Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
C-2 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Kawasaki C-2 |
|---|---|---|
| Type | Light aircraft[source] | Military transport aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Kawasaki Aerospace Company[source] |
| Number built | 2,084 (through 2025)[source] | 21[source] |
| Manufactured | 1999–present[source] | 2010–present[source] |
43.9 m (144 ft 0 in)[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]
C-2 · 2 × General Electric CF6 -80C2K1F turbofan engines thrust each
Single source2 × General Electric CF6 -80C2K1F turbofan engines, 265.7 kN (59,740 lbf) thrust each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[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 January 2010[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 32 t limited to + 2.5g ; 36 t limited to + 2.25g ; maximum payload 37.6 t Field Operation System or Truck Crane or 8 463L Pallets or 1 UH-60JA helicopter or 1 Type 16 maneuver combat vehicle wheeled tank destroyer[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Japan[source] |
|---|
| Status | — | In service, in production[source] |
|---|
| Primary user | — | Japan Air Self-Defense Force[source] |
|---|
| Introduction date | — | 30 June 2016[source] |
|---|
| Minimum takeoff distance | — | 500 m (1,641 ft)[source] |
|---|