The 260AG is a low-wing monoplane with a single seat and fixed tailwheel undercarriage. Development commenced in 1971 as the AG.235/260, but various problems forced the project to stagnate and it was not revived until the 1990s.
Specifications (AG.235/260)
Data from Jane's all the World's Aircraft 1988–89[2]
General characteristics
Crew: 1
Capacity: 500 L (109.98 imp gal) of liquid or 500 kg (1,102 lb) of powder.