(3)
Make sure that the warning notice is in position to tell persons not to operate the landing gear doors.
(4)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the slat/flap control lever.
Subtask 27-84-44-865-050
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
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PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-84-44-860-050
C. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position below the applicable torque shaft.
(2)
Make sure that the main gear doors are open (Ref. TASK 32-12-00-010-001).
(3)
Make sure that the GROUND LOCK SLEEVE is on the applicable main gear door actuator.
(4)
Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. TASK 27-50-00-400-003) as follows: - on the torque shaft inboard of the removed component - on the torque shaft outboard of the removed component.
4. Procedure
_________
Subtask 27-84-44-420-056
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) 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 (5) and the steady bearing bracket (2)
-
the shanks of the bolts (3).
Subtask 27-84-44-420-057
B. Installation of the Steady Bearing FIN 6007CM (6057CM)
(1)
Attach the steady bearing (5) to the torque shaft (4) and the steady bearing bracket (2) with the bolts (3) and the nuts (1).
(2)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the nuts (1)
-
the bolts (3)
-
the flange of the steady bearing (5).
(3)
Install the applicable torque shaft (6) (Ref. TASK 27-84-45-400-003): FOR 6007CM install the torque shaft FIN 6006CM FOR 6057CM install the torque shaft FIN 6056CM.
Subtask 27-84-44-710-050
C. Test
(1) Do an operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001).
5. Close-up
________
Subtask 27-84-44-865-063
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 6CV, 7CV.
Subtask 27-84-44-410-052
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
Subtask 27-84-44-942-050
C. 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.
TASK 27-84-44-000-002
Removal of the Steady Bearings FIN 6017CM(6067CM)/6019CM(6069CM)
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
__________________
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵7(115)
