Antonov AN-12
| Entry into service | 1966 |
| Dimensions | Length : 33.10 m |
| Wing span : 38 m | |
| Height : 10.53 m | |
| Weights | Maximum take off weight : 61,000 kg |
| Maximum landing weight : | |
| Operating empty weight : | |
| Maximum payload : 20.000 kg | |
| Powerplant | 4 x 4,000shp (2,983 kw) Ivtchenko AI-20K turboprops. |
| Fuel capacity | |
| Performance | Maximum cruise speed : 324 kt - 373 mph - 600 km/h |
| Maximum cruising altitude : 33,500 ft - 10,200 m | |
| Design range : 3,400 km with 22,050 lb (10,000 kg) cargo. | |
| Accommodations | 1-class : - |
| 2-class : - | |
| 3-class : - |