Summary
On December 28, 1994, a Wyman SCORPION II (N65562) was involved in an incident near Cornish Flat, NH. All 1 person aboard were uninjured. The aircraft was destroyed.
The National Transportation Safety Board determined the probable cause of this incident to be: PARTIAL FAILURE AND SUBSEQUENT PARTIAL SEPARATION OF SKIN ON THE UNDERSIDE OF ONE MAIN ROTOR BLADE, WHICH RESULTED IN A SEVERE VIBRATION, IN-FLIGHT LOSS OF AIRCRAFT CONTROL, AND IMPACT WITH THE GROUND DURING AN ATTEMPTED AUTOROTATION.
On December 28, 1994, at 1400 eastern standard time, a homebuilt, experimental, Scorpion II, helicopter, N65662, was destroyed during a forced landing, at Cronish Flat, New Hampshire. The student pilot, Curtis Wyman, was not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the flight which operated under 14 CFR Part 91.
The helicopter was on approach to a landing in an open field, when a vibration, which the pilot described as severe, developed. The pilot attempted to make an autorotation; however, he was unable to maintain directional control of the helicopter. It rotated 180 degrees, and struck the ground while traveling backwards.
This incident is documented in NTSB report NYC95DNC01. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N65562.
Accident Details
Probable Cause and Findings
PARTIAL FAILURE AND SUBSEQUENT PARTIAL SEPARATION OF SKIN ON THE UNDERSIDE OF ONE MAIN ROTOR BLADE, WHICH RESULTED IN A SEVERE VIBRATION, IN-FLIGHT LOSS OF AIRCRAFT CONTROL, AND IMPACT WITH THE GROUND DURING AN ATTEMPTED AUTOROTATION.
Aircraft Information
Registered Owner (Historical)
Analysis
On December 28, 1994, at 1400 eastern standard time, a homebuilt, experimental, Scorpion II, helicopter, N65662, was destroyed during a forced landing, at Cronish Flat, New Hampshire. The student pilot, Curtis Wyman, was not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the flight which operated under 14 CFR Part 91.
The helicopter was on approach to a landing in an open field, when a vibration, which the pilot described as severe, developed. The pilot attempted to make an autorotation; however, he was unable to maintain directional control of the helicopter. It rotated 180 degrees, and struck the ground while traveling backwards.
Examination of the helicopter revealed that the lower blade surface had separated, from the tip to within 30 inches of the hub. The aluminum blades were constructed by the owner as part of the kit. They had 50.9 hours on them since being built.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC95DNC01