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 · 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]
2 × Pratt & Whitney Canada PT6A-42 turboprop engines (850 shp) each
Single source2 × Pratt & Whitney Canada PT6A-42 turboprop engines, 630 kW (850 shp) each[source]
Wing area
Single source41.5 m 2 (447 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Cirrus SR20 | Indonesian Aerospace N219 |
|---|---|---|
| Type | Light aircraft[source] | Utility aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Indonesian Aerospace[source] |
| Number built | 2,084 (through 2025)[source] | 2 prototypes (December 2024)[source] |
| Manufactured | 1999–present[source] | 2017–present[source] |
| First flight | 21 March 1995[source] | 16 August 2017[source] |
| Developed into | Cirrus SR22[source] | — |
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 19 passengers[source] |
| Propellers | 3-bladed[source] | 4-bladed Hartzell Propeller aluminum autofeathering or 5-bladed MT-Propeller CFRP autofeathering[source] |
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 109 km/h (68 mph, 59 kn)[source] |
| National origin | United States[source] | Indonesia[source] |
| Status | — | In production[source] |
| Fuel capacity | — | 1,600 kg[source] |
| g limits | — | -1.2 g to +3.0 g (flaps retracted)[source] |
| Takeoff distance | — | 435 meters (1,427 feet)[source] |
| Landing distance | — | 509 meters (1,670 feet)[source] |
| Alternative designation | — | N219[source] |