Stall / Spin · NTSB ERA17FA153
HOWARD AIRCRAFT DGA 15P — Monongahela, PA
| Date | April 12, 2017 |
| Location | Monongahela, PA |
| Aircraft | HOWARD AIRCRAFT DGA 15P |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Approach-VFR go-around Aerodynamic stall/spin |
| Pilot age | 42 |
| Pilot total time | 1,109 hrs · Experienced |
| Time in type | 30 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-Angle of attack-Not attained/maintained - C
- Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Not specified
What happened
Witnesses observed the airplane touch down left of the runway centerline in gusting crosswind conditions and then attempt to go-around. As the engine noise increased, the airplane yawed 90° left and banked left, perpendicular to the runway. The airplane's nose pitched up, and the airplane subsequently entered an aerodynamic stall and rolled inverted before impacting a ravine about 400 ft left of the runway. Examination of the wreckage did not reveal any preimpact mechanical malfunctions that would have precluded normal operation. The airplane was equipped with a 450-hp radial engine. It is likely that, upon application of engine power to initiate the go-around, the pilot failed to adequately compensate for the extreme left-turning tendencies of the high-powered engine, which resulted in a subsequent loss of control and aerodynamic stall.