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Cirrus SR20
The SR20 is the smaller-engined SR, approved by the FAA in 1998 with a 200 hp Continental IO-360-ES; the current SR20 has a 215 hp Lycoming IO-390. The figures are those of the current airplane: a maximum weight of 3,150 pounds, 56 US gallons of usable fuel, a maximum operating altitude of 17,500 feet and a maximum cruise speed of 155 knots true airspeed, as Cirrus states it. Span, length and height are from the EASA data sheet. It seats four, five in later aircraft.
- Cruise speed
- 155 knots (290 km/h)
- Seats
- About 4 (up to 5)
- Engines
- One piston engine in the nose: Lycoming IO-390-C3B6; Continental IO-360-ES (earlier aircraft)
- Max takeoff weight
- 3,200 lb (1,429 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 | 60 US gal (212 L) |
| Status | In service |
| Type codes | ICAO SR20 |
Private aircraft show specs only. No flight data is shown for them.