Built
by North American Aviation, radar guided, rocket armed, all-weather
fighter-interceptor. Originally designated the F-86D, the aircraft
underwent modifications to upgrade the original radar/fire control
systems to provide 'data-link' capability between the aircraft and
ground controllers, eliminating the use of vocal instructions during
intercept missions. New wing slats and an increase in wing span of
2 feet improved performance of the -L over the -D.
The
XF86 made it's first test flight on Oct 1, 1947. The first production
model F86A was test flown in May 1948 and the Air Force received the
Sabre jet on August 16, 1948. In September 1948, the F86A set a world
record of 570 miles per hour.
In
the fall of 1950, the Communist forces in Korea introduced the Soviet
made swept wing MiG15 FAGOT jet fighter. To meet this threat, the
USAF rushed the F86A to Korea since the MiG's out flew straight wing
jets. The F86 was well suited for its mission with a shoot down record
of 15 to 1 over the MiG's. The MiG 15 was faster than the F86A and
the newer E models above 32,000 feet in level flight; it had a tighter
turning radius, and could climb faster. However, the F86 bested the
MiG15 primarily due to its electronic gun sight, better armament and
superior pilot skill.
From
the beginning, the USAF accepted 6,353 F86's (all models included.)
5,893 of them for its own use and 460 ordered into production for
allies. A breakdown of the USAF F86 total showed 3 experimental and
prototype F86A's, 554 F86A's, 393 F86E's, 1,959 F86F's, 2 F-86H's,
473 F86H's, 2 YF86D's and 2,540 F86D's (all F86L's being converted
F86D's.)
On
April 15, 1950, the 1st Fighter Wing was re-designated the 1st Fighter
Interceptor Wing, a more appropriate designator. The Wing was relieved
from assignment to Strategic Air Command and assigned to the Continental
Air Command for air defense purposes on July 1, 1950. There after
Perrin Air Force Base became a part of the Aerospace Defense Command
with almost 100 F86's assigned at Perrin Air Force Base, Denison-Sherman,
Texas.
SPECIFICATIONS:
Crew: One.
Power Plant: one General Electric J47-GE-27, 5,970 lb. thrust turbojet.
Dimensions: Span: 39 ft 1 in., Length: 41 ft., Height: 14 ft.
Weight: Max 16,500 lbs.
Performance: Max. Speed: 670 mph., Service ceiling: 53,000 ft. Tactical
Radius: 535 miles.
Armament: Twenty-four 2.75 inch unguided rockets carried in an internal
tray in fuselage.