The Airbus A340 is a long-range, four-engine, wide-body commercial passenger jet airliner that was developed and produced by the European aerospace company Airbus. The A340 was assembled in Toulouse, France. It seats up to 375 passengers in the standard variants and 440 in the stretched -600 series. Depending on the model, it has a range of 6,700 to 9,000 nautical miles (12,400 to 16,700 km; 7,700 to 10,400 mi). Its distinguishing features are four high-bypass turbofan engines and three-bogie main landing gear.
Combining performance, comfort and range for highly efficient ultra-long-haul operations, Airbus’ A340-500 is popular with passengers and airlines alike. The four-engine, twin-aisle widebody jetliner’s range of up to 9,000 nautical miles allows the A340-500 to operate some of the world’s longest non-stop routes, while its optimised 222-inch fuselage cross-section gives airlines the cabin versatility to match market requirements.
Dimensions
Overall length |
67.93 m |
Cabin length |
53.56 m |
Fuselage width |
5.64 m |
Max cabin width |
5.28 m |
Wing span (geometric) |
63.45 m |
Height |
17.53 m |
Track |
10.69 m |
Wheelbase |
27.59 m |
Capacity
Pax |
Typical seating |
293 |
|
Max |
440 |
Freight |
LD3 capacity underfloor |
31 |
|
Max pallet number underfloor |
10 |
|
Bulk hold volume |
19.7 m³ |
|
Total volume |
153.9 m³ |
Performance
Range |
16 670 km |
Mmo |
M0.86 |
Max ramp weight |
381.20 tonnes |
Max take-off weight |
380.00 tonnes |
Max landing weight |
246.00 tonnes |
Max zero fuel weight |
232.00 tonnes |
Max fuel capacity |
222 850 litres |
Dimensions
Overall length |
222 ft 10 in |
Cabin length |
175 ft 9 in |
Fuselage width |
18 ft 6 in |
Max cabin width |
17 ft 4 in |
Wing span (geometric) |
208 ft 2 in |
Height |
56 ft 8 in |
Track |
35 ft 1 in |
Wheelbase |
90 ft 6 in |
Capacity
Pax |
Typical seating |
293 |
|
Max |
440 |
Freight |
LD3 capacity underfloor |
31 |
|
Max pallet number underfloor |
10 |
|
Bulk hold volume |
695 ft³ |
|
Total volume |
5 435 ft³ |
Performance
Range |
9 000 nm |
Mmo |
M0.86 |
Max ramp weight |
840.40 lb x 1000 |
Max take-off weight |
837.80 lb x 1000 |
Max landing weight |
542.30 lb x 1000 |
Max zero fuel weight |
511.30 lb x 1000 |
Max fuel capacity |
58 875 USG |
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