Probable cause
The pilot's failure to maintain directional control during the hover taxi with a quartering tailwind.
NTSB analysis
The pilot reported that while hover taxiing, the helicopter encountered a quartering tailwind and immediately started to spin. The pilot attempted to correct the spin by reducing engine power; however, the helicopter touched down hard. During the hard landing, the left skid collapsed and the main rotor blades impacted the ground, which resulted in substantial damage to the main rotor system. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. At the time of the accident, the pilot was hover taxiing the helicopter to the north with wind from 170° at 18 knots.
Text from the NTSB. Open the NTSB docket for CEN26LA154 for the full record.
Event
- Date
- Mar 29, 2026
- Type
- Accident
- Place
- Oelwein, Iowa
- Nearest airport
- Oelwein Municipal Airport (OLZ)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Enstrom F-28F
- N-number
- N942MA
- Category
- Helicopter
- Year built
- 1988
- 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.