Stall / Spin · NTSB ERA15FA076
TITAN TORNADO II — Catlett, VA
| Date | December 14, 2014 |
| Location | Catlett, VA |
| Aircraft | TITAN TORNADO II |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Maneuvering-low-alt flying Aerodynamic stall/spin |
| Pilot age | 33 |
| Pilot total time | 157 hrs · Low time |
| Time in type | 2 hrs |
| Fatalities | 1 |
Probable cause
NTSB findings
- Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Not attained/maintained - C
What happened
The sport pilot departed on a local flight, his third flight in the accident airplane. Review of radar data indicated that the flight maneuvered in the local area for about 13 minutes before the accident occurred. One witness stated that the airplane was flying level about 150 feet above ground level when the engine began to sound like it was "missing." He then stated that the airplane then began a series of three 360-degree, level right-hand turns while over a wooded area. Upon completion of the third turn, the engine noise stopped, and the airplane descended vertically into the trees below. Examination of the accident site indicated a relatively short debris path, consistent with a steep descent. The witness observations and the impact geometry are consistent with the pilot's failure to maintain adequate airspeed while maneuvering, resulting in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall.
The engine was successfully operated after the accident at power settings ranging from idle to full power. While the weather conditions around the time of the accident were conducive to the formation of carburetor icing at glide engine power settings, the airplane was maneuvering in level flight before the accident so the throttle was likely set above a glide power setting. Examination of the engine and fuel system revealed no evidence of pre-impact failure or malfunction; however, no definitive determination could be made regarding the engine's operational state at the time of impact.