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| Model |
A340-200 |
A340-300 |
A340-500 |
A340-600 |
| Cockpit crew |
Two |
| Seating capacity |
300 (2-class, typical)
240 (3-class, typical)
375/420 (1-class, maximum) |
335 (2-class, typical)
295 (3-class, typical)
375/440
(1-class, maximum) |
359 (2-class, typical)
313 (3-class, typical)
375 (1-class, maximum) |
419 (2-class, typical)
380 (3-class, typical)
440 (1-class, 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 volume |
162.8 cubic metres (5,750 cu ft) |
162.8 cubic metres (5,750 cu ft) |
153.9 cubic metres (5,430 cu ft) |
207.6 cubic metres (7,330 cu ft) |
| Operating empty weight, typical |
129,000 kilograms (284,000 lb) |
130,200 kilograms (287,000 lb) |
170,900 kilograms (376,800 lb)
HGW: 174,800 kilograms (385,400 lb) |
177,800 kilograms (392,000 lb)
HGW: 181,900 kilograms (401,000 lb) |
| Maximum take-off weight (MTOW) |
275,000 kilograms (606,000 lb) |
276,500 kilograms (609,600 lb) |
372,000 kilograms (820,000 lb)
HGW: 380,000 kilograms (840,000 lb) |
368,000 kilograms (811,000 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) |
Takeoff distance at MTOW
(sea level, ISA) |
2,990 metres (9,810 ft) |
3,100 metres (10,200 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) |
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