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) R 53-11-00-991-016 Fig. 623
EFF : ALL
53-11-00Page 685
3. Job Set-up
__________
Subtask 53-11-00-941-063
A. Get Access
(1) Put an access platform in position at the zone 211 (212).
Subtask 53-11-00-110-072
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.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
4. Procedure
_________
Subtask 53-11-00-220-080
A. Inspection
(Ref. Fig. 623/TASK 53-11-00-991-016)
(1) Do a detailed inspection of the structure of the external surface of
the upper junction of the side windows. This inspection is applicable R forward and aft of the frame, 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.
EFF : ALL
53-11-00Page 686
R External Surface of the Upper Junction of the Side Window Stucture - Forward R and Aft of the Frame R Figure 623/TASK 53-11-00-991-016
EFF : ALL
53-11-00Page 687
May 01/03
CES EFF : ALL
R R R (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 53-11-00-942-063
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).
53-11-00Page 688
TASK 53-11-00-210-017
R Detailed Inspection of Door Stop Fittings on FR 16 and FR 20, LH/RH
1. Reason for the Job
__________________
Refer to the MPD TASK: 531151-01
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)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
25-23-45-000-002 Removal of the Door Frame Linings at the Right FWD Passenger/Crew Door 25-23-45-000-005 Removal of the Door Frame Linings at the Left FWD Passenger/Crew Door 25-23-45-400-006 Installation of the Door Frame Linings at the Left FWD Passenger/Crew Door 25-23-45-400-007 Installation of the Door Frame Linings at the Right
FWD Passenger/Crew Door
52-10-00-010-001 Opening of the Passenger/Crew Door
52-10-00-410-001 Closing of the Passenger/Crew Door
SRM 511100 P.Block 001 (for corrective action)
EFF : ALL
53-11-00Page 689
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
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(54)
