TCH.1C-27J-2-27JG
2-44.2
) (Cont'd)
13.Remove the stiffening tools (AGE NO. 00016) from
the LH stabilizer.
2-44.3
)
1.Install the template (AGE NO. 00065) on LH (RH)
elevator trailing edge.
2.Stiffen by proper tools (AGE NO. 00016) the RH
Stabilizer in order to avoid loss of reading accuracy on
elevator.
3.Connect external AC power supply to aircraft (refer to
).
4.Connect the hydraulic test cart (AGE NO. 00263), via
the adaptor, to the aircraft and supply both hydraulic
systems at 3000 psi (210 Kg/cm
²
).
5.Insert and remove a 0.193 in (4.915 mm) diameter
rigging pin (AGE NO. 00181) in the proper hole of the
Pilot or Copilot control column in order to check that it
is in neutral position.
6.Fit on the template, installed on the left elevator
trailing edge the comparator (AGE NO. 00062) and
set it to zero.
NOTE
The comparator must be no more zeroed
until the test is terminated.
NOTE
Care should be taken to apply the load to
the elevator T.E. and not to the tab T.E.
7.Apply, by a dynamometer (AGE NO. 00034), on the
right elevator trailing edge, a vertical load and
measure the elevator displacement as follows:
(Cont'd)
27-30-10
2-365