-
there are no cracks
-
there is no corrosion
-the paint finish is in the correct condition.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575300) for the
____
correct repair procedure.
Outboard Double-Slotted Flap - Inspection
Figure 640/TASK 57-53-00-991-045
1EFF : 301-399, 1 57-53-00 Page B671
1 1 Nov 01/04
1 1
1CES 1
5. Close-up
________
Subtask 57-53-00-865-142
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-53-00-860-132
B. Aircraft Maintenance Configuration
(1) Fully retract the flaps (Ref. TASK 27-50-00-866-009). Subtask 57-53-00-942-095
C. Removal of Equipment
(1)
Remove the warning notice(s).
(2)
Remove the access platform(s).
(3)
Remove the safety barriers.
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
**ON A/C ALL
TASK 57-53-00-200-015
Inspection of Outboard Flap, Bottom Surface, Drain Holes and Inspection Holes
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
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.
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 notices
R No specific 5.0mm (0.2 in.) dia. non-metallic probe No specific access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-061A D DAN 220
ALUMINIUM FOIL ADHESIVE TAPE (Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground
27-50-00-866-009 Retraction of the Flaps on the Ground
**ON A/C 001-049, 051-056,
57-53-00-991-046-B Fig. 641
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
57-53-00-991-046-C Fig. 641A
**ON A/C 301-399,
57-53-00-991-046-A Fig. 641BR **ON A/C ALL
3. Job Set-up
__________
Subtask 57-53-00-941-100
A. Safety Precautions
(1) Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2) Put the safety barriers in position.
Subtask 57-53-00-860-133
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
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