1 fatality

2019-05-15: Beechcraft 60 Duke (N60RK) — Private United States of America — Loveland, United States of America

Loveland, United States of AmericaLanding (descent or approach)

On May 15, 2019, a Beechcraft 60 Duke (registration N60RK) operated by Private United States of America was involved in an aviation accident near Loveland, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: A loss of control due to an inflight right engine fire due to the loose fuel hose between the engine-driven fuel pump and the flow transducer. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781190965Data APIEditorial standards

A commercial pilot reported an engine failure and smoke in the cockpit while relocating a multiengine airplane after an avionics upgrade. Witnesses observed fire from the right wing, and the airplane impacted the ground near the airport perimeter fence. Investigation revealed a loose fuel hose on the right engine.

Accident Description

A commercial pilot was relocating a multiengine airplane following the completion of an extensive avionics upgrade, which also included the installation of new fuel flow transducers. As the pilot neared the destination airport, he reported over the common traffic advisory frequency that he had "an engine out [and] smoke in the cockpit." Witnesses observed and airport surveillance video showed fire emanating from the airplane's right wing. As the airplane turned towards the runway, it entered a right-rolling descent and impacted the ground near the airport's perimeter fence.

Examination Findings

Post-impact examination revealed that the right propeller was found feathered. Examination of the right engine showed evidence of a fire aft of the engine-driven fuel pump. The fuel pump was discolored by the fire. The fire sleeves on both the fuel pump inlet and outlet hoses were burned away. The fuel outlet hose from the fuel pump to the flow transducer was found loose. The reason the hose was loose was not determined. It is likely that pressurized fuel sprayed from the fuel pump outlet hose and was ignited by the hot turbocharger, which resulted in the inflight fire.

Probable Cause

The official probable cause stated by the investigation was a loss of control due to an inflight right engine fire due to the loose fuel hose between the engine-driven fuel pump and the flow transducer.