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Cirrus SR22
The SR22, approved by the FAA in 2000, is the SR with a 310 hp Continental IO-550-N and no turbocharger. The figures are those of the later aircraft, from the FAA and EASA data sheets: a maximum weight of 3,600 pounds, 92 US gallons of usable fuel and a maximum operating altitude of 17,500 feet. Cirrus gives a maximum cruise speed of 183 knots true airspeed. Span, length and height are from the EASA data sheet. It seats four, five in later aircraft, and is ICAO code SR22.
- Cruise speed
- 183 knots (340 km/h)
- Seats
- About 4 (up to 5)
- Engines
- One piston engine in the nose: Continental IO-550-N
- Max takeoff weight
- 3,600 lb (1,633 kg)
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Specifications
| Length | 26 ft 0 in (7.92 m) |
|---|---|
| Wingspan | 38 ft 3 in (11.67 m) |
| Height | 8 ft 11 in (2.71 m) |
| Fuselage width | 4 ft 1 in (1.25 m) |
| Ceiling | 17,500 ft (5,300 m) |
| Fuel capacity | 90 US gal (348 L) |
| Status | In service |
| Type codes | ICAO SR22 |
Private aircraft show specs only. No flight data is shown for them.