No fatalities

2003-01-17: BAe Jetstream 31 (CP-2404) — Servicio Aéreo Vargas España - SAVE — Yacuiba, Bolivia

Yacuiba, BoliviaLanding (descent or approach)

On January 17, 2003, a BAe Jetstream 31 (registration CP-2404) operated by Servicio Aéreo Vargas España - SAVE was involved in an aviation accident near Yacuiba, Bolivia during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The accident was the consequence of the combination of the following factors: - Excessive speed upon landing, - Delayed application of the brake systems, - The runway length available was limited according to the conditions in force, - The total weight of the… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781201350Data APIEditorial standards

During takeoff roll at Yacuiba Airport, right engine lost power at V2. Crew continued takeoff and returned for emergency landing, but aircraft overran runway 20 after touchdown. All 21 occupants escaped uninjured; aircraft damaged beyond repair.

Incident Details

During the takeoff roll at Yacuiba Airport, the right engine lost power precisely when the aircraft reached V2 speed. The captain decided to continue the takeoff procedure. During the initial climb, the crew decided to return for an emergency landing. The crew shut down the right engine and feathered its propeller.

After touchdown on runway 20, the aircraft was unable to stop within the remaining distance. It overran the runway, lost its nose gear, and collided with bushes and small trees. The aircraft came to rest approximately 50 metres past the runway end. All 21 occupants escaped uninjured, while the aircraft was damaged beyond repair.

Probable Cause

The official investigation determined that the accident was the consequence of the combination of the following factors: - Excessive speed upon landing, - Delayed application of the brake systems, - The runway length available was limited according to the conditions in force, - The total weight of the aircraft upon landing, - The aircraft configuration, - The direction and intensity of the wind, - An inadequate crew training. Additionally, the exact cause of the loss of power on the right engine was not clearly determined at the time the final report was published.