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On most constant fuel injection aircraft systems, the fuel flow sensor (turbine
wheel) is placed between the injector servo and the distribution spider (rail). The
fuel return line is from the servo to the tank. Therefor the turbine only measures
the fuel delivered to the spider and the cylinders. Or did I miss something here?

Bruce
Glasair III

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Please send your photos and drawings to marvkaye@olsusa.com.