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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.
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 |
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