Mechanical & Engine Failure · NTSB ANC16FA057
CHAMPION 7ECA — Chugiak, AK
| Date | August 13, 2016 |
| Location | Chugiak, AK |
| Aircraft | CHAMPION 7ECA |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Emergency descent Loss of control in flight |
| Pilot age | 43 |
| Pilot total time | 206 hrs · Low time |
| Time in type | Unknown |
| 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
- Aircraft-Aircraft power plant-Engine (reciprocating)-(general)-Inoperative - C
- Not determined-Not determined-(general)-(general)-Unknown/Not determined
What happened
According to multiple witnesses at the airport, they observed the airplane perform several touch-and-go landings throughout the late morning and early afternoon on the day of the accident. They added that the pilot then landed and taxied to a local fuel vendor's facility and refueled. The pilot then departed. Two witnesses who were near the departure runway reported that, after the airplane departed, they heard the engine making a "pop pop" sound and that it then appeared to lose power. Another witness near the runway reported hearing the engine "sputtering" and added that the airplane appeared to stall. All the witnesses reported that they observed the airplane turn right steeply, that its right wing and nose dropped abruptly, and that it then descended in a steep, nose-down attitude, consistent with an aerodynamic stall. A postimpact fire immediately ensued, which destroyed the airplane.
A postaccident examination of the airframe and engine revealed no mechanical malfunctions that would have precluded normal operation. The witnesses reported hearing noises consistent with an engine misfiring and it was likely losing power; however, the reason for the loss of engine power could not be determined based on the postaccident examination. After the loss of engine power, the pilot attempted a steep turn at low altitude, during which he failed to maintain proper airspeed and exceeded the airplane's critical angle of attack, which resulted in an aerodynamic stall and a loss of control at too low of an altitude to recover.