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02-09-2014, 05:05 PM
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Join Date: Feb 2006
Location: Valley Forge, Pa
Posts: 636
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Photos Please
Photos of the gear and socket,please. Has the wheel strut been lose of wobbly of late?
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02-09-2014, 05:26 PM
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Join Date: Sep 2005
Location: Maple Grove, MN
Posts: 2,329
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On my 6A, the edges of the hole in the gear leg were quite sharp. I took the gear leg off for inspection after a couple years' use, and I could not get the bolt out without significant effort, like a couple hours' worth. It appeared that the sharp edge on the gear leg hole had caused quite a bit of disruption to the bolt. Additionally, the stock AN bolt seems to leave too much clearance, allowing some wobble (even if not perceived). There is discussion elsewhere on these forums about using a close tolerance bolt in this location. I also chamfered the hole in the leg.
It could be causal in this case - very glad nothing worse happened!
__________________
Alex Peterson
RV6A N66AP 1700+ hours
KADC, Wadena, MN
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02-09-2014, 05:29 PM
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Join Date: Jun 2011
Location: Houston, TX
Posts: 405
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I'll try to get and post some photos of the sheared bolt, strut, socket, etc. I didn't notice any wobble at all. Generally I'm able to land on the mains and briefly hold the nosewheel off. Less than 10% grass field ops.
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flytoday
RV7A - purchased flying 05/2020
RV6A - purchased flying 07/2011
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Last edited by flytoday : 02-09-2014 at 05:32 PM.
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02-09-2014, 05:43 PM
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Join Date: Jan 2005
Posts: 626
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Quote:
Originally Posted by flytoday
I recovered the sheared bolt and a washer from under the plane. Bolt end had the nut still on it. I might be able to informally get a lab to examine the failure plane. No prior shopping cart wobble.
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So the "headless" bolt with nut still on was found out of the hole - it fell out?
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02-09-2014, 06:49 PM
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Join Date: Jan 2005
Location: Kansas
Posts: 384
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With concern for the wear on both the NLG bolt and the hole thru the fitting I removed mine a couple of months ago during the conditional inspection. With over 325 hours my bolt and fitting still looked like new. This was accomplished in less than an hour and I'll probably inspect this more often since it is easier to replace a worn bolt instead of a damaged mount due to a worn bolt.
Last edited by curtis : 02-09-2014 at 06:59 PM.
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02-09-2014, 06:57 PM
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Join Date: Aug 2010
Location: Marshall TX (KASL)
Posts: 1,783
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Contact Vans. They might be interested in doing metallurgical tests. Maybe a bad bolt?
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02-09-2014, 07:05 PM
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Join Date: Jun 2011
Location: Houston, TX
Posts: 405
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Quote:
Originally Posted by mikehoover
So the "headless" bolt with nut still on was found out of the hole - it fell out?
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I found what looked like part of a bolt, with a nut on it, and a washer on the taxiway right under my engine. I'll assume it fell from my plane.
I'm not a builder, pretty ignorant to the internal structures, so since then I'm learning that it isn't just a simple bolt through a hole.
Carl
__________________
flytoday
RV7A - purchased flying 05/2020
RV6A - purchased flying 07/2011
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02-10-2014, 05:42 AM
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Join Date: Jun 2011
Location: Houston, TX
Posts: 405
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Bolt under engine
Zoomed in on the right edge of the picture, here's the bolt on the taxiway...
Carl
__________________
flytoday
RV7A - purchased flying 05/2020
RV6A - purchased flying 07/2011
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02-10-2014, 06:24 AM
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Join Date: Jan 2005
Location: Yukon Ok
Posts: 106
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Stronger bolt
May be a good application for a titanium bolt from Doug's new advertiser!
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Jerry Calvert
Yukon Ok
RV6 N296JC
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02-10-2014, 07:02 AM
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Join Date: Aug 2011
Location: Jeffersonville, IN
Posts: 391
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If you get a good closeup picture of the break we can fairly easily see if a crack existed prior.
1 Common way bolts break is they get loose, slop, etc followed by sudden load.
We can calculate shear load force fairly easy with diameter and material type. Not a hard calculation at all.
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Jeff Scott
RV9A First Flight 9/30/19
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