2 fatalities

2021-04-23: Swearingen SA226T Merlin III (N59EZ) — Global Air — Winslow, United States of America

Winslow, United States of AmericaFlight

On April 23, 2021, a Swearingen SA226T Merlin III (registration N59EZ) operated by Global Air was involved in an aviation accident near Winslow, United States of America in flight. 2 people were killed. Investigators recorded the probable cause as: The loss of engine power to the right engine for reasons that could not be determined. Contributing to the accident was the pilot’s failure to maintain control of the airplane. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781190086Data APIEditorial standards

During a personal flight, the airplane descended toward the destination airport, performing several turns. Witnesses saw a low-flying airplane turn and veer toward the ground. A postcrash fire ensued. Investigation revealed the right engine had lost power for undetermined reasons, and the pilot failed to maintain control.

Accident Sequence

The pilot was conducting a personal flight and was descending the airplane toward the destination airport. Automatic dependent surveillance-broadcast (ADS-B) data showed that the airplane performed several turning maneuvers near the airport. These turns occurred from an elevation of 6,000 to 4,950 ft mean sea level, at which point the data ended. At that time, the airplane was 80 ft above ground level. Witnesses reported observing a low-flying airplane perform a turn and then veer toward the ground. The airplane came to rest about 4 miles east of the destination airport and 70 ft from the last data target. A postcrash fire ensued.

Postaccident Examination

Examination of the airframe and engines found no mechanical anomalies that would have precluded normal operation. The left engine was likely producing power at impact. The right engine examination revealed damage consistent with low or no rotation at the time of the accident, including distinct, localized contact marks on the rotating propeller shaft. No metal spray was found in the turbine section, and no dirt was found within the combustor section. The right propeller blades showed chordwise scoring with the blades bent aft and twisted toward a low-pitch setting. The fuel system had no anomalies.

The airplane was equipped with a single redline (SRL) autostart computer. Examination of the right (R) SRL-OFF annunciator panel light bulb showed signatures of hot filament stretch, consistent with illumination of the light at the time of the accident. The SRL light normally extinguishes above an engine speed of 80% rpm. Given the low rotational signatures on the right engine and the illuminated "R SRL-OFF" warning light, it is likely that the right engine lost engine power during the flight for reasons that could not be determined.

Probable Cause

The probable cause of the accident is the loss of engine power to the right engine for reasons that could not be determined. Contributing to the accident was the pilot’s failure to maintain control of the airplane.