Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
EMB 110P1A/41 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Embraer EMB 110 Bandeirante |
|---|---|---|
| Type | Light aircraft[source] | Turboprop regional airliner[source] |
| Manufacturer | Cirrus Aircraft[source] | Embraer[source] |
| Number built | 2,084 (through 2025)[source] | 503[source] |
| Manufactured | 1999–present[source] | 1968–1990 |
15.1 m (49 ft 6 in)[source]
EMB 110P1A/41 · econ. cruise + 45 min reserve
Single source1,964 km (1,220 mi, 1,060 nmi) econ. cruise + 45 min reserve[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]
EMB 110P1A/41 · 2 × Pratt & Whitney Canada PT6A-34 turboprop engines (750 shp) each
Single source2 × Pratt & Whitney Canada PT6A-34 turboprop engines, 560 kW (750 shp) each[source]
EMB 110P1A/41 · Wing area
Single source29.1 m 2 (313 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight | 21 March 1995[source] | 26 October 1968[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 18 passengers[source] |
|---|
| Propellers | 3-bladed[source] | 3-bladed Hartzell HC-B3TN-3C/T10178H-8R, 2.36 m (7 ft 9 in) diameter fully-feathering reversible-pitch constant-speed propellers[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Brazil[source] |
|---|
| Status | — | In limited commercial service, in active military service[source] |
|---|
| Primary users | — | Brazilian Air Force Wiggins Airways Transportes Aereos Guatemaltecos[source] |
|---|
| Introduction date | — | 16 April 1973[source] |
|---|
| Fuel capacity | — | 1,308 kg (2,884 lb) / 1,720 L (450 US gal; 380 imp gal) in four integral wing tanks[source] |
|---|
| Airfoil | — | root: NACA 23016 mod. ; tip: NACA 23012[source] |
|---|
| Economical cruise speed | — | 341 km/h (212 mph; 184 kn) at 3,050 m (10,000 ft)[source] |
|---|
| Take-off run | — | 807 m (2,648 ft) (FAR23.135 / SFAR 41A)[source] |
|---|
| Landing run | — | 868 m (2,848 ft) at MLW[source] |
|---|