3. Job Set-up__________
Subtask 24-92-00-862-056
A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 24-92-00-869-063
B. Connect the aircraft to the ground (Ref. TASK 12-34-24-869-002).
Subtask 24-92-00-010-056
C. Get Access
R R R (1) Put the adjustable access platform in position at the wing and the center fuselage.
R (2) For the center fuselage.
R (a) Remove the access panels: 191BB, 191KB, 192FB, 192KB.
R R (b) Open the L and R main landing-gear doors at zone 734 and 744 (Ref. TASK 32-12-00-010-001).
4. Procedure_________
Subtask 24-92-00-210-056
A. Inspection of the End Fittings of Electrical Conduits (Ref. Fig. 602/TASK 24-92-00-991-006, 610/TASK 24-92-00-991-014, 611/TASK 24-92-00-991-015)
WARNING : BE CAREFUL NOT TO CUT YOUR FINGERS. FLAKES OF NICKEL ARE SHARP._______
(1) At each fitting use the procedure that follows to protect against corrosion:
(a) Use CLEANING AGENTS (Material No. 11-004) and a lint-free cloth to remove any contamination from the fitting.
(b) Remove any flakes or blisters, make sure that the you do not damage the base metal while you do this task.
NOTE : A dental or a seal tools are recommended for the removal____ of flakes and blisters.
Electrical Harness Conduits - Corrosion Protection Figure 610/TASK 24-92-00-991-014
R 1EFF : 1 1 1CES ALL 1 111 24-92-00 Page 636 Feb 01/04
INTENTIONALLY BLANK
R 1 1
24-92-00Page 637
1 1 Aug 01/01 1 1 1CES 1
Location of Conduit Fittings Figure 611/TASK 24-92-00-991-015- 12 (SHEET 1)
R 1EFF : 1 1 1CES ALL 1 111 24-92-00 Page 638 Feb 01/04
Location of Conduit Fittings Figure 611/TASK 24-92-00-991-015- 22 (SHEET 2)
R 1EFF : 1 1 1CES ALL 1 111 24-92-00 Page 639 Feb 01/04
(c) Use a brush or an airless spray to apply a continuous coat of STORAGE PRESERVATION (Material No. 15-008) with a thickness of 0.030 mm (0.001 in.), to cover all the fitting.
5. Close-up________
Subtask 24-92-00-410-057
A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) For the center fuselage.
R (a) Install the access panels: 191BB, 191KB, 192FB, 192KB.
R R (b) Close the L and R main landing-gear doors at zone 734 and 744 (Ref. TASK 32-12-00-410-001).
R (3) Disconnect the aircraft from the ground (Ref. TASK 12-34-24-869-002).
R (4) Remove the access platform(s).
TASK 24-92-00-210-008
Inspection of the End Fittings of electrical Conduits in Vertical Stabilizer Trailing-Edge
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND THE CAUTIONS INCLUDED IN
_______ THE REFERENCED PROCEDURES.
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. Reason for the Job
__________________
Refer to the MPD TASK: 240000-13
Apply temporary protection to end fittings of electrical conduits in
vertical stabilizer trailing-edge.
R 1EFF : ALL 1 24-92-00Page 641 1 1 Feb 01/04 1 1 1CES 1
2. Job Set-up Information
______________________
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 ELECTRICAL POWER 電源2(155)
