I do the same thing but I also crimp the threaded sleeve (carefully
with dikes) 4 times in 90 degree opposed locations.
Stew

--- In [EMAIL PROTECTED], [EMAIL PROTECTED] wrote:
>
> Hi Bob,
>
> I use a carbon rod about .075 diameter, then sand the very ends
slightly so
> that they slip fit into a Sullivan threaded clevis.  I glue one end
in with
> thick CA and then mount everything up in the wing, turn on the RX
and let the
> everything center.  The rod end that is not glued just slips to its
length
> inside the clevis hole for perfect length...then I just work that
surface a bit
> with the appropriate TX stick so that the end of the rod gets
exposed, then I
>  put some CA on it, let go of the stick and hit it with Kicker.
>
> If you need to adjust for some reason after, or remove the clevis'
to use
> somewhere else, just use a lighter on the glued end, it will light
on fire a
> bit, burning away the CA.  A little clean up and you are ready to
use the
> clevis again or re-glue the joint you wanted to adjust.
>
> If you'd like some photos of this, just ask :-).
> Gordy
>
>
>
> In a message dated 4/4/2008 6:08:43 A.M. Eastern Daylight Time,
> [EMAIL PROTECTED] writes:
>
> There  are several types of servo savers.  Some have spings on the
rod to
> relieve the stress of a flap down landing.  Last ones I saw were
10  years
> ago and I think Skip Schow had them on a plane.  If now, he
probably knows
> who did.
>
> ----- Original Message -----
> From:  Michael Whitman
> To: Robert P Buxton
> Cc: [EMAIL PROTECTED]
> Sent:  Thursday, April 03, 2008 9:36 PM
> Subject: Re: [RCSE] Aileron & Flap  Carbon Fiber Pushrods
>
>
> I haven't had first hand experience with  carbon pushrods but I
would guess
> that you could also run the risk of  stripping a servo with a
stiffer linkage
> if you failed to retract the  flaps on landing again.  It's cheaper
to
> replace or fix the pushrod  instead of a wing servo.
>
>
> Mike
>
>
>
>
>
> On Apr 3,  2008, at 2:56 PM, Robert P Buxton wrote:
>
> Open Question to the  group:  Has anyone had experience (good or
bad) with
> using carbon  fiber push rods for their aileron & flap servo
linkage.  This
> past season, due to slow thumb response at that critical moment of
> retracting flaps just before touch down, I was bending the flap
push rods
> (bottom hinged, linkage on top of flap, servo arm on bottom of
wing.   Carbon
> fiber rods would give stiffness/rigidity but would they be prone
to
> breakage?  This set up was/and is on a F3J 144" Shadow.  All
comments and
> suggestions would be greatly  appreciated.
>
> Regards,
>
> Robert
>
> Robert P  Buxton
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