Comparison of Curtiss P-36 Hawk and North American T-28 Trojan [S]ave
| Attribute |  Curtiss P-36 Hawk × |  North American T-28 Trojan × |
|---|---|---|
| General | ||
| Manufacturer | Curtiss | North American Aviation NAA |
| Model | Curtiss P-36 Hawk | North American T-28 Trojan |
| Country | United States | United States |
| Manufactured from (year) | 1938 | 1950 |
| Manufactured to (year) | 1944 | 1957 |
| Type | Military Propellor Planes | Military Trainers |
| Icao | P36 | T28 |
| Performance | ||
| Engine | 1x Pratt & Whitney R-1830-17 Twin Wasp | 1x Wright R-1820-86 Cyclone |
| Power, hp (hp) | 1,050 | 1,425 |
| Max cruise speed (km/h) | 504 | 556 |
| Approach speed (km/h) | 120 | 115 |
| Travel range (km) | 1,389 | 1,704 |
| Service ceiling (m) | 10,058 | 10,820 |
| Rate of climb (m/sec) | 17.27 | 17.98 |
| Take off distance (m) | - | 400 |
| Landing distance (m) | - | 400 |
| Weights | ||
| Max take off weight (kg) | 2,726 | 3,856 |
| Max landing weight (kg) | 2,563 | 3,542 |
| Max payload (kg) | 550 | 600 |
| Fuel tank capacity (l) | 511 | 674 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 8.7 | 10.4 |
| Tail height (m) | 2.84 | 3.86 |
| Fuselage diameter (m) | 1.2 | 1.6 |
| 1↑Wing span (m) | 11.38 | 12.3 |
| Wing tips | No Winglets | No Winglets |
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