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fuel lines, tunnel to wing

 
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rnewman(at)tcwtech.com
Guest





PostPosted: Wed Dec 05, 2007 6:52 pm    Post subject: fuel lines, tunnel to wing Reply with quote

Over the last couple of weeks we had a thread on flexible fuel lines and the Van's hard tubing lines. I've made my choice and decided to machine bushings to allow the use of standard bulkhead fittings at the tunnel and wing root. I've added a photo gallery on this on our web site. Here's the direct link. Just scroll to the bottom of the page on this link

http://www.tcwtech.com/RV-10%20construction%20project.htm

Bob Newman
TCW Technologies


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AV8ORJWC



Joined: 13 Jul 2006
Posts: 1149
Location: Aurora, Oregon "Home of VANS"

PostPosted: Wed Dec 05, 2007 7:38 pm    Post subject: fuel lines, tunnel to wing Reply with quote

Flexible fuel lines are exactly the kind of consumable that must be
periodically replaced in all aircraft (based on date of product
manufacture) and are subject to the ravages of Ethanol mandated into
gasoline. We need to hear Dick VanGrunsven weigh in on Oregon's new
bill - HB2210B. Numerous states were approached by Greenies at the same
time (Michigan, Massachusetts, Pennsylvania). Oregon's Department of
Agriculture just had a meeting yesterday and admitted a poorly crafted
and detrimental piece of legislation and yet the freight train is still
coming down the tracks next month.



Choose those lines wisely. Know if the VAN supplied fuel quantity
sending unit gaskets are susceptible to Ethanol laden gasoline products
in our tanks. The Help Desk at VANS needs to hear your concerns. GAMIs
PRISM product remains years from availability to help with ignition
timing control.



John Cox - 40600



________________________________

From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Bob-tcw
Sent: Wednesday, December 05, 2007 6:50 PM
To: rv10-list(at)matronics.com
Subject: fuel lines, tunnel to wing



Over the last couple of weeks we had a thread on flexible fuel lines and
the Van's hard tubing lines. I've made my choice and decided to
machine bushings to allow the use of standard bulkhead fittings at the
tunnel and wing root. I've added a photo gallery on this on our web
site. Here's the direct link. Just scroll to the bottom of the page
on this link



http://www.tcwtech.com/RV-10%20construction%20project.htm



Bob Newman

TCW Technologies


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rv10(at)sinkrate.com
Guest





PostPosted: Wed Dec 05, 2007 7:42 pm    Post subject: fuel lines, tunnel to wing Reply with quote

I have been fretting over the fuel line installation lately and I too have
considered installing standard bulkhead fittings in some similar fashion.
The one thing that has kept me from making up my mind and doing this is the
following from the 43.13. I don't think this was mentioned in the last go
around on fuel lines so I thought I would bring it up.



Chapter 8, Section 3, Paragraph 8-31, part c Alignment states:



"Never install a straight length of tubing between two rigidly mounted
fittings. Always incorporate at least one bend between such fittings to
absorb strain caused by vibration and temperature changes."



Does the fitting in the tunnel wall qualify as a rigidly mounted? If so
does anyone "in the know" know what qualifies as a proper bend? I am
wondering if this is the primary reason for the way Vans has done it without
fittings? I'm curious of others thoughts.



Ben Westfall

#40579

PDX





_____

From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Bob-tcw
Sent: Wednesday, December 05, 2007 6:50 PM
To: rv10-list(at)matronics.com
Subject: fuel lines, tunnel to wing



Over the last couple of weeks we had a thread on flexible fuel lines and the
Van's hard tubing lines. I've made my choice and decided to machine
bushings to allow the use of standard bulkhead fittings at the tunnel and
wing root. I've added a photo gallery on this on our web site. Here's
the direct link. Just scroll to the bottom of the page on this link



http://www.tcwtech.com/RV-10%20construction%20project.htm



Bob Newman

TCW Technologies


- The Matronics RV10-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

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Kellym



Joined: 10 Jan 2006
Posts: 1705
Location: Sun Lakes AZ

PostPosted: Wed Dec 05, 2007 8:12 pm    Post subject: fuel lines, tunnel to wing Reply with quote

John,
I don't know why there is much thinking of using mogas in an RV. Most
have relatively high compression pistons requiring at least 91/96 octane
avgas, which is somewhere around 96-98 pump octane mogas...pretty
unobtainable. 92 octane mogas is likely to be okay if one is careful not
to push the timing, etc.

Also, I don't know about the current formulations of PRC, but the PRC
compounds used in the '60s model Mooneys won't stand up to the aromatics
in mogas and turns to leaking mush. I saw one such plane that the owner
pretty much had to convert to bladders because of his illicit use of
premium mogas in 180hp Mooney.
So, I'd worry more about the PRC with mogas than having to replace any
flex lines. One could obtain teflon flex lines that would tolerate any
hydrocarbon, with no life limit. Parker 124J is one variety.
John W. Cox wrote:
Quote:

Flexible fuel lines are exactly the kind of consumable that must be
periodically replaced in all aircraft (based on date of product
manufacture) and are subject to the ravages of Ethanol mandated into
gasoline. We need to hear Dick VanGrunsven weigh in on Oregon’s new
bill – HB2210B. Numerous states were approached by Greenies at the
same time (Michigan, Massachusetts, Pennsylvania). Oregon’s Department
of Agriculture just had a meeting yesterday and admitted a poorly
crafted and detrimental piece of legislation and yet the freight train
is still coming down the tracks next month.

Choose those lines wisely. Know if the VAN supplied fuel quantity
sending unit gaskets are susceptible to Ethanol laden gasoline
products in our tanks. The Help Desk at VANS needs to hear your
concerns. GAMIs PRISM product remains years from availability to help
with ignition timing control.

John Cox - 40600



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_________________
Kelly McMullen
A&P/IA, EAA Tech Counselor # 5286
KCHD
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jesse(at)saintaviation.co
Guest





PostPosted: Wed Dec 05, 2007 8:38 pm    Post subject: fuel lines, tunnel to wing Reply with quote

We usually rivet in a little plate over the hold in the tunnel wall and drill the hole the size needed for the fitting, then use a washer like in the firewall. The line from there all the way to the tank is very easy because it just has two 90 degree bends in it. This keeps the connections down, keeps all rigid lines, and avoids the rigid line without bends between two fixed fittings.
do not archive

Jesse Saint
Saint Aviation, Inc.
jesse(at)saintaviation.com (jesse(at)saintaviation.com)
Cell: 352-427-0285
Fax: 815-377-3694



On Dec 5, 2007, at 10:40 PM, Ben Westfall wrote:
Quote:
I have been fretting over the fuel line installation lately and I too have considered installing standard bulkhead fittings in some similar fashion. The one thing that has kept me from making up my mind and doing this is the following from the 43.13. I don’t think this was mentioned in the last go around on fuel lines so I thought I would bring it up.

Chapter 8, Section 3, Paragraph 8-31, part c Alignment states:

“Never install a straight length of tubing between two rigidly mounted fittings. Always incorporate at least one bend between such fittings to absorb strain caused by vibration and temperature changes.”

Does the fitting in the tunnel wall qualify as a rigidly mounted? If so does anyone “in the know” know what qualifies as a proper bend? I am wondering if this is the primary reason for the way Vans has done it without fittings? I’m curious of others thoughts.

Ben Westfall
#40579
PDX



From: owner-rv10-list-server(at)matronics.com (owner-rv10-list-server(at)matronics.com) [mailto:owner-rv10-list-server(at)matronics.com (owner-rv10-list-server(at)matronics.com)] On Behalf Of Bob-tcw
Sent: Wednesday, December 05, 2007 6:50 PM
To: rv10-list(at)matronics.com (rv10-list(at)matronics.com)
Subject: fuel lines, tunnel to wing


Over the last couple of weeks we had a thread on flexible fuel lines and the Van's hard tubing lines. I've made my choice and decided to machine bushings to allow the use of standard bulkhead fittings at the tunnel and wing root. I've added a photo gallery on this on our web site. Here's the direct link. Just scroll to the bottom of the page on this link



http://www.tcwtech.com/RV-10%20construction%20project.htm



Bob Newman

TCW Technologies





.

Quote:
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style="color: blue; text-decoration: underline; ">http://www.matronics.com/Navigator?RV10-List
blue; text-decoration: underline; ">http://forums.matronics.com



[quote][b]


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dlm46007(at)cox.net
Guest





PostPosted: Wed Dec 05, 2007 8:46 pm    Post subject: fuel lines, tunnel to wing Reply with quote

One thing to consider is that most of the tubing around the fuel selector
already has some bends in each section; additionally the fixed fittings are
also aluminum and fixed in aluminum, so they all have the same coefficient
of linear expansion; They will expand together and shrink together.

_____

From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Ben Westfall
Sent: Wednesday, December 05, 2007 8:40 PM
To: rv10-list(at)matronics.com
Subject: RE: fuel lines, tunnel to wing

I have been fretting over the fuel line installation lately and I too have
considered installing standard bulkhead fittings in some similar fashion.
The one thing that has kept me from making up my mind and doing this is the
following from the 43.13. I don't think this was mentioned in the last go
around on fuel lines so I thought I would bring it up.



Chapter 8, Section 3, Paragraph 8-31, part c Alignment states:



"Never install a straight length of tubing between two rigidly mounted
fittings. Always incorporate at least one bend between such fittings to
absorb strain caused by vibration and temperature changes."



Does the fitting in the tunnel wall qualify as a rigidly mounted? If so
does anyone "in the know" know what qualifies as a proper bend? I am
wondering if this is the primary reason for the way Vans has done it without
fittings? I'm curious of others thoughts.



Ben Westfall

#40579

PDX





_____

From: owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Bob-tcw
Sent: Wednesday, December 05, 2007 6:50 PM
To: rv10-list(at)matronics.com
Subject: fuel lines, tunnel to wing



Over the last couple of weeks we had a thread on flexible fuel lines and the
Van's hard tubing lines. I've made my choice and decided to machine
bushings to allow the use of standard bulkhead fittings at the tunnel and
wing root. I've added a photo gallery on this on our web site. Here's
the direct link. Just scroll to the bottom of the page on this link



http://www.tcwtech.com/RV-10%20construction%20project.htm



Bob Newman

TCW Technologies


- The Matronics RV10-List Email Forum -
 

Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:

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Back to top
pitts_pilot(at)bellsouth.
Guest





PostPosted: Thu Dec 06, 2007 5:18 am    Post subject: fuel lines, tunnel to wing Reply with quote

John W. Cox wrote:
Quote:

Flexible fuel lines are exactly the kind of consumable that must be periodically replaced in all aircraft (based on date of product manufacture) and are subject to the ravages of Ethanol mandated into gasoline.
The steel braided, teflon lined hose should be rather immune to ethanol. Or any other 'new' additive to gasoline ...... or 100LL
Linn
do not archive
[quote]
We need to hear Dick VanGrunsven weigh in on Oregon’s new bill – HB2210B. Numerous states were approached by Greenies at the same time (Michigan, Massachusetts, Pennsylvania). Oregon’s Department of Agriculture just had a meeting yesterday and admitted a poorly crafted and detrimental piece of legislation and yet the freight train is still coming down the tracks next month.

Choose those lines wisely. Know if the VAN supplied fuel quantity sending unit gaskets are susceptible to Ethanol laden gasoline products in our tanks. The Help Desk at VANS needs to hear your concerns. GAMIs PRISM product remains years from availability to help with ignition timing control.

John Cox - 40600
[b]


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pitts_pilot(at)bellsouth.
Guest





PostPosted: Thu Dec 06, 2007 5:37 am    Post subject: fuel lines, tunnel to wing Reply with quote

Ben Westfall wrote:
Quote:
v\:* {behavior:url(#default#VML);} o\:* {behavior:url(#default#VML);} w\:* {behavior:url(#default#VML);} .shape {behavior:url(#default#VML);} <![endif]--> st1\:*{behavior:url(#default#ieooui) } <![endif]--> <![endif]--> <![endif]-->
I have been fretting over the fuel line installation lately and I too have considered installing standard bulkhead fittings in some similar fashion. The one thing that has kept me from making up my mind and doing this is the following from the 43.13. I don’t think this was mentioned in the last go around on fuel lines so I thought I would bring it up.

Chapter 8, Section 3, Paragraph 8-31, part c Alignment states:

“Never install a straight length of tubing between two rigidly mounted fittings. Always incorporate at least one bend between such fittings to absorb strain caused by vibration and temperature changes.”

Does the fitting in the tunnel wall qualify as a rigidly mounted?
Yes.
Quote:

If so does anyone “in the know” know what qualifies as a proper bend?
Strain relief for hard tubing is usually a 360 degree loop. The biggest problem is accurately making the tubing so that no tension or compression forces are placed on the tubing. That will cause premature cracking of the hard tubing. For flexible (read hoses) tubing, a little extra length is sufficient. No tension allowed, however.
Quote:

I am wondering if this is the primary reason for the way Vans has done it without fittings?
Reading Vans mind has been tough for me. It could be that making the tubing one single part is time consuming and helps qualify the kit for the 51% rule.
Linn
do not archive
[quote]
I’m curious of others thoughts.

Ben Westfall
#40579
[b]


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MauleDriver(at)nc.rr.com
Guest





PostPosted: Thu Dec 06, 2007 9:48 am    Post subject: fuel lines, tunnel to wing Reply with quote

MauleDriver wrote: [quote] I came to understand the purpose of this istem 43.13 before I knew it was a standard. I found it aggravating to no end that none of the components of the fuel system that reside in the tunnel are lined up. Each one (boost pump, filter, flow meter) are all misaligned slightly so one can never "install a straight length of tubing between two rigidly mounted fittings". the fittings all require a job in the tubing between them.

I did the same bulkhead fitting thing that Bob and others have done. Note that there are 90 degree bends in both pieces of tubing so it would appear to conform to 8-31. Bob did a real nice job on the bushings so that there are 2 inner bushing to keep the fitting centered in the oversize hole, and 2 outer bushing to capture it in the hole. I took a simpler route and just used 2 outer bushing that depend on being clamped in place by the nut on the bulkhead fitting. Given 8-31, the lazy approach would possibly provide even greater allowance for vibration and temperature changes. Though I would emphasize there is no need for this in this situation. And Bob's bushings really looks like the proper way to do it.

Overall, I'm thinking that the bulkhead fitting is the best way to handle this situation next to Van's original design. It simplies the bending required and facilitates installation of the Andair valve. It does add more points of possible failure.

Bill Watson

Ben Westfall wrote:
Quote:
v\:* {behavior:url(#default#VML);} o\:* {behavior:url(#default#VML);} w\:* {behavior:url(#default#VML);} .shape {behavior:url(#default#VML);} <![endif]--> st1\:*{behavior:url(#default#ieooui) } <![endif]--> <![endif]--> <![endif]-->
I have been fretting over the fuel line installation lately and I too have considered installing standard bulkhead fittings in some similar fashion. The one thing that has kept me from making up my mind and doing this is the following from the 43.13. I don’t think this was mentioned in the last go around on fuel lines so I thought I would bring it up.

Chapter 8, Section 3, Paragraph 8-31, part c Alignment states:

“Never install a straight length of tubing between two rigidly mounted fittings. Always incorporate at least one bend between such fittings to absorb strain caused by vibration and temperature changes.”

Does the fitting in the tunnel wall qualify as a rigidly mounted? If so does anyone “in the know” know what qualifies as a proper bend? I am wondering if this is the primary reason for the way Vans has done it without fittings? I’m curious of others thoughts.

Ben Westfall
#40579
PDX

[b]


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rnewman(at)lutron.com
Guest





PostPosted: Thu Dec 06, 2007 11:56 am    Post subject: fuel lines, tunnel to wing Reply with quote

I looked into this straight tube between rigid supports thing as
discussed in 43.13 and I identified two issues regarding this specific
installation that allow me to be satisfied that in this particular
installation I'm not going to have a problem.

First, the mounting point at the tunnel is not very stiff. The
tunnel is 0.050" aluminum and there is no support stiffening in the area
in the same axis as the fuel line. (ie no other bulkheads at a right
angle to the tunnel) So effectively there is not a lot holding the
tunnel end fitting thereby allowing expansion, contraction and vibration
to provide little stress to the tube. Try pushing on the tunnel
sheetmetal near the location where this tube fitting goes and you'll see
how much and easily the tunnel flexes at this point.
Second, This area of the aircraft is incrediblly stiff in the
bending direction allong the axis of the fuel tube. The fuel line is
running parallel to the wing spar and about 8" in front of the spar,
the amount of structural flexing in this area better be darn little!
So those were the two things I considered before I made the
bushings,

I do note though, ensuring the fuel tubing length is correct is now
much more important, and if I'm not satisfied with this approach, I'll
loose the bulkhead fitting at the wing root and just use the one that
allows a nice transition into the tunnel.
-Bob Newman


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AV8ORJWC



Joined: 13 Jul 2006
Posts: 1149
Location: Aurora, Oregon "Home of VANS"

PostPosted: Fri Dec 07, 2007 3:01 pm    Post subject: fuel lines, tunnel to wing Reply with quote

If you builders can find other RV-10 builders who ignore this maxim. Either conclude they understand little on fluid dynamics or they are just uninformed and need to open the book for a refresher. The danger is just not worth it. Pictures of tunnels can show a lot about understanding tubing bends and use of flex tubing. Ben’s edit is DEAD ON. “Never”.

John Hilger’s tunnel is one of the most beautiful jobs I have laid eyes on yet. John… its time to post a picture or two as a tease for clarification.

John Cox
#40600
KUAO


From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of MauleDriver
Sent: Thursday, December 06, 2007 9:21 AM
To: rv10-list(at)matronics.com
Subject: Re: fuel lines, tunnel to wing


MauleDriver wrote:
I came to understand the purpose of this istem 43.13 before I knew it was a standard. I found it aggravating to no end that none of the components of the fuel system that reside in the tunnel are lined up. Each one (boost pump, filter, flow meter) are all misaligned slightly so one can never "install a straight length of tubing between two rigidly mounted fittings". the fittings all require a job in the tubing between them.

I did the same bulkhead fitting thing that Bob and others have done. Note that there are 90 degree bends in both pieces of tubing so it would appear to conform to 8-31. Bob did a real nice job on the bushings so that there are 2 inner bushing to keep the fitting centered in the oversize hole, and 2 outer bushing to capture it in the hole. I took a simpler route and just used 2 outer bushing that depend on being clamped in place by the nut on the bulkhead fitting. Given 8-31, the lazy approach would possibly provide even greater allowance for vibration and temperature changes. Though I would emphasize there is no need for this in this situation. And Bob's bushings really looks like the proper way to do it.

Overall, I'm thinking that the bulkhead fitting is the best way to handle this situation next to Van's original design. It simplies the bending required and facilitates installation of the Andair valve. It does add more points of possible failure.

Bill Watson

Ben Westfall wrote:
I have been fretting over the fuel line installation lately and I too have considered installing standard bulkhead fittings in some similar fashion. The one thing that has kept me from making up my mind and doing this is the following from the 43.13. I don’t think this was mentioned in the last go around on fuel lines so I thought I would bring it up.

Chapter 8, Section 3, Paragraph 8-31, part c Alignment states:

“Never install a straight length of tubing between two rigidly mounted fittings. Always incorporate at least one bend between such fittings to absorb strain caused by vibration and temperature changes.”

Does the fitting in the tunnel wall qualify as a rigidly mounted? If so does anyone “in the know” know what qualifies as a proper bend? I am wondering if this is the primary reason for the way Vans has done it without fittings? I’m curious of others thoughts.

Ben Westfall
#40579
PDX

[quote] http://www.matronics.com/contributionhttp://www.matronics.com/Navigator?RV10-Listhttp://forums.matronics.com [b]


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Tim Olson



Joined: 25 Jan 2007
Posts: 2872

PostPosted: Sat Dec 08, 2007 5:44 am    Post subject: fuel lines, tunnel to wing Reply with quote

Here are photos of John's line that he sent me to post. If you're
going hard lines, John's are about as nice as I've seen.
http://www.myrv10.com/miscphotos/JohnHilger/fuel_lines.html

Tim Olson - RV-10 N104CD - Flying
do not archive
John W. Cox wrote:
Quote:
If you builders can find other RV-10 builders who ignore this maxim.
Either conclude they understand little on fluid dynamics or they are
just uninformed and need to open the book for a refresher. The danger
is just not worth it. Pictures of tunnels can show a lot about
understanding tubing bends and use of flex tubing. Ben’s edit is DEAD
ON. “Never”.



John Hilger’s tunnel is one of the most beautiful jobs I have laid eyes
on yet. John… its time to post a picture or two as a tease for
clarification.



John Cox

#40600

KUAO



------------------------------------------------------------------------

*From:* owner-rv10-list-server(at)matronics.com
[mailto:owner-rv10-list-server(at)matronics.com] *On Behalf Of *MauleDriver
*Sent:* Thursday, December 06, 2007 9:21 AM
*To:* rv10-list(at)matronics.com
*Subject:* Re: fuel lines, tunnel to wing



MauleDriver wrote:

I came to understand the purpose of this istem 43.13 before I knew it
was a standard. I found it aggravating to no end that none of the
components of the fuel system that reside in the tunnel are lined up.
Each one (boost pump, filter, flow meter) are all misaligned slightly so
one can never "/install a straight length of tubing between two rigidly
mounted fittings". / the fittings all require a job in the tubing
between them. /
/
I did the same bulkhead fitting thing that Bob and others have done.
Note that there are 90 degree bends in both pieces of tubing so it would
appear to conform to 8-31. Bob did a real nice job on the bushings so
that there are 2 inner bushing to keep the fitting centered in the
oversize hole, and 2 outer bushing to capture it in the hole. I took a
simpler route and just used 2 outer bushing that depend on being clamped
in place by the nut on the bulkhead fitting. Given 8-31, the lazy
approach would possibly provide even greater allowance for vibration and
temperature changes. Though I would emphasize there is no need for this
in this situation. And Bob's bushings really looks like the proper way
to do it.

Overall, I'm thinking that the bulkhead fitting is the best way to
handle this situation next to Van's original design. It simplies the
bending required and facilitates installation of the Andair valve. It
does add more points of possible failure.

Bill Watson

Ben Westfall wrote:

I have been fretting over the fuel line installation lately and I too
have considered installing standard bulkhead fittings in some similar
fashion. The one thing that has kept me from making up my mind and
doing this is the following from the 43.13. I don’t think this was
mentioned in the last go around on fuel lines so I thought I would bring
it up.



/Chapter 8, Section 3, Paragraph 8-31, part c Alignment states:/

/ /

/“Never install a straight length of tubing between two rigidly mounted
fittings. Always incorporate at least one bend between such fittings to
absorb strain caused by vibration and temperature changes.” /



Does the fitting in the tunnel wall qualify as a rigidly mounted? If so
does anyone “in the know” know what qualifies as a proper bend? I am
wondering if this is the primary reason for the way Vans has done it
without fittings? I’m curious of others thoughts.



Ben Westfall

#40579

PDX





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AV8ORJWC



Joined: 13 Jul 2006
Posts: 1149
Location: Aurora, Oregon "Home of VANS"

PostPosted: Sat Dec 08, 2007 8:14 am    Post subject: fuel lines, tunnel to wing Reply with quote

Thanks for posting Tim. And oh by the way, John Hilger discarded the
VAN kit supplied 1100 tubing for the 5100 series from Lancair to get
those beautiful bends and straight runs after the radii. (A really smart
touch).

I will be doing the same. The 5100 is for guys who want it looking
professional. The 1100 is for guys bending it with a spring or broom
stick of wood cause it will never be seen. In any case a straight run
of tubing between two fixed points has to be too short to install and
then remove. Once flow begins the tubing flexs. No one wants a fuel
leak. Hence the beautiful flowing lines found in John Hilger's tunnel,
which are 43.13 compliant.

John

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