Probable cause
The partial loss of engine power due to fuel contamination.
NTSB analysis
While performing an aerial application flight, the helicopter experienced a partial loss of engine power when the pilot advanced engine power to reverse course. The helicopter was substantially damaged during the forced landing when it contacted trees and landed hard. A postaccident examination of the helicopter’s engine found evidence of fuel contamination due to water and a non-ferrous material in the engine driven fuel pump/filter, fuel control unit, and fuel nozzle. The fuel control unit operated outside of acceptable limits during postaccident testing.
The airframe was stored outside and subjected to the elements after the accident; however, the location of the water and debris in the engine were in areas where contamination from the elements cannot normally collect. It could not be determined when the contamination occurred or whether it originated within the company’s fuel truck tank or within the helicopter’s fuel tank.
Text from the NTSB. Open the NTSB docket for CEN19LA309 for the full record.
Event
- Date
- Sep 9, 2019
- Type
- Accident
- Place
- Walkerton, Indiana
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Bell 206
- N-number
- N19TV
- Category
- Helicopter
- Year built
- 1979
- 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.