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McDonnell Douglas MD-90
First flight year — 1993
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McDonnell Douglas MD-90 Specifications
| MD-90-30 | |
| Dimensions | |
| Length (m) | 46.5 |
| Wingspan (m) | 32.8 |
| Height (m) | 9.0 |
| Wing area (m2) | 112 |
| Weight | |
| Maximum take-off weight (kg) | 70 760 |
| Maximum landing weight (kg) | 64 410 |
| Operating empty weight (kg) | 39 990 |
| Maximum zero fuel weight (kg) | 55 970 |
| Maximum payload (kg) | 17 800 |
| Standard fuel capacity (litres) | 22 130 |
| Performance | |
| Range with max payload (km) | 4 400 |
| Maximum cruise speed (km/h) | 810 |
| Maximum operating altitude (km) | 11 300 |
| Take-off field length (m) | 2 160 |
| Landing field length (m) | 1 600 |
| Engines | IAE V2500-D5, 2 x 28000 lb |
| Cabin Data | |
| Passengers (1-class) | 172 |
| Passengers (2-class) | 152 |
| Cabin width (m) | 3.14 |
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