-the MLG spare-seal activating-valve has been closed.
NOTE : It is recommended that ALL gland seals on the applicable MLG
____ are replaced at a subsequent scheduled maintenance procedure.
Subtask 32-11-13-611-051
B. Check the Contents of the MLG Shock Absorber
(1) Make sure that the contents of the MLG shock absorber are at the correct level (Ref. TASK 12-12-32-611-004).
1EFF : ALL 1 32-11-13Page 207 1 1 May 01/05R 1 1 1CES 1
Spare-Seal Activating-Valve Figure 202/TASK 32-11-13-991-004
1EFF : 1 1R 1CES ALL 1 11 1 32-11-13 Page 208 May 01/05
5. Close-up
________ Subtask 32-11-13-942-052
A. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
1EFF : ALL 1 32-11-13Page 209 1 1 May 01/05R 1 1 1CES 1
TASK 32-11-13-860-002 To Open the Spare-Seal Activating-Valve 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. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1.
Reason for the Job
__________________
To reactivate the lower gland seals after gland seal replacement
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notices R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire, corrosion resistant steel 0.8 mm (0.032 in) dia.
1EFF : ALL 1 32-11-13Page 210 1 1 May 01/05 1 1 1CES 1
C. Expendable Parts -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
1 cap screw 32-11-11 65A-180
1 cap screw 32-11-11 65C-180
1 cap screw 32-11-11 65D-180
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
-------------------------------------------------------------------------------32-11-13-991-004 Fig. 202
3. Job Set-up
__________ Subtask 32-11-13-941-053
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Put a warning notices in the cockpit to tell persons not to operate the landing gear.
4. Procedure
_________
(Ref. Fig. 202/TASK 32-11-13-991-004) Subtask 32-11-13-860-053
A. To Open the Spare-Seal Activating-Valve
(1)
Remove and discard the lockwire from the spindle (2).
(2)
Turn the spindle (2) counter-clockwise by hand to its stop, to open the spare-seal activating-valve.
(3)
Install the cap screw (1).
(4)
Torque the cap screw (1) to between 0.4 and 0.45 m.daN (35.39 and
39.82 lbf.in).
1EFF : ALL 1 32-11-13Page 211 1 1 May 01/05 1 1 1CES 1
(5)
Safety the cap screw (1) with lockwire, corrosion resistant steel 0.8
mm (0.032 in) dia..
(6)
Make a note in the aircraft technical log that the spare-seal activating-valve has been opened.
5. Close-up
________ Subtask 32-11-13-942-053
A. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Make a record in the aircraft log that the spare-seal
activating-valve is open.
1EFF : ALL 1 32-11-13Page 212 1 1 May 01/05 1 1 1CES 1 SHOCK ABSORBER ASSY - MLG - REMOVAL/INSTALLATION 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 LANDING GEAR 起落架2(13)
