Probable cause
The fuel exhaustion during cruise flight and the unsuitable terrain encountered by the pilot-in-command. A contributing factor was the trees.
NTSB analysis
The helicopter sustained substantial damage during a forced landing after a total loss of engine power during cruise flight. The helicopter was recently purchased by the left seat pilot, who did not hold a rotorcraft rating, and was being piloted by the right sear pilot at the time of the accident. The right seat pilot stated that he performed an autorotation on a hilltop, which was "sparsely populated" by 7-1/2 to 8 foot high trees. He also stated that the hilltop was the only available landing area, which was surrounded by "hostile" terrain. During the forced landing, the tail boom sustained damage on impact with trees. Examination of the helicopter revealed no usable fuel aboard.
Text from the NTSB. Open the NTSB docket for CHI08CA097 for the full record.
Event
- Date
- Mar 21, 2008
- Type
- Accident
- Place
- Franklin Furnac, Ohio
- Nearest airport
- Ashland Regional Airport (DWU)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Hughes 269A
- N-number
- N9333V
- Category
- Helicopter
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.