
Loading the evidence…
Preparing your view.
Preparing your view.


At a glance
Measured figures
E-767 · Length
Single source159 ft 2 in (48.5 m)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Boeing E-767 | Dassault Falcon 900 |
|---|---|---|
| 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] | Active service, in production |
20.21 m (66 ft 4 in)[source]
E-767 · Height
Single source52 ft 0 in (15.8 m)[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 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceE-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 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]
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 900B · Wing area
Single source49.0 m 2 (527 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 | >500[source] |
|---|
| Introduction date | 10 May 2000[source] | — |
|---|
| First flight | 4 October 1994 (without rotodome) 9 August 1996 (with rotodome )[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Boeing 767[source] | Dassault Falcon 50[source] |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Manufactured | — | 1984–present[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | — | 19 passengers[source] |
|---|
| Fuel capacity | — | 8,690 kg (19,160 lb)[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|