TCH.1C-27J-2-27JG
2-6.2
AILERON AND GEAR TRIM TAB TRAVEL
(Cont'd)
9.Turn control wheel fully left and keep it in this position:
-the left aileron must travel 26
°
±
1
°
upwards and
the right aileron must travel 19
°
±
1
°
downwards
position;
-the left gear trim tab must travel downwards 19.75
°
±
1
°
and right gear tab must travel upwards
15.75
°
±
1
°
(Make the difference between the
readings of the inclinometers (AGE NO. 00061)).
10.Remove all tools previously installed.
2-6.3
MEASUREMENT OF AILERON MANOUVRE
EFFORT (refer to figure
)
CAUTION
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Be sure that the No. 1 and No. 2
Hydraulic systems are not powered.
––––––––––––––––––––––––––––––––––
NOTE
This procedure is valid for LH control wheel.
For RH control wheel is similar.
1.Ensure that there aren't installed templates on Aileron
surface.
2.On the control wheel install the force measurement
fixture (AGE NO. 00025).
3.Rotate the control wheel fully rightwards and check
that the manoeuvre force required does not exceed 70
N (7.14 kg) (15.74 lb).
4.Rotate the control wheel fully leftwards and check that
the manoeuvre force required does not exceed 70 N
(7.14 kg) (15.74 lb).
5.By means of hydraulic test stand (AGE NO. 00262)
apply the hydraulic supply 3000 psi (210 Kg/cm
²
) and
verify that the results step 3 and 4 are the same.
(Cont'd)
27-10-00
2-20