Breguet 500 Colmar

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Role Airliner
National origin France
Manufacturer Breguet Aviation
First flight 27 February 1945
Retired October 1947
Primary user French Air Force
Number built 1

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[edit]

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and after testing the sole Colmar was delivered to the French Air Force for use as a VIP transport.[2] The Colmar was withdrawn from service in October 1947 and scrapped.




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)[edit]

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


  • Cruising speed: 400 km/h (249 mph; 216 kn) approx
  • Range: 2,000 km (1,243 mi; 1,080 nmi)


  1. ^ a b c Orbis 1985, p. 876
  2. ^ a b c d e f g h i Chillon et al 1980, p. 156
  3. ^ "French Substratosphere Transport Was Hidden From Nazis", November 1948, Popular Science US magazine editors had wrongly named aircraft photo Bellatrix - rare photo in article