Specifications
| Model | A340-200 | A340-300 | A340-500 | A340-600 |
|---|---|---|---|---|
| Cockpit crew | Two | |||
| Seating capacity | 300 (2-class, typical) 240 (3-class, typical) 375/420 (maximum) |
335 (2-class, typical) 295 (3-class, typical) 375/440 (maximum) |
359 (2-class, typical) 313 (3-class, typical) 375 (maximum) |
419 (2-class, typical) 380 (3-class, typical) 440/520 (maximum) |
| Overall length | 59.39 metres (194 ft 10 in) | 63.60 metres (208 ft 8 in) | 67.90 metres (222 ft 9 in) | 75.30 metres (247 ft 1 in) |
| Wingspan | 60.30 metres (197 ft 10 in) | 63.45 metres (208 ft 2 in) | ||
| Wing area | 361.6 square metres (3,892 sq ft) | 439.4 square metres (4,730 sq ft) | ||
| Wing sweepback | 30 degrees | 31.1 degrees | ||
| Overall height | 16.70 metres (54 ft 9 in) | 16.85 metres (55 ft 3 in) | 17.10 metres (56 ft 1 in) | 17.30 metres (56 ft 9 in) |
| Maximum cabin width | 5.28 metres (17 ft 4 in) | |||
| Fuselage width | 5.64 metres (18 ft 6 in) | |||
| Cargo capacity | 152.3 cubic metres (5,380 cu ft) | |||
| Operating empty weight, typical | 129,000 kilograms (280,000 lb) | 130,200 kilograms (287,000 lb) | 170,900 kilograms (377,000 lb) HGW: 174,800 kilograms (385,000 lb) |
177,800 kilograms (392,000 lb) HGW: 181,900 kilograms (401,000 lb) |
| Maximum take-off weight (MTOW) | 275,000 kilograms (610,000 lb) | 276,500 kilograms (610,000 lb) | 372,000 kilograms (820,000 lb) HGW: 380,000 kilograms (840,000 lb) |
368,000 kilograms (810,000 lb) HGW: 380,000 kilograms (840,000 lb) |
| Cruising speed | Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft) | Mach 0.83 (881 km/h/543 mph at 11,000 m/36,000 ft) | ||
| Maximum Operating speed | Mach 0.86 (913 km/h/563 mph at 11,000 m/36,000 ft) | |||
| Maximum range, fully loaded | 8,000 nautical miles (15,000 km; 9,200 mi) | 7,400 nautical miles (13,700 km; 8,500 mi) | 8,670 nautical miles (16,060 km; 9,980 mi) HGW: 9,000 nautical miles (17,000 km; 10,000 mi) |
7,750 nautical miles (14,350 km; 8,920 mi) HGW: 7,900 nautical miles (14,600 km; 9,100 mi) |
| Take off run at MTOW | 2,990 metres (9,810 ft) | 3,000 metres (9,800 ft) | 3,050 metres (10,010 ft) | 3,100 metres (10,200 ft) |
| Maximum fuel capacity | 155,040 litres (34,100 imp gal; 40,960 US gal) | 147,850 litres (32,520 imp gal; 39,060 US gal) | 214,810 litres (47,250 imp gal; 56,750 US gal) HGW: 222,000 litres (49,000 imp gal; 59,000 US gal) |
195,880 litres (43,090 imp gal; 51,750 US gal) HGW: 204,500 litres (45,000 imp gal; 54,000 US gal) |
| Service ceiling | 12,500 metres (41,000 ft) | |||
| Engines (×4) | CFM56-5C | RR Trent 500 | ||
| Thrust (×4) | 139–151 kilonewtons (31,000–34,000 lbf) | 248–260 kilonewtons (56,000–58,000 lbf) | 260–275 kilonewtons (58,000–62,000 lbf) | |
Sources: Airbus for −200 for −300 for −500 for −600.
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