This tool is designed for aerospace professionals to calculate the weight and balance of aircraft, ensuring safe and efficient flight operations.
All calculations are based on the standard aerospace engineering formulas. For further reading, refer to the official FAA guidelines on weight and balance.
The total weight is calculated as the sum of empty weight, fuel weight, and payload weight: W_{\text{total}} = W_{\text{empty}} + W_{\text{fuel}} + W_{\text{payload}}.
The center of gravity is determined using: \text{CG} = \frac{\sum (W_i \times \text{arm}_i)}{W_{\text{total}}}.
Consider an aircraft with an empty weight of 1000 lbs, fuel weight of 300 lbs, and payload weight of 200 lbs. Input these values into the calculator to discover the total weight and center of gravity.
Proper weight and balance are critical for aircraft performance and safety, affecting handling, efficiency, and compliance with regulatory requirements.
Ensure all weights are measured accurately, and double-check the units used in calculations.
Exceeding weight limits can impair aircraft handling, increase fuel consumption, and may lead to regulatory violations.
This calculator is generally applicable but always consult specific aircraft manuals for precise limits and procedures.