Carlsbad – Reno

On August 28, 2006 at 03:06 PM, Carlsbad – Reno experienced a crash involving Hawker 800XP, operated by NetJets, with the event recorded near Carson City Nevada.

The flight was categorized as charter/taxi (non scheduled revenue flight) and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

5 people were known to be on board, 0 fatalities were recorded, 5 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 2, crew fatalities: 0, passengers on board: 3, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. The Hawker and the glider collided in flight at an altitude of about 16,000 feet above mean sea level about 42 nautical miles south-southeast of the Reno/Tahoe International Airport (RNO), Reno, Nevada, which was the Hawker's destination. The collision occurred in visual meteorological conditions in an area that is frequently traversed by air carrier and other turbojet airplanes inbound to RNO and that is also popular for glider operations because of the thermal and mountain wave gliding opportunities there. Before the collision, the Hawker had been descending toward RNO on a stable northwest heading for several miles, and the glider was in a 30-degree, left-banked, spiraling climb. According to statements from the Hawker's captain and the glider pilot, they each saw the other aircraft only about 1 second or less before the collision and were unable to maneuver to avoid the collision in time. Damage sustained by the Hawker disabled one engine and other systems; however, the flight crew was able to land the airplane. The damaged glider was uncontrollable, and the glider pilot bailed out and parachuted to the ground. Because of the lack of radar data for the glider's flight, it was not possible to determine at which points each aircraft may have been within the other's available field of view. Although Federal Aviation Regulations (FARs) require all pilots to maintain vigilance to see and avoid other aircraft (this includes pilots of flights operated under instrument flight rules, when visibility permits), a number of factors that can diminish the effectiveness of the see-and-avoid principle were evident in this accident. For example, the high closure rate of the Hawker as it approached the glider would have given the glider pilot only limited time to see and avoid the jet. Likewise, the closure rate would have limited the time that the Hawker crew had to detect the glider, and the slim design of the glider would have made it difficult for the Hawker crew to see it. Although the demands of cockpit tasks, such as preparing for an approach, have been shown to adversely affect scan vigilance, both the Hawker captain, who was the flying pilot, and the first officer reported that they were looking out the window before the collision. However, the captain saw the glider only a moment before it filled the windshield, and the first officer never saw it at all.

Aircraft reference details include registration N879QS, MSN 258379, year of manufacture 1998.

Geospatial coordinates for this crash are approximately 39.1663°, -119.7670°.