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时间:2011-02-11 09:46来源:蓝天飞行翻译 作者:admin
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 |  |  |  cylinder  |  |  |  |  |  |
 |  |  | for distortion, cracks, pulled or torn|  |  |  |  |  |
 |  |  | fasteners and damaged paintwork.  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  D.|  | Examine the nose landing-gear and  |  X  |  |  |  |  | 
R  |  |  | specially:  |  |  |  |  |  |
 |  |  | - the components  |  |  |  |  |  |
 |  |  | - the pipes  |  |  |  |  |  |
 |  |  | - the electrical looms  |  |  |  |  |  |
 |  |  | - the control cables  |  |  |  |  |  |
 |  |  | - the pulleys  |  |  |  |  |  |
 |  |  | - the linkages  |  |  |  |  |  |
 |  |  | - the mount.  |  |  |  |  |  |

 -------------------------------------------------------------------------------


 Subtask 05-51-15-210-052

 C. Inspection of the Fuselage (FR35 to FR50)
 (Ref. TASK 32-11-00-200-001)

 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Belly Fairing | | | | | | | | | | | | | | | |  A.| | Examine the belly fairing panels for  |  X  | | | | | | | | holes, delamination, cracked or | | | | | | | | | flaking paint and loose fasteners. | | | | | | | | | Make sure that the panels are | | | | | | | | | correctly attached. | | | | | | R | | | If you find damage: | | | | | | | | | (1) Remove the panels and internally  | |  X  | | | | | | | examine the belly fairing | | | | | | | | | structure for buckling, cracks and| | | | | | | | | damaged paintwork. | | | | | | R  | | | (2) Examine: | |  X  | | | | | | | - the pipes | | | | | | | | | - the ducts | | | | | | | | | - the electrical looms | | | | | | | | | - the mounts | | | | | | | | | for fluid leakage, distortion, | | | | | | | | | rupture, breaks, cracks. | | | | | | | | | Make sure that the components are | | | | | | | | | correctly attached and examine the | | | | | | | | | condition of the safety devices. | | | | | | | | | | | | | | | |2. | | Main Landing-Gear Well | | | | | | | | | | | | | | | |  A.| | In the main landing-gear well, examine|  X  | | | | | | | | the protective panels and the | | | | | | | | | structure for distortion, cracks, | | | | | | | | | pulled or torn fasteners, honeycomb | | | | | | | | | delamination, core damage. | | | | | | | | | | | | | | | |  B.| | Examine the main landing gear and |  X  | | | | | R | | | specially: | | | | | | | | | - the pipes | | | | | | | | | - the ducts | | | | | | | | | - the electrical looms | | | | | | | | | - the mounts | | | | | | | | | - the control actuators | | | | | |


 -------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | for fluid leakage, distortion, | | | | | | | | | rupture, breaks, cracks. | | | | | | | | | Make sure that the components are | | | | | | | | | correctly attached and examine the | | | | | | | | | condition of the safety devices | | | | | | | | | (Ref. TASK 32-11-00-200-001). | | | | | | | | | | | | | | | | 3. | | Main Landing-Gear Main-Doors | | | | | | | | | | | | | | | R  |  A.| | Examine: |  X  | | | | | | | | - the door | | | | | | | | | - the hinges | | | | | | | | | - the actuating cylinder attachments | | | | | | | | | - the sequence valve mounts | | | | | | | | | - the linkage | | | | | | | | | for distortion, cracks, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | |  B.| | Examine the actuating cylinder, the |  X  | | | | | | | | sequence valve, the hoses and the | | | | | | | | | pipes for distortion, cracks, rupture | | | | | | | | | and fluid leakage. Also examine the | | | | | | | | | condition of the safety devices. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-15-210-053
 D. Inspection of the Nacelles, Engines and Pylons R (Ref. TASK 71-13-11-200-001) (Ref. TASK 72-00-00-200-006)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Nacelles and Engine | | | | | | | | | | | | | | | |  A.| | Externally examine the nacelle and the|  X  | | | | | R | | | primary nozzle for: | | | | | | | | | distortion, cracks, delamination, | | | | | | | | | cracked or flaking paint, loose rivets| | | | | | | | | and signs of shearing. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the cowls and internally | |  X  | | | |
 
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