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 121A1 Xingu II · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Embraer EMB 121 Xingu |
|---|---|---|
| Type | Light aircraft[source] | Utility aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Embraer[source] |
| Number built | 2,084 (through 2025)[source] | 106[source] |
| Manufactured | 1999–present[source] | 1977-1987[source] |
12.25 m (40 ft 2 in)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
EMB 121A1 Xingu II · at 6,100 m (20,000 ft) maximum fuel with 45 minutes reserve
Single source1,230 km (760 mi, 660 nmi) at 6,100 m (20,000 ft) maximum fuel with 45 minutes 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 121A1 Xingu II · 2 × Pratt & Whitney Canada PT6A-135 turboprop engines each
Single source2 × Pratt & Whitney Canada PT6A-135 turboprop engines, 559 kW (750 hp) each[source]
EMB 121A1 Xingu II · Wing area
Single source27.5 m 2 (296 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] | 10 October 1976[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 9 passengers or 770 kg (1,700 lb) cargo with 1 pilot[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed Hartzell HC-B4TN-3C/T9212B, 2.36 m (7 ft 9 in) diameter constant-speed metal propeller with auto-feathering and full reverse-pitch[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 141 km/h (87 mph, 76 kn) power off, flaps down[source] |
|---|
| National origin | United States[source] | Brazil[source] |
|---|
| Status | — | Active[source] |
|---|
| Primary users | — | French Air and Space Force Brazilian Air Force French Navy[source] |
|---|
| Introduction date | — | 20 May 1977[source] |
|---|
| Developed from | — | EMB 110 Bandeirante[source] |
|---|
| Fuel capacity | — | 1,308 kg (2,884 lb)[source] |
|---|
| Aspect ratio | — | 7.18[source] |
|---|
| Wing loading | — | 206.2 kg/m 2 (42.2 lb/sq ft)[source] |
|---|
| Fuel consumption | — | 0.52 kg/km (1.86 lb/mi) : 250 lb (110 kg)/h per engine at 234 kn (433 km/h) TAS, FL200, -4°C[source] |
|---|
| Power/mass | — | 0.197 kW/kg (0.12 shp/lb)[source] |
|---|