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Boeing E-4 National Airborne Operations Center

Photo by Coil B. Thouanel

In the late 1960s the US Air Force decided that it needed six examples of an AABNCP (Advanced Airborne Command Post) plane with greater endurance than the Boeing EC-135. This was intended to survive the first exchanges of a nuclear war and provide a command facility as well as a communication capability between the national command authority and US strategic forces, both conventional and nuclear. The platform selected was the Model 747-200B version of the civil "jumbo jet". In July 1973 the U. S. A. F. contracted for three E-4As with command and communication equipment stripped from EC-135s and updated by E-Systems. Three entered service in 1974/75 as National Emergency Airborne Command Post with in-flight refueling capability, shielding against nuclear radiation, and enormously comprehensive communication systems. In December 1974 a fourth plane was order as the E-4B with more advanced equipment, and the three E-4As have been upgraded to this standard. 

 

 

TECHNICAL DATA

Description Specifications
Manufacturer: Boeing Length: 231 ft. 4 in. 
Date Deployed: 1974/75 Height: 63 ft. 5 in. 
Model: E-4A Wing Span: 195 ft. 8 in. 
Crew: Eight  Wing Area: 5,500.0 sq. ft. 
Nickname:  Empty Weight: 
Basic Role: Advanced airborne national command post plane.  Max. Weight: 800,000 lb. 
Other Versions: E-4A: initial model, E-4B: upgraded mod. Payload: Up to 86 command and communication personnel on two decks. 
Principal User: U. S. A.

Propulsion

Performance

Power Plant: General Electric F103-GE-100 turbofans.  
Range: Endurance 72 hours with in-flight Refueling.  Horsepower: 52,500-lb thrust. 
Max. Speed: 602 mph.  No. Of Engines: Four 
Ceiling: 45,000 ft.   
Climb Rate:  

 

 

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