Probable cause
The pilot receiving instruction’s failure to maintain rotor rpm during the pinnacle landing. Contributing to the accident was the flight instructor’s delayed remedial action.
NTSB analysis
During descent for an off-airport pinnacle landing, the helicopter encountered a downdraft about 75 to 100 feet above ground level (agl), and the pilot receiving instruction increased collective input. The flight instructor advised the pilot receiving instruction to be less aggressive using the collective as the flight continued to the landing area. As the helicopter descended through about 10 to 25 feet agl, it encountered a second downdraft, and the pilot receiving instruction increased collective again, which was followed by a decrease in rotor rpm. The flight instructor took control of the helicopter as it contacted the ground and then became airborne again. The helicopter yawed to the right and landed upright on sloping terrain. Postaccident examination of the helicopter revealed that the tailboom was substantially damaged just aft of the fuselage attach point. The pilots reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.
Text from the NTSB. Open the NTSB docket for WPR13CA155 for the full record.
Event
- Date
- Mar 18, 2013
- Type
- Accident
- Place
- Chino Valley, Arizona
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Robinson Helicopter R22 BETA
- N-number
- N223G
- Category
- Helicopter
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Instructional
Other records under this N-number
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.