The aircraft shown has been weighed and the following information has been determined. The aircraft was weighed with unusable fuel and full oil. Calculate the Empty Weight and Empty Weight Center of Gravity. Location Weight Tare Arm Left Main Wheel 1107 2 323 Right Main Wheel 1100 4 323 Nose Wheel 1203 3 54 Weight and Balance Form Make Model; SN Tach Scale Calibration Due Aircraft as Weighed Position Scale Reading Tare Net Weight Right Whee Let Wheel Tal or Nose Wheel items not to be included in the Empty Weight Weight (1ba) Arm in ) Moment Fuel Oil Other Other Total Items to be added to the Empty Weight Weight (lbs) Am in Moment Fuel Other Other Total Final Calculations Weight (Ibs) Arm in Moment Right Wheel Let Wheel Tal or Nose Wheel Total to Remove Total to Add Empty Weight Empty Weight CG Signature Maximum Gross WI Certification No. Empty Weight Date Useful Load