TCH.1C-27J-2-27JG
2-6.5
SPRING TAB FREE TRAVEL CHECK (refer to
figure
) (Cont'd)
6.On LH and RH spring tab fit the digital inclinometer
(AGE NO. 00061), parallel to the aileron balance tab
check template (AGE NO. 00064), using adhesive
tape. Switch on the inclinometer (AGE NO. 00061),
select the related angle and perform the calibration so
that the inclinometer shown its 0° position.
2-6.6
SPRING TAB FREE TRAVEL CHECK (refer to
figure
).
1.On left aileron install balance tab templates and
aileron travel template put the double side
adhesivetape on the top surface of the ailerons and of
the tabs, non in contact with their rivets, andposition
on it the digital inclinometers, parallel to the templates.
2.Ensure that L aileron trim tab and the L balance tab
are to neutral position.
3.Reset the inclinometers, then remove the templates.
4.Check that the clearance between L balance tab and
aileron and between L aileron trim tab andaileron is
0.08 in + 0.04 / - 0 in (2 mm + 1 / - 0 mm); check that
the clearance between L balancetab and flap is 0.393
in ± 0.078 in (10 mm ± 2 mm), between L aileron
balance tab and L ailerontrim tab is 0.20 in ± 0.08 in
(5 mm ± 2 mm) and between L trim tab and aileron tip
is 0.24 in ± 0.08in (6 mm ± 2 mm).
5.Ensure that R outer balance tab and the R inner
balance tab are to neutral position.
(Cont'd)
27-10-00
2-23