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F-4B (F4H-1) Phantom II 148390f, VF-74 "Bedevilers", CVA-59 USS Forrestal, US Navy, 1962
General Background
One of the most famous and easily recognized fighter aircraft of the post-WWII era was the McDonnell F-4 Phantom II. This aircraft was developed as a private venture by the aircraft company but was soon ordered by the USN as a carrier-based attack aircraft. Its first flight took place on May 27, 1958 and it entered active service in December 1960. It wasn’t long after the F-4B appeared that a fly-off was set up with USAF front-line fighters. It was no contest, the F-4 performed so well that the USAF ordered their own variant, the F-4C. As time went on, the F-4 evolved into well over a dozen variants.
The Aircraft
VF-74 “Bedevilers” were the first USN squadron to deploy with the F-4 Phantom II. In July 1961 VF-74 traded their Douglas F4D Skyrays for the F4H-1, later to become the F-4B thereby becoming the “First In Phantom”. During the next twenty years VF-74 would fly three variants of the Phantoms 13 times on Mediterranean cruises and twice to SEA. 148390 was the 75th F-4B constructed for the USN and the USMC. The F-4B was eventually upgraded to F-4N standards.
Specifications :
F4H-1 later became the F-4B | |
Number of “B” variant built for USN and USMC: | 649 |
Powerplant : | 2 x General Electric J79-GE-8A/-8B/-8C turbojets, 10,900 lb.s.t. dry, 17,000 lb.s.t. with afterburner |
Performance | |
Max Speed: | @ Sea level - 845 mph |
@ 48,000 ft - 1,485 mph | |
Initial climb rate: | 28,000 fpm |
Service ceiling: | 62,000 ft |
Combat Ceiling: | 56,850 ft |
Combat range | |
Normal: | 400 miles |
Maximum range: | 2,300 miles with maximum fuel load |
Weights | |
Empty: | 28,000 pounds |
Gross: | 44,600 |
Combat: | 38,500 pounds |
Maximum take-off: | 54,600 pounds |
Dimensions | |
Wingspan: | 38 ft 5 in |
Wing area: | 530 sq. ft |
Length: | 58 ft 3.75 in |
Height: | 16 ft 3 in |
Fuel | |
Maximum fuel load: | |
Internal in fuselage: | 1,358 U.S. Gallons |
Internal in wings: | 630 U.S. Gallons |
Total external fuel load: | 1,988 U.S. Gallons |
Maximum external fuel load | |
In center-line tank under the fuselage: | 600 U.S. Gallons |
In 2 x under-wing tanks: | 740 U.S. Gallons |
Combined fuel load: | 3,328 U.S. Gallons |
Armament | 4 x AIM-7D or -7E Sparrow semi-active radar homing missiles in under-fuselage recesses |
Inner under-wing pylons could each accommodate an additional Sparrow or a pair of AIM-9 Sidewinder infrared homing missiles | |
In ground attack mode, could carry up to 16,000 pounds of ordnance on centerline pylon underneath the fuselage and on four under-wing hard-points |