| Manufacturer |
Savoia-Marchetti |
Bréguet Aviation |
| Description |
The Savoia-Marchetti S.84 was an Italian twin-engined airliner developed in Italy, from the three-engined Savoia-Marchetti S.73; only the prototype was completed and the designation was re-used for the Savoia-Marchetti SM.84. |
The Bréguet 500 Colmar was a 1940s French airliner designed by Bréguet Aviation. |
| First Flight |
1936-01-01 |
1945-02-27 |
| Service End |
|
1947-10-01 |
| Designer |
Savoia-Marchetti |
Bréguet Aviation |
| Type |
Twin-engined airliner |
|
| Length (m) |
19.8 |
19.95 |
| Height (m) |
|
4.8 |
| Cockpit Crew |
4 |
|
| Max Seating |
18 |
|
| Max Speed (km/h) |
354.0557 |
|
| Cruise Speed (km/h) |
315.4314 |
400 |
| Max Ceiling (m) |
7798.003 |
|
| Capacity Description |
18 passengers, 594 lb of baggage and 1144 lb of cargo and mail |
23 |
| National Origin |
Italy |
France |
| Number Built |
1 |
1 |
| Powerplant Description |
2 × Gnome-Rhône 14Krsd 14-cylinder air-cooled radial piston engines, 671 kW (900 hp) each |
2 × Gnome-Rhône 14R-04 radial piston engine, 1193 kW (1600 hp) each |
| Primary Users |
|
French Air Force |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Savoia-Marchetti_S.84 |
en.wikipedia.org/wiki/Br%C3%A9guet_500_Colmar |
| Flat Wing Span (m) |
24 |
24.1 |
| Flat Wing Area (m²) |
|
66.7 |
| Number of Engines |
2 |
2 |