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At a glance
Measured figures
Queen Air B80 · Length
Single source35 ft 6 in (10.82 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Beechcraft Queen Air | Cirrus SR20 |
|---|---|---|
| Type | Utility aircraft Airliner[source] | Light aircraft[source] |
| Manufacturer | Beech Aircraft Corporation[source] | Cirrus Aircraft[source] |
| Designer | Beech Aircraft Corporation[source] | — |
| Status | In service[source] | — |
| Number built | 1,005[source] |
26 ft 0 in (7.92 m)[source]
Cruise; Queen Air B80 · at 15,000 ft (4,600 m), 45% power (econ cruise)
Single sourceMaximum; Queen Air B80 · at 11,500 ft (3,500 m)
Single source215 kn (247 mph, 398 km/h) at 11,500 ft (3,500 m)[source]
159 kn (183 mph, 294 km/h) at 15,000 ft (4,600 m), 45% power (econ cruise)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Queen Air B80 · at 15,000 ft (4,600 m), 45% power
Single source1,317 nmi (1,516 mi, 2,439 km) at 15,000 ft (4,600 m), 45% power[source]
Queen Air B80 · 2 × Lycoming IGSO-540 A1D supercharged, air-cooled flat-6 engines each
Single source2 × Lycoming IGSO-540 A1D supercharged, air-cooled flat-6 engines, 380 hp (280 kW) each[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]
Queen Air B80 · Wing area
Single source293.9 sq ft (27.30 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
2,084 (through 2025)[source] |
| Manufactured | 1960-1978[source] | 1999–present[source] |
|---|
| Introduction date | 1960[source] | — |
|---|
| First flight | August 28, 1958[source] | 21 March 1995[source] |
|---|
| Developed from | Beechcraft Twin Bonanza[source] | — |
|---|
| Developed into | Beechcraft U-21 Ute Beechcraft King Air Beechcraft Model 99[source] | Cirrus SR22[source] |
|---|
| Capacity | 4–9 passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Airfoil | NACA 23020 at root, NACA 23012 at tip[source] | — |
|---|
| Fuel capacity | 214 US gal (178 imp gal; 810 L) normal, 264 US gal (220 imp gal; 1,000 L) with optional auxiliary tanks[source] | — |
|---|
| Propellers | 3-bladed Hartzell constant speed[source] | 3-bladed[source] |
|---|
| Stall speed | 71 kn (82 mph, 131 km/h) wheels and flaps down, IAS[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Takeoff distance to 50 ft (15m) | 2,556 ft (779 m)[source] | — |
|---|
| Landing distance from 50 ft (15m) | 2,572 ft (784 m)[source] | — |
|---|
| Country of origin | United States[source]Country/countries explicitly given in the equipment row Origin column; not the country operating the row. Beech 80 Queen Air | — |
|---|
| National origin | — | United States[source] |
|---|