Stall / Spin · NTSB WPR19FA159

Titan TITAN II — Summerville, OR

1 fatal Low altitude
DateJune 5, 2019
LocationSummerville, OR
AircraftTitan TITAN II (amateur-built)
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceManeuvering-low-alt flying Aerodynamic stall/spin
Pilot age29
Pilot total timeUnknown
Time in typeUnknown
Fatalities1

Probable cause

The noncertificated pilot’s exceedance of the airplane’s critical angle of attack while maneuvering at low altitude, which resulted in an aerodynamic stall/spin and impact with terrain.

NTSB findings

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Not attained/maintained
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Not specified

What happened

The non-certificated pilot was seen by witnesses flying at low altitude, which they described as near treetop and powerline level. One witness reported that the airplane entered a “straight up” climb about 300 ft, then dove to the ground and leveled the airplane about 50 ft above ground; the pilot did this three times before the accident occurred during the fourth maneuver. Another witness reported that, during the last maneuver, at the top of the climb, the airplane aerodynamically stalled, spun to the left, and impacted the ground.

Postaccident examination of the airframe and engine revealed no mechanical anomalies that would have precluded normal operation. Given the available evidence, it is likely that the pilot exceeded the airplane’s critical angle of attack, and the airplane entered an aerodynamic stall and spin.

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 →