A320飞机维护手册 AMM 时间限制/维护检查 2(86)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 |  |  |  (Ref. TASK 32-21-13-400-001)  |  |  |  |  |  |
 |  |  |  - for the axle sleeve  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-41-12-400-002)  |  |  |  |  |  |
 |  |  |  - for the wheels  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-41-12-400-001)  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |3.  |  | Inspection of the MLG after the  |  |  |  |  |  |
 |  |  | aircraft goes off the runway and the  |  |  |  |  |  |
 |  |  | MLG wheels sank into the ground and/or|  |  |  |  |  |
 |  |  | the MLG found an obstacle on its path.|  |  |  |  |  |
 |  |  | NOTE: If the MLG followed the same  |  |  |  |  |  |
 |  |  |  path as the NLG (straigh line  |  |  |  |  |  |
 |  |  |  and/or same obstacles) and NLG  |  |  |  |  |  |
 |  |  |  inspection showed no damage, do |  |  |  |  |  |
 |  |  |  directly the inspection given  |  |  |  |  |  |
 |  |  |  in item 4.  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  |  A.| Initial inspection  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  |  | (1) Lift the aircraft:  |  X  |  |  |  |  |
 |  |  |  (Ref. TASK 07-11-00-581-001)  |  |  |  |  |  |
 |  |  |  - make sure that extension of the |  X  |  |  |  |  |
 |  |  |  shock absorber is smooth and  |  |  |  |  |  |
 |  |  |  full.  |  |  |  |  |  |
 |  |  |  - examine the sliding rod (the  |  X  |  |  |  |  |
 |  |  |  (part you can see) for blue  |  |  |  |  |  |
 |  |  |  color, signs of bronze or chrome|  |  |  |  |  |
 |  |  |  damage.  |  |  |  |  |  |
 |  |  | (2) Do a check of the pressure in the |  X  |  |  |  |  |

 

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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | 1  | 2  | 3 |  4  |  5  |  6  |  7 | 8 | |----|----|---------------------------------------|-----|-----|-----|----|----| | | | MLG shock absorber | | | | | | | | | (Ref. TASK 12-14-32-614-003) | | | | | | | | | (3) Examine the shock absorber for |  X  | | | | | | | | external leakage. | | | | | | | | | (4) Do the inspection of the MLG |  X  | | | | | | | | (Ref. TASK 32-11-00-200-005) for: | | | | | | | | | - out-of-roundness of shock | | | | | | | | | absorber sliding-rod. | | | | | | | | | - distortion of side-stay lower | | | | | | | | | cardan pin-joint (side-stay | | | | | | | | | disconnected). | | | | | | | | | - distortion of torque link pin. | | | | | | | | | - detailed visual inspection of | | | | | | | | | the barrel in the drag stay | | | | | | | | | blend area | | | | | | | | | - detailed visual inspection of | | | | | | | | | the barrel forward pintle-pin | | | | | | | | | area | | | | | | R | | | - detailed visual inspection of | | | | | | R | | | the rear pintle pin mounting | | | | | | | | | (5) Do the functional test of the |  X  | | | | | | | | Normal Extension/Retraction of the| | | | | | | | | landing gear | | | | | | | | | (Ref. TASK 32-31-00-720-002) | | | | | | | | | - with the MLG door open and the | | | | | | | | | safety lock installed, make sure| | | | | | | | | that the MLG is correctly | | | | | | | | | engaged in the MLG uplock (MLG | | | | | | | | | centered in uplock). | | | | | | | | | (6) Do the functional test of the free|  X  | | | | | | | | fall extension of the landing gear| | | | | | | | | (Ref. TASK 32-33-00-720-001) | | | | | | | | | | | | | | | | B.| | Subsequent inspection | | | | | | | | | | | | | | | | | | (1) If the initial inspection shows no| | | | | | | | | unsatisfactory condition: | | | | | | | | | (a) Do the inspection given in |  X  | | | | | | | | item 4. (inspection of the MLG| | | | | | | | | after the aircraft goes off | | | | | | | | | the runway but the MLG wheels | | | | | |
　
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