Objectives
Observation of the exit from a spin and verification of the stability on 3
axes.
Procedures
With the trim in Vmax position (if available), the pilot slows down
the wing until Vmin, then applies full brake on a side, releasing
completely the other, maintaining this position for 360 degrees, then
equilibrates the commands.
Required results
Standard
The wing must return spontaneously to normal flight, but can prosecute the
rotation for not more than 360 degrees in the same direction of the spin.
Performance
The wing can prosecute the rotation for not more than 360 degrees, the must
return spontaneously to normal flight in less than 90 degrees.
Competition
Test not imposed.
Twin
Same as Performance
