(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,...):
R R Cockpit Windshield - Lower Front Fitting at FR4 Figure 637/TASK 53-11-00-991-050
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-If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100 P.Block 001) for damage classification and corrective action.
5. Close-up
________ Subtask 53-11-00-420-051
A. Close Access
(1)
Install the lower retainers (Ref. TASK 56-11-11-400-001).
(2)
Make sure that the inspection area is clean and clear of tools and other items.
(3)
Remove the access platform.
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R
CES
TASK 53-11-00-210-039
Special Detailed Inspection of Cockpit Windshield, Lower Front Fitting at FR 4, Lower Attachment, External Surface, LH/RH
1. Reason for the Job
__________________
Refer to the MPD TASK: 531170-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific non metallic scraper
No specific access platform 4.5 m (14 ft. 9 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 -------------------------------------------------------------------------------
56-11-11-000-001 Removal of the Windshield
56-11-11-400-001 Installation of the Windshield
NTM 531170,P.Block-601
SRM 511100,P.Block 001 (for corrective action)
SRM 512200,P.Block 001 (for corrective action)
R 53-11-00-991-076 Fig. 638
3. Job Set-up
__________
Subtask 53-11-00-020-054
A. Get Access
(1)
Put an access platform in position at the zone 210 in front of the windshield.
(2)
Remove the lower retainers (Ref. TASK 56-11-11-000-001).
Subtask 53-11-00-110-087
B. Preparation of the Inspection Area R (Ref. Fig. 638/TASK 53-11-00-991-076)
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)
Remove the sealant from the inspection area with a non metallic scraper.
(2)
Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
(3)
Make sure that the surface of the inspection area is clean and smooth.
(4)
Do a visual check of the inspection area for damage or discontinuities.
(5)
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...):
R Cockpit Windshield - Lower Front Fitting at FR4 Figure 638/TASK 53-11-00-991-076
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CES
-If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) for damage classification and corrective action. 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(67)
