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Extra resources for A numerical analysis of three-dimensional vortex trapping
The weight and balance data of the airplane in Figure 3-10 states that the MAC is from stations 144 to 206 and the CG is located at station 161. indd 7 3/14/07 10:24:32 PM Figure 3-10. Aircraft weight and balance calculation diagram. indd 8 3/14/07 10:24:33 PM Small Fixed Wing Aircraft Operational Chapter Weight and Balance Computations Weight and balance data allows the pilot to determine the loaded weight of the aircraft and determine whether or not the loaded CG is within the allowable range for the weight.
6. 8. Enter all of these weights and moment indexes in the loading schedule chart and add all of the weights and moment indexes to determine the totals. Transfer these values to the CG moment envelope in Figure 4-8. The CG moment envelope is an enclosed area on a graph of the airplane loaded weight and loaded moment. If lines drawn from the weight and loaded moment cross within this envelope, the airplane is properly loaded. Figure 4-8. CG moment envelope. Multiengine Airplane Weight and Balance Computations Weight and balance computations for small multiengine airplanes are similar to those discussed for single-engine airplanes.
Station 549 To determine the change in CG, or __CG, caused by shifting 2,500 pounds of cargo from the forward cargo hold to the aft cargo hold, use this formula: 8. Then, determine new CG in % MAC: Since the weight was shifted aft, the CG moved aft, and the CG change is positive. If the shift were forward, the CG change would be negative. 59% MAC. 5% MAC. 36 inches, so the new CG is: When cargo is shifted from one cargo hold to another, the CG changes, but the total weight of the aircraft remains the same.