(Ref. Fig. 401/TASK 27-54-45-991-001) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 27-54-45-991-001-A)R **ON A/C ALL

 Subtask 27-54-45-941-051
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice in position to tell persons not to operate the landing-gear doors.

 (3)
 Put a warning notice in position to tell persons not to operate the flap/slat controls.

 Subtask 27-54-45-860-051
 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 (1)
 Extend the flaps fully (Ref. TASK 27-50-00-866-008).

 (2)
 Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever on panel 114VU.

 Subtask 27-54-45-865-051
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 Subtask 27-54-45-010-051
 D. Get Access
 (1)
 Open the main gear doors (Ref. TASK 32-12-00-010-001).

 (2)
 Install the GROUND LOCK SLEEVE on the applicable main gear door actuator.

 (3)
 Put the access platform in the applicable position.

 4. Procedure
_________
 **ON A/C 001-049, 051-061, 101-103, 201-203,

 (Ref. Fig. 401/TASK 27-54-45-991-001) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 27-54-45-991-001-A)
 **ON A/C ALL

 (Ref. Fig. 402/TASK 27-54-45-991-002)
 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING

_______
 EDGE:

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 Subtask 27-54-45-020-051
 A. Removal of the Torque Shaft 6204CM(6254CM)
 (1)
 Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) on a flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the component to be removed.

 (2)
 Remove the nuts (4) and (8), the bolts (3) and (9) and the torque shaft (2). If applicable, remove the spacers.

 NOTE : Spacers between the universal joint (1), the torque shaft (2)
____ and the universal joint (7), adjust the length of the transmission. It is possible that there are none or more than one installed.
 (3)
 Remove the universal joint (1).

 (4)
 Remove the retaining ring (5), the pin (6) and the universal joint (7).

 TASK 27-54-45-400-002
 Installation of the Torque Shaft 6204CM(6254CM)
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING_______ NOTICES ARE IN POSITION.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR. 
R R R R R  CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:_______ - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific No specific No specific No specific  safety barrierswarning noticeaccess platform 2.5 m (8 ft. 2 in.)Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft)

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(22)