
EN
Center of Gravity (CG)
Control Direction Tests
Assemble the aircraft and bind your transmitter to the receiver before
performing this test.
After binding a transmitter to the aircraft receiver, set the trims and
sub-trims to 0, then adjust the clevises to center the control surfaces.
Move the controls on the transmitter to make sure the aircraft control
surfaces move in the proper direction.
Transmitter
Command
Aircraft Reaction
Elevator
Up Elevator
Command
Down
Elevator
Command
Aileron
Stick Right
Stick Left
Rudder
Stick Right
Stick Left
The CG location is measured from the leading edge of the wing at the root.
This CG location has been determined with the recommended Li-Po battery
installed near the center of the battery compartment.
Tip: You can fl y your aircraft inverted to confi rm CG is correct. The aircraft
should fl y level when fl ying inverted at ¾ throttle with little or no elevator
down pressure. If the aircraft CG is too far forward (nose-heavy), signifi cant
down elevator is required to fl y level. If the aircraft CG is too far aft (tail-heavy),
up elevator is required to fl y level.
125-130mm
back from lead-
ing edge at
the root.
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