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Fokker 50
First flight year — 1985
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Fokker 50 Specifications
| Fokker 50HP | |
| Dimensions | |
| Length (m) | 25.2 |
| Wingspan (m) | 29.0 |
| Height (m) | 8.3 |
| Wing area (m2) | 70.0 |
| Weight | |
| Maximum take-off weight (kg) | 19 950 |
| Maximum landing weight (kg) | 19 500 |
| Operating empty weight (kg) | 12 520 |
| Maximum zero fuel weight (kg) | 18 600 |
| Maximum payload (kg) | 6 080 |
| Standard fuel capacity (litres) | 5 140 |
| Performance | |
| Range with max payload (km) | 3 000 |
| Maximum cruise speed (km/h) | 530 |
| Maximum operating altitude (km) | 7 600 |
| Take-off field length (m) | 1 050 |
| Landing field length (m) | 1 120 |
| Engines | P&WC PW127B, 2 x 2750 hp |
| Fuel flow rate (kg/h) | 800 |
| Cabin Data | |
| Passengers (1-class) | 50 |
| Cabin width (m) | 2.5 |
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