Q. Inspection of the Fuselage - Tail Section
 (Ref. Fig. 607/TASK 05-51-11-991-011)

 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Fuselage/Tail Section | | | | | | | | | | | | | | | | | |Examine the unpressurized area behind | | | | | | | | |the pressure bulkhead - Between FR70 | | | | | | | | |and FR77 - and the adjacent structure. | | | | | | | | | | | | | | | | A.| |Examine the skin and the stringers for:| | | | | | | | |- wrinkles, buckles, cracked or flaking| | | | | | | | | paint, loose rivets, | | | | | | | | |- signs of shearing, distorted and | | | | | | | | | twisted stringers. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-11-210-065
 R. Inspection of the Fuselage Section - between FR35 and FR47 (Ref. Fig. 608/TASK 05-51-11-991-012, 609/TASK 05-51-11-991-013, 610/TASK 05-51-11-991-014)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Fuselage section between FR35 and FR47| | | | | | | | | | | | | | | |  A.| | Examine the belly fairing panels for: |  X  | | | | | | | | - loose fasteners, cracked or flaking | | | | | | | | | paint, correct attachement, | | | | | | | | | delamination. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the panels and examine | |  X  | | | | | | | internally the belly fairing for: | | | | | | | | | - the correct attachment of all | | | | | | | | | the components, | | | | | | | | | - loose rivets. | | | | | | | | | (2) Examine the fuselage skin | |  X  | | | | | | | externally below the belly fairing| | | | | | | | | zone for: | | | | | |
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 Main Structure of the Cone/Rear Fuselage Figure 607/TASK 05-51-11-991-011 
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 Lower Part of the Center Fuselage Figure 608/TASK 05-51-11-991-012
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 Center Section Figure 609/TASK 05-51-11-991-013
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 Component Location in the Belly Fairing Structure Figure 610/TASK 05-51-11-991-014
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 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - buckling, loose rivets, cracked | | | | | | | | | or flaking paint. | | | | | | | | | | | | | | | |  B.| | Examine the canted frames at the |  X  | | | | | | | | boundaries of the wheel wells, their | | | | | | | | | junctions, the fittings at FR42 and | | | | | | | | | the adjacent areas. | | | | | | | | | | | | | | | |  C.| | Examine the main-gear locking-system  |  X  | | | | | | | | attachment at FR44 | | | | | | | | | | | | | | | |  D.| | Examine the longitudinal edging spars |  X  | | | | | | | | of the keel beam section. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the structure of the keel | |  X  | | | | | | | beam. | | | | | | | | | (2) Examine the structure of the | |  X  | | | | | | | passenger compartment floor in | | | | | | | | | the main gear well. | | | | | | | | | If you find damage: | | | | | | | | | (a) From FR35 to FR47, examine | | |  X  | | | | | | internally the panels junction of | | | | | | | | | the upper fuselage at stringers | | | | | | | | | 6L and 6R. | | | | | | -------------------------------------------------------------------------------
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R **ON A/C 001-003,

 Subtask 05-51-11-210-066-A
 S. Inspection of the Tail Unit (Ref. TASK 55-10-00-210-001) (Ref. TASK 55-30-00-200-001) (Ref. TASK 49-16-00-200-002) (Ref. TASK 55-16-00-200-001) (Ref. TASK 55-36-00-210-001)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Tail Unit (Fuselage Tail Section) | | | | | | | | |(Zones 310-320-330-340) | | | | | | | | | | | | | | | |  A.| |Do a general visual inspection of: |  X  | | | | | | | |- the attachment areas of the | | | | | | | | | horizontal and vertical stabilizers, | | | | | | | | |- the APU air-intake areas of the tail | | | | | | | | | cone. | | | | | | | | |Horizontal stabilizer | | | | | | | | |(Ref. TASK 55-16-00-200-001) | | | | | | | | |Vertical stabilizer | | | | | | | | |(Ref. TASK 55-36-00-210-001) | | | | | | | | |APU intake (Ref. TASK 49-16-00-200-002)| | | | | | | | |If you find damage: | | | | | | | | |(1) Do a detailed visual inspection | |  X  | | | | | | | of the vertical stabilizer center | | | | | | | | | box (Ref. TASK 55-30-00-200-001) | | | | | | | | |(2) Do a visual inspection of the THS | | | | | | | | | sparbox | | | | | | | | | (Ref. TASK 55-10-00-210-001) | | | | | | | | |(3) Examine the hinges of the elevator | |  X  | | | | | | | and the rudder for cracks | | | | | | -------------------------------------------------------------------------------R **ON A/C 051-054,
　
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