| Attribute | Rockwell OV-10 Bronco × | Martin 167 Maryland × |
|---|---|---|
| General | ||
| Manufacturer | Rockwell International | Glenn L. Martin Company |
| Model | Rockwell OV-10 Bronco | Martin 167 Maryland |
| Country | United States | United States |
| Manufactured from (year) | 1965 | 1939 |
| Manufactured to (year) | 1986 | 1941 |
| Type | Military Aircraft | Military Propellor Planes |
| Icao | V10 | M167 |
| Performance | ||
| Engine | 2x 2 × Garrett T76-G-420/421 | 2x Pratt & Whitney R-1830-S1C3-G "Twin Wasp" |
| Power, hp (hp) | 1,040 | 1,050 |
| Max cruise speed (km/h) | 463 | 489 |
| Approach speed (km/h) | 83 | - |
| Travel range (km) | 2,222 | 2,037 |
| Fuel economy (km/l) | 0.969 | - |
| Service ceiling (m) | 7,925 | 9,144 |
| Rate of climb (m/sec) | 13.46 | 12.19 |
| Take off distance (m) | 853 | - |
| Landing distance (m) | 381 | - |
| Weights | ||
| Max take off weight (kg) | 6,552 | 7,624 |
| Max payload (kg) | 1,679 | 1,100 |
| Fuel tank capacity (l) | 954 | 2,336 |
| Baggage volume (m³) | 3.1 | - |
| Dimensions | ||
| Seats | 2 | 3 |
| Exterior length (m) | 13.41 | 14.2 |
| Tail height (m) | 4.6 | 5 |
| Fuselage diameter (m) | 1.2 | 1.2 |
| Wing span (m) | 12.19 | 18.7 |
| Wing tips | No Winglets | No Winglets |