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Kern is a published author and public relations contractor for a number of companies in the aviation industry. He told AOPA that an accumulation of fatal mistakes related to miscalculation of weight, balance, or both, drove his desire to automate the task. He said too many aircraft have crashed because they were overloaded, or had a center of gravity outside of limits, rendering them uncontrollable. Kern believes very few pilots take off knowing their aircraft’s CG is out of limit, yet it happens. More common, he said, are cases where aircraft are flown overweight.
The formula for calculating weight and balance is simple, and there are many calculators available, including many built into aviation apps. But they all depend to some degree on estimates and manual input. Kern said the ones he has examined lack functionality to flag obvious errors, such as entering 2,000 instead of 200 pounds for a passenger’s weight. Very few pilots (if any) require passengers to step on scales before boarding. Many pilots he has talked to don’t even bother to calculate weight and balance in aircraft they fly routinely with similar loads.
Fueling errors can also leave aircraft heavier than the pilot expects, Kern said “or grandma sneaks her cannonball collection on board, and she knows that you don’t want her to do that so she sticks it behind the back seat.”
Kern has applied for a utility patent for his automated solution, which he said can be retrofitted to virtually any airplane with minimal modification. He programmed a small computer to accept inputs from sensors that measure weight by monitoring the pressure in landing gear struts.
“You don’t modify the strut,” Kern explained. “You take the pressure off the strut and you use that as a surrogate.”
Kern said his system is designed to calibrate itself on every flight, compensating for changes in temperature. If the airplane does not have struts, he added, strain gauges or bending gauges can perform the same function. Measuring the weight resting on each wheel (or ski, or float, as the case may be) and adding the known weight of the landing gear below the sensor—the “unsprung” weight of the aircraft including the fluid in brake lines—allows the system to accurately measure the actual ramp weight, along with the aircraft balance, Kern said. This information can be displayed graphically, instantly calling attention to a problem even before the engine
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