Lockheed L-100-30
| Entry into service | 1970 |
| Dimensions | Length : 34.35 m |
| Wing span : 40.41 m | |
| Height : 11.66 m | |
| Weights | Maximum take off weight : 70,308 kg |
| Maximum landing weight : 61,235 kg | |
| Operating empty weight : 32,386 kg | |
| Maximum payload : 24,312 kg | |
| Powerplant |
4 x 4,050 hp Allison 501D-22. Option : 4 x 4,508 hp Allison 501D-22A. |
| Fuel capacity | 26,344 l |
| Performance | Maximum cruise speed : 327 kt - 607 km/h |
| Maximum cruising altitude : 33,000 ft - 10,000 m | |
| T-O distance : 1,829 m | |
| Landing field length : 1,472 m | |
| Design range : 3,425 km/24,312 kg payload | |
| Accommodations | 1-class : - |
| 2-class : - | |
| 3-class : - |