Objectives
Verification of the possibility of returning to normal flight in
consequence of an involuntary asymmetrical stall.
Procedures
The pilot slows down the wing until Vmin, then apply full brake to
one side, until he provokes an asymmetrical stall, then releases quickly both
the commands.
Required results
Standard
Spontaneous return to normal flight, with a course change less than 90 degrees.
Performance
If the wing does not reinflates by itself, the pilot applies the indication
of the wing Owner's Manual, and the wing must return to normal flight
with a course change less than 90 degrees.
Competition
Test not imposed.
Twin
Same as Performance
