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1. 07:55 AM - Re: Riveting wing nose rib through spar and tail rib on CH-701 (Vance Simons)
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| Subject: | Re: Riveting wing nose rib through spar and tail rib |
on CH-701
Doesn't matter on this application. You could alternate them if you wanted.
In a case were its not clear I install the rivet the same way I would
install a bolt. Head towards the front of the aircraft.
Vance
On Aug 25, 2014 10:09 PM, "Perry Delano" <pdelano@telus.net> wrote:
> Hi All,
>
>
> Just started assembling the primered left wing skeleton, and It is a bit
> late to ask, as the right wing is setting in storage, but does it matter
> which direction the 4 rivets through the rear rib on the 701 go. Does one
> insert the rivet through the nose rib, then spar then rear rib and pull the
> head on the rear rib side or the other way round or does it matter given
> the tip rib and rear rib are the same thickness. The spar cap is definetly
> thicker than the tip rib so the upper and lower rivet direction through the
> tip rib is defined, but I cannot find anything definite for the
> aforementioned 4 rivets. It is clear from the construction manual which
> direction the rivets go in the three L angle stiffeners and implied for the
> spar tip extension. Any help forthcoming will be greatly appreciated.
>
>
> Regards,
>
>
> Perry Delano
>
> *
>
>
> *
>
>
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