000EX EASy versions and F2000S]

24-313

24-32-00-710-802 CMR CHECK OF THE BATTERY REVERSE CURRENT PROTECTION 7500 FH 7500 FH [F2000EX]

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FALCON 2000EX 

CHAPTER 5-40

26 : FIRE PROTECTION

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

26-104

26-10-17-720-801 CMR FUNCTIONAL TEST OF THE PINPOINT FIRE DETECTORS 20000 FH 20000 FH

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Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

27 : FLIGHT CONTROLS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

27-003

27-00-00-220-801 INTEGRITY CHECK AND VISUAL INSPECTION FOR CORROSION AND 4000 FH

EXTERNAL LEAKS ON FLIGHT CONTROL HYDRAULIC COMPONENTS

CMR 4000 FH See note (5)

27-000

27-00-00-710-801 CMR OPERATIONAL TEST OF THE FLIGHT CONTROLS 1650 FH 1650 FH

27-009

27-00-00-720-804-01 CHECK OF THE AUXILIARY AFU NON-DISCONNECTION - INSPECTION 10000 FH

OF LH ROLL AAFU (L66CR)

CMR 10000 FH

27-009

27-00-00-720-804-03 CHECK OF THE AUXILIARY AFU NON-DISCONNECTION - INSPECTION 10000 FH

OF RH ROLL AAFU (R66CR)

CMR 10000 FH

27-009

27-00-00-720-804-05 CHECK OF THE AUXILIARY AFU NON-DISCONNECTION - INSPECTION 10000 FH

OF YAW AAFU (20CL)

CMR 10000 FH

27-009

27-00-00-720-804-07 CHECK OF THE AUXILIARY AFU NON-DISCONNECTION - INSPECTION 10000 FH

OF PITCH AAFU (20CP)

CMR 10000 FH

27-007

27-00-00-790-803 CMR CHECK OF THE SERVO-ACTUATOR INTERNAL DAMPING 1800 FH 1800 FH

27-104

27-14-05-720-801 CMR FUNCTIONAL TEST OF THE ROLL TRIM CONTROL SAFETY RELAYS 20000 FH 20000 FH

27-206

27-24-05-720-802 CMR FUNCTIONAL TEST OF THE YAW TRIM CONTROL SAFETY RELAYS 20000 FH 20000 FH

27-409

27-40-01-350-801 RESTORATION OF THE HORIZONTAL STABILIZER ACTUATOR (FULL 7725 FC

DISASSEMBLY, INSPECTION/CHECK AND NDT)

CMR 7725 FC

27-411

27-40-15-710-801 OPERATIONAL TEST OF THE RELAY IN THE HORIZONTAL STABILIZER 16000 FH

EMERGENCY CONTROL BOX

CMR 16000 FH

27-405

27-40-17-720-801 CMR FUNCTIONAL TEST OF THE HORIZONTAL STABILIZER RELAY BOX 5000 FH 5000 FH

27-502

27-50-00-720-802 CMR FUNCTIONAL TEST OF THE FLAP ASYMMETRY DETECTION SYSTEM 450 FH 450 FH

27-53-01-350-801-01 RESTORATION OF THE FLAP SCREW JACKS (OVERHAUL) - LH 4500 LDG

OUTBOARD FLAP SCREW JACK (40CF)

RetEx 4500 LDG

P/N 1-5319-3

27-53-01-350-801-02 RESTORATION OF THE FLAP SCREW JACKS (OVERHAUL) - LH 3500 LDG

INBOARD FLAP LATERAL SCREW JACK (L25CF)

RetEx 3500 LDG

P/N 5318-3

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FALCON 2000EX 

CHAPTER 5-40

27 : FLIGHT CONTROLS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

27-53-01-350-801-03 RESTORATION OF THE FLAP SCREW JACKS (OVERHAUL) - LH 3500 LDG

INBOARD FLAP CENTER SCREW JACK (L20CF)

RetEx 3500 LDG

P/N 5318-3

27-53-01-350-801-04 RESTORATION OF THE FLAP SCREW JACKS (OVERHAUL) - RH 3500 LDG

INBOARD FLAP CENTER SCREW JACK (R20CF)

RetEx 3500 LDG

P/N 5318-3

27-53-01-350-801-05 RESTORATION OF THE FLAP SCREW JACKS (OVERHAUL) - RH 3500 LDG

INBOARD FLAP LATERAL SCREW JACK (R25CF)

RetEx 3500 LDG

P/N 5318-3

27-53-01-350-801-06 RESTORATION OF THE FLAP SCREW JACKS (OVERHAUL) - RH 4500 LDG

OUTBOARD FLAP SCREW JACK (30CF)

RetEx 4500 LDG

P/N 2-5319-3

27-504

27-53-01-720-803-01 CHECK OF THE SCREW / NUT PLAY ON FLAP SCREW JACKS (AVIAC) - 450 FH

LH OUTBOARD FLAP SCREW JACK (40CF)

RetEx 3000 LDG

P/N 1-5319-3

27-504

27-53-01-720-803-02 CHECK OF THE SCREW / NUT PLAY ON FLAP SCREW JACKS (AVIAC) - 450 FH

LH INBOARD FLAP LATERAL SCREW JACK (L25CF)

RetEx 3000 LDG

P/N 5318-3

27-504

27-53-01-720-803-03 CHECK OF THE SCREW / NUT PLAY ON FLAP SCREW JACKS (AVIAC) - 450 FH

LH INBOARD FLAP CENTER SCREW JACK (L20CF)

RetEx 3000 LDG

P/N 5318-3

27-504

27-53-01-720-803-04 CHECK OF THE SCREW / NUT PLAY ON FLAP SCREW JACKS (AVIAC) - 450 FH

RH INBOARD FLAP CENTER SCREW JACK (R20CF)

RetEx 3000 LDG

P/N 5318-3

27-504

27-53-01-720-803-05 CHECK OF THE SCREW / NUT PLAY ON FLAP SCREW JACKS (AVIAC) - 450 FH

RH INBOARD FLAP LATERAL SCREW JACK (R25CF)

RetEx 3000 LDG

P/N 5318-3

27-504

27-53-01-720-803-06 CHECK OF THE SCREW / NUT PLAY ON FLAP SCREW JACKS (AVIAC) - 450 FH

RH OUTBOARD FLAP SCREW JACK (30CF)

RetEx 3000 LDG

P/N 2-5319-3

27-610

27-61-00-720-801 FUNCTIONAL TEST OF THE AUTOMATIC AIRBRAKE EXTENSION 440 FH

CIRCUIT ("BSCU HARDWARE" RELAY)

CMR 440 FH [F2000EX EASy versions and F2000S]

27-611

27-61-00-720-802 FUNCTIONAL TEST OF THE AUTOMATIC AIRBRAKE EXTENSION 440 FH

CIRCUIT ("LH THROTTLE" and "RH THROTTLE" RELAYS)

CMR 440 FH [F2000EX EASy versions and F2000S]

27-612

27-61-00-720-803 FUNCTIONAL TEST OF THE AUTOMATIC AIRBRAKE EXTENSION 1240 FH

CIRCUIT ("BSCU SOFTWARE" RELAY)

CMR 1240 FH [F2000EX EASy versions and F2000S]

Page 20 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

27 : FLIGHT CONTROLS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

27-615

27-61-00-720-806 FUNCTIONAL TEST OF THE AUTOMATIC AIRBRAKE EXTENSION 440 FH

CIRCUIT (MONITORING SYSTEM)

CMR 440 FH [F2000EX EASy versions and F2000S]

27-616

27-61-00-720-807 FUNCTIONAL TEST OF THE AUTOMATIC AIRBRAKE EXTENSION 150 FH

CIRCUIT

CMR 150 FH [F2000EX]

27-801

27-80-00-710-806 OPERATIONAL TEST OF THE GROUND / FLIGHT RELAYS AND ANGLE- 1800 FH

OF-ATTACK SENSOR CONTACTS

CMR 1800 FH [F2000EX]

27-80-00-710-807 OPERATIONAL TEST OF SLAT EXTENSION THROUGH LH SOLENOID 440 FH

(S1)

CMR 440 FH [F2000EX EASy versions and F2000S]

A/C 263-600 and >=701

27-80-00-710-808 OPERATIONAL TEST OF THE SLAT MONITORING SYSTEM (INBOARD 3240 FH

SLAT EXTENDED POSITION MICROSWITCHES)

CMR 3240 FH [F2000EX EASy versions and F2000S]

A/C 263-600 and >=701

27-80-00-710-809 CMR OPERATIONAL TEST OF SLAT STALL 1 AND STALL 2 1840 FH 1840 FH [F2000EX EASy versions and F2000S]

A/C 263-600 and >=701

27-803

27-80-00-720-801 CMR FUNCTIONAL TEST OF THE SLATS 1800 FH 1800 FH [F2000EX EASy versions and F2000S]

Page 21 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

29 : HYDRAULIC POWER

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

29-114

29-12-05-710-801 CMR OPERATIONAL TEST OF THE HYDRAULIC SHUT-OFF VALVES 450 FH 450 FH

A/C with hydraulic shut-off valves (M0749)

Page 22 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

31 : INDICATING - RECORDING SYSTEMS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

31-501

31-54-00-720-801 CMR FUNCTIONAL TEST OF THE TAKE-OFF SAFETIES: ALARM TEST 700 FH 700 FH [F2000EX]

31-600

31-60-00-710-801-08 OPERATIONAL TEST OF THE CENTRAL DISPLAY SYSTEM (CDS) - 1640 FH

REVERSION CONTROLLER (364NH)

CMR 1640 FH [F2000EX EASy versions and F2000S]

Page 23 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

32 : LANDING GEAR

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

32-471

32-41-00-710-803-01 CMR OPERATIONAL TEST OF THE AUTO-BRAKE SYSTEM 1650 FH 1650 FH [F2000EX EASy versions]

A/C 6 and 28-262 and 601-604

P/N 5527-4610 or with M3177

32-470

32-41-00-720-803-01 FUNCTIONAL TEST OF THE AUTO-BRAKE SYSTEM - TEST OF 850 FH

POSITIVE COIL OF PCB

CMR 850 FH [F2000EX EASy versions]

A/C 6 and 28-262 and 601-604

P/N 5527-4610 or with M3177

32-470

32-41-00-720-803-02 FUNCTIONAL TEST OF THE AUTO-BRAKE SYSTEM - TEST OF 850 FH

NEGATIVE COIL OF PCB

CMR 850 FH [F2000EX EASy versions]

A/C 6 and 28-262 and 601-604

P/N 5527-4610 or with M3177

32-470

32-41-00-720-803-03 FUNCTIONAL TEST OF THE AUTO-BRAKE SYSTEM - TEST OF 1650 FH

INDICATING SYSTEM

CMR 1650 FH [F2000EX EASy versions]

A/C 6 and 28-262 and 601-604

P/N 5527-4610 or with M3177

32-472

32-41-59-710-801 CMR OPERATIONAL TEST OF THE AUTO-BRAKE PCB'S 6500 FH 6500 FH [F2000EX EASy versions]

A/C 6 and 28-262 and 601-604

P/N 5527-4650 or with M3551

32-408

32-42-05-720-801 CMR FUNCTIONAL TEST OF THE PARK BRAKE ACCUMULATOR CAPACITY 1240 FH 1240 FH [F2000EX and F2000EX EASy versions]

A/C 001-117

Page 24 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

34 : NAVIGATION

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

34-209

34-21-00-700-801-01 CHECK OF THE GENERAL-PURPOSE BUSES TO THE INERTIAL 5000 FH

REFERENCE SYSTEM (IRS) - IRU 1

CMR 5000 FH [F2000EX EASy versions and F2000S]

34-209

34-21-00-700-801-02 CHECK OF THE GENERAL-PURPOSE BUSES TO THE INERTIAL 5000 FH

REFERENCE SYSTEM (IRS) - IRU 2

CMR 5000 FH [F2000EX EASy versions and F2000S]

34-324

34-31-00-720-801 CMR FUNCTIONAL TEST OF THE HGS DUAL POWER SUPPLY 1400 FH 1400 FH [F2000EX]

Page 25 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

35 : OXYGEN

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

35-200

35-20-00-720-801 CMR FUNCTIONAL TEST OF THE PASSENGER OXYGEN SYSTEM 1740 FH 1740 FH [F2000EX]

35-200

35-20-00-720-801 CMR FUNCTIONAL TEST OF THE PASSENGER OXYGEN SYSTEM 1640 FH 1640 FH [F2000EX EASy versions and F2000S]

Page 26 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

36 : PNEUMATIC

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

36-00-01-710-802 CMR OPERATIONNAL TEST OF ARINC LINK BETWEEN BASC AND MAU 9000 FH 9000 FH [F2000EX EASy versions and F2000S]

36-200

36-21-21-710-801 CMR OPERATIONAL TEST OF THE ENGINE PYLON OVERHEAT PROBES 1800 FH 1800 FH

Page 27 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

52 : DOORS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

52-205

52-20-00-610-801-01 SERVICING OF THE EMERGENCY EXIT DOOR - TEST OF THE 24 M

EMERGENCY EXIT DOOR UNLOCKING FROM INSIDE THE CABIN

RetEx 24 M

Page 28 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

53 : FUSELAGE

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

53-025

53-00-00-200-803-01 INSPECTION OF THE FUSELAGE SKIN - FRAME 4 TO FRAME 26 - 3750 FC

GENERAL VISUAL INSPECTION

FD 11250 FC

53-025

53-00-00-200-803-02 INSPECTION OF THE FUSELAGE SKIN - FRAME 4 TO FRAME 26 - 3750 FC

DETAILED INSPECTION IN SPECIFIC AREAS

FD 11250 FC

53-024

53-10-00-200-810-01 INSPECTION OF THE FUSELAGE SKIN - FRAME 0 TO FRAME 4 - 3750 FC

GENERAL VISUAL INSPECTION OF SKIN

FD 7500 FC

53-024

53-10-00-200-810-02 INSPECTION OF THE FUSELAGE SKIN - FRAME 0 TO FRAME 4 - 3750 FC

DETAILED INSPECTION IN SPECIFIC AREAS

FD 11250 FC

53-031

53-10-03-250-801 SPECIAL DETAILED INSPECTION OF THE UPPER PASSENGER DOOR 3750 FC

FRAME EDGING

FD 11250 FC

53-052

53-10-11-250-801 FD SPECIAL DETAILED INSPECTION OF THE SPLICE AT FRAME 11 11250 FC 3750 FC

53-037

53-10-39-220-802 DETAILED INSPECTION OF THE COCKPIT WINDSHIELD / WINDOW 3750 FC

FRAMES

FD 11250 FC

53-028

53-30-00-250-801 EDDY CURRENT INSPECTION OF THE PASSENGER CABIN SKIN 3750 FC

PANEL AROUND EMERGENCY EXIT DOOR ROUNDED ANGLES

FD 7500 FC

53-027

53-30-00-250-802 EDDY CURRENT INSPECTION OF THE SKIN PANELS AROUND CABIN 3750 FC

WINDOW CUT-OUTS

FD 7500 FC

53-043

53-30-26-220-801 FD DETAILED INSPECTION AT FRAME 26 11250 FC 3750 FC

53-042

53-30-26-250-801-01 FD EDDY CURRENT INSPECTION AT FRAME 26 - VERTICAL BEAMS 3750 FC 3750 FC

53-042

53-30-26-250-801-02 FD EDDY CURRENT INSPECTION AT FRAME 26 - STIFFENER 17 7500 FC 3750 FC

53-042

53-30-26-250-801-03 EDDY CURRENT INSPECTION AT FRAME 26 - KEEL BEAM FLANGE 3750 FC

CONNECTION

FD 11250 FC

53-034

53-41-00-220-802 FD DETAILED INSPECTION OF THE LOWER WING ROOT BOLT RECESSES 11250 FC 3750 FC

53-053

53-50-23-250-801 FD SPECIAL DETAILED INSPECTION OF FRAME 23 (LH LOWER PART) 11250 FC 3750 FC

Page 29 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

53 : FUSELAGE

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

53-030

53-50-23-250-802 EDDY CURRENT INSPECTION OF THE BAGGAGE COMPARTMENT 3750 FC

SKIN PANELS AROUND DOOR LOWER ROUNDED ANGLE AT FRAME 23

FD 11250 FC

53-054

53-50-29-220-801 FD DETAILED INSPECTION OF SPLICE AT FRAME 29 11250 FC 3750 FC

53-044

53-50-30-250-801 FD EDDY-CURRENT INSPECTION AT FRAME 30 11250 FC 3750 FC

53-045

53-50-33-250-801 FD EDDY-CURRENT INSPECTION AT FRAME 33 11250 FC 3750 FC

53-047

53-50-43-250-801 EDDY-CURRENT INSPECTION OF THE LOWER FIN FRONT SPAR 3750 FC

FLANGES

FD 11250 FC

Page 30 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

54 : NACELLES AND PYLONS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

54-011

54-50-00-220-801 FD DETAILED VISUAL INSPECTION OF RIBS 29 AND 29-A 11250 FC 3750 FC

Page 31 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

55 : STABILIZERS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

55-002

55-10-00-270-801 ULTRASONIC INSPECTION OF THE HORIZONTAL STABILIZER HINGE 3750 FC

FITTINGS

FD 11250 FC

55-501

55-10-31-220-801 DIMENSIONAL CHECK OF HORIZONTAL STABILIZER REAR HINGE 3750 FC

BUSHINGS

FD 3750 FC

55-003

55-10-39-220-801 DETAILED INSPECTION OF THE HORIZONTAL STABILIZER ACTUATOR 3750 FC

ATTACHMENT FITTINGS AND PINS

FD 11250 FC

55-004

55-30-00-270-801 ULTRASONIC INSPECTION OF THE VERTICAL STABILIZER / STUB 3750 FC

ATTACHMENTS

FD 11250 FC

Page 32 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

57 : WINGS

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

57-008

57-10-01-210-801 FD GENERAL VISUAL INSPECTION OF THE WING LOWER PANELS 11250 FC 3750 FC

57-060

57-10-14-220-801 DETAILED INSPECTION OF THE WING FRONT SPAR FROM ROOT TO 7500 FC

RIB 17 EXCEPT RIB 6 TO RIB 9

FD 11250 FC

57-070

57-10-14-220-802 DETAILED INSPECTION OF THE WING FRONT SPAR FROM RIB 6 TO 3750 FC

RIB 9

FD 11250 FC

57-090

57-10-15-220-801 DETAILED INSPECTION OF THE WING REAR SPAR 1 FROM ROOT TO 3750 FC

RIB 3

FD 11250 FC

57-080

57-10-15-220-802 DETAILED INSPECTION OF THE WING REAR SPAR 2 FROM RIB 3 TO 7500 FC

RIB 17

FD 11250 FC

57-005

57-10-15-250-801 EDDY-CURRENT INSPECTION OF THE RIB 8 REAR WING SPAR SPLICE 7500 FC

PLATE

FD 11250 FC

Page 33 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

71 : POWER PLANT

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

54-012

71-20-02-250-801 SPECIAL DETAILED INSPECTION OF THE ENGINE FRONT MOUNTS 3750 FC

(YOKE ASSEMBLY)

FD 7500 FC

71-20-05-350-801 RESTORATION OF THE ENGINE FRONT VIBRATION ISOLATORS 11250 FC

(OVERHAUL)

FD 11250 FC

71-20-09-350-801 RESTORATION OF THE ENGINE REAR VIBRATION ISOLATORS 11250 FC

(OVERHAUL)

FD 11250 FC

Page 34 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

73 : ENGINE FUEL AND CONTROL

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

73-302

73-40-00-700-801 CMR INDICATION TEST OF APR 450 FH 450 FH

73-301

73-40-00-710-801 CMR OPERATIONAL TEST OF APR 1800 FH 1800 FH [F2000EX]

Page 35 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
FALCON 2000EX 

CHAPTER 5-40

78 : EXHAUST

Scheduled

maintenance

task number

Origin Title / Operation First Inspection Interval Remarks

78-300

78-30-00-210-801 CMR GENERAL VISUAL INSPECTION OF THE THRUST REVERSER 1800 FH 1800 FH

78-350

78-31-03-220-801 DETAILED INSPECTION OF THRUST REVERSER PIVOT LINK 7500 FH

ASSEMBLIES

CMR 7500 FH

78-351

78-32-00-720-801 CMR FUNCTIONAL TEST OF THE INHIBIT ARM COMMAND CIRCUIT 1800 FH 1800 FH [F2000EX]

78-316

78-32-00-760-802 CMR TEST OF THE TRCU CONTROL INPUT CIRCUITS 1800 FH 1800 FH

78-349

78-32-45-700-801 CMR TEST OF THE THRUST REVERSER CONTROL UNIT 7500 FH 7500 FH

Page 36 / 37

“DASSAULT AVIATION Proprietary Data”

Effectivity : ALL – Reference DGT 113877

Rev. Date : 02/2013
F2000EX 

CHAPTER 5-40 

Effectivity : ALL-Reference DGT 113877 

Rev. Date : 02/2013 

Page 37 / 37 

“DASSAULT AVIATION Proprietary Data”

 END OF DOCUMENT