WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
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YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
1. Reason for the Job
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R This task gives the information for the removal of the Power Plant.
R The power plant can be removed in particular configuration. It is allowed to
R remove the power plant with or without the air intake cowl installed.
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E E May 01/04 E E ECES E 2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
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No specific adhesive tape No specific blanking plugs No specific circuit breaker(s) safety clip(s) No specific protective covers No specific soft nose pliers No specific warning notice No specific access platform 1 m (3 ft. 3 in.) No specific container (1 USgal) 4 l (1.0566 USgal) No specific Torque Wrench : range 36.00 to 220.00 lbf.in
(0.40 to 2.60 m.daN) No specific Torque Wrench : range 2.00 to 20.00 m.daN
(15.00 to 150.00 lbf.ft) S487ETT2 1 ENGINE TROLLEY S587-2BH0 1 BRACE - HOLD OPEN COWLS S686CR56-5 1 ENGINE CRADLE TMHBS10-10-00 1 BRACE - HOLD OPEN COWLS TMHEC28-00-00 1 ENGINE CRADLE TMHET06-00-00 1 ENGINE TROLLEY 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER 98D71203500000 1 BOOTSTRAP SYSTEM 98D71203501000 1 BOOTSTRAP SYSTEM
B. Consumable Materials
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Material No. CP8001 USA MIL AMS 5687 lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00) Material No. CP8006 * safety cable 0.032 in. (0.8 mm) dia. (Ref. 70-30-00)
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C. Referenced Information
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05-57-00-200-001 Aircraft Stability
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
31-36-00-740-007 Printout of the Engine Hours and Cycles
71-13-00-010-040 Opening of the Fan Cowl Doors
78-30-00-481-041 Make the Thrust Reverser Unserviceable for
Maintenance
78-36-00-010-040 Opening of the Thrust Reverser Doors
SIL 54-031
71-00-00-991-910 Fig. 401
71-00-00-991-911 Fig. 402
71-00-00-991-912 Fig. 403
R **ON A/C 001-049, 051-099, 101-149, 151-152, 154-199, 201-299, 301-399, R 401-499,
71-00-00-991-913 Fig. 404
**ON A/C 153-153,
71-00-00-991-913-A Fig. 404A
**ON A/C ALL
71-00-00-991-914 Fig. 405
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
71-00-00-991-915 Fig. 406
R **ON A/C 151-199, 401-499,
71-00-00-991-915-A Fig. 406A
**ON A/C 153-153,
71-00-00-991-929 Fig. 407
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**ON A/C ALL
71-00-00-991-916 Fig. 408 71-00-00-991-917 Fig. 409 71-00-00-991-918 Fig. 410
3. Job Set-up
__________ Subtask 71-00-00-740-052
A. Do a print-out of the engine hours and cycles and keep the print with the engine for follow-up (Ref. TASK 31-36-00-740-007).
Subtask 71-00-00-941-066
B. Safety Precautions
(1) Make sure that aircraft is stable (Ref. TASK 05-57-00-200-001). NOTE : If the aircraft is on jacks, make sure that it is leveled
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before you remove the engine.
(2) On the center pedestal, on the ENG panel 115VU:
(a) Put a warning notice to tell persons not to start the engine.
(3) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(4) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM 動力裝置 POWER PLANT 1(15)
