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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 | |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (6) Examine the side stay assembly and|  X  | | | | | | | | its attachment fittings for | | | | | | | | | distortion, cracks and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the side-stay assembly | |  X  | | | | | | | for overhaul. | | | | | | | | | (Ref. TASK 32-11-16-000-001) | | | | | | | | | (refer to the manufacturer's | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | | (b) Do the dimensional inspection | |  X  | | | | | | | of the side-stay cardan | | | | | | | | | pin-joint lugs on MLG leg. | | | | | | R | | | (Ref. TASK 32-11-00-220-004) | | | | | | | | | If you find damage: | | | | | | | | | - remove the MLG | | |  X  | | | | | | (Ref. TASK 32-11-11-000-001)| | | | | | | | | (c) On the aircraft, continue the | |  X  | | | | | | | inspection of the side-stay | | | | | | | | | attachment fitting. | | | | | | | | | If you find damage: | | | | | | | | | - tell Airbus Industrie about | | |  X  | | | | | | the results. | | | | | | | | | (7) Examine the lockstay assembly and |  X  | | | | | | | | lockstay actuator for distortion, | | | | | | | | | cracks and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the lockstay assembly  | |  X  | | | | | | | and lockstay actuator for | | | | | | | | | overhaul | | | | | | | | | (Ref. TASK 32-11-17-000-001) | | | | | | | | | (Ref. TASK 32-11-21-000-001) | | | | | | | | | (refer to the manufacturer's | | | | | | | | | instructions for the overhaul | | | | | | | | | procedure). | | | | | | | | | (b) On the aircraft, continue the | |  X  | | | | | | | inspection of the attachment | | | | | |

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

 |  |  |  fittings for damage.  |  |  |  |  |  |
 |  |  |  If you find damage:  |  |  |  |  |  |
 |  |  |  - tell Airbus Industrie about |  |  |  X  |  |  |
 |  |  |  the results  |  |  |  |  |  |
 |  |  | (8) Examine the MLG retraction  |  X  |  |  |  |  |
 |  |  |  actuator and its attachment  |  |  |  |  |  |
 |  |  |  fittings for distortion, cracks,  |  |  |  |  |  |
 |  |  |  and damaged paintwork.  |  |  |  |  |  |
 |  |  |  If you find damage:  |  |  |  |  |  |
 |  |  |  (a) Remove the retraction actuator|  |  X  |  |  |  |
 |  |  |  for strip-down inspection  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-31-46-000-001)  |  |  |  |  |  |
 |  |  |  (refer to the manufacturer's  |  |  |  |  |  |
 |  |  |  instructions for the  |  |  |  |  |  |
 |  |  |  strip-down procedure).  |  |  |  |  |  |
 |  |  |  (b) On the aircraft, continue the |  |  X  |  |  |  |
 |  |  |  inspection of the attachment  |  |  |  |  |  |
 |  |  |  fittings for damage.  |  |  |  |  |  |
 |  |  |  If you find damage:  |  |  |  |  |  |
 |  |  |  - tell Airbus Industrie about |  |  |  X  |  |  |
 |  |  |  the results.  |  |  |  |  |  |
 |  |  | (9) Examine the MLG well (all the  |  X  |  |  |  |  |
　
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