The Starck AS-80 Holiday is a conventional two-seat, single-engine high-wing monoplane designed and built in France around 1950.

The fin is straight edged, the rudder generous, rounded and fitted with a trim tab.

The conventional fixed undercarriage has mainwheels with low pressure tyes on faired V-struts and half axles hinged on an underside cabane.

The prototype Holiday first flew powered by a 56 kW (75 hp) Régnier 4D.2 four cylinder inverted inline air-cooled piston engine, but there was a wide range of suitable engines, both inline and flat fours, in the power range 44-63 kW (59-85 hp).

[1] Though the inline Régnier engine was fully cowled,[1] some of the flat fours have had exposed cylinder heads.