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At a glance
Measured figures
Empty; Cessna S550 Citation S/II · Empty weight
Single sourceMaximum take-off; Cessna S550 Citation S/II · Max takeoff weight
Single source8,059 lb (3,656 kg)[source]
15,100 lb (6,849 kg)[source]
Empty; SR20-G3 · Empty weight
Single sourceGross; SR20-G3 · Gross weight
Single sourceCessna S550 Citation S/II · with max fuel
Single source1,998 nmi (2,299 mi, 3,700 km) (with max fuel)[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
Cessna S550 Citation S/II · 2 × Pratt & Whitney Canada JT15D -4B turbofans thrust each
Single source2 × Pratt & Whitney Canada JT15D -4B turbofans , 2,500 lbf (11 kN) thrust each[source]
Cessna S550 Citation S/II · Wing area
Single source342.6 sq ft (31.83 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Cessna Citation II | Cirrus SR20 |
|---|---|---|
| Type | Corporate jet[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Number built | 1184: 688 II and II/SP, 160 S/II, 336 Bravo[source] | 2,084 (through 2025)[source] |
| Manufactured | 1978–2006[source] | 1999–present[source] |
| First flight | January 31, 1977[source] | 21 March 1995[source] |
| Developed from | Cessna Citation I[source] | — |
| Developed into | Cessna Citation V[source] | Cirrus SR22[source] |
| Capacity | Six to eight passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
| Fuel capacity | 862 US gal (718 imp gal; 3,260 L) usable fuel[source] | — |
| Airfoil | NACA 23000[source] | — |
| Stall speed | 82 kn (94 mph, 152 km/h) ( CAS )[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
| Propellers | — | 3-bladed[source] |