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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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 MAIN STRUCTURE 53-31-00
 CLEANING/PAINTING 701 ALL
 Apply Type I Grade 2 or 3 701 ALL
 Temporary Protection to Pressure
 Bulkhead AFT Face at FR35 and
 Bottom Surface of Pressure Deck
 between FR35 and FR36.
 Apply Type I Grade 2 or 3 706 ALL
 Temporary Protection to fuselage
 internal structure below cabin
 floor panels, including cabin
 floor structure between FR36 and
 FR46
 53-CONTENTS Page 17 Aug 01/05 R CES


 CHAPTER 53
__________
 FUSELAGE
 TABLE OF CONTENTS
_________________
 SUBJECT_______  CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________
 FLOOR PANELS 53-32-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Cabin Floor Panels 1 001-049, 051-099 101-149, 151-199 201-299, 401-499 Cabin Floor Panels 1 301-399, Door Threshold Heater Panels 1 301-399, Description and Operation 1 ALL Cabin Floor Panels 1 001-049, 051-099 101-149, 151-199 201-299, 401-499 Cabin Floor Panels 2 301-399, Door Threshold Heater Panels 2 301-399, PANELS - CABIN FLOOR 53-32-12 REMOVAL/INSTALLATION 401 ALL Removal of the Cabin Floor Panels 401 ALL Installation of the Cabin Floor 406 ALL Panels
 SUPPORT STRUTS 53-33-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Description 1 ALL Support Struts 1 ALL Floor Support Struts 1 ALL
 FAIRINGS 53-35-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Description 1 ALL
 FAIRINGS  53-35-00
 INSPECTION/CHECK 601 ALL
 Inspection of the Wing to Fuselage 601 ALL
 Fairings and Belly Fairing Access
 Panels for Missing Fasteners
 Inspection of the Vanes of the 619 ALL
 Belly-Fairing Louver-Panels

 Refer to the CDL TASK: TBD 619 ALL
 FAIRINGS - WING TO FUSELAGE 53-35-11
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Wing-to-Fuselage 401 ALL

 53-CONTENTS Page 18 Aug 01/05 R CES


 CHAPTER 53
__________
 FUSELAGE
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Fairings Installation of the 429 ALL Wing-to-Fuselage Fairings
 FAIRINGS - COOLING AIR INLET 53-35-12
 REMOVAL/INSTALLATION 401 ALL Removal of the Belly Fairing 401 ALL Blowout Panel Installation of the Belly Fairing 406 ALL Blowout Panel
 ACCESS PANELS 53-35-13
 REMOVAL/INSTALLATION 401 ALL Removal of the Belly Fairing 401 ALL Access Panels Installation of the Belly Fairing 414 ALL Access Panels Removal of the Quick-Release 428 ALL Access Panels from the Belly Fairing Structure Installation of the Quick-Release 441 ALL Access Panels on the Belly Fairing Structure Removal of the Louver Panel -447 ALL Panel 147FB (148FB) Installation of the Louver Panel -450 ALL Panel 147FB (148FB)
 FITTINGS 53-36-00
 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Description 1 ALL
 MISCELLANEOUS (EG : DRAINS) 53-39-00 DESCRIPTION AND OPERATION 1 ALL
 General 1 ALL Drain Assemblies 1 ALL Overpressure Valves 1 ALL
 Component Location 1 ALL Description 1 ALL
 MISCELLANEOUS (EG : DRAINS) 53-39-00
 INSPECTION/CHECK 601 ALL Operational Check of Rubber Flap 601 ALL Drain Valve Holes in Pressure Floor from MLG Bay
 VALVE - OVERPRESSURE 53-39-41
 53-CONTENTS Page 19 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 Overpressure Valve 401 ALL Installation of the Overpressure 404 ALL Valve
 REAR FUSELAGE 53-40-00
_____________ DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 2 ALL Description 3 ALL Rear Fuselage Main Structure 3 ALL Cargo Compartments 3 001-049, 051-099 101-149, 221-221 224-224, 228-228 Cargo Compartments 3 151-199, 201-220 222-223, 225-227 229-299, 301-399 401-499, Dorsal Fin 7 ALL Drains 7 ALL
 MAIN STRUCTURE 53-41-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Description 1 ALL Skin Plates 1 ALL Frames 1 ALL Stringers and Skin Stiffeners 1 ALL Crossbeams 1 ALL Top Beams and Seat Tracks 1 ALL Floor Panels 4 ALL Junction Rear-Fuselage/Cone 4 ALL Rear-Fuselage Fittings 4 ALL
 MAIN STRUCTURE 53-41-00
 INSPECTION/CHECK 601 ALL
 Detailed Visual Inspection of Skin 601 ALL
 around ADF-2 Antenna Cutout
 between FR48 and FR49 and between
 Stringers 1 LH/RH, External
 Surface (Optional)
 Detailed Visual Inspection of 605 ALL
 Internal Structure around AFT
 
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