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R Subtask 57-51-37-020-052
R A. Removal of the Access Panels
R (1) For the access panel 575AB(675AB) (4):
R (a) Release the ten camloc fasteners (3) then remove the access panel
R (4).
R (2) For the access panel 575BB(675BB) (2):
R (a) Release the eleven camloc fasteners (1) then remove the access
R panel (2).
R (3) For the access panel 575CB(675CB) (12):
R (a) Release the nine camloc fasteners (11) then remove the access
R panel (12).
R (4) For the access panel 575DB(675DB) (10):
R (a) Release the twelve camloc fasteners (9) then remove the access
R panel (10).
R (5) For the access panel 575EB(675EB) (8):
R (a) Release the eleven camloc fasteners (7) then remove the access
R panel (8).
R (6) For the access panel 575FB(675FB) (6):
R (a) Release the nine camloc fasteners (5) then remove the access
R panel (6).
R (7) For the access panel 575GB(675GB) (16):
R (a) Release the six camloc fasteners (15) then remove the access
R panel (16).
R (8) For the access panel 575HB(675HB) (14):
R (a) Release the nine camloc fasteners (13) then remove the access
R panel (14).
TASK 57-51-37-400-004
Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
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 safety barriers No specific warning notices No specific access platform 4.0 m (13 ft. 1 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (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)
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C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-080-002 Removal of the Flap/Slat Control-Lever Locking Tool
(98D27803000000) R 57-51-37-960-001 Replacement of the Lower Trailing Edge Access Panel R Seals
57-51-37-991-005 Fig. 403
3. Job Set-up
__________
Subtask 57-51-37-941-057
A. Safety Precautions
(1)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed on the flap/slat control lever.
(2)
Make sure that the warning notices are in position in the cockpit to tell persons not to operate the flaps or slats.
(3)
Make sure that the safety barriers are in position.
Subtask 57-51-37-860-052
B. Aircraft Maintenance Configuration
(1) Make sure that the access platform is in position below the applicable zone 575(675).
4. Procedure
_________
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.
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