Cirrus Aircraft
Vision Jet G2
The second-generation Vision Jet, with a higher operating altitude and revised cockpit and cabin features.
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Aircraft profile
Development and lineage
- Manufacturer
- Cirrus Aircraft
- Family
- Vision Jet G2
- Aircraft category
- Personal Jet
- Propulsion
- Jet
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
- 31,000 ft, with RVSM capability
- High-speed cruise reference
- 313 KTAS at 27,000 ft
- Range reference
- Approximately 1,100 nautical miles at high-speed cruise; up to 1,275 at economy cruise
- Cabin pressure differential
- 7.1 psi
- Flight deck
- Cirrus Perspective Touch+ with autothrottle
- Airframe parachute
- Cirrus Airframe Parachute System (CAPS)
2019 G2 reference configuration. Cruise speed and range use different operating points; equipment and empty weight vary.
Overview
The G2 Vision Jet develops the original single-engine personal jet with a 31,000-foot operating altitude, Perspective Touch+ avionics and an available autothrottle. Cabin and acoustic refinements accompany the mission and cockpit changes.
Program history
Cirrus introduced the G2 in 2019 as an evolution of the SF50. Its development aimed to make longer personal and business journeys more practical while retaining the original aircraft’s owner-pilot focus.