FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
HS.125 Series 600 · Length
Single source50 ft 6 in (15.39 m)[source]
Falcon 20F · Length
Configuration
| Specification | British Aerospace 125 | Dassault Falcon 20 |
|---|---|---|
| Type | Mid-size business jet[source] | Business jet[source] |
| Manufacturer | de Havilland (design) Hawker Siddeley (to 1977) British Aerospace (1977–1993) Raytheon (1993–2007) Hawker Beechcraft (2007–2013)[source] | Dassault Aviation[source] |
| Status | Active service[source] | Out of production, in active service[source] |
| Primary users | Japan Air Self-Defense Force Brazilian Air Force[source] |
17.15 m (56 ft 3 in)[source]
Empty; HS.125 Series 600 · Empty weight
Single sourceMaximum take-off; HS.125 Series 600 · Max takeoff weight
Single source12,530 lb (5,684 kg)[source]
25,000 lb (11,340 kg)[source]
Empty; Falcon 20F · Empty weight
Single sourceMaximum take-off; Falcon 20F · Max takeoff weight
Single sourceCruise; HS.125 Series 600 · maximum cruise at 28,000 ft (8,500 m)
Single sourceMach 0.78[source]
454 kn (522 mph, 841 km/h) maximum cruise at 28,000 ft (8,500 m)[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]
HS.125 Series 600 · 1,000 lb (454 kg) payload, 45 minutes reserve plus allowances for take-off and landing
Single source1,650 nmi (1,900 mi, 3,060 km) 1,000 lb (454 kg) payload, 45 minutes reserve plus allowances for take-off and landing[source]
Falcon 20F · Range
Single source3,350 km (2,080 mi, 1,810 nmi)[source]
HS.125 Series 600 · 2 × Rolls-Royce Viper 601-22 turbojet engines thrust each
Single source2 × Rolls-Royce Viper 601-22 turbojet engines, 3,750 lbf (16.7 kN) thrust 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]
HS.125 Series 600 · 4,900 ft/min (
Single source4,900 ft/min (25 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Federal Express (formerly) French Navy United States Coast Guard[source] |
| Number built | 1,720[source] | 512[source] |
|---|
| Manufactured | 1963–2013[source] | 1965–1991[source] |
|---|
| First flight | 13 August 1962[source] | 4 May 1963[source] |
|---|
| Variant | Hawker 800[source] | — |
|---|
| Capacity | 8 passengers (normal layout), 14 passengers in high density layout[source] | 8–14 passengers[source] |
|---|
| Fuel capacity | 1,181 imp gal (1,418 US gal; 5,369 L) usable fuel[source] | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
|---|
| Aspect ratio | 6.25:1[source] | 6.4:1[source] |
|---|
| Stall speed | 83 kn (96 mph, 154 km/h) EAS flaps down[source] | 152 km/h (94 mph, 82 kn)[source] |
|---|
| Never exceed speed | 475 kn (547 mph, 880 km/h) IAS[source] | — |
|---|
| Take-off run | 4,400 ft (1,300 m)[source] | — |
|---|
| Take-off balanced field length | 5,350 ft (1,630 m)[source] | — |
|---|
| Landing run | 3,400 ft (1,000 m) -600A at typical landing weight[source] | — |
|---|
| Landing distance from 50 ft (15 m) | 2,130 ft (650 m) at typical landing weight[source] | — |
|---|
| Country of origin | United Kingdom[source] | — |
|---|
| Introduction date | — | 3 June 1965[source] |
|---|
| Developed into | — | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| National origin | — | France[source] |
|---|