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Organization Chart
E-3A Component
History
Participating Nations
Emblem
Aircraft
NATO Midterm Upgrade
Mission & Crew
Operations 1990-2012
TCA History
FOBs & FOL
The NATO E-3A Aircraft
E-3A at Day
Dimensions: Aircraft
Wingspan: 44.45 m / 145 ft 9 in
Length: 46.68 m / 152 ft 11 in
Height: 12.70 m / 41 ft 9 in
Rotodome
Diameter: 9.1 m / 30 ft
Thickness: 1.8 m / 6 ft
Height: 3.35 m / 11 ft
Rotation: once every 10 seconds

Radar coverage: One E-3A flying at 30,000 ft / 9,150 m has over 312,000 km² in its field of view.
Three E-3As in overlapping orbits can provide complete coverage of Central Europe.
An E-3A can detect low flying targets within 400 km or 215 nautical miles; and at medium altitude targets within 520 km or 280 nautical miles.

Primary function: Airborne surveillance, command, control and communications.
 

Armament: None.

Power plant: Four TF-33 Pratt & Whitney 100A turbofan engines.

Speed: More than 800 km / 500 miles per hour

Operational altitude: Above 9,150 m / 30,000 ft

Maximum take-off weight:  147,429 kg / 325,000 lbs

Fuel capacity: 89,610 liters / 70,371 kg
22,768 gallons / 148,000 lbs

Endurance: More than 10 hours (unrefueled). All air-refuelable.

Aircrew: Flight crew
2 pilots
1 navigator
1 flight engineer
Mission crew
1 tactical director
1 fighter allocator
2 weapons controllers
1 surveillance controller
3 surveillance operators
1 passive controller
1 communications technician
1 radar technician
1 system technician

Total number can vary for a specific mission.

Prime contractor: Boeing Aerospace Co., Seattle, Washington, United States.