The Cirrus Vision SF50 (also known as the Vision Jet) is a single-engine very light jet designed and produced by Cirrus Aircraft of Duluth, Minnesota, United States.
| Role | Very light jet |
|---|---|
| National origin | United States |
| Manufacturer | Cirrus Aircraft |
| First flight | First prototype: 3 July 2008 Conforming prototype: 24 March 2014 First production: 5 May 2016 |
| Status | In production |
| Produced | December 2016–present |
| Number built | 200 delivered (July 2020) |
Specifications (G2 model)
General characteristics
- Crew: one
- Capacity: six passengers
- Length: 30 ft 11 in (9.42 m)
- Wingspan: 38 ft 8 in (11.79 m)
- Height: 10 ft 11 in (3.32 m)
- Empty weight: 3,550 lb (1,610 kg)
- Gross weight: 6,000 lb (2,722 kg)
- Fuel capacity: 2,000 pounds (910 kg)
- Cabin Width×Height: 5.1×4.1 ft (1.56×1.24 m)
- Max payload: 1,328 lb (602 kg)
- Powerplant: 1 × Williams FJ33-5A turbofan, 1,846 lbf (8.21 kN) thrust
Performance
- Maximum speed: 311 kn (358 mph, 576 km/h) maximum cruise speed
- Cruise speed: 305 kn (351 mph, 565 km/h)
- Stall speed: 67 kn (77 mph, 124 km/h) with flaps
- Range: 600 nmi (690 mi, 1,100 km) with 1,200 lb (544 kg) payload at max cruise to 1,200 nmi (2,222 km; 1,381 mi) with 200 lb (91 kg) payload at economical cruise
- Service ceiling: 31,000 ft (9,400 m)
- Mach Maximum Operating: Mach 0.53
- Fuel consumption: 462 lb (210 kg)/h at maximum cruise, 315 lb (143 kg)/h at economical cruise
- Takeoff: 621 metres (2,036 ft) roll, 973 metres (3,192 ft) over 15 m (50 ft) obstacle
- Landing: 496 metres (1,628 ft) ground roll
Avionics
- Garmin G3000 based Cirrus Perspective Touch+
Photos Rob Vogelaar