FP 303

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Pterodactyl Ascender Part 103 Ultralight Aircraft

Copy 1

Power options as an ultralight include the 32 HP Kawasaki 340, and the Hirth 28 HP, F 33. 

Heading ultralight.

Pterodactyl Ascender Part 103 Ultralight Aircraft

Copy 2

Heading Specifications

Empty weight:
235 lbs (107 kg)
MTOW:
550 lbs (249 kg)
Stall speed:
23 kts (26 mph) (43 kph)
Cruise speed:
48 kts (55 mph) (89 kph)
VNE:
65 kts (75 mph) (120 kph)


Climb:
1000 ft/min (5.1 m/s)
Glide ratio:
9 to 1
Take-off distance:
300 ft (91 m)
Landing distance:
300 ft (91 m)
Engine:
28-50 hp Hirth
Fuel consumption:
2-4.5 GPH (7.6 LPH)

Heading - Contact Information

Phone

+1 386-738-4444
+1 740-407-4491

Website
http://www.uflyit.com/
sportplane@uflyit.com 

FAR Part 103 ultralight aircraft definition.

Single place Part 103 ultralights in the United States are defined as single place ultralight aircraft that weigh 254 lbs or less, have a stall speed not more than 24 knots, a top speed of 55 knots, and carry no more than 5 gallons of fuel. To fly a legal Part 103 ultralight aircraft in the United States the pilot does not require a pilot license. 

Single place aircraft weighing more than 254 lbs. in the U.S. require a pilots license and must be built as experimental, amateur built, homebuilt aircraft. These include weight shift aircraft, more commonly known as trikes, powered parachutes, and powered para-gliders.