N232RP
We’re still collecting data for this aircraft. Routes appear once we’ve seen it fly enough times.
Safety history
- April 21, 1987Accident
VIBRATION WAS EXPERIENCED SHORTLY AFTER TOUCHDOWN CAUSED BY THE FAILURE OF THE PROPELLER BLADE AS A RESULT OF FATIGUE CRACKING WHICH WAS INITIATED FROM A LINEAR AREA IN A DEFECT FREE PORTION OF THE CAMBER FACE OF THE BLADE. PROPAGATION WAS THROUGH 60% OF THE BLADE CROSS SECTION BEFORE FINAL FAILURE. THE PROP BLADE HAD SEPARATED 23 INCHES FROM THE TIP AND DEFLECTED OFF THE RWY AWAY FROM THE FUSELAGE.