FORCETALLY
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At a glance
Measured figures
E-767 · Length
Single source159 ft 2 in (48.5 m)[source]
Falcon 20F · Length
Single sourceConfiguration
| Specification | Boeing E-767 | Dassault Falcon 20 |
|---|---|---|
| Type | Airborne Warning and Control System (AWACS)[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Boeing Integrated Defense Systems[source] | Dassault Aviation[source] |
| Status | In service[source] | Out of production, in active service |
17.15 m (56 ft 3 in)[source]
Empty; E-767 · Empty weight
Single sourceGross; E-767 · Gross weight
Single sourceMaximum take-off; E-767 · Max takeoff weight
Single source188,705 lb (85,595 kg)[source]
284,110 lb (128,870 kg)[source]
385,000 lb (175,000 kg)[source]
Empty; Falcon 20F · Empty weight
Single sourceMaximum take-off; Falcon 20F · Max takeoff weight
Single sourceCruise; E-767 · Cruise speed
Single sourceMach 0.86[source]
460 kn (530 mph, 851 km/h)[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]
E-767 · 2 × General Electric CF6-80C2 turbofan thrust each
Single source2 × General Electric CF6-80C2 turbofan , 61,500 lbf (274 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]
E-767 · at 300-nautical mile radius (no aerial refueling capability)
Single sourceE-767 · on station at 1,000 nautical-mile radius
Single source9.25 hours on station at 1,000 nautical-mile radius; 13 hours at 300-nautical mile radius (no aerial refueling capability).[source]
Falcon 20F · Wing area
Single source41.00 m 2 (441.3 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | Japan Air Self-Defense Force[source] | — |
|---|
| Number built | 512[source] |
|---|
| Introduction date | 10 May 2000[source] | 3 June 1965[source] |
|---|
| First flight | 4 October 1994 (without rotodome) 9 August 1996 (with rotodome )[source] | 4 May 1963[source] |
|---|
| Developed from | Boeing 767[source] | — |
|---|
| Primary users | — | Federal Express (formerly) French Navy United States Coast Guard[source] |
|---|
| Manufactured | — | 1965–1991[source] |
|---|
| Developed into | — | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | — | 8–14 passengers[source] |
|---|
| Fuel capacity | — | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
|---|
| Aspect ratio | — | 6.4:1[source] |
|---|
| Stall speed | — | 152 km/h (94 mph, 82 kn)[source] |
|---|