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The prop balance service will use high tech equipment to pick up an imbalance of one thousandth of an inch per second (IPS) in your powerplant installation (engine/propeller combination), and gives the procedures and techniques to install permanent weights onto the propeller spinner assembly which will dynamically balance the propeller assembly. An accelerometer is place on the engine, preferably on the center line of the crankcase, longitudinally in-line with the crankshaft and as close as possible to the propeller assembly. A photocell (or laser optic) is placed on the exterior cowling to pick-up the placement of some reflective tape affixed to one of the propeller blades. The accelerometer senses vibration and the photocell notes the location of the vibration (or highest point of vibration). Both of these data points are inputted into a computer box through harness connections between the three units. The computer box gives actual propeller rpm, vibration level, vibration location and what weight to install to gain a perfect 0.000 inch per second of vibration. This vibration is lateral displacement, the difference of the two spinning masses, the propeller and the engine.
Once the initial engine run is complete to sense the initial vibration level, the first temporary weights are installed, per the computer's recommendation, then a second engine run is performed and the computer will take both first and second engine run data to compute if more weights are to be installed or moved to a better location to obtain a "smooth" propeller. It is this third engine run that I use the previous steps data to gain the permanent weight location to be installed on the propeller assembly.
As time goes by and hours are incurred on your engine and propeller, normal wear-n-tear will take its toll on the static balances set by the engine and propeller manufacturers. Remember, each of these manufacturers produced their product independent of one another, and the static balance and turning mass of one unit (the engine) will not match the turning mass and static balance of another unit (the propeller). This is where a dynamic balance procedure of the powerplant assembly would verify if the inches per second of vibration is more than 0.1 IPS (inch per second) desired. Note, that the less vibration your powerplant produces and has to incur, the longer it will last, as well as less stress is put on the accessories, airframe and passengers.
To have our powerplant assembly dynamically balance with A&P Aviation Services, the cost includes a 2-3 hour completion of this procedure and an accuracy check of the mechanical engine tachometer is conducted. All work is performed in accordance with Dynamic Solutions Systems MicroVib II, which meets FAA standards for this minor alteration.
Please contact A&PAS to schedule your dynamic propeller service: |