01
DEC
2009

Safety Aspects of Light Aircraft Spin Resistance Concept

EASA_REP_RESEA_2008_3

The primary objective of the project is to investigate safety criteria and relevant test methods which will form the fundamental basis for proposing a change to CS-23 Certification Specification. To demonstrate that the proposed criteria are satisfactory flight trials with an existing spin resistant aircraft or modified aircraft will be carried out.

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