2 fatalities

Loss of Control During Return to Airport Following Engine Power Loss (N149R)

Quincy-Baldwin Field, United States of AmericaLanding (descent or approach)

On February 18, 1987, a Beechcraft E18 (registration N149R) operated by Active Aero Charter was involved in an aviation accident near Quincy-Baldwin Field, United States of America during landing or approach. 2 people were killed. Investigators recorded the probable cause as: Occurrence #1: loss of engine power, reason undetermined. Occurrence #2: loss of control - in flight due to propeller feathering performed by pilot, improper in-flight planning/decision, improper emergency procedure, and airspeed (Vmc) not maintained. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

An aircraft on initial climb experienced a loss of engine power. The pilot attempted to return to the airport but stalled during a left bank and descended vertically, resulting in a fire and both occupants killed. The left propeller was found feathered.

Overview

On January 28, 1987, an aircraft at near gross weight (center of gravity unknown) was on initial climb after takeoff. A witness reported that the engines sounded normal. At about 400 feet above ground level, the aircraft pitched up approximately 10°, then leveled off and entered a left turn. The aircraft made another left turn to the south-southwest. The pilot reported that he was returning to the field, but did not state the nature of the problem.

Sequence of Events

The witness stated that the aircraft was in a 30° left bank, turning toward the airport, when the aircraft stalled and descended to the ground in a vertical nose-down attitude. A fire and explosion occurred after impact. The left propeller was found in the feathered position. No engine problem was found during post-accident examination.

Previous Incidents

On the same date, the left engine had lost power after takeoff; however, no problem was found and the condition could not be duplicated. The pilot had experienced two previous engine-out events in the same airplane, both at low weight. The surrounding terrain was suitable for an off-airport landing.

Probable Cause

The official probable cause findings were: Occurrence #1: loss of engine power, reason for occurrence undetermined. Occurrence #2: loss of control during maneuvering turn to landing area, attributed to propeller feathering performed by the pilot, improper in-flight planning/decision, improper emergency procedure, and failure to maintain airspeed (Vmc). Additionally, a wheels-up landing was not performed. Occurrence #3: in-flight collision with terrain during uncontrolled descent.