-
the adjacent area(s) (1) and (2).
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B. Inspection
(1) Do a special detailed inspection of the areas at point 'Y' of the spoilers 2 thru 4 actuator and hinge fittings (Ref. NTM 57-51-30 PART 6).
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. ________
5. Close-up
Subtask 57-51-00-865-051
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 6CV, 7CV, 8CV, 21CE1, 21CE2, 21CE3, 22CE.
Subtask 57-51-00-860-053
B. Aircraft Maintenance Configuration
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(3)
Retract the flaps (Ref. TASK 27-50-00-866-009).
(4) Retract the spoilers (Ref. TASK 27-60-00-866-002). Subtask 57-51-00-942-050
C. Removal of Equipment
(1)
Remove the access platform(s).
(2)
Remove the warning notice(s).
(3)
Remove the safety barriers.
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 57-51-00-210-001
Detailed Visual Inspection of Outer Wing Trailing Edge Spoilers 1, 2, 3, 4 and 5 Hinge Pins
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: 575106-01
NOTE : This Task is an alternative to the Task 575100-220-015.
____
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 adjustable access platform 4 m (13 ft. 1 in.)
98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
INTENTIONALLY BLANK
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57-51-00Page 612
1 1 May 01/04 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
-------------------------------------------------------------------------------
27-64-41-000-001 Removal of the Spoiler 1
27-64-41-400-001 Installation of the Spoiler 1
27-64-42-000-001 Removal of the Spoiler 2
27-64-42-400-001 Installation of the Spoiler 2
27-64-43-000-001 Removal of the Spoiler 3
27-64-43-400-001 Installation of the Spoiler 3
27-64-44-000-001 Removal of the Spoiler 4
27-64-44-400-001 Installation of the Spoiler 4
27-64-45-000-001 Removal of the Spoiler 5
27-64-45-400-001 Installation of the Spoiler 5
R 57-51-37-000-002 Removal of the Access Panels 573AB(673AB), 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(83)
