Boeing 767-300ER
| Entry into service | 1988 | |
| Dimensions | Length : 54.94 m | |
| Wing span : 47.57 m | ||
| Height : 15.85 m | ||
| Weights | Maximum take off weight : | 184,170 kg |
| Option : 186,880 kg | ||
| Maximum landing weight : | 136,200 kg | |
| Option : 145,150 kg | ||
| Operating empty weight : 90,540 kg | ||
| Maximum payload : 43,270 kg | ||
| Powerplant |
2 x 57,000-63,000 lb General Electrics CF6-80C2B/ 2 x 57,000 - 63,000 lb Pratt & Whitney PW 4000/ 2 x 60,670 lb Rolls-Royce RB211-524G/H |
|
| Fuel capacity | 91,380 l | |
| Performance | Maximum cruise speed : 492 kt - 911 km/h | |
| Maximum cruising altitude : 43,100 ft - 13,137 m | ||
| T-O distance : 2,713 m | ||
| Landing field length : 1,676 m | ||
| Design range :11,400 km/218 pax. | ||
| Accommodations | 1-class : 328 | |
| 2-class : 269 | ||
| 3-class : 218 | ||