57-51-37-000-004
FOR FIN 14CE1 57-51-37-400-004
FOR FIN 14CE2 57-51-37-400-004
FOR FIN 14CE3 57-51-37-400-004
FOR FIN 14CE4 57-51-37-400-004
3. Job set up
__________ Subtask 27-92-19-941-052
A. Safety Precautions
Removal of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in the cockpit to tell persons not to pressurize the Yellow and Green hydraulic systems.
(3)
Make sure that the warning notice is in position in the cockpit to tell persons not to operate the flight controls.
Subtask 27-92-19-860-050
B. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is below the applicable access panel.
(2)
Make sure that the applicable access panel has been removed (Ref. TASK 57-51-37-000-004):
-
FOR 14CE1
remove 575EB
-
FOR 14CE2
remove 675EB
-
FOR 14CE3
remove 575GB
-
FOR 14CE4
remove 675GB.
(3)
Make sure that the Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).
(4)
Make sure that the applicable hydraulic reservoir has been depressurized (Ref. TASK 29-14-00-614-001).
(5)
Make sure that the applicable accumulator has been depressurized (Ref. TASK 27-64-46-000-001).
(6)
Make sure that the flaps have been extended (Ref. TASK 27-50-00-866-008).
(7)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the flap/slat control lever.
(8)
Make sure that the applicable spoiler has been extended (Ref. TASK 27-60-00-866-002).
(9)
Make sure that the COLLAR-SAFETY, SPOILER (98D27604000000) is on the piston rod of the servo-control.
Subtask 27-92-19-865-051
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
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.
Subtask 27-92-19-420-051
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.
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(37)
