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时间:2011-03-27 08:44来源:蓝天飞行翻译 作者:admin
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 53-CONTENTS Page 6 May 01/05 R CES


 CHAPTER 53
__________
 FUSELAGE
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Installation of the Radome Seal 450 ALL Removal of the Seal at Frame 1 454 ALL Installation of the Seal at Frame 457 ALL 1
 RADOME 53-15-11
 ADJUSTMENT/TEST 501 ALL
 Tap Test of the Radome 501 ALL
 RADOME 53-15-11
 INSPECTION/CHECK 601 ALL
 Detailed Inspection of the Radome 601 ALL
 RADOME 53-15-11
 REPAIRS 801 ALL
 Temporary Repair of the Radome 801 ALL
 SCUFF PLATES - DOOR ENTRANCE 53-15-15

 REMOVAL/INSTALLATION 401 ALL
 Removal of the FWD Passenger/Crew 401 ALL
 Door Scuff Plates
 Installation of the FWD 404 ALL
 Passenger/Crew Door Scuff Plates

 MOUNT FITTING - CABIN 53-16-11
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Mount Fitting at FR 401 ALL
 14
 Installation of the Mount Fitting 405 ALL
 at FR 14

 MISCELLANEOUS (EG : DRAINS) 53-19-00
 DESCRIPTION AND OPERATION 1 ALL
 General 1 ALL
 Description 1 ALL

 MISCELLANEOUS (EG : DRAINS) 53-19-00
 INSPECTION/CHECK 601 ALL Inspection of the Cockpit Grid 601 001-049, 054-099 Collector Assy 101-149, 151-199
 201-299, 301-399
 401-499, Operational Check of the Cockpit 605 001-049, 054-099 Drainage Pipe 101-149, 151-199
 201-299, 301-399
 401-499, Operational Check of Piston Type 609 ALL Drain Valves in Lower Fuselage Shell from Outside
 DRAINS - NOSE FORWARD FUSELAGE 53-19-41
 53-CONTENTS Page 7 Aug 01/05 R CES


 CHAPTER 53
__________
 FUSELAGE
 TABLE OF CONTENTS
_________________
 SUBJECT_______  CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________
 REMOVAL/INSTALLATION 401 ALL Removal of the Collector Grid and 401 001-049, 054-099 the Container 101-149, 151-199
 201-299, 301-399
 401-499, Installation of the Collector Grid 405 001-049, 054-099 and the Container 101-149, 151-199
 201-299, 301-399
 401-499, Removal of the Drain Valves 409 ALL Installation of the Drain Valves 413 ALL
 BLANKING PLATE - STATIC PORT  53-19-42
 REMOVAL/INSTALLATION 401  106-149, 154-199 207-299, 301-399 401-499,
 Removal of the Static Port 401 106-149, 154-199 Blanking-Plate 207-299, 301-399
 401-499, Installation of the Static Port 404 106-149, 154-199 Blanking-Plate 207-299, 301-399
 401-499,
 FORWARD FUSELAGE  53-20-00
________________ DESCRIPTION AND OPERATION 1 ALL General 1 ALL
 Location 1  001-049, 051-099 101-149, 151-199 201-299, 401-499
 Location 1  301-399,
 Description 7 ALL Frames 7 ALL Stringers 8 ALL Skin 8 001-049, 051-099
 101-149, 151-199
 201-299, 401-499 Skin 11 301-399, Cabin Floor Structure 11 ALL Structure of Cargo Compartment 19 ALL Floor Cabin Windows 19 ALL Cargo Door Frame 19 ALL
 MAIN STRUCTURE  53-21-00
 INSPECTION/CHECK 601 ALL
 Detailed Inspection of Internal 601 301-399,
 Structure around Forward Emergency

 53-CONTENTS Page 8 Aug 01/05 R CES


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

 Exit Cutouts, between FR 35 and FR
 35.3 from Stringer 23 LH to Stringer 7 LH... Detailed Inspection of Door Stop 608 301-399, Fittings on FR 35.1 and FR 35.2A, LH/RH Detailed Inspection of Escape 612 301-399, Chute Slide Compartment, Internal Structure, between FR 35.1 and FR 35.2A, from Stringer 24 to Stringer 28, LH/RH Detailed Inspection of Forward 617 301-399, Emergency Exit Cutout Underneath the Scuff-plate, LH/RH Detailed Inspection of Frame Webs 621 001-049, 051-099 at Stringer 18 LH/RH for: FR25, 101-149, 201-299 26, 27, 28, 32, 33, 34 301-399, Detailed Inspection of Frame Webs 629 151-199, 401-499 at Stringer 18 LH/RH for: FR25, 26, 27, 28, 29, 30, 34 Detailed Inspection of FR 24 633 ALL Junction with Cabin Floor Beam at Stringer 23, Internal Side, RH Detailed Inspection of Fuselage 638 ALL Forward Cargo Door Hinge Fitting and External Attachment Area Detailed Inspection of Forward 644 ALL Cargo Door Cutout Panels, Upper and Lower Corners, External Surface Detailed Inspection of Forward 649 ALL Cargo Door Eccentric Bolts of Locking Mechanism at Lock Fittings, between FR 25 and FR 27A Detailed Inspection of 653 ALL Circumferential Joint at FR 24, between Stringer 6 LH and Stringer 6 RH, Internal Side Special Detailed Inspection of 657 ALL Circumferential Joint at FR 35, between Stringer 10 LH and Stringer 10 RH, External Side General Visual Inspection of 662 ALL Fuselage External Surface around Water Drain Panel Cutout, between FR 25 and FR 29 at Stringer 43 LH
 
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