Cessna P210N accident near Burley, ID

On August 14, 2011, a Cessna P210N (airplane) was involved in an accident near Burley, ID. 4 people died. Damage to the aircraft: substantial.

Date
August 14, 2011
Place
Burley, ID
Aircraft
Cessna P210N · Airplane
Injuries
4 fatal, 0 serious, 0 minor
Damage
Substantial
Position
42.537°N, 113.773°W
NTSB ID
20110815X10520

Official records · WPR11FA382

NTSB summary

HISTORY OF FLIGHT On August 14, 2011, about 1430 mountain daylight time, a Cessna P210N, N7825K, impacted the terrain about one-eight mile off the departure end of runway 020 at Burley Municipal Airport, Burley, Idaho. The private pilot and his three passengers received fatal injuries, and the airplane, which was owned and operated by the pilot, sustained substantial damage. The 14 Code of Federal Regulations Part 91 personal transportation flight, which was in the takeoff sequence at the time of the accident, was departing for Provo Municipal Airport, Provo, Utah. No flight plan had been filed. On the day of the accident, the pilot and his immediate family were brought to the airport by extended family members who they had been visiting. After loading the family’s baggage into the airplane’s aft baggage compartment, the pilot was observed preforming a preflight inspection and then loading his family into the airplane. He then started the airplane’s engine and taxied to the approach end of runway 20. Because the view of the witnesses was temporarily blocked, it could not be determined if the pilot performed a run-up prior to turning onto the runway. Also, because of the distance from which family members were watching, it was also not possible to determine whether he started his takeoff roll where he first turned onto the runway, or whether he pulled forward to the 300-foot displaced threshold line prior to applying takeoff power. The airplane was then seen accelerating down the runway and lifting off at a location that was identified by a witness, and later determined to b

Probable cause

The pilot's failure to attain sufficient altitude and maintain aircraft control during a turn shortly after liftoff while operating at maximum gross weight, with a tailwind, and in high density altitude conditions.

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