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]
Ka-31 · rotors folded
Single sourceConfiguration
| Specification | Cirrus SR20 | Kamov Ka-31 |
|---|---|---|
| Type | Light aircraft[source] | Airborne early warning and control[source] |
| Manufacturer | Cirrus Aircraft[source] | Kamov[source] |
| Number built | 2,084 (through 2025)[source] | 28[source] |
| Manufactured | 1999–present[source] | 1985–present[source] |
12.5 m (41 ft 0 in) rotors folded[source]
SR20-G3 · Wingspan
Single source38 ft 4 in (11.68 m)[source]
Ka-31 · 2 ×
Single source2 × 15.9 m (52 ft 2 in)[source]
Ka-31 · max. fuel with radar antenna stowed
Single source600 km (370 mi, 320 nmi) max. fuel with radar antenna stowed[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]
Ka-31 · 2 × Isotov TV3-117VMA turboshaft engines each take-off / contingency rating
Single source2 × Isotov TV3-117VMA turboshaft engines, 1,864 kW (2,500 hp) each take-off / contingency rating[source]
SR20-G3 · Service ceiling
Single source17,500 ft (5,300 m)[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Ka-31 · on-station loiter at 3,500 m (11,500 ft)
Single source2 hours 30 minutes on-station loiter at 3,500 m (11,500 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] | 1987[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | — |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | — |
|---|
| Status | — | In service, In production[source] |
|---|
| Primary users | — | Russian Navy Indian Naval Air Arm People's Liberation Army Navy[source] |
|---|
| Introduction date | — | 1995[source] |
|---|
| Developed from | — | Kamov Ka-27[source] |
|---|
| Main rotor area | — | 397.2 m 2 (4,275 sq ft)[source] |
|---|