TCH.1C-27J-2-27JG
2-17.1 REMOVAL (refer to figure
) , (refer
to figure
) and (refer to figure
CAUTION
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Install protection caps on the
disconnected electrical connectors.
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1.Disconnect the electrical connectors 8CBA (1) and
8CBB (2).
2.Disconnect the position transmitter control rod (13)
from intermediate lever (9) by removing special bolt
(14), washers (8, 12 and 15), castellated nuts (7 and
11) and cotter pins (6 and 10). Discard removed cotter
pins.
3.Disconnect the trim tab actuator (19) from
intermediate lever (9) by removing bolt (21), washers
(3 and 20), castellated nut (5) and cotter pin (4).
Discard removed cotter pin.
4.Disconnect the trim tab actuator (19) from structure by
removing bolt (18), washer (17) and nut (16).
2-17.2 INSTALLATION (refer to figure
(refer to figure
)
CAUTION
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Install aileron trim tab actuator (19) in
neutral position 8.79 in (223.3 mm)
between the connection axis
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1.Connect the trim tab actuator (19) at the structure by
using bolt (18), washer (17) and nut (16). Torque
tighten (AGE NO. 00054) bolt to 30 thru 35 in lb
(0.346 thru 0.403 m Kg).
(Cont'd)
27-10-10
2-135