Comparison of Fairchild AC-119 and Northrop Grumman E-2C Hawkeye 2000 [S]ave
| Attribute |  Fairchild AC-119 × |  Northrop Grumman E-2C Hawkeye 2000 × |
|---|---|---|
| General | ||
| Manufacturer | Fairchild | Northrop Grumman |
| Model | Fairchild AC-119 | Northrop Grumman E-2C Hawkeye 2000 |
| Country | United States | United States |
| Manufactured from (year) | 1968 | 1988 |
| Type | Military Aircraft | Military Propellor Planes |
| Icao | AC119 | E2 |
| Performance | ||
| Engine | 2x Wright R-3350-85 "Duplex Cyclone" | 2x 2 X Rolls-Royce T56-A-427 turboprops |
| Power, hp (hp) | 3,500 | 5,100 |
| Avionics | - | Advanced Control Indicator Set |
| Max cruise speed (km/h) | 333 | 648 |
| Approach speed (km/h) | - | 191 |
| Travel range (km) | 3,100 | 2,856 |
| Fuel economy (km/l) | - | 1.864 |
| Service ceiling (m) | 7,102 | 11,278 |
| Rate of climb (m/sec) | 4.83 | 12.78 |
| Take off distance (m) | - | 793 |
| Landing distance (m) | - | 439 |
| Weights | ||
| Max take off weight (kg) | 28,125 | 26,082 |
| Max payload (kg) | 3,335 | 1,800 |
| Fuel tank capacity (l) | 8,479 | 7,003 |
| Dimensions | ||
| Seats | 8 | 5 |
| Exterior length (m) | 26.36 | 17.56 |
| Tail height (m) | 8.12 | 5.58 |
| Fuselage diameter (m) | 3.3 | 1.9 |
| Wing span (m) | 33.3 | 24.56 |
| Wing tips | No Winglets | No Winglets |
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