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Excessive weight reduces the flight performance in almost every respect. The most important performance deficiencies of an overloaded aircraft are: Higher takeoff speed. Longer takeoff run.
Weight and balance have a direct effect on the stability and performance of the aircraft. If a plane is too heavy, it may never get off the ground. If it's out of balance, it may be uncontrollable when it does take flight. Obviously, neither of these scenarios will produce a desired outcome.
14 CFR part 125 requires aircraft with 20 or more seats or maximum payload capacity of 6,000 pounds or more to be weighed every 36 calendar months. Multi-engine aircraft operated under 14 CFR part 135 are also required to be weighed every 36 months.
Among these vital factors is proper weight and balance control. The weight and balance system commonly employed among aircraft consists of three equally important elements: the weighing of the aircraft, the maintaining of the weight and balance records, and the proper loading of the aircraft.
So, are we required by the FARs to calculate a weight and CG for every flight? And, does the weight and balance information located in the Pilot's Operating Handbook satisfy the requirement for having a current weight and balance on-board? The answer to both questions is No.
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Weight and balance have a direct effect on the stability and performance of the aircraft. If a plane is too heavy, it may never get off the ground. If it's out of balance, it may be uncontrollable when it does take flight. Obviously, neither of these scenarios will produce a desired outcome.
The structural strength of the aircraft also limits the maximum weight the aircraft can safely carry. The designers carefully determine the ideal center of gravity (CG) and calculate the maximum allowable deviation from this specific location. 3.
Having current weight and balance documentation on board the aircraft for flight is not, in fact, a general requirement for operation under §91.
The total weight W of the aircraft is simply the sum of the weight of all of the individual components. W = w(fuselage) + w(wing) + w(engines) + w(payload) + w(fuel) + ...
\u201cYou need to have the current weight and balance data on board the aircraft. This includes basic empty weight and moment, as well as the approved envelope for the aircraft.

weight and balance form pdf