(2)
One at a time, remove the five hinge pins from the RH aileron and replace them with the SLAVE PIN - AILERON (98D27104004000) (Ref. TASK 27-14-41-000-001).
R Aileron Hinge Pins Figure 623/TASK 57-51-00-991-023
1EFF : 1 1 1CES ALL 1 111 57-51-00 Page A640 Nov 01/04
Subtask 57-51-00-110-080
B. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the hinge pins.
Subtask 57-51-00-240-055
C. Inspection
(1) Do a magnetic particle inspection of all the aileron hinge pins (Ref. NTM 57-51-20 PART 7).
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) for the
____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.
Subtask 57-51-00-420-076
D. Installation of the Aileron Hinge Pins
(1) One at a time, remove the five slave bolts from each aileron and replace them with the hinge pins (Ref. TASK 27-14-41-400-001).
5. Close-up
________ Subtask 57-51-00-410-077
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
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 57-51-00-865-094
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 16CE1, 16CE2, 6CV, 15CE1, 15CE2, 8CV.
1EFF : ALL 1 57-51-00Page A641 1 1 Nov 01/04R 1 1 1CES 1
Subtask 57-51-00-942-075
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.
1EFF : ALL 1 57-51-00Page A642 1 1 Nov 01/04R 1 1 1CES 1
TASK 57-51-00-220-015
Special Detailed Inspection of Outer Wing Trailing Edge Spoilers 1, 2, 3, 4 and 5 Hinge Pins
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.
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: 575106-02
NOTE : This Task is an alternative to the Task 575100-210-001.
____
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 adjustable access platform 4 m (13 ft. 1 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
1EFF : ALL 1 57-51-00Page A643 1 1 Nov 01/04R 1 1 1CES 1
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
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(114)
