Comparison of Lockheed L-188 Electra and Lockheed Martin C-130J Super Hercules [S]ave
| Attribute |  Lockheed Martin C-130J Super Hercules × |  Lockheed L-188 Electra × |
|---|---|---|
| General | ||
| Manufacturer | Lockheed Martin Aeronautics | Lockheed Martin Aeronautics |
| Model | Lockheed Martin C-130J Super Hercules | Lockheed L-188 Electra |
| Country | United States | United States |
| Manufactured from (year) | 1996 | 1957 |
| Manufactured to (year) | - | 1961 |
| Type | Military Transport Planes | Passenger Turbo Props |
| Icao | C130 | L188 |
| Performance | ||
| Engine | 4x Rolls-Royce AE 2100D3 | 4x Allison 501-D13 |
| Power, hp (hp) | 4,700 | 3,750 |
| Avionics | Lockheed C-130X AMP Avionics | Bendix Weather Radar, MLS, GPS |
| Max cruise speed (km/h) | 676 | 648 |
| Approach speed (km/h) | 222 | 222 |
| Travel range (km) | 4,426 | 3,519 |
| Fuel economy (km/l) | 0.108 | - |
| Service ceiling (m) | 10,058 | 8,656 |
| Rate of climb (m/sec) | 9.3 | 10.01 |
| Take off distance (m) | 1,573 | 1,439 |
| Landing distance (m) | 792 | 1,311 |
| Weights | ||
| Max take off weight (kg) | 79,365 | 51,256 |
| Max landing weight (kg) | 58,957 | 44,499 |
| Max payload (kg) | 21,500 | 15,300 |
| Fuel tank capacity (l) | 36,643 | 20,895 |
| Baggage volume (m³) | 170 | 15 |
| Dimensions | ||
| Seats | 92 | 98 |
| Cabin height (m) | 2.74 | 1.93 |
| Cabin width (m) | 3.12 | 2.74 |
| Cabin length (m) | 16.9 | 20.02 |
| Exterior length (m) | 34.37 | 31.85 |
| Tail height (m) | 11.84 | 10.01 |
| Fuselage diameter (m) | 4.32 | 3.2 |
| Wing span (m) | 40.4 | 30.18 |
| Wing tips | No Winglets | No Winglets |
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