B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 15-008 AIB TN 10138 TYPE II GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-34-24-869-002 Aircraft Grounding for the Maintenance Operations 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 24-92-00-991-006 Fig. 602 24-92-00-991-031 Fig. 625
3. Job Set-up
__________ Subtask 24-92-00-862-062
A. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 24-92-00-869-075
B. Connect the aircraft to the ground (Ref. TASK 12-34-24-869-002). Subtask 24-92-00-010-062
C. Get Access
(1)
Put the adjustable access platform in position at the dry bay.
(2)
For the left wing.
(a) Remove and retain the access panel: 560AB.
1EFF : ALL 1 24-92-00Page 683 1 1 May 01/04R 1 1 1CES 1
(3) For the right wing.
(a) Remove and retain the access panel: 660AB.
4. Procedure
_________ Subtask 24-92-00-210-062
A. Inspection of the End Fittings of Electrical Conduits
(Ref. Fig. 602/TASK 24-92-00-991-006, 625/TASK 24-92-00-991-031)
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.
(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 24-92-00-410-063
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
For the left wing.
(a) Install the access panel: 560AB.
(3)
For the right wing.
(a) Install the access panel: 660AB.
(4)
Disconnect the aircraft from the ground (Ref. TASK 12-34-24-869-002).
1EFF : ALL 1 24-92-00Page 684 1 1 May 01/04R 1 1 1CES 1
Electrical Harness Conduits - Corrosion Protection Figure 625/TASK 24-92-00-991-031
1EFF : 1 1R 1CES ALL 1 11 1 24-92-00 Page 685 May 01/04
(5) Remove the access platform(s).
1EFF : ALL 1 24-92-00Page 686 1 1 May 01/04R 1 1 1CES 1
TASK 24-92-00-210-018
General Visual Inspection of Elements Fitted on the Following Harnesses: 405VB to 409VB (LH side) and 400VB to 404VB (RH side) 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.
1.
Reason for the Job
__________________
Refer to the MPD TASK: 200002-01
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY 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 ELECTRICAL POWER 电源2(163)
