(d)
 Install the washers (34) and (41) and the nuts (35) and (40) on the hinge pins (32) and (44).

 (e)
 TORQUE the nuts (26) and (53) to between 3.0 and 3.5 m.daN (22.12 and 25.81 lbf.ft).

 (f)
 TORQUE the nuts (35) and (40) to between 5.5 and 6.0 m.daN (40.56 and 44.24 lbf.ft).

 (g)
 Install the locking cap (2) on the nut (3).

 (h)
 Install the locking caps (27) and (52) on the nuts (26) and (53).

 (i)
 Install the locking caps (36) and (39) on the nuts (35) and (40).

 (23)
 Safety the items that follow:

 -
the locking cap (2) with the new cotter pin (1)

 -
the locking cap (27) with the new cotter pin (28)

 -
the locking cap (36) with the new cotter pin (37)

 -
the locking cap (39) with the new cotter pin (38)

 -
the locking cap (52) with the new cotter pin (51).

 (24)
 Clean the parts:

 (a) Clean the interfaces of the bolt (29) and the spacer (20) with a clean MISCELLANEOUS (Material No. 19-003) and CLEANING AGENTS (Material No. 11-026).
R 1EFF : 001-003, 051-052, 1 27-64-45Page 425 1 1 May 01/05 1 1 1CES 1

 (25)
 Apply a thin layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the interfaces of the bolt (29) and the spacer (20).

 (26)
 Install the bolt (29) and the spacer (20).

 (27)
 Install the locking plates (22), (31) and (45) and attach them with the nuts (21), (30) and (46).

 (28)
 TORQUE the nuts (21), (30), and (46) to between 0.25 and 0.30 m.daN

 (22.12 and 26.54 lbf.in).

 (29)
 Attach the bonding strips (48) to each end of the spoiler with the bolts (47), the washers (50) and the nuts (49) (Ref. TASK 20-28-00-912-004).

 Subtask 27-64-45-916-051
 E. Application of Special Materials
 If the spoiler is safetied with STA-LOK nuts, do the steps that follow:
 (1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
 -
the STA-LOK washers (1), (27), (33), (35) and (45)

 -
the STA-LOK nuts (2), (26), (32), (34) and (46)

 -
the hinge pins (4), (24), (30), (38) and (47)

 -
the nuts (22), (28) and (40)

 -
the bolt (20).

 If the spoiler is safetied with ABS 0738 nuts, do the steps that follow:
 (2) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
 -
the cotter pins (1), (28), (37), (38) and (51)

 -
the locking caps (2), (27), (36), (39) and (52)

 -
the nuts (3), (26), (35), (40) and (53)

 -
the washers (4), (25), (34), (41) and (54)

 -
the hinge pins (6), (23), (32), (44) and (55)

 -
the nuts (21), (30) and (46)

 -
the bolt (29).

R 1EFF : 001-003, 051-052, 1 27-64-45Page 426 1 1 May 01/05 1 1 1CES 1

R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,

 Subtask 27-64-45-420-051-A
 B. Preparation for Installation
 (1)
 Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 (2)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Apply COMMON GREASE (Material No. 04-022) to the:

 -
hinges on the rear spar

 -
hinges on the spoiler

 -sliding bushes (5), (24), (33), (42) and (43)
 -flanged bush (7)
 -hinge pins (6), (23), (32), (44) and (55). Subtask 27-64-45-916-050-A
 C. Application of Special Materials
 (1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the eye-end (8) on the rounded surface only.
 NOTE : Do not get Material 15-007 on the servo control spherical
____
 bearing.

 Subtask 27-64-45-420-050-A
 D. Installation of the Spoiler 5
 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.

 (1)
 Install the sliding bushes (24), (33), (42) and (43).

 (2)
 Make sure there are supports below the spoiler 5 to hold it in the correct position.
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱7(4)