Specifications
Year: 1975
Status: Active, In-Service
Manufacturer(s): Boeing - USA
Production: 4
Capabilities:
Status: Active, In-Service
Manufacturer(s): Boeing - USA
Production: 4
Capabilities:
Crew: 4
Length: 231.30 ft (70.5 m)
Width: 195.87 ft (59.7 m)
Height: 63.32 ft (19.3 m)
Weight (Empty): 418,878 lb (190,000 kg)
Weight (MTOW): 826,403 lb (374,850 kg)
Length: 231.30 ft (70.5 m)
Width: 195.87 ft (59.7 m)
Height: 63.32 ft (19.3 m)
Weight (Empty): 418,878 lb (190,000 kg)
Weight (MTOW): 826,403 lb (374,850 kg)
Power: 4 x General Electric CF6-50E2 turbofan engines developing 52,500 lb of thrust each.
Speed: 603 mph (970 kph; 524 kts)
Ceiling: 45,932 feet (14,000 m; 8.7 miles)
Range: 7,140 miles (11,490 km; 6,204 nm)
Ceiling: 45,932 feet (14,000 m; 8.7 miles)
Range: 7,140 miles (11,490 km; 6,204 nm)
Operators: United States
The fleet were born through a 1973 USAF initiative which originally called for two aircraft and these were designated as "E-4A" while being powered by 4 x Pratt & Whitney JT9D engines. By the end of 1975, a third aircraft was added to the group and this new entry was powered by 4 x General Electric GE F103 (CF6) engines instead. The "E-4B" variant was a "one-off" conversion aircraft with additional equipment (including a noticeable dorsal spine bulge) and this entry joined the fleet during December of 1979. In 1985, the original three aircraft were revised to the B-model operating standard and the CF6 engine was selected to power them all. A modernization of the entire fleet was had in 2005 during the post-9/11 period and the start of the global 'War on Terror'.
Externally the aircraft retains much of the form of the Boeing 747 airliner complete with its two-story front fuselage section, four-engined (underwing, nacelled) layout, and a single tail fin aft. A series of antenna protrude from the spine of the fuselage which gives away the many systems and sensors the aircraft carries. Internally, the aircraft is arranged as a series of compartments which are used to accomplish various tasks in the event of a national emergency. While the standard operating crew is four (including two pilots), the fuselage can situate up to 112 personnel and specialists to cover the critical functions of the USAF and government during a national emergency. The aircraft is fully-equipped with advanced systems as well as countermeasures and other protective means (including EMP resistance and nuclear shielding). Additionally, an in-flight refueling capability can be used to extend the range of the E-4 command post considerably over the previous EC-135J platforms they replaced.
At least one E-4 is held "on-call" at any given time by the USAF/U.S. government and regularly deploys with the President of the United States when overseas trips are had. When the President is aboard the E-4 himself, the aircraft uses the callsign of "Air Force One".
The Northrop Grumman E-10 MC2A, built upon the framework of the Boeing Model 767-400ER, was intended as the direct successor to the E-4 but the project was cancelled in 2007.
Program Updates
December 2019 - The United States Air Force has officially launched a successor project for its E-4B fleet. The service requests that the replacement product, which will include the Survivable Airborne Operations Center (SAOC) weapons system, be based in an existing commercial airliner product. It can be assumed that this new aircraft will sport a wide array of the latest USAF active/passive countermeasures technology as well as missile-killing solutions (possibly by way of air-launched drones).
Armament
None.
Cockpit Picture
Variants / Models
• E-4A - Initial Production Models; three examples produced; later brought to E-4B standard.
• E-4B - Fitted with CF6-50E2 engines of 52,500lb thrust each; EMP protection; special shielding from thermal and nuclear sources; additional specialized equipment.
