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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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December 28, 1994 · Wyman Scorpion II Scorpion I · N65562

Cornish Flat, NH

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 28, 1994
Injury Outcomes
No injuries (1 uninjured)
Location
Cornish Flat, NH
Aircraft
Wyman Scorpion II Scorpion I
Tail Number
N65562
Injuries
None
Aircraft Damage
Destroyed
NTSB Number
NYC95DNC01

THE KIT BUILT HELICOPTER WAS ON FINAL APPROACH, WHEN THE PILOT EXPERIENCED A 'SEVERE' VIBRATION. HE ENTERED AN AUTOROTATION; HOWEVER, THE HELICOPTER ROTATED 180 DEGREES, AND STRUCK THE GROUND TRAVELING BACKWARDS. THE LOWER SURFACE OF ONE MAIN ROTOR BLADE HAD SEPARATED FROM THE TIP TO WITHIN 30 INCHES OF THE HUB. THE ALUMINUM BLADES HAD A TOTAL FLIGHT TIME OF 51 HOURS AND HAD BEEN CONSTRUCTED BY THE KIT BUILDER.

NTSB Probable Cause

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.

Full Narrative

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.

Flight

Event TypeAccident
Event Time14:00 EST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftWyman Scorpion II Scorpion I
Tail NumberN65562
Aircraft CategoryHeli
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotorway · RW-152G · Reciprocating · 152

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 45 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point36 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data