Comparison of Beechcraft Staggerwing C-17 and North American NA-16 [S]ave
| Attribute |  Beechcraft Staggerwing C-17 × |  North American NA-16 × |
|---|---|---|
| General | ||
| Manufacturer | Hawker Beechcraft | North American Aviation NAA |
| Model | Beechcraft Staggerwing C-17 | North American NA-16 |
| Country | United States | United States |
| Manufactured from (year) | 1933 | 1935 |
| Manufactured to (year) | 1949 | 1939 |
| Type | Private Single Engine | Military Trainers |
| Icao | - | NA16 |
| Performance | ||
| Engine | 1 × Pratt & Whitney R-985-AN-1 - | 1x Wright R-975 Whirlwind |
| Power, hp (hp) | 850 | 400 |
| Max cruise speed (km/h) | 341 | 278 |
| Approach speed (km/h) | - | 98 |
| Travel range (km) | 1,078 | 1,130 |
| Fuel economy (km/l) | 1.957 | - |
| Service ceiling (m) | 7,620 | 6,553 |
| Rate of climb (m/sec) | 7.62 | 9.14 |
| Take off distance (m) | 186 | - |
| Landing distance (m) | 229 | - |
| Weights | ||
| Max take off weight (kg) | 1,928 | 2,300 |
| Max payload (kg) | 617 | 200 |
| Fuel tank capacity (l) | 549 | 379 |
| Dimensions | ||
| Seats | 3 | 2 |
| Exterior length (m) | 8.18 | 8.41 |
| Tail height (m) | - | 3.58 |
| Fuselage diameter (m) | - | 1.2 |
| Wing span (m) | 9.75 | 13 |
| Wing tips | No Winglets | No Winglets |
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