Summary
On September 01, 2008, a Cessna 560 (N839QS) was involved in an incident near Telluride, CO. 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 failure to maintain control during landing. A factor was the reported wind shear.
On final approach to land, the twin jet airplane encountered an increasing headwind accompanied by a "Caution Wind shear" audio alert, while approximately 50 feet above ground level. The airplane landed hard and bounced several times before departing the left side of the runway. The airplane came to rest in an upright position and the pilot and copilot were able to exit the unassisted. The forward pressure bulkhead, fuselage, and left aileron sustained structural damage during the accident. In addition, the nose wheel assembly was found separated from the fuselage. An examination of the nose wheel assembly reveled that the fracture was consistent with an overload failure. No anomalies were reported with the airplane’s flight controls or engines.
This incident is documented in NTSB report DFW08CA221. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N839QS.
Accident Details
Probable Cause and Findings
The pilot's failure to maintain control during landing. A factor was the reported wind shear.
Aircraft Information
Analysis
On final approach to land, the twin jet airplane encountered an increasing headwind accompanied by a "Caution Wind shear" audio alert, while approximately 50 feet above ground level. The airplane landed hard and bounced several times before departing the left side of the runway. The airplane came to rest in an upright position and the pilot and copilot were able to exit the unassisted. The forward pressure bulkhead, fuselage, and left aileron sustained structural damage during the accident. In addition, the nose wheel assembly was found separated from the fuselage. An examination of the nose wheel assembly reveled that the fracture was consistent with an overload failure. No anomalies were reported with the airplane’s flight controls or engines.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW08CA221