Hobby Master 1/72 Air Power Series
HA2111
F-100D-25NA (55-3616)  Super Sabre
188th TFG, Arkansas ANG

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

Optional armament has been provided

Canopy displays open or closed

Pilot figure

Extremely heavy metal with a minimum of plastic

Highly collectable
The North American F-100 Super Sabre served the USAF from 1954 to 1971
shortened version of “one hundred” was the first US fighter capable of
attaining supersonic speed in level flight. The Hun was used extensively as
close-air-support in South Vietnam. The F-100 suffered from landing gear and
brake parachute failures, electrical problems, 500 of the 1,274 F- 100Ds that
were built were lost mostly due to these failures.

Prior to belonging to the 188th TFG of the Arkansas ANG aircraft 55-3616 c/n 223-298
was the property of the 20th TFW/ 77th TFS that had been stationed at RAF
Wethersfield. In 1969 the 77th and 20th moved to RAF Upper Heyford and transitioned to
the F-111. Prior to receiving the F-100D in 1972 the 188th was designated 188th TRG
(Tactical Reconnaissance Group) but with the “Huns” came the new designation 188th
TFG “Flying Razorbacks”. They flew the F-100D until 1979 when they transitioned to the
F-4C.


Specifications North American Aviation (F-100D)

General characteristics
Crew: 1

Dimensions
Length: 50 ft (15.2 m)
Wingspan: 38 ft 9 in  (11.81 m)
Height: 16 ft 2¾ in (4.95 m)
Wing area: 400 ft² (37 m²)

Weights
Empty weight: 21,000 lb (9,500 kg)
Loaded weight: 28,847 lb (13,085 kg)
Maximum take-off weight: 34,832 lb (15,800 kg)

Engine Performance
Powerplant: 1× Pratt & Whitney J57-P-21/21A turbojet
Dry thrust: 10,200 lbf (45 kN)
Thrust with afterburner: 16,000 lbf (71 kN)
Zero-lift drag coefficient:: 0.0130
Drag area: 5.0 ft² (0.46 m²)
Aspect ratio: 3.76

Performance
Maximum speed: 750 kn (864 mph, 1,390 km/h)
Range: 1,733 NM (1,995 mi, 3,210 km)
Service ceiling: 50,000 ft (15,000 m)
Rate of climb: 22,400 ft/min (114 m/s)
Wing loading: 72.1 lb/ft² (352 kg/m²)
Thrust/weight: 0.55
Lift-to-drag ratio: 13.9

Armament
Guns: 4× 20 mm (0.787 in)  M39 cannon
Missiles: 4× AIM-9 Sidewinder Missiles or GAM-83 Bullpup Missile
Bombs: 7,040 lb (3,190 kg) of weapons, including
Conventional bombs or
Mk. 7 nuclear bomb or
Mk. 28 nuclear bomb or  
Mk. 38  nuclear bomb or  
Mk. 43 nuclear bomb or
Mk. 57 nuclear bomb or  
Mk. 61 nuclear bomb

Avionics
Minneapolis-Honeywell MB-3 automatic pilot
AN/AJB-1B low-altitude bombing system
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