Comparison of Douglas DC-1 and Martin B-10 [S]ave
| Attribute |  Douglas DC-1 × |  Martin B-10 × |
|---|---|---|
| General | ||
| Manufacturer | Douglas Aircraft Co. | Glenn L. Martin Company |
| Model | Douglas DC-1 | Martin B-10 |
| Country | United States | United States |
| Manufactured from (year) | 1933 | 1933 |
| Manufactured to (year) | 1933 | 1940 |
| Type | Passenger Turbo Props | Military Propellor Planes |
| Icao | DC1 | B10 |
| Performance | ||
| Engine | 2x Wright SGR-1820F3 Cyclone | 2x Wright R-1820-33 Cyclone |
| Power, hp (hp) | 710 | 775 |
| Max cruise speed (km/h) | 333 | 343 |
| Travel range (km) | 1,611 | 2,000 |
| Service ceiling (m) | 7,010 | 7,376 |
| Rate of climb (m/sec) | 5.08 | 7.01 |
| Weights | ||
| Max take off weight (kg) | 7,938 | 7,440 |
| Max payload (kg) | 1,800 | 1,025 |
| Fuel tank capacity (l) | 3,028 | 2,801 |
| Dimensions | ||
| Seats | 14 | 3 |
| Exterior length (m) | 18.3 | 13.64 |
| Tail height (m) | - | 4.7 |
| Fuselage diameter (m) | 2 | 1.3 |
| Wing span (m) | 25.9 | 21.5 |
| Wing tips | No Winglets | No Winglets |
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