TCH.1C-27J-2-27JG
2-45.2 INSTALLATION (refer to figure
(refer to figure
) , (refer to figure
) and (refer to figure
) (Cont'd)
7.In order to connect the supports assembly (45 and 57)
with the aircraft insert to the upper part the washers
(43 and 51) and the castellated nuts (41 and 53).
Torque (AGE NO. 00054) tighten to 30 to 40 in lb
(0.34 to 0.46 mkg) the castellated nuts. Insert the new
cotter pins (LCM NO. 00052) (42 and 52).
8.Insert the LH (RH) rod assy (6 and 47) to the supports
(45 and 57) assy upper axle.
9.In order to install the rod assy (6 and 47) insert the
bolts (5 and 46), the washers (7 and 48) and the new
self-locking nuts (LCM NO. 00025 and LCM NO.
00013) (8 and 49). Torque (AGE NO. 00054) and
tighten to 59 to 66 in lb (0.67 to 0.76 mkg) the
self-locking nuts.
NOTE
Perform step 10 to install Pilot tension
regulator else go to step 11.
10.In order to connect the rudder input lever (30) insert
the bolt (10) the washer (9) and tighten the castellated
nut (11). Tighten (AGE NO. 00054) the nut to 25 to 71
in lb (0.28 to 0.81 mkg) and insert the new cotter pin
(LCM NO. 00052) (31).
11.In order to connect the LH (RH) elevator input levers
(27 and 66) insert the bolts (29 and 68) the washers
(26 and 65) and tighten the castellated nuts (24 and
63). Tighten (AGE NO. 00054) the nuts to 25 to 71 in
lb (0.28 to 0.81 mkg) and insert the new cotter pins
(LCM NO. 00052) (25 and 64).
12.Insert rig pin to rudder (12) (LH side only) and elevator
LH (RH) quadrants (19 and 58).
(Cont'd)
27-30-05
2-347