2 Remove the HP filter 2048GM from the manifold (26).
_
(b)
Remove the relief valve 2063GM (Ref. TASK 29-12-32-000-001).
(c)
Remove the priority valve 2064GM (Ref. TASK 29-12-33-000-001).
(d)
Remove the hydraulic pressure transducer 2065GN (Ref. TASK 29-32-11-000-002).
(e)
Remove the system pressure switch 2151GN (Ref. TASK 29-32-12-000-002).
R 1EFF : 059-099, 102-149, 151-199, 201-299, 1 29-12-14Page 431 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(f)
Remove the flight-control pressure switch 10CE1 (Ref. TASK 27-92-17-000-003).
(g)
Remove the fluid sampling valve 2187GM (Ref. TASK 29-12-34-000-001).
(h)
Remove the check valve 2022GM as follows:
(i)
Remove the bobbins (12), (30), (39) (Ref. TASK 20-23-21-911-001). NOTE : There are three different sizes of bobbins.
____
(j)
Install the blanking plugs in the open ports of all of the removed components.
(k)
Install the blanking plugs on the open ports of the manifold (26).
(l)
Remove and discard these items from the bobbins:
-square-section seals (13), (31), (40)
-O-rings (87), (94), (97)
-back-up rings (85), (86), (95), (96), (98), (38).
(m)
Put the bobbins into the BAG - PLASTIC to keep them clean.
1_ Loosen the check valve 2022GM and remove it at the same time
with the O-ring (58).
2_ Remove and discard the O-ring (58).
(2) Install the removed parts on the replacement manifold (26) as follows:
NOTE : If the replacement manifold (26) was not installed before,
____ then you must install the threaded inserts (25) and the cylindrical pin (14).
(a)
Remove the blanking plugs from the manifold (26) and the components.
(b)
Apply the HYDRAULIC FLUIDS (Material No. 02-003) to the new O-rings and the threads of the unions.
(c)
Install the check valve 2022GM as follows: 1 Put the new O-ring (58) in position on the check valve 2022GM.
_
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 29-12-14Page 432 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
2_ Install the check valve 2022GM in port G of the manifold (26).
3_ TORQUE the check valve 2022GM to between 7.5 and 8.3 m.daN
(55.30 and 61.20 lbf.ft).
(d)
Install the fluid sampling valve 2187GM (Ref. TASK 29-12-34-400-001).
(e)
Install the system pressure switch 2151GN (Ref. TASK 29-32-12-400-002).
(f)
Install the flight-control pressure switch 10CE1 (Ref. TASK 27-92-17-400-003).
(g)
Install the hydraulic pressure transducer 2065GN (Ref. TASK 29-32-11-400-002).
(h)
Apply the HYDRAULIC FLUIDS (Material No. 02-003) to the new square-section seals, back-up rings and the O-rings.
(i)
Put the two new back-up rings (85) in position on the sides of the bobbins (12) without the identification grooves (equipment side).
(j)
Put the two new square-section seals (13) in position on the sides of the bobbins (12) without the identification grooves (equipment side).
(k)
Put the two new back-up rings (86) in position on the sides of the bobbins (12) with the identification grooves (manifold side).
(l)
Put the two new O-rings (87) in position on the sides of the bobbins (12) with the identification grooves (manifold side).
(m)
Install the two bobbins (12) with the identification grooves in the ports of the manifold (26) (Ref. TASK 20-23-21-911-001).
(n)
Put the two new back-up rings (96) in position on the sides of the bobbins (30) without the identification grooves (equipment side).
(o)
Put the two new square-section seals (31) in position on the sides of the bobbins (30) without the identification grooves (equipment side).
(p)
Put the two new back-up rings (95) in position on the sides of the bobbins (30) with the identification grooves (manifold side).
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 29-12-14Page 433 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(q)
Put the two new O-rings (94) in position on the sides of the bobbins (30) with the identification grooves (manifold side).
(r)
Install the two bobbins (30) with the identification grooves in the ports of the manifold (26) (Ref. TASK 20-23-21-911-001).
(s)
Put the two new back-up rings (38) in position on the sides of the bobbins (39) without the identification grooves (equipment side).
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 HYDRAULIC POWER 液压3(29)