M. Gerard Feugray has designed a number of high
performance aircraft including the single seat Feugray ASA 200 which
participated in the 1986 World Aerobatic Championships. This aircraft
was similar to the Mudry CAP 21 and was powered by a 230hp (171kW)
Lycoming. The single seat Feugray TR.260 was similar to the Stephens
Akro and was powered by a 330hp (246kW) Lycoming and had a maximum
take-off weight of 1874lb (850kg). The TR.200 has been the most
successful Feugray design and partial kits or plans are available from
Tech-Aero of Glisolles, France.
F-PSFG
c/n 05
France
2 seat aerobatic aircraft first flown in 1995
Engine: 200hp(149kW) Lycoming IO-360-A1B6D
Length: 22’4"(6.8m)
Height: 8’6"(2.6m)Wingspan: 24’4"(7.42m)
No.built: 15+ Range: 669miles(1070km)
Cruising speed: 168mph(270kmh) Empty weight: 1130lb(488kg)
Maximum take-off weight: 1918lb(870kg) |