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aft wing spar

 
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cjhukill(at)cox.net
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PostPosted: Sat Jan 30, 2010 7:32 am    Post subject: aft wing spar Reply with quote

I have tried and tried to find mention in the plans for the procedure for countersinking or dimpling the aft spar flange for the lower skin. I called Vans and was told to do it using standard procedures which was to dimple, then countersink to get the required amount of depth to accept the skins. I was also told that the plans don't specify that procedure for the QB, because back in the plans where the other skins are attached in the Philippines, that procedure is specified, and I am supposed to review all that previous work, step by step, as I'm the manufacturer, not some QB'er. I humbly agreed, and went back AGAIN to review the wing plans step by step, and still couldn't find it (it's probably there, I just couldn't find it). Anyway, I don't remember ever using that procedure, dimple then countersink, on this project or the RV8 I built. Reviewing chapter 5, we're told to dimple up to a certain thickness, then beyond that , countersink, just as I remember. Screw it, I'll drill out a QB installed rivet on the inboard skin, and see what they did. Viola, it's countersunk, just as what I'd expect. So that's what I plan on doing to the rest of this .060 spar flange, countersink it. Anyone have any info on this, that I can't find.
Chris Hukill
Frustrated, but at least not covered in fiberglass dust.
[quote][b]


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ricksked(at)cox.net
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PostPosted: Sat Jan 30, 2010 8:01 am    Post subject: aft wing spar Reply with quote

YOU'RE not covered in YOUR fiberglass dust....I'm covered in YOUR fiberglass dust!!! :)Rick SkedN246RSDo not archive
Sent via BlackBerry by AT&TFrom: "Chris Hukill" <cjhukill(at)cox.net>
Date: Sat, 30 Jan 2010 07:31:48 -0800
To: <rv10-list(at)matronics.com>
Subject: RV10-List: aft wing spar

I have tried and tried to find mention = in the plans=20 for the procedure for countersinking or dimpling the aft spar flange for = the=20 lower skin. I called Vans and was told to do it using standard = procedures which=20 was to dimple, then countersink to get the required amount of depth to = accept=20 the skins. I was also told that the plans don't specify that procedure = for the=20 QB, because back in the plans where the other skins are attached in the=20 Philippines, that procedure is specified, and I am supposed to review = all that=20 previous work, step by step, as I'm the manufacturer, not some  = QB'er. I=20 humbly agreed, and went back AGAIN to review the wing plans step by = step, and=20 still couldn't find it (it's probably there, I just couldn't find it). = Anyway, I=20 don't remember ever using that procedure, dimple then countersink, on = this=20 project or the RV8 I built. Reviewing chapter 5, we're told to dimple up = to a=20 certain thickness, then beyond that , countersink, just as I remember. = Screw it,=20 I'll drill out a QB installed rivet on the inboard skin, and see what = they did.=20 Viola, it's countersunk, just as what I'd expect. So that's what I plan = on doing=20 to the rest of this .060 spar flange, countersink it. Anyone have any = info on=20 this, that I can't find.
Chris Hukill
Frustrated, but at least not covered in = fiberglass=20 dust.
[quote][b]


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