Mechanical & Engine Failure · NTSB ERA16FA168

RYSKAMP BRUCE A ACRODUSTER — Belton, SC

1 fatal
DateApril 24, 2016
LocationBelton, SC
AircraftRYSKAMP BRUCE A ACRODUSTER (amateur-built)
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceApproach-VFR pattern downwind Loss of engine power (total)
Pilot age62
Pilot total time420 hrs · Building experience
Time in typeUnknown
Fatalities1

Probable cause

A loss of engine power for reasons that could not be determined due to extensive postcrash fire damage. Also causal was the pilot's loss of airplane control, resulting in an aerodynamic stall and subsequent impact with terrain.

NTSB findings

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Engine out control-Not attained/maintained - C
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
  • Aircraft-Aircraft power plant-(general)-(general)-Inoperative - C

What happened

The pilot was returning to the airport from a local personal flight. The airplane completed two low approaches and then made a left turn to reenter the traffic pattern. Two witnesses reported that, when the airplane was on the downwind leg of the traffic pattern, the engine sound changed; one reported that the engine sputtered and "cut out." The airplane then banked left and pitched nose down before impacting the ground, consistent with an aerodynamic stall. The propeller governor was examined, and no pre-impact anomalies were noted. The examination noted scrape marks on the propeller governor. According to the manufacturer, the scrape marks were made when the gears were turning opposite the direction of normal rotation, indicating that the propeller was not rotating to propel the airplane forward when the marks were made. An examination of the airframe and engine revealed no evidence of pre-impact mechanical malfunctions or failures; however, extensive thermal damage precluded a detailed examination. Additionally, the airplane's fuel state prior to the accident could not be accurately determined.

Toxicological testing identified 0.024 ug/ml of diphenhydramine in heart blood and detected diphenhydramine in urine. The postmortem blood diphenhydramine level was below the therapeutic range, which suggests that the pilot's level was likely below therapeutic and impairing levels at the time of the crash. Therefore, it is unlikely that the pilot's use of diphenhydramine at some time before the accident flight contributed to the accident.

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 →