Comparison of Martin 4-0-4 and Martin B-26 Marauder [S]ave
| Attribute |  Martin 4-0-4 × |  Martin B-26 Marauder × |
|---|---|---|
| General | ||
| Manufacturer | Glenn L. Martin Company | Glenn L. Martin Company |
| Model | Martin 4-0-4 | Martin B-26 Marauder |
| Country | United States | United States |
| Manufactured from (year) | 1951 | 1941 |
| Manufactured to (year) | 1953 | 1945 |
| Type | Passenger Turbo Props | Military Propellor Planes |
| Icao | M404 | B-26 |
| Performance | ||
| Engine | 2x Pratt & Whitney R-2800-CB16 | 2x Pratt & Whitney R-2800-43 Double Wasp |
| Power, hp (hp) | 2,400 | 2,200 |
| Max cruise speed (km/h) | 502 | 461 |
| Approach speed (km/h) | 130 | 176 |
| Travel range (km) | 4,260 | 4,593 |
| Service ceiling (m) | 8,839 | 6,401 |
| Rate of climb (m/sec) | 9.68 | 6.1 |
| Take off distance (m) | 600 | 704 |
| Landing distance (m) | 530 | 430 |
| Weights | ||
| Max take off weight (kg) | 20,366 | 16,783 |
| Max landing weight (kg) | 18,231 | 15,513 |
| Max payload (kg) | 4,050 | 1,800 |
| Fuel tank capacity (l) | 7,571 | 4,588 |
| Dimensions | ||
| Seats | 4 | 7 |
| Exterior length (m) | 22.7 | 17.75 |
| Tail height (m) | 8.6 | 6.2 |
| Fuselage diameter (m) | 2.9 | 2 |
| Wing span (m) | 28.42 | 21.64 |
| Wing tips | No Winglets | No Winglets |
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