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The STOL N-62 was designed at Nihon University under
the leadership of Dr. H. Kimura. Rights to the design were acquired by
the C.Itoh Aircraft Maintenance and Engineering Co. Ltd. In 1966. It is
believed that one example remains in airworthy condition.
JA3255
c/n 0103
Japan
4 seat light aircraft first flown in 1964
Engine: 160hp(119kW) Lycoming O-320-B2B
Length: 23’9"(7.21m)
Height: 8’10"(2.7m)Wingspan: 35’5"(10.8m)
No.built: 3+ Range: 620miles(1000km)
Cruising speed: 124mph(200kmh) Empty weight: 1100lb(500kg)
Maximum take-off weight: 1985lb(900kg) |
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