B. Get Access
(1)
Put the access platform in position below the applicable bypass-valve: FOR 2517GM below zone 731 FOR 2518GM below zone 741.
(2)
Put a container below the applicable bypass-valve.
(3) Open the applicable MLG door (Ref. TASK 32-12-00-010-001). R (4) Make sure that a GROUND LOCK SLEEVE is installed on the applicable
R MLG door actuating cylinder (Ref. TASK 32-00-00-481-002). Subtask 32-31-13-860-052
C. Aircraft Maintenance Configuration
(1)
Make sure that the Yellow and Green hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).
(2)
Make sure that the applicable hydraulic reservoirs are depressurized (Ref. TASK 29-14-00-614-001).
(3)
Disconnect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-001).
4. Procedure
_________
(Ref. Fig. 401/TASK 32-31-13-991-001)
Subtask 32-31-13-020-050
A. Removal of the MLG Door Ground-Opening Bypass-Valve WARNING : DO NOT LET OIL STAY ON YOUR SKIN FOR A LONG TIME AS IT CAN
_______
CAUSE INJURY.
CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT
_______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER.
1EFF : ALL 1 32-31-13Page 403 1 1 May 01/99 1 1 1CES 1
MLG Door Ground-Opening Bypass-Valve - Location and Detail
Figure 401/TASK 32-31-13-991-001
1EFF : ALL 1 32-31-13Page 404 1 1 Feb 01/98 1 1 1CES 1
(1)
Disconnect the end-fittings (1) of the hydraulic pipe-lines from the unions (2).
(2)
Put blanking plugs on the disconnected line ends.
(3)
Disconnect the control-rod (11) of the door-uplock from the bypass-lever (7).
(a)
Remove and discard the cotter pin (9).
(b)
Remove the nut (10), the washer (8), the bolt (13) and the bush (12).
(c)
Disconnect the flexible control assembly (29) from the bypass-lever (26) as follows:
(4)
Hold the bypass-valve (4) and remove the nuts (18) and the bolts (5). Remove the bypass-valve (4).
(5)
If you are to replace the bypass-valve (4), do these steps:
(a)
Remove and discard the cotter pin (15).
(b)
Remove the nut (14), the washer (16) and the bolt (6).
(c)
Remove the bypass-lever (7).
(d)
Remove and discard the cotter pin (22).
(e)
Remove the nut (19), the washer (20) and the bolt (21).
(f)
Remove the bypass-lever (26).
(g)
Put tape, protective on the splines at each end of the shaft (17).
(h)
Remove the unions (2) from the bypass-valve (4) and put the blanking plugs in the hydraulic openings.
(i)
Remove and discard the packings (3).
1_ Remove and discard the cotter pin (24).
2_ Remove the nut (23), the washer (25), the bolt (28) and the
bush (27).
1EFF : ALL 1 32-31-13Page 405 1 1 Aug 01/04R 1 1 1CES 1
TASK 32-31-13-400-001
Installation of the MLG Door Ground-Opening Bypass-Valve 2517GM (2518GM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
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 LANDING GEAR 起落架4(104)