Fuji / Rockwell FA-300 / Commander 700
Corporate Aircraft
The Fuji FA-300 and Rockwell Commander 700 is a twin-engined six-seat corporate aircraft with pressurized cabin produced jointly by the Japanese manufacturer Fuji Heavy Industries and the US-American manufacturer Rockwell International.
| Propulsion | 2 Piston Engines |
| Engine Model | Lycoming TIO-540-R2AD |
| Engine Power (each) | 254 kW | 340 hp |
| Speed | 409 km/h | 221 kts
254 mph |
| Service Ceiling | 8.352 m | 27.400 ft |
| Range | 2.226 km | 1.202 NM
1.383 mi. |
| Empty Weight | 2.134 kg | 4.705 lbs |
| max. Takeoff Weight | 3.151 kg | 6.947 lbs |
| Wing Span | 12,94 m | 42 ft 5 in |
| Wing Area | 18,6 m² | 200 ft² |
| Length | 12,03 m | 39 ft 6 in |
| Height | 4,05 m | 13 ft 3 in |
| First Flight | 13. Nov. 1975 |
| Production Status | out of production |
| Total Production | 49 |
| ICAO Code | RC70 |
| Data for (Version) | Fuji FA-300 / Rockwell Commander 700 |
| Variants | Commander 710 / FA-300 Kai |
