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03-14-2018, 11:15 AM
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Join Date: Sep 2016
Location: Joseph, Oregon
Posts: 561
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Static Port Conundrum
Installing the static ports (Dynon) was next on my list.
All was well, I had the port locations marked on both sides of the fuselage, researched wether I was going to use the Dynon ports or order the Van's rivets (Dynon) and was ready to drill the holes.
Annnnnd.... then I came across Van's Static Port Kit instructions.
The -7 plans show the static port location just ahead of bulkhead F-708. The Kit instruction show the static ports just ahead of bulkhead F-707.
Now, if push comes to shove...I'll install the ports where the -7 plans indicate. BUT, The kit instruction have their appeal due to the ports and tubing being one bulkhead further forward and I like that...less tubing, easier access...
I know this topic has been discussed almost as much as primer but I haven't seen any discussions on the merits of being at one bulkhead or the other.
Plans location with the kit location added.
The Static Kit instructions.
What do you think??
__________________
Michael Fleming
Joseph, OR
sagriver at icloud dot com
RV-7 Slider #74572
Started 11/2016
Empennage completed 11/2016 (sans fiberglass)
Ailerons and flaps completed 3/2017.
Wings completed 12/2017
Started on QB fuselage 01/2018
Donated for 2020 and so should you
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03-14-2018, 11:35 AM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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I read it differently... the static kit instructions say that the picture shown is for a RV-6 and to use Drawing 28 from the -7 plans for a static location.
Go with the -7 plans. 
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
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03-14-2018, 11:56 AM
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Join Date: Sep 2016
Location: Joseph, Oregon
Posts: 561
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Quote:
Originally Posted by az_gila
I read it differently... the static kit instructions say that the picture shown is for a RV-6 and to use Drawing 28 from the -7 plans for a static location.
Go with the -7 plans. 
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How the heck did I miss that line
OK ... thoroughly embarrassed
Everyone can move on....nothing to see here ...
__________________
Michael Fleming
Joseph, OR
sagriver at icloud dot com
RV-7 Slider #74572
Started 11/2016
Empennage completed 11/2016 (sans fiberglass)
Ailerons and flaps completed 3/2017.
Wings completed 12/2017
Started on QB fuselage 01/2018
Donated for 2020 and so should you
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03-14-2018, 12:54 PM
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Join Date: Jan 2005
Location: Yorkshire, England
Posts: 2,048
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Just before you continue......
The rivet needs good support before you knock out the mandrel.
We used a thick wall tube on the inside to support the structure and a correct sized punch. Deep breath and a good whack !
Enjoy.
__________________
"I add a little excitement, a little spice to your lives, and all you do is complain!" - Q
Donated in 2020
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03-14-2018, 01:14 PM
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Join Date: Oct 2006
Location: Garden City, Tx
Posts: 5,122
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And you might give some thought to strain relief on the tubing, or at least route it in such a way that it is nearly strain-free. I followed the instructions with my 9A and by the time it was ready for inspection one side had come off and I had to crawl back there and re-work them.
__________________
Greg Niehues - SEL, IFR, Repairman Cert.
Garden City, TX VAF 2020 dues paid 
N16GN flying 700 hrs and counting; IO360, SDS, WWRV200, Dynon HDX, 430W
Built an off-plan RV9A with too much fuel and too much HP. Should drop dead any minute now.
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03-14-2018, 01:45 PM
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Join Date: May 2011
Location: Ontario, Canada
Posts: 262
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Static port
Just a comment on the static port itself, since the location is resolved.
I initially used the ACS "STATIC PORT ALUMINUM 15160" due to it's nicer connection to the line and my own stupidity. Big mistake. After much experimentation I have changed to the Vans rivet installed into the base of the old port for the best of both worlds. IAS is now finally accurate. Can't comment on the Dynon port but there are many posts regarding issues with non Vans rivet installations.
Al
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03-14-2018, 02:39 PM
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Join Date: Sep 2016
Location: Joseph, Oregon
Posts: 561
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Quote:
Originally Posted by RV7 To Go
Just a comment on the static port itself, since the location is resolved.
I initially used the ACS "STATIC PORT ALUMINUM 15160" due to it's nicer connection to the line and my own stupidity. Big mistake. After much experimentation I have changed to the Vans rivet installed into the base of the old port for the best of both worlds. IAS is now finally accurate. Can't comment on the Dynon port but there are many posts regarding issues with non Vans rivet installations.
Al
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Yesterday I talked with Van's support (Eric). We discussed the various options. Van's sells the rivet and a nicer port that has a threaded connection. Basically the advice I received was, just don't use a flush port.
I have read about non rivet ports that caused all sorts headaches but others had fine results.
The fancy Van's port looks like it mimics the rivet head.
The Dynon port looks similar but the area behind the skin is much bigger.
I guess the only sure thing is using the rivet.
__________________
Michael Fleming
Joseph, OR
sagriver at icloud dot com
RV-7 Slider #74572
Started 11/2016
Empennage completed 11/2016 (sans fiberglass)
Ailerons and flaps completed 3/2017.
Wings completed 12/2017
Started on QB fuselage 01/2018
Donated for 2020 and so should you
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03-14-2018, 05:31 PM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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The new Vans one looks similar to the ones from Cleaveland tools, but the Cleaveland one is designed to be bonded on and use a push-on tubing fitting.
http://www.cleavelandtool.com/Push-O.../#.Wqmv8NJy5hE
The slightly raised portion fits though a 1/2 hole in the skin.
NOTE - These are quite different from the old ones I put on my -6A. The old ones (10+ years, I think from Cleaveland) were simply flush on the outside and just provided a barbed connection on the inside. They only worked properly after I bonded in a 3/16 flat head rivet and then filed it down to get less than 1 kt error.
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
Last edited by az_gila : 03-14-2018 at 10:28 PM.
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03-14-2018, 05:44 PM
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Join Date: Oct 2005
Location: Estes Park, CO
Posts: 3,931
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Static port
I will add to the confusion. I modified the SafeAir ports. Vans location.
Lots of threads on the mod. Basically the SafeAir port is drilled to accommodate the Vans rivet. It allows the use of the Vans rivet on the exterior for accuracy and the SafeAir fitting on the inside. I ran both to the top to a "T" then back down toward the Port side and forward to the ADAHRS.
__________________
Larry Larson
Estes Park, CO
http://wirejockrv7a.blogspot.com
wirejock at yahoo dot com
Donated 12/03/2019, plus a little extra.
RV-7A #73391, N511RV reserved (2,000+ hours)
HS SB, empennage, tanks, wings, fuse, working finishing kit
Disclaimer
I cannot be, nor will I be, held responsible if you try to do the same things I do and it does not work and/or causes you loss, injury, or even death in the process.
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03-14-2018, 06:10 PM
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Join Date: Sep 2007
Location: Central IL
Posts: 5,515
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Quote:
Originally Posted by wirejock
I will add to the confusion. I modified the SafeAir ports. Vans location.
Lots of threads on the mod. Basically the SafeAir port is drilled to accommodate the Vans rivet. It allows the use of the Vans rivet on the exterior for accuracy and the SafeAir fitting on the inside. I ran both to the top to a "T" then back down toward the Port side and forward to the ADAHRS.
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+1 It yielded a 0.12 kt TAS difference with GPS ground speed using 3 leg method (166KTAS). Has the print RV7 location.
That new button with the barb looks good!

__________________
Bill
RV-7
Lord Kelvin:
“I often say that when you can measure what you are speaking about,
and express it in numbers, you know something about it; but when you
cannot measure it, when you cannot express it in numbers, your knowledge
is of a meager and unsatisfactory kind.”
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