Credit
Marko Stojkovic · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Length
Single source23.8 m (78 ft 1 in)[source]
Falcon 20F · Length
Single sourceConfiguration
| Specification | Antonov An-26 | Dassault Falcon 20 |
|---|---|---|
| Type | Transport aircraft / regional airliner[source] | Business jet[source] |
| National origin | Soviet Union[source] | France[source] |
| Manufacturer | Antonov Serial Production Plant[source] | Dassault Aviation[source] |
| Designer | Antonov[source] | — |
17.15 m (56 ft 3 in)[source]
Cruise; Cruise speed
Single source440 km/h (270 mph, 240 kn)[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]
2 × Progress AI-24VT Turboprop engines each
Single source2 × Progress AI-24VT Turboprop engines, 2,103 kW (2,820 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]
1,600 ft/min
Single source8 m/s (1,600 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status |
|---|
In service[source] |
Out of production, in active service[source] |
| Primary users | Soviet Air Forces (former) Russian Aerospace Forces Ukrainian Air Force People's Liberation Army Air Force[source] | Federal Express (formerly) French Navy United States Coast Guard[source] |
|---|
| Number built | 1,403[source] | 512[source] |
|---|
| Manufactured | 1969–present (in China as Y-7)[source] | 1965–1991[source] |
|---|
| Introduction date | 1972[source] | 3 June 1965[source] |
|---|
| First flight | 21 May 1969[source] | 4 May 1963[source] |
|---|
| Developed from | Antonov An-24[source] | — |
|---|
| Developed into | Xi'an Y-7 Antonov An-32[source] | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | 40 passengers / 5,500 kg (12,100 lb)[source] | 8–14 passengers[source] |
|---|
| Aspect ratio | 11.7:1[source] | 6.4:1[source] |
|---|
| Propellers | 4-bladed Constant speed metal bladed propellers, 3.90 m (12 ft 10 in) diameter[source] | — |
|---|
| Range with max payload | 1,100 km (680 mi)[source] | — |
|---|
| Fuel capacity | — | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
|---|
| Stall speed | — | 152 km/h (94 mph, 82 kn)[source] |
|---|