2 fatalities

Night Approach Accident at Barcelona Airport (EC-GDG)

Barcelona, SpainLanding (descent or approach)

On February 19, 1998, a Swearingen SA226 Metro II (registration EC-GDG) operated by Ibertrans Aérea was involved in an aviation accident near Barcelona, Spain during landing or approach. 2 people were killed. Investigators recorded the probable cause as: Inappropriate angle of descent during approach to runway 07 in low visibility, combined with possible crew fatigue and a potential left engine malfunction requiring yaw compensation, causing deviation from the approach path and descent below MDA. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A twin-engine aircraft crashed into a palm grove short of Runway 07 at Barcelona Airport during a night approach to Brussels. The incident resulted in the destruction of the airframe and the fatalities of both pilots.

Incident Overview

Shortly after departing Barcelona Airport for Brussels, the crew reported technical difficulties to air traffic control during a night operation. Following this report, the flight was authorized to return for an emergency landing on Runway 07.

Approach and Deviation

The crew initiated the approach procedure, descending sequentially to 6,000 feet and then 3,000 feet. At 00:15 seconds into the final phase, the aircraft crossed the outer marker at an altitude of 1,500 feet while maintaining a speed of 170 knots. As the aircraft progressed to a distance of six kilometers from the runway threshold, it began to drift laterally to the right of the intended approach path.

Impact and Aftermath

Approximately one minute after the deviation commenced, the aircraft impacted the ground at a speed of 130 knots. The crash site was located in a palm grove situated 3.2 kilometers short of the runway threshold. A post-crash fire subsequently destroyed the airframe completely. Both members of the flight crew were killed in the accident.

Investigation Findings

Official investigations could not definitively identify the specific technical issues reported by the crew, though a partial failure of the left engine remained a possibility that was not excluded. The probable cause was attributed to an inappropriate descent angle during the approach under low visibility conditions. Contributing factors included potential crew fatigue resulting from a long duty period and the need for yaw compensation due to a possible left engine malfunction. These elements combined led to the aircraft deviating from the glide path and descending below the minimum descent altitude until ground impact.