Probable cause
A loss of engine power during takeoff for reasons that could not be determined, resulting in impact with terrain.
NTSB analysis
After takeoff from an agricultural load truck in a helicopter loaded with mixed liquid product to apply to a corn field, the pilot noticed a drop in rotor rpm. The pilot followed an area of terrain that sloped downward in an attempt to gain airspeed. The pilot attempted to increase rotor rpm but was unsuccessful. The pilot flared the helicopter while attempting to land; however, the helicopter impacted an area of rising terrain and came to rest on its left side. The pilot was able to exit the helicopter without further incident. The helicopter sustained substantial damage to the fuselage, main rotor system, tail cone, and tail rotor system.
Examination of the helicopter and engine revealed no indication of a pre-impact malfunction or failure that would have precluded normal operation. The governor system components were tested and no failures or malfunctions were found.
Although the atmospheric conditions at the time of the accident were conducive to serious icing at glide power, the reported power loss occurred while at takeoff power. Based on the available evidence, the reason for the loss of engine power described by the pilot could not be determined.
Text from the NTSB. Open the NTSB docket for CEN24LA303 for the full record.
Event
- Date
- Aug 3, 2024
- Type
- Accident
- Place
- Bryant, Iowa
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Robinson Helicopter R44
- N-number
- N225ML
- Category
- Helicopter
- Year built
- 2007
- Damage
- Substantial
- Operating rule
- Part 137 (agricultural)
- Purpose of flight
- Aerial application
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.