Probable cause
A loss of helicopter control for reasons that could not be determined because postaccident examination did not reveal any evidence of mechanical malfunctions or failures of the main rotor and tail rotor systems that would have precluded normal operation.
NTSB analysis
The commercial pilot stated that he was using the helicopter to round up cattle. He applied power to stabilize in a hover about 50 ft above the ground when he heard a single loud bang and "felt it in the pedals." The helicopter spun to the right, and the pilot applied full left pedal, which had no effect on the helicopter. The pilot stated that after about two spins, he entered an autorotation to remove torque from the rotor system. The helicopter contacted trees as it descended to the ground and came to rest upright with the tailboom separated.
Postaccident examination of the wreckage did not reveal any evidence of mechanical malfunctions or failures of the main rotor and tail rotor systems that would have precluded normal operation; thus, the reason for the loss of control could not be determined.
Text from the NTSB. Open the NTSB docket for CEN18LA069 for the full record.
Event
- Date
- Jan 8, 2018
- Type
- Accident
- Place
- Albany, Texas
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Robinson Helicopter Company R44 II
- N-number
- N797JR
- Category
- Helicopter
- Year built
- 2006
- 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.