The company produced a 2/3-seat light aircraft, the GV 103L, which first flew on 1 May 1969. Subsequently built a second example with the intention of finding a sponsor for production of the type.
The GV 10-20 was an aerobatic two-seat version with 115 hp Lycoming engine.
The GV 10-31 was a four-seat version.
GV 10-31
Engine: Lycoming O-320, 150 hp
Wingspan: 28 ft 8.5 in / 8.75 m
Length: 21 ft 7.75 in / 6.60 m
Empty weight: 1212 lb / 550 kg
MTOW: 2182 lb / 990 kg
Max cruise 75%: 122 kt / 140 mph / 225 kph
ROC SL: 787 fpm / 240 m/min
Service ceiling: 14,760 ft / 4500 m
Range: 594 nm / 683 mi / 1100 km
Seats: 4
Max rear seat load: 340 lb / 154 kg
Baggage: 22 lb / 10 kg
All Aero 