Specifications
| Measurement | A300B4 | A300-600R | A300-600F |
|---|---|---|---|
| Typical capacity | 220 passengers (three-class) 266 passengers (two-class) 375 passengers (one-class) |
15 (21) pallets | |
| Overall length | 54.08 metres (177.4 ft) | ||
| Wingspan | 44.85 metres (147.1 ft) | ||
| Wing area | 260 square metres (2,800 sq ft) | ||
| Overall height | 16.62 metres (54.5 ft) | ||
| Max cabin width | 5.28 metres (17.3 ft) | ||
| Fuselage diameter | 5.64 metres (18.5 ft) | ||
| Operating empty weight typical | 90,060 kilograms (198,500 lb) | 90,900 kilograms (200,000 lb) | 81,900 kilograms (181,000 lb) |
| MTOW | 165,000 kilograms (360,000 lb) | 171,700 kilograms (379,000 lb) | 170,500 kilograms (376,000 lb) |
| Takeoff field length (MTOW, SL, ISA) | N/A | 2,324 metres (7,625 ft) | |
| Cruising speed | mach 0.78 (833 km/h, 518 mph, 450 knots at 35,000 ft) | ||
| Maximum speed | mach 0.86 | mach 0.82 (876 km/h, 544 mph, 473 knots at 35,000 ft) | |
| Range fully loaded | 6,670 kilometres (3,600 nmi) | 7,540 kilometres (4,070 nmi) | 4,850 kilometres (2,620 nmi) |
| Maximum fuel capacity | 62,900 litres (16,600 US gal) | 68,150 litres (18,000 US gal) | |
| Engines | CF6-50C2 or JT9D-59A | CF6-80C2 or PW4158 | |
| Cockpit crew | Three | Two | |
Read more about this topic: Airbus A300