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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 ...
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Note: for military transports, it's probably easier to use the corresponding civil template and add an armament section from the base template if necessary. Aircraft name goes here Image caption
Takeoff weight components. The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft, also known as the maximum structural takeoff weight or maximum structural takeoff mass, [1] is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits.
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.
|empty weight= – the unloaded, unfuelled, unoccupied weight of the aircraft. In most cases, this will be the Basic Aircraft Empty Weight. For lighter-than-air or hybrid aircraft, this will be the structural weight of the aircraft. |gross weight= – the fully-loaded weight of the aircraft. In most cases, this will be the Maximum Take Off Weight.
For example, the quantity 'empty weight' is specified by the parameters {{{empty weight main}}} and {{{empty weight alt}}}. The choice of which is the given first will depend on origin and period. A U.S. aircraft would have U.S. System of customary units given first (in the example of weight 'main' would be given in pounds (lb), and the value ...
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