| Manufacturer |
Bréguet Aviation |
Grumman |
| Description |
The Bréguet 500 Colmar was a 1940s French airliner designed by Bréguet Aviation. |
The Grumman Gulfstream I (company designation G-159) is a twin-turboprop business aircraft. |
| First Flight |
1945-02-27 |
1958-08-14 |
| Production End |
|
1969-01-01 |
| Service End |
1947-10-01 |
|
| Designer |
Bréguet Aviation |
Grumman |
| Type |
|
Business aircraft |
| Length (m) |
19.95 |
19.2024 |
| Height (m) |
4.8 |
6.7056 |
| Cockpit Crew |
|
2 |
| Max Seating |
|
24 |
| Cruise Speed (km/h) |
400 |
560.0517 |
| Max Ceiling (m) |
|
10241.28 |
| Rate of Climb (m/s) |
|
9.652 |
| Capacity Description |
23 |
10–24 passengers / 4270 lb maximum payload |
| National Origin |
France |
United States of America |
| Number Built |
1 |
200 |
| Powerplant Description |
2 × Gnome-Rhône 14R-04 radial piston engine, 1193 kW (1600 hp) each |
2 × Rolls-Royce Dart Mk.529 or Mk.529-8E turboprop, 1633 kW (2190 hp) each |
| Primary Users |
French Air Force |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Br%C3%A9guet_500_Colmar |
en.wikipedia.org/wiki/Grumman_Gulfstream_I |
| Flat Wing Span (m) |
24.1 |
23.7744 |
| Flat Wing Area (m²) |
66.7 |
56.6987 |
| Flat Wing Aspect Ratio |
|
10 |
| Number of Engines |
2 |
2 |