External Surface from STGR23 LH/RH to Crown Centerline Figure 654/TASK 53-41-00-991-082
R EFF : 001-049, 051-099, 101-149, 201-299, 53-41-00 Page B660 May 01/05
CES
R **ON A/C 151-199, 401-499,
(Ref. Fig. 654A/TASK 53-41-00-991-082-A)
**ON A/C 301-399,
(Ref. Fig. 654B/TASK 53-41-00-991-082-B)
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 53-41-00-210-125
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
-the external surface of the fuselage between FR47 and FR 70 from STGR 23LH to the crown centerline and from STGR 23RH to the crown centerline.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for
____
the correct repair procedure.
R **ON A/C 151-199, 401-499,
Subtask 53-41-00-210-125-A
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
-the external surface of the fuselage between FR47/51 and FR 70 from STGR 23LH to the crown centerline and from STGR 23RH to the crown centerline.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for
____
the correct repair procedure.
External Surface from STGR23 LH/RH to Crown Centerline Figure 654A/TASK 53-41-00-991-082-A
R EFF : 151-199, 401-499, 53-41-00 Page B662 Aug 01/05
CES
External Surface from STGR23 LH/RH to Crown Centerline Figure 654B/TASK 53-41-00-991-082-B
R EFF : 301-399, 53-41-00 Page B663 Nov 01/04
CES
**ON A/C ALL
5. Close-up
________ Subtask 53-41-00-942-102
A. Remove the ground support equipment.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
EFF : ALL 53-41-00Page B664
Nov 01/04
R
CES TASK 53-41-00-210-824
General Visual Inspection of the Fuselage Internal Structure, From FR 47 to FR 70, above the Cabin Floor Level
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific lint-free cloth
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
25-23-41-000-001 Removal of the Ceiling Panels 25-23-41-400-001 Installation of the Ceiling Panels 25-23-42-000-001 Removal of the Ceiling Panels - Forward Utility Area 25-23-42-400-001 Installation of the Ceiling Panels - Forward Utility
Area 25-23-43-000-001 Removal of the Upper Sidewall Panel(s) 25-23-43-400-001 Installation of the Upper Sidewall Panel(s) 25-23-44-000-001 Removal of the Lower Sidewall-Panels (Dado Panels) 25-23-44-400-001 Installation of the Lower Sidewall-Panels (Dado
Panels) 25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew Doors
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-46-400-002 Installation of the Door Linings at the AFT
Passenger/Crew Doors 25-23-47-000-001 Removal of the Lining from the Emergency Exit Hatches 25-23-47-400-001 Installation of the Lining on the Emergency Exit
Hatches 25-24-41-000-001 Removal of the Overhead Stowage Compartments 25-24-41-400-001 Installation of the Overhead Stowage Compartments 25-33-41-000-001 Removal of the AFT Galley Unit (6480MM) 25-33-41-000-002 Removal of the AFT Galley Unit (6481MM or 6483MM) 25-33-41-400-001 Installation of the AFT Galley Unit (6480MM) 25-33-41-400-002 Installation of the AFT Galley Unit (6481MM or
中國航空網 m.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3(47)
