This weekend, I'm going to visit a ~12yr-old 914 and try to troubleshoot a recent development. We noticed that the (differemtial) fuel pressure drops from 0.15bar at 30"MAP to something close to 0bar at 40". This causes the engine to stutter, the wastegate to open, the power and RPM to drop, and then the cycle can repeat (if we allow it).
Since we knew we could get within spec (placard on instrument panel says 0.25bar +-0.1bar) at 30", we flew the plane to get some idea of what's going on. What we noticed is that as we climbed higher, the fuel pressure would drop. By throttling back bit by bit as we climbed, the fuel pressure would stay within the acceptable window. We got to 5k' feet or so and then decided to glider around for a while, so we didn't test if the fuel pressure would climb as we descended.
Looking at the Rotax documents, this screams "regulation problem". However, while I was gone an A&P tested for vacuum leaks and proper regulation and he said it all looks fine.
If it were a fuel pump/fuel filter issue, then the fuel pressure would only drop at high volumetric flow rates, it certainly wouldn't have dropped linearly with increasing altitude, only to return when the throttle was brought out a little bit more.
Thoughts? Any easy checks to do while I'm in front of it? Could the power drop be due to anything other than fuel starvation relating to overly low float bowl pressures?
P.S. The placard and manual says 0.25bar +-0.10bar, but is that really correct? Reading through the way the float bowl works, I feel like in order to run the engine at the correct fuel-air mixture that the regulated pressure should be very, very close to 0.25bar.