Now a question on reassembly.
 I was taught last century that the newly installed greased bearings were
installed on the wheel/axle assembly and the axle nut tightened to a good
snug fit.  The wheel was rotated to 'work" out the excess grease. Next the
axle nut was loosened and retightened to take up all slack in the bearing.
Then the nut was cotter pinned to the axle as is or went to the next tighter
position to perform the cotter pin operation.  This was done to prevent
false brinelling created by the vibrating wheel in flight on a loose
bearing.
Is this still true or has the technology of aircraft wheels, bearings, and
or lubrication got us past this problem?
Bb Morrissey, New Bern, NC
----- Original Message ----- 
From: "Mark Langford" <n5...@hiwaay.net>
To: "KRnet" <kr...@mylist.net>
Sent: Wednesday, August 31, 2005 10:00 PM
Subject: Re: KR> removing Cleveland bearings?


> OK, I guess I answered this one myself (before I read Orma's reply).  Once
I
> had it split, there was still no way to get them out, so closer
examination
> revealed a thin snapring on the outside.  So I split them for no reason.
> The snapring popped right out, and the bearings fell out.  Indeed, there's
> not much grease in there.  So little that they rattle!  To the airport
> tomorrow, and hopefully flying this weekend.  The weather's supposed to be
> gorgeous.  Ran the engine some more today, for a total of about 2.5 hours
so
> far.  It runs fine so far...
>
> Mark Langford, Huntsville, Alabama
> see KR2S project N56ML at http://home.hiwaay.net/~langford
> email to N56ML "at" hiwaay.net
> --------------------------------------------------------------
>
>
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