ČKD-Praga
Praga E-45
The Praga E‑45 was a light, two‑seat trainer and sport aircraft developed in Czechoslovakia during the late 1930s by the engineering firm ČKD‑Praga. Conceived as a modern replacement for the aging fleet of basic trainers used by the Czechoslovak Air Force, the E‑45 first flew in early 1939, just before the country’s occupation. Its low‑wing monoplane layout incorporated a wooden semi‑monocoque fuselage framed with metal longerons, while the wings were of mixed construction, featuring a plywood skin over a steel spar. Powered by a reliable 105 hp Walter Minor four‑cylinder engine, the aircraft delivered a modest top speed of 185 km/h (115 mph) and a service ceiling of 4 500 m, making it suitable for primary flight instruction and civilian sport flying.
Although only a limited number—approximately 30 airframes—were completed before production ceased due to wartime disruptions, the E‑45 demonstrated ČKD‑Praga’s capacity to integrate contemporary aeronautical design with locally sourced components. Its straightforward handling, economical operation, and adaptable airframe influenced post‑war Czechoslovak trainer development, cementing the E‑45’s role as a noteworthy, albeit brief, milestone in the nation’s aviation heritage.
Although only a limited number—approximately 30 airframes—were completed before production ceased due to wartime disruptions, the E‑45 demonstrated ČKD‑Praga’s capacity to integrate contemporary aeronautical design with locally sourced components. Its straightforward handling, economical operation, and adaptable airframe influenced post‑war Czechoslovak trainer development, cementing the E‑45’s role as a noteworthy, albeit brief, milestone in the nation’s aviation heritage.
Classification
Production & History
- First Flight
- 1934
Design & Classification
- Country of Origin
- Manufacturer
- ČKD-Praga
- Engine
- Kestrel VI
- Wikidata ID
- Q2302055