TCH.1C-27J-2-27JG
Consumable Material Required:
None
Safety Conditions:
maintenance.
PROCEDURE:
2-15.1
LEFT AILERON GEARED TRIM TAB TRAVEL
(refer to figure
) , (refer to figure
)
and (refer to figure
1.On left aileron fit the Aileron trim check template (AGE
NO. 00039) and aileron check templates (AGE NO.
00064).
2.Put the double side adhesive tape on the top surface
of the aileron and the geared trim tab, non in contact
with their rivets, and position on it the digital
inclinometers (AGE NO. 00061), parallel to the
templates. Put the aileron and the geared trim tab in
neutral position and reset the inclinometers, then
remove the templates.
3.Ensure the cover of the AILERON EMER switch (1),
on FCS 2 Control Panel (104 VE) (2), is lowered.
4.Set the trim button (8), on the Pilot control wheel (7)
from neutral position, to LH and maintain. Check that
the geared trim tab moves to 15.25
°
±
1
°
downwards
and the LH nipple of the aileron trim indicator (3) on
the Combined Trim Indicator (4) shows 15
°
down
(Tolerance -1 mm respectly to red strep).
(Cont'd)
27-10-10
2-120