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Airflow performance orings aircraft11/16/2023 ![]() To fuel your dream, contact Don, Kyle, or Colleen today. For more than 30 years, Airflow Performance has offered the best possible value in fuel metering design, systems integration, and customer service. An aircraft with a laminar flow airfoil should have its pitot tube located further aft to some point where the maximum camber of the wing occurs. ![]() Laboratory services are available for airbox tests, high pressure ratio air flow testing, and of course, fuel flow calibration. for aircraft utilizing the older airfoils (Clark Y, etc.), just so long as the pitot tube opening is about 5' or more below the surface of the wing. Complete installation of fuel systems can be done in-house, with appropriate documentation. The staff is capable of engineering, design, prototype machining, and fabrication to meet any fuel system requirement. API systems are found on a wide variety of wheeled vehicles, boats, and aircraft. Airflow Performance has designed and built fuel injection systems for 2-stroke, 4-stroke, rotary, radial, air cooled, liquid cooled, naturally aspirated, and turbo/supercharged engines ranging from 60 to 3000 horsepower. Part Number 953516-10 is an O-RING manufactured or catalogued by Cessna Aircraft.95. Don ultimately became the Project Engineer responsible for the RS and RSA product line. ![]() It is recommended to use a 40-micron maintainable filter in composite aircraft applications. This maintainable filter incorporates a 125 or 74 micron pleated stainless steel filter element with a anodized aluminum housing. An engineer and A&P, Don began his career at the Bendix Energy Controls Division, working for Elmer Haase, the inventor of the RS and RSA fuel injection system. filter Airflow Performance recommends for this application is P/N1090079 or 1090079-74.
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