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时间:2011-03-27 08:44来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 35.8 and between ... Detailed Inspection of FR 35.1 and A687 301-399, FR 35.2A Web and Door Stop Intercostals, at Junction Area, between Door Stop No1 and No8 (LH)/No6 (RH), LH/RH Detailed Inspection of Attachment A692 301-399, Area of FR35.1 and FR35.2A to Cabin Floor Beams, LH/RH Detailed Inspection of Skin of A696 151-199, 401-499 Circumferential Joint at FR 35, between Stringer 10 LH and Stringer 10 RH, External Side General Visual Inspection of B600 301-399, Fuselage Skin Around Forward Emergency Exit Skin Cutout between FR 35 and FR 35.3 and from Stringer 8 to Stringer 23 External...
 PANELS - CABIN FLOOR  53-22-12
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Cabin Floor Panels 401 ALL
 Installation of the Cabin Floor 407 ALL
 Panels

 PANELS - FWD CARGO COMPARTMENT FLOOR 53-22-14
 REMOVAL/INSTALLATION  401 ALL
 Removal of the FWD 401 ALL
 Cargo-Compartment Floor-Panels

 53-CONTENTS Page 12 Aug 01/05 R CES


 CHAPTER 53
__________
 FUSELAGE
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Installation of the FWD 409 ALL Cargo-Compartment Floor-Panels Removal of the Maintenance Panels 414 301-399, at Frame 35.5 Installation of the Maintenance 417 301-399, Panels at Frame 35.5
 FAIRINGS - WING TO FUSELAGE 53-25-11
 REMOVAL/INSTALLATION 401 ALL Removal of the Wing-to-Fuselage 401 ALL Fairings (191AT, 191AB, 192AT, 192AB) Installation of the 410 ALL Wing-to-Fuselage Fairings (191AT, 191AB, 192AT, 192AB)
 SCUFF PLATES - EMERGENCY EXIT DOOR 53-25-41
 REMOVAL/INSTALLATION 401 301-399, Removal of the FWD Emergency-Exit 401 301-399, Scuff-Plate Installation of the FWD 404 301-399, Emergency-Exit Scuff-Plate
 MISCELLANEOUS (EG : DRAINS) 53-29-00
 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Description 1 ALL
 DRAINS - FORWARD FUSELAGE 53-29-41
 REMOVAL/INSTALLATION 401 ALL Removal of the Drain Valves 401 ALL Installation of the Drain Valves 406 ALL
 CENTER FUSELAGE 53-30-00
_______________
 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Description 1 ALL
 MAIN STRUCTURE 53-31-00
 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Description 1 ALL Wing Center Box 1 ALL Belly Fairing 3 ALL Center Fuselage 3 ALL
 MAIN STRUCTURE 53-31-00
 53-CONTENTS Page 13 Aug 01/05 R CES


 CHAPTER 53
__________
 FUSELAGE
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________
 INSPECTION/CHECK 601 ALL
 Detailed Visual Inspection of 601 ALL
 Pressure Bulkhead at FR46, FWD
 Face
 Detailed Visual Inspection of MLG 605 ALL
 Bay Fuselage Side Panels inside
 MLG Bay, between FR42 and FR46,
 including Slanted Frames and Side
 Box, LH/RH
 Detailed Visual Inspection of MLG 609 ALL
 Bay Fuselage Side Panels, Outboard
 Face, between FR42 and FR47, from
 STGR26 to STGR36, LH/RH
 Detailed Visual Inspection of 614 ALL
 Upper Surfaces of Pressure Deck
 Membranes, Side Boxes between FR42
 and FR46 including Connections to
 all Beams and Ribs, LH/RH
 Detailed Visual Inspection of 618 ALL
 Lower Surface of Pressure Deck
 Membranes between FR42 and FR46
 Including Connections to
 Longitudinal Beams
 Detailed Visual Inspection of 622 ALL
 Keelbeam Box
 Detailed Visual Inspection of 629 ALL
 Pressure Bulkhead at FR46, AFT
 Face, Including Vertical Beams,
 Above Cargo Floor Level
 Detailed Visual Inspection of 635 001-049, 051-099
 Internal Structure around the 101-149, 151-199
 Emergency Exit Cutouts, Both 201-299, 401-499
 Sides, from STGR10 to STGR23,
 LH/RH
 Detailed Visual Inspection of Skin 643 ALL
 around Anti-Collision Light
 Cutout, between FR40 and FR41 and
 between Stringer 1, LH/RH,
 External Surface
 Detailed Visual Inspection of Skin 647 ALL
 around ADF-1 Antenna Cutout,
 between FR44 and FR45 and between
 Stringer 1, LH/RH, External
 Surface
 Detailed Visual Inspection of 651 ALL
 Pressure Bulkhead FWD Face and the
 53-CONTENTS Page 14 Aug 01/05 R CES


 CHAPTER 53__________
 FUSELAGE
 TABLE OF CONTENTS_________________
 SUBJECT_______  CH/SE/SU________  C_  PAGE EFFECTIVITY____ ___________
 
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