10. The lift vector is 3" aft of the CG. The down force on the horizontal stabilizer is 105" aft of the CG. The weight o
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10. The lift vector is 3" aft of the CG. The down force on the horizontal stabilizer is 105" aft of the CG. The weight o
10. The lift vector is 3" aft of the CG. The down force on the horizontal stabilizer is 105" aft of the CG. The weight of the aircraft is 2200 lb. co PH What is the down force on the horizontal stabilizer? What is the lift?
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