Hobby Master 1-72 Air Power
HA19045 McDonnell Douglas F-4J Phantom II
US Blue Angels, 1969
(with decal for No.1 to No.6 airplanes)
The last version of the Phantom II produced for the USN and USMC was the F-4J. Between 1966 and 1972 there were 522 F-4Js built. The USN received their first F-4Js in 1966 and the USMC in 1967. The F-4J had the distinction of scoring the only USMC air-to-air combat victory in Vietnam and it also was the last US operational aircraft in South East Asia. In mid 1970 the F-4 Phantom II was being replaced by the new and improved F-14 Tomcat.
In 1969 the Blue Angels re-equipped with the McDonnell Douglas two-seat F-4J Phantom II. The first F-4Js for the Blue Angels arrived on December 23, 1968. This was the first time they had used a two-seater and the first time both the Blue Angels and the USAF Thunderbirds flew the same equipment. The F-4 allowed the team to add more maneuvers to their routine increasing it to 22 minutes. The aircraft had lead ballast in the nose to compensate for the lack of the AWG-10 radar. The team operated their F-4Js until 1974.
Specification for the F-4J
Engines: 2 X General Electric J79-GE-8B/8C/10 turbojets, 11,870 lb.s.t dry,
17,900 lb.s.t. with afterburner.
Maximum speed 1,584 mph at 48,000 ft. (Mach 2.4), 875 mph at sea level (Mach 1.15).
Initial climb rate: 41,250 fpm.
Service ceiling: 70,000 ft. Combat ceiling: 54,700 ft.
Combat range: 596 miles, maximum range 1,956 miles with maximum external fuel.
30,770 lbs empty.
46,833 lbs gross.
41,399 lbs combat weight,
Wingspan: 38 ft. 5 in.
Wing area: 530 square ft.
Length: 58 ft. 3.75 in.
Height: 16 ft. 3 in.
Maximum internal fuel: in fuselage tanks 1,347 US gal.
Internal wing tanks: 630 gal.
Maximum external fuel: 3,317 US gal.
600 US gal in a centerline tank, 370 US gal in each of two tanks that could be
carried underneath the outer under wing pylons.
4 X AIM-7 Sparrow semi-active radar homing air-to-air missiles in semi-
recessed slots in the fuselage belly.
2 X to 4 AIM-9 Sidewinder infra-red homing air-to-air missiles carried under
the wings on the inboard pylons.
Maximum offensive load of up to 16,000 lbs carried on the centerline and 4
under wing hard points.