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]
Il-62M · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Ilyushin Il-62 |
|---|---|---|
| Type | Light aircraft[source] | Narrow-body jet airliner[source] |
| Manufacturer | Cirrus Aircraft[source] | Ilyushin, Kazan Aircraft Production Association[source] |
| Number built | 2,084 (through 2025)[source] | 292 (5 prototypes; 94 Il-62; 193 Il-62M)[source] |
| Manufactured | 1999–present[source] | 1963–1995 |
53.12 m (174 ft 3 in)[source]
Il-62M · with 10,000 kg (22,046 lb) payload
Single source10,000 km (6,200 mi, 5,400 nmi) with 10,000 kg (22,046 lb) payload[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]
Il-62M · 4 × Soloviev D-30KU turbofan engines thrust each
Single source4 × Soloviev D-30KU turbofan engines, 107.9 kN (24,300 lbf) thrust each[source]
Il-62M · Wing area
Single source279.55 m 2 (3,009.1 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] | 3 January 1963[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 168–186 passengers[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Soviet Union[source] |
|---|
| Designer | — | Ilyushin[source] |
|---|
| Built by | — | KAPO[source] |
|---|
| Status | — | In limited service[source] |
|---|
| Primary users | — | Russian Air Force Air Koryo Rada Airlines Aeroflot (historical)[source] |
|---|
| Introduction date | — | Il-62 – 15 September 1967 Il-62M – 9 March 1974[source] |
|---|
| Fuel capacity | — | 105,300 L (27,800 US gal; 23,200 imp gal) / 84,240 kg (185,720 lb)[source] |
|---|