Breguet 500 Colmar
The Breguet 500 Colmar was a 1940s French airliner designed by Breguet Aviation.[1] Two prototypes were built during the Second World War but only one survived to fly in 1945. The prototype went on to operate as a VIP transport with the French Air Force but no others were built.[1][2]
Design and development
Originally started under the designation 483T the Colmar was designed as a twin-engined airliner or VIP and staff transport based on the earlier four-engined Breguet 482 bomber.[2] It was an all-metal mid-wing cantilever monoplane with twin fins and rudders and a retractable tailwheel landing gear. The fuselage cabin was divided into two due to the main spar, up to six passengers in the forward cabin and 17 in the rear.[2] Work started at Montaudran on two prototypes during the German occupation which were given the designation Breguet 500 Colmar.[2] In April 1944 one of the almost completed prototypes was destroyed by the Royal Air Force during a bombing raid on the factory.[2]
Following the liberation of France the surviving prototype powered by two Gnome-Rhône 14R-04 / Gnome-Rhône 14R-05 radial engines first flew on 27 February 1945.[2][3] Plans to put the type into production as the Breguet 510 Colmar were abandoned and after testing the sole Colmar was delivered to the French Air Force for use as a VIP transport.[2] The Colmar was withdrawn from service in October 1947 and scrapped.
Operators
Variants
- 500 Colmar
- Twin-engined airliner prototype, one built and one destroyed before completion.[2]
- 510 Colmar
- Proposed production variant with longer fuselage, not built.[2]
Specifications (500 Colmar)
Data from [1]Illustrated Encyclopedia of Aircraft
General characteristics
- Capacity: 23
- Length: 19.95 m (65 ft 5 in)
- Wingspan: 24.10 m (79 ft 1 in)
- Height: 4.80 m (15 ft 9 in)
- Wing area: 66.70 m2 (718.0 sq ft)
- Max takeoff weight: 14,380 kg (31,702 lb)
- Powerplant: 2 × Gnome-Rhône 14R-04 / Gnome-Rhône 14R-05 radial piston engine, 1,200 kW (1,600 hp) each
Performance
- Cruising speed: 400 km/h (249 mph; 216 kn) approx
- Range: 2,000 km (1,243 mi; 1,080 nmi)
References
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- Notes
- Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
- Chillon, J; J-P Dubois and J.Wegg (1980). French Postwar Transport Aircraft. Tonbridge, England: Air-Britain (Historian) Limited. ISBN 0-85130-078-2.
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