Today's Message Index:
----------------------
1. 07:17 AM - Re: Aluminum extrusion (Larry Martin)
2. 07:17 AM - Re: Rivets (pounding or squeezing) (RURUNY@aol.com)
3. 07:17 AM - Re: Fuel fitting leaks, Pipe thread sealant (Larry Martin)
4. 08:33 AM - Re: [Please Read] Matronics Email Server Upgrade... (Richard Hutson)
5. 09:29 AM - Re: Re: Possible group Insurance for 601XXX Owners (John Karnes)
6. 03:24 PM - Horiz Stab Question (Joe Kerr)
7. 03:41 PM - 3300 downthrust (Jeff Small)
8. 06:09 PM - Re: Horiz Stab Question (Don Mountain)
9. 06:16 PM - Engines for 601 XL (Don Mountain)
10. 06:34 PM - stabilizer front attach points (Brad Cohen)
11. 08:47 PM - stabilizer front attach points (Joe Kerr)
12. 09:33 PM - [Please Read] Matronics Email Server Upgrade Complete! (Matt Dralle)
Message 1
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Subject: | Re: Aluminum extrusion |
--> Zenith-List message posted by: "Larry Martin" <lrm@isp.com>
Since you are in Canada, you might check with the PegaStol people. My
PegaStol wings came with extruded struts, I don't know what grade they are,
but they ain't going anywhere.
Larry, N1345L www.angelfire.com/un/ch701
----- Original Message -----
From: "N5SL" <nfivesl@yahoo.com>
Subject: Re: Zenith-List: Aluminum extrusion
> --> Zenith-List message posted by: N5SL <nfivesl@yahoo.com>
>
> Hi Peter:
>
> I assume you are talking about extruded angle. Here in the States we have
to cut and bend .063 sheet or just use the 1/8" X 1/8" 6061-T6. I chose to
use the 1/8" angle on my 601XL. It's very strong and adds very little
weight. You should be able to find 1/8" angle by the boatload in Canada.
>
> Good luck,
>
> Scott Laughlin
> N5SL (reserved)
> www.cooknwithgas.com
> Wishing I was in Lakeland, Florida today.
>
> DO NOT ARCHIVE
>
> Peter Dolamore <petes15515@msn.com> wrote:
> Does ANYONE on the list know where I can get 3/4 x 3/4 x
> .062 6061 T6 extrusion in Ontario,
>
> ---------------------------------
>
>
> --
>
>
--
Message 2
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Subject: | Re: Rivets (pounding or squeezing) |
--> Zenith-List message posted by: RURUNY@aol.com
Keith,
I used a hand squeezer on all the trailing edges of wings, slats, flaperons,
elevator. Its advantage is consistancy. Once the squeezer is set up for
proper amount of squeeze every rivet will be exactly the same which is great for
looks. Its also much quicker than pulling rivets. I clecoed every other hole
and dropped a solid rivet in every other hole, squeezing took less than 3
minutes.
This works great with the normal yoke provided with a hand squeezer, the
spar might take a much bigger yoke which is much bigger bucks. A pneumatic
riveter will come in handy when you do the flaperon and elevator bellcranks.
Brian
What are the advantages/disadvantages of either pounding rivets
or using a squeezer, as I am getting ready to build my spars (CH701).
Message 3
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Subject: | Re: Fuel fitting leaks, Pipe thread sealant |
--> Zenith-List message posted by: "Larry Martin" <lrm@isp.com>
Loctite 592 is what you need, it is a Teflon based sealant made for the job.
Larry, N1345L www.angelfire.com/un/ch701
----- Original Message -----
From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com>
Subject: RE: Zenith-List: Fuel fitting leaks, Pipe thread sealant
> --> Zenith-List message posted by: "Hinde, Frank George (Corvallis)"
<frank.hinde@hp.com>
>
> I think pro seal is not really intended for threads.
>
> I used teflon based thread sealant for plumbing fixtures from the
> hardware store (says it works with all fuels). Never had a leak in 6
> years.
>
> Frank
>
> -----Original Message-----
> From: owner-zenith-list-server@matronics.com
> [mailto:owner-zenith-list-server@matronics.com] On Behalf Of
> ruruny@aol.com
> To: zenith-list@matronics.com
> Subject: Zenith-List: Fuel fitting leaks, Pipe thread sealant
>
> --> Zenith-List message posted by: ruruny@aol.com
>
> Recently I made a post that Permatex high temperature thread sealant
> worked on sealing the threads for the fingerscreen and the hose nipple
> that screws into the fingerscreen. I take it back and hope no one has
> used this stuff. I leaked checked both tanks for my left wing this week
> by simply filling them up full with gas and letting them sit for a
> while. I
>
>
> --
>
>
--
Message 4
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Subject: | Re: [Please Read] Matronics Email Server Upgrade... |
--> Zenith-List message posted by: "Richard Hutson" <rhutson@midsouth.rr.com>
I second the best of luck, Matt
Subject: Zenith-List: [Please Read] Matronics Email Server Upgrade...
>
>
>
>
>
Message 5
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Subject: | Re: Possible group Insurance for 601XXX Owners |
Seal-Send-Time: Sun, 17 Apr 2005 09:25:52 -0700
--> Zenith-List message posted by: "John Karnes" <jpkarnes2000@msn.com>
Please put my name on your list. thanks.
John Karnes
N601JK
----- Original Message -----
From: Jeffrey Glasserow<mailto:jeffglass@starband.net>
To: zenith-list@matronics.com<mailto:zenith-list@matronics.com>
Sent: Thursday, April 14, 2005 5:43 AM
Subject: Zenith-List: Re: Possible group Insurance for 601XXX Owners
--> Zenith-List message posted by: "Jeffrey Glasserow" <jeffglass@starband.net<mailto:jeffglass@starband.net>>
Given the fact that many in this group are at Sun & Fun this wekk I'll post
this next week as well.
If you're interested in participating in a group insurance scheme, send me a
note and I'll put your name on a list.
Once I get a sizable list together I'll approach a few of the big
underwriters to see if they're interested in writing a group policy.
Jeff Glasserow
Ch 601 HDS
N6384E
Message 6
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Subject: | Horiz Stab Question |
--> Zenith-List message posted by: "Joe Kerr" <kerrjf@charter.net>
A couple of builders have noted on their web sites that the ends of the horizontal
stab are bowed inward slightly because the four center-most ribs are installed
on top of the spar doublers, but the doubler does not extend all the way
to the end of the spar. This leaves the third rib from the center on each side
drawing the spar inward because it is not installed on top of spar doublers,
so the fore-aft span is shorter. The rivet line of the skin needs to take this
into consideration or else the rivets may end up too close to the spar flange
bend, if I understand the problem correctly. I am just wondering how many
of you altered your rivet line to account for the slight bowing of the spar, OR
have any of you inserted a shim between the ribs or spar, OR is it really no
big deal either way and you ignored the bow and all the rivet placements worked
even with a straight rivet line?
-Joe
Message 7
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Seal-Send-Time: Sun, 17 Apr 2005 18:38:26 -0400
--> Zenith-List message posted by: "Jeff Small" <zodiacjeff@msn.com>
Jim,
I have just hung my engine on my 601XL. It is nose down by 2 degrees when
measured between the top of the engine and the lingering. Is that normal?
+++ Very normal. If you want to get rid of some AFTER test flights you can make
C-shaped washers out of .063 or .090 aluminum and slip 'em in between the bottom
mount pads and the firewall. You won't have to disassemble anything, just
loosen the bottom nuts. Make them a bit bigger than the engine mount pads and
safety 'em.
+++ This is another "cure" for you guys who think you have to realign the stab
because you need a bit too much up trim (in cruise) as it takes out a bit of the
downthrust.
regards jeff HDS/3300 235 hours
Message 8
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Subject: | Re: Horiz Stab Question |
--> Zenith-List message posted by: Don Mountain <mountain4don@yahoo.com>
I am not sure if this is the same problem, but I had a
similar problem with the rear spar bowing in when I
strapped the skin down with the blocks on the rear
spar to keep the straps from bending down the skin.
The force on these blocks buckled the ribs out of
line, and bowed the rear spar. So what I did was cut
blocks of wood that just fit inside the ribs on each
side, and gave the correct spacing from the front to
rear spars. I bolted these through holes already
drilled in the ribs to clamp the rib webs straight.
Then I strapped the skin down and the webs of the ribs
didn't buckle, maintaining the spar spacing with the
straps in place. And everything on my stabilizer
drilled and clamped up straight.
Don
601 XL
tail done, working on wings.
> A couple of builders have noted on their web sites
> that the ends of the horizontal stab are bowed
> inward slightly because the four center-most ribs
> are installed on top of the spar doublers, but the
> doubler does not extend all the way to the end of
> the spar. This leaves the third rib from the center
> on each side drawing the spar inward because it is
> not installed on top of spar doublers, so the
> fore-aft span is shorter.
__________________________________
Message 9
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Subject: | Engines for 601 XL |
--> Zenith-List message posted by: Don Mountain <mountain4don@yahoo.com>
I am working on the wings of my 601 XL, and starting
to think about engines. Flying a Piper Cherokee with
a Lycoming that looks like an antique out of the dark
ages, I have been thinking of something a little more
modern. I know a lot of people have tried various car
engines, like Volkswagon, Corvair, Sabaru, and a few
others. And of course the non-certified airplane
engines from Jabaru and Rotax. All of these seem
either expensive, old or exotic here in the midwestern
United States. The designs for the Volkswagon and
Corvair engines are more than 30 years old now, so I
consider that rather antique.
So the question is, has anybody tried something a
little more common and modern in design for their
airplane. Something designed and built within the
last 5 years, but common enough to be easy to get and
still get parts at the local dealer?
I was looking at the engine in my wife's 2003
Chevrolet Cavalier the other day, and wondered if
anybody had tried one of those. Its a double overhead
cam engine, thats all aluminum, and fuel injected that
takes regular fuel and seems to run real good and
smooth. And it looks pretty lightweight. Probably
some of the other manufactures have similar engines
that are plentiful in the junk yards or from a dealer
brand new. I wonder what kind of design problem there
would be installing one of these in a plane? It would
be nice to use the same oil filter in the car and
plane. Or if I needed spare parts, I could borrow
them from my wife's car?
Don
601 XL
tail done, working on wings
Message 10
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Subject: | stabilizer front attach points |
Seal-Send-Time: Sun, 17 Apr 2005 21:31:49 -0400
--> Zenith-List message posted by: "Brad Cohen" <bradfnp@msn.com>
I just made the first (of many) mistakes on the stabilzer and I was wondering
if anyone else has had a similar problem;
I measured the 233mm measurement for the front spar attachment, cut the plywood
blank and mounted both pieces of 6t2-2.
Once I drilled the holes for both 6t2-2 I realized that those rivet holes were
too close to the inside bend radius of 6t2-2 which put the corresponding rivets
in 6t2-1 right next to the edge, which of course was much less than the specified
10mm for edge distance. I will order new 6t2-2 fron ZAC but I don't know
where I measured incorrectly. I rechecked the plywood blank and it is indeed
233mm. I remeasured the placement of both 6t2-1 and 6t2-2 without the plywood
(I measured both equidistant fron centerline and also from the end of the spar
itself) and I think I have it about right now, the edge distance on 6t2-1 is
now ~8-9mm and almost the same for 6t2-2.
how accurate does this measurement have to be? I am +/- 1-1.5 mm as it is now,
before adding the new pieces which I will order this week. Any thoughts? has
anyone else had similar problems with spacing of the front attach points or am
I just going nuts????
Do not archive
Brad Cohen
6-5803
N969BC (reserved)
Message 11
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Subject: | stabilizer front attach points |
--> Zenith-List message posted by: "Joe Kerr" <kerrjf@charter.net>
Brad-
I mounted 6T2-1 and 6T2-2 two weeks ago and didn't run into the same problem.
I have 8mm edge distance on 6T2-2 and 10mm on 6T2-1. The 233mm wooden spacer
is a recent plans revision (2/05), the plans from 12/04 call for a wooden spacer
of 219mm. If you have a pre-drilled spar, perhaps you have the earlier version
that is drilled for the 12/04 spacing.
Joseph Kerr
#5860
Reno, NV
Message 12
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Subject: | [Please Read] Matronics Email Server Upgrade Complete! |
--> Zenith-List message posted by: Matt Dralle <dralle@matronics.com>
9:24pm PDT 4/17/2005
Dear Listers,
The upgrade of the Matronics Email Server can be considered complete at
this time. All known issues related to the upgrade process have been
resolved and email services are running normal. The Nightly Digest
processing has not yet been tested and will wait for tonight's update.
If you encounter any odd behavior with respect to the Matronics Email
Server over the next few days, please contact me via email at
dralle@matronics.com or if that fails try dralle@speakeasy.net.
Thanks to everyone for being patient through this arduous process of a
major system upgrade!
Matt Dralle
Email List Administrator
At 12:37 PM 4/16/2005 Saturday, Matt Dralle wrote:
>Dear Listers,
>
>I will be upgrading the Matronics Email Server this weekend. This
>includes some hardware improvements - more memory, faster, more capable
>processors - as well as a complete operating system upgrade from
>scratch. I hope to have both the old system and the new system running at
>the same time to minimize the actual impact of the upgrade.
>
>Hopefully there will be little actual downtime during the transition, but
>a few posts may get lost in the shuffle. If you don't see your post show
>up on the List in the normal amount of time (plus a little bit), then
>please just try posting it again.
>
>Upgrading the Matronics Email Server operating system (from Redhat Linux
>7.2 to Redhat Linux WS 4) is a sizeable undertaking and requires a great
>deal of work to port all of the utilities, programs, and scripts over to
>the new system. As I've already mentioned, both the old and new systems
>will be on line at the same time, so interruption should be held to an
>absolute minimal. You might see a couple of odd test messages during the
>cut-over or other odd messages; please just ignore them.
>
>I have setup a new System Status Web Page that I will use to update List
>Members on the current status of the email and web systems. Please refer
>to it as often as you like:
>
> http://www.matronics.com/SystemStatus/
>
>
>Thank you for your continued support of the List Services at
>Matronics! Its your yearly Contributions that make these major upgrades
>possible!
>
>Best regards,
>
>Matt Dralle
>Matronics Email List Administrator
Matt G Dralle | Matronics | PO Box 347 | Livermore | CA | 94551
925-606-1001 V | 925-606-6281 F | dralle@matronics.com Email
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