R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 05-51-17Page 606
1221-221, 224-224, 228-228, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
R
R
R
R
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | the upper fuselage section (exter-| | | | | | | | | nal): | | | | | | | | | - examine the frames, skin panels, | | | | | | | | | splices, stringers and riveting for | | | | | | | | | distortion, cracks, pulling, tears | | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Examine the upper fuselage section| | | X | | | | | | internally (the frames, stringers,| | | | | | | | | cleats, and splices) for : | | | | | | | | | - distortion, cracks pulled or | | | | | | | | | torn fasteners, damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | D.| | From FR47 to FR70 : | | | | | | | | | - examine the frames, skin panels, | | | | | | | | | splices, stringers and rivets for: | | | | | | | | | - distortion, cracks, pulling, tears | | | | | | | | | and damaged paintwork. | | | | | | | | | | | | | | | | E.| | Examine the cut-out corners and rivets| | | | | | | | | of the emergency-exit surround panel | | | | | | | | | for : | | | | | | | | | - distortion, cracks, pulling, tears | | | | | | | | | and damaged paintwork. | | | | | | | | | | | | | | | | F.| | Examine the hinge fittings of the bulk| | X | | | | | | | cargo-compartment door for cracks, | | | | | | | | | pulled or torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | G.| | Examine the cut-out corner and rivet | | X | | | | | | | areas of the surround panel of the | | | | | | | | | bulk cargo-compartment door for : | | | | | | | | | - distortion, cracks, pulling, tears | | | | | | | | | and damaged paintwork. | | | | | | | | | | | | | | | |4. | | Horizontal stabilizer cut-out | | | | | | | | | | | | | | | | A.| | Examine the cut-out corners for | X | | | | | | | | cracks. | | | | | | | | | If you find damage : | | | | | | | | | Examine the cut-out edges of the top | | X | | | |
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 05-51-17Page 607
1221-221, 224-224, 228-228, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | and bottom stringers for : | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | NOTE: Do these inspections together, | | | | | | | | | with the horizontal stabilizer | | | | | | | | | inspection. | | | | | | -------------------------------------------------------------------------------
**ON A/C 201-220, 222-223, 225-227, 229-299, 301-399,
Subtask 05-51-17-210-063-A
B. Inspection of the Fuselage
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Belly fairing | | | | | | | | | | | | | | | | A.| | Examine externally all the belly | X | | | | | | | | fairing panels, specially the leading-| | | | | | | | | edge roof fairing and upper and lower | | | | | | | | | wing fairings, for : | | | | | | | | | - correct attachment, delamination, | | | | | | | | | damaged paintwork, pulled or torn | | | | | | | | | fasteners. | | | | | | | | | If you find damage : | | | | | | | | | (1) Remove the damaged panel and | | X | | | | | | | internally examine the belly | | | | | | | | | fairing structure. | | | | | | | | | (2) Examine all the components, pipes,| | X | | | | | | | ducts, electrical looms and their | | | | | | | | | mounts, for distortion, cracks, | | | | | | | | | breaks and fluid leakage. | | | | | | | | | | | | | | | |2. | | Fuselage (FR36 to FR46) | | | | | | | | | | | | | | | | A.| | At the joint of the wing spar box with| X | | | | | | | | the wing, rib1, examine : | | | | | | | | | - the rear-spar web splice, | | | | | | | | | - the fuselage skin panels, | | | | | |
R 1EFF : ALL 1 05-51-17Page 608 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the panel splices. | | | | | | | | | For distortion, cracks, pulled or torn| | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | | | | | | | | B.| | At and around FR46, examine the lower | X | | | | | | | | skin panel of the fuselage between the| | | | | | | | | R stringer 41RH and the L stringer | | | | | | | | | 41LH for : | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | | | | | | | |3. | | Fuselage (FR29 to FR70) | | | | | | | | | If you find damage (refer to 1 or 2 | | | | | | | | | above): | | | | | | | | | | | | | | | | A.| | From FR26 to FR35 : | | X | | | | | | | - externally examine the skin panels, | | | | | | | | | the splicing and the riveting for | | | | | | R | | | distorsion, cracks, pulling, tears | | | | | | | | | and damaged paintwork. | | | | | | | | | If you find damage : | | | | | | | | | (1) Remove the forward cargo-| | | X | | | | | | compartment panels and examine the| | | | | | | | | floor support structure, frames, | | | | | | | | | skin panels, splicing, rivets and | | | | | | | | | stringers for: | | | | | | | | | - distortion, cracks, pulled and | | | | | | | | | torn fasteners, damaged | | | | | | | | | paintwork. | | | | | | | | | | | | | | | | B.| | At FR35, examine the top of the joint | | | | | | | | | between the R stringer 6 and the L | | | | | | | | | stringer 6 for: | | | | | | | | | - distortion, cracks, pulled or torn | | | | | | | | | fasteners, damaged paintwork. | | | | | | | | | | | | | | | | C.| | From FR35 to FR47: | | | | | | | | | - in the main landing-gear well and on| | X | | | | | | | the upper fuselage section (exter-| | | | | | | | | nal): | | | | | | | | | - examine the frames, skin panels, | | | | | | | | | splices, stringers and riveting for | | | | | | R | | | distortion, cracks, pulling, tears | | | | | |
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 2(52)
