Casualties unknown

Cessna F150L Crash in Straßwalchen, Austria

im Gemeindegebiet Straßwalchen, Salzburg, AT

On June 21, 2012, a Cessna F150L was involved in an aviation accident near im Gemeindegebiet Straßwalchen, Salzburg, AT. Investigators recorded the probable cause as: A temporary malfunction of the wing flap system, combined with the use of an incorrect fuse type in the flap circuit, caused the fuse to blow. This prevented the fully extended wing flaps from being retracted, reducing climb performance. This summary draws on records from the Austrian Federal Safety Investigation Authority (SUB).

Sourcesthe Austrian Federal Safety Investigation Authority (SUB)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Cessna F150L crashed in a meadow in Straßwalchen, Austria, on June 21, 2012, killing both occupants. The aircraft was conducting a private pilot checkride with simulated emergency landings.

Incident Overview and Flight Details On June 21, 2012, a Cessna F150L, a two-seat, high-wing, metal-framed aircraft with a fixed tricycle landing gear, crashed in a meadow in the municipality of Straßwalchen, Austria. The accident occurred at approximately 13:21 UTC. The aircraft was operated by a flight training organization and was on a cross-country flight from Salzburg Airport to Gmunden-Laakirchen Airport. The purpose of the flight was to conduct a private pilot checkride, which included simulated emergency landings. The aircraft landed at Gmunden-Laakirchen at 12:48 UTC and departed for Salzburg at 13:08 UTC. During the return flight, the crew conducted low-level overflights near the ground at an alternate landing site in Voglhub, Straßwalchen. After the third go-around maneuver, the aircraft gained altitude slowly, crossed a high-voltage power line with less clearance than previous passes, and then rolled left and crashed into a meadow. Both occupants, a pilot and a student pilot, were killed. The aircraft was destroyed, and there was ground damage and fuel contamination.

Probable cause

A temporary malfunction of the wing flap system, combined with the use of an incorrect fuse type in the flap circuit, caused the fuse to blow. This prevented the fully extended wing flaps from being retracted, reducing climb performance. The aircraft then entered an asymmetric stalled flight condition to the left after dropping below minimum flight speed in this configuration, and the altitude was too low to recover.