TCH.1C-27J-2-27JG
2-16.2
(refer to figure
) (Cont'd)
2.Connect the trim tab actuator (19) at the intermediate
lever (9) by using bolt (21), washers (3 and 20),
castellated nut (5) and new cotter pin (4)(LCM NO.
00010). Torque tighten (AGE NO. 00054) bolt to 30
thru 35 in lb (0.346 thru 0.403 m Kg).
3.Connect the position transmitter control rod (13) at the
intermediate lever (9) by using special bolt (14),
washers (8, 12 and 15), castellated nuts (7 and 11)
and new cotter pins (6 and 10) (LCM NO. 00010).
Torque tighten (AGE NO. 00054) bolt to 30 thru 35 in
lb (0.346 thru 0.403 m Kg).
NOTE
Remove protection caps from the electrical
connectors to be installed.
4.Connect the electrical connectors 8CBA (1) and 8CBB
(2)
FOLLOW ON MAINTENANCE:
1.Install the access panel 544E.
2.Install the cover tip.
3.Install the Sequencer Unit (refer to manual
).
4.Remove maintenance platform (AGE NO. 00074).
5.Restore hydraulic power (refer to manual
6.Connect electrical power to aircraft (refer to manual
7.Perform the required test:
A.AILERON AND GEAR TRIM TAB TRAVEL (STEP
1, 4 AND 6) (refer to para
) .
27-10-10
2-131