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R R R R R R R R R |ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Refer to the manufacturer's | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | | NOTE: If fuse plug is melted, also | | | | | | | | | remove the adjacent wheel for| | | | | | | | | overhaul. | | | | | | | | |(2) Remove the brake for overhaul | X | | | | | | | | (Ref. TASK 32-42-27-000-001). | | | | | | | | | (Refer to the manufacturer's | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | |(3) Remove the axle sleeve | X | | | | | | | | (Ref. TASK 32-42-27-000-001). | | | | | | | | |(4) Do the Inspection of the MLG Axles | X | | | | | | | | after Brake Overheat | | | | | | | | | (Ref. TASK 32-11-00-200-007). | | | | | | | | |(5) Examine the axle sleeve for | X | | | | | | | | distortion and damaged surface. | | | | | | | | |(6) Installation of the removed | | | | | | | | | components | | | | | | | | | (a) Install serviceable components:| | | | | | | | | - for the axle sleeve | | | | | | | | | (Ref. TASK 32-42-71-400-001) | | | | | | | | | - for the brakes | | | | | | | | | (Ref. TASK 32-42-27-400-001) | | | | | | | | | - for the wheels | | | | | | | | | (Ref. TASK 32-41-11-400-006). | | | | | | -------------------------------------------------------------------------------
**ON A/C ALL
5. Close-up________
Subtask 05-51-16-710-050
A. Operational Test of the Systems
R (1) Do an operational test of the normal braking system (Ref. TASK 32-42-00-710-001).
R (2) Do an operational test of the alternate braking system (Ref. TASK 32-43-00-710-001).
Subtask 05-51-16-942-051
B. Put the aircraft back to its initial configuration.
(1)
Remove the warning notice(s).
(2)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : ALL 1 05-51-16Page 612 1 1 May 01/05 1 1 1CES 1 INSPECTION AFTER FLIGHT IN EXCESSIVE TURBULENCE OR IN EXCESS OF VMO/MMO
_______________________________________________________________________ INSPECTION/CHECK
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TASK 05-51-17-200-001
Inspection after in Flight Excessive Load Factor due to Turbulence or Maneuver or in Excess of VMO/MMO
1. Reason for the Job
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本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 時(shí)間限制/維護(hù)檢查 4(42)
