Tupolev TU-134A
| Entry into service | 1970 |
| Dimensions | Length : 37.10 m |
| Wing span : 29.00 m | |
| Height : 9.02 m | |
| Weights | Maximum take off weight : 47,000 kg |
| Maximum landing weight : 43,000 kg | |
| Operating empty weight : 29,000 kg | |
| Maximum payload : 8,200 kg | |
| Powerplant | 2 x 14,990 lb (6,800 kgp) Soloviev D-30-2. |
| Fuel capacity | 16,500 l |
| Performance | Maximum cruise speed : 477 kt - 885 km/h |
| Maximum cruising altitude : 39,000 ft - 11,900 m | |
| T-O distance : 1,000 m | |
| Landing field length : 865 m | |
| Design range : 1,740 km/8,200 kg payload. | |
| Accommodations | 1-class : 80 |
| 2-class : 72 | |
| 3-class : - |