AFNOR test 14: Exit form spin
Objectives
Observation of the exit form a spin and verification of the stability on 3
axis.
Procedures
With the trim in Vmax position (if available), the pilot slow down
the wing until Vmin, then apply full brake on a side, releasing
completely the other, maintaining this position for 3600, then
equilibrate the commands.
Required results
Standard
The wing must return spontaneously to normal flight, but can prosecute the
rotation for not more than 3600 in the same direction of the spin.
Performance
The wing can prosecute the rotation for not more than 3600, the must
return spontaneously to normal flight in less than 900.
Competition
Test not imposed.
Twin
Same as Performance
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