CHAPTER 53
__________
FUSELAGE
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Detailed Inspection of Forward 614 ALL Face of Pressure Bulkhead, Vertical Angle (Y=675) at Crossing Areas with Horizontal Stiffeners (Z=1 and Z=1329), LH/RH General Visual Inspection of 618 ALL Avionics Compartment Doors, Surround Corners, External Surface (4 Doors) General Visual Inspection of 623 ALL Fuselage Side Panel, below Cockpit Side Windows, between FR 1 and FR 12, External Surface, LH/RH General Visual Inspection of Area 627 ALL Forward of Windshield, above Side Panel, from FR 0 to FR 4, External Surface, LH/RH Detailed Inspection of Fuselage 631 ALL Lower Panel at NLG Bay Aft Corners, External Surface, LH/RH Detailed Inspection of Fuselage 635 ALL Skin above Windshield, between FR 4 and FR 12, External Surface, LH/RH Detailed Inspection of Upper Skin 639 ALL of Lower Longitudinal Lap Joint, between FR 9 and FR 20, External Surface, LH/RH Detailed Inspection of Upper Skin 643 ALL of Upper Longitudinal Lap Joint, between FR 15 and FR 16 and FR 20 and FR 24, External Surface, LH/RH Detailed Inspection of Outer Skin 647 ALL of Lateral Longitudinal Lap Joint, between FR 11 and FR 14 and FR 20 and FR 24, LH/RH Detailed Inspection of Outer Skin 651 ALL of Lateral Longitudinal Lap Joint, between FR 1 and FR 24, LH/RH Detailed Inspection of FR 20 655 ALL Splice, between Stringer 30 and Stringer 32, LH/RH Special Detailed Inspection of 659 001-049, 051-099 Sliding Window Frame at FR4 Lower 101-149, 201-299 Forward Corners, Internal Side, LH/RH
53-CONTENTS Page 2 May 01/05 R CES
CHAPTER 53
__________
FUSELAGE
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Detailed Inspection of Windshield 663 ALL Center Post, Upper Attachment Area, Internal Side Detailed Inspection of Windshield 667 001-049, 051-099 Side Post at FR 4, Lower 101-105, 201-207 Attachment, Internal Side, LH/RH Special Detailed Inspection of 672 001-049, 051-099 Windshield Side Post at FR 4, 101-105, 151-154 Lower Attachment, Internal Side, 201-207, LH/RH Special Detailed Inspection of 677 ALL Windshield Side Post at Frame 4, Upper Attachment, Internal Side, LH/RH Detailed Inspection of Side Window 685 ALL Structure, Upper Junction, between Forward and Rear FR, External Surface, LH/RH Detailed Inspection of Door Stop 689 ALL Fittings on FR 16 and FR 20, LH/RH Special Detailed Inspection of 693 ALL Door Frame 16, at Double Joggle Area in Outer Flange of Frame at Door Stops Number 1 and 7 Location, LH/RH Special Detailed Inspection of A600 ALL Door FR 20, at Double Joggle Area in Outer Flange of FR, at Door Stops Number 1 and 7 Location, LH/RH Detailed Inspection of Continuity A607 ALL Fitting between FR 20 and FR 21, and Angle Fitting, Both Sides of FR 21, at Stringer 41 Location, LH/RH General Visual Inspection of NLG A613 ALL Bay, all Panels, LH/RH Detailed Inspection of NLG Bay, A617 ALL Rear Panel Aft Face, Lower Corners, LH/RH Detailed Inspection of Internal A622 ALL Structure around Forward Passenger/Crew Door above Cabin Floor Level, between FR 15 and FR 21 and between Stringer 8 and... Detailed Inspection of Fuselage A628 ALL
53-CONTENTS Page 3 May 01/05 R CES
CHAPTER 53__________
FUSELAGE
TABLE OF CONTENTS_________________
SUBJECT_______ CH/SE/SU________ C_ PAGE EFFECTIVITY____ ___________
Internal Structure, below Forward
Passenger/ Crew Doors and Cabin
Floor Level, from FR 15 to FR 21
and between Stringer ...
Detailed Inspection of Fuselage A633 ALL
Internal Structure, below
Batteries, between FR 10 and FR
16, RH
General Visual Inspection of A639 ALL
Fuselage Internal Structure below
Galley and Toilet, between FR12
and FR15 and between STRG 23 LH
and STRG 23 RH
Detailed Inspection of Cockpit A644 ALL
Windshield, Lower Front Fitting at
FR 4, Lower Attachment, External
Surface, LH/RH
Special Detailed Inspection of A648 ALL
Cockpit Windshield, Lower Front
Fitting at FR 4, Lower Attachment,
External Surface, LH/RH
Detailed Inspection of NLG, A653 ALL
Secondary Door Hinge Supports on
Fuselage, LH/RH
Detailed Inspection of Fuselage A657 ALL
Skin, between FR 21 and FR 23 LH
and FR 17 and FR 18 RH, from
Stringer 31 to Stringer 36
Detailed Inspection of Forward A662 ALL
Face of Front Pressure Bulkhead
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身1(18)
