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Weight and balance can be a confusing topic. Start by understanding these terms...
The weight of an empty airplane including unusable fuel, full operating fluids (hydraulic fluids) and full engine oil.
Standard Empty Weight plus optional equipment. This is the starting point of weight and balance calculations.
Useful load is total usable fuel, cargo, passengers, and drainable fuel. Equation: Maximum Ramp Weight - Basic Empty Weight = Useful Load
This one is simple. Think of payload as what's "paying" for the flight: passengers, bags, and cargo. It's how much weight you can carry besides basic empty weight and fuel.
This is the maximum allowable weight mass for ground operations. MRW assures acceptable ground maneuverability and includes fuel for taxi, run-up and start.
Maximum allowable mass for the initiation of a takeoff roll. Depending on how big your airplane is, you may have a variety of MTOWs limited by: structural limitations, runway distance, climb performance, or landing weight limits.
Minimum certificated weight for flight as limited by aircraft strength and airworthiness requirements. This weight has a lot to do with the balance of weight considering fuel/payload distribution.
Maximum landing weight is usually a structural limit, but may include calculations based on missed approach climb performance.
Did we miss anything? What other terms should pilots know for weight and balance? Tell us in the comments below.
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