Stall / Spin · NTSB MIA08FA081

Cirrus SR22 — Waxhaw, NC

1 fatal Base-to-final turn
DateMarch 20, 2008
LocationWaxhaw, NC
AircraftCirrus SR22
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceApproach-VFR pattern final Aerodynamic stall/spin
Pilot age51
Pilot total time604 hrs · Building experience
Time in type248 hrs
Fatalities1

Probable cause

The pilot's failure to maintain adequate airspeed while maneuvering to land, resulting in an aerodynamic stall. Contributing to the accident was the tailwind.

NTSB findings

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Not specified - F

What happened

The pilot announced over the common traffic advisory frequency his intention to land. The airplane approached the airport from the south at an altitude of approximately 800 feet, crossed the airport near mid-field, entered the traffic pattern for a left downwind to runway 6, and then crashed during the turn from left base to final. Winds were 310 degrees at 11 knots, gusting to 20 knots. This combination of wind direction and speed created a situation where grounds speed was higher than airspeed for the turn from base leg to final. The higher ground speed would have required a larger turning radius than normal, or an increased angle of bank than if the winds were calm. (Higher bank angles increase the probability of an airplane entering an aerodynamic stall.) Examination of the wreckage did not reveal any evidence of preimpact mechanical anomalies. Data extracted from the onboard global positioning system revealed that the airplane's last altitude was 838 feet; vertical speed was down -444 feet per minute, indicated airspeed was 60.3 knots, with a pitch attitude of up 4.98 degrees and a left roll of -31.73 degrees. These parameters indicate the airplane had or was about to enter the early phase of an aerodynamic stall.

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 →