Josh,

Did you happen to get a look at the broken bolt looking across the face of the break?  Good possibility it was a fatigue failure which occurs at stresses well below the breaking strength, in which case you can sometimes see the "beach marks" as the failure works its way across the section.

Neil Gallagher
Weatherly 35-1
Glen Cove, NY


On 2/24/2021 8:47 PM, Josh Muckley via CnC-List wrote:
Dennis,

Your number of 7500 lbs confirms my number of 7200 lbs.  That just seems incredibly high considering the OEM decided that 2 bolts would be required.  It also seems ridiculous that one of them broke.  I am at a complete loss as to how that would have happened.

Josh




On Tue, Feb 23, 2021, 12:00 Dennis C. via CnC-List <cnc-list@cnc-list.com <mailto:cnc-list@cnc-list.com>> wrote:

    I'm guessing the thread degradation doesn't have much effect on
    the strength as long as the shaft is not damaged.  Having said
    that, the shear strength of a M12 10.9 hardness bolt is about 7500
    lbs.

    Did I win?  What's my prize?  Can it be shipped or do I need to
    pick it up/sail it home?

    Dennis C.
    Touche' 35-1 #83
    Mandeville, LA

    On Tue, Feb 23, 2021 at 9:42 AM Josh Muckley via CnC-List
    <cnc-list@cnc-list.com <mailto:cnc-list@cnc-list.com>> wrote:

        Engineering discussion for the group.

        Here's the background.  For about 9 years I have known about
        having 1 of the 2 bolts broken on the forward starboard engine
        mount. These bolts hold a piece of 1/2 inch plate steel which
        was bent at a 90° angle to the vertical side of the engine. 
        This creates a horizontal shelf. The shelf then rests directly
        on the vibration dampening mount which is then bolted to the
        boat. Periodically, I have made attempts to extract the bolt
        but only a few days ago was I finally successful.  The bolt
        was a M12x1.75.  I don't know what hardness the OEM called
        for.  Years ago when I discovered the broken bolt I was quick
        to replace the remaining good one with one having a hardness
        of 10.9.  For a fresh start, I now intend to replace both of
        them with new and again a hardness of 10.9.  In removing the
        old bolt, my drill hole was off center and ended up cutting
        some of the threads.  I approximate not more than 1/4 of the
        thread integrity was compromised.

        https://drive.google.com/folderview?id=15GCOH3qKIWXl1lmjsbZqsf-ECGCrl1fN

        Here comes the question(s).  Just for kicks, I decide to
        attempt to figure out what the sheer strength of the engine
        mounting bolts are individually.  I came up with an answer but
        would like hear what the group comes up with.

        I also now have a bunch of other questions tumbling around
        like:  How much weight would it take to break one?  How much
        margin to failure did I have while operating for the last 9
        years?  What could have possibly caused this bolt to break
        prior to my ownership?  Theories and ponderings are welcome.

        With 1/4 of the threads degraded on the newly available bolt
        hole, I plan to only torque the bolt to ~50% of max (90
        ft-lbs) which would be ~45 ft-lbs.  I'll also make sure that
        the lock washer is fully collapsed but I'm confident that that
        will happen well before final torque is reached.  In sheer, I
        believe this bolt is providing as much or more strength simply
        by being there than anything to do with its torque.  All
        though, I have heard the engineering theory that (when built
        appropriately) the bolts apply the pressure which creates the
        friction to prevent the pieces from moving in sheer.  Under
        this argument the 2 pieces of metal don't actually ride on the
        bolt shank specifically, and the surface area where the 2
        pieces touch is of particular importance.  Looking at the
        engine castings, it would appear that maximizing surface area
        contact was not considered.  As such, I can only fall back on
        my previous thought that the bolt shank is in fact carrying
        the load in sheer and torque is more or less irrelevant except
        for the purpose of keeping the bolt tight.  I'm also aware of
        various thread repair options but in the awkward location I am
        fearful that I would cause more damage than good by attempting
        any of them.  Particularly if the value added by the second
        bolt truly is its presence not its torque.

        All thoughts and insights are encouraged.


        All the best,

        Josh Muckley
        S/V Sea Hawk
        1989 C&C 37+
        Solomons, MD
        Thanks to all of the subscribers that contributed to the list
        to help with the costs involved.  If you want to show your
        support to the list - use PayPal to send contribution --
        https://www.paypal.me/stumurray Thanks - Stu



-- Dennis C.
    Touche' 35-1 #83
    Mandeville, LA
    Thanks to all of the subscribers that contributed to the list to
    help with the costs involved.  If you want to show your support to
    the list - use PayPal to send contribution --
    https://www.paypal.me/stumurray Thanks - Stu



Thanks to all of the subscribers that contributed to the list to help with the 
costs involved.  If you want to show your support to the list - use PayPal to 
send contribution --   https://www.paypal.me/stumurray  Thanks - Stu

Thanks to all of the subscribers that contributed to the list to help with the 
costs involved.  If you want to show your support to the list - use PayPal to 
send contribution --   https://www.paypal.me/stumurray  Thanks - Stu

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