Lockheed L-1011-1 Tristar
| Entry into service | 1972 |
| Dimensions | Length : 54.17 m |
| Wing span : 47.34 m | |
| Height : 16.87 m | |
| Weights | Maximum take off weight : 195,045 kg |
| Maximum landing weight : 162,385 kg | |
| Operating empty weight : 109,633 kg | |
| Maximum payload : 36,288 kg | |
| Powerplant | 3 x 42,020 lb (19,100 kgp) Rolls-Royce RB211-22B. |
| Fuel capacity | 89,450 l |
| Performance | Maximum cruise speed : 520 kt - 963 km/h |
| Maximum cruising altitude : 42,000 ft - 12,700 m | |
| T-O distance : 2,423 m | |
| Landing field length : 1,737 m | |
| Design range : 5,735 km/310 pax. | |
| Accommodations | 1-class : 400 |
| 2-class : 310 | |
| 3-class : 280 |