FORCETALLY
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Preparing your view.
At a glance
Measured figures
E-767 · Length
Single source159 ft 2 in (48.5 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Boeing E-767 | Cirrus SR20 |
|---|---|---|
| Type | Airborne Warning and Control System (AWACS)[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Boeing Integrated Defense Systems[source] | Cirrus Aircraft[source] |
| Status | In service[source] | — |
| Primary user |
26 ft 0 in (7.92 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; SR20-G3 · Empty weight
Single sourceGross; SR20-G3 · Gross weight
Single sourceE-767 · Range
Single source5,600 nmi (6,440 mi, 10,370 km)[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[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]
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]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Japan Air Self-Defense Force[source] |
| — |
| Number built | 2,084 (through 2025)[source] |
|---|
| Introduction date | 10 May 2000[source] | — |
|---|
| First flight | 4 October 1994 (without rotodome) 9 August 1996 (with rotodome )[source] | 21 March 1995[source] |
|---|
| Developed from | Boeing 767[source] | — |
|---|
| Manufactured | — | 1999–present[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Capacity | — | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|