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R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-55-11-410-057
B. Lifting of the Movable Fairing
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)
Lift the movable fairing, to align the link control rod (7) with the flap drive lever.
(2)
Apply a thin layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the interfaces of the sliding bush (5) and the bolt (11), but not the threads.
(3)
Install the bolt (11) the sliding bush (5), the washer (4) and the nut (3).
(4)
Torque the nut (3) to between 1.4 and 1.5 m.daN (10.32 and 11.06 lbf.ft).
(5)
Examine the related positions of the hole in the bolt (11) and the slot in the nut (3).
(6)
Torque the nut (3) until the next slot aligns with the hole to 2.0 m.daN (14.74 lbf.ft) maximum.
(7)
Safety the nut (3) with the new cotter pin (6).
(8)
Install the bonding strap (8) on the flap drive lever with the bolt (9), and the washer (10) (Ref. TASK 20-28-00-912-004).
(9)
Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-004) to clean the screws (2) and the interfaces of the cover (1).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-55-11Page 435 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(10)
Apply a thin layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) and SPECIAL MATERIALS (Material No. 05-064) to the interfaces of the cover (1).
(11)
Apply a thin layer of SPECIAL MATERIALS (Material No. 05-002) to the screws (2).
(12)
Install the cover (1) with the screws (2).
(13)
Apply a bead of SEALANTS (Material No. 09-016) in the groove between the cover (1) and the movable fairing.
R **ON A/C ALL
Subtask 57-55-11-865-071
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-55-11-860-063
D. Aircraft Configuration
(1) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap control-lever.
Subtask 57-55-11-710-054
E. Test
(1) Do an operational test of the flap system (Ref. TASK 27-54-00-710-001). Make sure that the movable fairing operates correctly.
5. Close-up
________
Subtask 57-55-11-942-055
A. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Remove the warning notice(s).
(4)
Remove the safety barriers.
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 57-55-11Page 437 1 1 May 01/04R 1 1 1CES 1
TASK 57-55-11-010-002
To Lower the Flap Track No. 3 & No. 4 Movable Fairings for Access
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 -------------------------------------------------------------------------------
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