= weight( ctrls1.elevator_trim, ctrls2.elevator_trim, ratio );
result.ctrls.rudder = weight( ctrls1.rudder, ctrls2.rudder, ratio );
result.ctrls.flaps = weight( ctrls1.flaps, ctrls2.flaps, ratio );
- result.ctrls.flaps_power
- = weight( ctrls1.flaps_power, ctrls2.flaps_power, ratio );
+ result.ctrls.flaps_power = ctrls1.flaps_power;
+ result.ctrls.flap_motor_ok = ctrls1.flap_motor_ok;
// Engine controls
for ( i = 0; i < ctrls1.num_engines; ++i ) {