Hawker Siddeley Trident 2E
| Entry into service | 1968 |
| Dimensions | Length : 34.97 m |
| Wing span : 29.87 m | |
| Height : 8.23 m | |
| Weights | Maximum take off weight : 65,090 kg |
| Maximum landing weight : 51,261 kg | |
| Operating empty weight : 33,203 kg | |
| Maximum payload : 12,156 kg | |
| Powerplant | 3 x 11,960 lb (5,425 kg) Rolls-Royce RB.163-25 Mk 512-5W. |
| Fuel capacity | 26,094 l |
| Performance | Maximum cruise speed : 525 kt - 972 km/h |
| Maximum cruising altitude : 33,000 ft - 10,000 m | |
| T-O distance : 1,950 m | |
| Landing field length : - m | |
| Design range : 4,025 km / 7,266 kg payload | |
| Accommodations | 1-class : 115 |
| 2-class : - | |
| 3-class : - |