CES
3. Job Set-up
__________
Subtask 53-11-00-020-056
A. Get Access
R (1) Put an access platform at the zone 831 (841).
R R (2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-010-001).
R R (3) Remove the scuff plates (Ref. TASK 53-15-15-000-001) of the forward passenger/crew doors.
Subtask 53-11-00-110-093
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 53-11-00-220-058
R A. Inspection (Ref. Fig. 646/TASK 53-11-00-991-055)
R R R (1) Do a detailed inspection of the structure of the forward passenger/crew door cutout left and right sides . This inspection is applicable below the scuff plate.
EFF : ALL 53-11-00Page A679 Aug 01/03
CES
R R Forward Passenger/Crew Door Cutout below Scuff Plate Figure 646/TASK 53-11-00-991-055
EFF : ALL 53-11-00 Page A680 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.
(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 53-11-00-420-054
A. Close Access
R R (1) Install the scuff plates (Ref. TASK 53-15-15-400-001) of the forward passenger/crew doors.
R R (2) Make sure that the work area is clean and clear of tool(s) and other items.
R R (3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-410-001).
R (4) Remove the access platform(s).
EFF : ALL 53-11-00Page A681 Aug 01/03
CES
TASK 53-11-00-210-035
R R Detailed Inspection of Fuselage Internal Structure and Lower Surface of Cabin Floor Structure, from FR 15 to FR 21, between STRG 23 and STRG 28 LH/RH
1. Reason for the Job__________________
Refer to the MPD TASK: 531181-01
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific adjustable access platform 1.80 m (5 ft. 11 in.)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R No specific Material No. 08-074 Material No. 11-004 Material No. 15-005 Material No. 15-006 Material No. 15-007 Material No. 15-008 Material No. 19-003 masking paper MASKING TAPE (Ref. 20-31-00)USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)AIB TN 10138 TYPE II GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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(73)
