Attribute | Value |
---|---|
General | |
Manufacturer | Glenn L. Martin Company |
Model | Martin 4-0-4 |
Country | United States |
Manufactured from | 1951 year |
Manufactured to | 1953 year |
Type | Passenger Turbo Props |
Icao | M404 |
Performance | |
Engine | 2x Pratt & Whitney R-2800-CB16 |
Power, hp | 2,400 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 502 km/h |
Approach speed | 130 km/h |
Travel range | 4,260 km |
Fuel economy | Add |
Service ceiling | 8,839 m |
Rate of climb | 9.68 m/sec |
Take off distance | 600 m |
Landing distance | 530 m |
Weights | |
Max take off weight | 20,366 kg |
Max landing weight | 18,231 kg |
Max payload | 4,050 kg |
Fuel tank capacity | 7,571 l |
Baggage volume | Add |
Dimensions | |
Seats | 4 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | Add |
Cabin width | Add |
Cabin length | Add |
Exterior length | 22.7 m |
Tail height | 8.6 m |
Fuselage diameter | 2.9 m |
Wing span | 28.42 m |
Wing tips | No Winglets |