The center of gravity (CG) of an aircraft is a critical factor in ensuring stability and performance during flight. As fuel burns from the wing tanks, the CG shifts forward, which can affect the aircraft’s handling characteristics.
To calculate the new CG position after fuel burn, you need to consider the initial CG position, the total weight of the aircraft, and the amount of fuel burned from each wing tank. The formula for calculating the new CG is:
Wtotal = total weight of the aircraft
CGinitial = initial center of gravity position
Wfuel = weight of fuel burned
D = distance from reference datum to wing tank
Understanding and accurately calculating the CG shift due to fuel burn is essential for maintaining the aircraft’s stability and ensuring safe flight operations.
How does fuel burning affect the aircraft’s center of gravity?
What information is needed to calculate the new CG position?
Can you explain the formula for calculating the new CG?
Why is it important to monitor the center of gravity during flight?
What happens if the CG shifts too far forward?
How often should I recalculate the CG during a flight?
Can this calculator also be used for other types of aircraft?
Results are for informational purposes only and do not constitute professional advice.
