(3)
Put a warning notice on the ground service connection to tell persons not to pressurize the Green and Yellow hydraulic systems.
(4)
On the panel 400VU:
-Make sure that the landing-gear control-lever 6GA is in the DOWN position.
-Put a warning notice in position to tell persons not to operate the landing gear.
Subtask 32-31-44-860-059
B. Aircraft Maintenance Configuration
(1)
To do this task it is necessary to put the aircraft on jacks (Ref. TASK 07-11-00-581-001)
(2)
Energize the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002)
(3)
Put the safety barriers in position. Subtask 32-31-44-010-054
C. Get Access
(1)
Open the applicable MLG door (Ref. TASK 32-12-00-010-001). Subtask 32-31-44-869-055
D. Disconnection of the PTU Isolation Coupling
(1)
Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
(2)
Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-001).
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(3)
Disconnect the PTU isolation coupling (Ref. TASK 29-23-00-860-001).
(4)
Obey the flight configuration precautions (Ref. TASK 32-00-00-860-001).
4. Procedure
_________ Subtask 32-31-44-020-054
A. Removal of MLG Uplock-Support Struts
(Ref. Fig. 406/TASK 32-31-44-991-006)
(1) Remove the support strut A.
(a) Make a note of the dimension "Y".
(Ref. Fig. 406/TASK 32-31-44-991-006)
NOTE : This dimension is necessary for the installation of the
____
new component.
(b)
Remove and discard the cotter pins (5) and (11).
(c)
Remove the nut (4) and the washer (3).
(d)
Remove the bolt (1) and the bush (2).
(e)
Remove the nut (12) and the washers (9) and (10).
(f)
Pull the bolt (6) out and removed the washers assembly (7).
(g)
Remove the support strut A (8).
(2) Remove the support strut B
(a) Make a note of the dimension "Z"
(Ref. Fig. 406/TASK 32-31-44-991-006)
NOTE : This dimension is necessary for the installation of the
____
new component.
(b)
Remove and discard the cotter pins (19) and (21).
(c)
Remove the nut (20) and the washer (22).
(d)
Remove the bolt (24) and the bush (23).
(e)
Remove the nut (18) and the washers (16) and (17).
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(f)
Pull the bolt (13) out and removed the washers assembly (14).
(g)
Remove the support strut B (15).
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Rigging of the MLG Uplock Assembly 2509GM (2510GM) Figure 406/TASK 32-31-44-991-006- 13 (SHEET 1)
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Rigging of the MLG Uplock Assembly 2509GM (2510GM) Figure 406/TASK 32-31-44-991-006- 23 (SHEET 2)
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Rigging of the MLG Uplock Assembly 2509GM (2510GM) Figure 406/TASK 32-31-44-991-006- 33 (SHEET 3)
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Installation of the MLG Uplock - Support Struts with A/C on Jacks
1. Reason for the Job
__________________
This task is applicaple if in the installation procedure the setting tool-uplock is used. This is necessary, if the uplock needs new adjustment.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific container No specific hydraulic cart No specific safety barriers No specific warning notice No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98D32104018000 1 SETTING TOOL-UPLOCK
B. Consumable Materials
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本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM LANDING GEAR 起落架5(11)
