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The Joint Aircraft System/Component (JASC) Code Tables was a modified version of the Air Transport Association of America (ATA), Specification 100 code. It was developed by the FAA's, Regulatory Support Division (AFS-600). This code table was constructed by using the new JASC code four digit format, along with an abbreviated code title.
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.
Weight and Balance When the weight of the aircraft is at or below the allowable limit(s) for its configuration (parked, ground movement, take-off, landing, etc.) and its center of gravity is within the allowable range, and both will remain so for the duration of the flight, the aircraft is said to be within weight and balance. Different maximum ...
The weight of the aircraft is the common factor that links all aspects of aircraft design such as aerodynamics, structure, and propulsion, all together. An aircraft's weight is derived from various factors such as empty weight, payload, useful load, etc. The various weights are used to then calculate the center of mass of the entire aircraft. [37]
The Convair NC-131H Samaritan, also known as the Total In-Flight Simulator (TIFS), is a modified Convair C-131 Samaritan that was used to study aircraft handling characteristics. Built as a C-131B, the aircraft underwent extensive conversion and modification by the United States Air Force , NASA , Calspan and others from the late 1960s until ...
Officers, pilots and navigators, were trained to perform weight and balance calculations and became responsible for load planning. Aerial engineers on bombers and four-engine transports were also trained in weight and balance calculations using special slide rules developed for each airplane and commonly known as "slipsticks".
While the aircraft is in the air, weight in the wings does not contribute as significantly to the bending moment in the wing as does weight in the fuselage. This is because the lift on the wings and the weight of the fuselage bend the wing tips upwards and the wing roots downwards; but the weight of the wings, including the weight of fuel in ...
RP8 - Aircraft Weight Estimating and SAWE RP8: The objectives of this one-day course are to provide an overview of weight estimating methods and the weight estimating process for aircraft, and to provide insight into the weight and balance reporting formats and requirements of SAWE Recommended Practice 8.