FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
Il-62M · Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Ilyushin Il-62 |
|---|---|---|
| Type | Business jet[source] | Narrow-body jet airliner[source] |
| National origin | France[source] | Soviet Union[source] |
| Manufacturer | Dassault Aviation[source] | Ilyushin, Kazan Aircraft Production Association[source] |
| Status | Active service, in production[source] | In limited service |
53.12 m (174 ft 3 in)[source]
Il-62M · Height
Single source12.35 m (40 ft 6 in)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single source10,255 kg (22,608 lb)[source]
20,640 kg (45,503 lb)[source]
Empty; Il-62M · Empty weight
Single sourceMaximum take-off; Il-62M · Max takeoff weight
Single sourceFalcon 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 lbf) thrust each[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 · 3,500 ft/min
Single source18 m/s (3,500 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] | Russian Air Force Air Koryo Rada Airlines Aeroflot (historical)[source] |
|---|
| Number built | >500[source] | 292 (5 prototypes; 94 Il-62; 193 Il-62M)[source] |
|---|
| Manufactured | 1984–present[source] | 1963–1995[source] |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 3 January 1963[source] |
|---|
| Developed from | Dassault Falcon 50[source] | — |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | 168–186 passengers[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | 105,300 L (27,800 US gal; 23,200 imp gal) / 84,240 kg (185,720 lb)[source] |
|---|
| Aspect ratio | 7.63:1[source] | — |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | — |
|---|
| Designer | — | Ilyushin[source] |
|---|
| Built by | — | KAPO[source] |
|---|
| Introduction date | — | Il-62 – 15 September 1967 Il-62M – 9 March 1974[source] |
|---|