(3)
Make sure that:
-you cannot see the spline engagement grooves on the shaft (83) at the movable joints
-the dimension A is a minimum of 6.5 mm (0.2559 in.) total end float at the movable joint.
Subtask 27-54-45-865-105
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-54-45-710-060
D. Operational Test of the Flap System
(1)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(2)
Retract the flaps fully (Ref. TASK 27-50-00-866-009).
(3)
Do an operational test of the flap system (Ref. TASK 27-54-00-710-001). Make sure that the operation of the torque shafts is satisfactory.
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5. Close-up
________
**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
Subtask 27-54-45-410-062
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the COLLAR-SAFETY, SPOILER from the piston rod of the servo-control.
(3)
Put the applicable spoiler back to the 'O' (Operation) position (Ref. TASK 27-60-00-866-002).
(4)
On the servo-control, make sure that the pointer on the hex-head is opposite the letter 'O' (Operation) on the housing.
(5)
Install the applicable access panel:
-
FOR 6224CM
install 575CB
-
FOR 6274CM
install 675CB
-
FOR 6230CM
install 575EB
-
FOR 6280CM
install 675EB.
Subtask 27-54-45-942-060
B. 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.
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TASK 27-54-45-000-012
Removal of the Torque Shaft 6228CM(6278CM)
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
______________________
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 sign No specific access platform 4.0 m (13 ft. 1 in.) 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27604000000 1 COLLAR-SAFETY, SPOILER 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
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B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-50-00-866-008 Extension of the Flaps on the Ground 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance
**ON A/C 001-049, 051-061, 101-103, 201-203,
27-54-45-991-001 Fig. 401 R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
27-54-45-991-001-A Fig. 401A
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵5(56)
