Probable cause
The pilot’s improper anti-torque pedal inputs during takeoff, which resulted in a loss of helicopter control during takeoff and subsequent dynamic rollover.
NTSB analysis
The pilot initially reported that while he was taking off, the tail dropped and hit the ground. After a postaccident review of a security video that captured the accident, the pilot along with his flight instructor concluded that he input excessive left anti-torque pedal as he increased collective. A National Transportation Safety Board review of the same security video showed the helicopter as it rotated counterclockwise about its vertical axis. The fuselage pivoted about the right skid and the helicopter exceeded its critical roll angle, which resulted in dynamic rollover. The helicopter sustained substantial damage to the fuselage and tailboom.
The pilot reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operations.
Text from the NTSB. Open the NTSB docket for WPR23LA214 for the full record.
Event
- Date
- Jun 3, 2023
- Type
- Accident
- Place
- Filer, Idaho
- Highest injury
- Minor
- Minor injuries
- 1
- Weather
- Visual (VMC)
- Light
- Day
Bell 206B
- N-number
- N205PA
- Category
- Helicopter
- Year built
- 1976
- 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.