The F-21 superseded the F-19 Sportsman in production
and was basically a higher powered version of the F-19. The F-21A (6
built) first flew in 1983 and had a revised fuel system. In 1986 the
company again changed hands and moved to Lock Haven, Pennsylvania. The
company was then resold to a new owner in 1989 and production was
restarted with the F-21B (15 built) which had an increase in fuel
capacity and a maximum take-off weight of 1750lb(794kg). The F-22
Classic was the name given to a revamped F-21B. Other versions were the
F-22A fitted with a tricycle undercarriage, the F-22B Ranger fitted with
a 180hp(134kW) Lycoming and the F-22C Trooper which was a F-22B with a
tricycle undercarriage. Small numbers of the F-21 and F-22 series remain
airworthy.
C-GJJN
c/n F.1011
USA
2 seat light aircraft first flown in 1980
Engine: 118hp(88kW) Lycoming O-235-C
Length: 22’3"(6.78m)
Height: 6’6"(1.98m)Wingspan: 36’0"(10.97m)
No.built: 22 Range: 400miles(643km)
Cruising speed: 115mph(185kmh) Empty weight: 990lb(449kg)
Maximum take-off weight: 1500lb(681kg) |