Fokker S.14 Machtrainer
Photo ©: Karsten Palt
S.14 Machtrainer
Jet Trainer
The Fokker S.14 Machtrainer is a two seat single engine jet trainer aircraft built by the Netherlands manufacturer Fokker N.V..
| Crew | 2 | |
| Propulsion | 1 Turbojet Engine | |
| Engine Model | Rolls-Royce Derwent VIII | |
| Engine Power | 15,5 kN | 3485 lbf |
| max. Cruise Speed | 1056 km/h | 570 kts 656 mph |
| max. Speed (vne) | 1352 km/h | 730 kts 840 mph |
| Service Ceiling | 11.200 m | 36.745 ft |
| Rate of climb | 945 m/min | 3100 ft/min |
| Range | 965 km | 521 NM 600 mi. |
| Empty Weight | 3.765 kg | 8.300 lbs |
| max. Takeoff Weight | 5.350 kg | 11.795 lbs |
| Wing Span | 12,00 m | 39,4 ft |
| Wing Area | 31,8 m² | 342 ft² |
| Length | 13,30 m | 43,6 ft |
| Height | 4,70 m | 15,4 ft |
| First Flight | 19.05.1951 | |
| Production Status | out of production | |
| Production Range | 1954-1956 | |
| Total Production | 21 | |
| Data for (Version) | Fokker S.14 | |
Remarks
The Fokker S.14 was the first jet trainer designed as such and entered into series production. The S.14 was in operation with the Royal Netherlands Air Force (Koninklijke Luchtmacht) only. Only three surviving aircraft left (c/n 6289, 7356 & 7662).
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