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TCH.1C-27J-2-27JG
2-6.3
MEASUREMENT OF AILERON MANOUVRE
EFFORT (refer to figure 
2-2, sheet 4/8
) (Cont'd)
6.Remove from the control wheel the force
measurement fixture (AGE NO. 00025).
2-6.4
AILERON BALANCE CHECK (refer to figure 
2-2,
sheet 5/8
)
NOTE
This procedure is valid for LH aileron. For
RH aileron is similar.
1.Fit aileron template (AGE NO. 00064) on the top
surface of left and right outer wings.
2.Disconnect the rod connecting aileron trim position
transmitter to the trim actuator from LH trim tab
bellcrank (refer to para 
2-16
) .
3.Disconnect rod (1) from bellcrank (6) by removing bolt
(7), flat washers (4 and 5), castellated nut (3) and
cotter pin (2). Discard removed cotter pin.
4.Disconnect mechanism connecting RH aileron geared
tab (refer to manual 
TCH.1C-27J-2-57JG
) .
5.Check aileron balance according to the procedure
described in Section I of AER(EP).1C-27J-3 manual.
6.Reconnect mechanism connecting RH aileron geared
tab (refer to manual 
TCH.1C-27J-2-57JG
) .
7.Reconnect rod (1) at the bellcrank (6) by using bolt
(7), washers flat (4 and 5), castellated nut (3) and new
cotter pin (2) (LCM NO. 00052).
8.Reconnect the rod connecting aileron trim position
transmitter to the trim actuator at the LH trim tab
bellcrank (refer to para 
2-16
) .
9.Remove template (AGE NO. 00064) from the top
surface of left and right outer wings.
27-10-00
2-21