Comparison of Martin 167 Maryland and North American Rockwell OV-10 Bronco [S]ave
| Attribute |  Martin 167 Maryland × |  North American Rockwell OV-10 Bronco × |
|---|---|---|
| General | ||
| Manufacturer | Glenn L. Martin Company | North American Aviation NAA |
| Model | Martin 167 Maryland | North American Rockwell OV-10 Bronco |
| Country | United States | United States |
| Manufactured from (year) | 1939 | 1965 |
| Manufactured to (year) | 1941 | 1986 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | M167 | V10 |
| Performance | ||
| Engine | 2x Pratt & Whitney R-1830-S1C3-G "Twin Wasp" | 2x Garrett T76-G-420/421 |
| Power, hp (hp) | 1,050 | 1,040 |
| Max cruise speed (km/h) | 489 | 463 |
| Approach speed (km/h) | - | 83 |
| Travel range (km) | 2,037 | 2,222 |
| Service ceiling (m) | 9,144 | 7,925 |
| Rate of climb (m/sec) | 12.19 | 13.46 |
| Take off distance (m) | - | 853 |
| Landing distance (m) | - | 381 |
| Weights | ||
| Max take off weight (kg) | 7,624 | 6,552 |
| Max payload (kg) | 1,100 | 1,679 |
| Fuel tank capacity (l) | 2,336 | 954 |
| Baggage volume (m³) | - | 3.1 |
| Dimensions | ||
| Seats | 3 | 2 |
| Exterior length (m) | 14.2 | 13.41 |
| Tail height (m) | 5 | 4.6 |
| Fuselage diameter (m) | 1.2 | 1.2 |
| Wing span (m) | 18.7 | 12.2 |
| Wing tips | No Winglets | No Winglets |
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