C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R 52-10-00-010-001 52-10-00-410-001 53-12-11-000-001 53-12-11-400-001 SRM 511100 P.Block 001 SRM 512200 P.Block 001 53-11-00-991-060 Opening of the Passenger/Crew Door Closing of the Passenger/Crew DoorRemoval of the Cockpit Floor Panels from FR1 Thru FR12Installation of the Cockpit Floor Panels from FR1 thru FR12(for corrective action)(for corrective action) Fig. 651
3. Job Set-up__________
Subtask 53-11-00-010-082
A. Get Access
R (1) Put an access platform in position at the zone 831 (841).
R R (2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-010-001).
R (3) Remove the floor panels of the cockpit (Ref. TASK 53-12-11-000-001).
R (4) Remove the rubber leveling strips.
Subtask 53-11-00-110-096
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.
EFF : ALL 53-11-00Page A698 Aug 01/03
CES CES
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 53-11-00-220-062
R A. Inspection (Ref. Fig. 651/TASK 53-11-00-991-060)
R R (1) Do a detailed inspection of the structure of the cockpit floor, between FR1 and FR12.
(2) Make sure that there is no:
R 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.
Subtask 53-11-00-916-071
R R B. Application of the Temporary Protection
CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS._______ MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET: -ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS,TEFLON BEARINGS. -ON LUBRICATED SURFACES. -IN DRAIN VALVES OR OTHER ORIFICES. TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE.
R R R (1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) on the equipment and fittings adjacent to the area.
(2) Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to the inspection area.
R (3) Remove the masking tape or the masking paper.
R Cockpit Floor Structure Figure 651/TASK 53-11-00-991-060
EFF : ALL 53-11-00 Page B600 Aug 01/03
CES
5. Close-up
________
Subtask 53-11-00-410-082
A. Close Access
(1) Install the rubber leveling strips.
(2) Install the floor panels of the cockpit (Ref. TASK 53-12-11-400-001).
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).
TASK 53-11-00-210-049
R Detailed Inspection of Cabin Floor Structure between FR 12 and FR 21
1. Reason for the Job__________________
Refer to the MPD TASK: 531189-01
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific access platform 3.5 m (11 ft. 6 in.)
B. Consumable Materials
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(77)
