Weight and Balance Calculations
When calculating the location of it is important to proceed in an organized and methodical manner. The following example will demonstrate how to perform basic weight and balance calculations for a single-engine general aviation aircraft.
Sample Question
An aircraft’s empty weight and moment are 1,582 pounds and 60,827.9 lb-in respectively. The pilot weighs 225 pounds and front and rear passengers weigh 200 and 150 pounds respectively. Baggage area one holds 34 pounds of baggage and baggage area two holds 13 pounds of baggage. Planned ramp fuel and fuel burn for the 1.2 hour flight are 50 gallons and 8.5 gallons per hour respectively. 8 pounds of fuel are consumed during engine start, taxi and runup. Using the charts provided, select the correct statement.
