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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Il-18D · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Ilyushin Il-18 |
|---|---|---|
| Type | Light aircraft[source] | Turboprop airliner and reconnaissance aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Moscow Machinery Plant No. 30[source] |
| Number built | 2,084 (through 2025)[source] | at least 678[source] |
| Manufactured | 1999–present[source] | 1957–1985 |
35.9 m (117 ft 9 in)[source]
Il-18D · with 13,500 kg (29,762 lb) maximum payload, at 84 - 85% of maximum continuous power
Single sourceIl-18D · with 6,500 kg (14,330 lb) payload, maximum fuel and reserves for one hour
Single source6,500 km (4,000 mi, 3,500 nmi) with 6,500 kg (14,330 lb) payload, maximum fuel and reserves for one hour. 3,700 km (2,299 mi; 1,998 nmi) with 13,500 kg (29,762 lb) maximum payload, at 84 - 85% of maximum continuous power.[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-18D · 4 × Ivchenko AI-20M axial flow turboprop engines each
Single source4 × Ivchenko AI-20M axial flow turboprop engines, 3,170 kW (4,250 hp) each[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Il-18D · Wing area
Single source140 m 2 (1,500 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] | 4 July 1957[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 65-120 passengers[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed AW-68 I constant speed feathering propellers, 4.5 m (14 ft 9 in) diameter Auxiliary power unit: TG-16M (28 Volt DC)[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Soviet Union[source] |
|---|
| Designer | — | Ilyushin[source] |
|---|
| Status | — | In limited service[source] |
|---|
| Primary users | — | Russian Air Force Russian Naval Aviation Air Koryo Aeroflot (historical)[source] |
|---|
| Variants | — | Ilyushin Il-20M Ilyushin Il-38[source] |
|---|
| Successors | — | Ilyushin Il-62[source] |
|---|
| Fuel capacity | — | 30,000 L (6,599 imp gal; 7,925 US gal)[source] |
|---|
| Fuselage diameter | — | 3.5 m (11 ft)[source] |
|---|
| Max. landing weight | — | 52,600 kg (115,963 lb)[source] |
|---|
| Max. zero-fuel weight | — | 48,800 kg (107,586 lb)[source] |
|---|
| Max. taxi weight | — | 64,500 kg (142,198 lb)[source] |
|---|
| Auxiliary power unit | — | TG-16M (28 Volt DC)[source] |
|---|
| Approach minima | — | ICAO CAT 1 Decision Height 60 m (200 ft) / 800 m (Visibility) or 550 m RVR[source] |
|---|
| Take-off run | — | 1,350 m (4,430 ft)[source] |
|---|
| Landing run | — | 850 m (2,790 ft)[source] |
|---|
| RPSN-2AMG | — | or RPSN-2N Emblema weather radar[source] |
|---|
| NAS-1B | — | autonomous navigation system DISS-1: doppler speed/drift sensor ANU-1: autonomous navigation computer[source] |
|---|
| DISS-1 | — | doppler speed/drift sensor[source] |
|---|
| ANU-1 | — | autonomous navigation computer[source] |
|---|
| Put'-4M | — | navigation system[source] |
|---|
| KS-6G | — | compass system[source] |
|---|
| DAK-DB | — | remote celestial compass[source] |
|---|
| RSBN-2S Svod | — | SHORAN ( Svod - Dome)[source] |
|---|
| SP-50 Materik | — | ILS[source] |
|---|
| RV-UM | — | radio altimeter[source] |
|---|
| NI-50BM-1 | — | navigation display[source] |
|---|
| ARK-11 | — | main and backup ADF (automatic direction finder)[source] |
|---|
| RSB-5/1230 | — | communications radio[source] |
|---|
| RSIU-5 (R802G) | — | command link radio, 2 of.[source] |
|---|
| SR-2M Khrom | — | IFF transponder ( Khrom - Chromium)[source] |
|---|
| MSRP-12-96 | — | flight data recorder[source] |
|---|