Solid riveting the main spar
Posted: Fri Aug 15, 2014 11:04 pm
I have started 'smashing' the solid rivets in the main wing spar. Stressing over it quite a bit. I was at Oshkosh and got to see the riveting done on a factory assembled spar. To my eye - not much different than what I have done so far. But I went so far to measure each of the completed rivets 'upset' height and width to compare against textbook spec. This is what I have:
Spec: Height: .09375 - .0625 / Width: .281 - .203
Mine:
.092 / .232
.0975 / .223
.097 /.219
.094 / .246
I've included couple of pictures (there is a shadow at the base of the rivet that makes it look like the rivet is dumped over a bit, but they are not).
Am I overstressing about this? Are my rivets 'close enough' to spec? I am using a back rivet tool and it seems the collar is bottoming out so that is as far as it will mash the rivet.
Spec: Height: .09375 - .0625 / Width: .281 - .203
Mine:
.092 / .232
.0975 / .223
.097 /.219
.094 / .246
I've included couple of pictures (there is a shadow at the base of the rivet that makes it look like the rivet is dumped over a bit, but they are not).
Am I overstressing about this? Are my rivets 'close enough' to spec? I am using a back rivet tool and it seems the collar is bottoming out so that is as far as it will mash the rivet.