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Diecast Aircraft Information  Diecast Aircraft Information MetalWings Diecast Aircraft Reference by Dauntless Aviation
Hobby Master 1/72 Air Power Series
HA1997
McDonnell Douglas F-4J Phantom
155890, VMFA-212, USMC, circa 1970s


True 1/72 scale
Professionally painted
Great attention to detail
All markings are Tampoed (pad applied)
Option to display the model on a stand that is provided
Model can be shown with the landing gear in the down or
up positions
Loads of optional armament has been provided
Canopy can be displayed open or closed
Extremely heavy metal with a minimum of plastic
Highly collectable
The F-4D was an improved “C” variant with most improvements being internal electronics
and avionics. The F-4D entered operational service in April 1966 and joined the combat
forces in Southeast Asia in May 1967. With the arrival of the “D” most of the “C” variant
were reassigned to ground attack with the “D”s taking on the air-to-air interceptor role. In
1968 – 1969 a total of 825 “D” models were produced 793 for the USAF and 32 for the
Iranian Air Force.


McDonnell Douglas F-4J Bu.No 155890 served with VF-143 “Pukin’ Dogs” as NK-114 in
1969 into 1970 before transferring to VF-21 “Freelancers” as NE-106 later that year. In
1977 155890 went to VMFA-212 “Lancers” as WD-10. In early 1965 and again in 1972
VMFA-212 deployed to Vietnam returning to Hawaii both times. From 1974 until 1987
operated from Japan before retiring their F-4s for the new F/A-18C “Hornet”. In 1985
155890 moved to VMFA-251 “Thunderbolts” DW-05 but in 1987 it was retired and
displayed at the Estrella Warbirds in California as VMFA-333 “Shamrocks”.

Type – Fighter

Entered Operational Service - April 1966

Crew - 2

Dimensions
Length - 62 ft. 10 in. (18.9 m)
Height - 16 ft. 6 in. (5.03 m)
Wingspan - 38 ft. 5 in. (11.71 m)
Wing area - 530 sq ft.  (49.23 sq m)

Weights
Empty Weight - 28,276 lbs  (12,823 kg)
Gross Weight - 50,341 lbs  (22,830 kg)
Max Weight - 58,000 lbs  (26,303 kg)

Powerplant
Engines - 2 X General Electric J79-GE-17 turbojets
Thrust
Dry - 11,870 lb. st
With Afterburners - 17,900 lb. st

Fuel load
Total - 3,230 US gallons  (12,226 l)
Maximum internal
Internal fuselage tanks - 1,260 gallons  (4,769 l)
Internal wing tanks - 630 gallons  (2,384 l)
Maximum external
600 US gallon (2,271 l) centerline tank
+
2 - 370 US gallon (1,400 l) tanks under each wing on the outer pylons.


Performance
Range - 1375 mi (2,214 km)
Cruise Speed - 587 mph (945 kph) (510.81 kt)
Max Speed
@ 42,000 ft - 1,432 mph (2,304.5 kph) (12,801 m) (Mach 2.17)
@ Sea Level - 826 mph (1,329.3 kph) (Mach 1.08)
Landing speed - 165 mph (265.5 kph)
Initial rate of climb - 40,100 fpm (12,222.5 m/min)
Maximum rate of climb - 48,300 fpm (14,721.1 m/min)
Ceiling - 59,400 ft (18,104 m)
Combat range - 502 miles (807.9 km)
Maximum range - 1,844 miles (2,967.6 km) with maximum external fuel.

Armament
(4) Aim-7D or (4) Aim-7E Sparrow missiles semi-recessed on slots in the fuselage belly
+ up to (4) Aim-9 Sidewinder missiles on the inboard pylons or up to (18) x 750 lb
(340 kg) bombs for a maximum offensive load of 16,000 lbs (7,257.48 kg)
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