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{Did you verify the fuel vents are working
properly? ....and that the check valves on the vents are
oriented correctly?}
There should be no check valves on vent lines. If you
take off at sea level with a wing tank at atmospheric pressure, 14.7 psia
trapped by a check valve, and climb to 18,000 feet, static pressure 7.35
psia, the differential pressure on the tank will be 7.35 psi, 1,058 pounds
per square foot trying to rip the skins off the spar and ribs.
Vent lines must be free flowing both
directions.
Regards,
Bill Hannahan
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