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 | |  | (Ref. TASK 27-54-46-200-001). | | |  |  |  |
 | |  | | | |  |  |  |
 |2. |  | Inspection of the flap track | | |  |  |  |
 | |  | attachments | | |  |  |  |
 | |  | | | |  |  |  |
 |  A.|  | Examine the attachment of the flap |  X  | |  |  |  |
 | |  | track No.1 at the wing root and their | | |  |  |  |
 | |  | attachment fittings for distortion, | | |  |  |  |
 | |  | cracks and damaged paintwork. | | |  |  |  |
 | |  | If you find damage: | | |  |  |  |
 | |  | (1) Get access to the main gear | |  X  |  |  |  |
 | |  | compartment and the aft cargo | | |  |  |  |
 | |  | compartment. | | |  |  |  |
 | |  | (2) Examine the FR45 and FR47 for | |  X  |  |  |  |
 | |  | distortion, cracks and damaged | | |  |  |  |
 | |  | paintwork. | | |  |  |  |
 | |  | | | |  |  |  |
 |  B.|  | Examine externally (as far as |  X  | |  |  |  |
 | |  | possible) the beam assemblies of the | | |  |  |  |
 | |  | flap tracks No. 2 to No. 4 and all the| | |  |  |  |
 | |  | the components installed on them for | | |  |  |  |
 | |  | distortion, cracks and damaged | | |  |  |  |
 | |  | paintwork. | | |  |  |  |
 | |  | If you find damage: | | |  |  |  |

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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (1) Do a detailed visual inspection of| |  X  | | | | | | | the flap track No.2 to No. 4 beams| | | | | | | | | Aft attachment (pay particular | | | | | | | | | attention to the failsafe devices | | | | | | | | | and the spigot pin). | | | | | | | | | (Ref. TASK 57-26-00-200-001). | | | | | | | | | NOTE: Make sure that the clearence| | | | | | | | | at failsafe pins (adjacent | | | | | | | | | to the spigot) is correct. | | | | | | | | | (2) Do a detailed visual inspection of| |  X  | | | | | | | the flap tracks No. 2 to No.4 | | | | | | | | | beams Fwd attachment (pay | | | | | | | | | particular attention to the | | | | | | | | | failsafe devices and the spigot | | | | | | | | | pin). | | | | | | | | | (Ref. TASK 57-26-00-200-006) | | | | | | | | | (3) Defuel the wing tank | |  X  | | | | | | | (Ref. TASK 28-25-00-650-001). | | | | | | | | | (4) Examine the ribs 6, 12 and 19 and | |  X  | | | | | | | the rear spar for distortion, | | | | | | | | | cracks and damaged sealant fillets| | | | | | -------------------------------------------------------------------------------
Subtask 05-51-13-210-054
 D. Inspection of the Slat System
 (Ref. Fig. 605/TASK 05-51-13-991-004, 606/TASK 05-51-13-991-003)
 (Ref. TASK 27-84-00-200-001) (Ref. TASK 27-84-00-210-001)
 (Ref. TASK 28-25-00-650-001) (Ref. TASK 28-10-00-910-002)

 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the slat assemblies and | | | | | | | | | slat transmission | | | | | | | | | | | | | | | |  A.| | Examine the slats for distortion, |  X  | | | | | | | | cracks, pulled or torn fasteners, | | | | | | | | | skin/honeycomb-core delamination and | | | | | | | | | damaged paintwork. | | | | | | | | | | | | | | | |  B.| | Examine the hold-down stop-bracket and|  X  | | | | |
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R R  Component Location of the Slat System Figure 605/TASK 05-51-13-991-004
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 Slat Components Figure 606/TASK 05-51-13-991-003
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
　
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