Subtask 27-84-44-865-057
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure
_________
Subtask 27-84-44-420-067
A. Preparation for Installation
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(1)
Use a MISCELLANEOUS (Material No. 19-003) maede moist with CLEANING AGENTS (Material No. 11-004) to clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Apply a layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to:
-
the mating faces of the steady bearing (42) and the nose rib (39)
-
the shanks of the bolts (38).
Subtask 27-84-44-420-069
B. Installation of the Steady Bearing FIN 6031CM (6081CM)
(1)
Attach the steady bearing (42) to the torque shaft (41) and the nose rib (39) with the bolts (38) and the nuts (40).
(2)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the bolts (38)
-
the nuts (40)
-
the flange of the steady bearing (42).
(3)
Install the applicable torque shaft (43) (Ref. TASK 27-84-45-400-008): FOR 6031CM install the torque shaft FIN 6030CM FOR 6081CM install the torque shaft FIN 6080CM.
Subtask 27-84-44-865-059
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-44-710-055
D. Test
(1) Do an operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001).
5. Close-up
________
Subtask 27-84-44-410-051
A. 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 6031CM
install 522EB
-
FOR 6081CM
install 622EB.
Subtask 27-84-44-942-055
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.
TORQUE SHAFT ASSY - TRANSMISSION (6002CM,6004CM,6006CM,6008CM,6010CM,6012CM,
____________________________________________________________________________ 6014CM,6016CM,6018CM,6020CM,6022CM,6024CM,6026CM...) - REMOVAL/INSTALLATION
___________________________________________________________________________
TASK 27-84-45-000-001
Removal of the Torque Shaft 6002CM(6004CM)
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
__________________
R R 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 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
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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(126)
