Cirrus Vision SF50 Specs, Interior, Cockpit, and Price – Cirrus Vision SF50 is a very lightweight single-engine business jet with seven seats designed and manufactured by Cirrus Design Corporation (CDC), United States. This business jet made its first flight on July 3, 2008. The SF50 was developed with the requirements of a lightweight private jet intended for the single pilot operating market.
In 2011, Cirrus was purchased by CAIGA, a Chinese company that funded the project a year later. The first adjustment prototype then flew on March 24, 2014, followed by two other prototypes that same year. On October 28, 2016, Cirrus Vision SF50 obtained a type certificate from the US Federal Aviation Administration.
These business jets are equipped with Cirrus airframe parachute system (CAPS) features, ice protection systems, large abdominal parts, double pelvic fins, steam cycle cooling systems, onboard oxygen generating systems, optional toilets, satellite telephones, lightning detection and ski tubes.
Cirrus Vision SF50 is equipped with a ballistic recovery system, emergency exits, retractable landing gear, dark windows, pusher sticks, single cabin pressure vessels, environmental control systems, and parachutes on large pointed noses.
The FJ33 engine is equipped with two stage low pressure turbines, centrifugal high pressure compressors, one stage high pressure turbines, one stage fan and annular combustion.
Cirrus Vision SF50 can fly with a maximum speed of 555 km / hour. The stall speed is 111 km / hour. The service ceiling is 8,500 m. Airplane takeoff and landing distances are 492m and 379m.
The cabin is 3.33 m long, 1.56 m wide and 1.24 m high. It features a luggage compartment of 0.88m3 on the back of the aircraft to place passenger luggage. The length, width and height of the luggage compartment are 0.91mX1.22mX0.79m.
Cirrus Vision SF50 avionics suite includes a 12-inch dual heading heading system (AHRS), dual wide area augmentation system (WAAS), global positioning system (GPS), active traffic system, GPS, XM radio, twin air data computer ( ADC)), Transponder Mode S, audio and telephone input, digital data processing A / P, ADL and SD 3-axis.
Other avionics installed include the second S Mode transponder, automatic direction finder (ADF), distance measuring equipment (DME), enhanced vision system (EVS) and warning and terrain systems (TAWS) to alert pilots of potential conflicts with obstacles and terrain.
In 2011, Cirrus was purchased by CAIGA, a Chinese company that funded the project a year later. The first adjustment prototype then flew on March 24, 2014, followed by two other prototypes that same year. On October 28, 2016, Cirrus Vision SF50 obtained a type certificate from the US Federal Aviation Administration.
Cirrus Vision SF50 Specs
Cirrus Vision SF50 has a low wing monoplane design and consists of carbon fiber composite material. The aircraft can operate day and night, and in an environment that is not friendly.These business jets are equipped with Cirrus airframe parachute system (CAPS) features, ice protection systems, large abdominal parts, double pelvic fins, steam cycle cooling systems, onboard oxygen generating systems, optional toilets, satellite telephones, lightning detection and ski tubes.
Cirrus Vision SF50 is equipped with a ballistic recovery system, emergency exits, retractable landing gear, dark windows, pusher sticks, single cabin pressure vessels, environmental control systems, and parachutes on large pointed noses.
Cirrus Vision SF50 Engine
Cirrus Vision SF50 is powered by a single William FJ33 turbofan engine with a maximum thrust of 8.5kN. This machine was designed and manufactured by US-based engine manufacturer William International. The length and diameter of the machines are 0.97 m and 0.53 m, respectively. The dry weight is 140kg. The time between repairs (TBO) of the engine is 4,000 hours.The FJ33 engine is equipped with two stage low pressure turbines, centrifugal high pressure compressors, one stage high pressure turbines, one stage fan and annular combustion.
Cirrus Vision SF50 can fly with a maximum speed of 555 km / hour. The stall speed is 111 km / hour. The service ceiling is 8,500 m. Airplane takeoff and landing distances are 492m and 379m.
Cirrus Vision SF50 Cabin and Interior
Cirrus Vision SF50 has a pressurized cabin in a single carbon shell. The cabin can accommodate six passengers in three rows in a parallel seating configuration. It has an optional seat between the second and third rows.The cabin is 3.33 m long, 1.56 m wide and 1.24 m high. It features a luggage compartment of 0.88m3 on the back of the aircraft to place passenger luggage. The length, width and height of the luggage compartment are 0.91mX1.22mX0.79m.
Cirrus Vision SF50 Cockpit and Avionics
Cirrus Vision SF50 digital cockpit can accommodate a stwo pilots. SF50 was initially integrated with the L-3 SmartDeck avionics suite which was later replaced with the Garmin G1000 avionics package. Garmin Avionics was selected as the main contractor for the avionics package by the CDC in March 2009.Cirrus Vision SF50 avionics suite includes a 12-inch dual heading heading system (AHRS), dual wide area augmentation system (WAAS), global positioning system (GPS), active traffic system, GPS, XM radio, twin air data computer ( ADC)), Transponder Mode S, audio and telephone input, digital data processing A / P, ADL and SD 3-axis.
Other avionics installed include the second S Mode transponder, automatic direction finder (ADF), distance measuring equipment (DME), enhanced vision system (EVS) and warning and terrain systems (TAWS) to alert pilots of potential conflicts with obstacles and terrain.
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