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Yesterday, shortly after takeoff, the 912UL in my Pipistrel Sinus began to run roughly. Half way through my turn back to the runway, the glider began to shake similarly to a stall. I pushed the nose down and rolled out on final then, at idle RPM, there was a "bang" that came from the front. I immediately turned the ignition switches and key off, closed the fuel valves, and pulled the feather knob. The propeller continued to windmill.

After rollout, I pushed the glider off the runway and inspected the prop. All four bolts had sheared off behind the gearbox flange. The prop was retained only by the feathering rod and lever! I was surprised to see that there is no mechanical "key" to lock the prop to the gearbox flange and that all of the engine torque is reacted through shear loads on the four bolts.

I had installed new nuts and bolts and torqued them to the value specified in the Heavy Maintenance Manual and I'm mystified as to why they sheared. Is it possible to install the propeller in the wrong "clock" position? I did not find guidance on the angle of the propeller with respect to the prop flange.

A final question: would it be OK to use higher strength bolts to reinstall the propeller (after inspection/repair)?
  • Re: Sheared Propeller Bolts

    by » 10 years ago


    Hi Dan,

    912 prop setups I see are not just bolted on with bolts only for shear strength. They have lugs that pass between the prop hub and engine prop flange. The prop hub shear lugs comes from the back of the engine prop flange into the prop hub or the prop hub has lugs that insert through the flange and the bolts pass through them. I never see only bolts. I would also make sure you are using the proper bolts for the flange.

    This absolutely shouldn't have happened.

    Roger Lee
    LSRM-A & Rotax Instructor & Rotax IRC
    Tucson, AZ Ryan Airfield (KRYN)
    520-349-7056 Cell


  • Re: Sheared Propeller Bolts

    by » 10 years ago


    Mine has no lugs, only the flat surface of the gear box flange mating to the flat surface of the spacer between the flange and the spinner bulkhead and propeller hub.

    Looking closely at the bolts, the shoulders of the bolts just enter the gear box flange and the threads continue through the flange. According to the illustrated parts catalog that the local dealer has, there are no washers. The bolts sheared right where the threaded portion exited the gear box flange to the rear. The bolt ends and nylock nuts were missing. The M8 bolts were torqued to 27 Nm per the heavy maintenance manual.

    The local dealer has new propeller bolts on order from the factory and, if they also have the threads inside the gear box flange, I think I'll look for bolts of the same hardness (8.8) with a shoulder which protrudes slightly through the gear box flange and use a washer to cover those threads as a surface to tighten the nuts.

  • Re: Sheared Propeller Bolts

    by » 10 years ago


    If you have nothing protecting those bolts it may happen again. There is nothing to keep them from shifting back and forth and to secure it from the shear forces without some type of lug. What kind of prop is it?

    Roger Lee
    LSRM-A & Rotax Instructor & Rotax IRC
    Tucson, AZ Ryan Airfield (KRYN)
    520-349-7056 Cell


  • Re: Sheared Propeller Bolts

    by » 10 years ago


    The prop is a Pipistrel Vario. I'll look at the illustrated parts catalog again, but there were definitely no lugs when I removed the propeller previously. Nor has the local distributor/mechanic mentioned any.

  • Re: Sheared Propeller Bolts

    by » 10 years ago


    Roger, some propeller manufacturers use the Rotax metric bolt pattern and do not use drive lugs. My KOOL Prop uses only the metric mounting bolts with no shear lugs. I believe that the Kiev prop is the same.

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