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 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Top Skin | | | | | | | | | | | | | | | |  A.| | Do an inspection of the wing top skin.|  X  | | | | | | | | Make sure that: | | | | | | | | | - there is no distortion, | | | | | | | | | - there are no cracks, | | | | | | | | | - the paint and the sealant are not | | | | | | | | | damaged, | | | | | | | | | - the fasteners are in the correct | | | | | | | | | condition. Pay particular attention | | | | | | | | | to the fasteners at the rear spar | | | | | | | | | between rib 3 and rib 5. | | | | | | | | | | | | | | | |2. | | Bottom Skin | | | | | | | | | | | | | | | |  A.| | Do an inspection of the wing bottom |  X  | | | | | | | | skin. Carefully examine the areas | | | | | | | | | adjacent to: | | | | | | | | | - the flap beams, | | | | | | | | | - the engine pylon, | | | | | | | | | - the MLG attachments. | | | | | | | | | Make sure that: | | | | | | | | | - there is no distortion, | | | | | | | | | - there are no cracks, | | | | | | | | | - there are no fluid leaks, | | | | | | | | | - the paint and the sealant are not | | | | | | | | | damaged, | | | | | | | | | - the fasteners are in the correct | | | | | | | | | condition. | | | | | | | | | | | | | | | |  B.| | If there are signs of damage adjacent | |  X  | | | | | | | to the beams of flaps N.2, 3 or 4. | | | | | | | | | (1) Remove the applicable flap beam | | | | | | | | | fairing | | | | | |
R 1EFF : 001-003, 051-054, 1 05-51-11Page 623 1 1 May 01/05 1 1 1CES 1

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

 |  |  |  (Ref. TASK 57-55-11-000-001).  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  C.|  | Do an inspection of the flap beam  |  |  X  |  |  |  |
 |  |  | assembly(ies). Make sure that:  |  |  |  |  |  |
 |  |  | - the clearance to the wing is  |  |  |  |  |  |
 |  |  |  correct,  |  |  |  |  |  |
 |  |  | - there are no cracks,  |  |  |  |  |  |
 |  |  | - the paint and the sealant are not  |  |  |  |  |  |
 |  |  |  damaged,  |  |  |  |  |  |
 |  |  | - there is no damage,  |  |  |  |  |  |
 |  |  | - the fasteners and safety devices are|  |  |  |  |  |
 |  |  |  in the correct condition.  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  D.|  | Do an inspection of the applicable  |  |  X  |  |  |  |
 |  |  | flap track. Make sure that there are  |  |  |  |  |  |
 |  |  | no cracks and damage. Do this  |  |  |  |  |  |
 |  |  | inspection with the flaps extended and|  |  |  |  |  |
 |  |  | retracted.  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  |  | NOTE : Use the applicable NTM  |  |  |  |  |  |
 |  |  |  procedure to find small cracks |  |  |  |  |  |
 |  |  |  into the track radii.  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  E.|  | If there are signs of damage to the  |  |  |  X  |  |  |
 |  |  | flap beam(s) or flap track(s).  |  |  |  |  |  |
 |  |  | (1) Remove the related flap beam  |  |  |  |  |  |
 |  |  |  assembly for component maintenance|  |  |  |  |  |
 |  |  |  - for the flaps N.2 beam assembly |  |  |  |  |  |
　
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