Comparison of Grumman OV-1 Mohawk and Grumman TBF Avenger [S]ave
| Attribute |  Grumman OV-1 Mohawk × |  Grumman TBF Avenger × |
|---|---|---|
| General | ||
| Manufacturer | Grumman | Grumman |
| Model | Grumman OV-1 Mohawk | Grumman TBF Avenger |
| Country | United States | United States |
| Manufactured from (year) | 1959 | 1941 |
| Manufactured to (year) | 1970 | 1945 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | OV1 | TBF |
| Performance | ||
| Engine | 2x Lycoming T53-L-701 | 1x Wright R-2600-8 Twin Cyclone |
| Power, hp (hp) | 1,400 | 1,700 |
| Max cruise speed (km/h) | 491 | 448 |
| Approach speed (km/h) | 135 | 111 |
| Travel range (km) | 1,519 | 1,611 |
| Service ceiling (m) | 7,620 | 9,144 |
| Rate of climb (m/sec) | 17.78 | 10.46 |
| Take off distance (m) | 358 | - |
| Landing distance (m) | 320 | - |
| Weights | ||
| Max take off weight (kg) | 8,215 | 8,115 |
| Max landing weight (kg) | 7,051 | 7,047 |
| Max payload (kg) | 1,050 | 1,000 |
| Fuel tank capacity (l) | 1,045 | 2,748 |
| Dimensions | ||
| Seats | 2 | 3 |
| Exterior length (m) | 12.5 | 12.23 |
| Tail height (m) | 3.86 | 5 |
| Fuselage diameter (m) | 1.7 | 1.5 |
| Wing span (m) | 14.63 | 16.51 |
| Wing tips | No Winglets | No Winglets |
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