1 fatality

Aircraft Collides with Terrain During Approach to Runway 36R (N6459L)

Charlotte-Douglas, United States of AmericaLanding (descent or approach)

On November 15, 1983, a Piper PA-31-310 Navajo (registration N6459L) operated by Southeast Airmotive was involved in an aviation accident near Charlotte-Douglas, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: reason for occurrence undetermined. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

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

Aircraft on radar vectors for runway 36R turned past assigned heading and descended, losing radar contact at 900 feet. Wreckage found along 245° heading. Runway edge lights not visible beyond 30° of centerline during night VFR inspection.

Incident Overview

An aircraft on an instrument approach to an airport was first identified on radar approximately 18 miles north of the field. Air traffic control provided radar vectors for a right downwind and base leg to runway 36R. While established on a downwind heading of 150°, the pilot was instructed to turn to a heading of 270° and asked if the airport was in sight. The pilot replied, '...we got it.' However, radar data indicated the aircraft continued its turn beyond the assigned heading, passing through 270° and reaching approximately 350°.

Sequence of Events

After traveling about half a mile on the 350° heading, the aircraft turned left to a heading of 250° and began descending. The turn continued until the aircraft was aligned on a southwest heading, roughly following a city street that passes south of the airport on a course of 250°. The altitude decreased at a consistent rate until reaching 900 feet, at which point radar contact was lost. The elevation at the approach end of runway 36R is 724 feet.

Wreckage and Lighting Conditions

The wreckage distribution was located along a heading of 245°. A flight inspection conducted at night under visual flight rules (VFR) determined that the edge lights of runway 36R were not visible beyond 30° of the runway centerline.

Pilot Activities

The pilot had awakened at 0730 on the day of the accident, November 14.

Probable Cause

The official probable cause was determined to be: reason for occurrence undetermined.