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Basic Insp

Basic inspection of falcon 2000 ex easy

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Rudro Kumar
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382 views17 pages

Basic Insp

Basic inspection of falcon 2000 ex easy

Uploaded by

Rudro Kumar
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
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DASSAULT FALCON FALCON 2000EX EASY AIRCRAFT MAINTENANCE MANUAL TASK 05-60-00-200-801 BASIC INSPECTION 4, OVERVIEW OF THE JOB Operation codes: + 06-60-00-200-801-01 Basic inspection + 06-60-00-200-801-03 Ground servicing checks NOTE: Operations marked with an", corresponding to operation code -03, are daily servicing checks, ‘They are also defined in the Ground Servicing Manual under Daily Servicing and may be signed off separately. Locistics A. References Reference Designation + 05-60-00-620-803 ‘SPECIFIC MAINTENANCE FOR A/C OPERATING IN COLD WEATHER CHECK AFTER AN INCIDENT ON THE HYDRAULIC SYSTEM ACCEPTANCE CRITERIA FOR HYDRAULIC LEAKS ENERGIZATION / DE-ENERGIZATION OF THE AIRCRAFT SYSTEMS. CHARGING OF THE AIRBRAKE PRESSURE HOLDING VALVE ACCUMULATOR ACCEPTANCE CRITERIA FOR FUEL LEAKS CHARGING OF THE HYDRAULIC SYSTEM ACCUMULATORS. CHECK OF THE MINIMUM HEIGHT OF MLG AND NLG SHOCK ABSORBERS MANUAL OPENING / CLOSING OF THE MLG DOORS REMOVAL / INSTALLATION OF THE BRAKES REMOVAL / INSTALLATION OF THE WING NAVIGATION LIGHTS (WINGLET LED MODULE) (A/C with winglets) REFILLING OF THE OXYGEN CYLINDER ‘SERVICING OF THE WATER SYSTEM (A/C 238 to 600) USE OF THE CENTRAL MAINTENANCE COMPUTER (CMC) DETAILED INSPECTION OF THE STATIC PRESSURE PROBES AND OF THE FUSELAGE SKIN IN THE PROBE AREAS OIL LEVEL CHECK OF THE ENGINE PNEUMATIC STARTER Designation Quantity FUSELAGE WATER DRAINING TOOL lop + T0.20-310 CHRONOMETER (A/C with M3317 (RIPS) and without SB F2000EX-242) ¢. Energy + ELECTRICAL * HYDRAULIC D. Access Efectinty. ALL Rev. Date: DEC 14/2016 05-60-00-200-801 page 1/17 “DASSAULT AVIATION Proprietary Data” DASSAULT FALCON FALCON 2000EX EASY AIRCRAFT MAINTENANCE MANUAL Reference Designation AFT SERVICING COMPARTMENT DOOR PASSENGER DOOR WATER SERVICING DOOR (A/C 238 to 600) ENGINE 1 LOWER COWLING ENGINE 2 LOWER COWLING RH MLG MAIN DOOR E, Miscellaneous + LINT-FREE CLOTH (LOCAL PROCUREMENT) +"DO NOT OPEN’ CAUTION FLAG (LOCAL PROCUREMENT) (A/C 238 to 600) + "GALLEY WATER SYSTEM INOPERATIVE PENDING MAINTENANCE OPERATIONS® INFORMATION FLAG (LOCAL PROCUREMENT) (A/C 238 to 600) + ANTI-DAZZLE GOGGLES (LOCAL PROCUREMENT) (A/C with winglets) PRELIMINARY STEPS A. Remove the following protective covers: + alr data probe covers, + temperature probe blanking covers, + engine and APU air intake and exhaust blanking covers, + AOA sensor protective covers, B. Inthe forward servicing compartment, check that batteries (150PC)/(50PC) are connected ©. Connect the electrical Ground Power Unit (GPU) (if to be used) (Refer to TASK 24.00-00-860-801), COCKPIT (1-FIG. 4 A. Energize the aircraft systems: + with the GPU (Refer to TASK. or + with the APU (refer to the Airplane Flight Manual). 160-801), B. (AIC with M3317 (RIPS) and without SB F2000EX-242) Test of the RIPS. + Charging of the RIPS battery + Make sure that the "VOICE RECORDER" circuit breaker (501FZ) is engaged. ‘+ Walt 15 min for the RIPS battery to charged. NOTE: If the ambient temperature is lower than 0°C (32°F), wait 15 min more. + Disengage the "VOICE RECORDER’ circuit breaker (501FZ) and, using a chronometer (TO-20-310), check that the amber "CVR 1 FAIL" CAS message is displayed after 10 min (# 30 s). + Ifthe amber "CVR 4 FAIL" CAS message is displayed before 10 min (+ 30 s), the RIPS is falled C. Make sure that the following CAS messages are consistent with the aircraft configuration Effectiviy: ALL Rev. Date: DEC 14/2016 05-60-00-200-801 page 2/17 “DASSAULT AVIATION Proprietary Data” DASSAULT FALCON FALCON 2000EX EASY AIRCRAFT MAINTENANCE MANUAL E. NOTE: Ifthe displayed CAS message is not listed below, analyze or troubleshoot, if necessary, per the Aircraft Maintenance Manual (AMM) or the Engine Maintenance Manual (EMM). amber "AIL ZERO" (displayed if roll emergency tim actuator (95GR) is not in the neutral position), + amber "BRAKE ACCU" (displayed if there is no pressure in park brake accumulator (140GG)), + amber "BUS LH ISOL" (displayed if LH bus is set to iso, + amber "BUS RH ISOL" (displayed if RH bus is set to isol), + white "BUS RH TIED" (displayed if "ESS BUS/MD BUS" tie selector (515PC) is set to the tied position, "BUS TIED"), + (AIC with front lavatory) red "DOOR FWD TOILET (displayed ifthe forward toilet servicing door (124AB) is open), + white "DOOR BAG" (displayed if baggage compartment door (BAG) is open), + white "DOOR PAX" (displayed if passenger door (PAX) is open), + white "FLAP OVRD" (displayed if the EGPWS flag override is selected) + white "FUEL LEVEL 1” (displayed if fuel level in LH tank group is less than 1000 lbs), + white "FUEL LEVEL 2" (displayed if fuel level in RH tank group is less than 1000 Ibs), + amber "FUELING" (displayed if fueling panel door (186DR) or fueling connector access door (186CR) is open), + white "GPU ON: BUS TIED" (displayed if the GPU is connected and energized), + white "IRS 1 ALIGNING’ (displayed if IRS 1 aligning on ground and excessive aircraft movement is detected), + white "IRS 2 ALIGNING" detected), + white "IRS 3 ALIGNING’ (displayed i IRS 3 aligning on ground and excessive aircraft movement is detected), + white "IRS 1 POS ENTRY" (displayed if RS 1 alignment is complete but no valid initial position has been received) + white "IRS 2 POS ENTRY" (displayed if IRS 2 alignment is complete but no valid intial position has been received), + white "IRS 3 POS ENTRY" (displayed if RS 3 alignment is complete but no valid initial position has been received) + amber "LOW FUEL 1" (displayed if fuel level in LH tank group is less than 250 lbs), + amber "LOW FUEL 2" (displayed if fuel level in RH tank group is ess than 250 Ibs), + white "PARK BRAKE ON’ (displayed if park brake is set to the ON position), + white "STAB EMERGENCY’ (displayed if horizontal stabilizer emergency is selected), + amber "STBY PUMP ON Cit" (displayed if stand-by pump selector valve is set to GROUND TEST position), + white "TERR INHIBIT" (displayed if terrain inhibit has been selected), + amber "UNABLE FMS/GPS MONITOR’, + amber "CVR 1 FAIL" (displayed if CVR is not energized). (displayed if IRS 2 aligning on ground and excessive aircraft movement is Go to the "ACTIVE MAINTENANCE MESSAGES" page on the lower MFD (3FQ) (Refer to TASK 45-10-00-910-802), and check that no maintenance messages are displayed. + If any maintenance messages are displayed, troubleshoot them. * Check the APU oil level on the "TEST" page: Effectiviy: ALL Rev. Date: DEC 14/2016 05-60-00-200-801 page 3/17 “DASSAULT AVIATION Proprietary Data”

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