*Stefan Balatchev wrote:> I am considering using Oilite bushings for my
tail movable surfaces. Press fit seems out of the reach for me, so I would
try the following method, please let me know if somebody else tried that
and if yes, what was the *outcome

Having spent a number of years in a landing gear overhaul shop, I have
learned a thing or two about bushing replacement-

No need to heat the part prior to any drilling operation. Heating is used
to open up the bore to ease installation of the bushing. Additionally,
bushings are usually cooled (submersed in liquid nitrogen) to "shrink" the
OD. The combination of heating the receiving bore and cooling the bushing
opens up dimensions which allows for ease of installation. When the temps
normalize, the interference fit will have been achieved. I have seen
bushings simply "drop" into place and then become very secure
when normalized.
As far as boring, the best method to hold .001" tolerances would be to
drill undersize and finish with an appropriately sized reamer.



On Fri, Aug 19, 2016 at 9:26 AM, Mark Langford via KRnet <
krnet at list.krnet.org> wrote:

> Stefan Balatchev wrote:
>
> > I am considering using Oilite bushings for my tail movable surfaces.
> Press fit seems out of the reach for me, so I would try the following
> method, please let me know if somebody else tried that and if yes, what was
> the outcome...<
>
> I just drilled a hole, maybe reamed it to size (I forget) and used
> Loctite 620 between bushing and aluminum. If it was a press fit, I
> probably just tapped it in place.  With 1130 hours on the plane, there
> is no noticeable play in the rudder hinges.  If you want to do as you
> plan, you can drill the hole in advance.  The hole will grow with the
> rest of the part.
>
> Mark Langford, Harvest, AL
> ML "at" N56ML.com
> www.N56ML.com
>
>
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