Objectives
Verification of the wing pitch stability.
Procedures
With trim set for Vmax, the pilot slows down the wing using the
commands. At the stall point, the commands are released quickly.
Required results
Standard
The forward surge must not exceed 45 degrees. Tucks are accepted if they do not
cause route changes.
Performance
The maximum forward surge is 90 degrees, Tucks are accepted if they do not cause
route change in excess of 90 degrees and the return to flight is spontaneous.
Competition
Test not imposed.
Twin
Test not imposed.
