Antonov AN-26
| Entry into service | 1970 |
| Dimensions | Length : 23.80 m |
| Wing span : 29.20 m | |
| Height : 8.57 m | |
| Weights | Maximum take off weight : 52,980 lb (24,000 kg) |
| Maximum landing weight : | |
| Operating empty weight : 33,157 lb (15,020 kg) | |
| Maximum payload : 11,037 lb (5,000 kg) | |
| Powerplant | 2 x 2,850 shp (2,103 kw) Ivtchenko AI-20K turboprops. |
| Fuel capacity | 4,740 kg |
| Performance | Maximum cruise speed : 243kt - 450 km/h |
| Maximum cruising altitude : 26,575 ft - 8,100 m | |
| Design range : 900 km with 9,934 lb (4,500 kg) cargo. | |
| Accommodations | 1-class : - |
| 2-class : - | |
| 3-class : - |