1 fatality

P.68 Prototype Crashes into Sea off Gaeta During Test Flight, Pilot Killed (I-RAIO)

Gaeta, ItalyFlight

On October 5, 1982, a Partenavia P.68 (registration I-RAIO) operated by Partenavia was involved in an aviation accident near Gaeta, Italy in flight. One person was killed. Investigators recorded the probable cause as: During the second experimental flight, due to turbulences generated by both turboprop engines, stabilizers were damaged in an extensive manner, causing the aircraft to become uncontrollable on its pitch axis. 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 2026-06-11Data APIEditorial standards

The second P.68 prototype, on a local test flight from Naples-Capodichino, crashed into the Gulf of Gaeta after experiencing controllability issues. The sole pilot was killed. Investigation attributed the accident to stabilizer damage from engine turbulence.

Accident

The second prototype of the P.68 twin-engine aircraft departed Naples-Capodichino for a local test flight. While cruising over the Gulf of Gaeta, the pilot encountered controllability problems. The aircraft entered a dive and struck the sea off Gaeta. The pilot, who was the sole occupant, was killed.

Investigation

Official investigation findings stated that during the second experimental flight, turbulence generated by both turboprop engines caused extensive damage to the stabilizers. This damage rendered the aircraft uncontrollable in the pitch axis, leading to the crash.

Aircraft

The aircraft involved was the second prototype of the P.68 series, a twin-engine turboprop design. It was on an experimental test flight at the time of the accident. No other details about the aircraft or its registration were provided in the source.

The accident occurred over water, and the wreckage was not recovered or at least not mentioned. The investigation focused on the aerodynamic effects of engine turbulence on the empennage.

Probable cause

During the second experimental flight, due to turbulences generated by both turboprop engines, stabilizers were damaged in an extensive manner, causing the aircraft to become uncontrollable on its pitch axis.