FALCON 10 MAINTENANCE MANUAL

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. FALCON 10 MAINTENANCE MANUAL – Scientific research. – Cargo transport. – Flight training. – Others types of operation than normal passengers transport. 3 – Maintenance must have been performed in accordance with: – Either Maintenance Manual and Structural Repair Manual recommended by DASSAULT AVIATION, – or approved maintenance procedures providing the same level of airworthiness. 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...). C . IMPORTANT Compliance with these maintenance requirements are mandatory by all 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. In order to help operators planing maintenance program and to reduce grounding due to scheduled maintenance, these mandatory maintenance operations are also listed in section 5–10, or 5–20, with time limits corresponding to the aircraft inspections (A, B, C, etc.) or expressed as a number of flights. If an operator installs a secondhand main structural part (example: landing gear), he must note on the aircraft logbook the number of flights or landings accumulated by this part since manufacturing. He must ensure that, during operation, the service life limit of this part, indicated in chapter 5–40, will not be exceeded. D . UPDATING OF SECTION 5–40–00 When a new maintenance operation is added due to a revision of chapter 5 section 5–40–00, this operation must be performed when the time at which it is scheduled falls due, unless otherwise specified in the “MAXIMUM TIME LIMIT” column. When the aircraft inspection have two limits (i.e., 12 years or 7500 flights) the due time will be whichever is reached the first. EFFECTIVITY: ALL 5–40–00 Page 4 Revision No. 10 “DASSAULT AVIATION Proprietary Data” FALCON 10 MAINTENANCE MANUAL E. CORROSION PREVENTION and 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 number 51-00-02 RPI). In order to control the aircraft structure to corrosion level 1 or better on PSE’s, the operator must implement a CPCP into his respective maintenance program. As a guideline to help operator to implement a CPCP, Dassault Aviation provides a Chapter 5-15 (baseline) which compiles all the Dassault Aviation maintenance recommendations (inspections and their thresholds) required for a standard aircraft. All these chapter 5-15 operations are scheduled in Chapter 5-10 and 5-20 (If the operator’s maintenance program is compliant with chapter 5-10 and chapter 5-20 operations and intervals, it is compliant with the chapter 5-15 recommendations). In accordance with the airworthiness mandate for CPCP inclusion in the operator’s maintenance program, it is the operator’s responsibility to take into account “non-standard” features, such as STC’s, repairs, … etc., and add appropriate supplemental CPCP instructions for continued airworthiness to his specific maintenance program. 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. F. INSTRUCTIONS FOR CPCP Operators are mandated to report any finding affecting a P SE 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 ageing of the fleet and the possible need for escalation or alleviation of maintenance program. EFFECTIVITY: ALL “DASSAULT AVIATION Proprietary Data” 5 – 40 –00 Page 5 Revision No. 11 FALCON 10 MAINTENANCE MANUAL EFFECTIVITY: ALL 5–40–00 Page 6 Revision No. 12 “DASSAULT AVIATION Proprietary Data” G. NOTES The following notes are used in the following tables: NOTE (1): 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. NOTE (2): The life limit shown corresponds to landings on paved runways. When the aircraft are used on unpaved runways, after application of SB F10–82, each landing on an unpaved runway is counted as corresponding to 7 landings on a paved runway. FALCON 10 MAINTENANCE MANUAL 1. AIRFRAME COMPONENTS WITH LIMITED LIFE 5 –40 –00 Page 7 Revision No. 13 “DASSAULT AVIATION Proprietary Data” EFFECTIVITY: ALL COMPONENT IDENTIFICATION PART NUMBER LIFE LIMIT OBSERVATIONS 30 – ICE AND RAIN PROTECTION Slat anti-icing hose 32 – LANDING GEAR Nose gear comprising: – Leg comprising: – Shock strut – Support – Half fork – Steering control – Strut actuator LH main landing gear hinged assembly comprising: – Strut – Rocker beam RH main landing gear hinged assembly comprising: – Strut – Rocker beam FLEXFAB FAL1007 MESSIER–DOWTY 747719 747724–XX 747726–XX 747727 or D22042–XX 747728 747729–XX 747721–XX 760557–XX 760561–XX 760563 760559–XX 760562–XX 760563 350 hours 18800 landings (A/C without SB F10–238) 17500 landings (A/C with SB F10–238) 18800 landings (A/C without SB F10–238) 15000 landings (A/C with SB F10–238) 18800 landings (A/C without SB F10–238) 15000 landings (A/C with SB F10–238) See NOTE (1) See NOTE (1) and (2) See NOTE (1) and (2) See NOTE (1) and (2) – inboard – outboard 115S017A315 115S018A315 SPIRAGAINE Slat anti-icing hose FALCON 10 MAINTENANCE MANUAL COMPONENT IDENTIFICATION PART NUMBER LIFE LIMIT OBSERVATIONS 54 – NACELLES / PYLONS Engine rear attachment auxiliary fitting bolt introduced by SB F10–225 associated with DGAC Airworthiness Directive No. 81–225–15 (B) 3073361–1 1050 hours 500 hours For A/C without thrust reversers (**) For A/C with thrust reversers (**) (option 78–30–01) (**) See NOTE (1) 5 –40 –00 Page 8 Revision No. 12 “DASSAULT AVIATION Proprietary Data” EFFECTIVITY: ALL FALCON 10 MAINTENANCE MANUAL 2. MANDATORY MAINTENANCE OPERATIONS DESCRIPTION OF OPERATION ATA 100 NUMBER MAXIMUM TIME LIMIT THRESHOLD REPEAT INTERVAL   5 –40 –00 Page  Revision No. 12 “DASSAULT AVIATION Proprietary Data” EFFECTIVITY: ALL 21 – AIR CONDITIONING – Check of overpressure tightness • Main regulating valve P/N 2091PC010202 • Emergency regulating valve P/N 2093PC010202 – Check of overpressure relief valve vacuum supply lines 25 – EQUIPMENT AND FURNISHINGS – Visual inspection of buckle spring of Anjou Aéronautique safety belts, extensions and restraint systems type 343 and 343-1 using Anjou Aéronautique Service Bulletin No. 343-1-25-01 and No. 343-25-02 (*) Life limit of 60 months 32 – LANDING GEAR – Ultrasonic inspection of the nose landing gear actuator piston P/N 747721 * Component landings 34 – NAVIGATION – COLLINS ADC functional test (Aircraft with one of SB F10–300 to 320 included: RVSM) 52 – DOORS – Unlocking test from inside of window emergency exits (EASA Airworthiness Directive No. 2006-0147) 21–32-01 21–32–01 21–32–01 32–20–12 34–10–01 52–20–00 1900 landings* 1250 hours  1250 hours 7500 hours 6HH127(  18 months (*) see CN 2002-105 (AB) and CN 2002-104 (AB) 700 landings* 6HH127(   13 months 6HH127(   24 months FALCON 10 MAINTENANCE MANUAL DESCRIPTION OF OPERATION ATA 100 NUMBER MAXIMUM TIME LIMIT THRESHOLD REPEAT INTERVAL 57 – WINGS (*) $IWHU DSSOLFDWLRQ RI PDQGDWRU\ 6% F0± – 'HWDLOHG LQVSHFWLRQ RI WKH /+ DQG 5+ LQERDUG IODS HQG ULEV 5–55–0   5 –40 –00 Page 0 Revision No. 12 “DASSAULT AVIATION Proprietary Data” EFFECTIVITY: ALL 6540FC (*) 6540FC