Summary
On March 08, 2007, a Sud Aviation SE3130 Alouette II (N226RW) was involved in an incident near Davenport, VA. All 2 people aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's inadequate visual lookout, which resulted in an in flight collision with utility wires during takeoff, and a subsequent impact with terrain.
The pilot of an Alouette II helicopter stated that he was flying a pipeline patrol, while the copilot monitored the pipeline on a laptop computer. During the patrol, the laptop computer malfunctioned, and the pilot landed in a field while the copilot attempted to repair the laptop computer. After the laptop computer was repaired, the pilot hover taxied to the end of the field, and began a takeoff run. During the takeoff run, at an altitude of 40 feet and airspeed of 30 to 40 knots, the helicopter struck utility wires. The helicopter subsequently impacted a field and came to rest on its right side. During the impact, the helicopter sustained substantial damage. The pilot did not report any preimpact mechanical malfunctions with the helicopter.
This incident is documented in NTSB report NYC07CA072. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N226RW.
Accident Details
Probable Cause and Findings
The pilot's inadequate visual lookout, which resulted in an in flight collision with utility wires during takeoff, and a subsequent impact with terrain.
Aircraft Information
Registered Owner (Historical)
Analysis
The pilot of an Alouette II helicopter stated that he was flying a pipeline patrol, while the copilot monitored the pipeline on a laptop computer. During the patrol, the laptop computer malfunctioned, and the pilot landed in a field while the copilot attempted to repair the laptop computer. After the laptop computer was repaired, the pilot hover taxied to the end of the field, and began a takeoff run. During the takeoff run, at an altitude of 40 feet and airspeed of 30 to 40 knots, the helicopter struck utility wires. The helicopter subsequently impacted a field and came to rest on its right side. During the impact, the helicopter sustained substantial damage. The pilot did not report any preimpact mechanical malfunctions with the helicopter.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC07CA072