TCH.1C-27J-2-27JG
2-19.1 ADJUSTMENT AILERON REAR QUADRANT
(refer to figure
-the total resulting play C is defined as the mean
value between C1 and C2.
NOTE
The test sequence as reported by this
document (roll axis, pitch axis, yaw axis) is
not strictly mandatory; it can also be
exchanged if considered more convenient.
2-19.2 CONTROL WHEEL CABLE STIFFNESS CHECK
(refer to figure
) , (refer to figure
)
1.Lock the left differential lever using the differential
control levers locking tool (AGE NO. 00024).
2.Fit on Pilot control wheel the fixture control wheel
travel measurement tool (AGE NO. 00025) plus
inclinometer (AGE NO. 00061).
NOTE
Before to apply on the control wheel the tool
fixture control wheel maneuver force
measurementl, remove the chart holder light
(refer to manual
).
3.Using rigging pin (AGE NO. 00181), set the Pilot
control wheel to neutral position. Perform the the zero
calibration of the inclinometer(AGE NO. 00061).
4.Apply on the Pilot control wheel, by the dynamometer
(AGE NO. 00034), a lateral load and measure the
control wheel rotation as follows (Pilot control wheel
vs left differential lever locked):
A.Gradually apply a load leftwards up to 67.44 lb
(30.59 kg) maximum, reading the related control
rotation by means of inclinometer.
(Cont'd)
27-10-15
2-148