Boeing 777-200ER
| Entry into service | 1995 | |
| Dimensions | Length : 63.73 m | |
| Wing span : 60.90 m | ||
| Height : 18.51 m | ||
| Weights | Maximum take off weight : | 263,080 kg |
| Option : 297,560 kg | ||
| Maximum landing weight : | 208,650 kg | |
| Option : 213,190 kg | ||
| Operating empty weight : | 141,205 kg | |
| Options : 143,835 kg | ||
| Maximum payload : 51,255 kg | ||
| Powerplant | 2 x 93,700 lb General Electrics GE90-94B/ 2 x 84,000 - 93,250 lb Pratt & Whitney PW 4084/4090 / 2 x 85,500 - 93,250 lb Rolls-Royce Trent 884/895 |
|
| Fuel capacity | 171,170 l | |
| Performance | Maximum cruise speed : 499 kt - 924 km/h | |
| Maximum cruising altitude : 43,100 ft - 13,137 m | ||
| T-O distance : 3,018 m | ||
| Landing field length : 1,630 m | ||
| Design range : | 10,750 km/305 pax. | |
| Option : 14,300/305 pax. | ||
| Accommodations | 1-class : 440 | |
| 2-class : 400 | ||
| 3-class : 301 | ||