Comparison of Aviat Pitts S-2C and Aviat Pitts S-1 [S]ave
| Attribute |  Aviat Pitts S-1 × |  Aviat Pitts S-2C × |
|---|---|---|
| General | ||
| Manufacturer | Aviat Aircraft | Aviat Aircraft |
| Model | Aviat Pitts S-1 | Aviat Pitts S-2C |
| Country | United States | United States |
| Manufactured from (year) | 1944 | 2008 |
| Type | Aerobatic | Aerobatic |
| Icao | PTS1 | PTS2 |
| Performance | ||
| Engine | 1x 1 X Lycoming IO-360 fuel injected | 1x 1 X Lycoming AEIO-540 |
| Power, hp (hp) | 200 | 260 |
| Max cruise speed (km/h) | 209 | 313 |
| Travel range (km) | 552 | 513 |
| Fuel economy (km/l) | 31.311 | 11.898 |
| Service ceiling (m) | 6,096 | 6,401 |
| Rate of climb (m/sec) | 13.21 | 13.72 |
| 1↑Take off distance (m) | 91 | 169 |
| Landing distance (m) | 152 | 229 |
| Weights | ||
| Max take off weight (kg) | 680 | 737 |
| Max payload (kg) | 168 | 247 |
| Fuel tank capacity (l) | 72 | 110 |
| Dimensions | ||
| Seats | 1 | 2 |
| Cabin height (m) | - | 1.1 |
| Cabin width (m) | - | 0.7 |
| Cabin length (m) | - | 2.1 |
| Exterior length (m) | 5.41 | 5.72 |
| Tail height (m) | 1.94 | 2.02 |
| Fuselage diameter (m) | - | 1 |
| Wing span (m) | 6.1 | 6.1 |
| Wing tips | No Winglets | No Winglets |
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