FALCON 50/50EX MAINTENANCE MANUAL

the chapter, with no technical change. The technical content of this revision is approved under DOA EASA.21J.051 authority by reference R5025. Effective date of this revision: January 30, 2013 - Revision 23: This revision 23 is the compilation of the following EASA approved changes, with no further technical change: · CP 012 approved by EASA under change reference M3261 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: August 5, 2015 - Revision 24: This revision 24 is the compilation of the following EASA approved changes, with no further technical change: · CP 011 approved by EASA under change reference M3236 · CP 014 approved by EASA under change reference M3272 . CH5-40-CP0001-CPAS approved by EASA under change reference M3280 The technical content of this revision is approved under DOA EASA.21J.051 authority by reference R5062. 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: August 9, 2017 FALCON 50/50EX CHAPTER 5-40 Page 6/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 B. GENERAL This document is applicable to Falcon F50/F50EX A/C S/N 001 to 352. This section contains instructions pertaining to Airworthiness of aircraft, including SSIP, CPCP and Safe Life limitations until the Limit of Validity (refer to paragraph A. 1). These instructions are rendered mandatory by Airworthiness Directives issued by the country of registration. For U.S. Registered aircraft, this section is European Aviation Safety Agency approved on behalf of FAA and specifies maintenance required under paragraphs 43.16 and 91.409 of the Federal Aviation Regulations, unless an alternative program has been FAA approved. Evaluations and reasons for this section do not take into account the influence of modifications or repairs not approved by DASSAULT AVIATION such as STC 1. Definition of the Limit Of Validity (L.O.V.) The Limit Of Validity represents the upper limit expressed in "flights" until which an aircraft can fly in total security without appearance of WFD (Widespread Fatigue Damages). The L.O.V. of a standard aircraft MYSTERE-FALCON 50 (refer to paragraph B.) is 40,000 flights/60,000 flying hours whichever occurs first. For a standard aircraft (refer to paragraph B.), to facilitate scheduling of maintenance operations expressed in "FLIGHTS", a flight is considered as equivalent to a landing. For a non-standard aircraft, a flight is not automatically considered as a landing. That is why, "flights" have to be recorded regarding a specific definition established by DASSAULT AVIATION. In this case, contact DASSAULT AVIATION for appropriate program. 2. 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,...) up to the L.O.V. 2.1. 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. FALCON 50/50EX CHAPTER 5-40 Page 7/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 2.2. 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 types 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 passenger transport. 2.3. Maintenance must have been performed in accordance with: - The Maintenance Manual or Structural Repair Manual (formerly Maintenance and Repair Instructions) recommended by DASSAULT AVIATION, or - Approved maintenance procedures. 3. 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 Manual 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. The section 5-40 gives mandatory time limits. In order to help operators planning maintenance program and to reduce grounding time due to the scheduled maintenance, these mandatory maintenance operations are also listed in sections 5-10 or 5-20 with recommended periodic values lower than or equal to the mandatory time limits, corresponding to the aircraft inspections or expressed as a number of flights, hours, landings or calendar. 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. FALCON 50/50EX CHAPTER 5-40 Page 8/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 4. Updating of 5-40 sections When a new maintenance operation is added, due to a revision of Chapter 5-40, this new operation must be performed when the time at which it is scheduled falls due, unless otherwise specified. 5. 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. FALCON 50/50EX CHAPTER 5-40 Page 9/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 C. SSIP AND CPCP PROGRAMS 1. Structural Supplemental Inspection Program (SSIP) SB F50-450 is a prerequisite to the application of SSIP program NOTE: SB F50-450 shall be embedded before applying the SSIP inspections defined in the section 5-40-00 § F “Mandatory Maintenance Operations” The Supplemental Structural Inspection Program (SSIP) must be applied to aircraft that have reached the "mid life" of their L.O.V. (20,000 flights/30,000 flying hours, whichever occur first) with a continuing structural integrity program in accordance with manufacturer Recommended Maintenance Schedule, T.B.O. and Chapter 5. The operator must include in his maintenance program the maintenance operations linked with structural inspection for fatigue defects. Those operations are marked with "SSIP" in the column "Origin" in section 5-40-00 § F “Mandatory Maintenance Operations” and are still present in section 5-10-01 (Chapter 5 SSIP, specific supplement list). An S inspection and its multiples must be considered as a supplemental inspection of the airframe scheduled every 3750 flights (after application of SB F50-450). NOTE: Those dedicated Supplemental Maintenance inspections are not included in AMM and not listed in Chapter 5-10-00. They are provided as part of the SB F50-450 package (AMM SSIP and Chapter 5 SSIP). 2. Corrosion Prevention Control Program (CPCP) 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 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 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 FALCON 50/50EX CHAPTER 5-40 Page 10/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 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. D. NOTES The following notes are the notes used in this document: NOTE 1: Each landing on an unpaved runway shall be multiplied by 2 for the nose gear when calculating limited service life. NOTE 2: Only applicable to A/C 1, 3 to 39 before SBF50-123 (equipped with MLG shock absorber end-fitting P/N D50493) NOTE 3: Only applicable to A/C 1 to 85 before SBF50-124 (equipped with MLG strut actuator dash-pot sleeve P/N D52369) NOTE 4: ENGINE 1 and 3 REAR ATTACHMENT AUXILIARY FITTING BOLT introduced by SB F50-0113 associated with French D.G.A.C. Airworthiness Directive No. 81-226-1 (B) NOTE 5: Inspection to be performed at the next C inspection from effective date of revision 20 NOTE 6: For A/C having exceeded 20,000 FC, NDT check to be performed within 3750 FC from effective date of revision 20 NOTE 7: For A/C having exceeded 7300 FC, NDT check to be done within 600 FC from effective date of revision 19 NOTE 8: This task must be performed on components. The value of the interval given for each component considers its cumulated presence on one or several aircraft. Unless specified (landings for example), the unit of the interval is expressed in measurable aircraft level figures (aircraft flight hours, aircraft cycles or age) and not in component operating time. FALCON 50/50EX CHAPTER 5-40 Page 11/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 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: Notes or comments related to the procedure/operation or its interval. The numbered notes are listed in § General.  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 50/50EX CHAPTER 5-40 Page 12/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 32: LANDING GEAR Component Functional Index P/N Limited service life Remark Scheduled maintenance task number Title / Operation L2GF - LH MLG leg P/N C23791-10XX 20000 LDG See Note (8) 32-11-00-960-801-01 REPLACEMENT OF THE MLG LEGS (DISCARD OF LIFE LIMITED PARTS) - LH MLG LEG (L2GF) R2GF - RH MLG leg P/N C23792-10XX 20000 LDG See Note (8) 32-11-00-960-801-02 REPLACEMENT OF THE MLG LEGS (DISCARD OF LIFE LIMITED PARTS) - RH MLG LEG (R2GF) L2GF7 - LH MLG pintle pin P/N D48611 or P/N D52554-1 or P/N D52554-2 18670 LDG A/C with SB F50-161 only (MTOW : 18.5T) See Note (8) 32-11-03-960-801-01 DISCARD OF THE MLG PINTLE PIN - LH MLG PINTLE PIN (L2GF7) R2GF7 - RH MLG pintle pin P/N D48611 or P/N D52554-1 or P/N D52554-2 18670 LDG A/C with SB F50-161 only (MTOW : 18.5T) See Note (8) 32-11-03-960-801-02 DISCARD OF THE MLG PINTLE PIN - RH MLG PINTLE PIN (R2GF7) L2GF5 - LH MLG shock absorber P/N C23795-10 or P/N C23795-1001 16000 LDG See Note (2) and (8) 32-11-05-350-801-01 RESTORATION OF THE MLG SHOCK ABSORBER (DISCARD OF END- FITTING) - LH MLG SHOCK ABSORBER (L2GF5) R2GF5 - RH MLG shock absorber P/N C23796-10 or P/N C23796-1001 16000 LDG See Note (2) and (8) 32-11-05-350-801-02 RESTORATION OF THE MLG SHOCK ABSORBER (DISCARD OF END- FITTING) - RH MLG SHOCK ABSORBER (R2GF5) FALCON 50/50EX CHAPTER 5-40 Page 13/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 32: LANDING GEAR Component Functional Index P/N Limited service life Remark Scheduled maintenance task number Title / Operation 12G1 - LH MLG brace strut actuator P/N C23925-11-1 3550 LDG See Note (3) and (8) 32-11-21-350-801-01 RESTORATION OF THE MLG BRACE ACTUATOR (DISCARD OF DASH-POT FITTING) - LH MLG BRACE STRUT ACTUATOR (12G1) 12G2 - RH MLG brace strut actuator P/N C23926-11-1 3550 LDG See Note (3) and (8) 32-11-21-350-801-02 RESTORATION OF THE MLG BRACE ACTUATOR (DISCARD OF DASH-POT FITTING) - RH MLG BRACE STRUT ACTUATOR (12G2) 3GF - NLG leg P/N C23787-10XX 20000 LDG See Note (1) and (8) 32-21-00-960-801-01 REPLACEMENT OF THE NLG LEG (DISCARD OF LIFE LIMITED PARTS) - NLG LEG (3GF) FALCON 50/50EX CHAPTER 5-40 Page 14/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 52: DOORS Component Functional Index P/N Limited service life Remark Scheduled maintenance task number Title / Operation 900MB1 - LH emergency exit door P/N F50B296001XX 26718 FC See Note (8) 52-20-01-960-801-01 DISCARD OF THE EMERGENCY EXIT DOORS - LH EMERGENCY EXIT DOOR (900MB1) 900MB2 - RH emergency exit door P/N F50B296001XX 26718 FC See Note (8) 52-20-01-960-801-02 DISCARD OF THE EMERGENCY EXIT DOORS - RH EMERGENCY EXIT DOOR (900MB2) FALCON 50/50EX CHAPTER 5-40 Page 15/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 53: FUSELAGE Component Functional Index P/N Limited service life Remark Scheduled maintenance task number Title / Operation [F50] P/N F50B237B5 17760 FC A/C 107 only 53-40-07-960-801-01 DISCARD OF THE CENTERWING TANK LOWER PANELS FALCON 50/50EX CHAPTER 5-40 Page 16/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 57: WINGS Component Functional Index P/N Limited service life Remark Scheduled maintenance task number Title / Operation L901CD - LH outboard airbrake center hinge P/N F50B165003001 or P/N FGFC165003001 20000 FC See Note (8) 57-70-03-960-801-01 DISCARD OF OUTBOARD AIRBRAKE CENTER HINGE - LH OUTBOARD AIRBRAKE CENTER HINGE (L901CD) R901CD - RH outboard airbrake center hinge P/N F50B165003001 or P/N FGFC165003001 20000 FC See Note (8) 57-70-03-960-801-02 DISCARD OF OUTBOARD AIRBRAKE CENTER HINGE - RH OUTBOARD AIRBRAKE CENTER HINGE (R901CD) FALCON 50/50EX CHAPTER 5-40 Page 17/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 71: POWER PLANT Component Functional Index P/N Limited service life Remark Scheduled maintenance task number Title / Operation L912EZ - rear attachment auxiliary fitting bolt for engine 1 [F50] P/N 3073361-1 1050 FH See Note (4) and (8) 71-20-07-960-801-01 DISCARD OF THE ENGINE REAR ATTACHMENT AUXILIARY FITTING BOLT - ENGINE 1 R912EZ - rear attachment auxiliary fitting bolt for engine 3 [F50] P/N 3073361-1 1050 FH See Note (4) and (8) 71-20-07-960-801-02 DISCARD OF THE ENGINE REAR ATTACHMENT AUXILIARY FITTING BOLT - ENGINE 3 FALCON 50/50EX CHAPTER 5-40 Page 18/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 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 or SSIP task 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 or SSIP task number. In this case, only the operation codes listed have to be performed at the required interval.  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 "FDBCK": In- service feedback. o Operations resulting from Airworthiness limitation identified by “ALI”, o Operations resulting from SSIP requirements identified by “SSIP” (refer to § C.1).  Column 3: Task title: Description of the task or the operation in accordance with the AMM or SSIP.  Column 4: First inspection: the task must have been performed no later than this maximum limit.  Column 5: Interval: the task must be repeated no later than this maximum interval thereafter.  Column 6: Remark: Notes, comments or effectivity related to the procedure/operation or its interval. The numbered notes are listed in § Notes. FALCON 50/50EX CHAPTER 5-40 Page 19/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 21: AIR CONDITIONING Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 21-30-00-790-802-01 CMR IN-FLIGHT CHECK OF CABIN SEALING 7000 FC then at 10000 FC 700 FC Or procedure 21-30-00-790-801 (Ground check of cabin sealing) 21-32-00-710-801-01 CMR OPERATIONAL TEST OF THE CABIN PRESSURIZATION SYSTEM 1550 FH 1550 FH A/C with pressurization controller P/N 22201N061000 or P/N 22201D131700 test to be performed in manual mode only 21-32-06-200-801-03 CMR INSPECTION / CHECK OF THE ELECTROPNEUMATIC AND PNEUMATIC VALVES - CHECK OF OVERPRESSURE TIGHTNESS OF ELECTROPNEUMATIC VALVE (L74H) 1640 FH 1640 FH See Note (8) 21-32-06-200-801-04 CMR INSPECTION / CHECK OF THE ELECTROPNEUMATIC AND PNEUMATIC VALVES - CHECK OF OVERPRESSURE TIGHTNESS OF PNEUMATIC VALVE (R74H) 1640 FH 1640 FH See Note (8) 21-32-06-200-801-05 CMR INSPECTION / CHECK OF THE ELECTROPNEUMATIC AND PNEUMATIC VALVES - CHECK OF OVERPRESSURE RELIEF VALVE VACUUM SUPPLY LINES (975HP) AND (976HP) 7500 FH 7500 FH See Note (8) 21-32-06-720-801-01 CMR FUNCTIONAL TEST OF THE ELECTROPNEUMATIC AND PNEUMATIC VALVES - ELECTROPNEUMATIC VALVE (L74H) 5000 FH 5000 FH See Note (8) 21-32-06-720-801-02 CMR FUNCTIONAL TEST OF THE ELECTROPNEUMATIC AND PNEUMATIC VALVES - PNEUMATIC VALVE (R74H) 5000 FH 5000 FH See Note (8) FALCON 50/50EX CHAPTER 5-40 Page 20/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 21: AIR CONDITIONING Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 21-32-17-720-801-01 CMR FUNCTIONAL TEST OF THE BAGGAGE COMPARTMENT PRESSURE RELIEF VALVES - LH POSITIVE AND NEGATIVE PRESSURE RELIEF VALVE (L536H) 3700 FH 3700 FH 21-32-17-720-801-02 CMR FUNCTIONAL TEST OF THE BAGGAGE COMPARTMENT PRESSURE RELIEF VALVES - RH POSITIVE AND NEGATIVE PRESSURE RELIEF VALVE (R536H) 3700 FH 3700 FH 21-32-33-710-801-01 CMR OPERATIONAL TEST OF THE BAGGAGE COMPARTMENT ISOLATION AND SUPPLY VALVES - BAGGAGE COMPARTMENT ISOLATION VALVE (153H) 650 FH 650 FH 21-32-33-710-801-02 CMR OPERATIONAL TEST OF THE BAGGAGE COMPARTMENT ISOLATION AND SUPPLY VALVES - BAGGAGE COMPARTMENT HOT AIR SUPPLY VALVE (154H) 650 FH 650 FH FALCON 50/50EX CHAPTER 5-40 Page 21/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 22: AUTO FLIGHT Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 22-13-01-350-801-01 CMR RESTORATION OF THE YAW DAMPER ACTUATOR (OVERHAUL) 3000 FH 3000 FH A/C with yaw damper actuator P/N 822-1793-001 or P/N 822-1795-001 See Note (8) FALCON 50/50EX CHAPTER 5-40 Page 22/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 25: EQUIPMENT / FURNISHINGS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 25-11-05-200-801-01 FDBCK VISUAL INSPECTION OF BUCKLE SPRING OF ANJOU AERONAUTIQUE SAFETY BELTS AND RESTRAINT SYSTEM (TYPE 343 AND 343-1) 18 M (*) (*) Life limit of 60 M for seat safety belt assembly See CN 2002-105 (AB) and CN 2002-104 (AB) FALCON 50/50EX CHAPTER 5-40 Page 23/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 26: FIRE PROTECTION Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 26-10-00-720-801-01 CMR FUNCTIONAL TEST OF THE PNEUMATIC FIRE DETECTORS - ENGINE 1 FIRE DETECTOR (L2W) 5600 FH 5600 FH See Note (8) 26-10-00-720-801-02 CMR FUNCTIONAL TEST OF THE PNEUMATIC FIRE DETECTORS - ENGINE 2 FIRE DETECTOR (M2W) 5600 FH 5600 FH See Note (8) 26-10-00-720-801-03 CMR FUNCTIONAL TEST OF THE PNEUMATIC FIRE DETECTORS - ENGINE 3 FIRE DETECTOR (R2W) 5600 FH 5600 FH See Note (8) 26-10-00-720-801-04 CMR FUNCTIONAL TEST OF THE PNEUMATIC FIRE DETECTORS - APU FIRE DETECTOR (72W) 5600 FH 5600 FH See Note (8) 26-10-00-720-801-05 CMR FUNCTIONAL TEST OF THE PNEUMATIC FIRE DETECTORS - REAR COMPARTMENT FIRE DETECTOR (22W) 5600 FH 5600 FH See Note (8) 26-10-00-720-801-06 CMR FUNCTIONAL TEST OF THE PNEUMATIC FIRE DETECTORS - LH MLG BAY FIRE DETECTOR (29W1) 5600 FH 5600 FH See Note (8) 26-10-00-720-801-07 CMR FUNCTIONAL TEST OF THE PNEUMATIC FIRE DETECTORS - RH MLG BAY FIRE DETECTOR (29W2) 5600 FH 5600 FH See Note (8) FALCON 50/50EX CHAPTER 5-40 Page 24/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 27: FLIGHT CONTROLS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 27-22-01-350-802-01 CMR RESTORATION OF THE RUDDER SERVO-ACTUATOR (FUNCTIONAL TEST) 10000 FH 10000 FH See Note (8) 27-32-01-350-801-01 CMR RESTORATION OF THE ELEVATOR SERVO-ACTUATOR (FUNCTIONAL TEST) 10000 FH 10000 FH See Note (8) 27-32-03-350-801-01 CMR RESTORATION OF THE GUST DAMPING VALVE (FUNCTIONAL TEST) 10000 FH 10000 FH See Note (8) 27-40-17-720-801-01 CMR FUNCTIONAL TEST OF THE HORIZONTAL STABILIZER RELAY BOX 5000 FH 5000 FH 27-60-00-720-802-01 CMR FUNCTIONAL TEST OF THE AIRBRAKE SYSTEM 10000 FH 10000 FH control panel microswitch test FALCON 50/50EX CHAPTER 5-40 Page 25/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 28: FUEL Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 28-21-13-790-801-01 CMR LEAK TEST OF THE FUEL SHUT-OFF VALVES - ENGINE 1 SHUT-OFF VALVE INTEGRATED IN BP 1 MANIFOLD (L14QD) 1530 FH 1530 FH 28-21-13-790-801-02 CMR LEAK TEST OF THE FUEL SHUT-OFF VALVES - ENGINE 2 SHUT-OFF VALVE INTEGRATED IN BP 2 MANIFOLD (M14QD) 1530 FH 1530 FH 28-21-13-790-801-03 CMR LEAK TEST OF THE FUEL SHUT-OFF VALVES - ENGINE 3 SHUT-OFF VALVE INTEGRATED IN BP 3 MANIFOLD (R14QD) 1530 FH 1530 FH 28-21-16-610-801-01 CMR SERVICING OF THE FUEL SHUT-OFF VALVES CONTROL CABLES - SERVICING OF THE CONTROL CABLES AND CHECKING OF THE SHUT-OFF VALVES OPENING/CLOSING 1000 FH or 13 M 1000 FH or 13 M FALCON 50/50EX CHAPTER 5-40 Page 26/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 31: INDICATING - RECORDING SYSTEMS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 31-60-00-710-801-01 CMR OPERATIONAL TEST OF THE ENGINE INDICATOR ELECTRONIC DISPLAY (EIED) 1530 FH 1530 FH A/C with TFE 731-40 ENGINES Test of EIED reconfiguration FALCON 50/50EX CHAPTER 5-40 Page 27/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 52: DOORS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 52-10-00-610-801-05 ALI SERVICING OF THE PASSENGER DOOR - CHECK OF DOOR LOCKED INDICATION 800 FH 800 FH 52-10-07-220-801-01 CMR DETAILED INSPECTION OF THE PASSENGER DOOR LOCKING HOOKS 5995 FC 2000 FC A/C without M141 52-10-07-220-801-01 CMR DETAILED INSPECTION OF THE PASSENGER DOOR LOCKING HOOKS 11435 FC 3750 FC A/C with M141 52-20-00-610-801-03 ALI SERVICING OF THE EMERGENCY EXIT DOOR - UNLOCKING TEST FROM INSIDE OF THE LH EMERGENCY EXIT DOOR 24 M 24 M EASA AD No 2006-0149 52-20-00-610-801-04 ALI SERVICING OF THE EMERGENCY EXIT DOOR - UNLOCKING TEST FROM INSIDE OF THE RH EMERGENCY EXIT DOOR 24 M 24 M EASA AD No 2006-0149 52-30-00-200-801-01 SSIP VISUAL INSPECTION OF THE BAGGAGE COMPARTMENT DOOR 26299 FC 3750 FC A/C with M142 (SB F50-177) 52-30-00-200-802-01 CMR INSPECTION OF THE BAGGAGE COMPARTMENT DOOR FORWARD SIDE FOLD 7034 FC 3028 FC [F50] A/C without M142 (SB F50-177) FALCON 50/50EX CHAPTER 5-40 Page 28/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 52: DOORS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 52-70-11-710-801-01 CMR OPERATIONAL TEST OF THE S-DUCT DOOR POSITION INDICATING MICROSWITCH 10000 FH 10000 FH FALCON 50/50EX CHAPTER 5-40 Page 29/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 53: FUSELAGE Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 53-00-00-200-802-01 SSIP VISUAL INSPECTION OF THE SKIN PANELS - FRAME 7 TO FRAME 31 20000 FC 3750 FC 53-00-00-250-802-01 SSIP EDDY-CURRENT INSPECTION OF THE FUSELAGE FRAMEWORK AROUND THE WINDOWS IN T2 AND T3 SECTIONS 31250 FC 7500 FC 53-04-01-220-801-01 SSIP DETAILED INSPECTION OF THE FLOOR PANEL OMEGAS AT FRAMES 18-19 27500 FC 7500 FC 53-04-05-250-801-01 SSIP EDDY-CURRENT INSPECTION OF FLOOR PANEL STIFFENERS BETWEEN FRAMES 31 AND 35 20000 FC 3750 FC 53-10-03-250-802-01 SSIP EDDY-CURRENT INSPECTION OF THE PASSENGER DOOR FRAME CORNERS 31250 FC 3750 FC 53-10-05-250-801-01 SSIP EDDY-CURRENT INSPECTION OF FRAME 12 AROUND PAX DOOR TELESCOPIC ROD FITTING 20000 FC 3750 FC 53-10-31-220-801-01 SSIP DETAILED INSPECTION OF COCKPIT UPPER SKIN JUNCTION WITH WINDSHIELD AND WINDOW FRAMES 20000 FC 1272 FC 53-10-39-220-801-01 SSIP DETAILED INSPECTION OF THE LOWER SECTION OF THE COCKPIT WINDSHIELD / WINDOW FRAMES 20000 FC 3750 FC 53-10-39-220-803-01 CMR DETAILED INSPECTION OF THE SCREWS ATTACHING THE WINDSHIELD FRAMES TO FRAME 0 6674 FC 3400 FC A/C without M281 FALCON 50/50EX CHAPTER 5-40 Page 30/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 53: FUSELAGE Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 53-10-39-220-803-01 CMR DETAILED INSPECTION OF THE SCREWS ATTACHING THE WINDSHIELD FRAMES TO FRAME 0 10525 FC 3750 FC A/C with M281 53-10-39-220-804-01 CMR DETAILED INSPECTION OF THE FRAME OF THE LH AND RH REAR COCKPIT WINDOWS - LH SIDE REAR WINDOW 12000 FC 2000 FC [F50] A/C (001-030 and 032-041) and with SB F50-198 53-10-39-220-804-01 CMR DETAILED INSPECTION OF THE FRAME OF THE LH AND RH REAR COCKPIT WINDOWS - LH SIDE REAR WINDOW 16192 FC 2854 FC [F50] A/C (001-030 and 032-041) and without SB F50-198 53-10-39-220-804-02 CMR DETAILED INSPECTION OF THE FRAME OF THE LH AND RH REAR COCKPIT WINDOWS - RH SIDE REAR WINDOW 12000 FC 2000 FC [F50] A/C (001-030 and 032-041) and with SB F50-198 53-10-39-220-804-02 CMR DETAILED INSPECTION OF THE FRAME OF THE LH AND RH REAR COCKPIT WINDOWS - RH SIDE REAR WINDOW 16192 FC 2854 FC [F50] A/C (001-030 and 032-041) and without SB F50-198 FALCON 50/50EX CHAPTER 5-40 Page 31/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 53: FUSELAGE Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 53-10-39-220-805-01 CMR DETAILED INSPECTION OF THE FRAME OF THE RH COCKPIT LATERAL WINDOW 10050 FC 2719 FC [F50] A/C without M322 53-10-39-250-802-01 SSIP EDDY-CURRENT INSPECTION OF THE COCKPIT WINDSHIELD / WINDOW FRAMES 20000 FC 3750 FC 53-10-39-270-802-01 SSIP ULTRASONIC CHECK OF THE VERTICAL POSTS OF THE COCKPIT WINDSHIELDS AND WINDOWS 20000 FC 3750 FC 53-10-41-220-801-01 CMR DETAILED INSPECTION OF THE ATTACHMENT FITTING OF THE NLG ACTUATOR 10000 LDG 7500 LDG 53-10-45-250-801-01 SSIP EDDY-CURRENT INSPECTION OF THE NLG BAY SKIN PANEL AND DOOR FRAME AT FRAME 7 31250 FC 3750 FC 53-30-00-220-802-01 CMR INSPECTION OF THE CENTER FLOOR ANGLE PIECE, RH SIDE BETWEEN FRAME 19 AND FRAME 26 16192 FC 4764 FC A/C without M313 53-30-00-220-802-01 SSIP INSPECTION OF THE CENTER FLOOR ANGLE PIECE, RH SIDE BETWEEN FRAME 19 AND FRAME 26 20000 FC 7500 FC A/C with M313 53-30-00-220-803-01 CMR DETAILED INSPECTION OF THE FLOOR PICK-UP ANGLE AT FRAME 27 AND OF THE FLOOR PANEL BETWEEN FRAME 26 AND FRAME 29 10000 FC 3750 FC 53-30-00-220-805-01 SSIP DETAILED INSPECTION OF FUSELAGE SKIN IN SPLICE AREA AT STRINGER 13 BETWEEN FRAME 13 AND 18 30000 FC 5000 FC FALCON 50/50EX CHAPTER 5-40 Page 32/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 53: FUSELAGE Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 53-30-00-250-801-01 SSIP EDDY-CURRENT INSPECTION OF THE EMERGENCY EXIT DOOR FRAME ROUNDED ANGLES 20000 FC 7500 FC 53-30-00-250-803-01 SSIP EDDY-CURRENT INSPECTION OF THE FINGER PLATE OF CIRCUMFERENTIAL SPLICE AT FRAMES 19 AND 26 20000 FC 7500 FC 53-30-01-220-801-01 CMR DETAILED INSPECTION OF THE FEEDER TANKS 74 M 74 M 53-30-01-790-801-01 CMR LEAK TEST OF THE FEEDER TANK 7 M 13 M A/C 222-286, 288, 290, 291 and without SB F50-328 53-40-00-220-802-01 CMR DETAILED INSPECTION OF THE FUSELAGE STRUCTURAL FUEL TANKS 74 M 74 M See Note (5) 53-40-07-220-801-01 SSIP DETAILED INSPECTION OF THE CENTERWING TANK LOWER PANELS 20000 FC 7500 FC 53-40-07-220-801-01 ALI DETAILED INSPECTION OF THE CENTERWING TANK LOWER PANELS Oct. 2012 74 M [F50] A/C 107 53-40-07-250-801-01 SSIP EDDY-CURRENT INSPECTION OF CENTERWING TANK LOWER PANEL SPLICE 20000 FC 7500 FC FALCON 50/50EX CHAPTER 5-40 Page 33/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 53: FUSELAGE Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 53-40-07-280-801-01 SSIP SPECIAL DETAILED INSPECTION (ULTRASONIC) OF CENTERWING TANK LOWER PANELS AND MAPPING OF REWORKED AREAS 20000 FC 7500 FC 53-50-34-220-801-01 SSIP DETAILED INSPECTION OF THE FRAME 34 UPPER AND LOWER SECTIONS 20000 FC 3750 FC 53-50-35-220-802-01 SSIP DETAILED INSPECTION OF THE FRAME 35 UPPER AND LOWER SECTIONS 20000 FC 3750 FC 53-50-35-250-801-01 SSIP EDDY-CURRENT INSPECTION OF THE FRAME 35 VERTICAL BEAMS 20000 FC 3750 FC 53-50-44-220-801-01 SSIP DETAILED INSPECTION OF THE FIN STUB FRONT SPAR 20000 FC 7500 FC FALCON 50/50EX CHAPTER 5-40 Page 34/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 54: NACELLES AND PYLONS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 54-50-00-220-802-01 SSIP DETAILED INSPECTION OF PYLON UPPER FLANGE RIBS AT FRAME 32 20000 FC 7500 FC FALCON 50/50EX CHAPTER 5-40 Page 35/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 55: STABILIZERS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 55-00-00-270-801-01 SSIP ULTRASONIC INSPECTION FOR STRESS CORROSION IN STABILIZER HINGES 20000 FC 3750 FC 55-10-00-220-803-01 SSIP DETAILED INSPECTION OF HORIZONTAL STABILIZER UPPER PANELS BETWEEN ROOT AND RIB 2 20000 FC 7500 FC 55-10-31-220-801-01 ALI DIMENSIONAL CHECK OF HORIZONTAL STABILIZER REAR HINGE BUSHINGS 3750 FC 3750 FC AD No 1997-370-020 R2 55-10-39-220-801-01 SSIP DETAILED INSPECTION OF HORIZONTAL STABILIZER ACTUATOR ATTACHMENT FITTINGS AND PINS 20000 FC 3750 FC 55-20-00-220-801-01 SSIP DETAILED INSPECTION OF THE ELEVATORS SKIN AND HINGE FITTINGS 20000 FC 3750 FC 55-40-00-220-801-01 SSIP DETAILED INSPECTION OF THE RUDDER SKIN AND HINGE FITTINGS 20000 FC 3750 FC FALCON 50/50EX CHAPTER 5-40 Page 36/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 57: WINGS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 57-10-00-290-801-01 CMR BORESCOPE INSPECTION OF THE WING TANKS 74 M 74 M 57-10-01-220-801-01 SSIP DETAILED INSPECTION OF LOWER WING PANELS 20000 FC 7500 FC 57-10-01-270-801-01 CMR ULTRASONIC INSPECTION OF THE WING LOWER SURFACE PANEL STIFFENERS BETWEEN RIBS 13 AND 17 14200 FC 5350 FC 57-10-01-280-801-01 SSIP SPECIAL DETAILED INSPECTION (ULTRASONIC) OF LOWER WING PANELS AND MAPPING OF REWORKED AREAS 20000 FC 7500 FC 57-10-14-200-801-01 SSIP INSPECTION OF WING FRONT SPAR FROM ROOT TO RIB 8 AND FROM RIB 9 TO RIB 17 20000 FC 7500 FC 57-10-14-200-802-01 SSIP INSPECTION OF WING FRONT SPAR FROM RIB 8 TO RIB 9 20000 FC 3750 FC 57-10-15-200-801-01 SSIP INSPECTION OF WING REAR SPAR 1 FROM ROOT TO RIB 3 20000 FC 3750 FC 57-10-15-200-802-01 SSIP INSPECTION OF WING REAR SPAR 2 FROM RIB 3 TO RIB 17 20000 FC 7500 FC 57-10-15-250-801-01 SSIP EDDY-CURRENT INSPECTION OF WING REAR SPAR RIB 8 SPLICE 20000 FC 3750 FC FALCON 50/50EX CHAPTER 5-40 Page 37/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 57: WINGS Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 57-45-25-250-801-01 SSIP EDDY CURRENT INSPECTION OF SLAT TRACKS 20000 FC 3750 FC See Note (6) 57-55-21-250-801-01 CMR EDDY-CURRENT INSPECTION OF THE FLAP TRACKS 2 AND 5 7900 FC 6800 FC See Note (7) 57-60-00-220-801-01 SSIP DETAILED INSPECTION OF THE AILERON SKIN AND HINGE FITTINGS 20000 FC 3750 FC FALCON 50/50EX CHAPTER 5-40 Page 38/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 71: POWER PLANT Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 71-20-01-220-801-01 SSIP DETAILED INSPECTION OF ENGINE 1 AND 3 FRONT AND REAR MOUNTS 20000 FC 3750 FC 71-20-11-220-801-01 SSIP DETAILED INSPECTION OF ENGINE 2 HOISTING PLATE AND MOUNTS 20000 FC 3750 FC FALCON 50/50EX CHAPTER 5-40 Page 39/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 73: ENGINE FUEL AND CONTROL Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 73-20-01-710-802-01 CMR OPERATIONAL TEST OF THE ENGINE 1 DIGITAL ELECTRONIC COMPUTER (DEEC 1) DUAL POWER SUPPLY 1530 FH 1530 FH A/C with TFE 731-40 ENGINES FALCON 50/50EX CHAPTER 5-40 Page 40/ 41 “DASSAULT AVIATION Proprietary Data” Effectivity : ALL – Reference DGT 113872 Rev. Date : July 2017 78: EXHAUST Scheduled maintenance task number Origin Title / Operation First Inspection Interval Remarks 78-31-00-250-802-01 CMR SPECIAL DETAILED INSPECTION (FLUORESCENT PENETRANT) OF THE THRUST REVERSER DOOR HINGE FITTINGS - LH THRUST-REVERSER DOOR (456DL) 28000 FC 1155 FC 78-31-00-250-802-02 CMR SPECIAL DETAILED INSPECTION (FLUORESCENT PENETRANT) OF THE THRUST REVERSER DOOR HINGE FITTINGS - RH THRUST-REVERSER DOOR (456DR) 28000 FC 1155 FC