Original version SR22
Launched in April 2007, the SR22 G3 variant hay, from 81 to 92 s an increased range and fuel capacitU.S. gallons (310 to 350 L; 67 to 77 imp gal), a lighter carbon fiber wing spar and longer landing gear for increased prop clearance.[63] Upgraded models, such as the GTS, come with airbag seatbelts
SR22T
Introduced in June 2010, with a turbocharged Continental TSIO-550-K producing 315 hp (235 kW). The engine has low-compression pistons, producing a 7.5 to 1 compression ratio to allow the engine to run on lower octane fuel, 94UL. The SR22T has a maximum cruise speed of 214 kn (396 km/h), empty weight of 2,348 lb (1,065 kg), and a maximum operating altitude of 25,000 ft (7,620 m). This model also has a decreased useful load of 1,052 lb (477 kg) and reduced range of 1,046 nmi (1,937 km), as well as a Hartzell three-blade lightweight composite prop.
Flight into known icing
Cirrus completed testing for flight into known icing conditions (FIKI) on 12 January 2009. The equipment change involved installing a larger fluid tank for the TKS Ice Protection System and protecting more areas of the aircraft. The FAA approved the new installation in April 2009.
SR22 Turbo G2
SR22T
SR22/22T G5
SR22/22T G6
General characteristics
Crew: one
Capacity: four passengers
Length: 26 ft 0 in (7.92 m)
Wingspan: 38 ft 4 in (11.68 m)
Height: 8 ft 11 in (2.72 m)
Empty weight: 2,269 lb (1,029 kg)
Gross weight: 3,600 lb (1,633 kg)
Fuel capacity: 92 US gallons (348 liters)
Powerplant: 1 × Continental IO-550-N Six cylinder horizontally opposed aircraft engine, 310 hp (230 kW)
Propellers: 3-bladed
Performance
Cruise speed: 183 kn (211 mph, 339 km/h)
Stall speed: 60 kn (69 mph, 110 km/h) flaps down
Range: 1,049 nmi (1,207 mi, 1,943 km) with reserves at 65% power
Service ceiling: 17,500 ft (5,300 m)
Rate of climb: 1,270 ft/min (6.5 m/s)
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