Diecast Aircraft Information

MetalWings Diecast Aircraft Reference by Dauntless Aviation

Hobby Master 1/72 Air Power Series
HA3707
McDonnell F-101B Voodoo
80274, 13th FIS, USAF, 1960s

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.

Optional armament provided.

Canopy can be displayed open or closed.

Pilot figure included.

Extremely heavy metal with a minimum of plastic.

Highly collectable.

The McDonnell F-101 Voodoo (nicknamed One-oh-Wonder") first flew in September 1954
with the first production F-101A making its first operational flight in May 1957. In September
1957 the F-101C became operational followed by the F-101B in January 1959. When
production ended 807 Voodoos had been created, 480 of them were the two-seat all-
weather interceptor F-101Bs. The RF-101 reconnaissance version was the world’s first
supersonic photo-recon aircraft. The only major foreign operator of the Voodoo was the
Royal Canadian Air Force (RCAF) that acquired 56 CF-101B and 10 CF-101F.

McDonnell F-101B 58-0274 entered service on March 31, 1960 assigned to the 15th FIS at
Davis Monthan AFB, Arizona. In June 1964 the aircraft was transferred to the 13th FIS at
Glasgow AFB, Montana. Just prior to the 13th FIS being deactivated on June 30, 1968 58-
0274 was transferred to the 62nd FIS at Sawyer AFB, Michigan June 12, 1968. After six
more transfers 58-0274 was dropped from the USAF inventory in September 1974 and in
1978 went to the Peterson Air and Space Museum at Peterson AFB, Colorado.

Specifications for the McDonnell F-101B Voodoo
Role – two-seat all-weather interceptor
Crew – 2
Dimensions
Length – 67 ft 5 in   (20.55 m)
Wing Span – 39 ft 8 in   (12.09 m)
Wing Area - 368 ft²   (34.20 m²)
Height – 18 ft 0 in   (5.49 m)
Weight
Empty - 28,495 lb   (12,925 kg)
Loaded - 45,665 lb   (20,715 kg)
Maximum Take Off - 52,400 lb   (23,770 kg)
Performance
Powerplant – 2 X Pratt & Whitney J57-P-55 afterburning turbojets
Dry thrust - 11,990 lbf   (53.3 kN) each
Thrust with afterburner - 16,900 lbf   (75.2 kN) each
Internal fuel capacity - 2,053 gal (7,771 liters)
or
With two external tanks - 2,953 gal   (11,178 liters)
Maximum speed - Mach 1.72   (1,134 mph / 1,825 km/h) @ 35,000 ft   (10,500 m)
Range - 1,520 mi   (1,320 nm / 2,450 km)
Service ceiling - 58,400 ft   (17,800 m)
Rate of climb - 49,200 ft/min   (250 m/s)
Armament
Missiles – 4 X AIM-4 Falcon
Or
2 X AIM-4 Falcon and 2 X AIR-2 Genie nuclear rockets
Avionics - Hughes MG-13 fire control system

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