Comparison of North American B-25 Mitchell and North American AJ Savage [S]ave
| Attribute |  North American B-25 Mitchell × |  North American AJ Savage × |
|---|---|---|
| General | ||
| Manufacturer | North American Aviation NAA | North American Aviation NAA |
| Model | North American B-25 Mitchell | North American AJ Savage |
| Country | United States | United States |
| Manufactured from (year) | 1940 | 1949 |
| Manufactured to (year) | 1945 | 1954 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | B25 | AJ |
| Performance | ||
| Engine | 2x Wright R-2600-92 Twin Cyclone | 2x Pratt & Whitney R-2800-44W Double Wasp |
| Power, hp (hp) | 1,700 | 2,400 |
| Max cruise speed (km/h) | 437 | 757 |
| Approach speed (km/h) | 148 | - |
| Travel range (km) | 2,167 | 2,785 |
| Service ceiling (m) | 7,376 | 13,106 |
| Rate of climb (m/sec) | 5.08 | 14.73 |
| Weights | ||
| Max take off weight (kg) | 15,876 | 23,112 |
| Max payload (kg) | 3,060 | 6,000 |
| Fuel tank capacity (l) | 3,687 | 6,208 |
| Dimensions | ||
| Seats | 5 | 3 |
| Exterior length (m) | 16.13 | 19.22 |
| 1↑Tail height (m) | 4.98 | 6.2 |
| Fuselage diameter (m) | 1.4 | 2 |
| Wing span (m) | 20.6 | 23 |
| Wing tips | No Winglets | No Winglets |
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