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R R Scuff plates of the FWD Emergency Exit Figure 604/TASK 53-21-00-991-023
R EFF : 301-399, 53-21-00 Page 619 May 01/04
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R (2) Make sure that there is no:
R (a) Corrosion damage:
R - If you find corrosion damage, refer to the Structural Repair
R Manual (Ref. SRM 512200 P.Block 001) for types of corrosion,
R inspection, removal and corrosion protection.
R (b) Other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up________
R Subtask 53-21-00-410-061
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the scuff-plates under the forward emergency exit (Ref. TASK
R 53-25-41-400-001) (left and right sides).
R (3) Close the forward emergency exit 833 (843) (Ref. TASK 52-22-00-410-
R 002).
R (4) Remove the access platform(s).
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R **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
TASK 53-21-00-200-001
Detailed Inspection of Frame Webs at Stringer 18 LH/RH for: FR25, 26, 27, 28, 32, 33, 34
1.
Reason for the Job
__________________
Refer to the MPD TASK: 532120-01
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
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No specific access platform 3.50 m (11 ft. 6 in.)
B. Consumable Materials
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REFERENCE DESIGNATION
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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)
R EFF : 001-049, 051-099, 101-149, 201-299, 53-21-00Page 621 301-399, May 01/05
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C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-43-000-001 25-23-43-400-001 25-23-44-000-001 25-23-44-400-001 25-23-48-000-001 25-23-48-400-001 52-10-00-010-001 52-10-00-410-001 SRM 511100 P.Block 001 SRM 512200 P.Block 001 Removal of the Upper Sidewall Panel(s)Installation of the Upper Sidewall Panel(s)Removal of the Lower Sidewall-Panels (Dado Panels)Installation of the Lower Sidewall-Panels (Dado Panels)Removal of the Cove Light PanelsInstallation of the Cove Light PanelsOpening of the Passenger/Crew DoorClosing of the Passenger/Crew Door(for corrective action)(for corrective action)
R **ON A/C 001-049, 051-099, 101-149, 201-299,
R 53-21-00-991-001 Fig. 605
**ON A/C 301-399,
53-21-00-991-001-B Fig. 605B
R **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
3. Job Set-up__________
R **ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 53-21-00-010-050
A. Get Access
(1) Put an access platform in position at the zone 831 (841).
(2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-010-001).
(3) Remove the linings and the insulation panels between FR21 and FR36 in the zone 231 (232) at the STGR18: 231DW, 231EW, 231FW, 231GW, 231HW, 231JW, 231KW, 231LW, 231MW, 231NW, 231PW, 231QW, 231RW, 231SW, 231TW, 231UW, 231VW, 231WW, 231XW, 231YW, 232DW, 232EW, 232FW, 232GW, 232HW, 232JW, 232KW, 232LW, 232MW, 232NW, 232PW, 232QW, 232RW, 232SW, 232TW, 232UW, 232VW, 232WW, 232XW, 232YW, (Ref. TASK 25-23-43-000-001), (Ref. TASK 25-23-44-000-001), (Ref. TASK 25-23-48-000-001). 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(137)
