Hughes 369D accident near Columbus, MT

On May 28, 2007, a Hughes 369D (helicopter) was involved in an accident near Columbus, MT. 1 person died. Damage to the aircraft: destroyed.

Date
May 28, 2007
Place
Columbus, MT
Aircraft
Hughes 369D · Helicopter
Injuries
1 fatal, 2 serious, 0 minor
Damage
Destroyed
Position
45.723°N, 109.155°W
NTSB ID
20070612X00715

Official records · SEA07LA135

NTSB summary

On May 28, 2007, approximately 1340 mountain daylight time, a Hughes 369D helicopter, N765HV, impacted the terrain during an attempted forced landing, after experiencing a complete loss of engine power near Columbus, Montana. The commercial pilot and one crewmember received serious injuries, and a second crewmember was killed. The helicopter, which was owned by Dylan Aviation, LLC., and operated by Haverfield Corporation, was destroyed by the impact and post-crash fire. The 14 CFR Part 91 aerial observation flight, which departed Billings Logan International Airport, Billings, Montana, about 50 minutes prior to the accident, was being operated in visual meteorological conditions. The flight, for which a company visual flight rules (VFR) flight plan had been filed and activated, was intended to terminate back at Billings. The ELT was activated by the accident sequence. According to the pilot, the helicopter, which was being used for comprehensive visual inspection of power lines and power line support structures, was in a stationary hover about 120 above ground level (AGL), when it experienced a sudden and complete loss of engine power. The pilot, who's direction of maneuver was limited by the presence of the power line support structure that was being inspected, initiated an autorotation to an emergency forced landing. Although the helicopter contacted the relatively level grassy ground in a upright attitude, the impact forces where high enough that both front seat crewmembers sustained serious injuries, and the helicopter's airframe was distorted. The two front seat crewme

Probable cause

The fatigue failure of a turbine blade due to a localized over-temperature of the turbine section as result of a non-uniform fuel distribution by the fuel nozzle. Contributing to the accident was the close proximity of a power line support structure which restricted maneuverability for a successful autorotation.

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