1 fatality

1989-03-22: Piper PA-60 Aerostar (Ted Smith 600) (N77BR) — Top Flight Air Service — Jacksonville-Intl, United States of America

Jacksonville-Intl, United States of AmericaLanding (descent or approach)

On March 22, 1989, a Piper PA-60 Aerostar (Ted Smith 600) (registration N77BR) operated by Top Flight Air Service was involved in an aviation accident near Jacksonville-Intl, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The pilot failed to properly execute the IFR approach, specifically failing to maintain the glide slope and identify the required decision height. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781214285Data APIEditorial standards

A single-engine aircraft crashed into trees approximately 1.8 miles from the runway while attempting an ILS approach, resulting in the death of the pilot.

What happened

While performing an arrival procedure, the pilot was instructed to follow an ILS approach for runway 07. During this process, air traffic control notified the pilot of a DC-9 operating approximately 4 miles ahead of his position, advising him to remain vigilant regarding potential wake turbulence.

As the aircraft progressed on its final approach, it drifted below the established ILS glide slope. The descent continued until the aircraft struck trees and crashed roughly 1.8 miles short of the runway threshold. There was only one fatality in the accident, as the pilot was the sole occupant of the aircraft.

Findings

Investigations into the wreckage revealed no evidence of engine failure, mechanical malfunction, or structural disintegration prior to the impact. Furthermore, the ILS system was found to be functioning correctly and passed all post-accident testing.

Data from radar indicated that the flight path did not involve excessive g-forces or bank angles exceeding 32 degrees. An NTSB performance analysis determined that the aircraft was trailing the preceding DC-9 by 2 minutes and 57 seconds. The investigation concluded that the accident was caused by the pilot's failure to maintain the proper glide path and his inability to identify the correct decision height during the IFR procedure.

Probable cause

The pilot failed to properly execute the IFR approach, specifically failing to maintain the glide slope and identify the required decision height.