2 fatalities

1988-03-25: Cessna 421A Golden Eagle I (C-GVDG) — Starcraft Aviation — Albuquerque-Sunport, United States of America

Albuquerque-Sunport, United States of AmericaLanding (descent or approach)

On March 25, 1988, a Cessna 421A Golden Eagle I (registration C-GVDG) operated by Starcraft Aviation was involved in an aviation accident near Albuquerque-Sunport, United States of America during landing or approach. 2 people were killed. Investigators recorded the probable cause as: Loss of engine power (partial) due to fuel system misunderstanding, fuel exhaustion, and inadvertent fuel dumping; subsequent loss of control during descent due to inadvertent stall/spin. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781215391Data APIEditorial standards

A pilot and passenger were killed when their aircraft crashed while turning from base leg to final at Albuquerque International Airport. The flight experienced fuel exhaustion after a 4.4-hour trip with strong winds.

Accident Overview

On a business trip from Canada to the United States, a pilot and one passenger were killed when their aircraft crashed during the approach to Albuquerque International Airport. The accident occurred while the aircraft was turning from the base leg to the final approach.

Flight Details

The pilot had the aircraft's fuel tanks 'topped off' before departing from Kansas City. The flight plan indicated an enroute time of 3 hours 30 minutes to Albuquerque, with 5 hours 30 minutes of fuel onboard. However, strong enroute winds and turbulence, as forecast, resulted in an actual flight time of 4.4 hours.

Examination and Findings

Examination of the wreckage revealed no evidence of fuel in or around the aircraft. The manufacturer recommends using the main tanks for 90 minutes before switching to any auxiliary tank to prevent venting of return fuel overboard, which can diminish the fuel supply.

Probable Cause

The official investigation determined the probable cause involved two occurrences: first, a partial loss of engine power due to fuel exhaustion and inadvertent fuel dumping by the pilot, compounded by unfavorable wind conditions. Second, a subsequent loss of control during an uncontrolled descent resulting from an inadvertent stall/spin.