A320飞机维护手册 AMM 时间限制/维护检查 4(42)

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R  |  |  |  (Ref. TASK 32-42-27-000-001).  |  |  |  |  |  | 
R  |  |  |  (Refer to the manufacturer's  |  |  |  |  |  | 
R  |  |  |  instructions for the overhaul  |  |  |  |  |  | 
R  |  |  |  procedure).  |  |  |  |  |  |
 |  |  |(3) Installation of the removed  |  |  |  |  |  |
 |  |  |  components  |  |  |  |  |  | 
R  |  |  |  (a) Install serviceable components:|  |  |  |  |  |
 |  |  |  - for the wheels  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-41-11-400-006)  |  |  |  |  |  |
 |  |  |  - for the brakes  |  |  |  |  |  | 
R  |  |  |  (Ref. TASK 32-42-27-400-001).  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  | 
R  |  B.|  |Inspection after wheel fuse-plug(s)  |  |  |  |  |  |
 |  |  |melt and/or the reported cockpit  |  |  |  |  |  |
 |  |  |indication of the brakes temperature  |  |  |  |  |  | 
R  |  |  |equal to or more than 900 deg.C (1472  |  |  |  |  |  |
 |  |  |deg.F)  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  |  |(1) Remove the related wheel for  |  X  |  |  |  |  |
 |  |  |  overhaul  |  |  |  |  |  | 
R  |  |  |  (Ref. TASK 32-41-11-000-006).  |  |  |  |  |  |

 

 -------------------------------------------------------------------------------
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
________________
 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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