Document: SLSA-MIP-5-4-0-US
Date of Issue: 05/2016
Revision: -
6-20
6.4.4.1
Adjusting aileron deflections
Range of deflections is adjusted by means of rod adjustable ends.
Adjust aileron neutral position by setting the terminal of the push rod in the center wing
or outer wing.
It is possible to adjust the aileron differentiation, i.e. difference in the lower and the upper
deflection of the aileron, by means of the terminal on the push rod leading from the
control lever in the fuselage to the bell crank in the wing or by means of the terminal of
the push rod leading from bell crank to the control lever on the aileron. The terminal is
accessible on the aileron lower side after lifting the aileron.
6.4.4.2
Adjusting wing flap deflections
Wing flap deflections are given by the torque tube and actuator positioning in the fuselage. It
is possible to adjust flap deflection by means of the terminals on push rods connected flaps
with control torque tube. The terminal is accessible on fully deployed flaps.
6.4.4.3
Adjusting elevator deflections
Range of elevator deflections is given by setting the push rod terminals in the fuselage. At
adjusting elevator deflections, proceed as follows:
Remove the chosen push rod from the bell crank.
Adjust the upper deflection as needed by means of the push rod terminal (or by means
of push rod terminal on the elevator lever).
Put push rod end back and check if the deflections corresponds to the values mentioned
in the Tab. 6-1.
6.4.4.4
Adjusting rudder deflections
Rudder deflections are given by setting the stops on the rudder control lever installed on fin
spar.
Set the foot control pedals to neutral position and check if the rudder is in the neutral
position.
Carry out correction of rudder deflection setting by adjusting the turnbuckles on the foot
pedal side in cockpit.
6.4.4.5
Adjusting trim tab deflections
Trim tab deflections are given by control actuator and they are fixed.
Summary of Contents for S-LSA
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