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  2. Center of gravity of an aircraft - Wikipedia

    en.wikipedia.org/wiki/Center_of_gravity_of_an...

    The center of gravity (CG) of an aircraft is the point over which the aircraft would balance. [ 1] Its position is calculated after supporting the aircraft on at least two sets of weighing scales or load cells and noting the weight shown on each set of scales or load cells. The center of gravity affects the stability of the aircraft.

  3. ATA 100 - Wikipedia

    en.wikipedia.org/wiki/ATA_100

    ATA 100. ATA 100 contains the reference to the ATA numbering system which is a common referencing standard for commercial aircraft documentation. This commonality permits greater ease of learning and understanding for pilots, aircraft maintenance technicians, and engineers alike. The standard numbering system was published by the Air Transport ...

  4. CubCrafters CC19 XCub - Wikipedia

    en.wikipedia.org/wiki/CubCrafters_CC19_XCub

    In production (2016) Number built. 20 (July 2016) Developed from. CubCrafters Carbon Cub EX. The CubCrafters CC19 XCub is an American light aircraft, designed and produced by Cub Crafters of Yakima, Washington, introduced in June 2016. The aircraft is supplied complete and ready-to-fly. [ 1][ 2]

  5. Manufacturer's empty weight - Wikipedia

    en.wikipedia.org/wiki/Manufacturer's_empty_weight

    Manufacturer's empty weight. In aviation, manufacturer's empty weight (MEW) (also known as manufacturer's weight empty (MWE)) is the weight of the aircraft "as built" and includes the weight of the structure, power plant, furnishings, installations, systems, and other equipment that are considered an integral part of an aircraft before ...

  6. Load factor (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Load_factor_(aeronautics)

    Load factor (aeronautics) In aeronautics, the load factor is the ratio of the lift of an aircraft to its weight [ 1][ 2]: § 5.22 and represents a global measure of the stress ("load") to which the structure of the aircraft is subjected: where. is the weight. Since the load factor is the ratio of two forces, it is dimensionless.

  7. Aircraft design process - Wikipedia

    en.wikipedia.org/wiki/Aircraft_design_process

    The aircraft design process is a loosely defined method used to balance many competing and demanding requirements to produce an aircraft that is strong, lightweight, economical and can carry an adequate payload while being sufficiently reliable to safely fly for the design life of the aircraft. Similar to, but more exacting than, the usual ...

  8. Aircraft gross weight - Wikipedia

    en.wikipedia.org/wiki/Aircraft_gross_weight

    The aircraft gross weight (also known as the all-up weight and abbreviated AUW) is the total aircraft weight at any moment during the flight or ground operation. [1] [2] [3] An aircraft's gross weight will decrease during a flight due to fuel and oil consumption. An aircraft's gross weight may also vary during a flight due to payload dropping ...

  9. SAWE - Wikipedia

    en.wikipedia.org/wiki/SAWE

    The SAWE. The Society of Allied Weight Engineers is an international organization whose primary purpose is to promote the recognition of “Mass Properties Engineering” as a specialized branch of engineering. The Society is organized into 22 chapters with members from across the United States, Brazil, Europe, United Kingdom, and Canada.

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