Cirrus Aircraft
SF50 Vision Jet / first generation (G1)
The original single-engine Vision Jet, created as a step into jet ownership for personal-aircraft operators.
Explore Cirrus Aircraft
Aircraft profile
Development and lineage
- Manufacturer
- Cirrus Aircraft
- Family
- SF50 Vision Jet
- Aircraft category
- Personal Jet
- Propulsion
- Jet
Aliases and related designations
first generation (G1)
Aircraft data
Key specifications
- Engine
- One Williams International FJ33-5A turbofan
- Rated thrust
- 1,846 lbf
- Maximum takeoff weight
- 6,000 lb
- Aircraft length
- 30 ft 8 in
- Wingspan
- 38 ft 8 in
- Aircraft height
- 10 ft 11 in
- Cabin length / width / height
- 11 ft 6 in / 5 ft 1 in / 4 ft 1 in
- Seating
- Up to five adults and two children, including the pilot; child seats limited to 90 lb each
- Usable fuel
- 296 US gallons
- Baggage allowance
- 23.5 cu ft; 300 lb maximum in the reference configuration
- Maximum operating altitude
- 28,000 ft
- High-speed cruise reference
- 308 KTAS at 23,000 ft
- Range reference
- Approximately 1,000 nautical miles at high-speed cruise; approximately 1,200 at economy cruise
- Takeoff distance over 50 ft
- 3,192 ft, standard-day gross-weight reference
- Flight deck
- Cirrus Perspective Touch, based on Garmin G3000
- Airframe parachute
- Cirrus Airframe Parachute System (CAPS)
First-generation SF50 reference figures. Range depends on cruise setting, reserves and payload.
Overview
The first-generation SF50 pairs a single dorsal-mounted Williams engine with a V-tail and a flexible family-sized cabin. Its whole-airframe parachute system carries a familiar Cirrus safety concept from the company’s piston aircraft into a jet.
Program history
The Vision Jet entered service in 2016 to bridge high-performance piston flying and the light-jet market. Later G2, G2+ and G3 versions add capabilities that should not be assumed to be present on an original G1.