B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-57-00-200-001 Aircraft Stability
32-41-11-000-006 Removal of the MLG Wheel
(2649GM,2650GM,2651GM,2652GM)
32-41-11-400-006 Installation of the MLG Wheel
(2649GM,2650GM,2651GM,2652GM)
07-12-00-991-002 Fig. 203
07-12-00-991-004 Fig. 204
3. Job Set-up
__________
Subtask 07-12-00-941-053
A. Not Applicable
Subtask 07-12-00-941-051
R B. Specification of the Hydraulic Jacks
-------------------------------------------------------------------------------| HYDRAULIC JACK DATA | capacity | closed height | hydraulic stroke | | | (min) | (max) | (min) | |----------------------|-------------------|---------------|------------------| | MAIN GEAR | 35 000 daN | 215 mm | 334 mm | | | (78 683.11 lbf) | (8.46 in) | (13.14 in) | -------------------------------------------------------------------------------
Subtask 07-12-00-210-053
C. Visual Check
(1)
Make sure that the aircraft is clear to lift.
(2)
Make sure that the parking brake is on.
(3) Make sure that the jack adapter is in the correct condition.
Subtask 07-12-00-480-051
D. Installation of the wheel chocks - on the wheels of the nose landing gear. - on the wheels of the main landing gear that it is not necessary to
change.
4. Procedure
_________
Subtask 07-12-00-820-051
A. Installation of the Hydraulic Jack (Ref. Fig. 203/TASK 07-12-00-991-002, 204/TASK 07-12-00-991-004)
R (1) Put the hydraulic jack TMH CR 15 or equivalent aft in position so R that its adapter touches the ball-pad of the shock absorber.
(2)
Make sure that the wheel jack is stable and in the vertical position.
(3)
Make sure that the aircraft is stable before you do the lifting (Ref. TASK 05-57-00-200-001).
Jacking Point of the Main Landing Gear
Figure 203/TASK 07-12-00-991-002
EFF : ALL 07-12-00 Page 208
Feb 01/98
CES
R Jacking of the Main Landing Gear Figure 204/TASK 07-12-00-991-004
EFF : CES ALL 07-12-00 Page 209 May 01/05
Subtask 07-12-00-210-055
B. Make sure that this assembly is level.
Subtask 07-12-00-582-051
C. Jacking
(1) Operate the jack to lift the tire off the ground.
R (2) Change the wheel (Ref. TASK 32-41-11-000-006) (Ref. TASK 32-41-11-400-006).
(3) Do not lower the aircraft on its wheels suddenly. To prevent this, slowly operate the hydraulic control of the jack.
5. Close-up
________
Subtask 07-12-00-080-051
A. Removal of Tools
(1) When the aircraft is on its wheels, remove the hydraulic jack.
(2) Remove the wheel chocks.
Subtask 07-12-00-942-051
B. Removal of Ground Support Equipment
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
SHORING - MAINTENANCE PRACTICES
_______________________________
TASK 07-20-00-583-003
Shoring of the Aircraft
1. Reason for the Job
__________________
Shoring is necessary to give a support to the wing in order to release the
loads on the structure when you do major work or modifications.
The AMM shoring procedure gives the general principle only.
Use the detailed shoring instructions given in:
-SRM 51-51-00, when shoring is required for specific Airbus Industrie repairs.
-ARM 3-28, when shoring is required for recovery of the aircraft.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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