Boeing 747-100
| Entry into service | 1969 | |
| Dimensions | Length : 70.66 m | |
| Wing span : 59.64 m | ||
| Height : 19.94 m | ||
| Weights | Maximum take off weight : | 322,050 kg |
| Maximum landing weight : | 255,825 kg | |
| Operating empty weight : 158,220 kg | ||
| Maximum payload : 80,596 kg | ||
| Powerplant | 4 x 56,071 lb Pratt & Whitney JT9D-3A | |
| Fuel capacity | 178,702 l | |
| Performance | Maximum cruise speed : 517 kt - 978 km/h | |
| Maximum cruising altitude : 45,000 ft - 13,715 m | ||
| T-O distance : 3,170 m | ||
| Landing field length : 2,057 m | ||
| Design range :6,460 km/74,000 kg | ||
| Accommodations | 1-class : 490 | |
| 2-class : 423 | ||
| 3-class : 366 | ||