-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
| | | (Ref. TASK 32-21-27-000-001). | | | | | | | | |(4) Manually move the upper torque link| X | | | | | | | | to turn the rotating tube: | | | | | | | | | - make sure that the rotating tube | | | | | | | | | turns freely. | | | | | | | | |(5) Connect the torque link | | | | | | | | | (Ref. TASK 32-21-27-400-001) | | | | | | | | |(6) Remove the NLG steering actuator | X | | | | | | | | (Ref. TASK 32-51-42-000-001): | | | | | | | | | (a) Examine the steering piston | X | | | | | | | | seals, the cylinders and the | | | | | | | | | piston attachment for: | | | | | | | | | - cracks, damaged paint and | | | | | | | | | deformation. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-23-720-050
B. Test (Ref. TASK 32-31-00-720-003) (Ref. TASK 32-51-00-720-003) (Ref. TASK 32-21-11-000-002)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
R |1. | | Do the test of normal extension and | X | | | | | | | | retraction of the NLG. | | | | | | | | | (Ref. TASK 32-31-00-720-003) | | | | | | | | | | | | | | | |2. | | Do a functional test of the nose wheel| X | | | | | | | | steering | | | | | | | | | (Ref. TASK 32-51-00-720-003) | | | | | | | | | If you hear an unusual noise: | | | | | | | | | - Remove the NLG leg for overhaul. | | X | | | | | | | (Ref. TASK 32-21-11-000-002) | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-23-410-052
C. Close Access
(1)
Close the NLG doors (Ref. TASK 32-22-00-410-001).
(2)
Lower the aircraft (Ref. TASK 07-11-00-586-001)
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
5. Close-up
________ Subtask 05-51-23-942-052
A. Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : ALL 1 05-51-23Page 606 1 1 Nov 01/00R 1 1 1CES 1
INSPECTION AFTER LEAVING RUNWAY OR TAXIWAY - INSPECTION/CHECK
_____________________________________________________________
TASK 05-51-24-200-001
Inspection after Leaving Runway or Taxiway
1. Reason for the Job
__________________
When an aircraft goes off a runway or taxiway, the loads on the landing gear and the structure can change. The inspection that is necessary must be in function of all the different possible causes of these load changes:
-
the speed of the aircraft,
-
the weight of the aircraft,
-
the type of the ground (soft or hard),
-
the distance the landing gear goes into the ground.
R NOTE : Recovery must obey the ARM requirement. If recovery is different to
____ R the ARM requirement or if no recovery report is available, refer to R Airbus for special instructions.
Thus, when this incident occurs, you must always do this full inspection
before the aircraft can do more flights.
You must tell Airbus Industrie all the details of the incident immediately.
Airbus Industrie will give you the data and the aid to help you get the
aircraft safely back into operation.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
No specific access platform 3 m (9 ft. 10 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-51-16-200-001 05-56-00-200-001
07-11-00-581-001 07-11-00-581-003
07-11-00-586-001
R 07-11-00-586-002 12-14-32-614-004 24-41-00-862-002
27-50-00-866-008 27-50-00-866-009 28-10-00-910-002 28-25-00-650-001 29-00-00-864-001
32-00-00-481-001
R 32-11-00-200-003 32-11-00-200-005
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本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 2(78)
