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Simple rivet test/unzip
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n85ae



Joined: 14 Mar 2007
Posts: 403

PostPosted: Fri Dec 12, 2008 7:50 pm    Post subject: Simple rivet test/unzip Reply with quote

This evening ...

I took two pieces of .025 500mm long, riveted them with A4's at 40mm
pitch. clamped the end of one in a vice, and grabbed the other piece
with a pair of vice grips. One sharp tug unzipped the entire strip with
very little effort .... Every single rivet head popped right off like butter.

Riveted with the zenith hand riveter and zenith concave head.

Food for thought.

Regards,
Jeff


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PostPosted: Fri Dec 12, 2008 9:58 pm    Post subject: Simple rivet test/unzip Reply with quote

What new gussets?

At 09:48 PM 12/12/2008, you wrote:

Quote:
add the new "triangle and house aileron gussets," use A5 SS rivets
on the gussets and try that again...


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PostPosted: Fri Dec 12, 2008 10:48 pm    Post subject: Simple rivet test/unzip Reply with quote

Thanks Sabrina,

Do you think the rest of us should consider adding these gussets? Do
they apply equally to hingeless or hinge type ailerons?

I still can't quite imagine exactly what these gussets do or where
they go. Which rivets on the aileron can unzip? The Hinge area? On the ribs?

Thanks,

Paul
XL getting close
At 10:18 PM 12/12/2008, you wrote:
Quote:
I designed my aileron gussets in January, they were/are external,
6061-T6 and .060 w/A5 SS rivets.

They were my response to the unzipping of 601 ailerons in light of
an examination of in-flight video by myself, my IA and my test
pilot. The inboard one looks like a triangle, the next outboard,
like a house.

Zenith has incorporated similar ones on the 650, I am told they are
internal and thinner. I know some builders have ordered them and
installed them on their 601s. Zenith has their own reasons for the
design change.


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PostPosted: Sat Dec 13, 2008 7:22 am    Post subject: Simple rivet test/unzip Reply with quote

Jeff, when you tugged on the strip, what angle were your tug with the clamped piece? Or, was the rivet in shear or tension. Would expect the rivet heads to pop off if your tug was 90 degrees to the clamped part but if it was 180 degrees then there is a problem. Jerry of Ga DO NOT ARCHIVE

In a message dated 12/12/2008 10:52:33 P.M. Eastern Standard Time, n85ae(at)yahoo.com writes:
Quote:
--> Zenith601-List message posted by: "n85ae" <n85ae(at)yahoo.com>

This evening ...

I took two pieces of .025 500mm long, riveted them with A4's at 40mm
pitch. clamped the end of one in a vice, and grabbed the other piece
with a pair of vice grips. One sharp tug unzipped the entire strip with
very little effort .... Every single rivet head popped right off like butter.

Riveted with the zenith hand riveter and zenith concave head.

Food for thought.

Regards,
Jeff


Read this topic online here:

http://forums.matronics.com/viewtopic.php?p=219159#219159


One site keeps you connected to all your email: AOL Mail, Gmail, and Yahoo Mai=emlcntaolcom00000019">The NEW AOL.com.
[quote][b]


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PostPosted: Sat Dec 13, 2008 8:12 am    Post subject: Simple rivet test/unzip Reply with quote

It's Saturday, which means Zenith is closed, and I'mn trying to identify a
part. Can any of you help me on this?

The part in question are the AS5 rivets. Where are they likely to be packed?
Are they identified specifically as AS5 rivets, or ?

TIA.

--
==============================================
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=================================================
Jim B. Belcher
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A&P/IA
Instrument Rated Pilot
General Radio Telephone Certificate
=================================================


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PostPosted: Sat Dec 13, 2008 8:45 am    Post subject: Simple rivet test/unzip Reply with quote

Mine in a small ziplock plastic bag maybe 1" x 3" Label written in marker on bag

On Sat, Dec 13, 2008 at 11:13 AM, Jim Belcher <Z601(at)anemicaardvark.com (Z601(at)anemicaardvark.com)> wrote:
[quote]--> Zenith601-List message posted by: Jim Belcher <Z601(at)anemicaardvark.com (Z601(at)anemicaardvark.com)>

It's Saturday, which means Zenith is closed, and I'mn trying to identify a
part. Can any of you help me on this?

The part in question are the AS5 rivets. Where are they likely to be packed?
Are they identified specifically as AS5 rivets, or ?

TIA.

--
==============================================
Those who can, do. Those who can't, sue.
=================================================
Jim B. Belcher
BS, MS Physics, math, Computer Science
A&P/IA
Instrument Rated Pilot
General Radio Telephone Certificate
=================================================




[b]


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PostPosted: Sat Dec 13, 2008 9:17 am    Post subject: Simple rivet test/unzip Reply with quote

As I am just finishing the wings, could someone at least describe the positioning of the aileron gussets? I'm too dense to visualize! Thanks.

Terry Turnquist
601XL-Plans
St. Peters MO

Sabrina <chicago2paris(at)msn.com> wrote:[quote] --> Zenith601-List message posted by: "Sabrina"

I would rely upon Zenith and install their gussets per their specifications. CH knows what he is doing. If anyone has the new plans, maybe they could describe the 650 versions. The AMD safety alert seems to talk to this issue:
http://www.newplane.com/Service_Letters_Bulletines/SAFETY_ALERT_october_29_2008.pdf


Read this topic online [quote][b]


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Tim Juhl



Joined: 21 Mar 2006
Posts: 488
Location: "Thumb" of Michigan

PostPosted: Sat Dec 13, 2008 9:19 am    Post subject: Re: Simple rivet test/unzip Reply with quote

Did anyone ever determine how many of the aircraft that experienced wing loss in flight had hinged ailerons? Could it be that the hingeless design is less prone to the problems that are currently the focus of investigators?

Sabrina, do you have any pictures of your installed aileron gussets?

Tim


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PostPosted: Sat Dec 13, 2008 9:38 am    Post subject: Simple rivet test/unzip Reply with quote

On Saturday 13 December 2008 10:45, Cndmovn wrote:
Quote:
Mine in a small ziplock plastic bag maybe 1" x 3" Label written in marker
on bag
Thanks! Armed with that information, I found them. You likely saved me an hour

or two of fumbling, as I had no idea what size container I should seek.
--
==============================================
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=================================================
Jim B. Belcher
BS, MS Physics, math, Computer Science
A&P/IA
Instrument Rated Pilot
General Radio Telephone Certificate
=================================================


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PostPosted: Sat Dec 13, 2008 6:33 pm    Post subject: Simple rivet test/unzip Reply with quote

I checked Zenith website and they added (for the 650) a gusset to Rib 1 & 2.
The stated reason was to reduce possible buckling when tied down in wind
gusts.

Randy
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n85ae



Joined: 14 Mar 2007
Posts: 403

PostPosted: Sun Dec 14, 2008 9:12 am    Post subject: Re: Simple rivet test/unzip Reply with quote

Well, my test was VERY unscientific, however ...

You are right, it was essentially in tension. But, the heads tear off so
easily, I was very unhappy. I repeated my simple test with A5's, and the
ball end pulls through, but the heads do not pop off. This to my mind
is ok. The rivets themself don't just break in half.
Regards,
Jeff

Jeyoung65(at)aol.com wrote:
Jeff, when you tugged on the strip, what angle were your tug with the clamped piece? Or, was the rivet in shear or tension. Would expect the rivet heads to pop off if your tug was 90 degrees to the clamped part but if it was 180 degrees then there is a problem. Jerry of Ga DO NOT ARCHIVE


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ashontz



Joined: 27 Dec 2006
Posts: 723

PostPosted: Tue Dec 16, 2008 6:55 am    Post subject: Re: Simple rivet test/unzip Reply with quote

Without looking at my plans, doesn't the wing call for A5 rivets anyway?

n85ae wrote:
Well, my test was VERY unscientific, however ...

You are right, it was essentially in tension. But, the heads tear off so
easily, I was very unhappy. I repeated my simple test with A5's, and the
ball end pulls through, but the heads do not pop off. This to my mind
is ok. The rivets themself don't just break in half.
Regards,
Jeff

Jeyoung65(at)aol.com wrote:
Jeff, when you tugged on the strip, what angle were your tug with the clamped piece? Or, was the rivet in shear or tension. Would expect the rivet heads to pop off if your tug was 90 degrees to the clamped part but if it was 180 degrees then there is a problem. Jerry of Ga DO NOT ARCHIVE


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PostPosted: Tue Dec 16, 2008 9:35 am    Post subject: Simple rivet test/unzip Reply with quote

unzip - a classic failure mode once the initial fastener fails and the structure goes into buckling.

David L. Downey
Harleysville (SE) PA, USA


--- On Tue, 12/16/08, Sabrina <chicago2paris(at)msn.com> wrote:
[quote]From: Sabrina <chicago2paris(at)msn.com>
Subject: Re: Simple rivet test/unzip
To: zenith601-list(at)matronics.com
Date: Tuesday, December 16, 2008, 11:36 AM

[quote]--> Zenith601-List message posted by: "Sabrina"
<chicago2paris(at)msn.com>

"Without looking at my plans, doesn't the wing call for A5 rivets
anyway?" Ashontz...

A4 for the aft portion of the aileron piano hinge....

A4 are rated at 165/230 pounds,

A5 are [quote][b]


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PostPosted: Tue Dec 16, 2008 11:43 am    Post subject: Simple rivet test/unzip Reply with quote

No sure about other 601 plans but the 601HD 6-V-10 drawing dated 06-04 has
"AN Rivet pitch 40" in the view for the Piano Hinged Aileron Option and for
the hingless aileron "A4 rivets pitch 40 last I/B - O/B rivet use A5". It
does not say what size AN rivets to use on the hinged system. Jerry of Ga


In a message dated 12/16/2008 11:37:02 A.M. Eastern Standard Time,
chicago2paris(at)msn.com writes:



"Without looking at my plans, doesn't the wing call for A5 rivets anyway?"
Ashontz...

A4 for the aft portion of the aileron piano hinge....

A4 are rated at 165/230 pounds,

A5 are rated at 255/375 pounds,

AS5 are rated at 750/1000 pounds. Correct?

When the force is upward tension at one end, as opposed to shear across all
the rivets in a row, does the full row of rivets give much support to the end
rivet being tensioned, or once a tension of 1X to 2X of an A4 is reached and
maintained, the connection will unzip? (Versus a shearing force across a
row where each rivet adds strength to the connection and the force would have
to be many times the shear limit of any one rivet for the connection to fail.)


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PostPosted: Tue Dec 16, 2008 11:46 am    Post subject: Simple rivet test/unzip Reply with quote

Hi Sabrina,

I just flew N130AW an AMD 601XL at The Flight school of Gwinnet (LZU)
and it had the same kink in the ailerons. According to the mechanic they
had showed photo's of the issue to the factory and they said it was
nothing to worry about. That plane has a bit less than 200 hrs and has
been in service for less than 2 yrs.

So it seems like it may not be such an uncommon situation as Zenith led
you to believe.

Can you post a picture or drawing of the gussets you installed ?

John Davis
N601JD
601XL - Jab 3300
Finally ready for first flight

Sabrina wrote:
Quote:


My test pilot noticed flexing at the inboard portion of the ailerons where Alex's kink is. We did not know of Alex's kink at the time and did not think too much of it. This was on the maiden flight, 11 months and 1 day ago. However, once this video was reviewed by my IA before the next test flight:

http://www.youtube.com/watch?v=r-ZcZPP18uk

My IA noted the movement as well, and also noted the stress created at the point the rear spar connects the inboard-forward corner of the aileron.

Zenith indicated we were the first to raise the issue. Zenith was informed that I had designed gussets and that they were or were about to be installed. Zenith proceeded to link to my videos from their web page. No mention was made of the internal 650 gussets to me at AirVenture and the exact issue was not raised again until a former European Zenith distributor raised a similar issue (which I can't talk about) recently in an e-mail, a person privy to the letter recently sent to CH by the European authorities. I have not seen the letter (some have asked off line.)

The flexing, which was most pronounced on the down aileron, has not re-occured since installing the four gussets.

Any opinions about the Hoerner wing tip sending air down or into the channel created by the aileron/spar gap, any opinions on whether the unsealed aileron hinge would amplify this effect, if any? http://www.zenithair.com/zodiac/6-design.html

The Germans did not impose a 111 MPH Vne for no reason at all, the left lane of the Autobahn would be quicker...

Does anyone remember if the Factory Demonstrator has PH ailerons or not?


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PostPosted: Tue Dec 16, 2008 4:11 pm    Post subject: Simple rivet test/unzip Reply with quote

I must have missed the location for the gussets. Would someone please help me out and give me some info on there design and location. Drawings?

Victor Kidd
N922VK
Would be fying except for the present WV weather.

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Tim Juhl



Joined: 21 Mar 2006
Posts: 488
Location: "Thumb" of Michigan

PostPosted: Tue Dec 16, 2008 5:09 pm    Post subject: Re: Simple rivet test/unzip Reply with quote

Sabrina,

The red & white factory demonstrator had hingeless ailerons.

I have been communicating with a friend who is going the 650 route and he advised me that the gussets are 0.025 aluminum and slipped between the skin and the rib. They are installed using A4 rivets.

Stated reason is to prevent damage due to flapping in the wind when the aircraft is parked outside. Caleb commented it was more of a problem with piano hinge ailerons inasmuch that the hingeless type offer more resistance to deflection.

Tim


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PostPosted: Tue Dec 16, 2008 6:02 pm    Post subject: Simple rivet test/unzip Reply with quote

I would have but the factory won't sell me (their registered builder) the 650 upgrade. (whine, sniffle)

David L. Downey
Harleysville (SE) PA, USA


--- On Tue, 12/16/08, Sabrina <chicago2paris(at)msn.com> wrote:
[quote]From: Sabrina <chicago2paris(at)msn.com>
Subject: Re: Simple rivet test/unzip
To: zenith601-list(at)matronics.com
Date: Tuesday, December 16, 2008, 7:36 PM

[quote]--> Zenith601-List message posted by: "Sabrina"
<chicago2paris(at)msn.com>

Does anyone have the 650 plans with the gussets shown?


Read this topic online [quote][b]


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PostPosted: Tue Dec 16, 2008 6:23 pm    Post subject: Simple rivet test/unzip Reply with quote

Wow, did you to something to make them mad? Mine just came via UPS. You should be able to get them if ordered before the first of the year.
The gussets are about 100mm - 110mm on a side. They are on the first and second aileron ribs. A right triangle on the first and an isosceles with the tip cut off on the second.
There have been a lot of queries about the anti-oil canning angles. They are in line with the back of the wing locker and run parallel with the main spar.
Ron

On Dec 16, 2008, at 8:59 PM, David Downey wrote:
[quote]I would have but the factory won't sell me (their registered builder) the 650 upgrade. (whine, sniffle)

David L. Downey
Harleysville (SE) PA, USA


--- On Tue, 12/16/08, Sabrina <chicago2paris(at)msn.com (chicago2paris(at)msn.com)> wrote:
Quote:
From: Sabrina <chicago2paris(at)msn.com (chicago2paris(at)msn.com)>
Subject: Re: Simple rivet test/unzip
To: zenith601-list(at)matronics.com (zenith601-list(at)matronics.com)
Date: Tuesday, December 16, 2008, 7:36 PM

Quote:



Quote:

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PostPosted: Tue Dec 16, 2008 7:01 pm    Post subject: Simple rivet test/unzip Reply with quote

I haven't looked at the existing plans (not that far along) but angle
of the front spare is 83 degrees (where 0 is horizontal and 90 is
vertical), leaning forward. This is measured where the top longeron
is level.

Without really studying them, I think the new plans are easier to
read. Looks to me like there are more drawings and they are better
annotated. This alone make the upgrade cost worth it to me.

Ron

On Dec 16, 2008, at 9:36 PM, Sabrina wrote:

Quote:

<chicago2paris(at)msn.com>

Is the main spar set the same as the 601XL?

In other words, do they just twist the wing to bring it down two
inches in the rear, or have they adjusted the main spar and side
skin cut outs too?


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