No fatalities

1973-11-27: Douglas DC-9 (N3323L) — Delta Airlines — Chattanooga-Lovell Field, United States of America

Chattanooga-Lovell Field, United States of AmericaLanding (descent or approach)

On November 27, 1973, a Douglas DC-9 (registration N3323L) operated by Delta Airlines was involved in an aviation accident near Chattanooga-Lovell Field, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The pilot did not recognize the need to correct an excessive rate of descent after the aircraft had passed decision height. This occurred despite two verbal reports of increasing sink rate by the first officer. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781232046Data APIEditorial standards

An aircraft on approach to Chattanooga Airport struck approach lights and terrain, resulting in minor injuries to seven passengers. The crew had received reports of increasing sink rate.

Incident Overview

An aircraft conducting a scheduled flight from Atlanta, Georgia, experienced an accident during its approach to Chattanooga Airport. The approach was conducted in poor weather conditions with heavy rain and limited visibility. On short final, the aircraft struck approach lights located 1,600 feet short of Runway 20 threshold. After striking the lights, the aircraft impacted the ground, separated its left wing, and skidded for an additional 1,200 feet before coming to rest 250 feet to the left of the runway centerline.

Occupant Status

All 79 occupants evacuated the aircraft safely. Seven passengers sustained minor injuries.

Probable Cause

The official investigation determined that the pilot did not recognize the need to correct an excessive rate of descent after the aircraft had passed decision height. This occurred despite two verbal reports of increasing sink rate by the first officer. The captain disregarded these reports, possibly due to the influence of a visual illusion caused by the refraction of light through the heavy rain on the windshield. The excessive rate of descent was initiated by a wind shear condition extending in the lower levels of the approach path and a glide slope that tended toward the lower signal limit.