R (4) Do one of the steps that follow:
R R CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______ GREASE AND ASSEMBLY PASTE DO NOT MIX.
R R R R (a) Apply a thin layer of COMMON GREASE (Material No. 04-022) to the torque shaft splines. - or
R R R (b) Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines.
Subtask 27-84-45-420-067
R B. Installation of the Torque Shaft 6006CM(6056CM)
(1) Install the universal joint (8).
(2) Install the shaft (9) and attach it with the bolts (11) and the nuts (10).
(3) TORQUE the nuts (10) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
(4) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to: - the nuts (10) - the bolts (11) - the flange of the universal joint (8) - the flanges of the shaft (9).
R (5) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003): - from the torque shaft, inboard of the applicable component - from the torque shaft, outboard of the applicable component.
Subtask 27-84-45-210-054
R C. Dimensional/Visual Checks (Ref. Fig. 402/TASK 27-84-45-991-002)
R R R R R (1) Make sure that: - you cannot see the spline engagement groove at the movable joint - the dimension A is a minimum of 6.5 mm (0.2559 in.) at the movable joint.
R Subtask 27-84-45-865-062
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-45-710-051
E. Test
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Do an operational test of the slat power-transmission system R (Ref. TASK 27-84-00-710-001). Make sure that the rotation of the torque shafts does not cause damage.
5. Close-up
________
Subtask 27-84-45-410-051
A. Close Access
(1) Install the applicable access panels 191BB, 192FB (Ref. TASK 53-35-13-400-002).
(2) Close the MLG doors (Ref. TASK 32-12-00-410-001).
Subtask 27-84-45-942-051
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
TASK 27-84-45-000-003
R Removal of the Torque Shaft 6008CM(6058CM)
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-80-00-866-005 Retracting the Slats on the Ground 27-84-44-000-001 Removal of the Steady Bearing FIN 6007CM(6057CM) 53-35-13-000-002 Removal of the Quick-Release Access Panels from the
Belly Fairing Structure
27-84-45-991-001 Fig. 401
27-84-45-991-002 Fig. 402
3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-941-073
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position to tell persons not to operate the slat controls.
Subtask 27-84-45-860-066
B. Aircraft Maintenance Configuration
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(131)
