Airbus A340-300
First flight year — 1991
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Airbus A340-300 Specifications
| A340-300 | |
| Dimensions | |
| Length (m) | 63.7 |
| Wingspan (m) | 60.3 |
| Height (m) | 16.8 |
| Wing area (m2) | 361.6 |
| Weight | |
| Maximum take-off weight (kg) | 271 000 - 275 000 |
| Maximum landing weight (kg) | 192 000 |
| Operating empty weight (kg) | 130 900 |
| Maximum zero fuel weight (kg) | 181 000 |
| Maximum payload (kg) | 50 900 |
| Standard fuel capacity (litres) | 141 500 |
| Performance | |
| Range with max payload (km) | 13 100 - 13 500 |
| Cruise speed (km/h) | 890 |
| Maximum operating altitude (m) | 12 500 |
| Take-off field length (m) | 3 000 |
| Landing field length (m) | 1 926 |
| Engines | CFMI CFM56-5C4, 4 x 34000 lb |
| Cabin Data | |
| Passengers (1-class) | 440 |
| Passengers (2-class) | 335 |
| Passengers (3-class) | 295 |
| Cabin width (m) | 5.28 |
Typical Cabin Configuration of Airbus A340-300
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