Aileron Installation
Figure 401 (Sheet 1)
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MAINTENANCE MANUAL
Aileron Installation
Figure 401 (Sheet 2)
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MAINTENANCE MANUAL
S 034-007
(2)
Disconnect the PCA input rods from the PCA input-levers (AMM 27-11-20/201).
S 034-008
(3)
Disconnect the PCA's from the aileron (1) at the rod end (AMM 27-11-20/201).
S 034-036
(4)
AIRPLANES WITH TWO BONDING JUMPERS AT HINGE 1;
Disconnect the bonding jumpers (2, 3) from hinge 1.
S 034-035
(5)
AIRPLANES WITH ONLY ONE BONDING JUMPER AT HINGE 1;
Disconnect the single bonding jumper from hinge 1.
S 034-038
(6)
Disconnect bonding jumpers (2, 3) from hinge 5.
S 034-010
(7)
Disconnect the hinges from the aileron (1).
S 024-011
(8)
Remove the aileron.
NOTE: If it is necessary, the trailing edge flaps can be operated
____ after the aileron has been removed. Make sure that there are no loose components near the flaps before they are operated.
S 034-012
(9) Remove the aileron sling from the aileron.
TASK 27-11-21-424-013
3. Install the Aileron
___________________
A. General
(1)
This procedure contains only the data that is necessary to install the aileron. Refer to AMM 27-11-21/601 for the applicable wear-limit data.
B.
Equipment
(1)
Aileron Sling - B27012-1
C.
Consumable Materials
(1)
D00633 Grease, Corrosion Preventive - BMS 3-33 (recommended)
(2)
D00015 Grease, Corrosion Preventive - BMS 3-24 (optional)
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MAINTENANCE MANUAL
(3)
D00013 Grease, Corrosion Preventive - MIL-G-23827 (optional)
D.
Parts
(1)
Refer to the AIPC for more data on the components that are contained in the tables that follow:
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Aileron | 27-11-21 | 01 | 140,145 | | | 2 | Jumper | | | 35 | | | 3 | Jumper | | | 40 | | | 4 | Bolt Retainer | | | 80 | | | 5 | Bolt | | | 15 | | | 6 | Washer | | | 25 | | | 7 | Nut | | | 30 | | | 8 | Bolt Retainer | | | 85 | | | 9 | Washer | | | 95 | | | 10 | Nut | | | 100 | | | 11 | Bushing | | | 105 | | | 12 | Washer | | | 95 | | | 13 | Bolt | | | 90 | | | 14 | Washer | | | 125 | | | 15 | Nut | | | 130 | | | 16 | Bushing | | | 135 | | | 17 | Washer | | | 120 | | | 18 | Bolt | | | 110,115 | 2.......….......…...................................…..........….....….........1
(2) GUN 003-999;
Refer to the table that follows:
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 19 | Control Rod | 27-18-01 | 01 | 60 | | | 20 | Screw | | | 20 | | | 21 | Bushing | | | 25 | | | 22 | Washer | | | 30 | | | 23 | Washer | | | 33 | | | 24 | Nut | | | 35 | 2......…........…...................................…..........…......…........1 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(113)
