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My DG-600 has paired sets of static ports on the fuselage, just above
the wing roots. These feed the factory installed angle of attack meter. My meter does not function, and I'd like to construct a replacement. I assume the AOA meter was simply measuring the pressure differential between these ports. Would anyone care to guess as to the magnitude of these pressure differentials? I believe these meters were installed to address two issues, touchy stall characteristics at rearward CGs, and helping the pilot avoid draggy portions of the polar. Does anyone know if the meters were effective? Thanks, Marc |
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