rvsimons
Joined: 18 Jan 2013
Posts: 22
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 Posted: Tue Aug 26, 2014 6:55 am Post subject: Riveting wing nose rib through spar and tail rib on CH-701 |
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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(at)telus.net (pdelano(at)telus.net)> wrote:[quote]
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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_________________
Vance Simons
Post Falls, Idaho
Zenith 701 |
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