Probable cause
The pilot’s failure to maintain sufficient rotor rpm when transitioning the helicopter from a hover to forward flight, which resulted in a loss of helicopter control.
NTSB analysis
The pilot reported that he was surveying ranch land and that the helicopter was hovering about 12 to 15 feet above the ground just before the accident. While transitioning to forward flight, the helicopter was unable to maintain sufficient power and altitude. The low rotor rpm horn sounded, and the pilot decreased the collective to try to "fly out of it," but the helicopter was too close to the ground. The helicopter subsequently lost tail rotor effectiveness and spun around once before impacting the ground and rolling over. The pilot reported no mechanical failures or malfunctions with the helicopter that would have precluded normal operation.
Text from the NTSB. Open the NTSB docket for CEN14LA149 for the full record.
Event
- Date
- Feb 24, 2014
- Type
- Accident
- Place
- Presidio, Texas
- Highest injury
- Serious
- Serious injuries
- 1
- Weather
- Visual (VMC)
- Light
- Day
Robinson Helicopter Company R44 II
- N-number
- N360AH
- Category
- Helicopter
- Year built
- 2009
- 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.