Fokker G.I
Heavy Fighter
Photo ©: Karsten Palt
The Fokker G.I is a twin-engined heavy fighter aircraft with a crew of 2 or 3 produced by the Dutch manufacturer Fokker, N.V. Koninklijke Nederlandsche Vliegtuigenfabriek.
Today, there are no surviving Fokker G.1.
| Crew | 2 / 3 | |
| Propulsion | 2 Radial Engines | |
| Engine Model | Bristol Mercury VIII | |
| Engine Power (each) | 619 kW | 830 hp |
| max. Cruise Speed | 356 km/h | 192 kts 221 mph |
| max. Speed (vne) | 474 km/h | 256 kts 295 mph |
| Service Ceiling | 9.300 m | 30.512 ft |
| Rate of climb | 835 m/min | 2740 ft/min |
| Range | 1.400 km | 756 NM 870 mi. |
| Empty Weight | 3.360 kg | 7.408 lbs |
| max. Takeoff Weight | 4.800 kg | 10.582 lbs |
| Wing Span | 17,15 m | 56 ft 3 in |
| Wing Area | 38,3 m² | 412 ft² |
| Length | 11,50 m | 37 ft 9 in |
| Height | 3,40 m | 11 ft 2 in |
| First Flight | 19.03.1937 | |
| Production Status | out of production | |
| Production Range | 1937-1940 | |
| Total Production | 62 | |
| Data for (Version) | Fokker G.Ia | |
| Variants | G.I, G.IA, G.IB | |
| [Photo-ID: 2462] © Karsten Palt 2009-06-25 | |
 | Fokker G.IA Royal Netherlands AF / Koninklijke Luchtmacht Reg.: 330 Replica |
| Militaire Luchtvaart Museum [Soesterberg] | |