(c)
Disconnect the water injector connector (57).
(d)
Put blanking plugs on the disconnected line ends.
(e)
Disconnect the electrical connector (58).
(f)
Put blanking caps on the disconnected electrical connectors.
(g)
Remove the bolts (30), the washers (31), the clamps (32) and the spacers (33).
(h)
Remove the bolts (34), the washers (31), the clamps (32) and (35) and the spacers (36).
(i)
Remove the nut (13), the washer (14), the clamp (15), the spacer
(16) and the screw (17).
(j)
Temporarily attach the disconnected electrical cable (39) to the aircraft structure.
(k)
Remove the nut (27), the washer (26), the bolt (24) and disconnect the support rod (38).
(l)
Hold the air inlet (3).
(m)
Remove the nut (21), the washer (20), the bolt (18) and disconnect the support rod (19).
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Air Inlet - Component Location Figure 403/TASK 21-61-51-991-004- 13 (SHEET 1)
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Air Inlet - Component Location Figure 403/TASK 21-61-51-991-004- 23 (SHEET 2)
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Air Inlet - Component Location Figure 403/TASK 21-61-51-991-004- 33 (SHEET 3)
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PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
(n)
Remove the nuts (27), the washers (26), the bolts (24) and disconnect the support rods (25) and (29).
(o)
Remove the screws (2), the washers (1) and the air inlet (3).
(p)
Put protective covers on the open ends of the bellows (5) and the air inlet (3).
(2) For the Right air inlet
(a)
Remove the clamp (4) and disconnect the bellows (5).
(b)
Remove the quick-release pins (10) and (44) and the cross beam (8).
(c)
Disconnect the water injector connector (57).
(d)
Put blanking plugs on the disconnected line ends.
(e)
Disconnect the electrical connector (58).
(f)
Put blanking plugs on the disconnected line ends.
(g)
Remove the bolts (30), the washers (31), the clamps (32) and the spacers (33).
(h)
Remove the bolts (34), the washers (31), the clamps (32) and (35) and the spacers (36).
(i)
Remove the nut (13), the washer (14), the clamp (15), the spacer
(16) and the screw (17).
(j)
Temporarily attach the disconnected electrical cable (55) to the aircraft structure.
(k)
Remove the nut (27), the washer (26), the bolt (24) and disconnect the support rod (40).
(l)
Hold the air inlet (6).
(m)
Remove the nuts (27), the washers (26), the bolts (24) and disconnect the support rods (41) and (42).
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PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
(n)
Remove the nut (53), the washer (52), the bolt (50) and disconnect the support rods (51) and (54).
(o)
Remove the nut (49), the washer (48), the bolt (46) and disconnect the support rod (47).
(p)
Remove the screws (2), the washers (1) and the air inlet (6).
(q)
Put protective covers on the open ends of the bellows (5) and the air inlet (6).
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PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
TASK 21-61-51-400-002
Installation of the Air Inlet
WARNING : MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM
_______ FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
1. Reason for the Job
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航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM AIR CONDITIONING 空調 5(56)
