A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(13)

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 (5) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to: - the nuts (16) - the bolts (17) - the flange of the universal joint (13) - the flange of the shaft (14). 
R R R  (6) Install the applicable steady bearing (15) (Ref. TASK 27-84-44-400-006): - FOR 6032CM install the steady bearing 6031CM - FOR 6082CM install the steady bearing 6081CM.
R R R  (7) 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  (8) 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 components - from the torque shaft, outboard of the applicable components.

 

 Subtask 27-84-45-865-103
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 27-84-45-710-061
 D. Test
 (1) The operational test of the slat power transmission system is contained in the installation of the steady bearing (Ref. TASK 27-84-44-400-004).
 5. Close-up
________ R (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-865-089
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 Subtask 27-84-45-410-058
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panel:

 -
FOR 6032CM
 install 522FB

 -
FOR 6082CM
 install 622FB.

 

 

 Subtask 27-84-45-865-090
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.

 Subtask 27-84-45-942-060
 D. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 27-84-45Page A405 1 1 Feb 01/00R 1 1 1CES 1

 TASK 27-84-45-000-012
R Removal of the Torque Shaft 6034CM(6084CM)
 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(s)
 No specific access platform 3.6 m (11 ft. 10 in.)
 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL 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
 27-84-45-991-001 Fig. 401
 27-84-45-991-003 Fig. 403

 

 3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-941-057
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice(s) in position to tell persons not to operate the slat controls.

 Subtask 27-84-45-860-074
 B. Aircraft Maintenance Configuration
 (1)
 Retract the slats fully (Ref. TASK 27-80-00-866-005).

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