No fatalities

1993-09-19: Swearingen SA227 Metro III (F-GILN) — Airlec — Troyes, France

Troyes, FranceTakeoff (climb)

On September 19, 1993, a Swearingen SA227 Metro III (registration F-GILN) operated by Airlec was involved in an aviation accident near Troyes, France during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The accident appears to be due to a combination of a positioning error of the Speed Levers at the time of take-off, leading to the overheating of both engines, which forced the take-off to stop, and to the preparation and insufficient management of the… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781209619Data APIEditorial standards

A chartered aircraft experienced right engine power loss during takeoff from Troyes-Barberey Airport, veered right, and was unable to stop, overrunning the runway and colliding with a localizer antenna. All 19 occupants escaped uninjured; the aircraft was written off.

Incident Details

A chartered aircraft was departing from Troyes-Barberey Airport in France, tasked with transporting 17 individuals who had been involved in a bus accident two days earlier to Biggin Hill, United Kingdom. During the takeoff roll, after covering 1,100 meters at a speed of approximately 100 knots, the right engine's power dropped from 93% to 40%. Simultaneously, the temperature of the right engine increased. The aircraft began to veer to the right, prompting the captain to abort the takeoff and initiate emergency braking.

Despite the braking effort, the aircraft could not stop within the remaining runway distance. It overran the runway, rolled for about 150 meters, penetrated a fence, and ultimately collided with the localizer antenna. All 19 occupants evacuated without injury, but the aircraft sustained substantial damage and was declared a total loss.

Probable Cause

The official investigation determined that the accident likely resulted from a combination of factors: a mispositioning of the Speed Levers at the time of takeoff, which caused overheating of both engines and forced the takeoff to be aborted; and inadequate preparation and management of the takeoff, leading to an underestimation of the acceleration-stop distance and a delayed decision to reject the takeoff.

Contributing Factors

Several contributing factors were identified:

  • Fouling of the brakes, which reduced their effectiveness.
  • Failure to update the aircraft's base weight in the operations manual.
  • The crew's very limited experience on the aircraft type.
  • The aircraft's total weight was 300 kg above its maximum takeoff weight (MTOW).

These factors collectively compromised the aircraft's ability to safely abort the takeoff within the available runway length.