Hobby Master 1/72 Air Power Series
McDonnell CF-101 Voodoo 409 Squadron "101057"
Hawk One Canada, Canadian Armed Forces,
May 1984
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.

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.

The first Hawk One CF-101 Voodoo came about in 1977 when the 409 Squadron from CFB
Comox, British Columbia was to receive its standard. A Voodoo was to be sent to Ottawa (the
Canada’s capitol) to pick it up so a special paint scheme using the squadrons colors and emblem
was applied to CF-101 101012. The aircraft was named “Hawk One Canada”. In 1984 the 409
Squadron wanted to mark the 60th anniversary of the RCAF/CAF so “Hawk One Canada” paint
scheme was applied to Voodoo 101057. Today CF-101 101057 “Hawk One Canada” can be
seen as the gate guard for 19 Wing at CFB Comox.

Specifications for the McDonnell F-101B Voodoo
Role – two-seat all-weather interceptor
Crew – 2
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)
Empty - 28,495 lb   (12,925 kg)
Loaded - 45,665 lb   (20,715 kg)
Maximum Take Off - 52,400 lb   (23,770 kg)
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)
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)
Missiles – 4 X AIM-4 Falcon
2 X AIM-4 Falcon and 2 X AIR-2 Genie nuclear rockets
Avionics - Hughes MG-13 fire control system
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