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๐‚๐ž๐ง๐ญ๐ž๐ซ ๐จ๐Ÿ ๐†๐ซ๐š๐ฏ๐ข๐ญ๐ฒ (๐‚๐†)



๐Ÿ›ซThe center of gravity (CG) of an aircraft is the point over which the aircraft would balance.

๐Ÿ›ซIts 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.

๐Ÿ›ซThe center of gravity affects the stability of the aircraft.

๐Ÿ›ซTo ensure the aircraft is safe to fly, the center of gravity must fall within specified limits established by the aircraft manufacturer.

๐Ÿ›ซCenter of gravity (CG) limits are specified longitudinal (forward and aft) and/or lateral (left and right) limits within which the aircraft's center of gravity must be located during flight.

๐Ÿ›ซThe CG limits are indicated in the airplane flight manual.

๐Ÿ›ซThe area between the limits is called the CG range of the aircraft.

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