That looks fine. Only rotational force on cotter pin hole. Wall thickness of axle is 3/16 not counting threads.
Thanks...
On another note....that axle must be hard...bits dulled fast![]()
I've been meaning to ask - is this method common across small aircraft? Just seems very hokey, particularly when things get a little loose - do you drill another hole? Or are there very thin shims available?
You have multiple holes in the nut, and chose one that’s on the looser side.
I just ordered some thin shims from mcmaster-carr - hopefully that will be a good solution - I want the wheels to rotate freely but not have any play.
Good info. I can see adjustment as described by shaving a bit on nut face to get to fit tight, but loose, initially.If you feel the need to get very precise, you can "face" the nut on an engine lathe, or vertical mill if you prefer.
Since you know the TPI is 16 - you know that each revolution = .063" advancement. With six "flats" on the nut, you also know that the advancement of each one = .0105".
So, as an example, if you estimate you need about a half a flat advancement for a proper fit, you need to face off .0105/2" = .0052". Any machinest, home schooled or otherwise should be able to do this with out problem.
I do this on all my "fit ups" to insure I get the fit I want instead of what the suppliers give me. Also, if needed, the depth of the nut itself can be cut down quite a bit, if doing so helps with the wheel pant install.
If you like the idea of using shims to "adjust" the fit for future wear, I would suggest the following:
Extremely thin shims (a few "thou") have the tendency to ball up in a wad when they are installed or are too fragile to remain intact during their service life. So, undercut the axle nut to allow a thicker shim to be installed initially, to give the desired fit. Then as conditions warrant, change the shim size (but still thick enough) as needed. From the Aviation Division of McMaster-Carr, for 1 1/4" diameter axles, their shim thickness from .031" on down are less than or equal to .005" - should be close enough.
YMMV - and probably will.
HFS
You have multiple holes in the nut, and chose one that’s on the looser side.
I treat my axle & nut alignment a bit differently. I want to have (or have available) finer adjustability of the bearing preload so instead of 60 degree, I drill the axle with a second hole to allow 30 degree increments. This comes notably relevant when it comes the day if I ever have to replace my bearings.
I also slot the cotter pin holes in the nuts to make them easier to install.
Sorry for the 'manual' graphics
I think Van's designed it like this so that the nut could be used to support the wheel pant via the bolt in the middle for the bracket.I was just re-reading this old post from when I was originally installing my wheels.
Now I'm putting two new tires on and am dealing with the fact that the holes are so hard to line up with the nut and the right tension. This is stupid, they should be a slotted nuts like most other aircraft axels nuts...why did Matco do this???
I get that the nut needs to support the wheel pants.I think Van's designed it like this so that the nut could be used to support the wheel pant via the bolt in the middle for the bracket.
A round needle file could be used to elongate the existing holes along the axis and that should make it easier to get the pin in.I get that the nut needs to support the wheel pants.
If I had a mill, I’d try slotting the existing holes in the stock nuts