Boeing E-767

Length
48.5 m
Flat Wing Span
47.6 m
Height
15.8 m
Cruise Speed
851 km/h
Max Mach
0.86 Mach
Max Ceiling
12200 m
Number of Engines
2
Aircraft Engine
First Flight
1994-10-04
Entry Into service
2000-05-10
Number Built
4
Maximum Take-Off Weight
175 t (paragliders: kg)
Maximum Range
10370 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Boeing E-767 175 10370

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Boeing KC-767 General Electric CF6 48.5 47.6 200 Compare
Boeing KC-46 Pegasus Pratt & Whitney PW4000 50.5 48.1 54 Compare
Airbus A310 MRTT 47.4 43.9 214 Compare
Airbus A310 Pratt & Whitney PW4000 46.66 43.9 243 Compare
767-200 Pratt & Whitney PW4000 54.94 47.57 Compare
Airbus CC-150 Polaris 46.66 43.9 194 Compare
All data (24 fields)
Name
Boeing E-767
Manufacturer
Boeing
Description
The Boeing E-767 is an Airborne Warning and Control System (AWACS) aircraft that was designed in response to the Japan Air Self-Defense Force's requirements.
ICAO Code
E767
First Flight
1994-10-04
Entry Into service
2000-05-10
Designer
Boeing
Type
Airborne Warning and Control System (AWACS)
Length (m)
48.5
Height (m)
15.8
Cockpit Crew
2
Cruise Speed (km/h)
851
Max Ceiling (m)
12200
Max Mach (Mach)
0.86
National Origin
United States of America
Number Built
4
Powerplant Description
2 × General Electric CF6-80C2 turbofan, 273.6 kN thrust each
Primary Users
Japan Air Self-Defense Force
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Boeing_E-767
Flat Wing Span (m)
47.6
Wake Category
H
Aircraft Engine
General Electric CF6
Number of Engines
2