Stall / Spin · NTSB ERA17FA123

JORDAN BRUCE C PITTS S2E — Apex, NC

1 fatal High-time pilotBase-to-final turn
DateMarch 8, 2017
LocationApex, NC
AircraftJORDAN BRUCE C PITTS S2E (amateur-built)
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceApproach-VFR pattern final Aerodynamic stall/spin
Pilot age80
Pilot total time1,933 hrs · Experienced
Time in type96 hrs
Fatalities1

Probable cause

The pilot's failure to maintain airplane control during the final approach to the runway in gusting tailwind conditions, which resulted in the airplane exceeding its critical angle of attack and an aerodynamic stall.

NTSB findings

  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on operation - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Not attained/maintained - C

What happened

The pilot was returning to the airport from a local personal flight in the airplane. The airplane approached runway 9 at an angle before rolling inverted, descending, and impacting terrain, consistent with an aerodynamic stall. A review of weather conditions revealed that, on final approach, the airplane likely experienced a tailwind of about 9 knots with wind gusts as high as 20 knots. Pilots familiar with the airport reported that, due to the slope of the runway, pilots preferred to land on runway 9 unless there was a tailwind of more than 10 knots. Postaccident examination of the airplane and engine revealed no evidence of mechanical malfunctions or anomalies that would have precluded normal operations. It is likely that, while maneuvering on final approach to the runway with a gusting tailwind, the pilot failed to maintain control of the airplane, which resulted in the exceedance of the airplane's critical angle of attack and 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 →