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Fokker 100
First flight year — 1986
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Fokker 100 Specifications
| Fokker 100 | |
| Dimensions | |
| Length (m) | 35.5 |
| Wingspan (m) | 28.1 |
| Height (m) | 8.5 |
| Wing area (m2) | 93.5 |
| Weight | |
| Maximum take-off weight (kg) | 45 810 |
| Maximum landing weight (kg) | 39 910 |
| Operating empty weight (kg) | 24 750 |
| Maximum zero fuel weight (kg) | 36 740 |
| Maximum payload (kg) | 12 000 |
| Standard fuel capacity (litres) | 13 360 |
| Performance | |
| Range with max payload (km) | 3 100 |
| Maximum operating altitude (km) | 10 700 |
| Take-off field length (m) | 1 820 |
| Landing field length (m) | 1 350 |
| Engines | R-R Tay 650, 2 x 15100 lb |
| Cabin Data | |
| Passengers (1-class) | 107 |
| Cabin width (m) | 3.1 |
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