Credit
航空自衛隊 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
KC-767 · Length
Single source159 ft 2 in (48.5 m)[source]
Falcon 20F · Length
Single sourceConfiguration
| Specification | Boeing KC-767 | Dassault Falcon 20 |
|---|---|---|
| Type | Tanker / transport[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; KC-767 · Empty weight
Single sourceMaximum take-off; KC-767 · Max takeoff weight
Single source181,610 lb (82,377 kg)[source]
395,000 lb (186,880 kg)[source]
Empty; Falcon 20F · Empty weight
Single sourceMaximum take-off; Falcon 20F · Max takeoff weight
Single sourceCruise; KC-767 · Mach 0.80
Single sourceMaximum; KC-767 · Mach 0.86
Single source570 mph (915 km/h, 500 kn) Mach 0.86[source]
530 mph (851 km/h, 460 kn) Mach 0.80[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 sourceFalcon 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 users | Italian Air Force Japan Air Self-Defense Force Colombian Aerospace Force[source] | Federal Express (formerly) French Navy United States Coast Guard[source] |
|---|
| Number built | 9 (8 originally built, 1 converted)[source] | 512[source] |
|---|
| Manufactured | 2003–present[source] | 1965–1991[source] |
|---|
| First flight | 21 May 2005[source] | 4 May 1963[source] |
|---|
| Developed from | Boeing 767[source] | — |
|---|
| Developed into | Boeing KC-46 Pegasus[source] | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | up to 200 passengers or 19 463L pallets[source] | 8–14 passengers[source] |
|---|
| Maximum Fuel Load | 160,660 lb (72,877 kg)[source] | — |
|---|
| Introduction date | — | 3 June 1965[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] |
|---|