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The aircraft was originally designed as a homebuilt aircraft, but was later lightened and adapted to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). In its ultralight version the aircraft has a standard empty weight of 250 lb (113 kg) when equipped with a lightweight engine ...
The flight test phase accomplishes two major tasks: 1) finding and fixing aircraft design problems and then 2) verifying and documenting the vehicle capabilities when the vehicle design is complete, or to provide a final specification for government certification or customer acceptance. The flight test phase can range from the test of a single ...
The Rotec Rally is a family of American ultralight aircraft that was designed by Bill Adaska in 1977 and produced by Rotec Engineering of Duncanville, Texas. Adaska had been an aeronautical engineer at Bell Helicopter and the French helicopter manufacturer, Aerospatiale, prior to starting Rotec. The aircraft was supplied as a kit for amateur ...
These environments include, but are not limited to: science platform aircraft and aircraft-deployable systems; space vehicles, space stations, habitats and lunar and planetary surface construction bases; and Earth-based control, experiment, launch, logistics, payload, simulation and test facilities. Earth analogs to space applications may ...
For instance, the aircraft described by the black altitude envelope on the right can fly at altitudes up to about 52,000 feet (16,000 m), at which point the thinner air means it can no longer climb. The aircraft can also fly at up to Mach 1.1 at sea level, but no faster. This outer surface of the curve represents the zero-extra-power condition ...
Up until 1998, Type I and Type II aircraft maintenance engineer (AME) licences were distinguished. In 1998 ICAO replaced these with a single AME licence. [1] In 2005 the relationship between the Canadian AME and the US A&P (AMT) was further revised, through a Bilateral Aviation Safety Agreement (BASA) between the US and Canada. [2]
Joints are designed to be stronger than the members. After the structure has been completed, the aircraft is covered in aircraft fabric (usually aircraft-grade polyester). The advantage of this type of construction is that it does not require complex tools and equipment, instead employing commonplace items such as saw, planer, file, sandpaper ...
ANSP 2: Authorization of Aircraft Network Security Program ANT Antenna (radio) ANSOG Airport Network Security Operator Guidance A/O Air oil In turbine engines AOA Angle of attack: AOC 1: Air operator's certificate: AOC 2: Aeronautical operational control: AOG Aircraft on ground: AOM 1: Aircraft operations manual AOM 2: Airport/aerodrome ...
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