-
for the right wing, install 631CB, 632CB, 633CB.
(3) Remove the access platform(s).
**ON A/C 301-399,
Subtask 57-26-00-410-067-A
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the applicable flap track fairing (Ref. TASK 57-55-11-400-004).
-
for the left wing, install 531CB, 532CB, 533CB
-
for the right wing, install 631CB, 632CB, 633CB.
(3) Remove the access platform(s).
**ON A/C ALL
Subtask 57-26-00-865-073
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-26-00-860-051
C. Aircraft Configuration
(1) Fully retract the flaps (Ref. TASK 27-50-00-866-009). Subtask 57-26-00-942-067
D. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
ATTACHMENT - PYLON, REAR - REMOVAL/INSTALLATION
_______________________________________________
TASK 57-26-12-000-001
Removal of the Pylon Rear Attachment Bearing
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific bearing extractor No specific safety barriers No specific warning notices No specific access platform 2 m (6 ft. 7 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER 98D57004026000 1 SOCKET - PYLON PICK-UP 98D57004027000 1 SPANNER - PYLON PICK-UP
1EFF : ALL 1 57-26-12Page 401 1 1 May 01/04R 1 1 1CES 1
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
54-51-17-000-002 Removal of the Pylon-to-Wing Aft Attach Fitting at RIB10
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-26-12-991-001 Fig. 401
**ON A/C 301-399,
57-26-12-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 57-26-12-941-050
A. Safety Precautions
(1)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(2)
Put the safety barriers in position.
(3)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-26-12-010-050
B. Get Access
(1)
Put the access platform in position below the applicable pylon rear-attachment point, zone 475(485).
(2)
Remove the applicable aft attach fitting (Ref. TASK 54-51-17-000-002).
4. Procedure
_________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 57-26-12-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 57-26-12-991-001-A)
**ON A/C ALL
Subtask 57-26-12-020-050
A. Removal of the Pylon Rear Attachment Bearing
(1)
Bend the tab washer (2) to release the slotted nut (1).
(2)
Hold the bearing (4) with the SPANNER - PYLON PICK-UP (98D57004027000) and use the SOCKET - PYLON PICK-UP (98D57004026000) to remove the slotted nut (1).
(3)
Make sure that the slotted nut (1) is in the correct condition.
(4)
Remove and discard the tab washer (2).
(5)
Do these steps to remove the bearing (4): CAUTION : DO NOT DAMAGE THE REAR BEARING ATTACHMENT WHEN YOU REMOVE
_______
THE BEARING.
(a) Use an applicable bearing extractor to remove the bearing (4). 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM WINGS 機(jī)翼2(40)
