3 fatalities

1991-02-22: Mitsubishi MU-2 Marquise (N274MA) — Corporate Aviation Services — Tulsa, United States of America

Tulsa, United States of AmericaTakeoff (climb)

On February 22, 1991, a Mitsubishi MU-2 Marquise (registration N274MA) operated by Corporate Aviation Services was involved in an aviation accident near Tulsa, United States of America during takeoff. 3 people were killed. Investigators recorded the probable cause as: The shutdown of one engine for undetermined reasons, and the pilot's failure to maintain VMCA during a critical phase of flight. A factor in the accident was the pilot's improper emergency procedure. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781212208Data APIEditorial standards

An airplane on a required maintenance test flight after both engines were replaced experienced a right bank at about 500 feet agl, entered a vertical bank, and impacted in an inverted steep nose-down attitude. The right engine was found secured and feathered. Investigation revealed no pre-impact failure of engines or airframe systems. All three occupants were killed.

Accident Details

The aircraft was departing on a required maintenance test flight following the replacement of both engines. Witnesses reported that the takeoff roll and initial climb appeared normal. However, at about 500 feet above ground level, the airplane entered a right bank that continued until the wings were vertical and the nose dropped through. The airplane then impacted the ground in an inverted, steep nose-down attitude.

Investigation Findings

Examination of the wreckage revealed that the right engine had been secured and feathered. The subsequent investigation did not find any evidence of pre-impact failure or malfunction of either engine or any of the airframe systems. Engine mounting and rigging continuity could not be established due to impact damage. Evidence indicated that the landing gear was retracted and that the left spoiler was deployed at impact. The rudder trim was found in the neutral position. The pilot was a principal in the operator's organization and not one of the regular line pilots.

Probable Cause

The official probable cause was determined to be: "The shutdown of one engine for undetermined reasons, and the pilot's failure to maintain VMCA during a critical phase of flight. A factor in the accident was the pilot's improper emergency procedure." The emergency procedure taught in transition training is to use rudder trim as soon as possible after engine failure to preclude deployment of spoilers.