The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high velocity. The airplane recovers almost immediately after any deviation from the prospin control positions, except for one maneuver with reduced flexibility in the elevator control system.
Spin tests of a single-engine, high-wing light airplane
1982-01-01
Report
Keine Angabe
Englisch
Spin Tests of a Single-Engine, High-Wing Light Airplane
NTIS | 1982
|SAE Technical Papers | 1989
|High-speed tests of model twin-engine low-wing transport airplane
Engineering Index Backfile | 1942
|