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Re: Throttle Cable Considerations

Subject: Re: Throttle Cable Considerations
From: Erich D Trombley <erichdtrombley@juno.com>
Date: Thu, 9 Aug 2001 16:58:47
John, sorry to hear about the accident.   Thanks for sharing this
unpleasant event.   I hope you are able to get her flying once again. 
Regarding the throttle cables I am using a solid wire vs stranded cable. 
I too had concerns about the cable kinking and thought the wire is
effective in either push or pull.  I don't recall at the moment but I
ordered the cable from Aircraft Spruce.  I did have to make up custom
ends but this wasn't difficult as I bent the wire around an AN111 cable
bushings and soldered it in place as a extra measure of safety, rather
easy.  The cable end is then attached to the throttle lever via the
mounting hardware for the Europa supplied cable.  I have yet to fly as I
am still months away from completing my plane.  But the system works well
on the ground.

Erich Trombley
A028


writes:
> 
> I  recently had a landing accident in N44EU which was
> precipitated by power failure during a go around;  N44EU, a Mark
> 1,  incurred "substantial damage"  (FAA assessment). I was
> fortunate to walk away with minor bruises and scratches.
> 
> In analyzing the accident later, I  concluded from all the
> details of the power failure that the most likely cause was that
> the throttle cables kinked within the throttle block when I
> attempted to rapidly apply full throttle, effectively locking the
> power at the existing setting.
> 
> With the throttle at idle, several inches of cable are within the
> throttle lever block and are not constrained by the sheath. When
> the throttle is advanced, the springs at the carburetors normally
> take up slack in the cable.  Should the throttle lever be
> advanced faster than the springs take up the slack, the cable can
> loop downwards and kink within the throttle lever block,
> effectively locking the throttle at a setting providing much less
> than commanded power.
> 
> I expect that the rate at which the springs can take up the slack
> will vary between aircraft depending on the routing of the
> throttle cables, cable lubrication, and any other friction or
> mass in the throttle cable system.  In my case, I used powdered
> graphite lubricant on all cables rather than oil (this to avoid
> dirt attracted by oil) - I doubt that this contributed to the
> problem, but each builder must make a choice of lubricant for
> himself.  The awkward part is that dirt, temperature, and other
> unknown conditions could affect the maximum rate of throttle
> application before kinking will occur and this could vary between
> flights.  Further, rapid throttle application tends to occur when
> power is needed rapidly so a pilot could exceed the critical rate
> inadvertently.
> 
> A further consideration with this throttle system design is that
> should one of the throttle springs break then a similar kinking
> failure will almost certainly occur.
> 
> My understanding of the reason the spring is incorporated by
> Rotax is to cause the engine to go to full power should a
> separation occur within the throttle linkage, the concept being
> that having full power is better than having less.
> 
> My inquiries turned up another report of a Europa which kinked a
> throttle cable on takeoff resulting in less than full power and
> an aborted takeoff with no serious consequences.  This lends at
> least a bit of credibility to my amateur accident investigation.
> 
> I don't know whether the XS model uses the same throttle design
> so this may not apply there.
> 
> Until the cause is officially established, I believe Europa
> builders who have throttles of the above described design should
> use some care when advancing the throttle rapidly.
> 
> John          Newtown, CT
> 
> The Europa List is supported by Aviators Network UK - 
> info@avnet.co.uk



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