5 fatalities

1987-04-08: Lockheed C-130 Hercules (N517SJ) — Southern Air Transport — Travis AFB, United States of America

Travis AFB, United States of AmericaLanding (descent or approach)

On April 8, 1987, a Lockheed C-130 Hercules (registration N517SJ) operated by Southern Air Transport was involved in an aviation accident near Travis AFB, United States of America during landing or approach. 5 people were killed. Investigators recorded the probable cause as: Inadequate Southern Air Transport engine maintenance which allowed the accumulation of oil residues in the engine compressor sections until two engines were incapable of responding to rapid demands for increased power. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781216556Data APIEditorial standards

A Hercules aircraft on a training flight struck the perimeter fence at Travis AFB after a go-around due to two engines decelerating. The probable cause was inadequate maintenance allowing oil residue accumulation.

Flight History

The Hercules aircraft departed Travis Air Force Base at 14:45 for the second of a series of local training flights. Approaches and practice landings were conducted at McClellan Air Force Base before returning to Travis. A runway 21L ILS approach and full stop landing were scheduled to be performed by a first officer candidate.

Accident Sequence

During the approach, a balked landing occurred, forcing the captain to assume control and initiate a go-around. As the throttles were advanced, both the number one and number two engines decelerated. Subsequently, the aircraft banked left and struck the airport perimeter fence in a nose-low and steep left-wing low attitude.

Probable Cause

The official investigation determined the probable cause to be inadequate Southern Air Transport engine maintenance, which allowed the accumulation of oil residues in the engine compressor sections until two engines were incapable of responding to rapid demands for increased power. Contributing to the accident was the continuation of the go-around by the captain after power had been lost from two engines and the movement of the flap handle to the flaps retracted position during the go-around.