Are the 4 main factors (torque, pitch factor (p-factor), gyroscopic force, slipstream) that contribute to left turning tendency in an aircraft something that has only recently been taught in the FAA Private curriculum? Is it taught in other country's civil aviation certification curricula?
The reason I bring this up is because I ask this question in the registration form to prove the registrant is not a spam bot, and about 25% don't answer 1 of the above factors. I suppose it really doesn't matter as it's only an anti-spam measure, but come on!
Some answers I've gotten:
heavy left wing (I think this one was tongue in cheek
up aileron
prop inertia
left rudder (clever)
wind
yawing
pitch
lift
angle of attack
Cue the political jokes.



