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Diehl AeroNautical XTC Hydrolight
The Diehl AeroNautical XTC Hydrolight is an American amphibious flying boat ultralight aircraft that was designed and produced by Diehl AeroNautical in the 1980s.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-46. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕
==Design and development==
The XTC was the first amphibious flying boat to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . It features a cantilever mid-wing, a canard, dual vertical tails, a single-seat, open cockpit, re-positionable tricycle landing gear and a single engine in pusher configuration.〔
The aircraft's hull is made from fiberglass, while the wing has a Kevlar-epoxy spar with its flying surfaces covered in bonded Mylar. Its span wing is located behind the cockpit. Some aircraft were delivered with optional enclosed cockpits for all-weather flying. The landing gear repositions clear of the hull for water landings and is sprung on all three wheels. The nose wheel is steerable. The control system is three-axis, with the canard for pitch, twin rudders for yaw and spoilers for roll control. The XTC is very aerodynamically clean and produces a 14:1 glide ratio. Strongly built, the aircraft is rated for +8/-8g.〔
The standard engine supplied was the twin-cylinder, two-stroke, single ignition, horizontally opposed KFM 107 aircraft engine of .〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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