(9)
Pull the spoiler rearwards and outboard to disengage it from the shaft (23) and then remove it from the aircraft. Collect the spacer (22).
(10) If it is necessary to remove the shaft (23):
-
remove the spoiler 3 (Ref. TASK 27-64-43-000-001)
-
remove the shaft (23).
If the spoiler is safetied with ABS 0738 nuts, do the steps that follow:
(11)
Remove the nuts (46), the washers (47) and the bolts (44) to disconnect the bonding straps (45) from each end of the spoiler 4.
(12)
Remove the nuts (27), (43) and (56) and the locking plates (28), (42) and (55).
(13)
Remove the spacer (57) and the bolt (48).
R 1EFF : 001-003, 051-052, 1 27-64-44Page 413 1 1 May 01/05 1 1 1CES 1
(14)
Remove the items that follow:
(a)
Remove and discard the cotter pin (1) from the locking cap (2).
(b)
Remove the locking cap (2), the nut (3) and the washer (4). Do not remove the hinge pin (6).
(c)
Remove and discard the cotter pins (26) and (49) from the locking caps (25) and (50).
(d)
Remove and discard the cotter pins (34) and (35) from the locking caps (33) and (36).
(e)
Remove the locking caps (25), (50), (33) and (36).
(f)
Remove the nuts (24), (51), (32) and (37).
(g)
Remove the washers (23), (52), (31) and (38).
(15)
Do not remove the hinge pins (29), (41) and (54).
(16)
Prepare the spoiler 4 for removal: CAUTION : SUPPORT THE SERVO CONTROL 7.5kg (16.5lb) AND THE SPOILER
_______ APPROXIMATELY 15kg (33lb). THIS WILL PREVENT DAMAGE TO:
-
THE HYDRAULIC LINES
-
THE ELECTRICAL CABLES
-
THE STRUCTURE.
(a) Put the spoiler 4 and the actuator on supports. Remove the hinge pin (6) from the actuator eye-end (8) and carefully lower the actuator.
(17)
Remove the sliding bush (5) and the flanged bush (7).
(18)
Leave the supports in position below the spoiler and remove the hinge pins (29), (41) and (54). Collect the sliding bushes (30), (39), (40) and (53).
(19)
Pull the spoiler rearwards and outboard to disengage it from the shaft (21) and then remove it from the aircraft. Collect the spacer (20).
(20)
If it is necessary to remove the shaft (21):
-
remove the spoiler 3 (Ref. TASK 27-64-43-000-001)
-
remove the shaft (21).
R 1EFF : 001-003, 051-052, 1 27-64-44Page 414 1 1 May 01/05 1 1 1CES 1R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 27-64-44-020-050-A
A. Removal of the Spoiler 4
(1)
Remove the nuts (46), the washers (47) and the bolts (44) to disconnect the bonding straps (45) from each end of the spoiler 4.
(2)
Remove the nuts (27), (43) and (56) and the locking plates (28), (42) and (55).
(3)
Remove the spacer (57) and the bolt (48).
(4)
Remove the items that follow:
(a)
Remove and discard the cotter pin (1) from the locking cap (2).
(b)
Remove the locking cap (2), the nut (3) and the washer (4). Do not remove the hinge pin (6).
(c)
Remove and discard the cotter pins (26) and (49) from the locking caps (25) and (50).
(d)
Remove and discard the cotter pins (34) and (35) from the locking caps (33) and (36).
(e)
Remove the locking caps (25), (50), (33) and (36).
(f)
Remove the nuts (24), (51), (32) and (37).
(g)
Remove the washers (23), (52), (31) and (38).
(5)
Do not remove the hinge pins (29), (41) and (54).
(6)
Prepare the spoiler 4 for removal: CAUTION : SUPPORT THE SERVO CONTROL 7.5kg (16.5lb) AND THE SPOILER
_______ APPROXIMATELY 15kg (33lb). THIS WILL PREVENT DAMAGE TO:
-
THE HYDRAULIC LINES
-
THE ELECTRICAL CABLES
-
THE STRUCTURE.
(a) Put the spoiler 4 and the actuator on supports. Remove the hinge pin (6) from the actuator eye-end (8) and carefully lower the actuator.
R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 27-64-44Page 415 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(7)
Remove the sliding bush (5) and the flanged bush (7).
(8)
Leave the supports in position below the spoiler and remove the hinge pins (29), (41) and (54). Collect the sliding bushes (30), (39), (40) and (53).
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 FLIGHT CONTROLS 飛行操縱6(165)
