May 01/05
R
 CES  3. Job Set-up

__________
 Subtask 53-21-00-941-074
 A. Get Access
 (1) Put an access platform in position at the zone 231 (232).
 Subtask 53-21-00-110-083
 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 a CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
 4. Procedure
_________
 Subtask 53-21-00-220-076
 A. Inspection
 (Ref. Fig. 634/TASK 53-21-00-991-036)

 (1) Do a detailed inspection of:
 -
the fuselage skin

 -
the part of the window forging doublers that you can see around the cabin windows.

 -this inspection is applicable to the external surface from FR35.3 to FR35.8, between STGR14 and STGR18, left and right sides.
 EFF : 301-399, 53-21-00Page A684

May 01/05
R
 CES

 Fuselage Skin and the Window Forging Doublers around the Cabin Windows, Left and Right Sides Figure 634/TASK 53-21-00-991-036
 EFF : 301-399, 53-21-00Page A685 May 01/05 R CES

 (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 of corrosion, 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.
 5. Close-up
________
 Subtask 53-21-00-942-079
 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).

 EFF : 301-399, 53-21-00Page A686

May 01/05
R
 CES

 TASK 53-21-00-220-006

 Detailed Inspection of FR 35.1 and FR 35.2A Web and Door Stop Intercostals, at Junction Area, between Door Stop No1 and No8 (LH)/No6 (RH), LH/RH
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 532115-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  access platform 3.5 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)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-47-000-004 Removal of the Door Frame Linings of the LH FWD Emergency Exit Door, zone 231 25-23-47-000-009 Removal of the Door Frame Linings of the RH FWD Emergency Exit Door, zone 232 25-23-47-400-004 Installation of the Door Frame Linings of the LH FWD Emergency Exit Door, zone 231 25-23-47-400-009 Installation of the Door Frame Linings of the RH FWD
 Emergency Exit Door, zone 232 52-22-00-010-002 Opening of the Emergency Exit Doors from the Outside 52-22-00-410-002 Closing of the Emergency Exit Doors from the Outside  -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

SRM 511100 P.Block 001 (for corrective action) SRM 512200 P.Block 001 (for corrective action) 53-21-00-991-037 Fig. 635
　
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2(23)