The 1983 PGO Aviation AJS 2000 is a two-seater tandem multiaxis ultralight. It was fitted with dual controls, hydraulic disc brake, and Fournalès shock absorbers.

 

Engine: Rotax 532, 65 hp

Wingspan: 10.60 m

Wing area: 16 sq.m

Fuel capacity: 40 lt

VNE: 145 km / h

Cruise: 110 km / h

VSo: 55km / h

Fuel consumption: 13 lt/hr