B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-001 Lifting for Aircraft Maintenance Operations 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU) 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears
1EFF : ALL 1 57-26-13Page 424 1 1 May 01/05R 1 1 1CES 1
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-002 Installation of the Safety Devices on the Landing
Gear Doors R 32-00-00-860-001 Flight Configuration Precautions with Electrical R Power
32-31-46-000-001 Removal of the MLG Actuating Cylinder 57-26-13-000-002 Removal of the Bearing Assembly of the MLG Actuator Attachment 57-26-13-991-004 Fig. 403
3. Job Set-up
__________
Subtask 57-26-13-941-055
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Install the safety devices on the landing gears (Ref. TASK 32-00-00-481-001) and the landing gear doors (Ref. TASK 32-00-00-481-002).
(3)
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.
(4)
Put a warning notice to tell persons not to pressurize the Green hydraulic system.
Subtask 57-26-13-582-050
B. Lift the Aircraft
(1) Lift the aircraft on jacks (Ref. TASK 07-11-00-581-001).
Subtask 57-26-13-860-055
C. Aircraft Maintenance Configuration
(1)
Make sure that the Yellow and Green hydraulic systems are de-pressurized (Ref. TASK 29-00-00-864-001).
(2)
Disconnect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-001).
Subtask 57-26-13-869-052
D. Flight Configuration Precautions
(1)
If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.
(2)
If the electrical power is necessary, do the precautions for flight configuration (Ref. TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.
Subtask 57-26-13-865-050
E. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
Subtask 57-26-13-010-054
F. Get Access
(1)
Put the access platform in position below the applicable main landing gear bay, zone 571 or 671.
(2)
Remove the applicable MLG actuating cylinder (Ref. TASK 32-31-46-000-001).
(3)
Remove the applicable MLG actuator attachment bearing assembly (Ref. TASK 57-26-13-000-002) .
1EFF : ALL 1 57-26-13Page 426 1 1 May 01/05R 1 1 1CES 1
4. Procedure
_________
(Ref. Fig. 403/TASK 57-26-13-991-004) Subtask 57-26-13-020-054
A. Removal of the Bearing Seals
(1) Remove the bearing-halves (1) from the bearing ball (2) as follows:
(a) Hold the applicable bearing-half (1) tightly. NOTE : Separation of the bearing-halves (1) from the bearing ball
____ (2) is not easy.
(b)
Carefully remove the bearing-halves (1) from the bearing ball (2).
(c)
Make sure that the distance between the bearing-halves (1) is constant during separation.
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼2(49)
