The Zlin 22 Junak, a two-seat cabin monoplane, debuted in the 1940s as an offshoot of the Zlin 381.
It was distinguished by its side-by-side seating configuration for two passengers.
The design featured a low-wing cantilever monoplane structure with a traditional tailwheel landing gear.
A 75 hp (56 kW) Praga D engine powered the aircraft, located at the front, although the initial prototype utilised a 57 hp (43 kW) Persy III engine.
Additionally, a three-seat variant named the Zlin 22M was developed, and two prototypes of a three- or four-seat tourer version, the Zlin 122, were also built.
Variants Zlin Z 22 Prototype with a 57 hp (43 kW) Persy III engine. Zlin Z 22D Production two-seat variant with a 75 hp (56 kW) Praga D engine. Zlin Z 22M Three-seat variant with a 105 hp (78 kW)) Walter Minor 4-III engine. Zlin Z 122 Three/four-seat development with a 105hp (78kW) Zlin Toma 4 engine, two prototypes only Specifications
22D
Crew
1
Capacity
1 passenger
Length
7.25 m (23 ft 9 in)
Wingspan
10.60 m (34 ft 9 in)
Height
1.96 m (6 ft 5 in)
Wing area
14.65 m2 (157.7 sq ft)
Empty weight
370 kg (816 lb)
Gross weight
650 kg (1,433 lb)
Fuel capacity
72 L (19 US gal; 16 imp gal) normal,
Provision for additional 65 L (17 US gal; 14 imp gal) tank
