TCH.1C-27J-2-27JG
2-42.1
REMOVAL (refer to figure
) , (refer
to figure
)
(Cont'd)
19.On workbench, remove the nuts spanner (22 and 61)
and washers (21 and 60) from the bottom of LH (RH)
elevator tension regulator (19 and 58). Collect nuts
spanner and washers.
20.On workbench, extract the LH (RH) elevator tension
regulator (19 and 58) from the assembly and remove
it.
2-42.2
(refer to figure
) , (refer to figure
)
1.On the workbench, insert the new LH (RH) elevator
tension regulator (19 and 58) to the assembly.
2.On workbench, insert the position washer (21 and 60)
on the elevator tension regulator (19 and 58) side.
3.On workbench, tighten the nuts spanner (22 and 61)
and torque (AGE NO. 00054) tighten to 195 to 200 in
lb (2.24 to 2.30 mkg). Lock the washers (21 and 60).
4.Position the tension regulator assembly to the aircraft
structure.
5.In order to connect the supports assembly (45 and 57)
with the aircraft insert the bolts (40, 44, 50 and 54).
6.In order to connect the supports assembly (45 and 57)
with the aircraft insert to the lower part the washers
(39 and 55) and the new self-locking nuts (LCM NO.
00025 and LCM NO. 00013) (37 and 56). Torque
(AGE NO. 00054) tighten to 59 to 66 in lb (0.67 to
0.76 mkg) the self-locking nuts.
(Cont'd)
27-30-05
2-342