Stall / Spin · NTSB WPR14LA305

CESSNA 150M — Russian Flat, MT

1 fatal High-time pilot
DateJuly 21, 2014
LocationRussian Flat, MT
AircraftCESSNA 150M
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceTakeoff Aerodynamic stall/spin
Pilot age46
Pilot total time1,400 hrs · Experienced
Time in typeUnknown
Fatalities1

Probable cause

The pilot's inadequate preflight performance planning and his operation of the airplane outside of the manufacturer's specified performance limitations, which resulted in his exceedance of the airplane's critical angle of attack and a subsequent aerodynamic stall/spin.

NTSB findings

  • Personnel issues-Experience/knowledge-Knowledge-Knowledge of equipment-Pilot - C
  • Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
  • Personnel issues-Task performance-Use of equip/info-Use of charts-Pilot - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Attain/maintain not possible - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded - C

What happened

The commercial pilot attempted to take off from an uncontrolled grass runway with an uphill grade; the airplane subsequently impacted an open area of swamp land about 570 ft beyond the end of the runway. The airplane impacted in a right-wing, nose-low attitude; the impact damage was consistent with a near-vertical descent. Postaccident examination of the airframe and engine revealed no mechanical malfunctions or anomalies that would have precluded normal operation.

The density altitude at the time of the accident was calculated to be over 8,200 ft. Review of airplane manufacturer's takeoff performance charts revealed that the conditions present at the time of the accident exceeded the airplane's takeoff performance limitations. It is likely that, as the pilot attempted to take off uphill in high density altitude conditions, he exceeded the airplane's critical angle of attack, and the airplane experienced an aerodynamic stall/spin at low altitude.

An editorial "what led to it / how to avoid it" analysis for this accident is generated separately and will appear here.

View the official NTSB docket →