(13)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the bolts (17)
-
the washers (10)
-
the nuts (11)
-
the STA-LOK nuts (12)
-
the STA-LOK washers (13)
-
the pins (15).
(14)
For hinge No.s 1, 2 and 3, apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the hinge pin (19)
-
the bolt (21)
-
the nut (22)
-
the STA-LOK nut (27)
-
the STA-LOK washer (28).
(15)
For hinge No.s 4 and 5, apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the hinge pin (42)
-
the bolt (44)
-
the STA-LOK nut (51)
-
the STA-LOK washer (52).
(16)
Remove the SUPPORT-AILERON ACTUATOR.
(17)
Move the aileron through its travel range and examine for:
-free movement
-the correct installation of the applicable bonding straps (25),
(40) and (49).
(18)
For hinge No.s 1, 2 and 3, seal the bonded items that follow (Ref. TASK 20-28-00-912-004):
-
the nut (23)
-
the washers (24) and (29)
-
the bonding strap (25)
-
the bolt (30).
(19)
For hinge No.s 4 and 5, seal the bonded items that follow (Ref. TASK 20-28-00-912-004):
-
the bolt (45)
-
the nut (55)
-
the washers (46) and (56)
-
the bonding strap (40).
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(20)
For hinge No. 5, seal the bonded items that follow (Ref. TASK 20-28-00-912-004):
-
the bolt (47)
-
the nut (53)
-
the washers (48) and (54)
-
the bonding strap (49).
(21)
Install the static dischargers (Ref. TASK 23-61-41-400-001). If the aileron is safetied with ABS 0738 nuts, do the steps that follow:
(22)
Use the crane to put the aileron in position.
(23)
For hinge No.s 1, 2 and 3, do the steps that follow:
(a)
Install the GUIDE CONE - AILERON (98D27104000001) on the hinge pin (71). Install the hinge pin (71) with the head outboard. Remove the GUIDE CONE - AILERON.
(b)
Make sure that the hinge pin (71) is correctly aligned, so that the locking plate (72) can be installed.
(c)
Install the washer (79) and the nut (80) on the hinge pin (71).
(d)
TORQUE the nut (80) to between 4.7 and 5.2 m.daN (34.66 and 38.34 lbf.ft).
(e)
Install the locking cap (81) on the nut (80).
(f)
Safety the locking cap (81) with the new cotter pin (82).
(g)
Install the locking plate (72), the bolt (73) and the nut (74).
(h)
Install the bonding strap (77), the washers (76) and (83), the bolt (84) and the nut (75) (Ref. TASK 20-28-00-912-004).
(24)
For hinge No.s 4 and 5, do the steps that follow:
(a)
Install the GUIDE CONE - AILERON (98D27104000001) on the hinge pin (92). Install the hinge pin (92) with the head outboard. Remove the GUIDE CONE - AILERON.
(b)
Make sure that the head of the hinge pin (92) is correctly aligned, so that the locking plate (93) can be installed.
(c)
Install the washer (101) and the nut (102) on the hinge pin (92).
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(d) TORQUE the nut (102) to between 4.7 and 5.2 m.daN (34.66 and
38.34 lbf.ft).
(e)
Install the locking cap (103) on the nut (102).
(f)
Safety the locking cap (103) with the new cotter pin (104).
(g)
Install the locking plate (93) and the bolt (94).
(h)
Install the bonding strap (90), the washers (96) and (108), the bolt (95) and the nut (107) (Ref. TASK 20-28-00-912-004).
(25)
For hinge No. 5, install the bonding strap (99), the washers (98) and (105), the bolt (97) and the nut (106) (Ref. TASK 20-28-00-912-004).
(26)
Hold the aileron, loosen the adjuster assemblies and remove the LIFTING FRAME ASSEMBLY (AILERON) from the aileron.
(27)
Install the flanged bushes (66) in the actuator attachment brackets.
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵1(94)
