F-100 SUPER SABRE
Aircraft at the Joe Davies Heritage Airpark at Palmdale Plant 42
Nicknamed "Hun"
Click for larger photo
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A/C SN
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54-2299
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Construction #
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223-179
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Date Acquired:
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August 1, 1998
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Acquired From:
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USAF George AFB, CA (Loan)
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Displayed:
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October 1, 1998
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History
F-100 recovery crew George AFB, Madison, Murphy, Pinkham, Sinclair & possibly Daniels.
Built at Inglewood, California; left production line on August 27, 1956.
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November 23, 1956
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8th TFW, 80th TFS (Headhunters) Itazuke AB, Japan: The 8th FBW became the 8th TFW
on July 1, 1958 with the wing converting from F-86 to the F-100. During this time
each squadron rotated to Kunsan Air Base, Korea for training missions and occasionally
an operational mission along the demilitarized zone.
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February 20, 1959
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8th TFW, 80th TFS, Osan AB, Korea: Wing transferred to Osan Air Base. Unit on dawn
to dusk alert status.
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December 21, 1959
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4520 CCTW, Nellis AFB, NV: Aircraft used as a Thunderbird during the Far East Tour
in 1959. Thunderbird aircraft were normally the F-100C model, however, these did
not possess aerial refueling capability necessary to cross the Pacific.
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August 11, 1960
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4520 CCTW, Nellis AFB, NV: Aircraft used for combat crew training.
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April 15, 1962
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4520 CCTW, Nellis AFB, NV: Aircraft crashed, but was repairable.
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July 18, 1962
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4520 CCTW, Nellis AFB, NV: Aircraft returned after repairs made.
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September 28, 1962
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4510 CCTW, Luke AFB, AZ: Aircraft transferred to 4510 CCTW; still used for combat
crew training.
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October 14, 1969
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58 TFTW, Luke AFB, AZ: Tactical fighter training wing.
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June 26, 1970
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114 TFG, 175 TFS, Joe Foss ANGB, SD : Transferred to South Dakota Air National Guard.
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July 31, 1970
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180 TFG, 112 TFS, Toldeo Expr. Airport, OH, : Transferred to Ohio Air National Guard.
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September 23, 1970
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114 TFG, 175 TFS, Joe Foss ANGB, SD: Transferred back to South Dakota Air National
Guard.
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1981
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George AFB, CA,: Displayed as gate guard at George AFB.
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October 1999
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Palmdale, CA, Transferred to Joe Davies Heritage Airpark and placed on display,
designated "Spirit of Palmdale".
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General Information
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MANUFACTURER:
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North American Aviation
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PRODUCTION PERIOD:
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1953 to 1959
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NUMBER PRODUCED:
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2,294
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PRODUCTION SERIES:
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USAF: F-100A, C, & D single-seat A/C, F-100F two-seat A/C
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ROLES:
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Originally designed as a land-based fair-weather air superiority fighter for the
US Air Force; later developed into a land-based all-weather multi-mission aircraft
for the US Air Force, capable of close air support, interception and forward air
control
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Performance and Specifications
(Figures given are for the F-100D model)
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MAXIMUM SPEED:
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910 mph (Mach 1.2)
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SERVICE CEILING:
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46,900 feet above sea level
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RANGE:
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1,995 miles
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WEAPONS:
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Four M39 20mm cannons, AIM-4 Falcon, AIM-9 Sidewinder missiles, and a variety of
air to ground rockets and bombs could be carried on the six wing and one fuselage
stations
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CREW:
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Pilot
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LENGTH:
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54 feet, 2 inches
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WINGSPAN:
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38 feet, 9 inches
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HEIGHT:
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16 feet, 2 inches
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MAXIMUM TAKEOFF WEIGHT:
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37,124 lbs.
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POWERPLANT:
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Pratt & Whitney J57-P-21/21A turbojet engine with afterburner providing 16,000 lbs.
of thrust
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ACHIEVEMENTS:
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First operational USAF aircraft to exceed the speed of sound in level flight; operated
by the USAF Thunderbirds and USAF Europe Skyblazers Flight Demonstration teams
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