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Aviation Supplies & Academics, Inc.
Industry: Aviation
Number of terms: 16387
Number of blossaries: 0
Company Profile:
Aviation Supplies & Academics, Inc. (ASA) develops and markets aviation supplies, software, and books for pilots, flight instructors, flight engineers, airline professionals, air traffic controllers, flight attendants, aviation technicians and enthusiasts. Established in 1947, ASA also provides ...
The maximum altitude at which a helicopter can support itself without forward motion. Hovering ceiling is normally given in two figures: in ground effect (IGE) and out of ground effect (OGE).
Industry:Aviation
The maximum altitude under standard atmospheric conditions at which an aircraft reciprocating engine can deliver its rated horsepower.
Industry:Aviation
The maximum amount of DC voltage that can safely be applied across the plates of a capacitor.
Industry:Aviation
The maximum amount of electrical pressure (voltage) that can be placed across an insulator before it breaks down and allows electrons to flow through it.
Industry:Aviation
The maximum amount of tensile load, in pounds per square inch, a material is able to withstand without being permanently deformed. Any time a material is loaded to less than its elastic limit and the load is released, the material will return to its original size and configuration. When loaded beyond its elastic limit, it will deform and not return to its original condition.
Industry:Aviation
The maximum amount of voltage that can be placed across a dielectric material without it breaking down and conducting. Dielectric strength is normally measured in volts per millimeter of thickness.
Industry:Aviation
The maximum authorized weight of the aircraft and all of its equipment as specified in the TCDS (Type Certificate Data Sheets) for the aircraft.
Industry:Aviation
The maximum distance from the localizer transmitter at a specified altitude as verified by flight inspection, at which reliable course information is continuously received.
Industry:Aviation
The maximum height above sea level at which an aircraft can maintain level flight under standard atmospheric conditions.
Industry:Aviation
The maximum load a component is designed to carry. The design load is made up of the actual load the component is expected to encounter, plus a factor of safety.
Industry:Aviation