Stall / Spin · NTSB DFW08FA060

CIRRUS DESIGN CORP SR22 — Lindsay, OK

2 fatal High-time pilotLow altitude
DateFebruary 2, 2008
LocationLindsay, OK
AircraftCIRRUS DESIGN CORP SR22
Purpose of flightInstructional
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceManeuvering Aerodynamic stall/spin
Pilot age53
Pilot total time1,327 hrs · Experienced
Time in type230 hrs
Fatalities2

Probable cause

The flight instructor's failure to maintain control of the airplane, which resulted in an inadvertent stall while maneuvering.

NTSB findings

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C

What happened

The certified flight instructor and the private pilot were returning to the airport in a single-engine airplane after completing a biennial flight review. Data obtained from the onboard primary flight display revealed that as the airplane approached the airport, it entered a snap roll maneuver, and began to descend. The airplane did not have enough altitude to recover and subsequently collided with terrain inverted approximately one-quarter of a mile away from the airport. Examination of the airframe and engine revealed there were no pre-mishap anomalies.

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 →