Comparison of Curtiss SB2C Helldiver and Grumman OV-1 Mohawk [S]ave
| Attribute |  Curtiss SB2C Helldiver × |  Grumman OV-1 Mohawk × |
|---|---|---|
| General | ||
| Manufacturer | Curtiss | Grumman |
| Model | Curtiss SB2C Helldiver | Grumman OV-1 Mohawk |
| Country | United States | United States |
| Manufactured from (year) | 1942 | 1959 |
| Manufactured to (year) | 1945 | 1970 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | SB2C | OV1 |
| Performance | ||
| Engine | 1x Wright R-2600-20 Twin Cyclone | 2x Lycoming T53-L-701 |
| Power, hp (hp) | 1,900 | 1,400 |
| Max cruise speed (km/h) | 474 | 491 |
| Approach speed (km/h) | 143 | 135 |
| Travel range (km) | 1,874 | 1,519 |
| Service ceiling (m) | 8,870 | 7,620 |
| Rate of climb (m/sec) | 9.14 | 17.78 |
| Take off distance (m) | 178 | 358 |
| Landing distance (m) | - | 320 |
| Weights | ||
| Max take off weight (kg) | 7,710 | 8,215 |
| Max landing weight (kg) | 7,537 | 7,051 |
| Max payload (kg) | 1,500 | 1,050 |
| Fuel tank capacity (l) | 1,344 | 1,045 |
| Dimensions | ||
| Seats | 2 | 2 |
| Exterior length (m) | 11.18 | 12.5 |
| Tail height (m) | 5.16 | 3.86 |
| Fuselage diameter (m) | 1.4 | 1.7 |
| Wing span (m) | 15.16 | 14.63 |
| Wing tips | No Winglets | No Winglets |
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