TCH.1C-27J-2-27JG
2-42.1
REMOVAL (refer to figure
) , (refer
to figure
)
(Cont'd)
12.Disconnect the cables (13, 23, 38 and 62) from the
rudder quadrant (12) (LH side only) and from the LH
(RH) elevator tension regulator quadrants (19 and 58).
NOTE
Perform steps 14 to remove Pilot tension
regulator else go to step 15.
13.Disconnect the rudder input lever (30) by removing
the cotter pin (31), castellated nut (11) washer (9) and
bolt (10). Discard the cotter pin.
14.Disconnect the elevator input levers (27 and 66) by
removing the cotter pins (25 and 64), castellated nuts
(24 and 63), washers (26 and 65) and bolts (29 and
68). Discard removed the cotter pins.
15.Disconnect rod assy LH (RH) (6 and 47) to the
support assy LH (RH) (45 and 57) upper axle by
removing the bolts (5 and 46), washers (7 and 48) and
self-locking nuts (8 and 49). Discard removed the
self-locking nuts.
16.Disconnect the support assy LH (RH) (45 and 57) to
upper axles assembly from the structure by removing
the bolts (40 and 54), washers (39 and 55) and lower
self-locking nuts (37 and 56). Discard removed the
self-locking nuts.
17.Disconnect the support assy LH (RH) (45 and 57) to
upper axles assembly from the structure by removing
the cotter pins (42 and 52), washers (43 and 51),
castellated nuts (41 and 53) and upper bolts (44 and
50). Discard removed the cotter pins.
18.Remove the assembly from aircraft.
(Cont'd)
27-30-05
2-341