Probable cause
The pilot’s inadvertent cyclic control input after landing, which resulted in the main rotor blades striking the ground.
NTSB analysis
The helicopter pilot was supporting a seismic drilling operation at a remote drill site. He had just completed moving one of the seismic drills via long line and had landed the high-skid, turbine-powered helicopter in a clear area to wait for the next move. After landing, before reducing the power to flight idle and locking the flight controls, the pilot opened the right-side door, returned his right hand to the cyclic, and leaned out to ensure the tail rotor was clear of obstacles. While looking rearward, the pilot inadvertently moved the cyclic to the right, and the helicopter rolled up on the right skid. He immediately applied left cyclic, but the main rotor blades struck the snow. The helicopter sustained substantial damage to the rotor system, tail boom, and fuselage. The pilot indicated there were no preaccident mechanical malfunctions or anomalies that would have precluded normal operation. The pilot noted that the accident might have been avoided if he had used the collective lock before engaging in activities outside the cockpit.
Text from the NTSB. Open the NTSB docket for ANC13CA035 for the full record.
Event
- Date
- Mar 24, 2013
- Type
- Accident
- Place
- Stevens Village, Alaska
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Eurocopter AS350B3
- N-number
- N353DL
- Category
- Helicopter
- Damage
- Substantial
- Operating rule
- Part 133 (external load)
- Purpose of flight
- Business
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.