14 fatalities

Air South Flight 168: In-Flight Control Issue Leads to Dive and Crash (N844NS)

Monroe, United States of AmericaFlight

On July 6, 1969, a Beechcraft 99 Airliner (registration N844NS) operated by Air South was involved in an aviation accident near Monroe, United States of America in flight. 14 people were killed. Investigators recorded the probable cause as: An unwanted change in longitudinal trim which resulted in a nosedown high-speed flight condition that was beyond the physical capability of the pilots to overcome. The initiating element in the accident sequence could not be specifically determined. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781237400Data APIEditorial standards

Air South Flight 168 experienced an unwanted change in longitudinal trim while cruising at 7,000 feet, leading to a nose-down dive that exceeded pilot control capabilities. Both wings failed at high speed before crashing.

Incident Overview

On a routine flight from Atlanta, Air South Flight 168 departed at 21:07. At 21:13, the crew reported reaching their assigned cruising altitude of 7,000 feet. The aircraft, a Beech, had been cruising for approximately eleven minutes when it gradually entered a nose-down attitude due to a change in longitudinal trim.

Pilot Response

Approximately six seconds after the trim change began, the pilots noticed the deviation and initiated recovery actions. However, the horizontal stabilizer continued to move to a full nose-down position. The pilots were required to apply excessive pulling force on the control column to attempt recovery from the resulting high-speed dive.

Aircraft Behavior

The necessary stick forces to control such an out-of-trim condition can exceed the physical capability of a single pilot, and in some cases, even two pilots. The Beech continued to descend until both wings failed at high speed, just before the airplane struck the ground in a near-vertical attitude.

Investigation Findings

The probable cause, as determined by the official investigation, was an unwanted change in longitudinal trim that resulted in a nose-down high-speed flight condition beyond the pilots' physical capability to overcome. The initiating element of the accident sequence could not be specifically determined. However, the design of the aircraft's flight control system was conducive to malfunctions that, if undetected by the crew, could lead to a loss of control.