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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) + ...
1. What is the datum and its purpose when making weight and balance computations? It is an imaginary vertical line or plane used in weight and balance calculations from which measurements are taken both forward and aft to determine the relative location of items in the aircraft.
Yes, a weight and balance issue can be more critical on smaller airplane because a even a small error accounts for a larger percentage of the total weight. A 500-lb. error on an airplane that weighs 5,000 lbs., adds up to a larger percentage of the total weight.
Typically, an operator calculates takeoff weight by adding the operational empty weight (OEW) of the aircraft, the weight of the passenger, cargo payload, and the weight of fuel. The objective is to calculate the takeoff weight and CG of an aircraft as accurately as possible.
Technique: Weight and balance Ascertain from the pilot's operating handbook the empty weight of the aircraft and determine the weights of people, baggage, and fuel. Multiply each weight by the arm\u2014the distance from the reference datum\u2014to find the moment. Add all the weights to find the gross weight.
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Typically, an operator calculates takeoff weight by adding the operational empty weight (OEW) of the aircraft, the weight of the passenger, cargo payload, and the weight of fuel. The objective is to calculate the takeoff weight and CG of an aircraft as accurately as possible.
Compliance with the weight and balance limits of any aircraft is critical to flight safety. Operating above the maximum weight limitation compromises the structural integrity of an aircraft and adversely affects its performance.
A sheet which records the distribution of weight in an aircraft and shows the center of gravity of an aircraft at takeoff and landing.
Arm (moment arm) is the horizontal distance in inches from the reference datum line to the CG of an item. The algebraic sign is plus (+) if measured aft of the datum and minus (\u2013) if measured forward of the datum. Moment is a force that causes an object to rotate.
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.

airplane weight and balance sheet