R **ON A/C 051-052, 062-099, 106-149, 151-199, 204-299, 401-499,
R TASK 27-54-00-820-001
R Adjustment of the LH (RH) Flap Drive System
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU_______
R START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:_______
R - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
R - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
R - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY.
R INCORRECT INSTALLATION CAN CAUSE DAMAGE.
R 1. Reason for the Job__________________
R Self Explanatory
R 2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R No specific circuit breaker(s) safety clip(s)
R No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
R No specific 1 SAFETY BARRIERS
R No specific 1 WARNING NOTICE
R No specific Torque Wrench : range 0.20 to 3.60 m.daN
R (2.00 to 26.00 lbf.ft)
R 460005835 1 GROUND LOCK SLEEVE
R 98D27504005000 1 PIN RIGGING-FLAPS (TRACK 1)
R 98D27504006000 1 PIN RIGGING FLAPS
R 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
R B. Consumable Materials
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R Material No. 04-018
R
R Material No. 04-022
R
R
R Material No. 11-026
R
R Material No. 15-007
R
R
R Material No. 19-003
R
GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00) USA MIL-PRF-81322 GRADE 2 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00) GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00) USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R C. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-41-00-861-002
R
R 24-41-00-862-002
R
R 27-50-00-000-003
R
R 27-50-00-400-003
R
R 27-50-00-866-008
R 27-50-00-866-009
R 27-51-44-820-001
R 27-54-00-710-001
R 31-32-00-860-006
R
R 32-00-00-481-002
R
R 32-12-00-010-001
R 32-12-00-410-001
R 57-51-37-000-002
R
Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) Extension of the Flaps on the Ground Retraction of the Flaps on the Ground Adjustment of the Interconnecting Strut Operational Test of the Flap System Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page Installation of the Safety Devices on the Landing Gear Doors Open the Main Gear Doors for Access Close the Main Gear Doors after Access Removal of the Access Panels 573AB(673AB), 573BB(673BB), 573CB(673CB) -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 57-51-37-000-004 R R R 57-51-37-400-002 R R 57-51-37-400-004 R R R 27-50-00-869-006 R R 27-51-00-820-001 R R 27-54-00-991-038 R 27-54-00-991-039 R 27-54-00-991-040
R 3. Job Set-up
__________
R Subtask 27-54-00-860-077 Removal of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB) Installation of the Access Panels 573AB(673AB), 573BB(673BB), 573CB(673CB) Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB) Reset of the Wing Tip Brake (WTB) of the Flap System on the Ground (for corrective action) Manual Adjustment of the Position Pick-Off Units (for corrective action) Fig. 501 Fig. 502 Fig. 503
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵4(150)
