Subtask 27-54-44-860-051
C. 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)
Retract the flaps fully (Ref. TASK 27-50-00-866-009).
(2)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever on panel 114VU.
Subtask 27-54-44-010-050
D. Get Access
R (1) Put the access platform in position below the applicable torque R shaft.
(2) Remove the applicable torque shaft (11) (Ref. TASK 27-54-45-000-008), (Ref. TASK 27-54-45-000-009), (Ref. TASK 27-54-45-000-010), (Ref. TASK 27-54-45-000-012), (Ref. TASK 27-54-45-000-013):
-
FOR 6215CM
remove the torque shaft 6216CM
-
FOR 6225CM
remove the torque shaft 6226CM
-
FOR 6265CM
remove the torque shaft 6266CM
-
FOR 6275CM
remove the torque shaft 6276CM
-
FOR 6219CM
remove the torque shaft 6218CM
-
FOR 6269CM
remove the torque shaft 6268CM
-
FOR 6223CM
remove the torque shaft 6222CM
-
FOR 6273CM
remove the torque shaft 6272CM
-
FOR 6229CM
remove the torque shaft 6228CM
-
FOR 6279CM
remove the torque shaft 6278CM
-
FOR 6231CM
remove the torque shaft 6232CM
-
FOR 6281CM
remove the torque shaft 6282CM.
R (3) For steady bearings FIN 6231CM (6281CM), remove the applicable access R panel (Ref. TASK 57-51-37-000-004):
-
FOR 6231CM
remove 575EB
-
FOR 6281CM
remove 675EB.
(4) Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is on the applicable torque shaft (Ref. TASK 27-50-00-400-003).
4. Procedure
_________
(Ref. Fig. 401/TASK 27-54-44-991-001)
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 27-54-44-020-051
A. Removal of the Steady Bearing Assemblies
(1) Remove the nuts (13), the bolts (12) and the steady bearing (16).
TASK 27-54-44-400-002
Installation of the Steady Bearings FIN 6215CM(6265CM)/6219CM(6269CM)/6223CM (6273CM)/6225CM(6275CM)/6229CM(6279CM)/6231CM(6281CM) 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.
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 safety barriers
No specific warning notice
No specific access platform 2.5 m (8 ft. 2 in.)
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(15)
