(3)
Remove the blanking caps from the spoiler servo-control and the hydraulic and electrical connections.
(4)
Connect the applicable hydraulic unions to the spoiler servo-control:
-
FOR 31CE1, 31CE2 the pipe (3) and the unions (1), (2) and (4)
-
FOR 31CE3 the pipes (22) and (26) and the unions (23), (24), (25) and (27)
-
FOR 31CE4 the pipes (6) and (9) and the unions (5), (7), (8) and (10)
-
FOR 31CE5 the pipe (19) and the unions (17), (18), (20), (21) and (22)
-
FOR 31CE6 the pipe (14) and the unions (11), (12), (13), (15) and (16)
-
FOR 31CE7
the unions (30) and (31)
-
FOR 31CE8
the unions (32) and (33)
-
FOR 31CE9 the pipe (35), the connector (39) and the unions (34), (36), (37),
(38) and (40)
-FOR 31CE10 the pipes (44) and (49), the connector (48) and the unions (41), (42), (43), (45), (46) and (47).
(5)
Install the washers (60) and the bolts (61).
(6)
TORQUE the bolts (61) to between 2.95 and 3.26 m.daN (21.75 and 24.04 lbf.ft).
(7)
If applicable, turn the eye-end (63) and the piston rod together so that the greaser points down.
(8)
Apply a thin layer of COMMON GREASE (Material No. 04-004) to:
-
the flanged bush (64)
-
the special bolt (65)
-
the sliding bush (66)
-
the spoiler attachment bracket.
(9)
Install the flanged bush (64) and the sliding bush (66) in the
spoiler attachment bracket.
(10)
Put the eye-end (63) in position in the spoiler attachment bracket and install the special bolt (65).
(11)
Make sure that the special bolt (65) engages correctly with the projection on the spoiler attachment bracket.
(12)
Measure the dimension Z. The dimension Z must not be more than 0.70 mm (0.0275 in.).
(13)
Install the washer (67) and the nut (68) on the special bolt (65), but do not tighten.
(14)
Remove the applicable spoiler support strut STRUT SUPPORT - SPOILER 1 (98D27604002000) or STRUT SUPPORT - SPOILER 2, 3, 4, AND 5 (98D27604001000).
(15)
Install the electrical connector (73).
(16)
Clean the electrical connector (73) with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(17)
Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-008) to the electrical connector (73).
(18)
Make sure that the work area is clean and clear of tool(s) and other items.
R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 27-64-51Page 431 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL
Subtask 27-64-51-865-062
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 21CE1, 21CE2, 21CE3, 22CE, 1701GK, 1702GK, 1801GL, 2701GJ, 2702GJ, 3700GD, 3801GX, 3802GX, 3803GX.
R **ON A/C 001-003, 051-052,
Subtask 27-64-51-860-054-A
E. Aircraft Maintenance Configuration
(1)
Retract the flaps fully (Ref. TASK 27-50-00-866-009).
(2)
Remove the COLLAR-SAFETY, SPOILER from the applicable spoiler servo-control and lower, by hand, the applicable spoiler.
(3)
Measure the distance between the applicable spoiler and the flap (Ref. TASK 27-64-00-820-001).
(4)
If the spoiler is safetied with STA-LOK nuts, do the steps that follow:
(a) When the clearance is correct, install the STA-LOK nut (67) and the STA-LOK washer (68) as follows (Ref. TASK 20-22-00-400-001):
1 TORQUE the STA-LOK nut (67) to between 4.7 and 6.5 m.daN
_ (34.66 and 47.93 lbf.ft) with the WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 (SL90-315-7500).
2 Install the STA-LOK washer (68) with the TOOL - INSTALLATION,
_ TAB WASHERS STA-LOK NSA5454 (SL90-313-7500).
(b)
On the spoiler servo-control, turn the SPOILER MAINTENANCE KEY (98D27603002000) or the SPOILER MAINTENANCE KEY (98D27603002001) in the maintenance device to the operation position and then remove it.
(c)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the washers (60), the bolts (61) and the special bolt (65)
-
the STA-LOK nut (67) and the STA-LOK washer (68)
-
the bolt of the maintenance device.
(d) Pressurize the applicable hydraulic system and reservoir:
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵7(24)
