TCH.1C-27J-2-27JG
2-34.1 REMOVAL (refer to figure
(refer to figure
3.Disconnect from the lever (5) the rod (9) by removing
bolt (10), washer (8), nut, self-locking (7) and pin (6).
Discard removed nut, self-locking.
4.Disconnect and remove from the aircraft structure the
rudder trim position transducer (10CC) (4) by
removing screws (2) and washers (3).
2-34.2 INSTALLATION (refer to figure
)
and (refer to figure
1.Position and install to the aircraft structure the rudder
trim position transducer (10CC) (4) by using screws
(2) and washers (3).
2.Connect to the lever (5) the rod (9) by using bolt (10),
washer (8), new nut, self-locking (LCM NO. 00370) (7)
and pin (6).
3.Connect the electrical connector (10CCA) (1) to the
rudder trim position transmitter (10CC) (4) .
4.Ensure that the rudder is to zero position.
5.Adjust and connect the linkage rod between the
rudder position transducer lever and rudder
attachment point.
6.Check that, on the Combined Trim Indicator (15CB)
(11), the RUDDER indication (12) shows about 0°.
7.It is necessary to re-adjust the linkage rod and /or the
transducer lever to get 0°.
8.Perform the fully trim travel leftward / rightward and
check that, on the Combined Trim Indicator (15CB)
(11), the RUDDER indication (12) shows about 11.6°.
9.Close the access panels 322B and 322D.
27-20-45
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