TCH.1C-27J-2-27JG
2-30.2 INSTALLATION (refer to figure
)
and (refer to figure
1.Connect the load-feel spring (5) at the fell unit lever
(7) by using bolt (6), washer (8), castellated nut (9)
and new cotter pin (10) (LMC NO. 00052) . Torque
tighten (AGE NO. 00054) to 10 thru 29 in lb.
2.Connect the load-feel spring (5) at the bellcrank (3) by
using bolt (4), washer (11), castellated nut (13) and
new cotter pin (12) (LMC NO. 00052). Torque tighten
(AGE NO. 00054) to 10 thru 29 in lb.
3.Remove the rigging pin (1) (AGE NO. 00181) from
rudder quadrant (2).
4.Verify that the rudder is in neutral position.
FOLLOW ON MAINTENANCE:
1.Connect electrical power to aircraft (refer to manual
2.Restore hydraulic power system (refer to manual
3.Close the access panel 322E.
4.Remove maintenance platform (AGE NO. 00074).
5.Perform the functional test:
A.CHECK OF RETURN TO NEUTRAL POSITION
) .
B.RUDDER CONTROL SYSTEM (refer to para
)
.
27-20-30
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