Probable cause
The pilot’s failure to maintain adequate rotor rpm while descending with a gusting tailwind condition, which resulted in a loss of helicopter control.
NTSB analysis
The pilot of the helicopter reported that, while flying in mountainous terrain, he decided to land on top of a ridge for a rest break. The pilot performed a circling reconnaissance of the area before he began his descent to his intended landing spot. During the descent, the pilot felt a wind gust from behind, then the rotor rpm began to decay, and the low rotor rpm light illuminated along with the aural warning horn. The pilot attempted to reestablish power without success as the helicopter continued to descend. To avoid going over the ridge, the pilot intentionally lowered the helicopter to the ground and rolled the helicopter onto its right side. The helicopter sustained substantial damage to the fuselage and tail boom. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation.
Text from the NTSB. Open the NTSB docket for WPR22LA132 for the full record.
Event
- Date
- Mar 22, 2022
- Type
- Accident
- Place
- Howe, Idaho
- Highest injury
- Minor
- Minor injuries
- 2
- Weather
- Visual (VMC)
- Light
- Day
Robinson Helicopter Company R44 II
- N-number
- N44DQ
- Category
- Helicopter
- Year built
- 2005
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
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.