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Chapter 16 - Weight and Balance: Let’s Wait & Balance
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          much does that weigh? Multiply 30
          times 6 pounds/gallon=180 pounds.
          The fuel tanks are located at an arm           Fig. 11
          of 96.0 inches aft of the datum. What
          moment does the fuel produce?
          Multiply 180 pounds times 96.0 inch-
          es=17,280 lb-in.
            To find the CG for the loaded air-
          plane you must divide the total
          moments by the total weights.
          Remember, all three arms that are
          shown in the middle column of
          Figure 11A are only used in comput-
          ing the moments. The arms aren’t
          added since this would serve no pur-
          pose. The next time that you will use
          the concept of arm is when you
          divide the airplane’s total moment
          by its total weight. The arm or dis-
          tance is now the point where the full
          airplane would balance (i.e., its cen-
          ter of gravity).

                   Weight X Arm=Moment
                  Arm (CG)=Total Moments
                                       Total Weight
            The total weight is 2,070 pounds.
           The total moments are 193,673 lb-in.
            Divide the total moments by the
          total weight to get the CG arm (the
          distance from the datum where the
          weights balance). Dividing 193,673
          by 2070=93.6 inches—the center of
          gravity as shown in Figure 11B.
            Considering that forward and aft
          CG limits are usually expressed in  appropriate limits for safe flight.  was 97.3 inches. In this instance,
          inches past the datum line, we can  Suppose the forward CG limit was  the airplane falls within the proper
          easily tell if the CG is within the  set at 89.0 inches and the aft limit  CG limits.

                    Determining Cargo Pallet Loads and Floor Loading Limits
             This may surprise you but as a private pilot, you can fly an airplane large enough to carry small pallets. Therefore, you should
           know something about the weight limits of the floor where these pallets can be placed in an airplane.
             The cargo or baggage area of an airplane has a load limit based on the structural integrity of that area. Think about it this way, if
           an airplane has a limit load factor of 3.8+Gs, then a 100 pound cargo load limit means the cargo area is stressed to hold 380
           pounds without experiencing damage. Exceed these weight limits and baggage area is subject to damage in high-G conditions.
             To determine the maximum weight of a loaded cargo pallet that can be carried in a cargo hold, divide its total weight, which
           includes the weight of the empty pallet and its tie down devices, by its area in square feet. This load per square foot must be equal
           to or less than the floor load limit.
             In this example, determine the maximum load that can be placed on this pallet without exceeding the floor-loading limit.
             Pallet dimensions..........................................36 by 48 in
             Empty pallet weight................................................47 lb
             Tie down devices....................................................33 lb
             Floor load limit ............................169 lb per square foot
             The pallet has an area of 36 inches (3 feet) by 48 inches (4 feet), which equals 12 square feet, and the floor has a load limit of 169
           pounds per square foot. Therefore, the total weight of the loaded pallet can be 169 × 12 = 2,028 pounds. Subtracting the weight of
           the pallet and the tie down devices gives an allowable load of 1,948 pounds (2,028 – [47 + 33]).
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