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Tecnam Astore 2015 with Rotax 914 Turbo. ~150 hours since new. Annual in March with no major problems.

Flying July 16, 2018, OAT 88F, Run up, take off normal. About three miles from runway, I switched off fuel boost pump. Engine died for a second. Recovered with partial power. A low "Hum" could be heard, varying in pitch and intensity. Gauges in green when I checked: CHT (One cylinder only), Fuel pressure, oil pressure and temp. Fuel tanks full of 91 octane, ethanol free auto gas (Shell).
Switching boost pump back on improved but did not eliminate the problem. Made it back to the airport.
Ran it up on the ground yesterday, July 17. Temp 77F. Started and ran mostly full throttle for 10 minutes. Experienced one slight hesitation but nothing like day before.
Inspection of engine after each of these episodes revealed no leaks, odors, stains, nothing loose. Always drain sumps (3). Never seen water.

Dx? Advice?
Inspection check list?
  • Re: 914 Turbo Partial Failure

    by » 6 years ago


    Did you ever adjust your fuel pressure regulator?

    What is your manifold PSI VS your fuel pressure (you need a differential pressure gauge to determine this)
    If you have too much manifold PSI (boost) over fuel pressure, you will blow your float bowls dry. IF you have too much fuel over boost, you will flood your engine, so its a fine balance.

    It could be vapor lock also (regardless of ethanol). The Tecnam should have data you can download from the Dynon/Garmin that will give you a fuel flow. If you ever see your fuel flow spike during your test run, it could be a sign of vapor passing over the transducer impeller speeding it up.

    My suggestion is get the engine run data from your Garmin/Dynon as it will tell a story of what's going on.

    Also, here is a video on checking fuel pressures on a Rotax 914. https://www.rotax-owner.com/en/videos-topmenu/elearning-videos/231-914press136

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