FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
An-28 · Length
Single source13.10 m (43 ft 0 in)[source]
Falcon 20F · Length
Single sourceConfiguration
| Specification | Antonov An-28 | Dassault Falcon 20 |
|---|---|---|
| Type | Short-range airliner , utility aircraft[source] | Business jet[source] |
| Designer | Antonov[source] | — |
| Built by | WSK PZL Mielec[source] | — |
| Status | In service[source] | Out of production, in active service[source] |
| Primary user | Aeroflot (former)[source] |
17.15 m (56 ft 3 in)[source]
Cruise; An-28 · at 3,000 m (9,800 ft)
Single sourceMaximum; An-28 · at 3,000 m (9,800 ft)
Single source350 km/h (220 mph, 190 kn) at 3,000 m (9,800 ft)[source]
335 km/h (208 mph, 181 kn) at 3,000 m (9,800 ft)[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 sourceAn-28 · 2 × Glushenkov TVD-10B turboprop engines (960 shp) each
Single source2 × Glushenkov TVD-10B turboprop engines, 720 kW (960 shp) 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]
An-28 · 1,640 ft/min
Single source8.3 m/s (1,640 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 191[source] | 512[source] |
|---|
| Manufactured | 1975–1993[source] | 1965–1991[source] |
|---|
| Introduction date | 1986[source] | 3 June 1965[source] |
|---|
| First flight | September 1969[source] | 4 May 1963[source] |
|---|
| Developed from | Antonov An-14[source] | — |
|---|
| Variant | PZL M28 Skytruck[source] | — |
|---|
| Developed into | Antonov An-38[source] | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | 17 passengers or 1,750 kg (3,860 lb)[source] | 8–14 passengers[source] |
|---|
| Aspect ratio | 12.3[source] | 6.4:1[source] |
|---|
| Airfoil | TsAGI R-II-14 (14% thickness)[source] | — |
|---|
| Fuel capacity | 1,960 L (430 imp gal; 520 US gal)[source] | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
|---|
| Propellers | 3-bladed AW-24AN, 2.80 m (9 ft 2 in) diameter[source] | — |
|---|
| Never exceed speed | 390 km/h (240 mph, 210 kn)[source] | — |
|---|
| g limits | +3[source] | — |
|---|
| Take-off run to 10.7 m (35 ft) | 410 m (1,350 ft)[source] | — |
|---|
| Landing run from 15 m (50 ft) | 315 m (1,033 ft)[source] | — |
|---|
| Manufacturer | — | Dassault Aviation[source] |
|---|
| Primary users | — | Federal Express (formerly) French Navy United States Coast Guard[source] |
|---|
| Stall speed | — | 152 km/h (94 mph, 82 kn)[source] |
|---|
| National origin | — | France[source] |
|---|