R (c) Carefully install the hydraulic motor (5) on the transfer tubes
R (8).
R (d) Attach the hydraulic motor (5) to the POB (9) with the washers
R (2) and the bolts (3).
R (e) TORQUE the bolts (3) to between 0.87 and 0.96 m.daN (76.99 and
R 84.95 lbf.in).
R (4) Do a bonding test between the main bonding point of the power control
R unit and the:
R - POB flange
R - hydraulic motor flange
R - valve block assembly flange.
R The resistance must not be more than 20 milliohms.
R (5) Connect the hydraulic lines.
R (a) Remove the blanking caps from the line end (4).
R (b) Make sure that the hydraulic line end-fittings are serviceable.
R (c) Apply the HYDRAULIC FLUIDS (Material No. 02-003) to the threads
R of the line end-fittings.
R (d) Connect the case drain line (4) to the hydraulic motor (5).
R (e) TORQUE the union nut of the case drain line (4) to between 1.5
R and 1.7 m.daN (11.06 and 12.53 lbf.ft).
R Subtask 27-54-54-860-056
R C. Preparation for the Test
R (1) Remove the PIN RIGGING-FLAPS from the left and right flap-track
R positions 1.
R (2) Pressurize the reservoirs of the Green and Yellow hydraulic systems
R (Ref. TASK 29-14-00-614-002).
R (3) Pressurize the Green and the Yellow hydraulic systems (Ref. TASK 29-
R 10-00-863-001) (Ref. TASK 29-10-00-863-002).
R (4) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (Ref. TASK 27-00-
R 00-080-002) from the slat/flap control lever.
R (5) Remove the warning notice(s).
R (6) Make sure that the work area is clean and clear of tool(s) and other
R items.
R Subtask 27-54-54-865-055
R D. Remove the safety clip(s) and the tag(s) and close this(these) circuit
R breaker(s):
R 6CV, 8CV
R Subtask 27-54-54-710-051
R E. Test
R (1) Do the operational test of the flap system (Ref. TASK 27-54-00-710-
R 001).
R 5. Close-up________
R Subtask 27-54-54-860-057
R A. Put the aircraft back to the serviceable condition.
R (1) Make sure that the level of fluid in the relevant hydraulic reservoir
R is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or
R (Ref. TASK 12-12-29-611-002).
R (2) Remove the container from below the hydraulic motor (5).
R (3) Remove the access platform(s).
R Subtask 27-54-54-410-051
R B. Close the main doors of the main gear (Ref. TASK 32-12-00-410-001).
LEVER ASSY - FLAP ACTUATOR - REMOVAL/INSTALLATION
_________________________________________________
TASK 27-54-55-000-001
Removal of the Flap-Actuator Lever Assembly - Tracks 1 and 2
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
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
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(163)
