| Be-550 Bibi | |
|---|---|
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| Beneš-Mráz Be.550 Bibi, 1939 | |
| Role | Sporting aircraft | 
| Manufacturer | Beneš-Mráz | 
| Designer | Pavel Beneš and Jaroslav Mráz | 
| First flight | 1936 | 
| Introduction | 1936 | 
| Number built | ca. 18 | 
The Beneš-Mráz Bibi was a 1930s Czechoslovak two-seat touring aircraft.
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Design and development
The Bibi was designed and manufactured by Beneš-Mráz, developed from the Beta-Minor design. The Bibi was a lighter, smaller aircraft in which the seats were side-by-side instead of in tandem, and the cockpits were fully enclosed, retaining the Beta-Minor's cantilever low-wing cantilever monoplane layout, with fixed tailwheel undercarriage. Development of the Bibi began with the Be-501 two-seat cabin tourer, and culminated with the Be-555 Super Bibi.[1]
Operational history
One example of the Be-550 Bibi (OK-BET) was imported into the United Kingdom, stored during World War II, then registered as G-AGSR until a fatal crash in 1951.[1]
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Variants
- Be-501 Bibi
 - Single seat, initial development aircraft for the Bibi cabin tourer.
 - Be-502 Bibi
 - Single seat development prototype for the Bibi series.
 - Be-550 Bibi
 - Initial production version introduced in 1936, with at least six built, including single exports to Egypt and the UK.
 - Be-555 Super Bibi
 - The final iteration of the Bibi with many improvements. Production continued after the start of WWII, with at least ten built.
 
Specifications (Be-550)
Data from L'Année Aéronautique 1938–1939[2]
General characteristics
- Crew: Two
 - Length: 7.31 m (24 ft 0 in)
 - Wingspan: 11.51 m (37 ft 9 in)
 - Height: 1.90 m (6 ft 3 in)
 - Wing area: 14.0 m2 (151 sq ft)
 - Empty weight: 330 kg (728 lb)
 - Gross weight: 560 kg (1,235 lb)
 - Powerplant: 1 × Walter Mikron II air-cooled 4-cylinder inverted inline engine, 45 kW (60 hp)
 
Performance
- Maximum speed: 200 km/h (120 mph, 110 kn) at 100 m (330 ft)
 - Cruise speed: 175 km/h (109 mph, 94 kn)
 - Range: 780 km (480 mi, 420 nmi)
 - Service ceiling: 5,200 m (17,100 ft)
 - Time to altitude: 6 min 30 s to 1,000 m (3,300 ft)
 
Notes
- 1 2 Jackson 1974, p. 358
 - ↑ Hirschauer & Dollfus 1939, p. 26
 
References
- Hirschauer, L; Dollfus, Ch (1939). L'Année Aéronautique 1938–1939 (in French). Paris: Dunod. Retrieved 11 December 2019 – via BnF Gallica.
 - Jackson, A.J. (1974). British Civil Aircraft since 1919. Putnam ISBN 0-370-10014-X
 - Němeček, V. (1968). Československá letadla. Praha: Naše Vojsko.
 - Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 152.
 - World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 25.
 
