| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Glenn L. Martin Company |
| Model | Martin B-10 |
| Country | United States |
| Manufactured from | 1933 year |
| Manufactured to | 1940 year |
| Type | Military Propellor Planes |
| Icao | B10 |
| Performance | |
| Engine | 2x Wright R-1820-33 Cyclone |
| Power, hp | 775 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 343 km/h |
| Approach speed | Add |
| Travel range | 2,000 km |
| Fuel economy | Add |
| Service ceiling | 7,376 m |
| Rate of climb | 7.01 m/sec |
| Take off distance | Add |
| Landing distance | Add |
| Weights | |
| Max take off weight | 7,440 kg |
| Max landing weight | Add |
| Max payload | 1,025 kg |
| Fuel tank capacity | 2,801 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 3 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 13.64 m |
| Tail height | 4.7 m |
| Fuselage diameter | 1.3 m |
| Wing span | 21.5 m |
| Wing tips | No Winglets |