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  • Chapter 10: Weight and Balance › Determining Loaded Weight and CG › Weight Shifting

    Shifting, Adding, and Removing Weight A pilot must be able to solve any problems accurately that involve the shift, addition, or removal of weight. For example, the pilot may load the aircraft within the allowable takeoff weight limit, then find…

  • Chapter 10: Weight and Balance › Determining Loaded Weight and CG › Weight Addition or Removal

    proportional to the distance the weight is shifted. Weight Addition or Removal In many instances, the weight and balance of the aircraft will be changed by the addition or removal of weight. When this happens, a new CG must ... limitations to see if the location is acceptable. This type of weight and balance problem is commonly encountered when the aircraft burns fuel in flight, thereby reducing the weight located at the fuel tanks. Most small aircraft are designed with…

  • Chapter 6: Aircraft Weight & Balance › Weight & Balance Terminology › Minimum Fuel

    check should be made to ensure that the CG will not shift out of limits when crew, passengers, cargo, and expendable weights are added or removed. If the limits are exceeded and the aircraft is flown in this condition…

  • Chapter 9: Weight and Balance Control— Commuter Category and Large Aircraft › Determining CG Changes Caused by Modifying the Cargo › Determining Which Limits Are Exceeded

    Determining the CG Shift When Cargo Is Added or Removed To calculate the CG when cargo is added or removed, add or subtract the weight and moment index of the affected cargo to the original loading chart. Determine ... takeoff weight is 16,600 pounds. • Maximum zero fuel weight is 14,000 pounds. • Maximum landing weight is 16,000 pounds. Figure 9-52. Flight manifest of a Beech 1900 in the cargo configuration. Figure 9-53. Shifting cargo from…