With gun armament the aircraft was designated GL-22 C1 (C = Chasse), but without armament it was designated GL-22 ET1 (ET = Entrainement de Transition) and was intended for the advanced training role. The first order for the GL-22 was placed with Gourdou-Leseurre on December 13, 1920, twenty examples of the single-seat fighter subsequently being built for export to Estonia, Latvia and Czechoslovakia, and thirty of the training version being supplied to France's Aviation Marine. In addition, a manufacturing licence was acquired by the newly-established Zmaj concern in Yugoslavia.
Span: 30 ft 10 in (9.40 m)
Length: 21 ft 1.125 in (6.43 m)
Wing area: 202.37 sq.ft (18.80 sq.m)
Empty weight: 1,301 lb (590 kg)
Loaded weight: 1,940 lb (880 kg)
Max speed: 153 mph (247 kmh) at sea level
Max speed: 137 mph (220 kmh) at 16,405 ft (5,000 m)
Climb: to 16,405 ft (5,000 m) 17 min 30 sec
Endurance: 2 hr 30 min
