Probable cause
The pilot's failure to maintain control of the helicopter.
NTSB analysis
The helicopter pilot and three passengers were circling over rural terrain at an altitude of 150 feet above ground level and approximately 219 pounds overweight for the flight conditions when the pilot slowed to 10 knots with a tailwind. The helicopter began to lose main rotor rpm and the low-rotor aural warning sounded. The pilot lowered the collective in an attempt to maintain rotor rpm, but there was insufficient altitude to recover. The helicopter hit the ground with the tail rotor first and the body of the helicopter landed hard and skidded forward, crushing the left skid. The main rotors flexed downward during impact and severed the tailboom. The pilot reported that there were no preimpact mechanical deficiencies, and that the accident would likely not have happened if he had turned into a headwind.
Text from the NTSB. Open the NTSB docket for CEN09CA270 for the full record.
Event
- Date
- Apr 23, 2009
- Type
- Accident
- Place
- Kent, Texas
- Nearest airport
- None (None)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Robinson Helicopter Company R44 II
- N-number
- N518SJ
- 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.