Probable cause
The pilot’s failure to maintain helicopter control during an external load operation, which resulted in the helicopter’s main rotor blades impacting the tail boom.
NTSB analysis
The pilot reported that he was relocating bundles of trees from the harvest field onto a truck bed. Approximately 30 minutes into the operation, the load hook did not immediately release when he was setting a bundle down. The pilot pressed the release button multiple times, as he had done in similar situations in the past. The helicopter’s momentum, as it moved back towards the field, caused the bundle to slide a few feet. One of the main rotor blades then struck the tail boom, and the other blade flapped down, cutting off the rear section of the tail boom, vertical stabilizer, and tail rotor. The helicopter spun several times before landing, resting flat on the skids. The landing impact was forceful enough to break the mast and dislodge the main transmission. The helicopter sustained substantial damage to the main rotor, tail boom, vertical stabilizer, tail rotor, and transmission. The pilot reported that there were no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operations.
Text from the NTSB. Open the NTSB docket for WPR24LA036 for the full record.
Event
- Date
- Nov 15, 2023
- Type
- Accident
- Place
- Estacada, Oregon
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Dawn
Bell OH-58A
- N-number
- N103WC
- Category
- Helicopter
- Year built
- 1969
- Damage
- Substantial
- Operating rule
- Part 133 (external load)
- Purpose of flight
- External load
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.