A320飞机维护手册 AMM 时间限制/维护检查 4(75)

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 |  |  | (2) If the initial inspection shows  |  |  |  |  |  |
 |  |  |  unsatisfactory condition(s):  |  |  |  |  |  |
 |  |  |  (a) Remove the NLG, the lockstay  |  |  X  |  |  |  |
 |  |  |  assembly and drag strut assem-|  |  |  |  |  |
 |  |  |  bly for overhaul:  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-21-11-000-002)  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-21-17-000-001)  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-21-16-000-002)  |  |  |  |  |  |
 |  |  |  (refer to the manufacturer's  |  |  |  |  |  |
 |  |  |  instructions for the overhaul |  |  |  |  |  |
 |  |  |  procedure)  |  |  |  |  |  |
 |  |  |  (b) On the aircraft, examine the  |  |  X  |  |  |  |
 |  |  |  attachment fittings and the  |  |  |  |  |  |
 |  |  |  bearings of the drag strut  |  |  |  |  |  |
 |  |  |  assembly for distortion,  |  |  |  |  |  |
 |  |  |  cracks and damaged paintwork. |  |  |  |  |  |

 1EFF : ALL 1 05-51-24Page 608 1 1 May 01/05R 1 1 1CES 1

 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | If you find damage: | | | | | | | | | - tell Airbus Industrie about | | |  X  | | | | | | the results. | | | | | | | | | (c) On the aircraft, examine the  | |  X  | | | | | | | attachment fittings of the | | | | | | | | | NLG for distortion, cracks and| | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | - tell Airbus Industrie about | | |  X  | | | | | | the results. | | | | | | | | | (d) Examine the NLG actuating | |  X  | | | | | | | cylinder and its attachment | | | | | | | | | fitting for distortion, cracks| | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | - remove actuating cylinder | | |  X  | | | | | | for a strip-down inspection | | | | | |
R | | | (Ref. TASK 32-31-22-000-001)| | | | | |
R | | | (refer to the manufacturer's| | | | | |
R | | | instructions for strip-down | | | | | |
R | | | inspection procedure). | | | | | |
R | | | - on the aircraft, continue | | |  X  | | | | | | the inspection of the | | | | | | | | | attachment fitting for da-| | | | | | | | | mage | | | | | | | | | If you find damage: | | | | | | | | | . tell Airbus Industrie | | | | | | | | | about the results. | | | | | | | | | (e) In the avionics compartment,  | |  X  | | | | | | | examine: | | | | | | | | | - the gear-well roof, | | | | | | | | | - roof-to-sidewall joint | | | | | | | | | - the floor support-strut | | | | | | | | | attach-fitting for distor-| | | | | | | | | tion, cracks, pulled or torn| | | | | | | | | fasteners and damaged paint-| | | | | | | | | work. | | | | | | | | | If you find damage: | | | | | | | | | - tell Airbus Industrie about | | |  X  | | | | | | the results. | | | | | | | | | (f) If you removed components, | |  X  | | | | | | | install serviceable compo-| | | | | | | | | nents: | | | | | | | | | - for the actuating cylinder | | | | | | | | | (Ref. TASK 32-31-22-400-001)| | | | | | | | | - for the drag strut assembly | | | | | | | | | (Ref. TASK 32-21-16-400-002)| | | | | |

 -------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
 | |CODE| |  1  |  2  |  3  |SIGN|FIG.|
 |----|----|---------------------------------------|-----|-----|-----|----|----|

 |  |  |  - for the lockstay assembly  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-21-17-400-001)|  |  |  |  |  |
 |  |  |  - for the NLG  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-21-11-400-002)|  |  |  |  |  | 
　
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