(1)
Do a visual inspection of the fuselage external surface between FR35.4 and FR 35.8. This inspection is applicable from STGR8 to STGR14 and STGR18 to STGR23, left and right sides.
(2)
Make sure that there is no:
(a)
Corrosion damage: If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200 P.Block 001) for types, inspection, removal and corrosion protection.
(b)
Other damage (cracks, scratches, stress, marks, dents, bumps,...): If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100 P.Block 001) for damage classification and corrective action.
Fuselage External Surface between FR35.4 and FR35.8 Figure 629/TASK 53-21-00-991-048
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5. Close-up
________
Subtask 53-21-00-942-083
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
TASK 53-21-00-210-005
General Visual Inspection of Fuselage External Surface, between FR 24 and FR 35, from Stringer 23 LH/RH to bottom Centerline, except Areas Covered...
1. Reason for the Job
__________________
Refer to the MPD TASK: 532165-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.8 m (5 ft. 11 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
SRM 511100 P.Block 001 (for corrective action) SRM 512200 P.Block 001 (for corrective action) 53-21-00-991-049 Fig. 630
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3. Job Set-up
__________
Subtask 53-21-00-941-078
A. Get Access
(1) Put an access platform in position at the zone 130.
Subtask 53-21-00-110-093
B. Cleaning of the Structure
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.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
4. Procedure
_________
Subtask 53-21-00-210-077
A. Inspection
(Ref. Fig. 630/TASK 53-21-00-991-049)
(1) Do a visual inspection of the fuselage external surface between FR24 and FR35, left and right sides. This inspection is applicable from the STGR23 to the bottom centerline left and right sides. It is not applicable to the area below the belly fairing.
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Fuselage External Surface between FR24 and FR35 Figure 630/TASK 53-21-00-991-049
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(2) Make sure that there is no: 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2(19)
