**ON A/C 001-049, 051-099, 101-149, 201-299,
53-41-00-991-083 Fig. 655
R **ON A/C 151-199, 401-499,
53-41-00-991-083-A Fig. 655A
**ON A/C 301-399,
53-41-00-991-083-B Fig. 655B **ON A/C ALL
3. Job Set-up
__________
Subtask 53-41-00-010-159
A. Get Access
(1)
Remove the AFT Galley (Ref. TASK 25-33-41-000-001) or (Ref. TASK 25-33-41-000-002) or (Ref. TASK 25-33-45-000-001).
(2)
Remove the AFT Lavatories (Ref. TASK 25-43-41-000-001) and/or (Ref. TASK 25-43-42-000-001) and/or (Ref. TASK 25-43-43-000-001) and or (Ref. TASK 25-43-44-000-001).
(3)
Remove the Overhead Stowage Compartments (Ref. TASK 25-24-41-000-001).
(4)
Remove the linings (Ref. TASK 25-23-41-000-001), (Ref. TASK 25-23-42-000-001), (Ref. TASK 25-23-43-000-001), (Ref. TASK 25-23-44-000-001), (Ref. TASK 25-23-46-000-002) and (Ref. TASK 25-23-47-000-001).
(5)
Remove the insulation blankets (Ref. TASK 25-80-00-000-001).
Subtask 53-41-00-110-107
B. Clean the inspection area with CLEANING AGENTS (Material No. 11-003) and a lint-free cloth.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 655/TASK 53-41-00-991-083) R **ON A/C 151-199, 401-499,
(Ref. Fig. 655A/TASK 53-41-00-991-083-A)
**ON A/C 301-399,
(Ref. Fig. 655B/TASK 53-41-00-991-083-B)
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 53-41-00-210-126
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
-the internal structure of the fuselage between FR47 and FR 70 above the cabin floor level.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-12-101) and
____ (Ref. ASRM 53-41-13-101) for the allowable damage limits.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-12-201) and
____ (Ref. ASRM 53-41-13-201) for the correct repair procedure.
R **ON A/C 151-199, 401-499,
Subtask 53-41-00-210-126-A
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
-the internal structure of the fuselage between FR47/51 and FR 70 above the cabin floor level.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-12-101) and
____ (Ref. ASRM 53-41-13-101) for the allowable damage limits.
Internal Structure above Cabin Floor Figure 655/TASK 53-41-00-991-083
R EFF : 001-049, 051-099, 101-149, 201-299, 53-41-00 Page B669 May 01/05
CES
Internal Structure above Cabin Floor Figure 655A/TASK 53-41-00-991-083-A
R EFF : 151-199, 401-499, 53-41-00 Page B670 Aug 01/05
CES
Internal Structure above Cabin Floor Figure 655B/TASK 53-41-00-991-083-B
R EFF : 301-399, 53-41-00 Page B671 Nov 01/04
CES
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-12-201) and
____ (Ref. ASRM 53-41-13-201) for the correct repair procedure.
**ON A/C ALL
5. Close-up
________ Subtask 53-41-00-410-156
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本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身3(48)
