Loss of control and fatal impact involving single-engine aircraft

1 fatality • Bargo, Australia • Takeoff (climb)

A solo pilot was killed after their aircraft entered a near vertical descent and struck the ground during its climb phase.

What happened

Following an approved Standard Instrument Departure, the aircraft began an unrestricted climb toward a target altitude of Flight Level 220. During the initial stage of the ascent, the aircraft maintained an average climbing rate of 1300 feet per minute, reaching Flight Level 130. Upon reaching this altitude, the performance changed as the climb rate decreased to 350 feet per minute through Flight Level 140. Shortly thereafter, the climb rate increased again to 1800 feet per minute.

At Flight Level 160, the aircraft transitioned into a near vertical descent. Radar tracking was lost approximately one minute after this maneuver began, at an altitude of 3100 feet. The aircraft subsequently struck the ground while maintaining a near vertical attitude. There was one fatality involving the pilot, who was the only person on board.

Findings

Investigators were unable to identify the specific reason for the loss of control that led to the crash. While the investigation noted that other incidents involving sudden loss of control have been reported in this aircraft type, a certification review conducted by the Federal Aviation Administration did not reveal any findings relevant to this specific event.

Probable cause

The exact cause of the aircraft's loss of control could not be determined by investigators.

Frequently asked questions

What happened in the 1983-05-24 Mitsubishi MU-2 Marquise accident near Bargo, Australia?

A solo pilot was killed after their aircraft entered a near vertical descent and struck the ground during its climb phase.

Were there any fatalities in the 1983-05-24 Mitsubishi MU-2 Marquise accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 1983-05-24 involved a Mitsubishi MU-2 Marquise, registration VH-MLU, operated by Interair, at Bargo, Australia.

What was the probable cause of the accident?

The exact cause of the aircraft's loss of control could not be determined by investigators.

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