Details of the Aileron Hinge Assembly Figure 604/TASK 57-51-00-991-003
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5. Close-up
________ Subtask 57-51-00-410-052
A. Close Access
(1) Install the access panels:
-for the left wing, install 575AT, 575JB, 575KB, 575LB, 575MB
-for the right wing, install 675AT, 675JB, 675KB, 675LB, 675MB. Subtask 57-51-00-865-053
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 57-51-00-942-052
C. Removal of Equipment
(1)
Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the safety barriers.
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 57-51-00-220-002
Detailed Visual Inspection of Outer Wing Trailing Edge Aileron Pins 1 thru 5
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
__________________
Refer to the MPD TASK: 575120-01
NOTE : This Task is an alternative to the Task 575100-220-013.
____
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 No specific access platform 3 m (9 ft. 10 in.) 98D27104004000 5 SLAVE PIN - AILERON 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
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B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 -------------------------------------------------------------------------------
27-14-41-000-001 Removal of the Aileron 27-14-41-400-001 Installation of the Aileron ASRM 575100 (for corrective action) 57-51-00-991-004 Fig. 605
3. Job Set-up
__________
Subtask 57-51-00-941-052
A. Safety Precautions
(1)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(2)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(3)
Put the safety barriers in position.
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Subtask 57-51-00-865-054
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 57-51-00-010-052
C. Get Access
(1)
Put the access platform in position below the applicable aileron, zone 575(675).
(2) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM WINGS 机翼3(86)
