Today's Message Index:
----------------------
1. 04:31 AM - Just a mile stone for me! (4RCSIMMONS@comcast.net (Rich Simmons))
2. 06:36 AM - Re: Just a mile stone for me! (cookwithgas)
3. 08:41 AM - Re: Just a mile stone for me! (Lawrence Webber)
4. 09:27 AM - Re: Re: Sight gage ()
5. 10:50 AM - Re: Re: Sight gage (George Swinford)
6. 11:36 AM - Playing in Clouds (cookwithgas)
7. 12:30 PM - Re: Playing in Clouds (Gig Giacona)
8. 02:22 PM - Control Surface Flutter ()
9. 02:35 PM - Re: Control Surface Flutter (Gig Giacona)
10. 02:54 PM - Re: Control Surface Flutter (Carlos Sa)
11. 03:11 PM - Re: Re: Sight gage (Bill Naumuk)
12. 03:39 PM - Re: Playing in Clouds (ALAN BEYER)
13. 03:53 PM - Re: Re: Control Surface Flutter (Al Hays)
14. 05:07 PM - Re: Re: Sight gage (Bryan Martin)
15. 05:32 PM - Re: Annual Condition Inspection (Tommy Walker)
16. 06:36 PM - Re: Re: Sight gage (Bill Naumuk)
17. 07:30 PM - Re: Just a mile stone for me! (KEVINBONDS@comcast.net)
18. 07:46 PM - Re: Re: Sight gage (Al Hays)
19. 08:33 PM - Re: Re: Sight gage (Bryan Martin)
20. 09:11 PM - Re: Control Surface Flutter (MaxNr@aol.com)
21. 10:03 PM - Re: Re: Control Surface Flutter (steve)
22. 10:14 PM - Re: Playing in Clouds (TxDave)
Message 1
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| Subject: | Just a mile stone for me! |
Hey list,
I don't talk much and lately haven't been reading much. I still have to share this
with some one though!
After 3.5 years, I have my hull setting on wheels.
Yup! It's a milestone!!
My wings are 95% and tail empenages are ready to attach. I have actually placed
but not truly located the Horizonal Satbilizer. Looks like an airplane!
Shew! Still more to do. I hope I see an engine under my christmas tree thie year!!!!!
I am going to attatche and go through the fitment process of the wings and tail
components now while as mentioning before, "Asking Santa for my engine!"
I also have to decide my panel configutration. Suggestions?
If some of you wish, send me a picture of what you are doing with your panels.
I could help me decide.
Thanks,
Rich Simmons
Do not Archive!
--
Thanks,
Rich Simmons
<html><body>
<DIV>
<DIV>Hey list,</DIV>
<DIV> </DIV>
<DIV>I don't talk much and lately haven't been reading much. I still have to share
this with some one though!</DIV>
<DIV> </DIV>
<DIV>After 3.5 years, I have my hull setting on wheels.</DIV>
<DIV> </DIV>
<DIV>Yup! It's a milestone!!</DIV>
<DIV> </DIV>
<DIV>My wings are 95% and tail empenages are ready to attach. I have actually placed
but not truly located the Horizonal Satbilizer. Looks like an airplane!</DIV>
<DIV> </DIV>
<DIV>Shew! Still more to do. I hope I see an engine under my christmas tree thie
year!!!!!</DIV>
<DIV> </DIV>
<DIV>I am going to attatche and go through the fitment process of the wings and
tail components now while as mentioning before, "Asking Santa for my engine!"</DIV>
<DIV> </DIV>
<DIV>I also have to decide my panel configutration. Suggestions?</DIV>
<DIV> </DIV>
<DIV>If some of you wish, send me a picture of what you are doing with your panels.
I could help me decide.</DIV>
<DIV> </DIV>
<DIV>Thanks,</DIV>
<DIV>Rich Simmons</DIV>
<DIV> </DIV>
<DIV>Do not Archive!</DIV></DIV>
<DIV> </DIV>
<DIV class=signature id=signature>--<BR>Thanks, <BR>Rich Simmons</DIV></body></html>
Message 2
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| Subject: | Re: Just a mile stone for me! |
Congratulations Rich. I remember when I was at that point and it is a great feeling.
Keep plugging away and I'll see you flying soon.
Scott Laughlin
601XL/Corvair
Omaha, Nebraska
finished & Flying
107 hours
www.cooknwithgas.com
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p 0895#200895
Message 3
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| Subject: | Just a mile stone for me! |
Hey Rich if you get some layouts of panels how about sending on to me
im ready to start my panel layout steam gauges and basic needed instrument
s
Kiss is my motto
Larry Webber rhode island601xl corvair chugger
From: 4RCSIMMONS@comcast.netTo: zenith-list@matronics.comSubject: Zenith-Li
st: Just a mile stone for me! Date: Wed=2C 27 Aug 2008 11:29:41 +0000
Hey list=2C
I don't talk much and lately haven't been reading much. I still have to sha
re this with some one though!
After 3.5 years=2C I have my hull setting on wheels.
Yup! It's a milestone!!
My wings are 95% and tail empenages are ready to attach. I have actually pl
aced but not truly located the Horizonal Satbilizer. Looks like an airplane
!
Shew! Still more to do. I hope I see an engine under my christmas tree thie
year!!!!!
I am going to attatche and go through the fitment process of the wings and
tail components now while as mentioning before=2C "Asking Santa for my engi
ne!"
I also have to decide my panel configutration. Suggestions?
If some of you wish=2C send me a picture of what you are doing with your pa
nels. I could help me decide.
Thanks=2C
Rich Simmons
Do not Archive!
--Thanks=2C Rich Simmons
_________________________________________________________________
Be the filmmaker you always wanted to be=97learn how to burn a DVD with Win
dows=AE.
Message 4
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That will work. As already posted you can run the fuel line from the wing tanks
into the bottom inlet that you show blocked off. This will eliminate a T fitting.
Jerry
---- Bill Naumuk <naumuk@alltel.net> wrote:
> All-
> Like I said, all the header tanks seem to have different in/outs. The
> stupid arrangement I portrayed is what I got with my tank.
> Since I have two outlets at the bottom of the tank, one is apparently
> worthless.
> I'm guessing that the alternative is to put a T at the top inlet, block
> off one of the bottom, run the main to one side of the T at the top, and the
> sight gauge between the other side of the top T and the uncapped bottom.
> Sketch attached. Once again, waddya think?
> XL builders have NO IDEA what HD/HDS people are talking about!!! I
> imagine the new 650 series will be sold from vending machines. Bless you,
> fellow sufferers! If it weren't for you people, my project would have been
> beer cans long ago. Not that that's necessarily a bad thing.
> Bill
> ----- Original Message -----
> From: <jlatimer1@cox.net>
> To: <zenith-list@matronics.com>
> Sent: Tuesday, August 26, 2008 8:55 PM
> Subject: Re: Zenith-List: Re: Sight gage
>
>
> > Bill,
> > As several people have already pointed out your sight glass diagram will
> > not work. Gas will not get into the sight glass loop. You need to attach
> > the sight glass at the top and bottom of the tank.
> >
> > My 8 gallon header tank came with two barbed connections at the top, a
> > barbed connection near the bottom of the tank, and a threaded connection
> > at the bottom of the tank.
> >
> > I plumbed the sight glass between one of the top and the bottom barbed
> > connection. My wing tanks are plumbed to the other barbed connection at
> > the top of the tank. And the threaded connection at the bottom goes to
> > the engine.
> >
> > I've tried to attach the original documentation from Zenith on how to
> > plumb the wing tanks to header tank. It also shows the sight glass.
> >
> > Everyone building an XL should get a kick out of the documentation that we
> > got with our 601HDS kits.
> > Jerry
> > ---- Bill Naumuk <naumuk@alltel.net> wrote:
> >> Gig, and everyone with a sight gage-
> >> It seems that every 8 gal header tank was plumbed differently. I've
> >> attached a sketch of what I think the layout in my case should look like.
> >> I
> >> searched the archives and not a whole hell of a lot to go on. Whaddya
> >> think?
> >> Bill
> >> ----- Original Message -----
> >> From: "Gig Giacona" <wrgiacona@gmail.com>
> >> To: <zenith-list@matronics.com>
> >> Sent: Tuesday, August 26, 2008 5:51 PM
> >> Subject: Zenith-List: Re: Sight gage
> >>
> >>
> >> >
> >> > Basically a port at the bottom and one at the top of the side facing
> >> > the
> >> > panel put a clear tube between them. you will need to play with the
> >> > position of the tube so you get a good reading.
> >> >
> >> > --------
> >> > W.R. "Gig" Giacona
> >> > 601XL Under Construction
> >> > See my progress at www.peoamerica.net/N601WR
> >> >
> >> >
> >> >
> >> >
> >> > Read this topic online here:
> >> >
> >> > http://forums.matronics.com/viewtopic.php?p 0758#200758
> >> >
> >> >
> >> >
> >> >
> >> >
> >> >
> >> >
> >> >
> >> >
> >> >
> >
Message 5
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One concern about a fuel inlet on the bottom of the fuselage tank: If the
valve (or check valve in a fuel pump) leaks a little bit, all the fuel in
the fuselage tank will try to drain back into the wing tanks. With the
inlet in the top of the fuselage tank, only the small amount of fuel in the
line will leak back. This is the reason I felt it necessary to relocate the
inlet to the top of my tank.
George
----- Original Message -----
From: <jlatimer1@cox.net>
Sent: Wednesday, August 27, 2008 9:25 AM
Subject: Re: Zenith-List: Re: Sight gage
>
> That will work. As already posted you can run the fuel line from the wing
> tanks into the bottom inlet that you show blocked off. This will
> eliminate a T fitting.
>
> Jerry
> ---- Bill Naumuk <naumuk@alltel.net> wrote:
>> All-
>> Like I said, all the header tanks seem to have different in/outs. The
>> stupid arrangement I portrayed is what I got with my tank.
>> Since I have two outlets at the bottom of the tank, one is apparently
>> worthless.
>> I'm guessing that the alternative is to put a T at the top inlet,
>> block
>> off one of the bottom, run the main to one side of the T at the top, and
>> the
>> sight gauge between the other side of the top T and the uncapped bottom.
>> Sketch attached. Once again, waddya think?
>> XL builders have NO IDEA what HD/HDS people are talking about!!! I
>> imagine the new 650 series will be sold from vending machines. Bless you,
>> fellow sufferers! If it weren't for you people, my project would have
>> been
>> beer cans long ago. Not that that's necessarily a bad thing.
>> Bill
>> ----- Original Message -----
>> From: <jlatimer1@cox.net>
>> To: <zenith-list@matronics.com>
>> Sent: Tuesday, August 26, 2008 8:55 PM
>> Subject: Re: Zenith-List: Re: Sight gage
>>
>>
>> > Bill,
>> > As several people have already pointed out your sight glass diagram
>> > will
>> > not work. Gas will not get into the sight glass loop. You need to
>> > attach
>> > the sight glass at the top and bottom of the tank.
>> >
>> > My 8 gallon header tank came with two barbed connections at the top, a
>> > barbed connection near the bottom of the tank, and a threaded
>> > connection
>> > at the bottom of the tank.
>> >
>> > I plumbed the sight glass between one of the top and the bottom barbed
>> > connection. My wing tanks are plumbed to the other barbed connection
>> > at
>> > the top of the tank. And the threaded connection at the bottom goes to
>> > the engine.
>> >
>> > I've tried to attach the original documentation from Zenith on how to
>> > plumb the wing tanks to header tank. It also shows the sight glass.
>> >
>> > Everyone building an XL should get a kick out of the documentation that
>> > we
>> > got with our 601HDS kits.
>> > Jerry
>> > ---- Bill Naumuk <naumuk@alltel.net> wrote:
>> >> Gig, and everyone with a sight gage-
>> >> It seems that every 8 gal header tank was plumbed differently.
>> >> I've
>> >> attached a sketch of what I think the layout in my case should look
>> >> like.
>> >> I
>> >> searched the archives and not a whole hell of a lot to go on. Whaddya
>> >> think?
>> >> Bill
>> >> ----- Original Message -----
>> >> From: "Gig Giacona" <wrgiacona@gmail.com>
>> >> To: <zenith-list@matronics.com>
>> >> Sent: Tuesday, August 26, 2008 5:51 PM
>> >> Subject: Zenith-List: Re: Sight gage
>> >>
>> >>
>> >> > <wrgiacona@gmail.com>
>> >> >
>> >> > Basically a port at the bottom and one at the top of the side facing
>> >> > the
>> >> > panel put a clear tube between them. you will need to play with the
>> >> > position of the tube so you get a good reading.
>> >> >
>> >> > --------
>> >> > W.R. "Gig" Giacona
>> >> > 601XL Under Construction
>> >> > See my progress at www.peoamerica.net/N601WR
>> >> >
>> >> >
>> >> >
>> >> >
>> >> > Read this topic online here:
>> >> >
>> >> > http://forums.matronics.com/viewtopic.php?p 0758#200758
>> >> >
>> >> >
>> >> >
>> >> >
>> >> >
>> >> >
>> >> >
>> >> >
>> >> >
>> >> >
>> >
>
>
>
Message 6
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| Subject: | Playing in Clouds |
I just posted another youtube video from my trip last week. I found myself in
lots of clouds on the way home. I have always wanted to fly amongst the clouds
and I finally got the chance. All of my training was on clear days and this
was a new experience for me at 8,000 feet.
http://www.youtube.com/watch?v=LI2JUeays88
Flying my airplane is a dream come true.
Scott Laughlin
601XL/Corvair
finished & flying
107 hours
www.cooknwithgas.com
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p 0963#200963
Attachments:
http://forums.matronics.com//files/big_clouds2_127.jpg
Message 7
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| Subject: | Re: Playing in Clouds |
And I'm sure you were 2000 feet away horizontally from those clouds at all times.
[Wink]
--------
W.R. "Gig" Giacona
601XL Under Construction
See my progress at www.peoamerica.net/N601WR
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p 0978#200978
Message 8
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| Subject: | Control Surface Flutter |
Here's one for our aeronautical engineers to ponder: While
staring at my ailerons, wondering if they were going to flutter if ever
I get this bird finished, a thought struck me.
Ailerons flutter because they are moving back and forth very fast.
They move back and forth very fast because they are light, and because
they have no mass balancing them on the other side of the hinge.
It then struck me that, to add inertial mass doesn't necessarily mean
putting a weight on an arm out front, or adding a flange so you can put
weight in front of the hinge.
AHA! EUREKA! ZOUNDS! How about placing a mass, not necessarily equal to
the weight of the aileron, on the pushrod itself? Mass is used to create
inertia, and inertia doesn't care which way it's being made to
reluctantly move. The aileron can't move very fast up and down if the
pushrod doesn't want to move very fast backward and forward. There's no
additional force needed to move the aileron, and if the weight is on the
pushrod, it's inside, out of the airstream, where the wind (and
supercritical observers)can't find it. I see a tubular lead weight on
the pushrod, threaded, to snug up against the locknut at the bellcrank
end of the pushrod.
Whaddayathink?
Paul Rodriguez
601XL/Corvair
Message 9
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| Subject: | Re: Control Surface Flutter |
I'm not saying that would or wouldn't work. Mainly because it has been a LONG time
since I took physics. But if it would work wouldn't weights attached to the
cables do the same thing? And since the cable run inside the fuselage you wouldn't
have to put the weight way out in the wing you could attach it to cable
inside the fuselage.
[quote="paulrod36(at)msn.com"] Here's one for our aeronautical engineers to ponder:
While staring at my ailerons, wondering if they were going to flutter
if ever I get this bird finished, a thought struck me.
Ailerons flutter because they are moving back and forth very fast.
They move back and forth very fast because they are light, and because they have
no mass balancing them on the other side of the hinge.
It then struck me that, to add inertial mass doesn't necessarily mean putting
a weight on an arm out front, or adding a flange so you can put weight in front
of the hinge.
AHA! EUREKA! ZOUNDS! How about placing a mass, not necessarily equal to the
weight of the aileron, on the pushrod itself? Mass is used to create inertia,
and inertia doesn't care which way it's being made to reluctantly move. The
aileron can't move very fast up and down if the pushrod doesn't want to move
very fast backward and forward. There's no additional force needed to move the
aileron, and if the weight is on the pushrod, it's inside, out of the airstream,
where the wind (and supercritical observers)can't find it. I see a tubular
lead weight on the pushrod, threaded, to snug up against the locknut at the
bellcrank end of the pushrod.
Whaddayathink?
Paul Rodriguez
601XL/Corvair
> [b]
--------
W.R. "Gig" Giacona
601XL Under Construction
See my progress at www.peoamerica.net/N601WR
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p 1004#201004
Message 10
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| Subject: | Re: Control Surface Flutter |
I don't think it would work. You need to increase the inertia of the part
subject to flutter.
In other words, the ailerons mass needs to go up by *rigidly* attaching a
weight to it.
Attaching the aileron to a brick wall won't help. Making it a brick wall
will, but unfortunately, it will mess with your CG... :-)
do not archive, in case I am wrong.
Carlos
2008/8/27 <paulrod36@msn.com>
....
AHA! EUREKA! ZOUNDS! How about placing a mass, not necessarily equal to the
weight of the aileron, on the pushrod itself? Mass is used to create
inertia, and inertia doesn't care which way it's being made to reluctantly
move.
....
>
>
> Whaddayathink?
>
> Paul Rodriguez
> 601XL/Corvair
>
Message 11
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|
Jerry-
After a day to get everyone's input and think about it, I figure the way
to plumb this puppy is in the attachment.
I obviously don't (Or didn't) know jack about fluid dynamics, but I
guess all you have to do is really think about it.
The first logical assumption is that it's easier on the pump to drop the
fuel in from the top rather than push it in from the bottom. Factor the
strain pushing fuel up an extra 2' versus squirting it in from the side,
along with the additional line under pressure (Which is a potential failure
mode) and the strain on the pump is about equal, while the potential for
pressurized failure is lessened.
Your HD/HDS instructions came through fine. Eat your hearts out, XL
people!
Bill
----- Original Message -----
From: <jlatimer1@cox.net>
Sent: Tuesday, August 26, 2008 9:07 PM
Subject: Re: Zenith-List: Re: Sight gage
>
> ---- jlatimer1@cox.net wrote:
>> Bill,
>> As several people have already pointed out your sight glass diagram will
>> not work. Gas will not get into the sight glass loop. You need to
>> attach the sight glass at the top and bottom of the tank.
>>
>> My 8 gallon header tank came with two barbed connections at the top, a
>> barbed connection near the bottom of the tank, and a threaded connection
>> at the bottom of the tank.
>>
>> I plumbed the sight glass between one of the top and the bottom barbed
>> connection. My wing tanks are plumbed to the other barbed connection at
>> the top of the tank. And the threaded connection at the bottom goes to
>> the engine.
>>
>> I've tried to attach the original documentation from Zenith on how to
>> plumb the wing tanks to header tank. It also shows the sight glass.
>>
>> Everyone building an XL should get a kick out of the documentation that
>> we got with our 601HDS kits.
>> Jerry
>> ---- Bill Naumuk <naumuk@alltel.net> wrote:
>> > Gig, and everyone with a sight gage-
>> > It seems that every 8 gal header tank was plumbed differently. I've
>> > attached a sketch of what I think the layout in my case should look
>> > like. I
>> > searched the archives and not a whole hell of a lot to go on. Whaddya
>> > think?
>> > Bill
>> > ----- Original Message -----
>> > From: "Gig Giacona" <wrgiacona@gmail.com>
>> > To: <zenith-list@matronics.com>
>> > Sent: Tuesday, August 26, 2008 5:51 PM
>> > Subject: Zenith-List: Re: Sight gage
>> >
>> >
>> > > <wrgiacona@gmail.com>
>> > >
>> > > Basically a port at the bottom and one at the top of the side facing
>> > > the
>> > > panel put a clear tube between them. you will need to play with the
>> > > position of the tube so you get a good reading.
>> > >
>> > > --------
>> > > W.R. "Gig" Giacona
>> > > 601XL Under Construction
>> > > See my progress at www.peoamerica.net/N601WR
>> > >
>> > >
>> > >
>> > >
>> > > Read this topic online here:
>> > >
>> > > http://forums.matronics.com/viewtopic.php?p 0758#200758
>> > >
>> > >
>> > >
>> > >
>> > >
>> > >
>> > >
>> > >
>> > >
>> > >
>
Message 12
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| Subject: | Re: Playing in Clouds |
Scott,=0A-=0AYou might want to rethink about what you did by the clouds.
- There are a lot of "Big Boys" and small boys flying thru the clouds IFR
.- You don't see many planes during the day, but they are there.- Just
go up and fly at night, I think you will be amazed how many planes light up
the sky.=0AFly Smart,=0AAl from Oshkosh=0A=0A=0A=0A----- Original Message
----=0AFrom: cookwithgas <cookwithgas@HOTMAIL.COM>=0ATo: zenith-list@matron
ics.com=0ASent: Wednesday, August 27, 2008 1:36:07 PM=0ASubject: Zenith-Lis
<cookwithgas@hotmail.com>=0A=0AI just posted another youtube video from my
trip last week.- I found myself in lots of clouds on the way home.- I h
ave always wanted to fly amongst the clouds and I finally got the chance.
- All of my training was on clear days and this was a new experience for
me at 8,000 feet.- =0A=0Ahttp://www.youtube.com/watch?v=LI2JUeays88=0A
=0AFlying my airplane is a dream come true.- =0A=0AScott Laughlin=0A601XL
/Corvair=0Afinished & flying=0A107 hours=0Awww.cooknwithgas.com=0A=0A=0A=0A
=0ARead this topic online here:=0A=0Ahttp://forums.matronics.com/viewtopic.
php?p 0963#200963=0A=0A=0A=0A=0AAttachments: =0A=0Ahttp://forums.matron
================
Message 13
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| Subject: | Re: Control Surface Flutter |
Without conjecturing on whether it would work regarding flutter, I
would be very concerned about that much added weight causing metal
fatigue in the pushrod tube, especially the threaded portion and rod
ends. Any added weight on the pushrod tubes would be bouncing up
and down putting bending forces on the tubes. JMHO. Thanks for
sharing the idea.
Al Hays
601XL/Corvair N5892H reserved
On Aug 27, 2008, at 5:35 PM, Gig Giacona wrote:
>
> I'm not saying that would or wouldn't work. Mainly because it has
> been a LONG time since I took physics. But if it would work
> wouldn't weights attached to the cables do the same thing? And
> since the cable run inside the fuselage you wouldn't have to put
> the weight way out in the wing you could attach it to cable inside
> the fuselage.
>
>
> [quote="paulrod36(at)msn.com"] Here's one for our aeronautical
> engineers to ponder: While staring at my ailerons,
> wondering if they were going to flutter if ever I get this bird
> finished, a thought struck me.
> Ailerons flutter because they are moving back and forth very fast.
> They move back and forth very fast because they are light, and
> because they have no mass balancing them on the other side of the
> hinge.
> It then struck me that, to add inertial mass doesn't necessarily
> mean putting a weight on an arm out front, or adding a flange so
> you can put weight in front of the hinge.
> AHA! EUREKA! ZOUNDS! How about placing a mass, not necessarily
> equal to the weight of the aileron, on the pushrod itself? Mass is
> used to create inertia, and inertia doesn't care which way it's
> being made to reluctantly move. The aileron can't move very fast
> up and down if the pushrod doesn't want to move very fast backward
> and forward. There's no additional force needed to move the
> aileron, and if the weight is on the pushrod, it's inside, out of
> the airstream, where the wind (and supercritical observers)can't
> find it. I see a tubular lead weight on the pushrod, threaded, to
> snug up against the locknut at the bellcrank end of the pushrod.
>
> Whaddayathink?
>
> Paul Rodriguez
> 601XL/Corvair
>
Message 14
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Unfortunately, your first logical assumption would be wrong. :)
Overall, the pump will be working harder pumping in to the top of the
tank than it will pumping it in to the bottom. The back pressure on
the pump depends entirely on the height of fuel above the pump, not on
how many gallons are sitting above the pump. The pressure two feet
below the surface in a 500 gallon tank is the same as two feet below
the surface in a five gallon tank. Pumping in at the top, height of
the fuel will always be the height to the top of the tank so the
pressure will always be at its maximum. Pumping in at the bottom, the
pressure will start out low and increase as the fuel level in the tank
increases. But this is no big deal, just use a pump that will deliver
more pressure than the maximum it will see in this application.
The one advantage to pumping in to the top is that you won't need a
check valve to prevent the fuel from draining back to the wing tank
>
> Jerry-
> After a day to get everyone's input and think about it, I figure
> the way to plumb this puppy is in the attachment.
> I obviously don't (Or didn't) know jack about fluid dynamics, but
> I guess all you have to do is really think about it.
> The first logical assumption is that it's easier on the pump to
> drop the fuel in from the top rather than push it in from the
> bottom. Factor the strain pushing fuel up an extra 2' versus
> squirting it in from the side, along with the additional line under
> pressure (Which is a potential failure mode) and the strain on the
> pump is about equal, while the potential for pressurized failure is
> lessened.
> Your HD/HDS instructions came through fine. Eat your hearts out,
> XL people!
> Bill
--
Bryan Martin
N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.
Message 15
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| Subject: | Re: Annual Condition Inspection |
Hi Chuck,
My original rubber spacers for the gear were opened large heater hose.
It didn't work for me. Perhaps I was over torquing the nuts. Roger said to
just tighten it to "firm"..
I prolly don't know what firm is.
Tommy
Tommy,
I sliced open large diameter auto heater hose and made landing gear
spacers, for top and bottom of gear.
They have been in place a couple of years and no signs of
deterioration.
Chuck D.
N701TX
Jab 2200
Message 16
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Bryan-
After sleeping on it, that's what I figured, too. Since the 105 has a
built in check valve, I'm thus best off with the arrangement in
theattachment to my last e-mail.
Bill
----- Original Message -----
From: "Bryan Martin" <bryanmmartin@comcast.net>
Sent: Wednesday, August 27, 2008 8:05 PM
Subject: Re: Zenith-List: Re: Sight gage
>
> Unfortunately, your first logical assumption would be wrong. :) Overall,
> the pump will be working harder pumping in to the top of the tank than it
> will pumping it in to the bottom. The back pressure on the pump depends
> entirely on the height of fuel above the pump, not on how many gallons
> are sitting above the pump. The pressure two feet below the surface in a
> 500 gallon tank is the same as two feet below the surface in a five
> gallon tank. Pumping in at the top, height of the fuel will always be the
> height to the top of the tank so the pressure will always be at its
> maximum. Pumping in at the bottom, the pressure will start out low and
> increase as the fuel level in the tank increases. But this is no big
> deal, just use a pump that will deliver more pressure than the maximum it
> will see in this application.
>
> The one advantage to pumping in to the top is that you won't need a check
> valve to prevent the fuel from draining back to the wing tank
>
>>
>> Jerry-
>> After a day to get everyone's input and think about it, I figure the
>> way to plumb this puppy is in the attachment.
>> I obviously don't (Or didn't) know jack about fluid dynamics, but I
>> guess all you have to do is really think about it.
>> The first logical assumption is that it's easier on the pump to drop
>> the fuel in from the top rather than push it in from the bottom. Factor
>> the strain pushing fuel up an extra 2' versus squirting it in from the
>> side, along with the additional line under pressure (Which is a
>> potential failure mode) and the strain on the pump is about equal, while
>> the potential for pressurized failure is lessened.
>> Your HD/HDS instructions came through fine. Eat your hearts out, XL
>> people!
>> Bill
>
>
> --
> Bryan Martin
> N61BM, CH 601 XL,
> RAM Subaru, Stratus redrive.
> do not archive.
>
>
>
Message 17
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| Subject: | Re: Just a mile stone for me! |
Congratulations Rich! I need to come see your project. It would be good therapy
for me. I just started another semester, but at the end I would like to come
out.
Kevin Bonds
Nashville Tn
-------------- Original message ----------------------
From: 4RCSIMMONS@comcast.net (Rich Simmons)
> Hey list,
>
> I don't talk much and lately haven't been reading much. I still have to share
> this with some one though!
>
> After 3.5 years, I have my hull setting on wheels.
>
> Yup! It's a milestone!!
>
> My wings are 95% and tail empenages are ready to attach. I have actually placed
> but not truly located the Horizonal Satbilizer. Looks like an airplane!
>
> Shew! Still more to do. I hope I see an engine under my christmas tree thie
> year!!!!!
>
> I am going to attatche and go through the fitment process of the wings and tail
> components now while as mentioning before, "Asking Santa for my engine!"
>
> I also have to decide my panel configutration. Suggestions?
>
> If some of you wish, send me a picture of what you are doing with your panels.
I
> could help me decide.
>
> Thanks,
> Rich Simmons
>
> Do not Archive!
>
> --
> Thanks,
Rich Simmons
From: 4RCSIMMONS@comcast.net (Rich Simmons)
Subject: Zenith-List: Just a mile stone for me!
Content-Type: Multipart/mixed;
boundary="NextPart_Webmail_9m3u9jl4l_12124_1219890538_1"
--NextPart_Webmail_9m3u9jl4l_12124_1219890538_1
Content-Type: multipart/alternative; boundary="NextPart_Webmail_9m3u9jl4l_1566_1219836581_1"
--NextPart_Webmail_9m3u9jl4l_1566_1219836581_1
Content-Type: text/plain
Content-Transfer-Encoding: 8bit
Hey list,
I don't talk much and lately haven't been reading much. I still have to share this
with some one though!
After 3.5 years, I have my hull setting on wheels.
Yup! It's a milestone!!
My wings are 95% and tail empenages are ready to attach. I have actually placed
but not truly located the Horizonal Satbilizer. Looks like an airplane!
Shew! Still more to do. I hope I see an engine under my christmas tree thie year!!!!!
I am going to attatche and go through the fitment process of the wings and tail
components now while as mentioning before, "Asking Santa for my engine!"
I also have to decide my panel configutration. Suggestions?
If some of you wish, send me a picture of what you are doing with your panels.
I could help me decide.
Thanks,
Rich Simmons
Do not Archive!
--
Thanks,
Rich Simmons
--NextPart_Webmail_9m3u9jl4l_1566_1219836581_1
Content-Type: text/html
Content-Transfer-Encoding: 8bit
<html><body>
<DIV>
<DIV>Hey list,</DIV>
<DIV> </DIV>
<DIV>I don't talk much and lately haven't been reading much. I still have to share
this with some one though!</DIV>
<DIV> </DIV>
<DIV>After 3.5 years, I have my hull setting on wheels.</DIV>
<DIV> </DIV>
<DIV>Yup! It's a milestone!!</DIV>
<DIV> </DIV>
<DIV>My wings are 95% and tail empenages are ready to attach. I have actually placed
but not truly located the Horizonal Satbilizer. Looks like an airplane!</DIV>
<DIV> </DIV>
<DIV>Shew! Still more to do. I hope I see an engine under my christmas tree thie
year!!!!!</DIV>
<DIV> </DIV>
<DIV>I am going to attatche and go through the fitment process of the wings and
tail components now while as mentioning before, "Asking Santa for my engine!"</DIV>
<DIV> </DIV>
<DIV>I also have to decide my panel configutration. Suggestions?</DIV>
<DIV> </DIV>
<DIV>If some of you wish, send me a picture of what you are doing with your panels.
I could help me decide.</DIV>
<DIV> </DIV>
<DIV>Thanks,</DIV>
<DIV>Rich Simmons</DIV>
<DIV> </DIV>
<DIV>Do not Archive!</DIV></DIV>
<DIV> </DIV>
<DIV class=signature id=signature>--<BR>Thanks, <BR>Rich Simmons</DIV></body></html>
--NextPart_Webmail_9m3u9jl4l_1566_1219836581_1--
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--NextPart_Webmail_9m3u9jl4l_12124_1219890538_1--
Message 18
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Bill,
It seems to me that your sight gage will work only while the engine
is not running if you tee into the line feeding the tank from the
pump as shown in your sketch. However, I have to wonder if one of
those fittings on the bottom might actually be connected to a tube
extending to near the top inside the tank. That would let the sight
gage "breath" properly with the existing fittings. If not, you
probably can make an adaptor to achieve the same thing. How that
would be done would, of course, depend on the type and size of those
fittings on the tank bottom. Hope this helps.
Al Hays
601XL N5892H reserved
On Aug 27, 2008, at 9:34 PM, Bill Naumuk wrote:
>
> Bryan-
> After sleeping on it, that's what I figured, too. Since the 105
> has a built in check valve, I'm thus best off with the arrangement
> in theattachment to my last e-mail.
> Bill
> ----- Original Message ----- From: "Bryan Martin"
> <bryanmmartin@comcast.net>
> To: <zenith-list@matronics.com>
> Sent: Wednesday, August 27, 2008 8:05 PM
> Subject: Re: Zenith-List: Re: Sight gage
>
>
>> <bryanmmartin@comcast.net>
>>
>> Unfortunately, your first logical assumption would be wrong. :)
>> Overall, the pump will be working harder pumping in to the top of
>> the tank than it will pumping it in to the bottom. The back
>> pressure on the pump depends entirely on the height of fuel above
>> the pump, not on how many gallons are sitting above the pump. The
>> pressure two feet below the surface in a 500 gallon tank is the
>> same as two feet below the surface in a five gallon tank. Pumping
>> in at the top, height of the fuel will always be the height to
>> the top of the tank so the pressure will always be at its
>> maximum. Pumping in at the bottom, the pressure will start out
>> low and increase as the fuel level in the tank increases. But
>> this is no big deal, just use a pump that will deliver more
>> pressure than the maximum it will see in this application.
>>
>> The one advantage to pumping in to the top is that you won't need
>> a check valve to prevent the fuel from draining back to the wing
>> tank
>>
>>>
>>> Jerry-
>>> After a day to get everyone's input and think about it, I
>>> figure the way to plumb this puppy is in the attachment.
>>> I obviously don't (Or didn't) know jack about fluid dynamics,
>>> but I guess all you have to do is really think about it.
>>> The first logical assumption is that it's easier on the pump
>>> to drop the fuel in from the top rather than push it in from
>>> the bottom. Factor the strain pushing fuel up an extra 2'
>>> versus squirting it in from the side, along with the additional
>>> line under pressure (Which is a potential failure mode) and the
>>> strain on the pump is about equal, while the potential for
>>> pressurized failure is lessened.
>>> Your HD/HDS instructions came through fine. Eat your hearts
>>> out, XL people!
>>> Bill
>>
>>
>> --
>> Bryan Martin
>> N61BM, CH 601 XL,
>> RAM Subaru, Stratus redrive.
>> do not archive.
>>
>>
>>
>>
>>
>>
>>
>
>
Message 19
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If you mean a Facet 105, I believe that the check valve in this pump
is designed to allow a small amount of back flow in order to let the
fuel line depressurize after shut down. If you use this pump to feed
to the bottom of the header tank, you will have to remember to shut
off the valves leading from the wing tanks to prevent the header tank
from gradually draining into them.
>
> Bryan-
> After sleeping on it, that's what I figured, too. Since the 105
> has a built in check valve, I'm thus best off with the arrangement
> in theattachment to my last e-mail.
> Bill
--
Bryan Martin
N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.
Message 20
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| Subject: | Re: Control Surface Flutter |
Interesting idea, Paul. I don't think that its ever been done. Sort of like a
poor man's shimmy dampener. Take a walk through any aviation museum and look
at what they were doing from the late 1930s on through to the present day.
They are what's called "accepted practices." Very eye opening. A good first step
would be to look at the articles that the late, great Tony Bingelis wrote over
the years for EAA about balancing control surfaces. They are archived on the
web site. Do a search for "Bingelis." Also see the Zenair Association
Newsletters for early 1987 (they are available on CD for $40) and you will find
drawings by CH for aileron mass balances. CH calls for less than 1.5 lbs of lead
poured into a piece of streamlined tubing. That's about standard for planes of
the size and speed of the 601.
I made mass balances for my project in 1967 or 68. It was a 1450 lb all metal
with a 220 vne. The ailerons were practically identical in design to a 601.
The designer called for 1.4 to 1.6 lb of lead on a 1/2" 4130 arm that passed
under the rear spar and into the bottom if the wing tip. I still have the
drawings.
A guy that I know lives about an hour away. He retired from USAF civil
service as an Aerodynamicist. He looked over my drawings and gave me some good
advice. I won't bore everybody with that.
Bob Dingley XL/Lyc Do not archive
**************
It's only a deal if it's
where you want to go. Find your travel deal here.
(http://information.travel.aol.com/deals?ncid=aoltrv00050000000047)
Message 21
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| Subject: | Re: Control Surface Flutter |
Please bore us. What was the advise????
SW
----- Original Message -----
From: MaxNr@aol.com
To: Zenith-List@matronics.com
Sent: Wednesday, August 27, 2008 9:10 PM
Subject: Zenith-List: Re: Control Surface Flutter
Interesting idea, Paul. I don't think that its ever been done. Sort of
like a poor man's shimmy dampener. Take a walk through any aviation
museum and look at what they were doing from the late 1930s on through
to the present day. They are what's called "accepted practices." Very
eye opening. A good first step would be to look at the articles that the
late, great Tony Bingelis wrote over the years for EAA about balancing
control surfaces. They are archived on the web site. Do a search for
"Bingelis." Also see the Zenair Association Newsletters for early 1987
(they are available on CD for $40) and you will find drawings by CH for
aileron mass balances. CH calls for less than 1.5 lbs of lead poured
into a piece of streamlined tubing. That's about standard for planes of
the size and speed of the 601.
I made mass balances for my project in 1967 or 68. It was a 1450 lb
all metal with a 220 vne. The ailerons were practically identical in
design to a 601. The designer called for 1.4 to 1.6 lb of lead on a 1/2"
4130 arm that passed under the rear spar and into the bottom if the wing
tip. I still have the drawings.
A guy that I know lives about an hour away. He retired from USAF civil
service as an Aerodynamicist. He looked over my drawings and gave me
some good advice. I won't bore everybody with that.
Bob Dingley XL/Lyc Do not archive
**************
It's only a deal if it's where you want to go. Find your travel deal
here.
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Message 22
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| Subject: | Re: Playing in Clouds |
This photo is now the desk top wallpaper on my computer. Gee, it must be nice.
Dave Clay
Temple, TX
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p 1102#201102
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