During a violent avoidance manoeuvre, a light twin aircraft, certified to FAR 23 requirements was subjected to an instantaneous load factor of 4.2. The Flight Manual specifies that the aircraft is certified in the normal category for a load factor of -1.9 to +3.8. Considering the certification requirements and taking into account that the manufacturer of the twin did not include, during its conception, a supplementary margin in the flight envelope, it might be possible to observe: A. rupture of one or more structural components B. a elastic deformation whilst the load was applied, but no permanent distortion C. no distortion, permanent or temporary of the structure D. a permanent deformation of the structure

 

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