1 fatality

1997-03-19: Cessna 421A Golden Eagle I (N4050L) — MTK Jet — League City, United States of America

League City, United States of AmericaLanding (descent or approach)

On March 19, 1997, a Cessna 421A Golden Eagle I (registration N4050L) operated by MTK Jet was involved in an aviation accident near League City, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The pilot's failure to refuel the airplane which resulted in the loss of power to the right engine due to fuel exhaustion, and the pilot's failure to maintain airspeed during the single engine landing approach which resulted in a stall/spin. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781206213Data APIEditorial standards

A twin-engine aircraft on a night instrument approach to Galveston, Texas, impacted a lake after the pilot reported right engine loss and low fuel. Radar contact was lost 1 mile from an alternate airport, and a witness observed a spin. Flight time exceeded planned fuel endurance.

Flight and Approach

The twin-engine airplane departed San Diego, California, on a non-stop cross-country flight to Galveston, Texas. The pilot had filed a flight plan indicating fuel for 7 hours and 30 minutes. At the time radar contact was lost, 7 hours and 32 minutes had elapsed since departure.

The pilot had been cleared for a night instrument approach to Galveston when he reported losing the right engine and noted a low fuel supply. The controller vectored the airplane toward the nearest airport.

Accident Sequence

When the airplane was approximately 1 mile northeast of that airport, radar contact was lost. A witness observed the airplane enter a spin, descend in a nose-down attitude, and impact near the center of a lake.

Aircraft Examination

Post-accident examination of the airplane revealed no evidence of preimpact mechanical discrepancies. The landing gear was found extended, the flaps were set to about 15 degrees, and neither propeller was feathered.

The single-engine approach procedure in the airplane owner's manual specified that the landing gear should be extended when within gliding distance of the field, and flaps should be lowered only after landing is assured.

Probable cause

The pilot's failure to refuel the airplane which resulted in the loss of power to the right engine due to fuel exhaustion, and the pilot's failure to maintain airspeed during the single engine landing approach which resulted in a stall/spin.