AFNOR test 16: Exit form symmetricla frontal tuck

Objectives

Simulation of a known effect of turbulence.

Procedures

Using the front risers, the pilot provoke a symmetrical frontal tuck, the release quickly the risers. During the maneuver the commands are not utilized.

Required results

Standard

Return spontaneous to normal flight in less than 4 sec, with a forward surge less than 450.

Performance

If the wing does not reinflate by itself, the pilot intervene and the wing must return to normal flight in less tan 4 sec, with a course change of less than 450 and a forward surge maximum of 900.

Competition

Test not imposed.

Twin

Test not imposed.
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