QQ CAP 232EX 60E Super PNP Manual

FLIGHT CONTROL SENSING DIRECTION TEST
Aircraft
Movement
Proper Control
Surface Deflection
AILERONELEVATOR
RUDDER
Perform a test of the gyro system to verify the corrections made for a given movement are correct. If any of the tests do not result in the
correct reaction for the airplane's gyro system, DO NOT FLY THE AIRPLANE, and contact us via email at [e-mail].
The flight control system activates with RF broadcast. Perform these tests in Mode 3 (higher gain) for better visibility, and then again in
Mode 2, and any other flight modes that have gyro gains assigned. (By default, Mode 1 has no gain assigned.) Control surface deflections
are exaggerated in the drawings below for clarity. Please note that the control surfaces will move ONLY while the aircraft is ROTATING.
16
10.7
10.7