-
FOR 31CE3, 31CE4, 31CE7, 31CE8 pressurize the Yellow Hydraulic system (Ref. TASK 29-10-00-863-002) and the Yellow Hydraulic system reservoir (Ref. TASK 29-14-00-614-002)
-
FOR 31CE5, 31CE6 pressurize the Blue Hydraulic system (Ref. TASK 29-10-00-863-003) and Blue Hydraulic system reservoir (Ref. TASK 29-14-00-614-002).
(e) Make sure that the work area is clean and clear of tool(s) and other items.
(5) If the spoiler is safetied with ABS 0738 nuts, do the steps that follow:
(a)
When the clearance is correct:
(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:
1_ TORQUE the nut (68) to between 5.2 and 6.5 m.daN (38.34 and
47.93 lbf.ft).
2_ Install the locking cap (69) on the nut (68).
3_ Safety the locking cap (69) with the new cotter pin (70).
-
the washers (60), the bolts (61) and the special bolt (65)
-
the washer (67), the nut (68), the locking cap (69) and the cotter pin (70)
-
the bolt of the maintenance device.
(d) Pressurize the applicable hydraulic system and reservoir:
-
FOR 31CE1, 31CE2, 31CE9, 31CE10 pressurize the Green Hydraulic system (Ref. TASK 29-10-00-863-001) and the Green Hydraulic system reservoir (Ref. TASK 29-14-00-614-002)
-
FOR 31CE3, 31CE4, 31CE7, 31CE8
R 1EFF : 001-003, 051-052, 1 27-64-51Page 433 1 1 May 01/05 1 1 1CES 1 pressurize the Yellow Hydraulic system (Ref. TASK 29-10-00-863-002) and the Yellow Hydraulic system reservoir (Ref. TASK 29-14-00-614-002)
-FOR 31CE5, 31CE6 pressurize the Blue Hydraulic system (Ref. TASK 29-10-00-863-003) and Blue Hydraulic system reservoir (Ref. TASK 29-14-00-614-002).
(e) Make sure that the work area is clean and clear of tool(s) and other items.
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 27-64-51-860-054
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)
When the clearance is correct:
(a)
TORQUE the nut (68) to between 5.2 and 6.5 m.daN (38.34 and 47.93 lbf.ft).
(b)
Install the locking cap (69) on the nut (68).
(c)
Safety the locking cap (69) with the new cotter pin (70).
(5)
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.
(6)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the washers (60), the bolts (61) and the special bolt (65)
-
the washer (67), the nut (68), the locking cap (69) and the cotter pin (70)
-
the bolt of the maintenance device.
(7)
Pressurize the applicable hydraulic system and reservoir:
-
FOR 31CE1, 31CE2, 31CE9, 31CE10 pressurize the Green Hydraulic system (Ref. TASK 29-10-00-863-001) and the Green Hydraulic system reservoir (Ref. TASK 29-14-00-614-002)
-
FOR 31CE3, 31CE4, 31CE7, 31CE8 pressurize the Yellow Hydraulic system (Ref. TASK 29-10-00-863-002) and the Yellow Hydraulic system reservoir (Ref. TASK 29-14-00-614-002)
-
FOR 31CE5, 31CE6 pressurize the Blue Hydraulic system (Ref. TASK 29-10-00-863-003) and Blue Hydraulic system reservoir (Ref. TASK 29-14-00-614-002).
(8)
Make sure that the work area is clean and clear of tool(s) and other items.
R **ON A/C ALL
Subtask 27-64-51-710-053
F. Test
(1)
Do an operational test of the spoilers (Ref. TASK 27-64-00-710-001).
(2)
Examine the spoiler servo-control for hydraulic leaks. No leaks are permitted.
5. Close-up
________
Subtask 27-64-51-410-050
A. Close Access
(1)
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(25)
