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