Fuel Exhaustion & Starvation · NTSB CEN19FA035
Piper PA 30 — Marion, IN
| Date | November 29, 2018 |
| Location | Marion, IN |
| Aircraft | Piper PA 30 |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Initial climb Loss of engine power (partial) |
| Pilot age | 60 |
| Pilot total time | 2,306 hrs · Experienced |
| Time in type | Unknown |
| Fatalities | 1 |
Probable cause
NTSB findings
- 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
- Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- Aircraft-Aircraft systems-Fuel system-(general)-Malfunction - F
- Not determined-Not determined-(general)-(general)-Unknown/Not determined - F
What happened
The airline transport pilot, who was also an airframe and powerplant mechanic, was conducting a personal flight in a twin-engine airplane after troubleshooting an unknown problem with the left engine fuel system; a family member described the flight as a "test flight." Witnesses reported that, after departure, the airplane climbed to about 500 ft above ground level and began a left turn. During the left turn, the airplane "nose dived" in a downward spiral, and the airplane impacted terrain.
Postaccident examinations revealed no mechanical anomalies with the airframe, right engine, or propellers that would have precluded normal operation. The left engine propeller blade damage was consistent with low or no power at the time of the accident, and the blades were found in an unfeathered position.
Evidence indicated that the pilot had recently replaced the left and right fuel selector valves and had been performing ground engine runs. A comprehensive examination of the airplane's fuel system was not possible due to the extensive fire damage to the system. However, given the unknown left engine fuel system issue, a loose left fuel selector fuel line, and the lack of power signatures on the left propeller blades, it is likely that the fuel system's performance was degraded and led to a partial or total loss of left engine power. The airplane's downward spiral was consistent with the pilot exceeding the airplane's critical angle of attack during a single-engine operation, which resulted in an aerodynamic stall and subsequent loss of control.
Toxicological testing detected a sedating antihistamine in the pilot's liver specimens, but not in his aortic blood specimens, making it less likely that the medication would be impairing. Thus, the pilot's use of this medication was likely not a factor in this accident.