8 fatalities

Flight Collides with Terrain During Base Turn in Fog (N2517X)

Lebanon-Springfield, United States of AmericaLanding (descent or approach)

On February 16, 1982, a Piper PA-31 Cheyenne (registration N2517X) operated by GNC Energy Corporation was involved in an aviation accident near Lebanon-Springfield, United States of America during landing or approach. 8 people were killed. Investigators recorded the probable cause as: Occurrence #1: in flight collision with terrain/water Phase of operation: approach - VFR pattern - base turn Findings 1. (f) light condition - dark night 2. (f) weather condition - fog 3. (c) aborted landing - not performed - pilot in command 4. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Source recordUpdated 2026-07-04Data APIEditorial standards

Aircraft on approach collided with terrain in left-wing-low attitude during base turn. Witnesses reported thick fog, limited visibility. Altimeter improperly set.

Background

The flight was cleared to maintain 3,000 ft mean sea level (msl) until over the airport, then cruise. The pilot reported seeing lights on the ground and stated he was 15 miles from the airport.

Flight Progress

At 2013, the pilot said, "we oughta be able to cancel here." At that time, the aircraft was approximately 6 miles from the airport. The airport operator heard an aircraft flying low overhead and was able to see stars. Ground witnesses closer to the impact point reported very thick patchy fog with visibility around 200 ft. One witness observed the aircraft's navigation lights performing unusual maneuvering, while another saw the lights very low.

Accident Sequence

The aircraft impacted the ground in a left wing low, near level flight attitude. The wreckage was found in an area consistent with a downwind-to-base leg turn.

Approach Information

The airport has a single VOR/DME approach to runway 11, with a minimum descent altitude (MDA) of 1,260 ft and required visibility of 1 mile. The circling approach has an MDA of 1,420 ft and also requires 1 mile visibility.

Altimeter Setting

The pilot received an altimeter setting of 29.77. However, the aircraft's altimeter was set between 30.29 and 30.30.

Probable Cause

The official probable cause findings cite an in-flight collision with terrain during the approach phase (VFR pattern, base turn). Identified factors include dark night, fog, the pilot not performing an aborted landing, not maintaining proper altitude, and improper altimeter setting.

Frequently asked questions

What happened in the 16 Feb 1982 Piper PA-31 Cheyenne accident near Lebanon-Springfield, United States of America?

Aircraft on approach collided with terrain in left-wing-low attitude during base turn. Witnesses reported thick fog, limited visibility. Altimeter improperly set.

Were there any fatalities in the 16 Feb 1982 Piper PA-31 Cheyenne accident?

The accident was fatal, resulting in 8 fatalities.

What aircraft was involved and where did it happen?

The accident on 16 Feb 1982 involved a Piper PA-31 Cheyenne, registration N2517X, operated by GNC Energy Corporation, at Lebanon-Springfield, United States of America.

What was the probable cause of the accident?

Occurrence #1: in flight collision with terrain/water Phase of operation: approach - VFR pattern - base turn Findings 1. (f) light condition - dark night 2. (f) weather condition - fog 3. (c) aborted landing - not performed - pilot in command 4. (c) proper altitude - not maintained - pilot in command 5. (f) altimeter…