TCH.1C-27J-2-27JG
2-6.5
SPRING TAB FREE TRAVEL CHECK (refer to
figure
)
1.Ensure thath the LH and the RH spring tab is installed
without the LH and RH fail safe rod is linked (LH and
RH spring tab freely to move around the its hinge).
2.Insert the rig pin 0.193 in ( 4,915 mm) (AGE NO.
00181) in the differential levers at rib 24 ( LH and RH
side) in order to set the LH and RH aileron in neutral
position.
3.On the LH and RH aileron, fit the aileron check
template (AGE NO. 00064) in order to ensure that LH
and RH aileron is really set to 0
°
position ( this is
verified using the situable control template tool that
aligns the central part of the surfaces against the zero
reference mark indicated on the aileron check
template). Do not move the LH / RH aileron from this
zero position. Fit the inclinometer (AGE NO. 00061)
(parallel to the template using biadhesive tape) on the
LH /RH aileron surface. Switch on the inclinometers
(AGE NO. 00061), select the related angle and
perform the calibration so that the inclinometer shown
its 0 ° position. Remove the aileron check template
(AGE NO. 00064) and the situable control template
tool.
4.Fit on the LH and RH the aileron spring tab check
template (AGE NO. 00064) and on it the control rod
tool.
5.With the LH and RH aileron set to 0 ° position, move
by hand the LH and RH spring tab so that the central
part of the surface is aligned with zero reference mark
indicated on the aileron spring tab check template
(AGE NO. 00064). Hold by hand this position until
next step 6. is completed.
(Cont'd)
27-10-00
2-22