CES
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 
 CES 
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). 
CES
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
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  access platform 3.50 m (11 ft. 6 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)
R  EFF : 001-049, 051-099, 101-149, 201-299, 53-21-00Page 621 301-399, May 01/05
 CES  CES
 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). 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:A320飞机维护手册 AMM FUSELAGE 机身1(137)