> Date: Wed, 6 Jan 2016 03:30:13 -0600
>> To: krnet at list.krnet.org
>> Subject: Re: KR> Aileron spar
>> From: krnet at list.krnet.org
>> CC: ppaulvsk at aol.com
>>
>> Why is the hinge binding? Holes misaligned and putting the hinge in a b
Pete,
As others stated, you can easily fix by shimming or sanding to square it up.
If you shim, then just fill with micro above the hinge to make it disappear in
the finish.?Once the plane is finished and flying, small details like that are
quickly forgotten.
?
-Jeff Scott
> The holes aren'
Pete Klapp wrote:
>The holes aren't misaligned, but there is about a 1/32+ bow in the aileron
>spar that is causing the bind.
If shims are not an option, filing a little off of each offset part of
the hinge in several adjacent locations near the bow ought to fix it
pretty easily. There's no suc
The holes aren't misaligned, but there is about a 1/32+ bow in the aileron spar
that is causing the bind.
Pete
> Date: Wed, 6 Jan 2016 03:30:13 -0600
> To: krnet at list.krnet.org
> Subject: Re: KR> Aileron spar
> From: krnet at list.krnet.org
> CC: ppaulvsk at aol.co
Subject: Re: KR> Aileron spar
The holes aren't misaligned, but there is about a 1/32+ bow in the aileron
spar that is causing the bind.
Pete
e options
-4705
Original message From: Pete Klapp via KRnet Date: 1/6/2016 11:02 AM (GMT-06:00) To: krnet at
list.krnet.org Cc: Pete Klapp Subject: Re: KR> Aileron
spar
The holes aren't misaligned, but there is about a 1/32+ bow in the aileron spar
that is causing the bind.
Pete
>
Why is the hinge binding? ?Holes misaligned and putting the hinge in a bend. I
would just redrill the hinge If so. Remember, keep it simple.?
Paul Visk?Belleville Il?618-406-4705
Netters
Have some difficulty with the aileron spars that I have floxed into the wing
(Diehl RAF-48 skins). Thoug
Klapp
> Date: Sun, 3 Jan 2016 14:11:37 -0600
> To: krnet at list.krnet.org
> Subject: Re: KR> Aileron spar
> From: krnet at list.krnet.org
> CC: flesner at frontier.com
>
> At 12:54 PM 1/3/2016, you wrote:
> >I saw that potential clearance issue with the hinge & an
some small patches with two layers of glass to
cover the holes. With a minimum amount of filler and sanding you could
not tell that I cut the holes.
Original Message
Subject: Re: KR> Aileron spar
From: Paul VISK via KRnet
List-Post: krnet@list.krnet.org
Date: Tue, January 05
At 07:16 AM 1/5/2016, you wrote:
>I think it has been proven that they work on belly boards going 130
>mph and they don't fall off.
++
One thing to consider. If I read Mark's post correctly, his belly
board screws are 3/4" long
Someone mentioned click bond nut plates earlier...I love them...I call them
out on dispositions whenever replacing the rivets is impractical. The
rubber plugs are intended to hold the proper pressure while the adhesive
cures...works great on sheet metal...then pulled out. Click bonds are
expensiv
Paul Visk wrote:
>>The point I was trying to make was. What's wrong with using wood screws on
>>the aileron hinges? Just curious. I think it has been proven that they work
>>on belly boards going 130 mph and they don't fall off. One think I can think
>>of. The plans call for Nut plates and gett
DAR might be an issue.
Being the ailerons are a primary flight control and the speed brake is
not.?Just a thought.
Paul Visk?Belleville Il618-406-4705
Original message From: Paul VISK via KRnet Date: 1/4/2016 9:09 AM (GMT-06:00) To: KRnet Cc: Paul VISK Subject: Re: KR>
53 AM (GMT-06:00) To: KRnet Cc: Flesner Subject: Re: KR> Aileron
spar
>? Has anyone had a securement issue using #6
> wood screws on there belly boards??? Paul ViskBelleville
I would not use screws for
> Has anyone had a securement issue using #6
> wood screws on there belly boards?? Paul ViskBelleville
I would not use screws for attachment. I used a
piece of 1/4" foam to construct my belly board
with glass w
bject: Re: KR> Aileron
spar
At 12:54 PM 1/3/2016, you wrote:
>I saw that potential clearance issue with the hinge & angle too. I
>guess the angle could be trimmed a bit to give clearance.
++
T
and the clamped
on the angle to promote a super tight radius. Let dry 24 hours and then pop off
the angle.
Mike Sylvester
kr2s builder
Birmingham,AL.
Cell no.205-966-3854
> Date: Sun, 3 Jan 2016 14:11:37 -0600
> To: krnet at list.krnet.org
> Subject: Re: KR> Aileron spar
>
At 12:54 PM 1/3/2016, you wrote:
>I saw that potential clearance issue with the hinge & angle too. I
>guess the angle could be trimmed a bit to give clearance.
++
The drawing for the setup using the alumi
I saw that potential clearance issue with the hinge & angle too. I guess
the angle could be trimmed a bit to give clearance. The PIK-26 has full
span ailerons so travel is likely less than what a KR would need for
similar roll rate. Differential too, so less down aileron than up. I
would stagge
Chris;
Looking at the drawing of the hinge setup using a section of angle, I don't see
how the aileron gets very much downward travel. It looks like the aileron
hinge half hits the end of the metal angle, but even if it doesn't, the ends of
the two bolts will hit each other before the aileron
Haven't got there yet but I like this solution from the PIK-26, an angle
bolted to the aft spar & piano hinge riveted or bolted to that:
Chris
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I had a few nuts get blocked with resin and flox after attaching the aileron
spar to the wing. After the resin set I used a 3/32" drill bit to cut through
the bulk of the overfill then used a tap to clean out the threads. Minimal
amount of effort.
Dan Prichard
Portland Oregon
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