Comparison of Curtiss P-36 Hawk and North American BT-14 [S]ave
| Attribute |  Curtiss P-36 Hawk × |  North American BT-14 × |
|---|---|---|
| General | ||
| Manufacturer | Curtiss | North American Aviation NAA |
| Model | Curtiss P-36 Hawk | North American BT-14 |
| Country | United States | United States |
| Manufactured from (year) | 1938 | 1936 |
| Manufactured to (year) | 1944 | 1938 |
| Type | Military Propellor Planes | Military Trainers |
| Icao | P36 | BT14 |
| Performance | ||
| Engine | 1x Pratt & Whitney R-1830-17 Twin Wasp | 1x Pratt & Whitney R-975-E3 |
| Power, hp (hp) | 1,050 | 420 |
| Max cruise speed (km/h) | 504 | 278 |
| Approach speed (km/h) | 120 | 104 |
| Travel range (km) | 1,389 | 1,411 |
| Service ceiling (m) | 10,058 | 6,599 |
| Rate of climb (m/sec) | 17.27 | 5.59 |
| Weights | ||
| Max take off weight (kg) | 2,726 | 2,065 |
| Max landing weight (kg) | 2,563 | 2,030 |
| Max payload (kg) | 550 | 280 |
| Fuel tank capacity (l) | 511 | 394 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 8.7 | 8.7 |
| Tail height (m) | 2.84 | 4.1 |
| Fuselage diameter (m) | 1.2 | 1.1 |
| Wing span (m) | 11.38 | 13.1 |
| Wing tips | No Winglets | No Winglets |
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