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Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
Il-18D · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Ilyushin Il-18 |
|---|---|---|
| Type | Business jet[source] | Turboprop airliner and reconnaissance aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Moscow Machinery Plant No. 30[source] |
| Status | Out of production, in active service[source] | In limited service[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | Russian Air Force Russian Naval Aviation Air Koryo Aeroflot (historical) |
35.9 m (117 ft 9 in)[source]
Cruise; Falcon 20F · at 12,200 m (40,000 ft) (econ. cruise)
Single sourceMaximum; Falcon 20F · at 7,620 m (25,000 ft) (max cruise)
Single source862 km/h (536 mph, 465 kn) at 7,620 m (25,000 ft) (max cruise)[source]
750 km/h (470 mph, 400 kn) at 12,200 m (40,000 ft) (econ. cruise)[source]
Cruise; Il-18D · at 8,000 m (26,000 ft)
Single sourceMaximum; Il-18D · Maximum speed
Single sourceFalcon 20F · Range
Single source3,350 km (2,080 mi, 1,810 nmi)[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]
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]
Falcon 20F · 2 × General Electric CF700 -2D-2 turbofans thrust each
Single source2 × General Electric CF700 -2D-2 turbofans , 20 kN (4,500 lbf) thrust each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 512[source] | at least 678[source] |
|---|
| Manufactured | 1965–1991[source] | 1957–1985[source] |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | 4 July 1957[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | 65-120 passengers[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 30,000 L (6,599 imp gal; 7,925 US gal)[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | — |
|---|
| National origin | France[source] | Soviet Union[source] |
|---|
| Designer | — | Ilyushin[source] |
|---|
| Variants | — | Ilyushin Il-20M Ilyushin Il-38[source] |
|---|
| Successors | — | Ilyushin Il-62[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] |
|---|
| Propellers | — | 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] |
|---|
| 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] |
|---|