53-CONTENTS Page 20 Aug 01/05 R CES
CHAPTER 53__________
FUSELAGE
TABLE OF CONTENTS_________________
SUBJECT_______ CH/SE/SU________ C_ PAGE EFFECTIVITY____ ___________
Passenger/Crew Door above Cabin Floor between FR65 and FR69 and from STGR6 to STGR23, LH/RH Detailed Visual Inspection of 610 ALL Fuselage Internal Structure around AFT Cargo Door Cutout from FR52 to FR57 and between STGR23 and STGR38 Detailed Visual Inspection of 615 ALL Fuselage Structure at Internal Attachment Area of AFT Cargo Door Hinge Fittings from FR52 to FR57 between STGR22 and STGR23 Detailed Visual Inspection of 621 ALL Fuselage AFT Cargo Door Hinge Fittings and External Attachment Area Detailed Visual Inspection of 626 001-049, 051-099 Fuselage Skin under Bulk Cargo 101-149, 221-221 Door Scuff Plate 224-224, 228-228 Special Detailed Inspection of 629 001-049, 051-099 Fuselage Skin of Bulk Cargo Door 101-149, 221-221 Cutout and Sealing Profile at 224-224, 228-228 Upper Corners Detailed Visual Inspection of 634 ALL Lower Skin of Longitudinal Lap Joints in Crack Stopper Areas at Stringer 32 LH between FR47 and FR53, External Surface Detailed Visual Inspection of AFT 641 ALL Passengers/Crew Door Cutout Upper Corners including Skin and Internally the Visible Portion of the Internal Doubler Detailed Visual Inspection of 645 ALL Frame Splices and Adjacent Area from FR53 to FR56 located above Stringer 18 RH Detailed Visual Inspection of AFT 649 ALL Cargo Door Lock Fittings and Surrounding Structure between FR53 and FR55A from Stringer 41 RH to Door Sill (6 places) Detailed Visual Inspection of 655 ALL Fuselage Internal Structure between FR46 and FR65 including AFT Face of Pressure Bulkhead from
53-CONTENTS Page 21 Aug 01/05 R CES
CHAPTER 53__________
FUSELAGE
TABLE OF CONTENTS_________________
SUBJECT_______ CH/SE/SU________ C_ PAGE EFFECTIVITY____ ___________
STGR 38 LH/RH to Bottom CenterLine Detailed Visual Inspection of 660 ALL Visible Part of Windows Forgings between FR47 and FR65 LH/RH, External Surface Detailed Visual Inspection of Skin 664 ALL in Circumferential Splice at FR70 between STGR10 LH/RH and Crown Center Line, including Cutout Corners for Fin Detailed Visual Inspection of Skin 668 ALL around VHF-3 Antenna Cutout between FR52 and FR53 and between Stringer 1 LH/RH, External Surface Detailed Visual Inspection of Skin 672 ALL in Circumferential Splice and Stringer Coupling Areas at FR64, from STGR10, LH/RH, to Crown Center Line Detailed Visual Inspection of AFT 675 ALL Passenger/Crew Door Cutout Lower Corners including Skin and Doubler underneath the Scuff Plate, LH/RH Detailed Visual Inspection of AFT 678 ALL Cargo Door Eccentric Bolts of Locking Mechanism at Lock Fittings between FR53 and FR55A (6 places) Detailed Visual Inspection of Bulk 681 001-049, 051-099 Cargo Door Stop Fittings and 101-149, 221-221 Back-up Structure at FR60 and FR62 224-224, 228-228 (10 places) Detailed Visual Inspection of 686 ALL Lower Skin of Longitudinal Lap Joints in Crack Stopper Areas at Stringer 6 LH/RH between FR47 and FR70, External Surface Detailed Visual Inspection of 689 001-049, 051-099 Fuselage Internal Structure around 101-149, 221-221 Bulk Cargo Door Cutout from FR59 224-224, 228-228 to FR63 and between STGR23 and STGR38 Detailed Visual Inspection of Door 693 ALL Stop Fittings on FR66 and FR68, LH/RH Detailed Visual Inspection of 697 ALL Fuselage Internal Structure, Below
53-CONTENTS Page 22 Aug 01/05 R CES
CHAPTER 53__________
FUSELAGE
TABLE OF CONTENTS_________________
SUBJECT_______ CH/SE/SU________ C_ PAGE EFFECTIVITY____ ___________
Cabin Floor Panels Including Floor
Structure from FR65 to FR70
Detailed Visual Inspection of AFT A602 ALL
Cargo Door Cutout Upper and Lower
Corners, External Surface
Detailed Visual Inspection of A606 ALL
Upper Segment of FR70, Fin to
Fuselage FWD Attach Fittings and
Area between FR69 and FR70 from
STGR6 LH/RH to Crown Center Line
Detailed Visual Inspection of A610 ALL
Cabin Floor Structure, below and
0.5m around Galleys and Toilets,
from FR47/54 (318), FR47/51 (319),
FR47 (320/321) to FR70
General Visual Inspection of AFT A617 ALL
Cargo Door Lock Fittings and
Surrounding Structure, External
Portion (6 places)
Detailed Visual Inspection of Aft A621 ALL
Passenger/Crew Door Cutout,
underneath the scuff-Plate, LH/RH
Detailed Visual Inspection of Skin A625 301-399,
in Circumferential Splice and
Stringer Coupling areas at FR47.5
from Stringer 16 LH/RH to Crown
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FUSELAGE 机身1(25)
