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  McDonnell-Douglas F-4C "Phantom II"    
     
   
   
 
SPECIFICATIONS            Serial # :  63-7485
Wingspan:  38 ft. Cost:  $1,900,000
Length:  58 ft. 2 in. Max. Speed:  1,400 mph
Height:  16 ft. 6 in. Range:  1,750 miles
Weight:  58,000 lbs. loaded Service Ceiling:  59,600 ft.
Engines:  (2) General Electric J79-GE-15s of 17,000 lbs. thrust each w/afterburner Cruising Speed:  590 mph
Armament:  Up to 16,000 lbs. of nuclear or conventional ombs, rockets, missiles, cannon pods
 
 
 
 
 
     
     
 

First flown in May 1958, the Phantom II originally was developed for U.S. Navy fleet defense and entered service in 1961. The USAF evaluated it for close air support, interdiction and counter-air operations and, in 1962, approved a USAF version. The USAF's Phantom II, designated the F-4C, made its first flight on May 27, 1963. Production deliveries began in November 1963. In its air-to-ground role the F-4 could carry twice the normal bomb load of a WWII B-17. USAF F-4s also flew reconnaissance and "Wild Weasel" anti-aircraft missile suppression missions. Phantom II production ended in 1979 after more than 5,000 had been built- more than 2,600 for the USAF.

Warner Robins Air Logistics Center managed the communications, fire control, air-to-air missiles, gun and electronic warfare systems for all the USAF F-4s. The F-4C on display was delivered to the USAF and the 12th Tactical Fighter Wing at MacDill AFB, FL in May 1964. In April 1966 it deployed with the 12th to Cam Rahn Bay AB, Vietnam, until December 1969 when it returned to the United States. It continued to serve with various stateside units until it's retirement from the 163rd Tactical Fighter Group (ANG), March AFB, CA in May 1967 and flown here to Robins AFB for display.