CES CES
3. Job Set-up__________
Subtask 53-11-00-010-080
A. Get Access
R (1) Put an access platform in position at the zone 121(122).
R (2) Open the avionics-compartment door 811 (Ref. TASK 52-41-00-010-002).
R (3) Remove the insulation blankets (Ref. TASK 25-80-00-000-001).
R (4) Move the wiring bundles.
Subtask 53-11-00-110-094
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.
R R R (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 53-11-00-220-060
R A. Inspection (Ref. Fig. 648/TASK 53-11-00-991-057)
R R R (1) Do a detailed inspection of the structure of the aft face of the forward pressure bulkhead. This inspection is applicable above the cockpit floor level as far as you can see, and includes FR1.
R R Aft Face of the Forward Pressure Bulkhead Figure 648/TASK 53-11-00-991-057
EFF : ALL 53-11-00 Page A689 Aug 01/03
CES
(2) Make sure that there is no:
R R (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.
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 53-11-00-410-080
A. Close Access
(1) Put the wiring bundles in position.
(2) Install the insulation blankets (Ref. TASK 25-80-00-400-001).
(3) Make sure that the work area is clean and clear of tool(s) and other items.
R (4) Close the avionics-compartment door 811 (Ref. TASK 52-41-00-410-002).
R (5) Remove the access platform(s).
EFF : ALL 53-11-00Page A690 Aug 01/03
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TASK 53-11-00-210-047
R Detailed Inspection of Cockpit Window Frames and Closing Panels, Internal Structure (FR 12 and Forward)
1. Reason for the Job__________________
Refer to the MPD TASK: 531187-01
2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R R R -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific access platform 1.50 m (4 ft. 11 in.)
R B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 Material No. 19-003 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R 25-13-41-000-001 25-13-41-000-002 Removal of the Ceiling Panels Removal of the Sidewall Panels 中國航空網(wǎng) m.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(75)
