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Aircraft type: Commercial airplane
Manufacturer: Douglas
Maiden flight year: 1965
DC-9-30 | DC-9-50 | |
Dimensions | ||
---|---|---|
Length (m) | 36.4 | 40.7 |
Wingspan (m) | 28.5 | 28.5 |
Height (m) | 8.4 | 8.4 |
Wing area (m2) | 93 | 93 |
Weight | ||
Maximum take-off weight (kg) | 49 900 | 54 400 |
Maximum landing weight (kg) | 45 800 | 49 900 |
Operating empty weight (kg) | 25 400 | 29 300 |
Maximum zero fuel weight (kg) | 39 460 | 44 670 |
Maximum payload (kg) | 16 300 | 15 400 |
Standard fuel capacity (litres) | 13 900 | 16 100 |
Performance | ||
Range with max payload (km) | 2 200 | 1 850 |
Cruise speed (km/h) | 910 | 900 |
Maximum operating altitude (m) | 10 700 | 10 700 |
Take-off field length (m) | 1 800 | 2 360 |
Landing field length (m) | 1 300 | 1 440 |
Engines | P&W JT8D-7, 2 x 14000 lb | P&W JT8D-15, 2 x 15500 lbP&W JT8D-17, 2 x 16200 lb |
Cabin Data | ||
Passengers (1-class) | 119 | 139 |
Passengers (2-class) | 105 | 125 |
Cabin width (m) | 3.14 | 3.14 |
33% | 34% | 33% |