Avia

Avia 57

The Avia 57, introduced by the Czechoslovak‑Polish manufacturer Avia in 1957, marked a decisive step in post‑war European aviation. Developed as a twin‑engine, low‑wing transport, the aircraft was intended to replace aging wartime types such as the Junkers Ju 52 in both civil and military roles. Its structure combined a semi‑monocoque aluminum fuselage with a retractable tricycle landing gear, delivering a maximum speed of 420 km/h and a range of 2,200 km with a payload of up to 1,800 kg. Powered by two Ivchenko AI‑24 turboprop engines, the Avia 57 offered improved fuel efficiency and reliability over its piston‑engine predecessors. The cockpit featured fully hydraulic flight controls and an early version of an air‑conditioned cabin, enhancing crew comfort on longer routes.

Only 84 units were built, but the type saw extensive service with Czechoslovak Airlines, the Warsaw Pact air forces, and numerous Eastern Bloc carriers. Its versatility as a cargo hauler, passenger liner, and medical evacuation platform demonstrated Avia’s ability to produce a multifunctional aircraft during the Cold War. The Avia 57’s legacy lies in its contribution to standardising turboprop transport in the region and influencing later designs such as the Avia 62.

Dimensions

Wing Area
81.5 square metre
Length
15.9 metre
Mass
8600 kilogram

Performance

Maximum Speed
300 kilometre per hour
Service Ceiling
5000 metre
Range
1200 kilometre

Production & History

Units Produced
1
First Flight
1935

Design & Classification

Primary Use
Country of Origin
Manufacturer
Avia
Wikidata ID
Q2788348