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FIG.ITEM |DESIGNATION |IPC-CSN
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22 backing ring 32-11-13 02E-320 22 lock washer 32-11-13 02G-020 22 backing ring 32-11-13 02G-320 23 lock washer 32-11-13 02E-020 23 lock washer 32-11-13 02G-020 24 lock washer 32-11-13 02E-020 24 lock washer 32-11-13 02G-020
D. Referenced Information
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REFERENCE DESIGNATION
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29-10-00-864-001 Depressurize the Green Hydraulic System 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
the Ground Connector 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
32-11-13-000-001 Removal of the MLG Shock Absorber
32-11-13-400-001 Installation of the MLG Shock Absorber
SIL 12-008 (for corrective action)
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 401-499,
32-11-13-991-011-A Fig. 405
**ON A/C 051-052,
32-11-13-991-011 Fig. 405A
**ON A/C 301-399,
32-11-13-991-011-B Fig. 405B
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3. Job Set-up
__________
Subtask 32-11-13-941-058
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notices are in the cockpit to tell persons not to operate the landing gear and the brakes.
(3)
Make sure that the warning notices are on the ground service connections to tell persons not to operate:
-
the green hydraulic system
-
the Blue hydraulic system.
(4)
Make sure that the warning notice is in position to tell persons not to operate the landing gear doors.
(5)
Make sure that the safety devices are on the landing gear (Ref. TASK 32-00-00-481-001).
Subtask 32-11-13-860-060
B. Aircraft Maintenance Configuration
(1)
Make sure that the Blue and the Green hydraulic systems are depressurized (Ref. TASK 29-10-00-864-001) and (Ref. TASK 29-10-00-864-003).
(2)
Make sure that the applicable hydraulic reservoirs are depressurized (Ref. TASK 29-14-00-614-001).
(3)
Make sure that MLG shock absorber is removed (Ref. TASK 32-11-13-000-001).
4. Procedure
_________ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 405/TASK 32-11-13-991-011-A)
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R **ON A/C 051-052,
R (Ref. Fig. 405A/TASK 32-11-13-991-011)
R **ON A/C 301-399,
R (Ref. Fig. 405B/TASK 32-11-13-991-011-B)
**ON A/C 001-003,
Subtask 32-11-13-420-055-A
A. Preparation for Installation
(1) Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean the seal grooves and the interfaces of the jacking dome (22).
(2) Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interface and/or the adjacent area.
(4) Use a clean lint-free cloth to dry the seal grooves.
(5) Lubricate the new items that follow with HYDRAULIC FLUIDS (Material No. 02-001) or HYDRAULIC FLUIDS (Material No. 02-004): - seal (1) - seal (2) - retainers (6) - packings (7) - seal (8) - seal (9) - sealing ring (10) - joint seal (11) - wiper ring (13) - O-ring (20) - backing ring (21).
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本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架2(37)
