The plt stated that during cruise flt, he felt a severe vibration from the rear of the acft (the acft was a pusher type). He secured the eng. After touchdown in a field during the forced landing, the acft rolled inverted & came to rest. Exam of the acft revealed that a portion of one propeller blade delaminated at a knot.

| FAA | NTSB Final | News |


Posted By: Brett Ferrell
Wednesday April 11th, 1990 at 8:51 PM

Categories: Accidents
Tags: 1990 Accident FL N125V Non-Fatal RG SE Swing Velocity Wimauma

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