Ads
related to: ultralight aircraft requirements for flyingsmartholidayshopping.com has been visited by 1M+ users in the past month
Search results
Results From The WOW.Com Content Network
Regulation of ultralight aircraft in the United States is covered by the Code of Federal Regulations, Title 14 (Federal Aviation Regulations), Part 103, or 14 CFR Part 103, which defines an "ultralight" as a vehicle that: has only one seat [1] [2] Is used only for recreational or sport flying [1] [2]
Huntair Pathfinder Mark 1 ultralight. Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailerons, elevator and rudder, calling the former "microlight" and the latter "ultralight".
The aircraft was first flown before the US FAR 103 Ultralight Vehicles rules were introduced and the early versions of the Goldwing did not meet the category's maximum empty weight of 254 lb (115 kg) or its maximum speed requirement of 63 mph (101 km/h). Later models were made lighter and slower to fit FAR 103.
(Age requirements for gliders and balloons are slightly lower.) This includes 100 hours in powered aircraft, 50 hours in airplanes, and 100 hours as pilot in command (of which 50 hours must be cross-country flight time). In addition, commercial pilots must hold an instrument rating, or otherwise they would be restricted to flying for hire only ...
It was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. The company name was later changed to Fisher Flying Products and production continued under that company name until the FP-101 was supplanted in production by the Fisher FP-202 Koala. [1]
The Avenger was designed to meet the requirements of the United States FAR 103 Ultralight Vehicles regulations, including the maximum 254 lb (115 kg) empty weight. Design goals included low cost, an attractive appearance, and accommodation for a 76 in (193 cm) tall, 240 lb (109 kg) pilot.
Designed to meet FAR 103 Ultralight Vehicles standards, the N3 Pup can accept various lightweight four stroke engines of between 37 and 60 hp (28 and 45 kW). If built to specifications with minimal additions, it can meet the requirements for a FAR 103 ultralight aircraft, with an empty weight of 254 lb (115 kg).
The Aero-Works Aerolite 103 is an American single seat, high-wing, pusher configuration ultralight aircraft, designed by Terry Raber and introduced by Aero-Works, Inc, of Millersburg, Ohio, in 1997. The aircraft's model number indicates that it was designed to comply with the Federal Aviation Administration FAR 103 ultralight rules. [1] [4] [5 ...