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]
Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Ilyushin Il-96 |
|---|---|---|
| Type | Light aircraft[source] | Widebody jet airliner[source] |
| Manufacturer | Cirrus Aircraft[source] | Voronezh Aircraft Production Association[source] |
| Number built | 2,084 (through 2025)[source] | 34[source] |
| Manufactured | 1999–present[source] | 1992–present |
55.35 m (181 ft 7 in)[source]
Range
Single source10,000 km (5,400 nmi )[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]
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]
Maximum payload
Single source40 t (88,105 lb)[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] | 28 September 1988 ( 1988-09-28 )[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] | Soviet Union / Russia[source] |
|---|
| Designer | — | Ilyushin[source] |
|---|
| Built by | — | Voronezh Aircraft Production Association[source] |
|---|
| Status | — | In service, in production[source] |
|---|
| Primary users | — | Russian Air Force Cubana de Aviación Sky Gates Airlines Aeroflot (historical)[source] |
|---|
| Introduction date | — | 29 December 1992 with Aeroflot[source] |
|---|
| Developed from | — | Ilyushin Il-86[source] |
|---|
| Wing geometry | — | 60.12 m (197 ft 3 in) span, 350 m 2 (3767.9 ft²), 30° sweep[source] |
|---|
| OEW | — | 120.4 t (265,198 lb)[source] |
|---|
| Fuel capacity | — | 152,620 L (40,322 US gal , 33,575 imp gal)[source] |
|---|