XTC Amphibious part 103 legal ultralight aircraft, by Diehl Aeronautics, Ultralight Aircraft Magazine.
XTC Amphibious Ultralight.
Ultralight Aircraft Magazine - Diehl XTC hydro light is an amphibious ultralight aircraft. It uses a twin cylinder 24 horsepower KFM engine in a pusher configuration for power. It uses a canard and has twin tail rudders, and spoilerons on the wings.The pilot sits in the middle of the craft, with a small windshield. All three wheels retract and the nosewheel is steerable. The craft is very pitch sensitive and the 24 hp engine is not enough power for this weight and design of craft.
XTC Amphibious
It has a retractable tricycle landing gear, with a steerable nose wheel. The Diehl AeroNautical XTC has suspension on all three wheels and main wheel brakes.The Diehl AeroNautical XTC was reported to have been stress tested to, + 8G's and -8 G's.
XTC Ultralight Aircraft Specifications And Images
XTC Amphibious Single Seat Ultralight Aircraft
Wingspan: 32 ft (9.8 m)
Wing area: 155 sq ft (14.4 m2)
Empty weight: 247 lb (112 kg)
Gross weight: 500 lb (227 kg)
Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
Powerplant: 1 × KFM 107 twin-cylinder, two-stroke, single ignition, horizontally opposed aircraft engine, 25 hp (19 kW)
Performance
Maximum speed: 62 mph (100 km/h; 54 kn)
Cruise speed: 50 mph (43 kn; 80 km/h)
Stall speed: 25 mph (22 kn; 40 km/h)
Range: 120 mi (104 nmi; 193 km)
G limits: +8/-8
Maximum glide ratio: 14:1
Rate of climb: 600 ft/min (3.0 m/s)
The XTC was one of a number of "canard" (tail-first) designs that came out at the height of the ultralight boom of the early 1980's
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