(c)
 Put the two back-up rings (63) in position on the sides of the bobbins (10) without the identification grooves (equipment side).

 (d)
 Put the two square-section seals (11) in position on the sides of the bobbins (10) without the identification grooves (equipment side).

R 1EFF : 001-049, 051-058, 101-101, 1 29-11-14Page 413 1 1 May 01/05 1 1 1CES 1

 (e)
 Put the two back-up rings (64) in position on the sides of the bobbins (10) with the identification grooves (manifold side).

 (f)
 Put the two O-rings (65) in position on the sides of the bobbins

 (10) with the identification grooves (manifold side).

 (g)
 Install the two bobbins (10) with the identification grooves in the ports of the manifold (13) (Ref. TASK 20-23-21-911-001).

 (h)
 Put the two back-up rings (69) in position on the sides of the bobbins (8) without the identification grooves (equipment side).

 (i)
 Put the two square-section seals (70) in position on the sides of the bobbins (8) without the identification grooves (equipment side).

 (j)
 Put the two back-up rings (9) in position on the sides of the bobbins (8) with the identification grooves (manifold side).

 (k)
 Put the two O-rings (68) in position on the sides of the bobbins

 (8) with the identification grooves (manifold side).

 (l)
 Install the two bobbins (8) with the identification grooves in the ports of the manifold (13) (Ref. TASK 20-23-21-911-001).

 (m)
 Put the back-up ring (61) in position on the side of the bobbin

 (6) without the identification groove (equipment side).

 (n)
 Put the square-section seal (60) in position on the side of the bobbin (6) without the identification groove (equipment side).

 (o)
 Put the back-up ring (7) in position on the side of the bobbin

 (6) with the identification groove (manifold side).

 (p)
 Put the O-ring (62) in position on the side of the bobbin (6) with the identification groove (manifold side).

 (q)
 Install the bobbin (6) with the identification groove in the port of the manifold (13) (Ref. TASK 20-23-21-911-001).

 (r)
 Put the back-up rings (33) in position on the sides of the bobbins (34) without the identification grooves (equipment side).

 (s)
 Put the square-section seals (35) in position on the sides of the bobbins (34) without the identification grooves (equipment side).

R 1EFF : 001-049, 051-058, 101-101, 1 29-11-14Page 414 1 1 May 01/05 1 1 1CES 1

 (t)
 Put the back-up rings (67) in position on the sides of the bobbins (34) with the identification grooves (manifold side).

 (u)
 Put the O-rings (66) in position on the sides of the bobbins (34) with the identification grooves (manifold side).

 (v)
 Install the two bobbins (34) with the identification grooves in the ports of the manifold (13) (Ref. TASK 20-23-21-911-001).

 (w)
 Apply the HYDRAULIC FLUIDS (Material No. 02-003) to the threads of the components.

 (x)
 Install the check valve 1022GM as follows:

 (y)
 Install the check valve 1059GM as follows: 1 Put the O-ring (28) in position on the check valve 1059GM.

 1_ Put the O-ring (19) in position on the check valve 1022GM.
 2_ Install the check valve 1022GM in port E of the manifold (13).
 3_ TORQUE the check valve 1022GM to between 9.10 and 10.24 m.daN
 (67.10 and 75.51 lbf.ft).

_ 2 Put the back-up rings (29) and the O-ring (27) in position on
_ the check valve 1059GM.
 3 Install the check valve 1059GM in the manifold (13).
_ 4 TORQUE the check valve 1059GM to between 10.24 and 11.379
_ m.daN (75.51 and 83.91 lbf.ft).
 5 Safety the check valve 1059GM with the lockwire, MISCELLANEOUS
_ (Material No. 19-010).
 (z) Install the fluid sampling valve 1187GM (Ref. TASK 29-11-34-400-001).
 (aa) Install the system pressure switch 1151GN (Ref. TASK 29-32-12-400-001).
 (ab) Install the flight-control pressure switch 10CE-2 (Ref. TASK 27-92-17-400-001).
 (ac) Install the relief valve 1063GM (Ref. TASK 29-11-32-400-001).
R 1EFF : 001-049, 051-058, 101-101, 1 29-11-14Page 415 1 1 May 01/05 1 1 1CES 1

 (ad) Install the HP filter 1048GM on the manifold (13) and install the bolts (30), (31) and the washers (32). (ae) TORQUE the bolts (30), (31) to between 1.6 and 1.8 m.daN (11.79 and 13.27 lbf.ft). (af) Install the leakage-measurement solenoid valve 1150GP (Ref. TASK 29-19-51-400-001). (ag) Put the O-ring (44) in position and install the pressure transducer 1065GN, the washers (42) and the bolts (41). (ah) Tighten the bolts (41). R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM HYDRAULIC POWER 液壓2(18)