No fatalities

2003-03-15: PZL-Mielec AN-2 (LY-KAG) — Klaipedos Avialinijos (Air Klaipeda) — Samedan, Switzerland

Samedan, SwitzerlandTakeoff (climb)

On March 15, 2003, a PZL-Mielec AN-2 (registration LY-KAG) operated by Klaipedos Avialinijos (Air Klaipeda) was involved in an aviation accident near Samedan, Switzerland during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The accident was caused by an engine failure in the climbing phase, in which the altitude of the aircraft was not sufficient for a 180° turn. The following possibly contributed to the engine failure: - Carburettor icing, - Incorrect mixture regulation setting. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781201230Data APIEditorial standards

A single-engine aircraft experienced engine failure while climbing after departure from Samedan Airport. The pilot attempted a 180° turn for landing but struck trees and crashed inverted. All three occupants were uninjured; the aircraft was destroyed.

Accident Overview

A single-engine aircraft took off from Samedan Airport's runway 03 for a local flight, carrying two passengers and a pilot/instructor. While climbing to an altitude of 125 metres, the engine failed.

Maneuver and Impact

The pilot initiated a 180° turn with the intention of making an immediate landing on runway 21. At a speed of 140 km/h, the aircraft struck tree tops and crashed inverted, coming to rest on the right side of the runway. The wreckage was located 350 metres past the runway threshold and 20 metres to the right.

Occupants and Damage

All three occupants escaped without injury. The aircraft sustained damage beyond repair.

Probable Cause

The official investigation determined that the accident was caused by an engine failure in the climbing phase, during which the altitude of the aircraft was insufficient to complete a 180° turn. Factors that may have contributed to the engine failure include carburettor icing and incorrect mixture regulation setting.