PilotDAR:
The aircraft was equipped with an accelerometer
May I ask where they installed these accelerometers? In the wingtips?
Thanks for all the insightful replies! From all the feedback it looks like a speed buildup during the spin or recovery can be the cause of increasing load factor.
Can an airplane in a fully developed spin build up speed on it's own accord without control inputs, as a result of a forward CG or nose- down attitude? Is a spin really ,,stable'' ?
I guess there are a number of statements about spinning that are probably true ,,under most circumstances in most types of airplanes.''
Never spun before, but like to do with an instructor this summer. Thanks all
