RV10-Archive.digest.vol-bw

December 16, 2006 - January 02, 2007



Subject: Re: Garmin 496 -Antenna
>Is that the "only" think you can conclude? What about the objective facts? >For example, I also concluded that there are functional differences such as >"you can't enter an airway into the 430". A fact - correct? Why, after all >the diatribe, do you brush away all the facts and revert to subjective >personal opinion? Worse yet, you revert to public opinion/market economics >rather than sound science/engineering? Perhaps a proven political move - >but very bad science/engineering! rtitsworth, Since you haven't figured it out, that was my way of saying that this debate is pointless. Again, If you go back and RE-READ my first post, I stated this very fact--there is no need for a conclusion on that since this was never debated. I am searching for a new fact, science/engineering in your post. Tell me what facts I have brushed away? I'm also still waiting for someone to tell me what negative or non "sound science/engineering" comments I'm made regarding the 480. William Curtis http://wcurtis.nerv10.com/ ________________________________________________________________________________
From: "Noel & Yoshie Simmons" <noel(at)blueskyaviation.net>
Subject: Cabin Top Mold Release
Date: Dec 16, 2006
Larry, Start with water; most mold releases today are waterborne. If that does not work go with the acetone Noel Simmons Blue Sky Aviation Inc LWT -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Larry Rosen Sent: Saturday, December 16, 2006 8:02 AM Subject: RV10-List: Cabin Top Mold Release Getting ready to start finishing the inside of the cabin top. There are some large voids (surprise surprise) that have a yellow to orange residue. Is this mold release? Should I use a solvent to remove it? Would acetone work? -- Larry Rosen RV-10 #356 http://lrosen.nerv10.com ________________________________________________________________________________
From: "Noel & Yoshie Simmons" <noel(at)blueskyaviation.net>
Subject: Smokin Rivets
Date: Dec 16, 2006
The anatomy of the smokin=92 rivet. What is smoke? The black residue that streams down wind of a rivet is Aluminum oxide, the second hardest substance on earth with the first being diamonds. Aluminum oxide is a by product of corrosion that naturally occurs. Aluminums is considered to be self lubricating, meaning it will continue to sluff, and the aluminum oxide being harder than the base metal will exponentially carve more aluminum oxide out of the base metal, A rivet that has been properly set will eventually smoke given a structure subjected to vibration that has been under engineered, meaning not enough rivets per inch. I have seen, and repaired these structures (again and again), mostly engine nacelles on jets, fortunately or unfortunately how every you want to look at the subject, Van=92s aircraft does not have any under engineered structures that would qualify for the under engineered place to look for smoking rivets. Yes all rivet joints move to one degree or another so a rivet can be set in such a way that it will smoke. In conclusion smoking rivets on RV is a builder flaw. How to set rivets that will smoke. First let us look at the parts that Van=92s sends us. The Punching process is extremely actuate, Fin Power CNC punch press have a tolerance of .004 in 8 linear feet. Van=92s has CAD people that really know their system and can tell the punch press exactly where to put holes. Given the .004 tolerance there are some places on the aircraft that have the same hole in 4 sheets of aluminum that each have this tolerance so you will see holes that are a little hard to put a reamer through, but is still very accurate. The punching action causes aluminum to =93flow=94. That is the cause of the volcano on the exit side of the sheet. This flow is not like the burr created from using a drill bit. You must remove the volcano completely with out countersinking the base metal. Below is how to cause voids and entrap, well let=92s call it =91Stuff=92 for lack of better words, which promote the corrosive environment to create copious amounts of SMOKE. 1. Use a drill bit instead of a reamer. a. Just for giggles take a =BC=94 drill bit and begin drilling a hole in a piece of .032 sheet metal. You will see that the hole that begins to develop is triangular, and as the drill bit finally passes the hole is not truly round. This is obviously a start of voids in the rivet joint. b. USE a Reamer they turn triangular holes into properly sized round ones. Reamers should be used everywhere on the van=92s pre-punched holes 2. Don=92t deburr/ deburr to deeply a. The punching process causes a volcano like structure on the punch exit. Not only will this cause a void but will chip the rim of the volcano into the joint acting like grist in a roller mill. b. The head and or shop head will sit up on the volcano and will not properly clamp the rivet joint. c. Deburring to deeply is a very, very common mistake RV builder=92s make due to the punching process. d. Look at some of the heavier aluminum that has been punched with 1/8=94 holes. You will see one side that is pressed in and the other side will be coned out like a volcano. If you take a 100 degree countersink or some of the other rotary deburring tools and cut this volcano off to the point that there is no aluminum that protrudes above the base metal you will have a shallow countersink. This shallow countersink WILL NOT be completely filled by the expansion of a rivet. This is the stating point of corrosion e. We use sand paper to deburr. The sand paper will remove the volcano with out causing a shallow countersink. Two notes WE PRIME, WE don=92t build polished aircraft. 3. Dimpling / countersinking the sub structure with the same dimple as the skin. a. Easy test, take two small pieces of scrap aluminum and drill #30 holes, Deburr. b. Dimple each with your #30 dimple dies. c. Mate the two pieces and you will see that they don=92t fit very well. This cause lots of voids and is the primary thing that RV builders do to cause smoke. d. Take those same two pieces of aluminum and dimple them together using your #30 dimple dies. i. Better fit isn=92t it! They don=92t rock like a bobble head doll e. Point here is that most people don=92t dimple the substructures (ribs) to =93receive=94 the overlaying dimple. f. We take a small =BD=94X 1/2=94 scrap and attach it to the male dimple die to dimple all the sub structure. This eliminates the rocking caused by having two improperly formed dimples pinched together by a rivet. g. I have seen people dimpling with the plastic sill in place, bad idea. h. I have seen people afraid of over dimpling so they hit the dimplier once instead of twice (real hard). Dimpling is a forming process that must be complete; a half dimple will cause the skin to warp, bad idea. Sorry if this is a little anal, I have spent many years trying to get the best looking rivets I can. I have piles of scrap that I drill holes in and look at with a magnifying glass. Rivet and inspect, change the technique a little here and there then drill and rivet inspect until ,In my opinion we do some of the finest riveting on RV=92s. Every airplane we do get=92s a little better and a little faster. Noel Simmons Blue Sky Aviation, Inc. www.blueskyaviation.net <http://www.blueskyaviation.net/> _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John W. Cox Sent: Friday, December 15, 2006 9:09 PM Subject: RV10-List: Smokin Rivets Now that builders have painted the landscape with why and why not to drill, then deburr, then dimple vs. deburr, dimple then drill or just skip it all together and just pop rivet. Let=92s move the discussion to the next level. I don=92t know if any RV-10s that have enough time on them yet but no one has addressed the cause for them, where they are likely to occur (so you can be watching), what corrective action can be taken or more importantly which of the two or three techniques being used is less likely to contribute to them. We are all prideful of our selected technique but a lot of builders might find the discussion enlightening. ' not to be confused with Lightning and the need for static suppression wicks. Deems, you referenced Dan Checkoway=92s advise (the self promoted high guru on Sheetmetal). What say Dan? Let=92s hear discussion about tensile vs. shear, wet rivets, use of reams vs. drill bits, fitment of the rivet to the opening and proper prep, or rivets in composite. VAN=92s says =93forgetaboutit=94 cause the RV-12 is going to skip steps in the effort to find a faster build and lazy group of builders. How about the advantages and applications of Icebox rivets, Monel or the common 1100 rivets? Come on Kelly ' let=92s play. During last night=92s Pacific NW storm we were hit by a rash of lightning strikes and smoking rivets all over the NW (scores of aircraft). Anyone remember Honest Abe=92s math on Four Score? We are building the finest High Speed, IFR cruisers at low cost out there right? John Cox #40600 ________________________________________________________________________________
From: "noel(at)blueskyaviation.net" <noel(at)blueskyaviation.net>
Subject: RE: smoking rivets
Date: Dec 16, 2006
Here are some drawings I did quickly to help picture acidental countersinking of the base metal=2E Noel -------------------------------------------------------------------- mail2web - Check your email from the web at http://mail2web=2Ecom/ =2E ________________________________________________________________________________
From: GRANSCOTT(at)AOL.COM
Date: Dec 16, 2006
Subject: Re: Garmin 496 -Antenna
Tim my take on the two units are pretty straight forward, both will get you from point A to point B...but the cnx 80/480 will provide you with airways and you can calculate closest point of approach...the 480 will provide WAAS approaches with data bases that contain these WAAS approaches. Buttons are slightly different as are some command words. The next generation 430's will have WAAS approaches and apparently Garmin will retro the current in the field 430's to WAAS units at some point in the future with an up charge. When I talked to Garmin several years ago about the apparent disconnect on the lack of Victor's in the 430/530 system their response was that they created their units with direct flights in mind...now I've also heard from others that at the time Garmin had a problem with memory and could not include all the Victor's plus all the other items they designed. Maybe that's why they are now making a major modification to update the old 430/530 with the WAAS approaches. Like Kelly out west, when one files up here in the east one does a lot of Victor's before you get cleared direct. I'd think that having Victors sure would make the routing easier than having to plug in all the way points...but all can be done with time and charts in hand. The MX 20 with the G1000/530 system is pretty easy but they do not have Victor's in it either. Or at least in the last 100 hours I've flown behind it I've yet to find a Victor airway...maybe I've got to punch a little deeper in the sub pages...but I don't think I'll find them...I know my partner Dan has the Victors in his system that in the 767 he drives. Patrick ________________________________________________________________________________
Date: Dec 16, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: RE: Garmin 496 -Antenna - Freeflight WAAS
All I want to know is my MX 20, 480, SL-30 with two CDI's OK? Rick S. 40185 heeheehee ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Cabin Top Mold Release
Date: Dec 16, 2006
As Hugo stated on the lastest email concerning this topic, if it is on the inside of the part it is lickely one of the following. 1) A lack of adequate fiberglass cloth over the core material and it is showing through. 2) A separator film, like peel ply(Absorbant)(usually white in color) or perforated release film plastic(non absorbant)that is laid over the part to separate it from the next material. 3) A breather cloth which allows all the air to be removed from the project prior to the vacuum bag touching down on the part while pulling vacuum. 4) unlikely to be the actual vacuum bag with all this other stuff in between during the entire process. On the outside, up against the mold, the wax they use is whiped off just like the finish on your car, you can't see it. Over that, they use PVA( poly vinyl acetate) an alcohol/water based release agent, green in color and leaves a transparent film so thin it would whipe off with a sponge and water. In any case, it doesn't speak to well for the manufactures of the part. John G. >From: Larry Rosen <LarryRosen(at)comcast.net> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: RV10-List: Cabin Top Mold Release >Date: Sat, 16 Dec 2006 10:01:42 -0500 > > >Getting ready to start finishing the inside of the cabin top. There are >some large voids (surprise surprise) that have a yellow to orange residue. >Is this mold release? Should I use a solvent to remove it? Would acetone >work? > >-- > >Larry Rosen >RV-10 #356 >http://lrosen.nerv10.com > > ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Re: Bad idea to skip section 32: Tailcone Attachment ?
Date: Dec 16, 2006
In complete agreement, I don't think you can do much of anything. Do not even try unless you wnat to rebuild the entire thing again. I have been working on this area for two weekends and I am skipping steps because my wires are in the mail and my baggage floors are not riveted in yet, but the tailcone has been on for a month now. This part seems to be going very slow as I keep having to plan ahead as to not fall into a trap. Ordering and waiting on mail deliveries. John G. >From: PJ Seipel <seipel(at)seznam.cz> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: Re: RV10-List: Bad idea to skip section 32: Tailcone Attachment ? >Date: Sat, 16 Dec 2006 10:03:25 -0500 > > >If you permanently attach the cabin top before you attach the tailcone, >you're going to have a heck of a time getting the tailcone on later. I had >a hard time getting things lined up properly with 2 people and the top wide >open where I could see what I was doing and had access to everything, I >can't imagine trying to do it with the cabin top in the way. > >I also don't think you can do a whole lot in the baggage area without the >tailcone on. > >PJ >RV-10 #40032 > >Lorenz Malmstrm wrote: >> >>Hello group >> >>I am quickly approaching section 32 where you attach the tailcone. As I am >>heavily shop space challenged, Id like to postpone this step as long as >>possible. My idea is to: >> >>- Temporarily attach (cleco) the tailcone and do what can be done in the >>baggage area. >> >>- Remove the tailcone and finish the rest of the fuselage (including cabin >>cover). >> >>- Install the engine, cowling & panel. >> >>- Finally install the tailcone completely. >> >>Jesse had an image recently where the cabin cover was installed without >>tailcone so it seems to be possible. What are the traps and gotchas with >>this approach? What can be done in the baggage area and what not? >> >>Thanks everybody in advance. >> >>Lorenz. >> >>#40280 >> >>http://www.malmstrom.ch/RV10.htm >> >>* >> >> >>* > > ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: door prep
Date: Dec 17, 2006
Below is a picture of a way to keep placing the door being trrimmed into the same location for each fit. About 3 hours per door to get a really nice fit. . The message is ready to be sent with the following file or link attachments: IMG_0001 ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: correct door prep picture
Date: Dec 17, 2006
The message is ready to be sent with the following file or link attachments: IMG_0012 ________________________________________________________________________________
Date: Dec 17, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: Setting trailing edges of control surfaces
Hi When I visited a couple of builders on Oregon, one mentioned that he wished he used a piece of angle to ensure that his rudder edge was straight. I did that with my rudder and was very happy with the result. I have just completed my elevator trailing edges the same way have achieved brutally straight elevators. Given that I had to muddle my way through this, I thought I would share what I did for the benefit of others. I picked up a 6 ft length of angle aluminum at Rona (a Canadian version of Home Depot), cut it in half and proceeded to drill #40 holes in each section. The hole spacing matching the holes in the skins. To get the spacing right, I used the trailing edge wedge to mark the holes and drilled accordingly. I also made sure that the holes were not too far from the edge of the aluminum so that when clecoed in place, the aluminum did not extend beyond the trailing edge wedge on onto the "unsupported skin. I didn't want to mark the skin forward of the trailing edge. After gluing the wedge in place, I clecoed a section of the aluminum angle to either side of the control surface putting a cleco in every hole. My guess is that the clecos have a combined pressure in excess of anything you could get using the Van's recommended method. Anyway, after letting the glue dry I removed the clecos and riveted as per the instructions. The end result was rudder and elevator trailing edges that are straight as an arrow. I did weight the skins as required for vans but this was to ensure that the internal foam spacers were properly set in place as the adhesive cured. Attached is a small photo of one of the elevators with the angle aluminum installed. The other small deviation from the plans was the use of LePage PL2000 adhesive rather than tank sealant to glue the wedges in place. This was based on a recommendation of a local RV builder. Given the purpose of the adhesive it seems a reasonable change especially given that it is much easier to use (no mixing) than tank sealant and cures in hours. Cheers Les Kearney RV10 - # 40643 - Lost in the empennage ________________________________________________________________________________
Date: Dec 17, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: Riveting the elevators
Hi Page 9-12 details how to use the special elevator bucking bar. I bought this at Cleaveland Tools for $29 and worth every penny. I ended up using the bucking bar to do all the rivets on the on the rear spar. After scoping things out, I thought I could do a better job than reaching under with a different bucking bar. I am very pleased with then end result. When doing the rear spar, I was concerned about making sure that the bucking bar was placed correctly. It seemed a bit too easy to not insert the bar all the way. To prevent this I put the bar in and then marked a line across the bar where it went under the skin. This gave an easy reference to ensure it was always inserted fully. As well, I marked a small box centered on the end of the bar using a red marker. If I could see the red box through the rivet hole, I knew I the bar was properly centered. This may seem like overkill to some, but I am paranoid about riveting on the skins. When assembling & riveting the elevators, I completed the riveting on one before doing the second. As a consequence I realized that a small change in the assembly sequence made riveting Tip Rib Assembly (steps 4- 6 Page 9-14) a bit easier. In the case of the second elevator, I didn't rivet the skin to the aft spar outboard of the last E-1008 ribs. This made it much easier to get access to the to the Tip Rib Assembly rivets as the skin could be lifted much easier without fear of creasing the skin along a rivet line. Once the Tip Rib rivets were in place, I finished riveting the skin to the aft spar. Just my $0.02 from a weekend of plodding away.. Cheers Les Kearney RV10 # 40643 - Lost in the empennage ________________________________________________________________________________
From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com>
Subject: tailcone rivets
Date: Dec 18, 2006
Anyone have any good advice as to how to get at the top skin tailcone rivets? No one in my family is small. I also worry about climbing around in there and bending or denting somthing. Words from the wiser? Dave Leikam 40496 ________________________________________________________________________________
From: "Rene Felker" <rene(at)felker.com>
Subject: tailcone rivets
Date: Dec 18, 2006
You can check the archives and see if this is in there. But if I remember right Jesse Saint stood his up on end and had someone stand up in the middle. I had mine on a piece of carpet and then filled the bottom with foam and pillows and crawled on in. My then two year kept wanting to come in and play, but other than that it was not that bad. Rene' Felker _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dave Leikam Sent: Monday, December 18, 2006 6:35 AM Subject: RV10-List: tailcone rivets Anyone have any good advice as to how to get at the top skin tailcone rivets? No one in my family is small. I also worry about climbing around in there and bending or denting somthing. Words from the wiser? Dave Leikam 40496 ________________________________________________________________________________
Subject: tailcone rivets
Date: Dec 18, 2006
From: "Lloyd, Daniel R." <LloydDR(at)wernerco.com>
I also did it this way, carpet on the floor and pillows inside. Worked well, we had the offset back rivet from Avery, and the barbell bucking bar from them as well. Dan _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rene Felker Sent: Monday, December 18, 2006 8:54 AM Subject: RE: RV10-List: tailcone rivets You can check the archives and see if this is in there. But if I remember right Jesse Saint stood his up on end and had someone stand up in the middle. I had mine on a piece of carpet and then filled the bottom with foam and pillows and crawled on in. My then two year kept wanting to come in and play, but other than that it was not that bad. Rene' Felker _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dave Leikam Sent: Monday, December 18, 2006 6:35 AM Subject: RV10-List: tailcone rivets Anyone have any good advice as to how to get at the top skin tailcone rivets? No one in my family is small. I also worry about climbing around in there and bending or denting somthing. Words from the wiser? Dave Leikam 40496 www.aeroelectric.com www.kitlog.com http://www.matronics.com/Navigator?RV10-List ________________________________________________________________________________
Subject: tailcone rivets
Date: Dec 18, 2006
From: "Chris Johnston" <CJohnston(at)popsound.com>
Me same as everyone else. Pillows, blankets, girlfriend. See below - http://www.perfectlygoodairplane.net/Tailcone/tailconefinish.htm cj #40410 fuse www.perfectlygoodairplane.net -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Lloyd, Daniel R. Sent: Monday, December 18, 2006 6:21 AM Subject: RE: RV10-List: tailcone rivets I also did it this way, carpet on the floor and pillows inside. Worked well, we had the offset back rivet from Avery, and the barbell bucking bar from them as well. Dan ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rene Felker Sent: Monday, December 18, 2006 8:54 AM Subject: RE: RV10-List: tailcone rivets You can check the archives and see if this is in there. But if I remember right Jesse Saint stood his up on end and had someone stand up in the middle. I had mine on a piece of carpet and then filled the bottom with foam and pillows and crawled on in. My then two year kept wanting to come in and play, but other than that it was not that bad. Rene' Felker ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dave Leikam Sent: Monday, December 18, 2006 6:35 AM Subject: RV10-List: tailcone rivets Anyone have any good advice as to how to get at the top skin tailcone rivets? No one in my family is small. I also worry about climbing around in there and bending or denting somthing. Words from the wiser? Dave Leikam 40496 www.aeroelectric.com www.kitlog.com http://www.matronics.com/Navigator?RV10-List href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/c h ref="http://www.matronics.com/Navigator?RV10-List">http://www.matronics . com/Navigator?RV10-List ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: tailcone rivets
Date: Dec 18, 2006
Never had to get inside. Used two saw horses and kept flipping the tailcone on its side while I accessed through the open hole in the side or top. Open hole is the forward tailcone skin off. Leaning in, I was able to use the gun while my partener was on the outside with the bucking bar. Put down a lot of foam to protect your knees from the ground. The flatness of the tailcone side skins allows all this to happen by sitting on the saw horses. Becareful when stretching inside while standing, to get at the rivets towards the back, take breaks, otherwise you might get a bad cramp in your calves and hamstrings. John G. >From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com> >Reply-To: rv10-list(at)matronics.com >To: "matronics" >Subject: RV10-List: tailcone rivets >Date: Mon, 18 Dec 2006 07:34:58 -0600 > >Anyone have any good advice as to how to get at the top skin tailcone >rivets? No one in my family is small. I also worry about climbing around >in there and bending or denting somthing. Words from the wiser? > >Dave Leikam >40496 ________________________________________________________________________________
From: "Jesse Saint" <jesse(at)itecusa.org>
Subject: tailcone rivets
Date: Dec 18, 2006
This has worked great for us. Jesse Saint I-TEC, Inc. jesse(at)itecusa.org www.itecusa.org Cell: 352-427-0285 Fax: 815-377-3694 _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Chris Johnston Sent: Monday, December 18, 2006 11:40 AM Subject: RE: RV10-List: tailcone rivets Me same as everyone else. Pillows, blankets, girlfriend. See below - http://www.perfectlygoodairplane.net/Tailcone/tailconefinish.htm cj #40410 fuse www.perfectlygoodairplane.net -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Lloyd, Daniel R. Sent: Monday, December 18, 2006 6:21 AM Subject: RE: RV10-List: tailcone rivets I also did it this way, carpet on the floor and pillows inside. Worked well, we had the offset back rivet from Avery, and the barbell bucking bar from them as well. Dan _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rene Felker Sent: Monday, December 18, 2006 8:54 AM Subject: RE: RV10-List: tailcone rivets You can check the archives and see if this is in there. But if I remember right Jesse Saint stood his up on end and had someone stand up in the middle. I had mine on a piece of carpet and then filled the bottom with foam and pillows and crawled on in. My then two year kept wanting to come in and play, but other than that it was not that bad. Rene' Felker _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dave Leikam Sent: Monday, December 18, 2006 6:35 AM Subject: RV10-List: tailcone rivets Anyone have any good advice as to how to get at the top skin tailcone rivets? No one in my family is small. I also worry about climbing around in there and bending or denting somthing. Words from the wiser? Dave Leikam 40496 www.aeroelectric.com www.kitlog.com http://www.matronics.com/Navigator?RV10-List href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/chref "http://www.matronics.com/Navigator?RV10-List">http://www.matronics.com/Navi gator?RV10-List -- Please Support Your Lists This Month -- (And Get Some AWESOME FREE Gifts!) November is the Annual List Fund Raiser. Click on the Contribution link below to find out more about this year's Terrific Free Incentive Gifts provided by: * AeroElectric www.aeroelectric.com * The Builder's Bookstore www.buildersbooks.com * Aeroware Enterprises www.kitlog.com * HomebuiltHELP www.homebuilthelp.com List Contribution Web Site --> http://www.matronics.com/contribution Thank you for your generous support! -Matt Dralle, List Admin. - The RV10-List Email Forum - --> http://www.matronics.com/Navigator?RV10-List ________________________________________________________________________________
Subject: tailcone rivets
Date: Dec 18, 2006
From: "Stovall Todd Lt Col AF/A4RX" <Todd.Stovall(at)pentagon.af.mil>
All, After reading all of the posts to this thread, are most folks backriveting the tailcone skins vs bucking with a flush set, or did I misunderstand some of the posts? Using the backrivet set with a bucking bar never occurred to me. Although I'm only on my HS (ready to rivet), the tailcone is close enough for me to begin thinking about it. Thanks, Todd #40631 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Gonzalez Sent: Monday, December 18, 2006 1:15 PM Subject: RE: RV10-List: tailcone rivets --> Never had to get inside. Used two saw horses and kept flipping the tailcone on its side while I accessed through the open hole in the side or top. Open hole is the forward tailcone skin off. Leaning in, I was able to use the gun while my partener was on the outside with the bucking bar. Put down a lot of foam to protect your knees from the ground. The flatness of the tailcone side skins allows all this to happen by sitting on the saw horses. Becareful when stretching inside while standing, to get at the rivets towards the back, take breaks, otherwise you might get a bad cramp in your calves and hamstrings. John G. >From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com> >Reply-To: rv10-list(at)matronics.com >To: "matronics" >Subject: RV10-List: tailcone rivets >Date: Mon, 18 Dec 2006 07:34:58 -0600 > >Anyone have any good advice as to how to get at the top skin tailcone >rivets? No one in my family is small. I also worry about climbing >around in there and bending or denting somthing. Words from the wiser? > >Dave Leikam >40496 ________________________________________________________________________________
From: "Ben Westfall" <rv10(at)sinkrate.com>
Subject: tailcone rivets
Date: Dec 18, 2006
I stuffed my petite wife into the padded tailcone for riveting while it was resting on our EAA plans workbench. Don't worry about climbing in there if the table or surface your tailcone is sitting on is sturdy and fully supported. Just move slow and be careful about putting any weight on the ribs. She bucked all the j-channel and rib rivets. When riveting the longerons to the side skins we switched places and back riveted. That was sure quite a site cause I'm no small guy (6'3" and big!). The rivets came out excellent. If we were to do it again I think we would have back-riveted the j-channel and as much else as possible. For back riveting w/o using the steel plates we have a rather large bucking bar that weights 5 pounds or so and has a 3" round face that we got on ebay with our rivet gun. We are definitely faster when we can back rivet cause you don't have to be as paranoid about unintended dimples in the skins. Right now we are riveting the top skins to the ribs and spars. I made a 12" back rivet set from a longer set that came with our gun from ebay. Would have been much better to just buy one but this got us riveting over the weekend instead of waiting for it to show up after ordering. I definitely recommend the method of using a large bucking bar on the machine head side flush with the skin and back-riveting wherever possible. Specially for highly visible areas like the tailcone and wing top skins. Ben Westfall #40579 Wing Top Skins Portland, OR _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dave Leikam Sent: Monday, December 18, 2006 6:35 AM Subject: RV10-List: tailcone rivets Anyone have any good advice as to how to get at the top skin tailcone rivets? No one in my family is small. I also worry about climbing around in there and bending or denting somthing. Words from the wiser? Dave Leikam 40496 www.aeroelectric.com www.kitlog.com http://www.matronics.com/Navigator?RV10-List href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/chref "http://www.matronics.com/Navigator?RV10-List">http://www.matronics.com/Navi gator?RV10-List ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: tailcone rivets
Date: Dec 18, 2006
Back rivetting everything except where it is too small to get yourself in there...and that would be for and aft of the second to last bulkhead, the one the HS sit on. The Use the big elevator bucking bar and lay it down on the rivets, about ten at a time. John G. >From: "Stovall Todd Lt Col AF/A4RX" <Todd.Stovall(at)pentagon.af.mil> >Reply-To: rv10-list(at)matronics.com >To: >Subject: RE: RV10-List: tailcone rivets >Date: Mon, 18 Dec 2006 13:45:43 -0500 > > > >All, >After reading all of the posts to this thread, are most folks >backriveting the tailcone skins vs bucking with a flush set, or did I >misunderstand some of the posts? Using the backrivet set with a bucking >bar never occurred to me. Although I'm only on my HS (ready to rivet), >the tailcone is close enough for me to begin thinking about it. > >Thanks, >Todd >#40631 > >-----Original Message----- >From: owner-rv10-list-server(at)matronics.com >[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Gonzalez >Sent: Monday, December 18, 2006 1:15 PM >To: rv10-list(at)matronics.com >Subject: RE: RV10-List: tailcone rivets > >--> > >Never had to get inside. Used two saw horses and kept flipping the >tailcone on its side while I accessed through the open hole in the side >or top. Open hole is the forward tailcone skin off. Leaning in, I was >able to use the gun while my partener was on the outside with the >bucking bar. > >Put down a lot of foam to protect your knees from the ground. The >flatness of the tailcone side skins allows all this to happen by sitting >on the saw horses. Becareful when stretching inside while standing, to >get at the rivets towards the back, take breaks, otherwise you might get >a bad cramp in your calves and hamstrings. > >John G. > > > >From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com> > >Reply-To: rv10-list(at)matronics.com > >To: "matronics" > >Subject: RV10-List: tailcone rivets > >Date: Mon, 18 Dec 2006 07:34:58 -0600 > > > >Anyone have any good advice as to how to get at the top skin tailcone > >rivets? No one in my family is small. I also worry about climbing > >around in there and bending or denting somthing. Words from the wiser? > > > >Dave Leikam > >40496 > > ________________________________________________________________________________
From: David Maib <dmaib(at)mac.com>
Subject: Re: tailcone rivets
Date: Dec 18, 2006
John, Shooting from the inside, did you use the back rivet set? David Maib #40559 tailcone On Dec 18, 2006, at 12:14 PM, John Gonzalez wrote: Never had to get inside. Used two saw horses and kept flipping the tailcone on its side while I accessed through the open hole in the side or top. Open hole is the forward tailcone skin off. Leaning in, I was able to use the gun while my partener was on the outside with the bucking bar. Put down a lot of foam to protect your knees from the ground. The flatness of the tailcone side skins allows all this to happen by sitting on the saw horses. Becareful when stretching inside while standing, to get at the rivets towards the back, take breaks, otherwise you might get a bad cramp in your calves and hamstrings. John G. > From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com> > Reply-To: rv10-list(at)matronics.com > To: "matronics" > Subject: RV10-List: tailcone rivets > Date: Mon, 18 Dec 2006 07:34:58 -0600 > > Anyone have any good advice as to how to get at the top skin > tailcone rivets? No one in my family is small. I also worry about > climbing around in there and bending or denting somthing. Words > from the wiser? > > Dave Leikam > 40496 ________________________________________________________________________________
Date: Dec 18, 2006
From: "bruce breckenridge" <bbreckenridge(at)gmail.com>
Subject: RE: tailcone rivets
John Jessen recorded how I did mine. I looked on his website, but just couldn't find the pics! I used a back rivet plate; flipped the cone over on it's top and made sure it was on the plate. Because the cone overhung my table, I could stand in the hole of the missing forward top skin and lean into the cone. To be sure I was flat on the back rivet plate, I used a 1" (or so) round stick-on bubble level laid right next to the rivet I was going to smash. Because it was a little bit of a tight fit between the stringers, I could lean left or right and the cone would rotate until the bubble was centered. I don't recall having to drill out any of the rivets set with this method. Hopefully, John will pipe in and direct you to his website where this technique is documented. Bruce Breckenridge 40018 Wings ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: door latched security system
Date: Dec 18, 2006
I spoke with Vans this week and discussed the latching system and the warning lights. They indicated that the two incidents of the convertible RV10 both occurred on the same airplane before and then after the light system was installed. I am debating whether to install a Vans modified system or just depend on the checklist and physical feel of the pins. For flying 10s: have you installed the warning light system? Opinion of its usefulness? For building 10s: are you installing? I have run the wiring and designed a simpler system whereby a light for each side is red when the door is unlatched (without all the automotive reversing relays). ________________________________________________________________________________
From: JSMcGrew(at)aol.com
Date: Dec 18, 2006
Subject: Re: door latched security system
I installed all 4 magnetic switches and connected them in series to my Advanced Flight Systems AF-2500 engine monitor. Part of my checklist is to ensure the doors are closed both manually and by ensuring the "DOORS" indicator is extinguished on the display. If I forget, it gives an audible warning "CANOPY" when the RPM exceeds 1500. Hearing that would be a good reason to abort a takeoff. I'm happy with the way it works. I set the magnets just right: the system caught a passenger who had properly engaged the door latch, but had not locked the handle all the way down. Overall, it was easy because of my engine monitoring system, however, I wasn't very interested in wiring up that relay system they sent. I used one of the unused warning lights as a stall warning light. I'd noticed Van's had done that in N220RV. The light sits directly over my PFD and comes on along with the supplied stall buzzer. Jim 40134 In a message dated 12/18/2006 8:46:14 P.M. Eastern Standard Time, dlm46007(at)cox.net writes: I spoke with Vans this week and discussed the latching system and the warning lights. They indicated that the two incidents of the convertible RV10 both occurred on the same airplane before and then after the light system was installed. I am debating whether to install a Vans modified system or just depend on the checklist and physical feel of the pins. For flying 10s: have you installed the warning light system? Opinion of its usefulness? For building 10s: are you installing? I have run the wiring and designed a simpler system whereby a light for each side is red when the door is unlatched (without all the automotive reversing relays). (http://www.buildersbooks.com/) (http://www.homebuilthelp.com/) (http://www.matronics.com/contribution) (http://www.matronics.com/Navigator?RV10-List) Jim "Scooter" McGrew _http://www.mit.edu/~jsmcgrew_ (http://www.mit.edu/~jsmcgrew) ________________________________________________________________________________
From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com>
Subject: Re: tailcone rivets
Date: Dec 18, 2006
Stand the thing up and stand inside it. Back rivet all but a couple of rivets. My fifteen year old son on the outside with the bar and me on the inside driving rivits. Finished the cone tonight. Happy:) Thanks for the tip Jesse. Dave Leikam 40496 empanage assembly! ----- Original Message ----- From: "David Maib" <dmaib(at)mac.com> Sent: Monday, December 18, 2006 6:26 PM Subject: Re: RV10-List: tailcone rivets > > John, > > Shooting from the inside, did you use the back rivet set? > > David Maib > #40559 > tailcone > > On Dec 18, 2006, at 12:14 PM, John Gonzalez wrote: > > > > Never had to get inside. Used two saw horses and kept flipping the > tailcone on its side while I accessed through the open hole in the > side or top. Open hole is the forward tailcone skin off. Leaning > in, I was able to use the gun while my partener was on the outside > with the bucking bar. > > Put down a lot of foam to protect your knees from the ground. The > flatness of the tailcone side skins allows all this to happen by > sitting on the saw horses. Becareful when stretching inside while > standing, to get at the rivets towards the back, take breaks, > otherwise you might get a bad cramp in your calves and hamstrings. > > John G. > > >> From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com> >> Reply-To: rv10-list(at)matronics.com >> To: "matronics" >> Subject: RV10-List: tailcone rivets >> Date: Mon, 18 Dec 2006 07:34:58 -0600 >> >> Anyone have any good advice as to how to get at the top skin >> tailcone rivets? No one in my family is small. I also worry about >> climbing around in there and bending or denting somthing. Words >> from the wiser? >> >> Dave Leikam >> 40496 > > > > > > > > > > > > > ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Re: tailcone rivets
Date: Dec 18, 2006
I should have said, "I never placed my weight inside." The saw horses held it upside down on the flat spots on the rear where the HS sits and in the front where the longerons are without the most forward top skin on. Also lay it on it side, right or left because the sides are flat. Was on my knees, up inside, like a pup tent, shooting up or out to the side while the freind was on the outside. Yes, back riveted everything I could. I got pretty contorted, back, neck and thighs get twisted and lower legs fell asleep a few times. I have tried throughout the project to minimize putting any weight on the parts before complete assembly into a rigid structure. Never want to build in a warp albeit unlikely with all the indexed dimples and clecoes, but why risk it. Plus each bulkhead is so flimsy by itself, but once together with everything else, it's one strong unit. Make sure you and your helper are on the same rivet!!!!! They cover the rivet with the plate or bucking bar, on the outside and they say,"Ready" they you put the back rivet gun tip on the rivet and say" Ready" then they say, "Go" Lower the pressure and a quick fire and never fire again, unless you let them know by going through the same ritual. The guy that was hunting with Chenny taught me this technique after his incident. Unlikely that you will have an accident if you follow this plan. Alcoholic beverages are also not a good thing before hunting, opps, I mean riveting. John G. >From: David Maib <dmaib(at)mac.com> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: Re: RV10-List: tailcone rivets >Date: Mon, 18 Dec 2006 18:26:12 -0600 > > >John, > >Shooting from the inside, did you use the back rivet set? > >David Maib >#40559 >tailcone > >On Dec 18, 2006, at 12:14 PM, John Gonzalez wrote: > > >Never had to get inside. Used two saw horses and kept flipping the >tailcone on its side while I accessed through the open hole in the side or >top. Open hole is the forward tailcone skin off. Leaning in, I was able >to use the gun while my partener was on the outside with the bucking bar. > >Put down a lot of foam to protect your knees from the ground. The >flatness of the tailcone side skins allows all this to happen by sitting >on the saw horses. Becareful when stretching inside while standing, to get >at the rivets towards the back, take breaks, otherwise you might get a bad >cramp in your calves and hamstrings. > >John G. > > >>From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com> >>Reply-To: rv10-list(at)matronics.com >>To: "matronics" >>Subject: RV10-List: tailcone rivets >>Date: Mon, 18 Dec 2006 07:34:58 -0600 >> >>Anyone have any good advice as to how to get at the top skin tailcone >>rivets? No one in my family is small. I also worry about climbing >>around in there and bending or denting somthing. Words from the wiser? >> >>Dave Leikam >>40496 > > ________________________________________________________________________________
Date: Dec 19, 2006
From: MauleDriver <MauleDriver(at)nc.rr.com>
Subject: Re: tailcone rivets
Every bit of this tailcone riveting discussion is being digested by this builder despite the archives. Thanks! and HA HA! Keep it up. John Gonzalez wrote: > > I should have said, "I never placed my weight inside." The saw horses > held it upside down on the flat spots on the rear where the HS sits > and in the front where the longerons are without the most forward top > skin on. Also lay it on it side, right or left because the sides are > flat. > > Was on my knees, up inside, like a pup tent, shooting up or out to the > side while the freind was on the outside. Yes, back riveted > everything I could. I got pretty contorted, back, neck and thighs get > twisted and lower legs fell asleep a few times. > > I have tried throughout the project to minimize putting any weight on > the parts before complete assembly into a rigid structure. Never want > to build in a warp albeit unlikely with all the indexed dimples and > clecoes, but why risk it. Plus each bulkhead is so flimsy by itself, > but once together with everything else, it's one strong unit. > > Make sure you and your helper are on the same rivet!!!!! They cover > the rivet with the plate or bucking bar, on the outside and they > say,"Ready" they you put the back rivet gun tip on the rivet and say" > Ready" then they say, "Go" > > Lower the pressure and a quick fire and never fire again, unless you > let them know by going through the same ritual. > > The guy that was hunting with Chenny taught me this technique after > his incident. Unlikely that you will have an accident if you follow > this plan. Alcoholic beverages are also not a good thing before > hunting, opps, I mean riveting. > > John G. > > >> From: David Maib <dmaib(at)mac.com> >> Reply-To: rv10-list(at)matronics.com >> To: rv10-list(at)matronics.com >> Subject: Re: RV10-List: tailcone rivets >> Date: Mon, 18 Dec 2006 18:26:12 -0600 >> >> >> John, >> >> Shooting from the inside, did you use the back rivet set? >> >> David Maib >> #40559 >> tailcone >> >> On Dec 18, 2006, at 12:14 PM, John Gonzalez wrote: >> >> >> >> Never had to get inside. Used two saw horses and kept flipping the >> tailcone on its side while I accessed through the open hole in the >> side or top. Open hole is the forward tailcone skin off. Leaning >> in, I was able to use the gun while my partener was on the outside >> with the bucking bar. >> >> Put down a lot of foam to protect your knees from the ground. The >> flatness of the tailcone side skins allows all this to happen by >> sitting on the saw horses. Becareful when stretching inside while >> standing, to get at the rivets towards the back, take breaks, >> otherwise you might get a bad cramp in your calves and hamstrings. >> >> John G. >> >> >>> From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com> >>> Reply-To: rv10-list(at)matronics.com >>> To: "matronics" >>> Subject: RV10-List: tailcone rivets >>> Date: Mon, 18 Dec 2006 07:34:58 -0600 >>> >>> Anyone have any good advice as to how to get at the top skin >>> tailcone rivets? No one in my family is small. I also worry about >>> climbing around in there and bending or denting somthing. Words >>> from the wiser? >>> >>> Dave Leikam >>> 40496 >> >> >> >> >> >> >> >> >> >> >> > > ________________________________________________________________________________
From: "Vicki Jones" <vickiajones(at)hotmail.com>
Subject: Lower Motor Mount Tube Clearance
Date: Dec 19, 2006
The clearance between the oil sump on my Mattituck TMXIO-540 D4A5 and the lower mount tube is 1/8". I have heard that Van's recommends a minimum of 3/16" but prefers 1/2". Has anyone had a 1/8" clearance but not had the modification completed by Vans? If so, have you had any problems? Thanks, Vicki _________________________________________________________________ Your Hotmail address already works to sign into Windows Live Messenger! Get it now ________________________________________________________________________________
From: "John Jessen" <jjessen(at)rcn.com>
Subject: RE: tailcone rivets
Date: Dec 19, 2006
Bruce, I had to hide them because it's a family web site. That rear shot of your was just to provocative. Try this: http://www.soundingsresearch.com/RV-10/Techniques/Techniques_08.htm Also, I noticed some screwy things happening on the site, and at least one person has pointed this out to me. I'll try to get it fixed today. Still an amateur at this stuff. John Jessen #40328 (bah humbug to all this Holiday stuff; got me some deburrrrrrrring to do) _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of bruce breckenridge Sent: Monday, December 18, 2006 5:24 PM Subject: RV10-List: RE: tailcone rivets John Jessen recorded how I did mine. I looked on his website, but just couldn't find the pics! I used a back rivet plate; flipped the cone over on it's top and made sure it was on the plate. Because the cone overhung my table, I could stand in the hole of the missing forward top skin and lean into the cone. To be sure I was flat on the back rivet plate, I used a 1" (or so) round stick-on bubble level laid right next to the rivet I was going to smash. Because it was a little bit of a tight fit between the stringers, I could lean left or right and the cone would rotate until the bubble was centered. I don't recall having to drill out any of the rivets set with this method. Hopefully, John will pipe in and direct you to his website where this technique is documented. Bruce Breckenridge 40018 Wings -- 1:45 PM -- 1:45 PM ________________________________________________________________________________
Date: Dec 19, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: door latched security system - Door Closer
Anyone have a solution to add a rear handle. How would it attach to the fiberglass door? Would any reinforcement be necessary. Here is a photo of the Lancair closer <http://lrosen.nerv10.com/door%5Fhandle/> and also what looks like one on Vic's RV-10 <http://lrosen.nerv10.com/Construct/SunNFun_2006/Vic%20RV10/slides/2006-04-07-SnF-13.html> Larry Rosen #356 Tim Olson wrote: > > there is no rear handle. ________________________________________________________________________________
Date: Dec 19, 2006
From: MauleDriver <MauleDriver(at)nc.rr.com>
Subject: Using Sandpaper for various deburring tasks
I find that sandpaper on an aluminum block makes deburring long straight edges pretty easy. The disksander works well on smaller parts. I'm thinking of using a rubber block on some of those gently curving skins on the tailcone. Any thoughts on optimal grit and type of paper for this kind of work? Aluminum oxide would seem to be a good choice but I just don't know. What do you do? Noel and Yoshie I believe mentioned using sandpaper for some hole deburring - can you comment as to how and with what? I assume they are using a block on prepunched sheets to knock down the 'volcanoes'. Would you wait until after dimpling or while it's flat? BTW, thanks for the tip about using a dimpled piece of scrap for dimpling sheet that will need to accept another dimpled piece. Will be trying that. Thanks all, Bill "disassembling the tailcone and still riveting the elevator/trim tab" Watson #40605 ________________________________________________________________________________
Subject: Stall Warning and/or AOA
From: "Michael Wellenzohn" <michael(at)wellenzohn.net>
Date: Dec 19, 2006
Hello group, for those who are flying did you build the standard stall warning into the wing or an AOA or both? Thanks Michael #40511 (QB Wings) http://www.wellenzohn.net -------- RV-10 builder (wings) #511 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=82466#82466 ________________________________________________________________________________
Date: Dec 19, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: Using Sandpaper for various deburring tasks
Another question, I have to drill a hole to put in a pop rivet since I cannot get to the back side. I can ream the hole, how do I debur the back side? Larry MauleDriver wrote: > > I find that sandpaper on an aluminum block makes deburring long > straight edges pretty easy. The disksander works well on smaller > parts. I'm thinking of using a rubber block on some of those gently > curving skins on the tailcone. > > Any thoughts on optimal grit and type of paper for this kind of work? > Aluminum oxide would seem to be a good choice but I just don't know. > What do you do? > > Noel and Yoshie I believe mentioned using sandpaper for some hole > deburring - can you comment as to how and with what? I assume they > are using a block on prepunched sheets to knock down the 'volcanoes'. > Would you wait until after dimpling or while it's flat? BTW, thanks > for the tip about using a dimpled piece of scrap for dimpling sheet > that will need to accept another dimpled piece. Will be trying that. > > Thanks all, > Bill "disassembling the tailcone and still riveting the elevator/trim > tab" Watson #40605 > > ________________________________________________________________________________
Date: Dec 19, 2006
From: James Hein <n8vim(at)arrl.net>
Subject: Re: Using Sandpaper for various deburring tasks
>how do I debur the back side? Use a Cogsdil Burraway tool. <http://www.cogsdill.com/pdf%20files/usdeb_burraway.pdf> Nifty little tool... -Jim 40384 Larry Rosen wrote: > > Another question, I have to drill a hole to put in a pop rivet since I > cannot get to the back side. I can ream the hole, how do I debur the > back side? > > Larry > > MauleDriver wrote: >> >> I find that sandpaper on an aluminum block makes deburring long >> straight edges pretty easy. The disksander works well on smaller >> parts. I'm thinking of using a rubber block on some of those gently >> curving skins on the tailcone. >> >> Any thoughts on optimal grit and type of paper for this kind of >> work? Aluminum oxide would seem to be a good choice but I just don't >> know. What do you do? >> >> Noel and Yoshie I believe mentioned using sandpaper for some hole >> deburring - can you comment as to how and with what? I assume they >> are using a block on prepunched sheets to knock down the >> 'volcanoes'. Would you wait until after dimpling or while it's >> flat? BTW, thanks for the tip about using a dimpled piece of scrap >> for dimpling sheet that will need to accept another dimpled piece. >> Will be trying that. >> >> Thanks all, >> Bill "disassembling the tailcone and still riveting the elevator/trim >> tab" Watson #40605 >> >> >> >> >> >> >> > > ________________________________________________________________________________
Subject: Stall Warning and/or AOA
Date: Dec 19, 2006
From: "Chris Johnston" <CJohnston(at)popsound.com>
Went with only AOA. Riveted stall warning holes closed with 426 3-3 rivets. cj #40410 fuse www.perfectlygoodairplane.net -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Michael Wellenzohn Sent: Tuesday, December 19, 2006 9:54 AM Subject: RV10-List: Stall Warning and/or AOA Hello group, for those who are flying did you build the standard stall warning into the wing or an AOA or both? Thanks Michael #40511 (QB Wings) http://www.wellenzohn.net -------- RV-10 builder (wings) #511 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=82466#82466 ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Using Sandpaper for various deburring tasks
Date: Dec 19, 2006
One of the tols I think works great are the fingernail emory boards, not the normal ones with the red/brown/orange sandpaper, but the ones with the black sandpaper and thick sanding core backing. There are two grits one on each side. John >From: MauleDriver <MauleDriver(at)nc.rr.com> >Reply-To: rv10-list(at)matronics.com >To: RV10-List Digest Server >Subject: RV10-List: Using Sandpaper for various deburring tasks >Date: Tue, 19 Dec 2006 12:47:07 -0500 > > >I find that sandpaper on an aluminum block makes deburring long straight >edges pretty easy. The disksander works well on smaller parts. I'm >thinking of using a rubber block on some of those gently curving skins on >the tailcone. > >Any thoughts on optimal grit and type of paper for this kind of work? >Aluminum oxide would seem to be a good choice but I just don't know. What >do you do? > >Noel and Yoshie I believe mentioned using sandpaper for some hole deburring >- can you comment as to how and with what? I assume they are using a block >on prepunched sheets to knock down the 'volcanoes'. Would you wait until >after dimpling or while it's flat? BTW, thanks for the tip about using a >dimpled piece of scrap for dimpling sheet that will need to accept another >dimpled piece. Will be trying that. > >Thanks all, >Bill "disassembling the tailcone and still riveting the elevator/trim tab" >Watson #40605 > > ________________________________________________________________________________
From: "Noel & Yoshie Simmons" <noel(at)blueskyaviation.net>
Subject: Using Sandpaper for various deburring tasks
Date: Dec 19, 2006
In certain cases you can deburr like piper aircraft. Noel -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Larry Rosen Sent: Tuesday, December 19, 2006 11:11 AM Subject: Re: RV10-List: Using Sandpaper for various deburring tasks Another question, I have to drill a hole to put in a pop rivet since I cannot get to the back side. I can ream the hole, how do I debur the back side? Larry MauleDriver wrote: > > I find that sandpaper on an aluminum block makes deburring long > straight edges pretty easy. The disksander works well on smaller > parts. I'm thinking of using a rubber block on some of those gently > curving skins on the tailcone. > > Any thoughts on optimal grit and type of paper for this kind of work? > Aluminum oxide would seem to be a good choice but I just don't know. > What do you do? > > Noel and Yoshie I believe mentioned using sandpaper for some hole > deburring - can you comment as to how and with what? I assume they > are using a block on prepunched sheets to knock down the 'volcanoes'. > Would you wait until after dimpling or while it's flat? BTW, thanks > for the tip about using a dimpled piece of scrap for dimpling sheet > that will need to accept another dimpled piece. Will be trying that. > > Thanks all, > Bill "disassembling the tailcone and still riveting the elevator/trim > tab" Watson #40605 > > ________________________________________________________________________________
From: Jeff Carpenter <jeff(at)westcottpress.com>
Subject: Skin Edge Deburring
Date: Dec 19, 2006
I see some discussion today about edge deburring, and thought I'd share a method I learned from another 10 builder (Nick Gautier) a couple of miles from me. This technique has cut my edge deburring time from 15-20 minutes per large skin down to 2-3 minutes and it is unbelievably simple: Take a curved tooth file (with the handle removed) and run it lengthwise flat to the edge of the skin. On the return trip, run the file lengthwise at a 45 degree angle to the top side of the edge and make a final pass with the file lengthwise at a 45 degree angle to the bottom side of the edge. The result is an edge that is far smoother than anything I've been able to accomplish with my double edge deburring tool... or any other method I've fumbled around with. Jeff Carpenter 40304 ________________________________________________________________________________
Subject: door latched security system
Date: Dec 19, 2006
From: "Vern W. Smith" <Vern(at)teclabsinc.com>
Thanks, I think I understand the problem more clearly. Another fix maybe to build the door or hang the hinges with a preload so the back of the door always comes in contact with frame opening before the front of the door contacts the frame. Or maybe install a fisheye mirror somewhere to visual check the doors. Anyway, I look forward to this new challenge. Till then it's time to pound the rivets:) Vern (#324 fuselage) -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Deems Davis Sent: Tuesday, December 19, 2006 10:59 AM Subject: Re: RV10-List: door latched security system I don't think the 'flimsyness' of the doors is related to their stucture per se, (There is some reinforcement vis a glass matt that 'locks' the doors internally) but rather to the manner in which they are attached to the Cabin Cover. they are attached with 2 hinges that are aprox 12-14" apart at the top of the door. Physics and legerage take over when you open the door and the long moment between the wide bottom of the door where the latches are located and the relatively narrow hinge attachment makes for an easily twistable situation. I believe that most of the 'twist' comes from the immediate area that surrounds the hinges in at the top of the door. You could try reinforcing that area, but the inherant nature and flex of fiberglass is still going to be an issue IMHO. The windows are also smack dab in the middle of this area. Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ Vern W. Smith wrote: > >If the doors are a bit flimsy, would it work to run some foam and fiber >glass "spars" inside to frame work between the inside and outside >shells? >Just looking at the drawing if an X shaped frame work was added above >and below the window it seems like it would help. Downside is it would >add some weight to the doors. > >Vern (#324 fuselage) > ________________________________________________________________________________
Date: Dec 19, 2006
From: "Fred Williams, M.D." <drfred(at)suddenlinkmail.com>
Subject: AOA
I built in both. Makes sense not to put in the regular stall warning device, but I opted to have the other as an starting backup. As I understand it, the AOA will not be calibrated until one "flys " the unit. I didn't want to be flying my new 10 and not be able to recognize an approaching stall. I do plan to get transition training and from what I understand that is one of the first things that one goes over in the training. Fred Williams 40515 working on wings. ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: Re: door latched security system - Door Closer
Date: Dec 19, 2006
I plan to add a rear handle and the easy way to do it is create a couple of 1/2" circular hardpoints in the doors then drill and tap. Also considering adding another hand inserted pin for each door at the rear. ----- Original Message ----- From: "Larry Rosen" <LarryRosen(at)comcast.net> Sent: Tuesday, December 19, 2006 10:46 AM Subject: Re: RV10-List: door latched security system - Door Closer > > Anyone have a solution to add a rear handle. How would it attach to the > fiberglass door? Would any reinforcement be necessary. > > Here is a photo of the Lancair closer > <http://lrosen.nerv10.com/door%5Fhandle/> > and also what looks like one on Vic's RV-10 > <http://lrosen.nerv10.com/Construct/SunNFun_2006/Vic%20RV10/slides/2006-04-07-SnF-13.html> > > Larry Rosen > #356 > > Tim Olson wrote: >> >> there is no rear handle. > > > ________________________________________________________________________________
From: "Mark Ritter" <mritter509(at)msn.com>
Subject: AOA
Date: Dec 19, 2006
I believe you can order an AOA that is calibrated for the RV-10. Mine was and it works great. Mark (N410MR Flying) >From: "Fred Williams, M.D." <drfred(at)suddenlinkmail.com> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: RV10-List: AOA >Date: Tue, 19 Dec 2006 13:00:57 -0600 > > > >I built in both. Makes sense not to put in the regular stall warning >device, but I opted to have the other as an starting backup. As I >understand it, the AOA will not be calibrated until one "flys " the unit. >I didn't want to be flying my new 10 and not be able to recognize an >approaching stall. > >I do plan to get transition training and from what I understand that is one >of the first things that one goes over in the training. > >Fred Williams >40515 >working on wings. > > _________________________________________________________________ Fixing up the home? Live Search can help ________________________________________________________________________________
Subject: AOA
Date: Dec 19, 2006
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Rob at AFS has a predefined profile for the -10 built into his units that is supposed to be fairly accurate out of the box. Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Fred Williams, M.D. Sent: Tuesday, December 19, 2006 1:01 PM Subject: RV10-List: AOA I built in both. Makes sense not to put in the regular stall warning device, but I opted to have the other as an starting backup. As I understand it, the AOA will not be calibrated until one "flys " the unit. I didn't want to be flying my new 10 and not be able to recognize an approaching stall. I do plan to get transition training and from what I understand that is one of the first things that one goes over in the training. Fred Williams 40515 working on wings. ________________________________________________________________________________
Date: Dec 19, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: Setting the elevator trim tab hinge
Hi A local builder passed on his method for getting perfect alignment of the elevator trim tab when installing the piano hinge. Based on his instruction this is what I did: * Cut a piece of thin aluminum stock into a template strip the same size as the hinge to be installed. * Cleco clamped the template strip to the trim tab as if it was the hinge matching sure that the inboard side lined up with the trim tab * Match drilled the template to the trim tab and clecoed every hole * Fitted the trim tab with the template piece in place to the elevator setting up the alignment desired (a piece of angle aluminum made a great straight edge for alignment) * Matched drilled a few holes on the elevator side of the template (roughly evenly spaced) * Drew a rivet line on the trim tab side of the piano hinge and cleco clamped the template to it. Care was taken to ensure that the rivet line went through the center of each hole on the trim tab side of the template. * Match drilled the piano hinge using the template. All the holes, including the few on the elevator side were drilled. * The piano hinge was clecoed to the trim tab and the elevator and all remaining holes were match drilled. At that pointed I riveted everything together. The end result is a trim tab trailing edge that exactly matches the trailing edge of the elevator. As well the outboard alignment is exact as well. I guess this method works so well because it eliminates using the piano hinge for whole alignment (there is a small bit of play in the hinge). Attached are three of pictures. * One shows the template installed (I had to redo it because I didn't size it correctly so it doesn't match the next photo). The template still has the blue vinyl sheath still on so it is quite visible where the hinge is to be installed. * The next shows the alignment of the trim tab to the elevator after I had match drilled a couple of holes on the elevator side of the template. The angle aluminum at the bottom was used to set the alignment. * The final photo shows the end result Cheers Les ________________________________________________________________________________
From: JSMcGrew(at)aol.com
Date: Dec 19, 2006
Subject: Re: Stall Warning and/or AOA
I built in both AOA and the standard stall warning. The stall warning works very well once the tab is adjusted correctly. Even more importantly my RV-10 really lets me know when it is going to stall. After training with Mike Seager and practice during flight testing I would have to be extremely distracted to miss the buffet and feel of the airplane before it stalls (actual mileage may vary). Maybe I failed to calibrate the AOA system correctly the first, second or third times, but I can't get it to provide useful information. Additionally, the "AOA PUSH!" voice is extremely distracting during slow flight, take off and flare to land. (The calibration was bad on my first flight and I had to listen to that voice continuously during my first flight - as if I didn't have enough to deal with). I loved AOA in the T-38 and F-15. In theory, it is a very nice back up system to have on board. I haven't given up yet, but I am struggling to get it to provide useful information in the RV-10. Jim 40134 In a message dated 12/19/2006 12:57:22 P.M. Eastern Standard Time, michael(at)wellenzohn.net writes: --> RV10-List message posted by: "Michael Wellenzohn" Hello group, for those who are flying did you build the standard stall warning into the wing or an AOA or both? Thanks Michael #40511 (QB Wings) http://www.wellenzohn.net ________________________________________________________________________________
From: JSMcGrew(at)aol.com
Date: Dec 19, 2006
Subject: Re: Stall Warning and/or AOA
-----------------------------1166567309-- ________________________________________________________________________________
From: JSMcGrew(at)aol.com
Date: Dec 19, 2006
Subject: Re: Stall Warning and/or AOA
Just to follow up on my previous post. Overall, my recommendation is: If you are on the fence about getting AOA, get it. But, keep Van's stall warning system as well. Jim 40134 In a message dated 12/19/2006 5:31:43 P.M. Eastern Standard Time, JSMcGrew(at)aol.com writes: I built in both AOA and the standard stall warning. The stall warning works very well once the tab is adjusted correctly. Even more importantly my RV-10 really lets me know when it is going to stall. After training with Mike Seager and practice during flight testing I would have to be extremely distracted to miss the buffet and feel of the airplane before it stalls (actual mileage may vary). Maybe I failed to calibrate the AOA system correctly the first, second or third times, but I can't get it to provide useful information. Additionally, the "AOA PUSH!" voice is extremely distracting during slow flight, take off and flare to land. (The calibration was bad on my first flight and I had to listen to that voice continuously during my first flight - as if I didn't have enough to deal with). I loved AOA in the T-38 and F-15. In theory, it is a very nice back up system to have on board. I haven't given up yet, but I am struggling to get it to provide useful information in the RV-10. Jim 40134 ________________________________________________________________________________
Date: Dec 19, 2006
From: Bruce Patton <bpattonsoa(at)yahoo.com>
Subject: Re: Skin Edge Deburring
Yes, but always wear a leather glove. If you slip off the edge, the result is a nice long cut.=0A=0A=0A----- Original Message ----=0AFrom: Jeff Carpe nter =0ATo: rv10-list(at)matronics.com=0ASent: Tuesday , December 19, 2006 11:30:22 AM=0ASubject: RV10-List: Skin Edge Deburring s.com>=0A=0AI see some discussion today about edge deburring, and thought I 'd =0Ashare a method I learned from another 10 builder (Nick Gautier) a =0Acouple of miles from me. This technique has cut my edge deburring =0At ime from 15-20 minutes per large skin down to 2-3 minutes and it is =0Aun believably simple:=0A=0ATake a curved tooth file (with the handle removed) and run it =0Alengthwise flat to the edge of the skin. On the return tri p, run the =0Afile lengthwise at a 45 degree angle to the top side of the edge and =0Amake a final pass with the file lengthwise at a 45 degree angl e to =0Athe bottom side of the edge.=0A=0AThe result is an edge that is fa r smoother than anything I've been =0Aable to accomplish with my double ed ge deburring tool... or any other =0Amethod I've fumbled around with.=0A ========= ________________________________________________________________________________
From: "ddddsp1(at)juno.com" <ddddsp1(at)juno.com>
Date: Dec 20, 2006
Subject: Door latch and Weld-On for windows
Thinking about this door latch issue and WHY the original design is no t sufficient for some is interesting. I would be curious to see some of the planes that are having an issue as to whether #1 : The door was f it and mounted well. #2 : Is the interior cloth/leather on the door i mpacting how it closes PRIOR to finishing it? It seems a lot of the t imes our modifications to make the plane nicer/attractive changes how th e plane was designed to work. We wonder after we get all done why it w eighs 90 lbs. more than other RV10's. Just a thought. Also, I called Vans today to order some K1100-8 nutplates (that they do not send enough of with the kit and 4 more dimpled END LUG nut plates w hich they send only 2 of), and asked about my out dated Weld-On. The we bsite and catalog says it has a shelf life of 12 months. I was told NO. .......it is only a 6 month shelf life! Could this be the cause of some of the CRACKING around the windows we are seeing on the RV10? Sure wou ld be nice if Van told people to NOT order the Weld-on until they are re ady to use it! I know when we got ours it was already on the shelf for 3 months. Hopes this saves others some trouble. Anybody wants 5 bottles of Weld-On ...........CHEAP? :) Venting, Dean 40449 ________________________________________________________________________

  Thinking about this door latch issue and WHY the origina l design is not sufficient for some is interesting.  I would be cur ious to see some of the planes that are having an issue as to whether&nb sp; #1 :  The door was fit and mounted well.   #2 :  Is the interior cloth/leather on the door impacting how it closes PRIOR to finishing it?    It seems a lot of the times our modi fications to make the plane nicer/attractive changes how the plane was d esigned to work.   We wonder after we get all done why it weig hs 90 lbs. more than other RV10's.  Just a thought.

Also,  I called Vans today to order some K1100-8 nutplates (that they do not send enough of with the kit and 4 more dimpled END LUG nut plates which they send only 2 of), and asked about my out dated Weld-On.   The website and catalog says it has a shelf life of 12 months.&nb sp; I was told NO........it is only a 6 month shelf life!  Could th is be the cause of some of the CRACKING around the windows we are seeing on the RV10?  Sure would be nice if Van told people to NOT order t he Weld-on until they are ready to use it!  I know when we got ours it was already on the shelf for 3 months.  Hopes this saves others some trouble.

Anybody wants 5 bottles of Weld-On ...........CHEAP?  :) 

Venting, 

Dean  40449



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From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Door latch and Weld-On for windows
Date: Dec 19, 2006
It is amazing that these chemicals have such a short self life. Why can McDonalds make hamburger buns last five months on the tray before they get mold or make meet which can go through ones digestive tract and come out the other end still looking like the meat patty when it went in? And these chemicals aren't even made for consumption. Go figure! I feel your pain. I've got a third right elevator trim tab bonded with an unproven flexible epoxy. My proseal was out of date. Leaves one with a dought and it keeps the economy going by forcing people to spend $$$$$$ to buy only that which the manual says to use. Yesterdays trailing edge bonding issue comes to mind. John G >From: "ddddsp1(at)juno.com" <ddddsp1(at)juno.com> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: RV10-List: Door latch and Weld-On for windows >Date: Wed, 20 Dec 2006 02:02:52 GMT > > Thinking about this door latch issue and WHY the original design is not >sufficient for some is interesting. I would be curious to see some of the >planes that are having an issue as to whether #1 : The door was fit and >mounted well. #2 : Is the interior cloth/leather on the door impacting >how it closes PRIOR to finishing it? It seems a lot of the times our >modifications to make the plane nicer/attractive changes how the plane was >designed to work. We wonder after we get all done why it weighs 90 lbs. >more than other RV10's. Just a thought. >Also, I called Vans today to order some K1100-8 nutplates (that they do >not send enough of with the kit and 4 more dimpled END LUG nut plates which >they send only 2 of), and asked about my out dated Weld-On. The website >and catalog says it has a shelf life of 12 months. I was told NO........it >is only a 6 month shelf life! Could this be the cause of some of the >CRACKING around the windows we are seeing on the RV10? Sure would be nice >if Van told people to NOT order the Weld-on until they are ready to use it! > I know when we got ours it was already on the shelf for 3 months. Hopes >this saves others some trouble. >Anybody wants 5 bottles of Weld-On ...........CHEAP? :) >Venting, >Dean 40449 > > >________________________________________________________________________ ________________________________________________________________________________
Subject: Door latch and Weld-On for windows
Date: Dec 19, 2006
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Keep your WeldOn in the freezer until you are ready to use it. It will greatly increase the shelf life. Michael From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of ddddsp1(at)juno.com Sent: Tuesday, December 19, 2006 8:03 PM Subject: RV10-List: Door latch and Weld-On for windows Thinking about this door latch issue and WHY the original design is not sufficient for some is interesting. I would be curious to see some of the planes that are having an issue as to whether #1 : The door was fit and mounted well. #2 : Is the interior cloth/leather on the door impacting how it closes PRIOR to finishing it? It seems a lot of the times our modifications to make the plane nicer/attractive changes how the plane was designed to work. We wonder after we get all done why it weighs 90 lbs. more than other RV10's. Just a thought. Also, I called Vans today to order some K1100-8 nutplates (that they do not send enough of with the kit and 4 more dimpled END LUG nut plates which they send only 2 of), and asked about my out dated Weld-On. The website and catalog says it has a shelf life of 12 months. I was told NO........it is only a 6 month shelf life! Could this be the cause of some of the CRACKING around the windows we are seeing on the RV10? Sure would be nice if Van told people to NOT order the Weld-on until they are ready to use it! I know when we got ours it was already on the shelf for 3 months. Hopes this saves others some trouble. Anybody wants 5 bottles of Weld-On ...........CHEAP? :) Venting, Dean 40449 ________________________________________________________________________ ________________________________________________________________________________
From: "Marcus Cooper" <coop85(at)bellsouth.net>
Subject: Lower Motor Mount Tube Clearance
Date: Dec 19, 2006
Vicki, Mine was a little over 1/8" so I checked with Van's and they said it wouldn't be a problem. To date with 119 hours it hasn't been an issue. However you could always check with Vans again to see if they have any newer thoughts. Marcus -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Vicki Jones Sent: Tuesday, December 19, 2006 9:24 AM Subject: RV10-List: Lower Motor Mount Tube Clearance The clearance between the oil sump on my Mattituck TMXIO-540 D4A5 and the lower mount tube is 1/8". I have heard that Van's recommends a minimum of 3/16" but prefers 1/2". Has anyone had a 1/8" clearance but not had the modification completed by Vans? If so, have you had any problems? Thanks, Vicki _________________________________________________________________ Your Hotmail address already works to sign into Windows Live Messenger! Get it now ________________________________________________________________________________
Subject: Re: Stall Warning and/or AOA
From: "Michael Wellenzohn" <michael(at)wellenzohn.net>
Date: Dec 20, 2006
Thanks you guys for the input. Michael do nor archive -------- RV-10 builder (wings) #511 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=82593#82593 ________________________________________________________________________________
From: "Russell Daves" <dav1111(at)cox.net>
Subject: Re: door latched security system - Door Closer
Date: Dec 20, 2006
I put a rear handle on my doors so it was easier to pull in the rear part of the door before closing the door handle. I used rivnuts into the inside door frame and made a cloth handle with grommets in each end and screwed it on. Works great to make sure the rear part of the door can be pulled in tight enough to allow both the front and rear pins to slide into the frame. I also as part of the pre-flight manually check both the pilots door and passenger door pins are fully seated by feel. My pilots door DID NOT come off during one of my test flights, however it came open on takeoff and I was lucky enough to have made a long pull down loop strap that I was able to grab with my left hand while making sure I was still flying the airplane and hold the door down enough to keep it from coming completely off while I advised the tower I had a problem and needed to come back around for landing. I made a somewhat normal close in downwind, base and final, landed and had to replace a bent hinge and do a little fiberglass work around the rear hinge which had pulled out. It is imperative to manually check each pin, front and rear, on each door as part of the pre-departure check list. The doors are in my opinion the weakest part of the Van's RV-10 design, but it is without a doubt the best airplane I have every flown in my 1500+ hours (owned 7, including an RV-6A). Russ Daves N710RV First Flight 7/28/06 ________________________________________________________________________________
Date: Dec 20, 2006
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: door latched security system - Door Closer
I don't want to make you a bad guy Russ....but get a feel for this with an honest question. Were you very diligent about checking the pin before this happened, or did this incident really set you in motion for doing it as part of a good preflight check? I'm just not yet installed on the warning kit, but I really don't think I could trust myself to simply rely on a latch warning kit any more than I could be trusted to check the pins. I heard way back about a door coming off, so I never really had a period where I wasn't checking the pins...but not everyone had heard these stories before, so it may be different for them. I'm just trying to get a feel for how it was for you. Tim Olson - RV-10 N104CD - 180 hrs Russell Daves wrote: > I put a rear handle on my doors so it was easier to pull in the rear > part of the door before closing the door handle. I used rivnuts into > the inside door frame and made a cloth handle with grommets in each end > and screwed it on. Works great to make sure the rear part of the door > can be pulled in tight enough to allow both the front and rear pins to > slide into the frame. > > I also as part of the pre-flight manually check both the pilots door and > passenger door pins are fully seated by feel. > > My pilots door DID NOT come off during one of my test flights, however > it came open on takeoff and I was lucky enough to have made a long pull > down loop strap that I was able to grab with my left hand while making > sure I was still flying the airplane and hold the door down enough to > keep it from coming completely off while I advised the tower I had a > problem and needed to come back around for landing. > > I made a somewhat normal close in downwind, base and final, landed and > had to replace a bent hinge and do a little fiberglass work around the > rear hinge which had pulled out. > > It is imperative to manually check each pin, front and rear, on each > door as part of the pre-departure check list. > > The doors are in my opinion the weakest part of the Van's RV-10 design, > but it is without a doubt the best airplane I have every flown in my > 1500+ hours (owned 7, including an RV-6A). > > Russ Daves > N710RV First Flight 7/28/06 > > > * > > > * ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: Re: door latched security system - Door Closer
Date: Dec 20, 2006
One other thing I saw a small knob that could be threaded into a single hardpoint; just something to grab to pull the door fully in before using the door handle. ----- Original Message ----- From: Russell Daves To: rv10-list(at)matronics.com Sent: Wednesday, December 20, 2006 4:40 AM Subject: Re: RV10-List: door latched security system - Door Closer I put a rear handle on my doors so it was easier to pull in the rear part of the door before closing the door handle. I used rivnuts into the inside door frame and made a cloth handle with grommets in each end and screwed it on. Works great to make sure the rear part of the door can be pulled in tight enough to allow both the front and rear pins to slide into the frame. I also as part of the pre-flight manually check both the pilots door and passenger door pins are fully seated by feel. My pilots door DID NOT come off during one of my test flights, however it came open on takeoff and I was lucky enough to have made a long pull down loop strap that I was able to grab with my left hand while making sure I was still flying the airplane and hold the door down enough to keep it from coming completely off while I advised the tower I had a problem and needed to come back around for landing. I made a somewhat normal close in downwind, base and final, landed and had to replace a bent hinge and do a little fiberglass work around the rear hinge which had pulled out. It is imperative to manually check each pin, front and rear, on each door as part of the pre-departure check list. The doors are in my opinion the weakest part of the Van's RV-10 design, but it is without a doubt the best airplane I have every flown in my 1500+ hours (owned 7, including an RV-6A). Russ Daves N710RV First Flight 7/28/06 ________________________________________________________________________________
From: "Eric Parlow" <ericparlow(at)hotmail.com>
Subject: MT Prop?
Date: Dec 20, 2006
I'm considering buying the 3B MT prop from Van's. Primary reason is the lower weight (47.7 lbs) will help off-set the weight of the turbo. Any feedback on how your experience was with MT/Van's/Prop Assy Shop? Suggestions or other alternatives? Also it's a 12 week lead time + assembly time :-( ERic-- 40014 ________________________________________________________________________________
Subject: MT Prop?
Date: Dec 20, 2006
From: "John W. Cox" <johnwcox(at)pacificnw.com>
Eric, which turbo were you going with? How were you dealing with the lower cowl for distance and heat separation? Is this the same kit that Rick Conti had for sale? John Cox #40600 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Eric Parlow Sent: Wednesday, December 20, 2006 5:28 AM Subject: RV10-List: MT Prop? I'm considering buying the 3B MT prop from Van's. Primary reason is the lower weight (47.7 lbs) will help off-set the weight of the turbo. Any feedback on how your experience was with MT/Van's/Prop Assy Shop? Suggestions or other alternatives? Also it's a 12 week lead time + assembly time :-( ERic-- 40014 ________________________________________________________________________________
Subject: door latched security system - Door Closer
Date: Dec 20, 2006
From: "Tom Deutsch" <deutscht(at)rhwhotels.com>
Russ, The best thing about your post below is that you first "flew the plane". I have been in the flight training business for 34 years and have personal knowledge of several fatalities because of lesser incidences (lost fuel caps, open baggage doors, ect.) GOOD JOB!!!!! To the rest of us NEVER, NEVER quit flying the plane! Even if a door does come off. Tom Deutsch, 40545 Waiting to paint ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of David McNeill Sent: Wednesday, December 20, 2006 7:14 AM Subject: Re: RV10-List: door latched security system - Door Closer One other thing I saw a small knob that could be threaded into a single hardpoint; just something to grab to pull the door fully in before using the door handle. ----- Original Message ----- From: Russell Daves <mailto:dav1111(at)cox.net> To: rv10-list(at)matronics.com Sent: Wednesday, December 20, 2006 4:40 AM Subject: Re: RV10-List: door latched security system - Door Closer I put a rear handle on my doors so it was easier to pull in the rear part of the door before closing the door handle. I used rivnuts into the inside door frame and made a cloth handle with grommets in each end and screwed it on. Works great to make sure the rear part of the door can be pulled in tight enough to allow both the front and rear pins to slide into the frame. I also as part of the pre-flight manually check both the pilots door and passenger door pins are fully seated by feel. My pilots door DID NOT come off during one of my test flights, however it came open on takeoff and I was lucky enough to have made a long pull down loop strap that I was able to grab with my left hand while making sure I was still flying the airplane and hold the door down enough to keep it from coming completely off while I advised the tower I had a problem and needed to come back around for landing. I made a somewhat normal close in downwind, base and final, landed and had to replace a bent hinge and do a little fiberglass work around the rear hinge which had pulled out. It is imperative to manually check each pin, front and rear, on each door as part of the pre-departure check list. The doors are in my opinion the weakest part of the Van's RV-10 design, but it is without a doubt the best airplane I have every flown in my 1500+ hours (owned 7, including an RV-6A). Russ Daves N710RV First Flight 7/28/06 href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/c h ref="http://www.matronics.com/Navigator?RV10-List">http://www.matronics . com/Navigator?RV10-List ________________________________________________________________________________
From: "Mark Ritter" <mritter509(at)msn.com>
Subject: MT Prop?
Date: Dec 20, 2006
Eric, I purchased my MT Prop from Jim Ayers at Less Drag. It came fully assembled and bolted right on. No problems and really think you will be pleased with the performance of the 3 blades. Jim was running some group buy specials and my recall is I saved some money buying from Less Drag. Mark (N410MR Flying) >From: "Eric Parlow" <ericparlow(at)hotmail.com> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: RV10-List: MT Prop? >Date: Wed, 20 Dec 2006 08:28:00 -0500 > > >I'm considering buying the 3B MT prop from Van's. > >Primary reason is the lower weight (47.7 lbs) will help off-set the weight >of the turbo. > >Any feedback on how your experience was with MT/Van's/Prop Assy Shop? > >Suggestions or other alternatives? > >Also it's a 12 week lead time + assembly time :-( > >ERic-- >40014 > > _________________________________________________________________ Fixing up the home? Live Search can help ________________________________________________________________________________
Subject: door latched security system - Door Closer
Date: Dec 20, 2006
From: "Tom Deutsch" <deutscht(at)rhwhotels.com>
Were are you guys positioning the rear handle so us with bad shoulders can reach around and grab it? Photos would help. Tom Deutsch ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Russell Daves Sent: Wednesday, December 20, 2006 5:40 AM Subject: Re: RV10-List: door latched security system - Door Closer I put a rear handle on my doors so it was easier to pull in the rear part of the door before closing the door handle. I used rivnuts into the inside door frame and made a cloth handle with grommets in each end and screwed it on. Works great to make sure the rear part of the door can be pulled in tight enough to allow both the front and rear pins to slide into the frame. I also as part of the pre-flight manually check both the pilots door and passenger door pins are fully seated by feel. My pilots door DID NOT come off during one of my test flights, however it came open on takeoff and I was lucky enough to have made a long pull down loop strap that I was able to grab with my left hand while making sure I was still flying the airplane and hold the door down enough to keep it from coming completely off while I advised the tower I had a problem and needed to come back around for landing. I made a somewhat normal close in downwind, base and final, landed and had to replace a bent hinge and do a little fiberglass work around the rear hinge which had pulled out. It is imperative to manually check each pin, front and rear, on each door as part of the pre-departure check list. The doors are in my opinion the weakest part of the Van's RV-10 design, but it is without a doubt the best airplane I have every flown in my 1500+ hours (owned 7, including an RV-6A). Russ Daves N710RV First Flight 7/28/06 ________________________________________________________________________________
Date: Dec 20, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Re: MT Prop?
I ordered mine through Jim Ayers at Less Drag Products. 20 week lead time but including assembly. Jim offered a group buy back a few years (wish I had hopped on it) and I like the fact I can pick up the phone and get an answer right away. He is also an authorized MT repair & assembly facility. I know I can get service after the sale with him. The cost from Van's may seem less but there are some charges that creep up like customs fees and shipping from several locations. He will let you know the most cost effective method up front, I have to pick mine up at customs but it will be fully assembled and I have a port of entry here in Las Vegas. If your assembler is far from a port of entry, they will need to pick it up$$, clear and pay customs$$, assemble$$ recrate and ship to you$$. Lots of variables. Contact him at the below address, he knows the props very well. http://www.lessdrag.com Rick S. 40185 ________________________________________________________________________________
Date: Dec 20, 2006
From: linn Walters <pitts_pilot(at)bellsouth.net>
Subject: door latched security system - Door Closer
I don't know if I have enough knowledge to comment here, so I'll ask a few questions? Why not add switches (sub-micro or reed) to the door to detect proper closure and wire them to disable the starter relay if the door isn't closed properly? Is the closure problem related all the door pins or just one or two per door? (how many pins are there???) As for the 'dings' when the door is closed with the latch pins out ..... would a piece of stainless embedded in the frame minimize the damage?? Linn ...... getting closer to my own kit! ________________________________________________________________________________
Subject: Carpet Install
Date: Dec 20, 2006
From: "Tom Deutsch" <deutscht(at)rhwhotels.com>
Does anyone have any good ideas on how to fasten the carpet and still keep it removable? I planned to use Velcro but it doesn't seem to stick to the carpet backing well enough. Tom Deutsch, #40545 ________________________________________________________________________________
From: "Jesse Saint" <jesse(at)itecusa.org>
Subject: door latched security system - Door Closer
Date: Dec 20, 2006
Answers below. Jesse Saint I-TEC, Inc. jesse(at)itecusa.org www.itecusa.org Cell: 352-427-0285 Fax: 815-377-3694 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of linn Walters Sent: Wednesday, December 20, 2006 8:29 AM Subject: RV10-List: door latched security system - Door Closer I don't know if I have enough knowledge to comment here, so I'll ask a few questions? Why not add switches (sub-micro or reed) to the door to detect proper closure and wire them to disable the starter relay if the door isn't closed properly?[Jesse Saint] When it is hot out it is nice to have the door open when you are taxiing to keep from getting killed by the heat before takeoff. Is the closure problem related all the door pins or just one or two per door? (how many pins are there???)[Jesse Saint] There are front and back pins. I have seen the front pin not make it in when the back does, but this is not really the problem, since you can see that easily when you close it. The back pin is harder to see from the front seat, especially from the same side as the door is on. From the opposite front seat it is a lot easier to see/check. As for the 'dings' when the door is closed with the latch pins out ..... would a piece of stainless embedded in the frame minimize the damage??[Jesse Saint] Yes, did you see my pictures? Linn ...... getting closer to my own kit! -- 1:17 PM ________________________________________________________________________________
Date: Dec 20, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Re: Carpet Install
Tom, The velcro I have seen on the carpet had been sewn to the carpet. Hot glue may be a good option though, similar to the seaming tape used on carpet. Rick S. 40185 ________________________________________________________________________________
From: <rvmail(at)thelefflers.com>
Subject: New RV Builder
Date: Dec 20, 2006
It's official...... I'm builder 40684 and the empennage kit is on the way. ________________________________________________________________________________
Subject: Trutrak Flatpack dimensions?
Date: Dec 20, 2006
From: "Chris Johnston" <CJohnston(at)popsound.com>
Hey all - Looked all over and can't seem to find what I'm lookin fer... anyone have dimensions on the "flat pack" controller for a Trutrak Digiflight IIVSGV? Thanks! cj #40410 fuse www.perfectlygoodairplane.net ________________________________________________________________________________
Date: Dec 20, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: Trutrak Flatpack dimensions?
Chris, I think I've got it in some of the documentation I have, I'm tied up right now (fiberglass) but if you don't hear from someone else, I'll get it and send it later this PM. Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ Chris Johnston wrote: > >Hey all - > >Looked all over and can't seem to find what I'm lookin fer... anyone >have dimensions on the "flat pack" controller for a Trutrak Digiflight >IIVSGV? > >Thanks! >cj >#40410 >fuse >www.perfectlygoodairplane.net > > > > ________________________________________________________________________________
From: "eagerlee" <eagerlee(at)comcast.net>
Subject: Skin Edge Deburring
Date: Dec 20, 2006
The best advice on the deburring of edge of skins came to me from a seasoned vet. He took a 6" stainless steel machinist ruler used as a knife and passed over the edge at about a 45=BA angle. Two passes in each direction ( ten seconds max) and the edge was deburred and burnished to a smooth finish. I use it every time now. Paul Hahn ________________________________________________________________________________
Subject: Re: New RV Builder
From: Michael D Chase <MChase(at)gdatp.com>
Date: Dec 20, 2006
Welcome I was builder 40644 starting back in October, boy it is getting crowded:-) Michael Chase General Dynamics Armament and Technical Products 802-657-6029 Office 802-922-5930 Cell mchase(at)gdatp.com This e-mail message (including attachments, if any) is for the sole use of the intended recipient(s) and may contain information that is private, confidential, or exempt from disclosure. Any unauthorized review, use, copying, printing, disclosure, retention, or distribution is strictly prohibited. If you are not the intended recipient, please contact the sender by reply to this e-mail, and delete all copies without disclosing this message to others. Thank you. Sent by: owner-rv10-list-server(at)matronics.com 12/20/2006 01:41 PM Please respond to rv10-list To: cc: Subject: RV10-List: New RV Builder It's official...... I'm builder 40684 and the empennage kit is on the way. ________________________________________________________________________________
From: "Eric Parlow" <ericparlow(at)hotmail.com>
Subject: MT Prop? (now Turbo)
Date: Dec 20, 2006
We're using a TIO-540-AK1A core from a Cessna T182T. The AK1 is rated(or de-rated) at 235 bhp, 2400 rpm, to 20k ft. Turning 2700 rpm it puts out 260 bhp. The IO-540-D4A5 weighs 400 lbs which does not include the exhaust system. The TIO-540-AK1A weighs of 472 lbs. including the exhaust system. We've calculated the installed engine weight to be +50 lbs over the IO. The CG is 0.5" lower and 1" farther aft. To help off-set the difference we've choosen to use the MT 3B prop (47 lbs vs 57 lbs Hartzell 2B). The prop CG is 25" forward of the engine CG. Which gives 10 lbs reduction of prop equals 15.2 lbs of engine increase to keep the same CG. Now we're down to 35 lbs difference from a IO-540-D4A5 with a Hartzell 2B. To maintain the forward CG limit of 107.84 with a 200 lbs pilot and no fuel the result is: -IO-540-D4A5 with Hartzell 2B requires 6 lbs in the baggage (1863 lbs net weight) -TIO-540-AK1A with MT requires 40 lbs in the baggage (1937 lbs net weight) Resulting in a 74 lbs gross weight penalty for single pilot flying with the turbo. I'll just have to carry a 5 gal can of water around with me, or maybe an A/C unit in back! The cowl will be modified to fit around the turbo and a relocated air inlet. Initial fit-up shows the lowest point of the turbo(oil drain) is approx 2" outside the current cowl envelope. This point is even with the level of the bottom of current cowl's air inlet/cooling outlet area but off to the left side 9". Which results in adding a 3" deep speed bulge to the lower left side of the cowl in a localized area. Yes, it was his kit. ERic-- FWF 40014 ________________________________________________________________________________
Date: Dec 20, 2006
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: switches?
You've got some good answers already Chris, but I'll try to explain mine, and in a different way. You can either do a double-pole double-throw, or you can get a quad-pole switch. There are 2 ARINC lines, and 1 serial lines that are in question. The serial line just gets the GPS position data from the GPS, so the Autopilot knows it's TRK. If you don't provide GPS, it would only know heading. The ARINC does the controlling of the autopilot. So now it gets fun... You can leave your Serial switch on one GPS all the time if you wish, if you have a GPS you can count on. Your ARINC you may want to switch between an EFIS or a NAV/COM/GPS unit. I have my Cheltons or my GNS480 drive my autopilot. Now, on the panel is a source select switch for those 2 systems. That one just switches the ARINC lines, in my case. So I can control the system from either source. My GPS signal I have on an under-panel hidden switch, that can select between my Chelton GPS, or the GNS-480. This switch I usually leave on the GNS-480 side, because that's my WAAS GPS that supposedly would be top notch. However, I did put the switch there, because if I need to run at minimum power draw, my GNS-480 is getting the boot and it shuts off with the master, when I'm running E-bus only. So therefore, I wanted a switch behind the panel that I could move to the other side for GPS source. It's just on a little L bracket on the panel so it's easy to feel for and find. Now for the stick stuff. I really like the way I did it, and here's how and why. On my panel I have a switch labeled like TRIM CONTROL - Pilot / Co-Pilot The labeling isn't what I'd want, and you'll see why. My PILOT side stick is always active, for everything. I didn't want ANY switch to knock me out of control. I will not let most anyone fly my plane from the Left seat. My CO-Pilot stick, however, has the switches for Trims, Frequency flip-flops, and anything else that I deemed something that the kids or another person could bump or mess with, as "restricted" devices. When the switch is in the PILOT position (should read PILOT ONLY), then those items have their grounds cut off....so the switches don't function. When it's in the Co-Pilot position (Should read PILOT/CO-PILOT), then those grounds are available and the functions will work. This allows me to basically deactivate that stick for all but a couple things, like PTT, unless I want it activated. When I fly with the wife, it's usually activated. When the kids come up, it's rarely activated. It works very well and should help keep people from bumping things they shouldn't. Note that since it's just one ground, the switch can be a SPST if you wish. There isn't a center position. Tim Olson - RV-10 N104CD - Flying Chris Johnston wrote: > > Hey all - > > I'm trying to nail down some ancillary components for the panel, and > have a couple of questions. For those of you who have installed a > trutrak ap, how many poles and throws are required of the switch that > switches the AP source from a NAV radio to the GPS (chelton)? I > couldn't find a reference to it in the Trutrak installation > instructions. Also, I plan to have a switch that will move all functions > except PTT from the pilot to co-pilot side. Are people using relays to > accomplish this? if so, I suspect a SPST or SPDT switch would fit the > bill? I'm away from all my reference materials, and I'm trying to nail > down what I need to order. > > Thanks all! > cj > #40410 > fuse > www.perfectlygoodairplane.net > ________________________________________________________________________________
From: "DejaVu" <wvu(at)ameritel.net>
Subject: Re: Carpet Install
Date: Dec 20, 2006
I used snap buttons - 1/2 fastened to the floor pans before they were rivet ed in place, 1/2 fastened to the carpet. I may sew velcro on the carpet la ter if needed. Anh ----- Original Message ----- From: Tom Deutsch To: rv10-list(at)matronics.com Sent: Wednesday, December 20, 2006 11:35 AM Subject: RV10-List: Carpet Install Does anyone have any good ideas on how to fasten the carpet and still kee p it removable? I planned to use Velcro but it doesn't seem to stick to t he carpet backing well enough. Tom Deutsch, #40545 ________________________________________________________________________________
Date: Dec 20, 2006
Subject: Re: door latched security system - Door Closer
From: wvu(at)ameritel.net
There are two pins per door, one fwd and one aft which engage the holes in the bulkheads to hold the doors shut. The closure problem is related to the rear pins because the door handles are positioned near the fwd edge of the doors, thus not enough pull power on the aft edge. Van's idiot lights are sufficient to ensure proper closure before engine start. However, IMHO the door latch mechanism needs to be redesign. I feel that sooner or later the holes in the bulkheads are going to be enlarged from normal usage and eventually lose their pressure on the door seals. Those white blocks are offering zero support IMHO being held on my two screws. One other similar design issue. I feel that the front seat adjustment handles can use some more thoughts. They are too close to the side panels to operate with one hand, especially if you're going to have covers on the side panels. I had to use my two index fingers to pull the handle up to slide the seat when flying with Alex last week. Also, it would be nice if you can slide the seats off without having to losen the bolts holding the handles on first. Anh > > > I don't know if I have enough knowledge to comment here, so I'll ask a > few questions? > > Why not add switches (sub-micro or reed) to the door to detect proper > closure and wire them to disable the starter relay if the door isn't > closed properly? > > Is the closure problem related all the door pins or just one or two per > door? (how many pins are there???) > > As for the 'dings' when the door is closed with the latch pins out ..... > would a piece of stainless embedded in the frame minimize the damage?? > Linn ...... getting closer to my own kit! > > ________________________________________________________________________________
From: "Eric Parlow" <ericparlow(at)hotmail.com>
Subject: Re: door latched security system - Inflatable Seals?
Date: Dec 20, 2006
Has anyone used an inflatable seal around the doors? Shut the door, engage the pins, inflate the seal...... ________________________________________________________________________________
From: "Steven DiNieri" <capsteve(at)adelphia.net>
Subject: Carpet Install
Date: Dec 21, 2006
No worries les, The most dangerous time for contact cement is when it is still wet. As it dries and the volatiles outgas the glue becomes mostly inert. I=92ve compared the contact cement supplied from airtex (which is used in certified installs) to commercially available =93dap=94 type glue and upholstery cement we use for auto tops, and found they are almost identical. The dried cement =93boogers =93we burn tested did burn a bit under direct flame, but did not support combustion. In a comparison test all types performed the same. In certified aircraft its common to use cardboard type upholstered panels with foam and a fabric or leather finish. I can tell you with some certainty that the board and foams burn vigorously and DO support a flame. But as long as the exposed surface has an approved burn spec it gets faa blessing or so it seems. I=92d not worry about the adhesive as much as wisely choose the materials used in the install. .02 Steve 40205 Hmmm Is there a fire issue here? Contact cement, IIRC is quite flammable. Is there a better way? Cheers Les Kearney RV10 #40643 ' Lost in the empennage 12/19/2006 -- 12/19/2006 ________________________________________________________________________________
From: "Russell Daves" <dav1111(at)cox.net>
Subject: Re: door latched security system - Door Closerdoor latched
security system - Door Closer
Date: Dec 21, 2006
Now now John, people who have: 1. As much RV-10 time as you, without flying up to Van's to get transition training, and 2. Who fly their RV-8 around the country on a regular basis; and 3. Who get to fly F-16's; and 4. Who get to fly predators; shouldn't have fragile egos. For the rest of you, John demonstrated really great flying skills his first flight in an RV-10. I already had over 60 hours in my RV-10 when he flew it and if I had a fragile ego I would have walked around mopping the rest of the day because John made all those landings like so easy. Russ Daves N710RV first flight 7/29/06 76+ hours ________________________________________________________________________________
Date: Dec 21, 2006
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Burn test on Plenum rated conduit
A couple weeks ago someone asked if someone would go and burn test that orange interduct plenum rated conduit that I used, to see what it did. It's commonly used as fiberoptic conduit in the networking and telcom world, so most of you probably have a friend who has some they could cut off for you. I took a piece and stuck it in front of my glowing red hot kerosene torpedo heater, holding it with a needle nose pliers. Those things get darn hot. It softened and sagged, and started to melt and flow, and I held it right next to the glowing dome. In a short time it started to blacken, but not charcoal, but it never did actually support a flame, even though it looked burned. It was very interesting, as I expected to at least get it burning kind of like a milk jug. (yeah, I've been known to throw things in the fire while camping to see what they do. ) So I came away impressed, and am now even more happy with the stuff than in the past. I also did not detect any fumes that smelled like the normal toxic plastic smell. So this stuff may be perfect for what we're doing. -- Tim Olson - RV-10 N104CD - Flying ________________________________________________________________________________
From: "ddddsp1(at)juno.com" <ddddsp1(at)juno.com>
Date: Dec 21, 2006
Subject: FS RV rear foam seats
Changed design on the seats and do not need the rear foam seats ordered from Vans. If your ordering the foam anyway here is a chance to save a few $$$. $275 Dean 402-560-9755 ________________________________________________________________________ FREE for 30 Days! - Holiday eCards from AmericanGreetings.com http://track.juno.com/s/lc?s=197335&u=http://www.americangreetings.c om/index.pd?c=uol5637

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From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: FS RV rear foam seats
Date: Dec 21, 2006
A little more info would be helpful JOhn G. >From: "ddddsp1(at)juno.com" <ddddsp1(at)juno.com> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: RV10-List: FS RV rear foam seats >Date: Thu, 21 Dec 2006 16:15:22 GMT > >Changed design on the seats and do not need the rear foam seats ordered >from Vans. If your ordering the foam anyway here is a chance to save a few >$$$. $275 >Dean >402-560-9755 > > >________________________________________________________________________ >FREE for 30 Days! - Holiday eCards from AmericanGreetings.com >http://track.juno.com/s/lc?s=197335&u=http://www.americangreetings.com/index.pd?c=uol5637 ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Baggage door
Date: Dec 21, 2006
Chris, I have worked on the door all the way up to riviting it. I have crimped the inner flanges of the door frame in several areas because the upper and lower skin edge was slightly bowed out in the middle. Now I believe I have crimped the flanges about as much as I would want to and the only thing still out of alignment is the middle of the top frame, which leaves the skin of the door in that area about 1/8" proud. The corners are all in alignment with the fuselage, everything looks good except this one bowed out spot. I certainly can build up the fuselage at the intersection of the cabin top and the metal fuse skin, but this will not be the true shape that the fuselage should ideally have. Any more suggestions would be welcomed, before I get the rivets out. Not that this will help my situation, but I have also thought about placing a fiberglass/kevlar super thin sheet which could laminate over the entire door to seal off the gap on the top/bottom and back. The hinge area will not allow coverage in that area. My mod would give better aerodynamics than the 3/32 to 1/8 gap around the perimeter(That is provided I can sinch it down tight to the skin) JOhn G. ________________________________________________________________________________
Subject: RV-10 vs. Turkey Vulture (the RV won)
Date: Dec 21, 2006
From: "Doerr, Ray R [NTK]" <Ray.R.Doerr(at)sprint.com>
Check this out on Van's Airforce http://www.vansairforce.net/ Thank You Ray Doerr 40250 (192 hours) ________________________________________________________________________________
Date: Dec 21, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: Baggage door
John, I found that the hand seamer was a great tool to 'adjust' the baggage door to match the contour of the fuse. just small adjustments seemed to bring everything in line for me. Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ John Gonzalez wrote: > > Chris, > > I have worked on the door all the way up to riviting it. I have > crimped the inner flanges of the door frame in several areas because > the upper and lower skin edge was slightly bowed out in the middle. > Now I believe I have crimped the flanges about as much as I would want > to and the only thing still out of alignment is the middle of the top > frame, which leaves the skin of the door in that area about 1/8" > proud. The corners are all in alignment with the fuselage, everything > looks good except this one bowed out spot. I certainly can build up > the fuselage at the intersection of the cabin top and the metal fuse > skin, but this will not be the true shape that the fuselage should > ideally have. > > Any more suggestions would be welcomed, before I get the rivets out. > > Not that this will help my situation, but I have also thought about > placing a fiberglass/kevlar super thin sheet which could laminate over > the entire door to seal off the gap on the top/bottom and back. The > hinge area will not allow coverage in that area. My mod would give > better aerodynamics than the 3/32 to 1/8 gap around the perimeter(That > is provided I can sinch it down tight to the skin) > > JOhn G. > > ________________________________________________________________________________
Date: Dec 21, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: RV-10 vs. Turkey Vulture (the RV won)
Anybody know who's plane this is? Where it happened? Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ Doerr, Ray R [NTK] wrote: > > Check this out on Van's Airforce http://www.vansairforce.net/ > > >Thank You >Ray Doerr >40250 (192 hours) > > > > ________________________________________________________________________________
Subject: Baggage door
Date: Dec 21, 2006
From: "Chris Johnston" <CJohnston(at)popsound.com>
Smack it with a hammer! Just kidding. I haven't been back to that section yet, I just moved on for awhile while waiting for new door pieces, but it sounds like you've got it just about as good as you can get it. seriously, some have reported that a bit of "man-handling" can improve the fit, but I'd be leery of that, cause you might just put the corners out of alignment while trying to improve the bow in the middle, or you might put a crease somewhere where you wish you didn't. Just a thought in the vein of the pursuit of perfection... someone posted somewhere that you really don't notice the slight imperfections when you're blasting along at 170 kts, or when you don't have a particular section under a microscope (as you do when you're constructing that area). It's really easy for me to get wound up in utter perfection, but sometimes, it really is good enough. personally, I'm not building a show winner. I think a first-time builder like myself might not have the skills to do so. What I AM trying to do is build it better than whatever airplane I rent to go buzzing around, and I think I'm doing that, both from a safety, and from an aesthetic standpoint. When I'm bummed that something isn't exactly perfect, I just take extra time doing my preflight of a rental 172, and I start to feel REALLY good about my building practices, and about the standard I've set for myself. cj #40410 fuse www.perfectlygoodairplane.net -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Gonzalez Sent: Thursday, December 21, 2006 10:22 AM Subject: RV10-List: Baggage door Chris, I have worked on the door all the way up to riviting it. I have crimped the inner flanges of the door frame in several areas because the upper and lower skin edge was slightly bowed out in the middle. Now I believe I have crimped the flanges about as much as I would want to and the only thing still out of alignment is the middle of the top frame, which leaves the skin of the door in that area about 1/8" proud. The corners are all in alignment with the fuselage, everything looks good except this one bowed out spot. I certainly can build up the fuselage at the intersection of the cabin top and the metal fuse skin, but this will not be the true shape that the fuselage should ideally have. Any more suggestions would be welcomed, before I get the rivets out. Not that this will help my situation, but I have also thought about placing a fiberglass/kevlar super thin sheet which could laminate over the entire door to seal off the gap on the top/bottom and back. The hinge area will not allow coverage in that area. My mod would give better aerodynamics than the 3/32 to 1/8 gap around the perimeter(That is provided I can sinch it down tight to the skin) JOhn G. ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Re: Baggage door
Date: Dec 21, 2006
Thanks Deems Sorry, but haven't used that tool for some time, it is the plyer like tool with the flat plate on each side. Seems like I could only change the angle of the frame flange with that tool and I think it is the entire piece that needs to be bent in slightly. Perhaps making some relief cuts in the frame (At the intersection of the flange and the aluminum which isn't joined to the skin or to the close out panel )with a dremel disk and then bending the material between the cuts would cause the flange to pull in. close out panel _Flange_____ _ _ cut here and crimp _ -----------> ___________ flange outside skin This should pull the outer fange in in the bulged out area. I only need a four inch area. JOhn >From: Deems Davis <deemsdavis(at)cox.net> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: Re: RV10-List: Baggage door >Date: Thu, 21 Dec 2006 11:51:51 -0700 > > >John, I found that the hand seamer was a great tool to 'adjust' the baggage >door to match the contour of the fuse. just small adjustments seemed to >bring everything in line for me. > >Deems Davis # 406 >Finishing - ( A Misnomer ! ) >http://deemsrv10.com/ > >John Gonzalez wrote: > >> >>Chris, >> >>I have worked on the door all the way up to riviting it. I have crimped >>the inner flanges of the door frame in several areas because the upper and >>lower skin edge was slightly bowed out in the middle. Now I believe I have >>crimped the flanges about as much as I would want to and the only thing >>still out of alignment is the middle of the top frame, which leaves the >>skin of the door in that area about 1/8" proud. The corners are all in >>alignment with the fuselage, everything looks good except this one bowed >>out spot. I certainly can build up the fuselage at the intersection of >>the cabin top and the metal fuse skin, but this will not be the true shape >>that the fuselage should ideally have. >> >>Any more suggestions would be welcomed, before I get the rivets out. >> >>Not that this will help my situation, but I have also thought about >>placing a fiberglass/kevlar super thin sheet which could laminate over the >>entire door to seal off the gap on the top/bottom and back. The hinge >>area will not allow coverage in that area. My mod would give better >>aerodynamics than the 3/32 to 1/8 gap around the perimeter(That is >>provided I can sinch it down tight to the skin) >> >>JOhn G. >> >> >> >> >> >> >> >> > > ________________________________________________________________________________
Date: Dec 21, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: RV-10 vs. Turkey Vulture (the RV won)
"In Florida, where I plan to retire, Turkey Buzzards are a constant hazard." hehe...so are the old buzzards... ;) Rick S. 40185 ________________________________________________________________________________
From: JSMcGrew(at)aol.com
Date: Dec 21, 2006
Subject: Re: RV-10 vs. Turkey Vulture (the RV won)
I thought that propeller comment might start something. I'm staying out of this one. In a message dated 12/21/2006 3:14:24 P.M. Eastern Standard Time, jjessen(at)rcn.com writes: --> RV10-List message posted by: "John Jessen" Ok, this must be one of those obvious things that I just cannot comprehend. What does going with a Hartzell prop have to do with Turkey Vultures hitting a wing? Aluminum can withstand this type of strike better than a composite? John Jessen $40328$ (Zen and the are of edge deburrrrrrrrring) -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Stovall Todd Lt Col AF/A4RX Sent: Thursday, December 21, 2006 11:38 AM Subject: RE: RV10-List: RV-10 vs. Turkey Vulture (the RV won) --> That's one of the reasons I'm going with a Hartzell prop. In Florida, where I plan to retire, Turkey Buzzards are a constant hazard. Do Not Archive Todd #40631 Still riveting the HS -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jesse Saint Sent: Thursday, December 21, 2006 2:03 PM Subject: RE: RV10-List: RV-10 vs. Turkey Vulture (the RV won) WOW! Looks like it's time for a new wing. That must have been a BIG BIRD! Do not archive. Jesse Saint I-TEC, Inc. jesse(at)itecusa.org www.itecusa.org Cell: 352-427-0285 Fax: 815-377-3694 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Doerr, Ray R [NTK] Sent: Thursday, December 21, 2006 1:26 PM Subject: RV10-List: RV-10 vs. Turkey Vulture (the RV won) Check this out on Van's Airforce http://www.vansairforce.net/ Thank You Ray Doerr 40250 (192 hours) ________________________________________________________________________________
Subject: RV-10 vs. Turkey Vulture (the RV won)
Date: Dec 21, 2006
From: "Stovall Todd Lt Col AF/A4RX" <Todd.Stovall(at)pentagon.af.mil>
I aspire to join their ranks :-) -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rick Sent: Thursday, December 21, 2006 2:53 PM Subject: RE: RV10-List: RV-10 vs. Turkey Vulture (the RV won) "In Florida, where I plan to retire, Turkey Buzzards are a constant hazard." hehe...so are the old buzzards... ;) Rick S. 40185 ________________________________________________________________________________
From: Jeff Carpenter <jeff(at)westcottpress.com>
Subject: IFR
Date: Dec 21, 2006
I'd like to expand this thread a bit to get some feedback on what I'd call Modern IFR equipment and the resulting training that's appropriate for using it. I've got about 250 hours, but haven't flown in over seven years. In many ways, I'll be starting over as I prepare to fly my RV-10. Instrument navigation, for me, was never more than triangulating off of a couple of VORs and perhaps getting some useful information off of a DME if the plane I was renting was so equipped. I plan to get back up to speed by getting my instrument rating. Starting over, I imagine that there are entire IFR systems I can do without... and not further clutter my head with "old fashioned" information. To what extent can I equip my plane without those things, still have safe alternatives should the gps system fail and avoid spending time instrument training for systems I won't be using? Jeff Carpenter 40304 ________________________________________________________________________________
Date: Dec 21, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: Baggage door
I was able to physically apply some torque to my door, using just hands, it didn't take very much and it got pretty close. the remainder I was able to use the hand seamer, and make small adjustments, no need to cut anything. Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ John Gonzalez wrote: > > Thanks Deems > > Sorry, but haven't used that tool for some time, it is the plyer like > tool with the flat plate on each side. Seems like I could only change > the angle of the frame flange with that tool and I think it is the > entire piece that needs to be bent in slightly. Perhaps making some > relief cuts in the frame (At the intersection of the flange and the > aluminum which isn't joined to the skin or to the close out panel > )with a dremel disk and then bending the material between the cuts > would cause the flange to pull in. > > > close out panel > _Flange_____ > _ > _ > cut here and crimp _ > -----------> ___________ > flange > outside skin > > This should pull the outer fange in in the bulged out area. I only > need a four inch area. > > JOhn > >> From: Deems Davis <deemsdavis(at)cox.net> >> Reply-To: rv10-list(at)matronics.com >> To: rv10-list(at)matronics.com >> Subject: Re: RV10-List: Baggage door >> Date: Thu, 21 Dec 2006 11:51:51 -0700 >> >> >> John, I found that the hand seamer was a great tool to 'adjust' the >> baggage door to match the contour of the fuse. just small adjustments >> seemed to bring everything in line for me. >> >> Deems Davis # 406 >> Finishing - ( A Misnomer ! ) >> http://deemsrv10.com/ >> >> John Gonzalez wrote: >> >>> >>> >>> Chris, >>> >>> I have worked on the door all the way up to riviting it. I have >>> crimped the inner flanges of the door frame in several areas because >>> the upper and lower skin edge was slightly bowed out in the middle. >>> Now I believe I have crimped the flanges about as much as I would >>> want to and the only thing still out of alignment is the middle of >>> the top frame, which leaves the skin of the door in that area about >>> 1/8" proud. The corners are all in alignment with the fuselage, >>> everything looks good except this one bowed out spot. I certainly >>> can build up the fuselage at the intersection of the cabin top and >>> the metal fuse skin, but this will not be the true shape that the >>> fuselage should ideally have. >>> >>> Any more suggestions would be welcomed, before I get the rivets out. >>> >>> Not that this will help my situation, but I have also thought about >>> placing a fiberglass/kevlar super thin sheet which could laminate >>> over the entire door to seal off the gap on the top/bottom and >>> back. The hinge area will not allow coverage in that area. My mod >>> would give better aerodynamics than the 3/32 to 1/8 gap around the >>> perimeter(That is provided I can sinch it down tight to the skin) >>> >>> JOhn G. >>> >>> >>> >>> >>> >>> >>> >>> >> >> >> >> >> > > ________________________________________________________________________________
Date: Dec 21, 2006
From: Niko <owl40188(at)yahoo.com>
Subject: Re: Baggage door
John,=0A=0AYour door sounds similar to the way mine came out. I slowly wor ked it with my hands and the fit improved drastically. I haven't put the s eal on but without it the fit looks pretty good to me. I am going to wait until I have the canopy on to install the seal and work it a bit more.=0A =0AGood luck with it.=0A=0ANiko=0A40188=0A=0A=0A----- Original Message ---- =0AFrom: John Gonzalez <indigoonlatigo(at)msn.com>=0ATo: rv10-list(at)matronics.c om=0ASent: Thursday, December 21, 2006 1:22:02 PM=0ASubject: RV10-List: Bag nlatigo(at)msn.com>=0A=0AChris,=0A=0AI have worked on the door all the way up to riviting it. I have crimped the =0Ainner flanges of the door frame in s everal areas because the upper and lower =0Askin edge was slightly bowed ou t in the middle. Now I believe I have crimped =0Athe flanges about as much as I would want to and the only thing still out of =0Aalignment is the midd le of the top frame, which leaves the skin of the door =0Ain that area abou t 1/8" proud. The corners are all in alignment with the =0Afuselage, every thing looks good except this one bowed out spot. I certainly =0Acan build up the fuselage at the intersection of the cabin top and the metal =0Afuse skin, but this will not be the true shape that the fuselage should =0Aideal ly have.=0A=0AAny more suggestions would be welcomed, before I get the rive ts out.=0A=0ANot that this will help my situation, but I have also thought about placing =0Aa fiberglass/kevlar super thin sheet which could laminate over the entire =0Adoor to seal off the gap on the top/bottom and back. Th e hinge area will =0Anot allow coverage in that area. My mod would give bet ter aerodynamics than =0Athe 3/32 to 1/8 gap around the perimeter(That is p rovided I can sinch it =0Adown tight to the skin)=0A=0AJOhn G.=0A=0A=0A=0A_ -======================== ======================= ________________________________________________________________________________
Subject: IFR
Date: Dec 21, 2006
From: "Chris Johnston" <CJohnston(at)popsound.com>
Hey Jeff - I'm with you about not cluttering your head with "non-useful" or outdated instrument flight training, and to a certain extent trying to train for the IFR environment that you'll be flying in - ie: super modern GPS with LPV approaches and EFIS systems that talk to the NAV and provide ILS needles on the display etc. the reality is that you have to know ALL of the stuff. I'm talking ADF OBS CDI DME arcs - everything. First of all, it's all going to be on the knowledge test (written), and second of all, the aircraft you'll be training in (unless you finish your build and train in your own aircraft) will most likely have a couple nav/coms, CDI/OBS, maybe even an ADF, and a slightly older IFR GPS like a KLN94 if it has one at all. and if the aircraft has it, you'll be expected to know how to navigate with it. The rule as it was explained to me is that for your checkride, you have to show proficiency with all the installed equipment. A friend of mine just got his IFR ticket, and he didn't have to do any GPS approaches. Why? No IFR GPS in the plane. Also, to a certain extent, it helps to understand the evolution of some of the equipment and know how to use it. not sure why. My approach to the whole IFR thing was basically that I will have to re-learn IFR operations in my aircraft, because it will be so different from how I trained. I'll have to get used to the EFIS, and cockpit resource management in general, then wrangle an instructor to do an IPC with me, and see what areas I need help in. cj #40410 fuse www.perfectlygoodairplane.net -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jeff Carpenter Sent: Thursday, December 21, 2006 12:56 PM Subject: RV10-List: IFR I'd like to expand this thread a bit to get some feedback on what I'd call Modern IFR equipment and the resulting training that's appropriate for using it. I've got about 250 hours, but haven't flown in over seven years. In many ways, I'll be starting over as I prepare to fly my RV-10. Instrument navigation, for me, was never more than triangulating off of a couple of VORs and perhaps getting some useful information off of a DME if the plane I was renting was so equipped. I plan to get back up to speed by getting my instrument rating. Starting over, I imagine that there are entire IFR systems I can do without... and not further clutter my head with "old fashioned" information. To what extent can I equip my plane without those things, still have safe alternatives should the gps system fail and avoid spending time instrument training for systems I won't be using? Jeff Carpenter 40304 ________________________________________________________________________________
Date: Dec 21, 2006
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: IFR
The only thing you will have to learn in your own aircraft is any new equipment beyond what you used for the checkride, and to determine what speeds and power settings work for the different phases of descent, climb, holding, approach, which you have to determine in any airplane. All planes made since about 1975 have a standard T instrument layout of steam gauges. If you choose to go to EFIS, that will just be learning a different presentation, but you need to know the standard steam gauges for your backup. You need to be proficient at flying the plane with a single gyro, compass, airspeed and altimeter, without all the glass panel gizmos. If you can't do that, how are you going to survive when you have one of those gizmos release the smoke they contain and you have to shutdown your full electrical system because you don't have the ability to crawl beneath the panel and fly the airplane too and you only know that fire follows smoke?? E bus means nothing if you have an electrically generated puff of smoke in the cockpit and are in the soup. Just keep that in mind when designing redunancy if you plan on flying IFR. Do you really want to be testing electrical circuits to see which one generated the smoke while trying to fly partial panel, solo? On 12/21/06, Chris Johnston wrote: > My approach to the whole IFR thing was basically that I will have to > re-learn IFR operations in my aircraft, because it will be so different > from how I trained. I'll have to get used to the EFIS, and cockpit > resource management in general, then wrangle an instructor to do an IPC > with me, and see what areas I need help in. > > cj > #40410 > fuse > www.perfectlygoodairplane.net > ________________________________________________________________________________
From: "ddddsp1(at)juno.com" <ddddsp1(at)juno.com>
Date: Dec 21, 2006
Subject: Re: FS RV rear foam seats
John, This is the foam Vans sells to put in the rear seats of an RV10. If yo u go to their website it is listed there. I can send pics if needed.... .....just 2 rear seat cushion foams and 2 backrest seat foams. Dean 40449 ________________________________________________________________________ FREE for 30 Days! - Holiday eCards from AmericanGreetings.com http://track.juno.com/s/lc?s=197335&u=http://www.americangreetings.c om/index.pd?c=uol5637

John,

 This is the foam Vans sells to put in the rear seats of an RV10 .  If you go to their website it is listed there.  I can send pics if needed.........just 2 rear seat cushion foams and 2 backrest sea t foams.

Dean

40449



______________________ __________________________________________________
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________________________________________________________________________________
Date: Dec 21, 2006
From: Niko <owl40188(at)yahoo.com>
Subject: Re: IFR
In light of this discussion I am attaching my current panel configuration f or informational purposes. Its probably going to still change quiet a bit but the layout is probably close. I think the location of the instuments a llows the pilot to use either a standard 6 pack or the EFIS tubes. I actua lly prefer a standard 6 pack in a lot of situations but want the HITS capab ility of the EFIS. The airplane will have a vacuum system and an EFIS.=0A =0ANiko=0A40188=0A=0A=0A----- Original Message ----=0AFrom: Kelly McMullen =0ATo: rv10-list(at)matronics.com=0ASent: Thursday, Decembe r 21, 2006 5:37:14 PM=0ASubject: Re: RV10-List: IFR=0A=0A=0A--> RV10-List m essage posted by: "Kelly McMullen" =0A=0AThe only thing you will have to learn in your own aircraft is any new=0Aequipment beyond w hat you used for the checkride, and to determine=0Awhat speeds and power se ttings work for the different phases of=0Adescent, climb, holding, approach , which you have to determine in any=0Aairplane. All planes made since abou t 1975 have a standard T=0Ainstrument layout of steam gauges. If you choose to go to EFIS, that=0Awill just be learning a different presentation, but you need to know=0Athe standard steam gauges for your backup. You need to b e proficient=0Aat flying the plane with a single gyro, compass, airspeed an d=0Aaltimeter, without all the glass panel gizmos. If you can't do that,=0A how are you going to survive when you have one of those gizmos release=0Ath e smoke they contain and you have to shutdown your full electrical=0Asystem because you don't have the ability to crawl beneath the panel=0Aand fly th e airplane too and you only know that fire follows smoke?? E=0Abus means no thing if you have an electrically generated puff of smoke=0Ain the cockpit and are in the soup. Just keep that in mind when=0Adesigning redunancy if y ou plan on flying IFR. Do you really want to=0Abe testing electrical circui ts to see which one generated the smoke=0Awhile trying to fly partial panel , solo?=0A=0A=0AOn 12/21/06, Chris Johnston wrote: o the whole IFR thing was basically that I will have to=0A> re-learn IFR op erations in my aircraft, because it will be so different=0A> from how I tra ined. I'll have to get used to the EFIS, and cockpit=0A> resource manageme nt in general, then wrangle an instructor to do an IPC=0A> with me, and see what areas I need help in.=0A>=0A> cj=0A> #40410=0A> fuse=0A> www.perfectl ========= ________________________________________________________________________________
Subject: IFR
Date: Dec 21, 2006
From: "Chris Johnston" <CJohnston(at)popsound.com>
Aaah... I sense an upcoming heated discussion about what constitutes acceptable backup systems for IFR. I definitely appreciate the gravity (pun intended) of the situation, and what's at stake, but I'll stay out of it. I think I can have enough fun perusing the archives on the subject! :) I guess the original question was is there a bunch of old IFR junk that you can skip over if you are flying a technically advanced aircraft? My admittedly limited experience sez nope. With the possible exception of the ADF. Unless you want to listen to an AM radio station! (but you still have to get those questions right on the written) Remember, I'm a low time pilot, and the ink is still drying on my IFR ticket. I don't really know anything. These are just things I think. cj #40410 fuse www.perfectlygoodairplane.net -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Thursday, December 21, 2006 2:37 PM Subject: Re: RV10-List: IFR The only thing you will have to learn in your own aircraft is any new equipment beyond what you used for the checkride, and to determine what speeds and power settings work for the different phases of descent, climb, holding, approach, which you have to determine in any airplane. All planes made since about 1975 have a standard T instrument layout of steam gauges. If you choose to go to EFIS, that will just be learning a different presentation, but you need to know the standard steam gauges for your backup. You need to be proficient at flying the plane with a single gyro, compass, airspeed and altimeter, without all the glass panel gizmos. If you can't do that, how are you going to survive when you have one of those gizmos release the smoke they contain and you have to shutdown your full electrical system because you don't have the ability to crawl beneath the panel and fly the airplane too and you only know that fire follows smoke?? E bus means nothing if you have an electrically generated puff of smoke in the cockpit and are in the soup. Just keep that in mind when designing redunancy if you plan on flying IFR. Do you really want to be testing electrical circuits to see which one generated the smoke while trying to fly partial panel, solo? On 12/21/06, Chris Johnston wrote: > My approach to the whole IFR thing was basically that I will have to > re-learn IFR operations in my aircraft, because it will be so different > from how I trained. I'll have to get used to the EFIS, and cockpit > resource management in general, then wrangle an instructor to do an IPC > with me, and see what areas I need help in. > > cj > #40410 > fuse > www.perfectlygoodairplane.net > ________________________________________________________________________________
Date: Dec 21, 2006
From: Bill DeRouchey <billderou(at)yahoo.com>
Subject: Muffler nit
Just finished the first oil change of our RV-10 and during inspection found that the muffler shroud or underlying muffler structure had shifted positions slightly and the row of stainless steel screws that are anchored by tinnermans needed to be tightened. This was quite easy to adjust on the port muffler but the starboard muffler screw heads are blocked by the engine mount and other stuff. Suggest to those that are still working on the muffler installation that you flip the row of screws over on the starboard muffler to permit easy access from the bottom. Bill DeRouchey billderou(at)yahoo.com N939SB, Flying ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Van's shipping department, where did everyone go??
Date: Dec 21, 2006
The last couple of times I have orderred parts through Van's I have been dissappointed in how long it took to get my stuff. Last Friday I orderred some accessories over the phone, just three or four and asked for standard UPS ground delivery. The following Monday morning, two and a half days later, I called to add a few small items, rivets and nuts. I was told that there was no way to include these items in my previous order so that shipping could be all together, no interest what so ever in even checking the status of my Friday order. Today I got a UPS confirmation that UPS received a package for shipment to me from Van's. For one week the order is sitting in Van's being filled before it even gets in the mail. So much for getting anything done on what I need to get done during this holiday weekend. Very frustrating and not the first time. I know that Aircraft, Spruce and Specialty has a west coast location, but i order through them anytime before 3pm and the next day it is sitting in my office. EVERYTIME! Just venting!!!!!!!!!!!!!!!!! I always try to not order the small stuff through Van's for this very reason. EEEEEEEEEEEEEEEEEE!!! John G. ________________________________________________________________________________
Date: Dec 21, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Re: IFR
Steve, I can see VOR and DME...not ILS. just a pennys worth... Rick S. 40185 ________________________________________________________________________________
Date: Dec 21, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: IFR
And you don't know nothing CJ?? Your well on your way young man. CJ wrote: "Hey Jeff - I'm with you about not cluttering your head with "non-useful" or outdated instrument flight training, and to a certain extent trying to train for the IFR environment that you'll be flying in - ie: super modern GPS with LPV approaches and EFIS systems that talk to the NAV and provide ILS needles on the display etc. the reality is that you have to know ALL of the stuff. I'm talking ADF OBS CDI DME arcs - everything. First of all, it's all going to be on the knowledge test (written), and second of all, the aircraft you'll be training in (unless you finish your build and train in your own aircraft) will most likely have a couple nav/coms, CDI/OBS, maybe even an ADF, and a slightly older IFR GPS like a KLN94 if it has one at all. and if the aircraft has it, you'll be expected to know how to navigate with it. The rule as it was explained to me is that for your checkride, you have to show proficiency with all the installed equipment. A friend of mine just got his IFR ticket, and he didn't have to do any GPS approaches. Why? No IFR GPS in the plane. Also, to a certain extent, it helps to understand the evolution of some of the equipment and know how to use it. not sure why. ________________________________________________________________________________
From: Richard Reynolds <rvreynolds(at)macs.net>
Subject: Re: tailcone rivets - Riveting Fuse Side Skins
Date: Dec 22, 2006
Dave, See attached pictures. For the floor (RV-9A), I erected two vertical posts and clamped two athwartship braces under the forward and aft spars. The floor is clamped to the braces. For the tailcone (RV-10), it was quicker to just set up a ladder and use the tail hook to secure it, Put some padding on the ladder. The bottom skin (J bars) had been completely back riveted before it was assembled into the sides and tops. Leave room at the floor to get inside. See the feet of person inside! The very aft end was finished by putting the tailcone on some low saw horses. In the pictures, the skins aft of F109? are still clecoed. If you do not have room in the workshop, move outside for the hour or so it takes to rivet the structure together, Make your supports secure. Do not drop the assembly on the floor. Richard Reynolds Norfolk, VA =EF=BC=EF=BC=EF=BC On Feb 23, 2006, at 6:02 PM, McGANN, Ron wrote: > Hi Richard, > > I'm intrigued. Can you shed some more light (a picture would be > awesome)? Did you suspend the fuse from the ceiling/rafter? If > so, did you suspend from the centre section spars? > > thanks > Ron > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list- > server(at)matronics.com]On Behalf Of Richard Reynolds > Sent: Friday, 24 February 2006 9:12 AM > To: rv10-list(at)matronics.com > Subject: Re: RV10-List: Riveting Fuse Side Skins > > We hung ours vertical resting against 2 2X4 at a height that > allowed easy access. Did the same for the tail cone. > > Richard Reynolds > Norfolk, VA > > > On Feb 22, 2006, at 5:58 PM, McGANN, Ron wrote: > >> G'day all, >> >> I'm about to start riveting the fuse side skins. Has anyone had >> any success backriveting these skins? If so, what is the trick >> for preventing damage to the ribs/floor panels while climbing >> around inside? >> >> If your are near this point, have a look at Rick Sked's fuse stand >> in Tim Olsons page under fuselage tips. Looks neat, easy to build >> and versatile. I had not noticed it before. I guess the only >> down side is the height is fixed. >> >> thanks in advance, >> Ron >> #187 fuse > ________________________________________________________________________________
From: neal.george(at)mchsi.com
Subject: Re: Trutrak Flatpack dimensions?
Date: Dec 22, 2006
Here you go, CJ... Neal > > Hey all - > > Looked all over and can't seem to find what I'm lookin fer... anyone > have dimensions on the "flat pack" controller for a Trutrak Digiflight > IIVSGV? > > Thanks! > cj > #40410 > fuse > www.perfectlygoodairplane.net ________________________________________________________________________________
Date: Dec 22, 2006
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: IFR
What I disagree with is the concept that there will be thousands of LPV approaches where there is no ILS today. Sure, the minimums are approved, but have you looked at what is required for a precision approach, regardless of the guidance? It isn't just designing an approach. You have to spend the money to ensure an obstacle free approach path, install approach lighting and runway lighting that doesn't exist today, to CAT 1 ILS standards. Without that, you will be limited to non-precision minimums. That is a fact. There is no big budget to pay for all that runway and approach lighting improvement. Unless the individual airports find a way to pay for it, it simply is not going to happen in less than a decade. On 12/22/06, Eric Ekberg wrote: > What exactly do you disagree with? > > As I stated, CAT 1 like minimums are available with LPV when the runway > supports it (that means appropriate lighting, obstruction clearance, etc. - > no ILS is required). The FAA is ramping LPV approach creation; they are > working their way to thousands of LPV approaches (remember LPV is not your > typical GPS approach at this point in time). Saying the typical GPS > approach is going to remain crappy for a LONG time depends upon your > definition of LONG. If long means anything more than a few years - you are > dead wrong. > ________________________________________________________________________________
Date: Dec 22, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: Rolling the leading edges of the elevator & rudder
Hi Yesterday, with the help of friend I rolled the leading edge of one of my elevators using the technique in the Van=92s docs. I used a 1 =BC=94 OD pipe to do the rolling. I found that using an edge seamer / hand seamer I was able to eliminate most of the gap between the skins along the rivet line (but not all). I also noted that there is a slight but noticeable high point along the rivet line were the seamers did their thing. This means the pop rivet head is not perfectly flush to the skin on all sides due to the high point. I suspect there is a better way to eliminate the puckers along the rivet line without causing a high spot. Any suggestions? I would like to do a better job on the rudder and remaining elevator. Inquiring minds need to know Les Kearney RV10 #40643 ' Lost in the empennage ________________________________________________________________________________
Date: Dec 22, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Ceramic exhaust coating
Anybody want to chime in on the plus and minus of having the exhaust coated? Rick S. 40185 ________________________________________________________________________________
From: "Brian Douglas" <bsponcil(at)belinblank.org>
Subject: Re: Van's shipping department, where did everyone go??
Date: Dec 22, 2006
Yeah, I've had similar experiences. One time after I got the "your order has already shipped so we can't add to it" answer, my wife called FedEx to confirm that (if you knew her this would make sense). Turns out FedEx hadn't shown up at Vans yet so she called them on it and insisted they add to my existing order. Most recently I ordered a replacement F-1010 bulkhead 1st thing monday morning, only to have it shipped the following Friday. Vans makes a tremendous product but I'd say the Marketing and Customer Service deptments are somewhat subpar. Oh well. I think from now on, I'll just plan to pay extra for the 2 day shipping to avoid extended buildus interruptus. Just my $.02 -Brian Iowa City, IA #40497 Tailcone rivets this weekend! ----- Original Message ----- From: "John Gonzalez" <indigoonlatigo(at)msn.com> Sent: Thursday, December 21, 2006 7:59 PM Subject: RV10-List: Van's shipping department, where did everyone go?? > > The last couple of times I have orderred parts through Van's I have been > dissappointed in how long it took to get my stuff. > > Last Friday I orderred some accessories over the phone, just three or four > and asked for standard UPS ground delivery. > > The following Monday morning, two and a half days later, I called to add a > few small items, rivets and nuts. I was told that there was no way to > include these items in my previous order so that shipping could be all > together, no interest what so ever in even checking the status of my > Friday order. > > Today I got a UPS confirmation that UPS received a package for shipment to > me from Van's. For one week the order is sitting in Van's being filled > before it even gets in the mail. So much for getting anything done on > what I need to get done during this holiday weekend. > > Very frustrating and not the first time. > > I know that Aircraft, Spruce and Specialty has a west coast location, but > i order through them anytime before 3pm and the next day it is sitting in > my office. EVERYTIME! > > Just venting!!!!!!!!!!!!!!!!! > > I always try to not order the small stuff through Van's for this very > reason. EEEEEEEEEEEEEEEEEE!!! > > John G. > > > ________________________________________________________________________________
Date: Dec 22, 2006
From: Bill DeRouchey <billderou(at)yahoo.com>
Subject: Elevator trim setting
I went through this issue with Vans couple of months ago hoping for a plans revision or service bulletin but those folks seem to be busy in other areas - but I believe it to be important and want to share my findings. I setup my elevator tabs per the instructions with both left and right 35 degrees below trail position when the servo is at the full up position. It is possible to meet this spec by making adjustments at the servo end of the cable. During my first cross country I happened to look back at the tail and saw it was twisted. The elevator counter weight was above the horizontal stablizer on one side and below on the other. This bothered me more than a little as the forces would need to be high to cause this twist. I had not noticed this during my test flights because I now had luggage in the back and needed more down trim. After a lot of measurements I determined that the problem was I followed the instructions. If you begin with both elevator trim surfaces down at exactly 35 degrees the port side will never rise to trail position do to the cam action of the two actuators. Yet, the starboard will rise .75 inch above trail causing the twist. At a minimum effort, all flying RV-10s should check for this condition. The fix is easy. Highly recommend that you set the trim as follows: 1. Run the trim servo to full nose up. 2. Set the starboard trim tab trailing edge to 3 inches below elevator trailing edge. 3. Run the starboard trim tab to trail. 4. Set the port trim tab to trail. Using these settings you will be able to trim out all pitch forces during final with the CG forward. Bill DeRouchey billderou(at)yahoo.com N939SB, flying straight ________________________________________________________________________________
Date: Dec 22, 2006
From: MauleDriver <MauleDriver(at)nc.rr.com>
Subject: Re: Van's shipping department, where did everyone go??
I think I'm experiencing that now. I ordered some parts Monday, it showed up on the "ship list" on Tuesday (that's good). But it's not in UPS's tracking system yet (which happens within minutes of actual pickup). I'm concluding that "ship list" means, "ordered rec'd and sent for picking/packing". The aircraft are so good, the kits so well engineered, and the overall experience so wonderful that I'm fine with Van's core compentencies being over in the design and engineering area. Receiving, picking, packing and otherwise processing parts orders is important for Amazon. I sense that suppling parts and accessories is a merely a requirement for Vans being in this business. Remember when it took 'everyone' 3 days to process an order for anything? Ship overnight? forgetaboutit! Bill "deburr, dimple, deburr, dimple, deburr dimple the tailcone" Watson Brian Douglas wrote: > > > > Yeah, I've had similar experiences. One time after I got the "your > order has already shipped so we can't add to it" answer, my wife > called FedEx to confirm that (if you knew her this would make sense). > Turns out FedEx hadn't shown up at Vans yet so she called them on it > and insisted they add to my existing order. Most recently I ordered a > replacement F-1010 bulkhead 1st thing monday morning, only to have it > shipped the following Friday. > > Vans makes a tremendous product but I'd say the Marketing and Customer > Service deptments are somewhat subpar. Oh well. I think from now on, > I'll just plan to pay extra for the 2 day shipping to avoid extended > buildus interruptus. > > Just my $.02 > > -Brian > > Iowa City, IA > #40497 > Tailcone rivets this weekend! > > ----- Original Message ----- From: "John Gonzalez" > > To: > Sent: Thursday, December 21, 2006 7:59 PM > Subject: RV10-List: Van's shipping department, where did everyone go?? > > >> >> >> The last couple of times I have orderred parts through Van's I have >> been dissappointed in how long it took to get my stuff. >> >> Last Friday I orderred some accessories over the phone, just three or >> four and asked for standard UPS ground delivery. >> >> The following Monday morning, two and a half days later, I called to >> add a few small items, rivets and nuts. I was told that there was no >> way to include these items in my previous order so that shipping >> could be all together, no interest what so ever in even checking the >> status of my Friday order. >> >> Today I got a UPS confirmation that UPS received a package for >> shipment to me from Van's. For one week the order is sitting in Van's >> being filled before it even gets in the mail. So much for getting >> anything done on what I need to get done during this holiday weekend. >> >> Very frustrating and not the first time. >> >> I know that Aircraft, Spruce and Specialty has a west coast location, >> but i order through them anytime before 3pm and the next day it is >> sitting in my office. EVERYTIME! >> >> Just venting!!!!!!!!!!!!!!!!! >> >> I always try to not order the small stuff through Van's for this very >> reason. EEEEEEEEEEEEEEEEEE!!! >> >> John G. >> >> >> >> >> >> >> >> > > ________________________________________________________________________________
Date: Dec 22, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Re: Rolling the leading edges of the elevator & rudder
Les, I used a smaller pipe on the overlap skin. It allowed me to get a tighter radius and it overlayed the under skin much better. Try to keep the bend outside of the rivet line, towards the edge, and don't make it to pronounced. It should cleco together and look just as good as if you had rivets holding it together. The less stress to get it together the better. Rick S. 40185 ________________________________________________________________________________
Date: Dec 22, 2006
From: "ivo welch" <ivowel(at)gmail.com>
Subject: RV-10 For Sale
Dear RV-10 group. I have reduced my asking price for N325HP (http://welch.econ.brown.edu/n325hp) to $209,000 . With any reasonable labor cost and capital cost, this RV-10 with this engine, avionics, interior, quality, etc. cannot be duplicated at this price. (It has about 160 hours, a lot of it being "flight-testing" for those people who do not want to be test pilots themselves.) If you know of someone interested in buying one, please let them know. The airplane is in Rhode Island. regards, /ivo ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Re: Van's shipping department, where did everyone go??
Date: Dec 22, 2006
Just because you guys request overnight or two day shipping does not bump it up in the order department at Van's As Tim Olson and several others can attest too, including me, be very reluctant to ship anything overnight or even two day. You will be blown away by how much it costs. And absolutely, never get anything for Saturday delivery. $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! Try it out or take my word for it...don't do it. John G >From: MauleDriver <MauleDriver(at)nc.rr.com> >Reply-To: rv10-list(at)matronics.com >To: rv10-list(at)matronics.com >Subject: Re: RV10-List: Van's shipping department, where did everyone go?? >Date: Fri, 22 Dec 2006 14:36:26 -0500 > > >I think I'm experiencing that now. I ordered some parts Monday, it showed >up on the "ship list" on Tuesday (that's good). But it's not in UPS's >tracking system yet (which happens within minutes of actual pickup). I'm >concluding that "ship list" means, "ordered rec'd and sent for >picking/packing". > >The aircraft are so good, the kits so well engineered, and the overall >experience so wonderful that I'm fine with Van's core compentencies being >over in the design and engineering area. Receiving, picking, packing and >otherwise processing parts orders is important for Amazon. I sense that >suppling parts and accessories is a merely a requirement for Vans being in >this business. > >Remember when it took 'everyone' 3 days to process an order for anything? >Ship overnight? forgetaboutit! > >Bill "deburr, dimple, deburr, dimple, deburr dimple the tailcone" Watson > >Brian Douglas wrote: >> >> >>Yeah, I've had similar experiences. One time after I got the "your order >>has already shipped so we can't add to it" answer, my wife called FedEx to >>confirm that (if you knew her this would make sense). Turns out FedEx >>hadn't shown up at Vans yet so she called them on it and insisted they add >>to my existing order. Most recently I ordered a replacement F-1010 >>bulkhead 1st thing monday morning, only to have it shipped the following >>Friday. >> >>Vans makes a tremendous product but I'd say the Marketing and Customer >>Service deptments are somewhat subpar. Oh well. I think from now on, >>I'll just plan to pay extra for the 2 day shipping to avoid extended >>buildus interruptus. >> >>Just my $.02 >> >>-Brian >> >>Iowa City, IA >>#40497 >>Tailcone rivets this weekend! >> >>----- Original Message ----- From: "John Gonzalez" >> >>To: >>Sent: Thursday, December 21, 2006 7:59 PM >>Subject: RV10-List: Van's shipping department, where did everyone go?? >> >> >>> >>>The last couple of times I have orderred parts through Van's I have been >>>dissappointed in how long it took to get my stuff. >>> >>>Last Friday I orderred some accessories over the phone, just three or >>>four and asked for standard UPS ground delivery. >>> >>>The following Monday morning, two and a half days later, I called to add >>>a few small items, rivets and nuts. I was told that there was no way to >>>include these items in my previous order so that shipping could be all >>>together, no interest what so ever in even checking the status of my >>>Friday order. >>> >>>Today I got a UPS confirmation that UPS received a package for shipment >>>to me from Van's. For one week the order is sitting in Van's being filled >>>before it even gets in the mail. So much for getting anything done on >>>what I need to get done during this holiday weekend. >>> >>>Very frustrating and not the first time. >>> >>>I know that Aircraft, Spruce and Specialty has a west coast location, but >>>i order through them anytime before 3pm and the next day it is sitting in >>>my office. EVERYTIME! >>> >>>Just venting!!!!!!!!!!!!!!!!! >>> >>>I always try to not order the small stuff through Van's for this very >>>reason. EEEEEEEEEEEEEEEEEE!!! >>> >>>John G. >>> >>> >>> >>> >>> >>> >>> >>> >> >> >> >> >> >> >> > > ________________________________________________________________________________
From: LIKE2LOOP(at)aol.com
Date: Dec 22, 2006
Subject: Re: Rolling the leading edges of the elevator & rudder
IApJbiBhIG1lc3NhZ2UgZGF0ZWQgMTIvMjIvMjAwNiAxMTo0MzozMCBBTSBFYXN0ZXJuIFN0 YW5kYXJkIFRpbWUsICAKa2Vhcm5leUBzaGF3LmNhIHdyaXRlczoKCkkgdXNlZCBhICAxIMK8 4oCdIE9EIHBpcGUgdG8gZG8gdGhlIHJvbGxpbmcuIEkgZm91bmQgdGhhdCB1c2luZyBhbiBl ZGdlIHNlYW1lciAvIApoYW5kICBzZWFtZXIgSSB3YXMgYWJsZSB0byBlbGltaW5hdGUgbW9z dCBvZiB0aGUgZ2FwIGJldHdlZW4gdGhlIHNraW5zIGFsb25nIAp0aGUgIHJpdmV0IGxpbmUg KGJ1dCBub3QgYWxsKS4gCgoKICAgICBHb29kIHN0YXJ0Li4uIGtlZXAgdHJ5aW5nLiAgT3Zl ciByb2xsIGl0IGEgIGJpdCBhbmQgd29yayBpdCBieSBoYW5kIGFzIAp3ZWxsLiAgQW55IGFy ZWEgdGhhdCBpcyBidWxnaW5nIGlzIGFuIGFyZWEgdGhhdCAgd2FzIHVuZGVyIGN1cnZlZCAo bm90IHJvbGxlZCAKZW5vdWdoKS4gIFRoZSBoYW5kIHNlYW1lciBmaW5pc2hlcyBpdCBmb3Ig YSAgc251ZyBmaXQsIGJ1dCB3aWxsIE5PVCBtYWtlIHVwIGZvciAKdGhlIHVuZGVyIHJvbGxp bmcuIFRoZSBoYW5kIHNlYW0gc2hvdWxkIGJlICB0aGUgc2FtZSBhbW91bnQgdGhlIGVudGly ZSAKbGVuZ3RoLCBkb250IHRyeSB0byBvdmVyIGJlbmQgdGhlIGVkZ2UsIGp1c3QgZ28gYmFj ayAgYW5kIHJvbGwgbW9yZSwgaXQga2lsbGVkIG15IApoYW5kcyB3b3JraW5nIHRoZSBtZXRh bCwgYnV0IGlzIGRvIGFibGUuIEl0IHRha2VzICBlZmZvcnQgdG8gcm9sbCBhbmQgTk9UIGJl bmQgCmF0IHRoZSBlZGdlIG9mIHRoZSBzcGFyLi4uIGp1c3QgYmUgcGVyc2lzdGFudCBhbmQg IGF3YXJlIG9mIHRoZSBkaXJlY3Rpb24gb2YgCnlvdXIgZm9yY2VzLiAgTG9vayBmcm9tIHRo ZSBlbmQgYW5kIGV5ZSBiYWxsIHRoZSAgYXJlYXMgdGhhdCBzZWVtIGZsYXQuLi4uIGl0IGlz IAphbiBhcnQsIG5vdCBhIHNjaWVuY2UhISEKIApTdGV2ZQogCmRvIG5vdCBhcmNoaXZlICAK CgpTdGVwaGVuICBCbGFuayAgICAgICAgICAgICAgIzQwNDk5ICAgICAtIGZpbmlzaGluZyBl bGV2YXRvciB0cmltIHRhYnMuICAgKCBpICAKa25vdy4uLiBnb2luZyBzbG93Li4uLi4pCjc2 NiBTRSBSaXZlciBMYW5lClBvcnQgU3QuIEx1Y2llLCBGTCAgMzQ5ODMKCjc3Mi00NzUtNTU1 NiBjZWxsIC0gZXZlbmluZ3MgYW5kICB3ZWVrZW5kcwoK ________________________________________________________________________________
From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com>
Subject: Re: Van's shipping department, where did everyone go??
Date: Dec 22, 2006
I just confirmed my order for QB wings, fuse, and finishing kit today. Told the kits should be ready to ship late Feb. to mid March. I was told as of today there are 688 RV-10s being built. I ordered parts for a new right trim tab on 12/20. Parts came today Fed Ex. I was told they wouldn't arrive till after Xmas. Shipping is a bit high I guess, $24.83 to Milwaukee, WI (roughly). But I guess I can never complain about getting something delivered across the country in two days for $25.00. The game is to try not to have to many odds and ends shipped in between major orders. I am one who thinks the USPS should just raise their stamp rate to .50 and get it over with for a while. Never had a problem with anything from Van's yet. Still waiting on Creativeair lights since 12/12 though. Dave Leikam 40496 tail assembly ----- Original Message ----- From: "John Gonzalez" <indigoonlatigo(at)msn.com> Sent: Friday, December 22, 2006 2:08 PM Subject: Re: RV10-List: Van's shipping department, where did everyone go?? > > > Just because you guys request overnight or two day shipping does not bump > it up in the order department at Van's > > As Tim Olson and several others can attest too, including me, be very > reluctant to ship anything overnight or even two day. You will be blown > away by how much it costs. And absolutely, never get anything for Saturday > delivery. > > $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! > > Try it out or take my word for it...don't do it. > > John G > >>From: MauleDriver <MauleDriver(at)nc.rr.com> >>Reply-To: rv10-list(at)matronics.com >>To: rv10-list(at)matronics.com >>Subject: Re: RV10-List: Van's shipping department, where did everyone go?? >>Date: Fri, 22 Dec 2006 14:36:26 -0500 >> >> >>I think I'm experiencing that now. I ordered some parts Monday, it showed >>up on the "ship list" on Tuesday (that's good). But it's not in UPS's >>tracking system yet (which happens within minutes of actual pickup). I'm >>concluding that "ship list" means, "ordered rec'd and sent for >>picking/packing". >> >>The aircraft are so good, the kits so well engineered, and the overall >>experience so wonderful that I'm fine with Van's core compentencies being >>over in the design and engineering area. Receiving, picking, packing and >>otherwise processing parts orders is important for Amazon. I sense that >>suppling parts and accessories is a merely a requirement for Vans being >>in this business. >> >>Remember when it took 'everyone' 3 days to process an order for anything? >>Ship overnight? forgetaboutit! >> >>Bill "deburr, dimple, deburr, dimple, deburr dimple the tailcone" Watson >> >>Brian Douglas wrote: >>> >>> >>> >>>Yeah, I've had similar experiences. One time after I got the "your order >>>has already shipped so we can't add to it" answer, my wife called FedEx >>>to confirm that (if you knew her this would make sense). Turns out FedEx >>>hadn't shown up at Vans yet so she called them on it and insisted they >>>add to my existing order. Most recently I ordered a replacement F-1010 >>>bulkhead 1st thing monday morning, only to have it shipped the following >>>Friday. >>> >>>Vans makes a tremendous product but I'd say the Marketing and Customer >>>Service deptments are somewhat subpar. Oh well. I think from now on, >>>I'll just plan to pay extra for the 2 day shipping to avoid extended >>>buildus interruptus. >>> >>>Just my $.02 >>> >>>-Brian >>> >>>Iowa City, IA >>>#40497 >>>Tailcone rivets this weekend! >>> >>>----- Original Message ----- From: "John Gonzalez" >>> >>>To: >>>Sent: Thursday, December 21, 2006 7:59 PM >>>Subject: RV10-List: Van's shipping department, where did everyone go?? >>> >>> >>>> >>>> >>>>The last couple of times I have orderred parts through Van's I have been >>>>dissappointed in how long it took to get my stuff. >>>> >>>>Last Friday I orderred some accessories over the phone, just three or >>>>four and asked for standard UPS ground delivery. >>>> >>>>The following Monday morning, two and a half days later, I called to add >>>>a few small items, rivets and nuts. I was told that there was no way to >>>>include these items in my previous order so that shipping could be all >>>>together, no interest what so ever in even checking the status of my >>>>Friday order. >>>> >>>>Today I got a UPS confirmation that UPS received a package for shipment >>>>to me from Van's. For one week the order is sitting in Van's being >>>>filled before it even gets in the mail. So much for getting anything >>>>done on what I need to get done during this holiday weekend. >>>> >>>>Very frustrating and not the first time. >>>> >>>>I know that Aircraft, Spruce and Specialty has a west coast location, >>>>but i order through them anytime before 3pm and the next day it is >>>>sitting in my office. EVERYTIME! >>>> >>>>Just venting!!!!!!!!!!!!!!!!! >>>> >>>>I always try to not order the small stuff through Van's for this very >>>>reason. EEEEEEEEEEEEEEEEEE!!! >>>> >>>>John G. >>>> >>>> >>>> >>>> >>>> >>>> >>>> >>>> >>> >>> >>> >>> >>> >>> >>> >> >> >> >> >> >> > > > ________________________________________________________________________________
Subject: Playstation 3
Date: Dec 22, 2006
From: "Lloyd, Daniel R." <LloydDR(at)wernerco.com>
Guys, I don't typically do this but I know that many kids are wanting these Playstation 3's for Christmas, I found 3 at Walmart. Thought I would give you guys first crack at them before I put them on E-Bay, if interested call me on my cell 724-988-9230. Dan Lloyd N289DT RV-10 E ________________________________________________________________________________
Date: Dec 22, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: Ceramic exhaust coating
Plus: lower temperature inside of cowl from exhaust radiation. Better for fiberglass cowls. Minus: Harder to pull heat off for heat muff, Debatable: Life of the exhaust system, I've had reports of it both shortening and lengthening the life of the exhaust. If you coat the inside of the exhaust (as well as the outside), one member from my EAA chapter reported that his EGT temps rose aprox 100 Degrees. Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ Rick wrote: > >Anybody want to chime in on the plus and minus of having the exhaust coated? > > > > ________________________________________________________________________________
From: GenGrumpy(at)aol.com
Date: Dec 22, 2006
Subject: RV 10 sun visors
I searched the archives, but there wasn't anything there. Have any of the other fliers come up with a good sunvisor for the front seats? I love the visibility, but the sun is really a killer, and I haven't found anything out there that readily adapts to our bird, either fastening into the fibergalss shell or attaching to the center post. Anyone found a good solution yet? grumpy #40404, 42 hrs and going strong ________________________________________________________________________________
Subject: Ceramic exhaust coating
Date: Dec 22, 2006
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Check the archives, this has been discussed a couple times. Another advantage in keeping the heat in the exhaust is that it helps to keep the exhaust velocity up which aides in scavenging. I'm still planning on doing it. Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Deems Davis Sent: Friday, December 22, 2006 7:24 PM Subject: Re: RV10-List: Ceramic exhaust coating Plus: lower temperature inside of cowl from exhaust radiation. Better for fiberglass cowls. Minus: Harder to pull heat off for heat muff, Debatable: Life of the exhaust system, I've had reports of it both shortening and lengthening the life of the exhaust. If you coat the inside of the exhaust (as well as the outside), one member from my EAA chapter reported that his EGT temps rose aprox 100 Degrees. Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ Rick wrote: > >Anybody want to chime in on the plus and minus of having the exhaust coated? > > > > ________________________________________________________________________________
From: "Dave Leikam" <DAVELEIKAM(at)wi.rr.com>
Subject: trim tab problem.
Date: Dec 23, 2006
Yeah, I've noticed your number. You may pass me up at some point, I got my emp kit a year ago and just finished the tail cone. The problem I had with my trim tab is that I drilled the hinge holes wrong and caused a curve or hook in the hinge. This caused the hinge to bind and the tab to twist. The hinge is very flimsy before it is mounted and can flex easily. My left tab has the same problem but ever so slight I don't think I will rebuild it at this point. And if I do, I will only need to replace the hinge. At first I didn't realize the real problem. I drilled out the hinge rivets on the tab and thought I could just clamp the tab flat, re-align the hinge and re-rivet. While re-riveting, I bent the hinge slightly with the squeezer and then trying to remove the bend I put an ugly dent in the top of the tab skin. I then discovered the real problem of drilling the holes wrong on the elevator side, which transferred the curve to the tab side. I could have just replaced the hinge, but I could not accept that dent. So, after an hour of frustrated thought on how to save the part, I succumbed and ordered new parts to rebuild the whole tab. My son asked if he could have the the old tab and hung it in his room. He thinks it's cool. I guess that's the priceless stuff. The way to line up those hinges is to draw a rivet line on the hinge, then put that line in the center of the rivet holes and drill. Don't rely on the straightness of the hinge as I did, it flexes as you drill. Keep that rivet line centered in the holes and cleco as you go. The old learning curve again, seems so simple now! Dave Leikam 40496 emp assembly ----- Original Message ----- From: LIKE2LOOP(at)aol.com To: DAVELEIKAM(at)wi.rr.com Sent: Friday, December 22, 2006 4:53 PM Subject: Re: Van's shipping department, where did everyone go?? In a message dated 12/22/06 5:06:23 P.M. Eastern Standard Time, DAVELEIKAM(at)wi.rr.com writes: I ordered parts for a new right trim tab on 12/20. Tell me more... i am ready to bend the end tabs on both trim tabs tomorrow.... how did you loose the right one? Thanks for sharing... i sent this direct to you , off list. We are almost RV-10 brothers... my kit is #40499... you are a few kits ahead of me..... Stephen Blank RV-10 Builder #40499 / C-170B flyer 766 SE River Lane Port St. Lucie, FL 34983 772-475-5556 cell ________________________________________________________________________________
Date: Dec 23, 2006
From: CHRISTOPHER HARRIS <cbpip(at)verizon.net>
Subject: Re: Mechanicsville MD. builder
Hi, my name is Chris Harris. I'm an A&P, student pilot, and RV-10 wannabee freak. During one of RV-10 internet wanderings I found a possible builder in Mechanicsville, MD. I was interested in contacting them to volunteer help and to check out the project, as I live about 25 mins from Mechanicsville.. If anyone knows of a way to do this, info would be appreciated. Thanks, I can be reached at cbpip(at)verizon.net ________________________________________________________________________________
Date: Dec 23, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Firewall Penetrations - Additional?
Prior to hanging my engine I would like to ensure I've planned/accounted for all of the holes that need to be made/placed in the firewall. So for those of you who have already crossed this bridge...... 1. What ADDITIONAL holes did you provide beyond those already called out for in the plans? 2. What advice/suggestions do you have for the placement/location of those holes? 3. Did you fireprotect those additional holes? How? (I'm installing a full engine monitoring system and know I need to provide thru holes for CHT/EGT) THANKS for any help Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ ________________________________________________________________________________
From: GenGrumpy(at)aol.com
Date: Dec 23, 2006
Subject: Re: Firewall Penetrations - Additional?
Deems, Think you have to do this one yourself based on what you are putting in your bird. I'd sit down with a clean sheet of paper and start listing everything that will have to break the firewall. Some things you can run thru same hole (like the engine monitor wires, fuel flow, fuel pressure, oil pressure, etc). Then there are others like the battery cables, cables for throttle, etc. After all was said and done, I ended up having to drill yet another one for the cable I installed to fix the tunnel heat problem...... I'd start that list, then sit on it for a while while you think through all of your connections. grumpy 40404 DO NOT ATRCHIVE In a message dated 12/23/2006 8:48:09 AM Central Standard Time, deemsdavis(at)cox.net writes: Prior to hanging my engine I would like to ensure I've planned/accounted for all of the holes that need to be made/placed in the firewall. So for those of you who have already crossed this bridge...... 1. What ADDITIONAL holes did you provide beyond those already called out for in the plans? 2. What advice/suggestions do you have for the placement/location of those holes? 3. Did you fireprotect those additional holes? How? (I'm installing a full engine monitoring system and know I need to provide thru holes for CHT/EGT) THANKS for any help Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ ________________________________________________________________________________
From: "DejaVu" <wvu(at)ameritel.net>
Subject: Re: Firewall Penetrations - Additional?
Date: Dec 23, 2006
Deems, I have two extra holes for all wiring using fire-proof 36-pin (I think) plugs installed near the hole for the MAP hose. I can't recommend to buy the plugs where I bought mine with good conscience but I'm sure they are available elsewhere. Anh ----- Original Message ----- From: "Deems Davis" <deemsdavis(at)cox.net> Sent: Saturday, December 23, 2006 9:37 AM Subject: RV10-List: Firewall Penetrations - Additional? > > > Prior to hanging my engine I would like to ensure I've planned/accounted > for all of the holes that need to be made/placed in the firewall. So for > those of you who have already crossed this bridge...... > > 1. What ADDITIONAL holes did you provide beyond those already called out > for in the plans? > 2. What advice/suggestions do you have for the placement/location of those > holes? > 3. Did you fireprotect those additional holes? How? > > (I'm installing a full engine monitoring system and know I need to provide > thru holes for CHT/EGT) > > > THANKS for any help > > Deems Davis # 406 > Finishing - ( A Misnomer ! ) > http://deemsrv10.com/ > > > ________________________________________________________________________________
Date: Dec 23, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: Rudder wiring
Hi I have been wandering through the archives for info on rudder wiring. I believe that the preferred exit for trim servo wiring as well as other wiring is at the base of the rudder. For me wiring is a dark art at the moment and I am a bit concerned about building myself into a corner. In particular, my access to the rudder interior will be somewhat limited if I roll and rivet the rudder leading edges. My question is: how are wires secured in the interior of the rudder so that they do not chaff against the rudder stiffeners? Should I wait until wiring is done to complete the rudder? Inquiring minds need to know Les Kearney #40643 - Lost in the empennage ________________________________________________________________________________
From: "Rick Gray" <rickgray(at)roadrunner.com>
Subject: Re: Rudder wiring
Date: Dec 23, 2006
Hi Les, 1-The servo wiring will terminate at the servo in the forward section of the tailcone. 2-The trim motor wiring will terminate at the trim motor just below the forward emp fairing. 3-As for the rudder....depending on your lighting....you'll end up with wires for the strobe and nav light passing through the lower section of the vertical stab spar. Easiest way (imo) is to drill just below the bottom rudder hinge bracket. You may need to place a grommet in from each end of the spar for protection. Also, you may want to drill just off to the side as to not penetrate the tail tie down reinforcement. This will line your wires up just below the lower rod end bearing, allowing you to pass the wires through the lower fairing. For clarity....the wires will pass through the leading edge of the rudder in the opening just above the fiberglass fairing. I've done 5 or 6 these now and I always use a good connector in this area. Leave your harness long enough so that you can pull the tail light out and disconnect the wires for a) tail light replacement and b) rudder removal. The harness and connector will be stowed inside the lower fairing...savvy?? Also, the wire for the lights can terminate at the bolt (use a ring terminal) at the lower rod end bearing attach.....rudder side of the spar. Hope this helps....Good Luck Les, Rick in Ohio at the Buffalo Farm http://rv6rick.tripod.com/ohiovalleyrvators/ ----- Original Message ----- From: Les Kearney To: rv10-list(at)matronics.com Sent: Saturday, December 23, 2006 12:51 PM Subject: RV10-List: Rudder wiring Hi I have been wandering through the archives for info on rudder wiring. I believe that the preferred exit for trim servo wiring as well as other wiring is at the base of the rudder. For me wiring is a dark art at the moment and I am a bit concerned about building myself into a corner. In particular, my access to the rudder interior will be somewhat limited if I roll and rivet the rudder leading edges. My question is: how are wires secured in the interior of the rudder so that they do not chaff against the rudder stiffeners? Should I wait until wiring is done to complete the rudder? Inquiring minds need to know Les Kearney #40643 - Lost in the empennage ________________________________________________________________________________
From: "Rick Gray" <rickgray(at)roadrunner.com>
Subject: Re: Rudder wiring
Date: Dec 23, 2006
Hey Les....the bottom part of my post should read 'ground wire' can terminate at the bolt at the lower rod end bearing attach. Sorry for any confusion :^). Rick in Ohio at the Buffalo Farm http://rv6rick.tripod.com/ohiovalleyrvators/ ----- Original Message ----- From: Rick Gray To: rv10-list(at)matronics.com Sent: Saturday, December 23, 2006 2:47 PM Subject: Re: RV10-List: Rudder wiring Hi Les, 1-The servo wiring will terminate at the servo in the forward section of the tailcone. 2-The trim motor wiring will terminate at the trim motor just below the forward emp fairing. 3-As for the rudder....depending on your lighting....you'll end up with wires for the strobe and nav light passing through the lower section of the vertical stab spar. Easiest way (imo) is to drill just below the bottom rudder hinge bracket. You may need to place a grommet in from each end of the spar for protection. Also, you may want to drill just off to the side as to not penetrate the tail tie down reinforcement. This will line your wires up just below the lower rod end bearing, allowing you to pass the wires through the lower fairing. For clarity....the wires will pass through the leading edge of the rudder in the opening just above the fiberglass fairing. I've done 5 or 6 these now and I always use a good connector in this area. Leave your harness long enough so that you can pull the tail light out and disconnect the wires for a) tail light replacement and b) rudder removal. The harness and connector will be stowed inside the lower fairing...savvy?? Also, the wire for the lights can terminate at the bolt (use a ring terminal) at the lower rod end bearing attach.....rudder side of the spar. Hope this helps....Good Luck Les, Rick in Ohio at the Buffalo Farm http://rv6rick.tripod.com/ohiovalleyrvators/ ----- Original Message ----- From: Les Kearney To: rv10-list(at)matronics.com Sent: Saturday, December 23, 2006 12:51 PM Subject: RV10-List: Rudder wiring Hi I have been wandering through the archives for info on rudder wiring. I believe that the preferred exit for trim servo wiring as well as other wiring is at the base of the rudder. For me wiring is a dark art at the moment and I am a bit concerned about building myself into a corner. In particular, my access to the rudder interior will be somewhat limited if I roll and rivet the rudder leading edges. My question is: how are wires secured in the interior of the rudder so that they do not chaff against the rudder stiffeners? Should I wait until wiring is done to complete the rudder? Inquiring minds need to know Les Kearney #40643 - Lost in the empennage href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/c href="http://www.matronics.com/Navigator?RV10-List">http://www.matronic s.com/Navigator?RV10-List ________________________________________________________________________________
Date: Dec 23, 2006
From: LES KEARNEY <Kearney(at)shaw.ca>
Subject: Re: Rudder wiring
Hi Rick I understand what you have posted - many thanks. Is there a chaffing issue for the wires that run the length of the rudder interior? I would be concerned about chaffing against the rudder stringers or is this a misplaced concern? Inquiring minds need to know Les Kearney RV10 #40643 - Lost in the empennage ----- Original Message ----- From: Rick Gray <rickgray(at)roadrunner.com> Date: Saturday, December 23, 2006 12:47 pm Subject: Re: RV10-List: Rudder wiring > Hi Les, > 1-The servo wiring will terminate at the servo in the forward > section of the tailcone. > > 2-The trim motor wiring will terminate at the trim motor just > below the forward emp fairing. > > 3-As for the rudder....depending on your lighting....you'll end up > with wires for the strobe and nav light passing through the lower > section of the vertical stab spar. Easiest way (imo) is to drill > just below the bottom rudder hinge bracket. You may need to place > a grommet in from each end of the spar for protection. Also, you > may want to drill just off to the side as to not penetrate the > tail tie down reinforcement. This will line your wires up just > below the lower rod end bearing, allowing you to pass the wires > through the lower fairing. For clarity....the wires will pass > through the leading edge of the rudder in the opening just above > the fiberglass fairing. I've done 5 or 6 these now and I always > use a good connector in this area. Leave your harness long enough > so that you can pull the tail light out and disconnect the wires > for a) tail light replacement and b) rudder removal. The harness > and connector will be stowed inside the lower fairing...savvy?? > > Also, the wire for the lights can terminate at the bolt (use a > ring terminal) at the lower rod end bearing attach.....rudder side > of the spar. > > Hope this helps....Good Luck Les, > > Rick in Ohio at the Buffalo Farm > http://rv6rick.tripod.com/ohiovalleyrvators/ > > ----- Original Message ----- > From: Les Kearney > To: rv10-list(at)matronics.com > Sent: Saturday, December 23, 2006 12:51 PM > Subject: RV10-List: Rudder wiring > > > Hi > > > > I have been wandering through the archives for info on rudder > wiring. I believe that the preferred exit for trim servo wiring as > well as other wiring is at the base of the rudder. For me wiring > is a dark art at the moment and I am a bit concerned about > building myself into a corner. In particular, my access to the > rudder interior will be somewhat limited if I roll and rivet the > rudder leading edges. > > > > My question is: how are wires secured in the interior of the > rudder so that they do not chaff against the rudder stiffeners? > Should I wait until wiring is done to complete the rudder? > > > > Inquiring minds need to know > > > > Les Kearney > > #40643 - Lost in the empennage > > > > > > > ________________________________________________________________________________
From: Sean Stephens <sean(at)stephensville.com>
Subject: Happy Holidays To All
Date: Dec 23, 2006
Here's wishing all the current and future RV-10 builders a happy holiday. May each of you not have to spend the last six months with your kit in storage as I have. :) -Sean #40303 (Waiting for new house to be built) ________________________________________________________________________________
Date: Dec 23, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: Firewall Penetrations - Additional?
Below is a list of what I think is going to go through my firewall. The list is probably incomplete and with some questions so any guidance from the list would be helpful. Engine sensors will all go through a 1" stainless steel firewall penetration from EPM.AV corp <http://www.epm-avcorp.com/tubeseal.html>. Most seem to be putting this penetration in the upper right corner (like Tim). I would like to mount it just to the right of center. Any concerns with this location? The wires through this penetration would be EGT CHT oil pressure oil temp fuel pressure rpm manifiol pressure Electrical power Main power feed Super 2 CCA fatwire <http://www.periheliondesign.com/fatwires.htm> will go through the firewall per vans location mid left Starter contactor per vans location Current limiter and loadmeter shunt located on oil cooler housing electric to the main bus and e bus penetration near the starter contactor Magneto wires, not sure where they will penetrate. Not sure what can be combined with these wires. Any guidance? Cable penetrations through Stainless Steel eye balls. Prop Throttle mixture Fuel purge valve (airflow performance FM-200 fuel injection) Alternate air - How does the alternate air actuate? Is it included with the FWF kit? 4 penetrations can be arranged where vans has the bushings located in a diamond shaped arrangement. Scott has some photos on his site. Not sure where I would locate the 5th if there is even a 5th. Anything missing? Larry Rosen #356 Deems Davis wrote: > > Prior to hanging my engine I would like to ensure I've > planned/accounted for all of the holes that need to be made/placed in > the firewall. So for those of you who have already crossed this > bridge...... > > 1. What ADDITIONAL holes did you provide beyond those already called > out for in the plans? > 2. What advice/suggestions do you have for the placement/location of > those holes? > 3. Did you fireprotect those additional holes? How? > > (I'm installing a full engine monitoring system and know I need to > provide thru holes for CHT/EGT) > > > THANKS for any help > > Deems Davis # 406 > Finishing - ( A Misnomer ! ) > http://deemsrv10.com/ > > ________________________________________________________________________________
From: "John Hasbrouck" <jhasbrouck(at)woh.rr.com>
Subject: Elevator rigging
Date: Dec 23, 2006
I have a question re: rigging of the elevators. I've used the neutral position jigs for the elevator bellcrank and the control sticks to set the pushtube lengths and come up with a situation where the control stick interconnect ( F1065 ) contacts the underlying structure before the elevator is at its full up travel. So I've adjusted the pushtubes to give full up elevator before any contact of the stick interconect. This leaves the elevator bellcrank at a different neutral angle than the jig but I can't see why it would matter. Unless, that is, if it interferes with the pitch servo of the TruTrak AP. No interference in the system now with full up or down elevator deflection. What say you all? On another topic, seems that my baggage door came out the same as everyone else. Top edge of it stood proud a bit but some massaging with my fingers and seamers it looks pretty good now. Thanks to everyone who contributes their help to this list. You've made my build experience go very smoothly. Merry Christmas and Happy New Year to all. John Hasbrouck #40264 ________________________________________________________________________________
Date: Dec 23, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Re: Elevator rigging
John, I don't think you have an issue as long as you get full travel without interference while using the stick. Once you engage the aouto pilot the servo knows it's hold position is and will move the controls, a very minimal amount to maintain either altitude or if your lucky, a rate of climb or decent based on the input from the AP head. I doubt you will ever ask the AP servo to try and move the control surfaces from stop to stop...but as CJ says...I don't know nuthin!!! :) Rick S. 40185 ________________________________________________________________________________
Date: Dec 23, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Baggage door
Chrome valve covers and nice paint :) lol...82????? it's not even 82 in Vegas right now!!! Barrett's is my engine builder, and that means nothing against anyone else...they spent the time talking to me at OSH, explained everything, have a great reputation and Rhonda and the gang monitor the list. Monty Barrett's reputation and knowledge was enough for me along with all the good things all their customers had to say..and I did check.. Ric kS. 40185 ________________________________________________________________________________
From: "John Hasbrouck" <jhasbrouck(at)woh.rr.com>
Subject: Re: Elevator rigging
Date: Dec 23, 2006
Thanks Rick for the reply. I don't think there's an issue here either but thought I'd ask around. ________________________________________________________________________________
Subject: Baggage door
Date: Dec 24, 2006
From: "Lloyd, Daniel R." <LloydDR(at)wernerco.com>
I too agree that Barrett's is the way to go for a Lycoming. I spent allot of time with them on the phone trying to make the decision, and they were really good at helping me understand the different models and options. If I had gone with a Lycoming, I would have chosen them to build mine. Dan -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rick Sent: Saturday, December 23, 2006 10:38 PM Subject: RE: RV10-List: Baggage door Chrome valve covers and nice paint :) lol...82????? it's not even 82 in Vegas right now!!! Barrett's is my engine builder, and that means nothing against anyone else...they spent the time talking to me at OSH, explained everything, have a great reputation and Rhonda and the gang monitor the list. Monty Barrett's reputation and knowledge was enough for me along with all the good things all their customers had to say..and I did check.. Ric kS. 40185 ________________________________________________________________________________
From: "Robert Woods" <rwshooter(at)cox.net>
Subject: Re: Baggage door
Date: Dec 24, 2006
Hey Rick S., Last weekend Bob K. was kind enough to show me the ropes on building by helping me with my toolbox kit from Vans. Many thanks Bob. He mentioned you several times while we were bangin away. I would love to see your -10 and help the both of you with anything I can. Reach me at 429-7291 anytime. And there is no time like the present:) Robb N192RL.....reserved ________________________________________________________________________________
From: DOUGPFLYRV(at)aol.com
Date: Dec 24, 2006
Subject: Re: D2 Update
Stein, I appreciate your EMAIL and will wait til you have more information for us. Really screws up the holiday season for lots of folks. Regards, Doug ________________________________________________________________________________
From: "Kevin Belue" <kdbelue(at)charter.net>
Subject: Re: D2 Update
Date: Dec 24, 2006
Stein, It's good to read your email. I was nervous about handing over $26k to D2A without a product shipping - I certainly didn't want to. I studied all of the systems available at the time (1.5 years ago) and determined that Chelton was what I wanted. So I reluctantly paid and waited - I had no other choice if I as an individual wanted their product. If everyone, especially the dealers, say no to this "pay now and receive the product at some later date" scheme, it would provide much better protection to consumers as well as insuring that companies have the backing to be a successful company and not a business that is hanging on a thread, using customer's money to keep them in business day-to-day. I believe there are a lot of customers that have bought Chelton systems and are still waiting on components. I hope everyone will stick together when considering future products and only buy from companies that require money when the product ships. Good luck Stein, and all of us involved in this. Kevin Belue RV6A flying RV10 finish ----- Original Message ----- From: Stein Bruch To: rv10-list(at)matronics.com Sent: Sunday, December 24, 2006 10:44 AM Subject: RE: RV10-List: D2 Update Guys/Gals, Since I'm out of town for the holidays (like many of you) I can't take the time to call each one of you individually so I'm going to make a post here. MANY of you guys purchased your Chelton systems through my business and henceforth we'll all be in this together. I'm embarrassed, upset and scared as to what is ultimately going to happen with this whole debacle. I do know it's pretty crappy that this was dropped on all of us 24hrs before the holidays. I'm not in the office and most of you aren't at home so we can't even communicate about it. Right now we just don't know all of the facts and what is going to happen so it's far to early to speculate as to the outcome. What I do know is that all of the dealers aren't sitting on your money. Per D2A, we sent your payments to them for systems. Some of you have complete systems, some of you have partial systems and a few have nothing. All of you can be guaranteed that us dealers are in contact with each other already, and we're all doing as much as we can to figure out this mess and find some sort of solution. This can't happen until after the holidays so don't expect much of an update before the new year. As dealers we're in a really horrible position....and if we had your money the solutions would be easy...we'd just give your money back or buy something else. But, the huge problem is that we don't have your money - and frankly not a single one of us dealers could survive or financially afford to eat this. Remember, we're not talking about a couple people, we're talking about many dozens of you. So, the end result is that we all have to just wait a few days and see what gets sorted out. We're all devastated, sick, scared and stressed as to what the ultimate outcome is. We all had some sort of "gut feeling" that things at D2A were tough, but we had literally NO idea it was this bad. Heck, it was just Friday that I received a shipment of SV-10 harnesses for a variety of customers from them. The only thing I can hope is that cooler heads prevail and everyone can still end up with a system. Personally I still think the actual units are good units, but this whole mess is leaving a really bad taste in my mouth. Suffice to say that as an outcome of this, as a business we WILL NOT ever sell another product to customers where the distributor or mfgr requires money up front, even 50% (like another EFIS mfgr). I'm able to run my business without using customers money up front, and I expect the same from mfgrs. If they can't do it, then something is wrong. I can't stand sitting on customers money when there is no product, hence the reason we just can't easily "pay everyone back". In closing, I'd urge everyone to try and be patient for a few days while all of us dealers sort out this mess and figure out our options both legally and professionally for us and out customers. Rest assured we've all had some initial legal counsel on this and there is no doubt going to be more. As the largest seller of Chelton products to the RV market, I can guarantee you I'll sleep less than anyone during the next few days/weeks. We're all working off of very little information, and what we do have is sketchy at best. Getting good, accurate & detailed information in the next week is going to be impossible. We're going to do our best to contact each one of you individually to review your specific situation, but at the moment there isn't going to be any solid answers because we just don't know where this is going to end up. Like I said, hopefully some intelligent and cool heads at Chelton will prevail. Like Tim, I'm deeply saddened by this mess because I was one the loudest proponents of the Chelton EFIS line and personally have the good fortune to call many of you my friends. Being treated like this isn't fair, good, or reasonable and not the way to do business. I sincerely apologize for what I can right now.....but we all need to sit tight for a few days and see what comes out of this. It just makes me sick to see this sort of thing happen over and over again in aviation. What is it with people who run these businesses that they just think it's ok to take/spend/loose people's hard earned money and then walk away? Dealing with issues like this makes my blood boil. I can't fathom treating people like that, and I can't imagine why anyone would let their business get to that point without even asking for help, warning the customers/dealers, etc......these sort of things don't happen overnight and to pretend they do is dubious at best and unfortuneately I'm sure this won't be the last time we see it. Best regards and try to have a happy holiday, Stein. ________________________________________________________________________________
From: "noel(at)blueskyaviation.net" <noel(at)blueskyaviation.net>
Date: Dec 24, 2006
Subject: cleco size
anyone on line right now that can give me the barel dimentions of a celeco and the largerest damiter pice that kees into the coleco plyers. Thank you noel -------------------------------------------------------------------- mail2web - Check your email from the web at http://mail2web.com/ . ________________________________________________________________________________
Date: Dec 24, 2006
From: NYTerminat <nyterminat(at)aol.com>
Subject: Re: short field performance
To all that are flying the RV10, What is your take on the short field performance of the 10? The Vans site is quoting a lightly loaded (2200lb) 10 will get off the ground in 325 ft and land in 525. Is this a real number of hype? I have a private strip with 1300 feet of grass and obstacles at both ends, will the 10 fit in it? I am considering building a 10 or a Sportsman 2+2. Believe it or not the 10 is less money for the kit. I am not a new pilot, 1400 hrs in single, multi and Helicopter. Thanks and have a Merry Christmas Bob Spudis ________________________________________________________________________________
From: "Rick Gray" <rickgray(at)roadrunner.com>
Subject: Re: Rudder wiring
Date: Dec 24, 2006
Hi Les....yup...I'm missed it (sorry).....posting my reply here for archives: -yes...build your rudder 'completely'...this includes top and bottom fairings. You can send it off for paint as well. -yes again...the wires will run through the lower vert stab spar...just below the lower rod end bearing attach bracket (off to the side of the internal tie down mount). Route the wires into the rudder about 1/8" above the upper cutout of the lower rudder fairing....you can notch the fairing in this area if needed to accept the wires. -as mentioned earlier....make your harness long enough to a) pull the harness out of the light attach fairing portion of the fairing for light replacement and b) to pull the wires 'forward' for rudder removal (you never know) using some type of plug connection (molex or spade will work...just makes sure it's small enough to pass through the hole for the light). -lastly...the wire loom will be laying in the bottom of the fairing for time and all eternity......your concerns of wire abrasion and chaffing are valid...the inside of the fiberglass fairing is rough. I always wrap my wire loom in this area with some 'spiral wrap'. You can buy it at ACS or at your local Radio Shack. The stuff at Radio Shack is a lot cheaper and will work fine in this area but the stuff from ACS is more heat tolerant. Good luck and Happy Holidays. Rick in Ohio at the Buffalo Farm http://rv6rick.tripod.com/ohiovalleyrvators/ Hi Rick I posted this after your last post on the RV10 list and perhaps you missed it. I have taken the liberty of sending it to you directly as I am still a bit confused / uncertain as to whether or not I can form the rudder leading edges in advance of installing the rudder wiring. I am assuming that the rudder lighting wires run through the interior of the rudder - is this the case? I have an opportunity to have some of my completed sections painted and would like to include the rudder section included when I drop them off at the paint shop. Regards & Merry Christmas Les Kearney ----- Original Message ----- From: LES KEARNEY To: rv10-list(at)matronics.com Sent: Saturday, December 23, 2006 3:12 PM Subject: Re: RV10-List: Rudder wiring Hi Rick I understand what you have posted - many thanks. Is there a chaffing issue for the wires that run the length of the rudder interior? I would be concerned about chaffing against the rudder stringers or is this a misplaced concern? Inquiring minds need to know Les Kearney RV10 #40643 - Lost in the empennage ----- Original Message ----- From: Rick Gray <rickgray(at)roadrunner.com> Date: Saturday, December 23, 2006 12:47 pm Subject: Re: RV10-List: Rudder wiring > Hi Les, > 1-The servo wiring will terminate at the servo in the forward > section of the tailcone. > > 2-The trim motor wiring will terminate at the trim motor just > below the forward emp fairing. > > 3-As for the rudder....depending on your lighting....you'll end up > with wires for the strobe and nav light passing through the lower > section of the vertical stab spar. Easiest way (imo) is to drill > just below the bottom rudder hinge bracket. You may need to place > a grommet in from each end of the spar for protection. Also, you > may want to drill just off to the side as to not penetrate the > tail tie down reinforcement. This will line your wires up just > below the lower rod end bearing, allowing you to pass the wires > through the lower fairing. For clarity....the wires will pass > through the leading edge of the rudder in the opening just above > the fiberglass fairing. I've done 5 or 6 these now and I always > use a good connector in this area. Leave your harness long enough > so that you can pull the tail light out and disconnect the wires > for a) tail light replacement and b) rudder removal. The harness > and connector will be stowed inside the lower fairing...savvy?? > > Also, the wire for the lights can terminate at the bolt (use a > ring terminal) at the lower rod end bearing attach.....rudder side > of the spar. > > Hope this helps....Good Luck Les, > > Rick in Ohio at the Buffalo Farm > http://rv6rick.tripod.com/ohiovalleyrvators/ > > ----- Original Message ----- > From: Les Kearney > To: rv10-list(at)matronics.com > Sent: Saturday, December 23, 2006 12:51 PM > Subject: RV10-List: Rudder wiring > > > Hi > > > > I have been wandering through the archives for info on rudder > wiring. I believe that the preferred exit for trim servo wiring as > well as other wiring is at the base of the rudder. For me wiring > is a dark art at the moment and I am a bit concerned about > building myself into a corner. In particular, my access to the > rudder interior will be somewhat limited if I roll and rivet the > rudder leading edges. > > > > My question is: how are wires secured in the interior of the > rudder so that they do not chaff against the rudder stiffeners? > Should I wait until wiring is done to complete the rudder? > > > > Inquiring minds need to know > > > > Les Kearney > > #40643 - Lost in the empennage > > > > > > > ________________________________________________________________________________
Date: Dec 24, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Re: Baggage door
Robb.. Glad to, easy week next week so I'll be in touch. I hope I can get to you soon enough, you know, to wipe out all those bad things Bob showed you. I'll give you a call Tuesday...family awaits till then. Before you flame me ...I just snuck away for a minute to peek at the emails...whew...wish I hadn't!! Rick S. 40185 do notarchive ________________________________________________________________________________
From: "Wayne Edgerton" <wayne.e(at)grandecom.net>
Subject: Re: Oxygen exterior fill port
Date: Dec 25, 2006
I have installed my Mountain High system bottle behind the baggage compartment mounted on the back of the wall with a remote fill extending into the baggage compartment through the wall. I got the idea from Randy D and I think it will work well for my needs. He has pictures posted on his web site at http://myrv10.com/N610RV/index.html Also Russ Daves built a really nice system where he put the bottle just behind the rear seat in the baggae compartment and built a protective cover that went over the bottle. That way he didn't have to worry about banging it with baggage. He did a really nice job on it. I'm sure if you asked him he would forward you the pictures of it. Both Russ's system and mine are four place systems. I will be installed the outlets in the rear somewhere in or near the arm rest area and in the front down near the knee area. Wayne Edgerton #40336 ________________________________________________________________________________
From: "Russell Daves" <dav1111(at)cox.net>
Subject: Re: short field performance
Date: Dec 25, 2006
Bob: A single pilot half gas 260HP RV-10 can take off and land on a 1300 foot grass strip on a no wind day but it is going to be tight. As far as obstacles at both end it is going to depend on height of the obstacles. Now for real life experience. I have flown my RV-10 (IO-540 260 HP with MT prop) in and out of a 1600 foot grass strip multiple times. Such strip 12TX (1235 MSL) shows on the FAA posting as being 2000 feet but it is really closer to 1600 feet with an over run at each end that should not be factored into determining the length of the runway. In addition 12TX has 80 foot trees at the south end (they may have been 30 feet when the runway was built but they are closer to 80 now - High line wires are lower than the tree tops). Occasionally the tree tops at the end of the runway get cut back by the power line company but I have never seen them cut back all the way to the high line wires, more to get the branches away from the high line wires. At the north end there are 30' High Line wires as well. The runway also slops sharply downhill to the south (probably at least a 50 feet elevation difference in the runway from north to south. I have flown in and out of 12TX with my RV-10 (4 times). Both with a fair amount of baggage, single pilot (240 lbs), and full fuel. Flown out with half tanks and minimum baggage with pilot and co-pilot (480 lbs) as well. On a no wind day I use the south runway for landing as it goes uphill and the north runway for takeoff. With wind, I use whichever runway the wind favors naturally. Is 12TX tight? You bet your bippie. Is it to tight? Not if you have good short field landing abilities. Would I take off with full passengers and full fuel on a no wind or light wind day? No, I would send the passengers over to BMQ and tell them I would pick them up there. Are Van's figures fluff? Probably not. I suspect that I could drag N710RV on a sea level runway and stop it using light brakes in less than 525 feet where there are no obstacles on a no wind day. I am not sure I could get it off the ground in 325 feet on a no wind day at sea level but it is possible. So far I have never flown N710RV out of a sea level location so I am somewhat shooting from the hip. I will say this for Van's, they have been really accurate on their specs and I have no doubt that Dick Vangrundson himself can do anything in any of his RV's that he says can be done. That doesn't mean that I am a good enough pilot to duplicate his abilities. The real question is would I as a 1500+ hour pilot (almost all being high performance)regularly fly in and out of a 1300 foot level strip with 30' highline wires at both ends? The answer is yes if the elevation is less than 1500 MSL and if I plan to fly it regularly with less than 500 lbs of gas and bodies. The answer is no if I planned on flying it regularly with more than 800 lbs of gas and bodies. Hope this helps you make a decision on the RV-10 vs. the sportsman 2+2. I will tell you that you won't find a better company than Van's to deal with or a better bunch of people than the RV crowd. I can't tell you how much more happier I have been switching from flying spam cans to flying RV's. Russ Daves N710RV - RV-10 first flight 7/28/06 76+ hours and climbing N610RV - RV-6A Sold (280 hours flight time) RV-8 - Under construction ________________________________________________________________________________
Date: Dec 25, 2006
Subject: Re: short field performance
From: "Jesse Saint" <jesse(at)itecusa.org>
I replied to this yesterday, but I guess it didn't go through because I forgot to resize the attachment. Now I am on a different computer using webmail, so I don't have the picture. My answer would be that my dad has tested N256H against Van's numbers and he feels that they are accurate. My dad, of course, has at least several hundred hours flying in and out of jungle strips in Ecuador, so he is self-trained and fairly avid Bush Pilot. I would say that it can be done at the weight you stated, given that it is not too high above sea level, that the strip is fairly flat and hard, and there aren't a bunch of ant hills like the strip we tested in FL. My dad would probably get in and out of a strip like that @ gross if he needed to. I would recommend you find an RV-10 and owner and see if they will give you a demo. If nothing else, find a strip that is similar in elevation and level-ness but longer and mark off your strip and see how it performs to that mark. If you are satisfied with that, then that makes a difference. I have researched the 2+2 a fair bit and even though it quotes being a lot more STOL than the -10, I would say that at the useful load you stated, it probably would give the 2+2 a run for its money on takeoff and landing performance. When it comes to all other performance, the -10 (IMHO) beats the 2+2 hands down. Where are you located? Jesse Saint > Bob: > > A single pilot half gas 260HP RV-10 can take off and land on a 1300 foot > grass strip on a no wind day but it is going to be tight. As far as > obstacles at both end it is going to depend on height of the obstacles. > > Now for real life experience. I have flown my RV-10 (IO-540 260 HP with > MT prop) in and out of a 1600 foot grass strip multiple times. Such strip > 12TX (1235 MSL) shows on the FAA posting as being 2000 feet but it is > really closer to 1600 feet with an over run at each end that should not be > factored into determining the length of the runway. > > In addition 12TX has 80 foot trees at the south end (they may have been 30 > feet when the runway was built but they are closer to 80 now - High line > wires are lower than the tree tops). Occasionally the tree tops at the > end of the runway get cut back by the power line company but I have never > seen them cut back all the way to the high line wires, more to get the > branches away from the high line wires. At the north end there are 30' > High Line wires as well. The runway also slops sharply downhill to the > south (probably at least a 50 feet elevation difference in the runway from > north to south. > > I have flown in and out of 12TX with my RV-10 (4 times). Both with a fair > amount of baggage, single pilot (240 lbs), and full fuel. Flown out with > half tanks and minimum baggage with pilot and co-pilot (480 lbs) as well. > On a no wind day I use the south runway for landing as it goes uphill and > the north runway for takeoff. With wind, I use whichever runway the wind > favors naturally. > > Is 12TX tight? You bet your bippie. Is it to tight? Not if you have > good short field landing abilities. Would I take off with full passengers > and full fuel on a no wind or light wind day? No, I would send the > passengers over to BMQ and tell them I would pick them up there. > > Are Van's figures fluff? Probably not. I suspect that I could drag > N710RV on a sea level runway and stop it using light brakes in less than > 525 feet where there are no obstacles on a no wind day. I am not sure I > could get it off the ground in 325 feet on a no wind day at sea level but > it is possible. So far I have never flown N710RV out of a sea level > location so I am somewhat shooting from the hip. I will say this for > Van's, they have been really accurate on their specs and I have no doubt > that Dick Vangrundson himself can do anything in any of his RV's that he > says can be done. That doesn't mean that I am a good enough pilot to > duplicate his abilities. > > The real question is would I as a 1500+ hour pilot (almost all being high > performance)regularly fly in and out of a 1300 foot level strip with 30' > highline wires at both ends? The answer is yes if the elevation is less > than 1500 MSL and if I plan to fly it regularly with less than 500 lbs of > gas and bodies. The answer is no if I planned on flying it regularly with > more than 800 lbs of gas and bodies. > > Hope this helps you make a decision on the RV-10 vs. the sportsman 2+2. I > will tell you that you won't find a better company than Van's to deal with > or a better bunch of people than the RV crowd. I can't tell you how much > more happier I have been switching from flying spam cans to flying RV's. > > Russ Daves > N710RV - RV-10 first flight 7/28/06 76+ hours and climbing > N610RV - RV-6A Sold (280 hours flight time) > RV-8 - Under construction Jesse Saint I-TEC, Inc. jesse(at)itecusa.org www.itecusa.org ________________________________________________________________________________
Date: Dec 25, 2006
Subject: Re: Oxygen exterior fill port
From: "Jesse Saint" <jesse(at)itecusa.org>
We have used the Sky-Ox portable 4-place tank and we lay it on the tunnel cover between the rear seats and use it as an arm rest for the back seat. You could easily install some straps on the tunnel cover(s) to hold it in place. The padded carrying back helps to keep it from being an eyesore or an elbowsore. Jesse > I have installed my Mountain High system bottle behind the baggage > compartment mounted on the back of the wall with a remote fill extending > into the baggage compartment through the wall. I got the idea from Randy D > and I think it will work well for my needs. He has pictures posted on his > web site at http://myrv10.com/N610RV/index.html > > Also Russ Daves built a really nice system where he put the bottle just > behind the rear seat in the baggae compartment and built a protective > cover that went over the bottle. That way he didn't have to worry about > banging it with baggage. He did a really nice job on it. I'm sure if you > asked him he would forward you the pictures of it. > > Both Russ's system and mine are four place systems. I will be installed > the outlets in the rear somewhere in or near the arm rest area and in the > front down near the knee area. > > Wayne Edgerton #40336 Jesse Saint I-TEC, Inc. jesse(at)itecusa.org www.itecusa.org ________________________________________________________________________________
Date: Dec 25, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: My Favorite Christmas present!
See attachment. <http://forums.matronics.com> *Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ Merry Christmas to all! * ________________________________________________________________________________
Date: Dec 25, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: My Favorite Christmas present!
Does that mean no building on Christmas. Happy Holidays Larry Deems Davis wrote: > > See attachment. > > <http://forums.matronics.com> > *Deems Davis # 406 > Finishing - ( A Misnomer ! ) > http://deemsrv10.com/ > > > Merry Christmas to all! > * > > ------------------------------------------------------------------------ > ________________________________________________________________________________
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: My Favorite Christmas present!
Date: Dec 25, 2006
I gotta get me one....where? BTW, nice looking -10 under construction in the background.... Merry Christmas and Happy New Year! ----- Original Message ----- From: "Deems Davis" <deemsdavis(at)cox.net> Sent: Monday, December 25, 2006 12:18 PM Subject: RV10-List: My Favorite Christmas present! > > See attachment. > > <http://forums.matronics.com> > *Deems Davis # 406 > Finishing - ( A Misnomer ! ) > http://deemsrv10.com/ > > > Merry Christmas to all! > * > ________________________________________________________________________________
Date: Dec 27, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: Surface Corrosion?
Hi This evening I was starting to prep my tail cone parts. When removing the vinyl wrap, one piece had some unusual surface discoloration. I thought it might be some adhesive and tried removing it with lacquer thinner but to no avail. It looks like a mineral deposit of some sort. Is this surface corrosion and if so how to handle this. I have attached a couple of pictures. Inquiring minds need to know Les Kearney RV10 # 40643 - Lost in the empennage PS: I hope everyone had a fun Christmas and is looking forward to a great New Year! ________________________________________________________________________________
From: "RV_10" <john_rv10(at)yahoo.com>
Subject: Surface Corrosion?
Date: Dec 28, 2006
Hi Les, Yes, that looks very much like filiform corrosion. You will find that alodine won't take to that area. A relatively painless but time consuming solution I found for the same problem is to remove the filiform corrosion with a small grinder with a felt pad with some aluminum polishing paste. This preps the surface for alodining then painting as you prefer. Other methods of removing the filiform corrosion I tried left the surface too marked for my liking. Cheers, John (wings) _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Les Kearney Sent: Thursday, 28 December 2006 1:08 PM Subject: RV10-List: Surface Corrosion? Hi This evening I was starting to prep my tail cone parts. When removing the vinyl wrap, one piece had some unusual surface discoloration. I thought it might be some adhesive and tried removing it with lacquer thinner but to no avail. It looks like a mineral deposit of some sort. Is this surface corrosion and if so how to handle this. I have attached a couple of pictures. Inquiring minds need to know Les Kearney RV10 # 40643 - Lost in the empennage PS: I hope everyone had a fun Christmas and is looking forward to a great New Year! ________________________________________________________________________________
From: <gommone7(at)bellsouth.net>
Subject: Re: Surface Corrosion?
Date: Dec 28, 2006
Hi Les,I did recive one of my wings bottom skins in the same conditions,it is a no brainer,I ask them if my dollars have some kind of surface corrosion,don't even ask what to do ,ask only for a replacement,that simple, Cheers ,Hugo #40456 > > From: Les Kearney <kearney(at)shaw.ca> > Date: 2006/12/27 Wed PM 09:08:03 EST > To: rv10-list(at)matronics.com > Subject: RV10-List: Surface Corrosion? > > Hi > > > > This evening I was starting to prep my tail cone parts. When removing the > vinyl wrap, one piece had some unusual surface discoloration. I thought it > might be some adhesive and tried removing it with lacquer thinner but to no > avail. It looks like a mineral deposit of some sort. Is this surface > corrosion and if so how to handle this. > > > > I have attached a couple of pictures. > > > > Inquiring minds need to know > > > > Les Kearney > > RV10 # 40643 - Lost in the empennage > > > > PS: I hope everyone had a fun Christmas and is looking forward to a great > New Year! > > > ________________________________________________________________________________
From: "Bob Leffler" <rvmail(at)thelefflers.com>
Subject: Surface Corrosion?
Date: Dec 28, 2006
Les's issue with corrosion reminded me of a topic I wanted to solicit opinions from the list. I attended a RV builder's class a couple weeks ago at Grov-Air in Indy. Troy Grover, the gentleman conducting the class stated that he has seen several RVs that have significant corrosion along the lines were the vinyl wrap was removed by a soldering iron. His conclusion was that dirt was collecting in the edge of the vinyl and absorbing moisture. He stated that he's seen this in the last couple kits that have come through his shop. Since my empennage kit is in route at the moment, I am thinking about the approach I want to take. My current desire is to leave the vinyl on as long as possible to minimize scratching. Does anyone know of anyone that has experienced corrosion along the lines of the vinyl that were cut with a soldering iron? It seems like the only way to prevent the issue that Les has discovered is to remove the vinyl when you inventory, but I would think would have disastrous effect of the quality of the surface. I am very interested in hearing on how Van's handles Les's issue. I am optimistic that they will replace the part for Les. _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Les Kearney Sent: Wednesday, December 27, 2006 9:08 PM Subject: RV10-List: Surface Corrosion? Hi This evening I was starting to prep my tail cone parts. When removing the vinyl wrap, one piece had some unusual surface discoloration. I thought it might be some adhesive and tried removing it with lacquer thinner but to no avail. It looks like a mineral deposit of some sort. Is this surface corrosion and if so how to handle this. I have attached a couple of pictures. Inquiring minds need to know Les Kearney RV10 # 40643 - Lost in the empennage PS: I hope everyone had a fun Christmas and is looking forward to a great New Year! ________________________________________________________________________________
From: "Bob Leffler" <rvmail(at)thelefflers.com>
Subject: Some more newbie questions
Date: Dec 28, 2006
For those that went the alumiprep, alodine, akzo prime (no primer war discussion), what quantity of these should be initially ordered? Is the shelf life long enough to order quantities for the entire aircraft? Is there a better source for these other than Aircraft Spruce? I understand that alodine can also be obtained in a powder form. Is it cost effective for us in the quantities needed for the RV10? If so, where is a good source to obtain the powder form? What quantities and sizes of "oops" rivets should I order? I'm also looking for recommendations on a spray gun to use for priming. I don't have any experience with HVLP guns, so I am looking for what has worked well for others. Thanks, Bob ________________________________________________________________________________
Date: Dec 28, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: Some more newbie questions - spray gun
Use an inexpensive HPLV detail gun for priming. A regular sized gun is just to big and non HPLV gives too much overspray. Harbor freight has a spray gun on sale for $40 and it does a fine job. <http://www.harborfreight.com/cpi/ctaf/Displayitem.taf?itemnumber=46719>. Also here is a link to a guide on setting up the gun <http://purplesagetradingpost.com/sumner/techinfo/HVLPspraygun.html> The 2 gallon kit should be enough for the entire project. 2 year shelf life. No shelf life on the alumiprep, 1 gal will be more than enough. Alodine does have a 1 year shelf life in liquid form. Watch out for the hazmat shipping charges. If you go the solid alodine route let me know if you want to split the order. Larry Rosen #356 Bob Leffler wrote: > > > For those that went the alumiprep, alodine, akzo prime (no primer war > discussion), what quantity of these should be initially ordered? Is the > shelf life long enough to order quantities for the entire aircraft? > > Is there a better source for these other than Aircraft Spruce? > > I understand that alodine can also be obtained in a powder form. Is it cost > effective for us in the quantities needed for the RV10? If so, where is a > good source to obtain the powder form? > > What quantities and sizes of "oops" rivets should I order? > > I'm also looking for recommendations on a spray gun to use for priming. I > don't have any experience with HVLP guns, so I am looking for what has > worked well for others. > > Thanks, > > Bob > > > ________________________________________________________________________________
Subject: Re: Work Table Size
Date: Dec 28, 2006
From: "John W. Cox" <johnwcox(at)pacificnw.com>
Michael - in one word....Safety. The PVC can get brittle and burst with pressure or age. I had PVC for twenty years. The ole line then sprang a leak. I just ignored it. Shortly thereafter (a few months) the line splintered and burst into pieces. It was cheap, fast, easy as well as stupid of me. $1,000 for a commercial compressor then I cut a few corners in not upgrading the distribution system. Copper or galvanized steel pipe are favorites. Black pipe for natural gas is a no-no. Remember that the heat process of compressing air squeezes moisture out. It is in the tank, in the trap or in the lines. Pneumatic tools will talk back if the moisture is allowed to reach them. Remember at least two traps, one at the tank, one at the low point well down the line and when I paint, the final one before the gun with a desiccant capture trap to read the results. And yes... Jesse said "AMEN" which I am sure was so as to beckon someone of higher authority so your PVC doesn't send a shard into your backside (wallet) while bending over riveting. John -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Thursday, December 28, 2006 6:20 AM Subject: RE: RV10-List: Re: Work Table Size I'm curious. Is there a reason that everyone is using copper and other metal pipe for their air runs? Good ole SCH 40 PVC from just about any hardware store is rated for several times the PSI you will ever see from your compressor. Use half inch PVC and you will be done in half the time at a fraction of the cost. Michael - ________________________________________________________________________________
Date: Dec 28, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: My Favorite Christmas present!
Ralph, the sticker on the back lists: www.sayingsandsuch.com ph # 623 780 7657 Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ Ralph E. Capen wrote: > > I gotta get me one....where? > ________________________________________________________________________________
Date: Dec 28, 2006
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: My Favorite Christmas present!
Cool - thanks! -----Original Message----- >From: Deems Davis <deemsdavis(at)cox.net> >Sent: Dec 28, 2006 11:05 AM >To: rv10-list(at)matronics.com >Subject: Re: RV10-List: My Favorite Christmas present! > > >Ralph, the sticker on the back lists: www.sayingsandsuch.com ph # 623 >780 7657 > > >Deems Davis # 406 >Finishing - ( A Misnomer ! ) >http://deemsrv10.com/ > > >Ralph E. Capen wrote: > >> >> I gotta get me one....where? >> > > ________________________________________________________________________________
Date: Dec 28, 2006
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Work Table Size
I guess the counter to that would be....am I going to use this distribution line for 20 yrs? I don't think I would keep one for more than 10 yrs, probably less...but part of that is a function of my age. Everyone will have a different answer. On 12/28/06, John W. Cox wrote: > > Michael - in one word....Safety. The PVC can get brittle and burst with > pressure or age. I had PVC for twenty years. The ole line then sprang > a leak. I just ignored it. Shortly thereafter (a few months) the line > splintered and burst into pieces. It was cheap, fast, easy as well as > stupid of me. $1,000 for a commercial compressor then I cut a few > corners in not upgrading the distribution system. > > Copper or galvanized steel pipe are favorites. Black pipe for natural > gas is a no-no. Remember that the heat process of compressing air > squeezes moisture out. It is in the tank, in the trap or in the lines. > Pneumatic tools will talk back if the moisture is allowed to reach them. > Remember at least two traps, one at the tank, one at the low point well > down the line and when I paint, the final one before the gun with a > desiccant capture trap to read the results. > > And yes... Jesse said "AMEN" which I am sure was so as to beckon someone > of higher authority so your PVC doesn't send a shard into your backside > (wallet) while bending over riveting. > > John > > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder > (Michael Sausen) > Sent: Thursday, December 28, 2006 6:20 AM > To: rv10-list(at)matronics.com > Subject: RE: RV10-List: Re: Work Table Size > > > > I'm curious. Is there a reason that everyone is using copper and other > metal pipe for their air runs? Good ole SCH 40 PVC from just about any > hardware store is rated for several times the PSI you will ever see from > your compressor. Use half inch PVC and you will be done in half the > time at a fraction of the cost. > > Michael > > - > > ________________________________________________________________________________
From: Fixitauto(at)aol.com
Date: Dec 28, 2006
Subject: Fwd: Tornadoes Damage Florida - AOL News
Return-Path: Received: from rly-yg05.mx.aol.com (rly-yg05.mail.aol.com [172.18.180.83]) by air-yg01.mail.aol.com (v114.2) with ESMTP id MAILINYG14-28d4593df3e79; Thu, 28 Received: from dhs-tw2.dhs.state.ia.us (dhs-tw2.dhs.state.ia.us [165.206.254.82]) by rly-yg05.mx.aol.com (v114.2) with ESMTP id MAILRELAYINYG53-28d4593df3e79; Received: from 192.168.1.7 by dhs-tw2.dhs.state.ia.us with ESMTP (DHS X-Server-Uuid: 569ABC8D-9B8E-4C89-91D4-B0DF101FA699 Content-class: urn:content-classes:message MIME-Version: 1.0 X-MimeOLE: Produced By Microsoft Exchange V6.5 Subject: Tornadoes Damage Hundreds of Florida Homes - AOL News Date: Thu, 28 Dec 2006 09:14:00 -0600 X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: Tornadoes Damage Hundreds of Florida Homes - AOL News Thread-Index: Accqks5yeB66iHSLReuOtRKe1JY4rg= From: "Kurschinski, Wayne" <wkursch(at)dhs.state.ia.us> X-TMWD-Spam-Summary: TS 061228151719; SEV=2.0.2; DFV=A2006122805; IFV=2.0.4,4.0-8; RPD=4.00.0004; ENG=IBF; RPDID=303030312E30413031303230362E34353933444441462E303036422D462D354D6B5771624878794D6F48336B5173625962506F513D3D; CAT=NONE; CON=NONE X-WSS-ID: 698D00751K8684037-01-01 Content-Type: multipart/mixed; boundary="----_=_NextPart_001_01C72A92.CD976189" X-AOL-IP: 165.206.254.82 ------_=_NextPart_001_01C72A92.CD976189 Content-Type: multipart/alternative; boundary="----_=_NextPart_002_01C72A92.CD976189" Content-Transfer-Encoding: 7bit ------_=_NextPart_002_01C72A92.CD976189 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable <> ------_=_NextPart_002_01C72A92.CD976189 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable Tornadoes Damage Hundreds of Florida Homes - AOL News

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------_=_NextPart_001_01C72A92.CD976189-- ________________________________________________________________________________
From: EMAproducts(at)aol.com
Date: Dec 28, 2006
Subject: OT Riteangle 3b customers
12/2006 Gentlemen, Currently I have less than 30% of our customers current e-mail addresses. I am attempting to update our mailing lists to see if they have any questions re their RiteAngle IIIb Angle of Attack systems. Occasionally I get a call from someone who purchased a system several years ago and still do not have system installed or set-up due to various reasons. Should you have any questions, comments, photos of system installed in your plane, endorsements or whatever re: the RiteAngle IIIb system please send it to this address _riteangle3(at)aol.com_ (mailto:riteangle3(at)aol.com) Thankfully, since the IIIb system has gone into production, we have had no changes in the electronics, however we now have a professional written setup manual. Sincerely Elbie EM Aviation, LLC ________________________________________________________________________________
Date: Dec 28, 2006
From: "Pascal" <rv10builder(at)verizon.net>
Subject: Re: Fwd: Tornadoes Damage Florida - AOL News
Imagine ERAU- http://www.eaa.org/communications/eaanews/061228_embryriddle.html ----- Original Message ----- From: Fixitauto(at)aol.com To: rv10-list(at)matronics.com Sent: Thursday, December 28, 2006 10:58 AM Subject: RV10-List: Fwd: Tornadoes Damage Florida - AOL News ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: In the Holiday Spirit, want to share with you.
Date: Dec 28, 2006
Hey gang, Since I will sooner or later be part of your community, that is the power one, I want to share with you my latest addition to my web page. Last Summer I visited Telluride, Colorado and brought my sailplane. I've included a video of that flight on my web site, but you need high speed internet and quicktime. I did the filming so you miss my glider, but you can see my clean machine by viewing the stills on the video aswell as from the sunset picture above the video link. Have a look at what its like to do it without an engine. Next month I will be forwarding something in print which I got included in an online newsletter which you can all benefit from once you finish your planes and if you fly it to Telluride. You better have the big engine or a smaller one with a turbo for that airport. Density altitude at the airport can be up to 12K on summer days. Go to: wwwjohngonzalezdds.com other interest section click on the picture which says, "Telluride Video Short" Enjoy and Happy New Year. JOhn Gonzalez, N112ST Lak17a, Also known as "2 Sierra Tango" in my other life. Building but stalled on electrical in fuse. #409 ________________________________________________________________________________
From: Jeff Carpenter <jeff(at)westcottpress.com>
Subject: When Pro Seal Goes Bad
Date: Dec 28, 2006
I've got a Pro Seal Kit which officially expires this month... though I've had it in the freezer for all but a few hours since I bought it. What does bad Pro Seal look like? How does it behave? Jeff Carpenter 40304 ________________________________________________________________________________
Subject: When Pro Seal Goes Bad
Date: Dec 28, 2006
From: "John W. Cox" <johnwcox(at)pacificnw.com>
It loses its adhesion characteristics. Wouldn't it be nice if it changed color radically when mixed. Oh yeh, it does... I just meant a truly different and more noticeable color. It remains paintable. John Cox 40600 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jeff Carpenter Sent: Thursday, December 28, 2006 1:41 PM Subject: RV10-List: When Pro Seal Goes Bad I've got a Pro Seal Kit which officially expires this month... though I've had it in the freezer for all but a few hours since I bought it. What does bad Pro Seal look like? How does it behave? Jeff Carpenter 40304 ________________________________________________________________________________
Subject: Surface Corrosion?
Date: Dec 28, 2006
From: "John W. Cox" <johnwcox(at)pacificnw.com>
Les, that's an Excellent read of all eleven (11) web pages. This is what I play with every night while other builder's sleep. It brings clarity to the issues of alodine, anodize and proper surface preparation including final topcoat application without a "declaration of war". The final corrective solution often involves Eddy Current, Ultra-sound or X-ray (all expensive diagnostics) and drives home the value of prevention rather than intervention due to poor preparation during initial construction. John Cox ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Les Kearney Sent: Thursday, December 28, 2006 8:25 AM Subject: RE: RV10-List: Surface Corrosion? Ooops I forgot to attach the link. It is: http://aluminium.matter.org.uk/content/html/eng/default.asp?catid=180&p a geid=2144416691 Cheers Les ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: D2A
Date: Dec 28, 2006
check this http://www.xbow.com/Support/Support_pdf_files/Service_Letter_NAV425-06-02 .pdf http://www.xbow.com/General_info/Info_pdf_files/AHRS425_Upgrade_Program.p df http://www.xbow.com/General_info/Info_pdf_files/D2A_Press_Release.pdf ________________________________________________________________________________
Subject: Copper vs PVC air lines
Date: Dec 28, 2006
From: "John W. Cox" <johnwcox(at)pacificnw.com>
Anyone cutting financial plumbing corners want some of my ole PVC shards? System worked just fine until it failed. I am now retro-fitting with approved materials. I know, some knucklehead will say the PVC of 2006 is new and improved over Schedule 40 PVC of 1983. Think Safety, do it Right, do it Once, save the time for Flying. John Cox #40600 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of JOHN STARN Sent: Thursday, December 28, 2006 10:41 AM Subject: RV10-List: Copper vs PVC air lines Being an ole plumbing contractor (25 years plus) I have installed thousands of feet of copper air lines (up to 4") and hundreds of feet of Sch. 40 & 80 PVC pipe. PVC sch 40 pipe is a lot better than thin wall sprinkler PVC but it will still shatter & explode IF a fracture occurs. It will whip about under pressure and throw shrapnel shards until the air is turned off. How do you fracture PVC ?, Good question. Pull too hard on the connected air line, accidentally hit it with a blunt object, allow it to be exposed to sunlight, "flip" the tangled air hose. Copper will bend, bent, split, crimp BUT it does not fly apart. Sch 80 ??, about the same cost as copper. Type "L" (blue printing on the pipe) copper is not cheap but will last forever. Type "M" (red printing) is OK ? ? BUT I use it ONLY for non pressure lines & wind chimes. Fittings ??, you will only find "L" fittings at Lowes & Home Depot....Why ??, 'cause they don't make "M" fittings. "M" is thinner & drawn harder, brittle, "L" just works better. Want to try a test....Take a 20' piece of sch 40 PVC (put on a jacket, gloves, eye protection (full motorcycle helmet) grab one end of the PVC & slam/snap onto your driveway. Then go back to Lowes & buy the copper right after you pick up the shattered remain of the PVC. KABONG Do Not Archive (It's in there several times from me over the years. 8*) ----- Original Message ----- From: "Jesse Saint" <jesse(at)itecusa.org> Sent: Thursday, December 28, 2006 6:56 AM > I'm curious. Is there a reason that everyone is using copper and other > metal pipe for their air runs? Good ole SCH 40 PVC from just about any > hardware store is rated for several times the PSI you will ever see from > your compressor. Use half inch PVC and you will be done in half the time > at > a fraction of the cost. > > Michael ________________________________________________________________________________
Date: Dec 28, 2006
From: "Pascal" <rv10builder(at)verizon.net>
Subject: Re: Copper vs PVC air lines
Sorry I asked the question, but also glad I did. I've decided I'll run a nylon air hose to the ceiling and make due. Less chance I'll need a heat gun, a motorcycle helmet nor any concern for PVC shrapnel, and it's just so much easier to run it and remove it if I ever need to move it somewhere. We are only talking a two car garage, of which I am renting half the space from my wife, If I ever decide to just use the hose off the ground I think my odds are safer to trip over 15 feet of hose and knock my head then the other more dangerous piping options. Seriously thou, I do appreciate the feedback and thank everyone for the thoughts. I'll (really) decide when the time comes what I'll do, even PVC might work as I have no intention of using it in the garage for more than this project and that, I hope, will not take 20 plus years. Thanks! Pascal ----- Original Message ----- From: "John W. Cox" <johnwcox(at)pacificnw.com> Sent: Thursday, December 28, 2006 2:26 PM Subject: RE: RV10-List: Copper vs PVC air lines > > Anyone cutting financial plumbing corners want some of my ole PVC > shards? System worked just fine until it failed. I am now > retro-fitting with approved materials. I know, some knucklehead will > say the PVC of 2006 is new and improved over Schedule 40 PVC of 1983. > > Think Safety, do it Right, do it Once, save the time for Flying. > > John Cox > #40600 > > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of JOHN STARN > Sent: Thursday, December 28, 2006 10:41 AM > To: rv10-list(at)matronics.com > Subject: RV10-List: Copper vs PVC air lines > > > Being an ole plumbing contractor (25 years plus) I have installed > thousands > of feet of copper air lines (up to 4") and hundreds of feet of Sch. 40 & > 80 > PVC pipe. PVC sch 40 pipe is a lot better than thin wall sprinkler PVC > but > it will still shatter & explode IF a fracture occurs. It will whip about > > under pressure and throw shrapnel shards until the air is turned off. > How do you fracture PVC ?, Good question. Pull too hard on the connected > air > line, accidentally hit it with a blunt object, allow it to be exposed to > > sunlight, "flip" the tangled air hose. Copper will bend, bent, split, > crimp > BUT it does not fly apart. Sch 80 ??, about the same cost as copper. > Type > "L" (blue printing on the pipe) copper is not cheap but will last > forever. > Type "M" (red printing) is OK ? ? BUT I use it ONLY for non pressure > lines & > wind chimes. Fittings ??, you will only find "L" fittings at Lowes & > Home > Depot....Why ??, 'cause they don't make "M" fittings. "M" is thinner & > drawn > harder, brittle, "L" just works better. > Want to try a test....Take a 20' piece of sch 40 PVC (put on a jacket, > gloves, eye protection (full motorcycle helmet) grab one end of the PVC > & > slam/snap onto your driveway. Then go back to Lowes & buy the copper > right > after you pick up the shattered remain of the PVC. KABONG Do Not > Archive > (It's in there several times from me over the years. 8*) > ----- Original Message ----- > From: "Jesse Saint" <jesse(at)itecusa.org> > To: > Sent: Thursday, December 28, 2006 6:56 AM > >> I'm curious. Is there a reason that everyone is using copper and > other >> metal pipe for their air runs? Good ole SCH 40 PVC from just about > any >> hardware store is rated for several times the PSI you will ever see > from >> your compressor. Use half inch PVC and you will be done in half the > time >> at >> a fraction of the cost. >> >> Michael > > > ________________________________________________________________________________
From: "noel anderson" <nandrand(at)xtra.co.nz>
Subject: Re: Copper vs PVC air lines
Date: Dec 29, 2006
John. How right you are. Me, I like old fashioned steel gas tube!!! Not that much differance in price........Put the tube on the ceiling, hang the air hose(or coil) down, coil will spring up out of the way of your work surface!!!!!! Use Aro fittings or simular (quick change) I don't sell them.................Just my 2cents...... Happy New Year to every body....... Regards Noel ----- Original Message ----- From: "John W. Cox" <johnwcox(at)pacificnw.com> Sent: Friday, December 29, 2006 11:26 AM Subject: RE: RV10-List: Copper vs PVC air lines > > Anyone cutting financial plumbing corners want some of my ole PVC > shards? System worked just fine until it failed. I am now > retro-fitting with approved materials. I know, some knucklehead will > say the PVC of 2006 is new and improved over Schedule 40 PVC of 1983. > > Think Safety, do it Right, do it Once, save the time for Flying. > > John Cox > #40600 > > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of JOHN STARN > Sent: Thursday, December 28, 2006 10:41 AM > To: rv10-list(at)matronics.com > Subject: RV10-List: Copper vs PVC air lines > > > Being an ole plumbing contractor (25 years plus) I have installed > thousands > of feet of copper air lines (up to 4") and hundreds of feet of Sch. 40 & > 80 > PVC pipe. PVC sch 40 pipe is a lot better than thin wall sprinkler PVC > but > it will still shatter & explode IF a fracture occurs. It will whip about > > under pressure and throw shrapnel shards until the air is turned off. > How do you fracture PVC ?, Good question. Pull too hard on the connected > air > line, accidentally hit it with a blunt object, allow it to be exposed to > > sunlight, "flip" the tangled air hose. Copper will bend, bent, split, > crimp > BUT it does not fly apart. Sch 80 ??, about the same cost as copper. > Type > "L" (blue printing on the pipe) copper is not cheap but will last > forever. > Type "M" (red printing) is OK ? ? BUT I use it ONLY for non pressure > lines & > wind chimes. Fittings ??, you will only find "L" fittings at Lowes & > Home > Depot....Why ??, 'cause they don't make "M" fittings. "M" is thinner & > drawn > harder, brittle, "L" just works better. > Want to try a test....Take a 20' piece of sch 40 PVC (put on a jacket, > gloves, eye protection (full motorcycle helmet) grab one end of the PVC > & > slam/snap onto your driveway. Then go back to Lowes & buy the copper > right > after you pick up the shattered remain of the PVC. KABONG Do Not > Archive > (It's in there several times from me over the years. 8*) > ----- Original Message ----- > From: "Jesse Saint" <jesse(at)itecusa.org> > To: > Sent: Thursday, December 28, 2006 6:56 AM > >> I'm curious. Is there a reason that everyone is using copper and > other >> metal pipe for their air runs? Good ole SCH 40 PVC from just about > any >> hardware store is rated for several times the PSI you will ever see > from >> your compressor. Use half inch PVC and you will be done in half the > time >> at >> a fraction of the cost. >> >> Michael > > > ________________________________________________________________________________
Date: Dec 28, 2006
From: Shawn Moon <moons1999(at)yahoo.com>
Subject: Re: Fwd: Tornadoes Damage Florida - AOL News
I got the below e-mail from the EAA on this as well. ERAU lost 50 aircraft and are looking for some short term replacements. As an alum (Prescott AZ campus) I can vouch that the maintenance on these airplanes is top notch a nd they are well taken care of. I have personal experience with this type of incident, although not as extreme. My freshman year ERAU purchased a do zen or so new American Grumman Tigers. One week before the start of the fa ll semester a thunderstorm came through and dropped quite a bit of hail on the airplanes. The Cessnas fared pretty well but the Tigers did not do so well. They were left with a lot of dimples on the tops of the wings. Most of them were still safe to fly and actually got much higher climb rates af ter that. Insurance kicked in and the aircraft were cycled one at a time b ack to the factory to get the wings re-skinned. It did have a bit of an ef fect on aircraft scheduling, but not as much as this will. If you have or know of an aircraft that might not get much use over the next few months please conta ct them.=0A=0A-------------=0A=0AEmbry Riddle flight department devastated by tornado=0A =0ASchool looking for replacement aircraft to lease=0A =0AWhi le most EAA members were celebrating the Christmas holiday on Monday,=0Athe staff at Embry Riddle Aeronautical University in Daytona Beach,=0AFla., wa s dealing with the aftermath of a tornado that ripped through=0Athe campus that day. More than 50 ERAU aircraft were destroyed or=0Adamaged by the to rnado, while nine campus buildings were also hit. The=0Adamage caused univ ersity officials to delay the start of classes for one=0Aweek following the holiday recess, with the spring semester now starting=0Aon Jan. 16.=0A =0A EAA immediately offered assistance to Embry Riddle in the aftermath of=0Ath e storm, and the university has asked EAA for possible assistance from=0Ait s members. The university is now looking to leaseback, or rent by the=0Afl ight hour, several late-model Cessna 172s (180-horsepower G 1000 or=0Aconve ntional equipped aircraft) to replace those lost in the Dec. 25=0Atornado. The leases/or hourly rentals would last up to four months. The=0Aaircraft will be maintained to Embry Riddle exacting maintenance=0Astandards and ret urned to the owner/operator with either a fresh=0A100-hour or annual inspec tion. =0A =0AIf you can assist, please send an e-mail to Frank Ayers, Chair man of the=0AFlight Department (ayersf(at)erau.edu) or Jack Haun, Director of =0AMaintenance (haunj(at)erau.edu) to discuss lease/rental terms. Please=0Apro vide the N-number of the aircraft and a general description. =0A =0AFor mor e information, visit www.eaa.org=0A=0A=0A----- Original Message ----=0AFrom : "Fixitauto(at)aol.com" =0ATo: rv10-list(at)matronics.com=0AS ent: Thursday, December 28, 2006 12:58:28 PM=0ASubject: RV10-List: Fwd: Tor nadoes Damage Florida - AOL News=0A=0A=0A=0A =0A=0A =0ATornadoes Damage H undreds of Florida Homes - AOL News=0A=0A=0A =0A =0A=0A=0A=0A=0A <> =0A=0A=0A=0A=0A=0A=0A =0A=0A=0A=0A__________________________________________________=0ADo You Yah ttp://mail.yahoo.com ________________________________________________________________________________
Date: Dec 28, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: Surface Corrosion?
Hi Again I spoke to Ken at Van's who suggested I clean the filiform corrosion using a scotchbright pad. After some serious scouring, I got it off with the pad. That being said, I was most unhappy with the result as I was almost certainly well into the substrate and removed the ALCLAD layer. As a result I am concerned that it may lead to greater problems in the future especially if my priming is compromised during assembly. Van's was quite happy to send out a replacement. As this is part of the forward tail cone bulkhead, this won't have too big an impact on my build schedule. Cheers Les RV10 #40643 - Lost in the empennage -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John W. Cox Sent: Thursday, December 28, 2006 3:52 PM Subject: RE: RV10-List: Surface Corrosion? Les, that's an Excellent read of all eleven (11) web pages. This is what I play with every night while other builder's sleep. It brings clarity to the issues of alodine, anodize and proper surface preparation including final topcoat application without a "declaration of war". The final corrective solution often involves Eddy Current, Ultra-sound or X-ray (all expensive diagnostics) and drives home the value of prevention rather than intervention due to poor preparation during initial construction. John Cox _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Les Kearney Sent: Thursday, December 28, 2006 8:25 AM Subject: RE: RV10-List: Surface Corrosion? Ooops I forgot to attach the link. It is: http://aluminium.matter.org.uk/content/html/eng/default.asp?catid=180 <http://aluminium.matter.org.uk/content/html/eng/default.asp?catid=180& pagei d=2144416691> &pageid=2144416691 Cheers Les ________________________________________________________________________________
From: "ddddsp1(at)juno.com" <ddddsp1(at)juno.com>
Date: Dec 29, 2006
Subject: Looking for 24 or 28 AWG tefzel
Where can I get some 24 AWG or 28 AWG tefzel wire. Need about 40 - 50 f eet. Thanks, DEAN ________________________________________________________________________ FREE for 30 Days! - Holiday eCards from AmericanGreetings.com http://track.juno.com/s/lc?s=197335&u=http://www.americangreetings.c om/index.pd?c=uol5637

Where can I get some 24 AWG or 28 AWG tefzel wire.  N eed about 40 - 50 feet. 

Thanks,

DEAN



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Date: Dec 29, 2006
From: Rodger Todd <rj_todd(at)yahoo.co.uk>
Subject: Re: D2A
I am wondering how many others are in the same situation I find myself if indeed D2A have stopped trading? I took advantage of their Sun n' Fun offer (SV-10 plus either FreeFlight GPS or Trutrak Digitrak 2 VSVG a/p head) and ordered the SV-10 with the Trutrak autopilot head - my intention being to upgrade to a Sorcerer. The system was due for delivery on the 28th of August. This date was of course not met - production hold ups - although eventually the system plus wiring loom was sent to my dealer. D2A later supplied a FreeFlight GPS receiver even though they were aware I wanted the a/p. I'm not sure if my dealer has returned this but I am in the fortunate position of not having either the autopilot or the Pinpoint GADHRS all of which, of course, I have paid in full for. When the wrong offer equipment was sent, my dealer tried to contact D2A to which they never replied. Interestingly, the customer agent for him at D2A had just left the company. I live in remote NW Australia so legal redress, if at all possible, will be exceptionally difficult for me to organise. So yes, at least one customer is likely to be finacially very disadvantaged and is awaiting confirmation of where to next with great interest. Despite this sad tale, Season's Greetings to all, Rodger --- David McNeill wrote: > check this > > http://www.xbow.com/Support/Support_pdf_files/Service_Letter_NAV425-06-02.pdf > > http://www.xbow.com/General_info/Info_pdf_files/AHRS425_Upgrade_Program.pdf > > http://www.xbow.com/General_info/Info_pdf_files/D2A_Press_Release.pdf > > > Send instant messages to your online friends http://uk.messenger.yahoo.com ________________________________________________________________________________
From: "Byron Gillespie" <bgill1(at)charter.net>
Subject: D2A
Date: Dec 29, 2006
There are apparently several of us in the same situation. I too "took advantage" of the Sun n' Fun special. I'll have to find out from Stein next week, exactly what I have on hand and just how bad my situation is.. I'll continue to try and patiently await the info as it becomes available and try and hope for a satisfactory outcome. Byron #40253 Firewall forward (Avionics in question) -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rodger Todd Sent: Friday, December 29, 2006 7:28 AM Subject: Re: RV10-List: D2A I am wondering how many others are in the same situation I find myself if indeed D2A have stopped trading? I took advantage of their Sun n' Fun offer (SV-10 plus either FreeFlight GPS or Trutrak Digitrak 2 VSVG a/p head) and ordered the SV-10 with the Trutrak autopilot head - my intention being to upgrade to a Sorcerer. The system was due for delivery on the 28th of August. This date was of course not met - production hold ups ............ ________________________________________________________________________________
Date: Dec 29, 2006
From: Jay Brinkmeyer <jaybrinkmeyer(at)yahoo.com>
Subject: Surface Corrosion?
The solution is to simply remove all of the plastic up front... Parts can't be properly dimpled, riveted, or deburred with plastic in the way. In addition, if you are planning to paint you'll end up buffing/sanding/scotch-briting every inch of the surface anyway. So add lots of hours to an already long project by oh-so-carefully removing plastic in nice straight lines? If the corrosion is minor, just buff it out and move on. I had a few (one or two) parts that also had this look and simply took a scotchbrite pad to it and the primer did stick. No big deal as there are lots of other way harder things to worry about. Cheers, Jay Fuse panel ribs From: "Bob Leffler" <rvmail(at)thelefflers.com> Subject: Surface Corrosion? Les's issue with corrosion reminded me of a topic I wanted to solicit opinions from the list. I attended a RV builder's class a couple weeks ago at Grov-Air in Indy. Troy Grover, the gentleman conducting the class stated that he has seen several RVs that have significant corrosion along the lines were the vinyl wrap was removed by a soldering iron. His conclusion was that dirt was collecting in the edge of the vinyl and absorbing moisture. He stated that he's seen this in the last couple kits that have come through his shop. Since my empennage kit is in route at the moment, I am thinking about the approach I want to take. My current desire is to leave the vinyl on as long as possible to minimize scratching. Does anyone know of anyone that has experienced corrosion along the lines of the vinyl that were cut with a soldering iron? It seems like the only way to prevent the issue that Les has discovered is to remove the vinyl when you inventory, but I would think would have disastrous effect of the quality of the surface. I am very interested in hearing on how Van's handles Les's issue. I am optimistic that they will replace the part for Les. __________________________________________________ ________________________________________________________________________________
Subject: Re: Work Table Size
From: "johngoodman" <johngoodman(at)earthlink.net>
Date: Dec 29, 2006
rvbuilder(at)sausen.net wrote: > I'm curious. Is there a reason that everyone is using copper and other metal pipe for their air runs? Good ole SCH 40 PVC from just about any hardware store is rated for several times the PSI you will ever see from your compressor. Use half inch PVC and you will be done in half the time at a fraction of the cost. > > Michael > > -- PVC is a no-no. If it ever fails, it will shatter; think of glass. Metal will only rupture. When I was planning my system, I happened to be in a military shop and asked one of the guys about their air system. He happened to be the safety guy and he gave me the whole speech. His recommendation was black iron pipe. There was a reason for not using galvanized but I've forgotten why. John -------- #40572 Empennage - Starting tailcone. N711JG reserved Read this topic online here: http://forums.matronics.com/viewtopic.php?p=84212#84212 ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: ELT?
Date: Dec 29, 2006
A quick question for those in the know. Is there electrical wiring that goes to the ELT to maintain a charge on the ELT's battery or is there simply the internal battery in the unit which it runs off off in mishap? Thanks, John G. ________________________________________________________________________________
Date: Dec 29, 2006
From: Les Kearney <kearney(at)shaw.ca>
Subject: ELT?
John My ELT (in my Cherokee) has an internal battery that is replaced on a scheduled basis. The ELT is also recertified every year. There is no external power source to it. Cheers Les Kearney RV10 # 40643 - Lost in the empennage -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Gonzalez Sent: Friday, December 29, 2006 12:29 PM Subject: RV10-List: ELT? A quick question for those in the know. Is there electrical wiring that goes to the ELT to maintain a charge on the ELT's battery or is there simply the internal battery in the unit which it runs off off in mishap? Thanks, John G. ________________________________________________________________________________
Date: Dec 29, 2006
From: Rick <ricksked(at)earthlink.net>
Subject: Re: ELT?
John, My 450 only has "D" batteries and basically a "phone cord" that runs from the ELT to the panel mounted switch. Only other connector is the antenna lead. Rick S. 40185 ________________________________________________________________________________
Date: Dec 29, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: ELT?
I am using the AmeriKing ELT (AK-450). It requires no power wiring. It is powered by the D size alkaline batteries. It does require a coax cable to the antenna (that I will mount in under the far rear tail fairing) and a RJ11 wire (phone wire and jacks) that goes from the ELT (mounted near the battery) to the remote display (mounted in the panel). Here is a link to the installation manual <http://www.ameri-king.com/pdf/9.1.22.pdf> Larry Rosen #356 John Gonzalez wrote: > > A quick question for those in the know. > > Is there electrical wiring that goes to the ELT to maintain a charge > on the ELT's battery or is there simply the internal battery in the > unit which it runs off off in mishap? > > Thanks, > > John G. > > ________________________________________________________________________________
Subject: California Breakfast
Date: Dec 29, 2006
From: "Scott Schmidt" <sschmidt(at)ussynthetic.com>
I know this is short notice but I was wondering if any of you had a recommendation for a good fly-in breakfast. I flew down to Redlands Muni today and wanted to take my brother and sister-in-law for breakfast somewhere tomorrow (Saturday) morning. I know there are a few resturants around but is there one that is better than the other? Thanks in advance -Scott Schmidt N104XP ________________________________________________________________________________
Date: Dec 29, 2006
From: rv10builder <rv10builder(at)bellsouth.net>
Subject: Re: ELT?
While we're on the subject, is there any real compelling reason to install a 406Mhz ELT (other than the obvious COSPAS-SARSAT discontinued service in 02/09?). I don't recall ever hearing of a GA aircraft being located with the assistance of satellites, and I'm not clear if this is a mandate. One other question...is one mfg. of ELT considered "trash" whereas another as "treasure"? Brian #40308 John Gonzalez wrote: > > A quick question for those in the know. > > Is there electrical wiring that goes to the ELT to maintain a charge > on the ELT's battery or is there simply the internal battery in the > unit which it runs off off in mishap? > > Thanks, > > John G. > > > . > ________________________________________________________________________________
From: "Dave Saylor" <Dave(at)AirCraftersLLC.com>
Subject: Cowling Mod Photos
Date: Dec 29, 2006
We just finished a mod I really like. Here is our big oil door. It takes about 30 seconds to open, a lot longer than a single latch but I like being able to see so much on preflight. Still have to seal the hinge forward of the baffle...any suggestions? Dave Saylor AirCrafters LLC 140 Aviation Way Watsonville, CA 831-722-9141 831-750-0284 CL www.AirCraftersLLC.com ________________________________________________________________________________
Date: Dec 30, 2006
From: Niko <owl40188(at)yahoo.com>
Subject: Cowl Shim Thickness
The cowl shim thikness specified in the instructions is 0.020in. The stock in the trim bundle that I got is 0.025in. In fact I have nothing thats 0. 020 in thick. Can someone verify the correct cowl shim thickness?=0A=0ATha nks=0A=0ANiko=0A40188 ________________________________________________________________________________
Date: Dec 30, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: Cowl Shim Thickness
Many have used the 0.025 shim successfully. There is no .020 shim included in the kit. Larry #356 Niko wrote: > The cowl shim thikness specified in the instructions is 0.020in. The > stock in the trim bundle that I got is 0.025in. In fact I have > nothing thats 0.020 in thick. Can someone verify the correct cowl > shim thickness? > > Thanks > > Niko > 40188 > * > > > * ________________________________________________________________________________
Date: Dec 30, 2006
From: <ibspud(at)adelphia.net>
Subject: RV10 Builders in SLC
I'm passing through SLC today and wonder if there are any builders available today. I can't remember the map address that shows the location of people accross the country either. Can anyone help? Albert Gardner Yuma, AZ ________________________________________________________________________________
Date: Dec 30, 2006
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: RV10 Builders in SLC
Al, I believe there are several builders in the SLC area, Scott Schmidt, Mike Howe, Jeff Dalton, and others I'm sure, here's the Frapper Map link http://www.frappr.com/rv10snorthamerica Deems Davis # 406 Finishing - ( A Misnomer ! ) http://deemsrv10.com/ ________________________________________________________________________________
Date: Dec 30, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: RV10 Builders in SLC
<http://www.frappr.com/rv10snorthamerica> for the RV10 google frappr. ibspud(at)adelphia.net wrote: > > I'm passing through SLC today and wonder if there are any builders available today. I can't remember the map address that shows the location of people accross the country either. Can anyone help? > Albert Gardner > Yuma, AZ > > > ________________________________________________________________________________
Date: Dec 30, 2006
From: <ibspud(at)adelphia.net>
Subject: Re: RV10 Builders in SLC
Thanks Deems. I'mabout to start my doors and looking for a project at about that stage. Albert ---- Deems Davis wrote: > > Al, I believe there are several builders in the SLC area, Scott Schmidt, > Mike Howe, Jeff Dalton, and others I'm sure, here's the Frapper Map > link http://www.frappr.com/rv10snorthamerica > > Deems Davis # 406 > Finishing - ( A Misnomer ! ) > http://deemsrv10.com/ > > > > > > ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Strobe wiring.
Date: Dec 30, 2006
To many this could sound like a stupid question. I am trying to finish up most of my wiring before I permanently attach the baggage floors. What I was trying to do was to have all my strobe wire bundles, both the right wing and the left wing bundles run down the same side of my fuselage. I've chosen the left side for them to go back to the battery compartment. Question: I realize the strobe wire bundle will be eminating out of each wing root aft of the main spar and infront of the rear spar attatchment connector. Can the strobe wire bundle go from this aft location forward to infront of the main spar(is there a any room in the large diameter hole that is in the main spar which eminates out of the wing root) or is this hole's space taken up with the control mechanism for the ailerons? Yes we have gone over the ideas of gasoline and electrical runs. I was going to keep all connectors away from fumes and gasoline. OR Should I simply put a hole in the fuselage skin, (obviously inside the wing root fairing area) aft of the main spar and infront of the rear spar connector? Then run the right wing wire bundle up and then across beneath the seats over to the left side and back to the battery compartment. I guess I was trying to not drill any holes in the fuselage skin, but I bet the two existing holes that Van's has in the fuselage infront of the main spar will be filled completely with aileron pushrods and fuel lines going out of the tanks and return lines going back to the tank. Thanks ahead of time. JOhn G. ________________________________________________________________________________
Date: Dec 30, 2006
From: Darton Steve <sfdarton(at)yahoo.com>
Subject: Re: RV10 Builders in SLC
I'm a "Salt Laker" so is Scott Schmidt and Mike Howe. You can call me at 801-971-1009. Steve Darton 40212 --- Larry Rosen wrote: > > > <http://www.frappr.com/rv10snorthamerica> for the > RV10 google frappr. > > ibspud(at)adelphia.net wrote: > > > > > I'm passing through SLC today and wonder if there > are any builders available today. I can't remember > the map address that shows the location of people > accross the country either. Can anyone help? > > Albert Gardner > > Yuma, AZ > > > > > > > > > > > > > > > > > browse > Subscriptions page, > FAQ, > http://www.matronics.com/Navigator?RV10-List > > Web Forums! > > > > > __________________________________________________ ________________________________________________________________________________
From: "Jesse Saint" <jesse(at)itecusa.org>
Subject: Strobe wiring.
Date: Dec 30, 2006
Unless I am mistaken, the skins have a pilot hole in them that you are supposed to drill out for wiring runs aft of the spar. That is where we do all of our wiring. Then I would recommend running the wire that crosses the fuse in the area where the flap control rod runs, drilling a small hole in each panel and putting a snap bushing in them. That is also a good way to get the flap wires from the side to the flap motor while keeping them as far from the bellcranks and controls as possible. Another place is to run them across the fuse between the two center sections, which is a place where there is nothing moving except the pushrods right in the center, but it is easy to keep the wires away from that. The wires can be supported on the spacers that go on the long AN3 bolts that hold the main gear supports to both the front and the back center section. Jesse Saint I-TEC, Inc. jesse(at)itecusa.org www.itecusa.org Cell: 352-427-0285 Fax: 815-377-3694 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Gonzalez Sent: Saturday, December 30, 2006 3:20 PM Subject: RV10-List: Strobe wiring. To many this could sound like a stupid question. I am trying to finish up most of my wiring before I permanently attach the baggage floors. What I was trying to do was to have all my strobe wire bundles, both the right wing and the left wing bundles run down the same side of my fuselage. I've chosen the left side for them to go back to the battery compartment. Question: I realize the strobe wire bundle will be eminating out of each wing root aft of the main spar and infront of the rear spar attatchment connector. Can the strobe wire bundle go from this aft location forward to infront of the main spar(is there a any room in the large diameter hole that is in the main spar which eminates out of the wing root) or is this hole's space taken up with the control mechanism for the ailerons? Yes we have gone over the ideas of gasoline and electrical runs. I was going to keep all connectors away from fumes and gasoline. OR Should I simply put a hole in the fuselage skin, (obviously inside the wing root fairing area) aft of the main spar and infront of the rear spar connector? Then run the right wing wire bundle up and then across beneath the seats over to the left side and back to the battery compartment. I guess I was trying to not drill any holes in the fuselage skin, but I bet the two existing holes that Van's has in the fuselage infront of the main spar will be filled completely with aileron pushrods and fuel lines going out of the tanks and return lines going back to the tank. Thanks ahead of time. JOhn G. -- 4:48 PM ________________________________________________________________________________
From: "Rene" <rene(at)felker.com>
Subject: RV10 Builders in SLC
Date: Dec 30, 2006
Sorry for the late response, just got back to the list. I am building up in Ogden. I am somewhere in finish stage........ Phone number is below. I have a hanger at KOGD..... Rene' 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of ibspud(at)adelphia.net Sent: Saturday, December 30, 2006 9:04 AM Subject: RV10-List: RV10 Builders in SLC I'm passing through SLC today and wonder if there are any builders available today. I can't remember the map address that shows the location of people accross the country either. Can anyone help? Albert Gardner Yuma, AZ ________________________________________________________________________________
From: "John Gonzalez" <indigoonlatigo(at)msn.com>
Subject: Strobe wiring.
Date: Dec 30, 2006
Thanks Jesse I used the center section of the spar in the fuse to cross over. I didn't see any pilot hole in the fuse side so I measures the bushing on the wing root and transferred that to the fuse. Sometimes I have to get over the idea that Van's doesn't always tell you where to drill and sometimes they don't mark it out for you. Got to get over the fear of cutting virgin metal. Thanks for responding. John >From: "Jesse Saint" <jesse(at)itecusa.org> >Reply-To: rv10-list(at)matronics.com >To: >Subject: RE: RV10-List: Strobe wiring. >Date: Sat, 30 Dec 2006 19:37:10 -0500 > > >Unless I am mistaken, the skins have a pilot hole in them that you are >supposed to drill out for wiring runs aft of the spar. That is where we do >all of our wiring. Then I would recommend running the wire that crosses >the >fuse in the area where the flap control rod runs, drilling a small hole in >each panel and putting a snap bushing in them. That is also a good way to >get the flap wires from the side to the flap motor while keeping them as >far >from the bellcranks and controls as possible. Another place is to run them >across the fuse between the two center sections, which is a place where >there is nothing moving except the pushrods right in the center, but it is >easy to keep the wires away from that. The wires can be supported on the >spacers that go on the long AN3 bolts that hold the main gear supports to >both the front and the back center section. > >Jesse Saint >I-TEC, Inc. >jesse(at)itecusa.org >www.itecusa.org >Cell: 352-427-0285 >Fax: 815-377-3694 >-----Original Message----- >From: owner-rv10-list-server(at)matronics.com >[mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Gonzalez >Sent: Saturday, December 30, 2006 3:20 PM >To: rv10-list(at)matronics.com >Subject: RV10-List: Strobe wiring. > > >To many this could sound like a stupid question. > >I am trying to finish up most of my wiring before I permanently attach the >baggage floors. > >What I was trying to do was to have all my strobe wire bundles, both the >right wing and the left wing bundles run down the same side of my fuselage. >I've chosen the left side for them to go back to the battery compartment. > >Question: I realize the strobe wire bundle will be eminating out of each >wing root aft of the main spar and infront of the rear spar attatchment >connector. Can the strobe wire bundle go from this aft location forward to >infront of the main spar(is there a any room in the large diameter hole >that > >is in the main spar which eminates out of the wing root) or is this hole's >space taken up with the control mechanism for the ailerons? Yes we have >gone over the ideas of gasoline and electrical runs. I was going to keep >all > >connectors away from fumes and gasoline. > >OR > >Should I simply put a hole in the fuselage skin, (obviously inside the wing >root fairing area) aft of the main spar and infront of the rear spar >connector? Then run the right wing wire bundle up and then across beneath >the seats over to the left side and back to the battery compartment. > >I guess I was trying to not drill any holes in the fuselage skin, but I bet >the two existing holes that Van's has in the fuselage infront of the main >spar will be filled completely with aileron pushrods and fuel lines going >out of the tanks and return lines going back to the tank. > > >Thanks ahead of time. > >JOhn G. > > >-- >4:48 PM > > ________________________________________________________________________________
From: "Sean Blair" <seanblair(at)adelphia.net>
Subject: Floor rivets
Date: Dec 30, 2006
Is everyone using the 470 rivets on the side flanges of the back floor pans? The front ones use pop rivets, why the solid ones for the back? Is there a strength issue I'm not thinking about? Also, how do you get the most forward rivets that are in between the front seat bracket and tunnel where the floor pan angles up? Thanks, Sean Blair #40225 Freezing in Colorado..too much snow. ________________________________________________________________________________
From: "Dave & Brenda Emond" <d_emond(at)mweb.co.za>
Subject: Re: Fuel tank sender gasket
Date: Dec 31, 2006
I fitted my tank sender units to the tank using just the rubber gaskets, and a little automotive sealer on the screws. After filling the tanks with Avgas to check for leaks, within a week the Avgas has caused the rubber gaskets to deform and bulge, causing a major leak. I am contemplating doing what many other builders before me recommended, leave the gasket out and proseal the sender unit in place. I want to share this experience with all those that might be thinking along the same lines as I was. Dave Emond RV10 - #40159 ________________________________________________________________________________
Subject: RV10 Builders in SLC
Date: Dec 30, 2006
From: "Scott Schmidt" <sschmidt(at)ussynthetic.com>
Sorry, I'm out of town or else you could drop by the hanger. I am actually down in California with the RV-10 this weekend. Had an awesome flight down. Today we went to Flabob for breakfast and then flew the coast a little. I will be back tommorrow so if you are in the area on Sunday afternoon or Monday give me a call. We are heading to French Valley airport tomorrow morning for breakfast before flying home. I hope everyone has a great last day of 2006!!!!! I am at KBTF (Bountiful Skypark). 801-319-3094. -Scott Schmidt ________________________________ From: owner-rv10-list-server(at)matronics.com on behalf of Rene Sent: Sat 12/30/2006 6:38 PM Subject: RE: RV10-List: RV10 Builders in SLC Sorry for the late response, just got back to the list. I am building up in Ogden. I am somewhere in finish stage........ Phone number is below. I have a hanger at KOGD..... Rene' 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of ibspud(at)adelphia.net Sent: Saturday, December 30, 2006 9:04 AM Subject: RV10-List: RV10 Builders in SLC I'm passing through SLC today and wonder if there are any builders available today. I can't remember the map address that shows the location of people accross the country either. Can anyone help? Albert Gardner Yuma, AZ ________________________________________________________________________________
From: Richard Reynolds <rvreynolds(at)macs.net>
Subject: Re: Floor rivets
Date: Dec 31, 2006
i called Van's about this. It's a cost issue, AN470AD4-4 rivets are cheaper than LP4-3 pop rivets, $.0089 vs $.05. God forbid if you ever wanted to drill out the 470's. I used LP4-3 pop rivets. Richard Reynolds On Dec 30, 2006, at 10:37 PM, Sean Blair wrote: > Is everyone using the 470 rivets on the side flanges of the back > floor pans? The front ones use pop rivets, why the solid ones for > the back? Is there a strength issue I=92m not thinking about? Also, > how do you get the most forward rivets that are in between the > front seat bracket and tunnel where the floor pan angles up? > > > Thanks, > > Sean Blair > > #40225 > > > Freezing in Colorado=85.too much snow. > > List > ======================== > ======================== > ________________________________________________________________________________
Subject: Use of tank sealant
From: Michael D Chase <MChase(at)gdatp.com>
Date: Dec 31, 2006
Guys, I have a quick question I am ready to put the foam wedges in my elevators and was wondering if anyone used something other then tank sealant. I live in VT and it is hard to come by up here. I made the mistake of only ordering 1oz t o cover the rudder trailing edge ohps. If I do have to order how much do I n eed to finish the tail? Thanks. -------------------------- This e-mail message (including attachments, if any) is for the sole use of th e intended recipient(s) and may contain information that is private, confiden tial, or exempt from disclosure. Any unauthorized review, use, copying, prin ting, disclosure, retention, or distribution is strictly prohibited. If you are not the intended recipient, please contact the sender by reply to this e- mail, and delete all copies without disclosing this message to others. Thank you. ----- Original Message ----- From: owner-rv10-list-server Sent: 12/23/2006 01:53 AM Subject: RV10-List: trim tab problem. Yeah, I've noticed your number. You may pass me up at some point, I got my e mp kit a year ago and just finished the tail cone. The problem I had with my trim tab is that I drilled the hinge holes wrong an d caused a curve or hook in the hinge. This caused the hinge to bind and the tab to twist. The hinge is very flimsy before it is mounted and can flex ea sily. My left tab has the same problem but ever so slight I don't think I wi ll rebuild it at this point. And if I do, I will only need to replace the hi nge. At first I didn't realize the real problem. I drilled out the hinge rivets o n the tab and thought I could just clamp the tab flat, re-align the hinge and re-rivet. While re-riveting, I bent the hinge slightly with the squeezer an d then trying to remove the bend I put an ugly dent in the top of the tab ski n. I then discovered the real problem of drilling the holes wrong on the ele vator side, which transferred the curve to the tab side. I could have just r eplaced the hinge, but I could not accept that dent. So, after an hour of fr ustrated thought on how to save the part, I succumbed and ordered new parts t o rebuild the whole tab. My son asked if he could have the the old tab and h ung it in his room. He thinks it's cool. I guess that's the priceless stuff. The way to line up those hinges is to draw a rivet line on the hinge, then pu t that line in the center of the rivet holes and drill. Don't rely on the st raightness of the hinge as I did, it flexes as you drill. Keep that rivet li ne centered in the holes and cleco as you go. The old learning curve again, seems so simple now! Dave Leikam 40496 emp assembly ----- Original Message ----- From: LIKE2LOOP(at)aol.com To: DAVELEIKAM(at)wi.rr.com Sent: Friday, December 22, 2006 4:53 PM Subject: Re: Van's shipping department, where did everyone go?? In a message dated 12/22/06 5:06:23 P.M. Eastern Standard Time, DAVELEIKAM@ wi.rr.com writes: I ordered parts for a new right trim tab on 12/20. Tell me more... i am ready to bend the end tabs on both trim tabs tomorro w.... how did you loose the right one? Thanks for sharing... i sent this direct to you , off list. We are almost RV-10 brothers... my kit is #40499. .. you are a few kits ahead of me..... Stephen Blank RV-10 Builder #40499 / C-170B flyer 766 SE River Lane Port St. Lucie, FL 34983 772-475-5556 cell ________________________________________________________________________________
Date: Dec 31, 2006
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: Use of tank sealant
I used RTV. Larry #356 Michael D Chase wrote: > > Guys, > I have a quick question I am ready to put the foam wedges in my > elevators and was wondering if anyone used something other then tank > sealant. I live in VT and it is hard to come by up here. I made the > mistake of only ordering 1oz to cover the rudder trailing edge ohps. > If I do have to order how much do I need to finish the taileless Handheld > > > This e-mail message (including attachments, if any) is for the sole > use of the intended recipient(s) and may contain information that is > private, confidential, or exempt from disclosure. Any unauthorized > review, use, copying, printing, disclosure, retention, or distribution > is strictly prohibited. If you are not the intended recipient, please > contact the sender by reply to this e-mail, and delete all copies > without disclosing this message to others. Thank you. > > ------------------------------------------------------------------------ > > ----- Original Message ----- > * From: *owner-rv10-list-server > * Sent: *12/23/2006 01:53 AM > * To: * > * Subject: *RV10-List: trim tab problem. > > > Yeah, I've noticed your number. You may pass = me up at some > point, I got my emp kit a year ago and just finished the tail = cone. > > The problem I had with my trim tab is that I drilled = the hinge > holes wrong and caused a curve or hook in the hinge. This caused = > the hinge to bind and the tab to twist. The hinge is very flimsy > before it = is mounted and can flex easily. My left tab has the > same problem = but ever so slight I don't think I will rebuild it > at this point. And = if I do, I will only need to replace the hinge. > > At first I didn't realize the real problem. I = drilled out the > hinge rivets on the tab and thought I could just clamp the = tab > flat, re-align the hinge and re-rivet. While re-riveting, I = bent > the hinge slightly with the squeezer and then trying to remove the > bend I = put an ugly dent in the top of the tab skin. I > then discovered = the real problem of drilling the holes wrong on > the elevator side, = which transferred the curve to the tab side. > I could have just replaced the hinge, = but I could not accept that > dent. So, after an hour of frustrated = thought on how to save the > part, I succumbed and ordered new parts to rebuild the whole = tab. > My son asked if he could have the the old tab and hung = it in his > room. He thinks it's cool. I guess that's the priceless stuff. > > The way to line up those hinges is to draw a rivet = line on the > hinge, then put that line in the center of the rivet holes and = > drill. Don't rely on the straightness of the hinge as I did, it > flexes as you drill. Keep that rivet line centered in the holes > and cleco as you = go. The old learning curve again, seems so simple > = now! > > Dave Leikam > 40496 > emp assembly > > ----- Original Message ----- > *From:* LIKE2LOOP(at)aol.com <3D%22mailto:LIKE2LOOP(at)aol.com%22> > *To:* DAVELEIKAM(at)wi.rr.com <3D%22mailto:DAVELEIKAM(at)wi.rr.com%22> > *Sent:* Friday, December 22, 2006 = 4:53 PM > *Subject:* Re: Van's shipping = department, where did everyone go?? > > In a message dated 12/22/06 5:06:23 P.M. Eastern = Standard > Time, DAVELEIKAM(at)wi.rr.com <3D%22mailto:DAVELEIKAM(at)wi.rr.com%22> > writes: > /I ordered parts for a new right > trim tab on 12/20./ > > Tell me more... i am ready to bend the end tabs on both = trim > tabs tomorrow.... how did you loose the right one? = Thanks > for sharing... i sent this direct to you , off list. We are = almost > RV-10 brothers... my kit is #40499... you are a few kits ahead of > = me..... > > Stephen Blank RV-10 Builder #40499 / C-170B flyer > 766 SE River Lane > Port = St. Lucie, FL 34983 > > 772-475-5556 cell > * > > ============================================ > electric.com > om">www.buildersbooks.com > tlog.com > mebuilthelp.com > matronics.com/contribution > ============================================ > ://www.matronics.com/Navigator?RV10-List > ============================================ > > * > * > > > * ________________________________________________________________________________
Date: Dec 31, 2006
From: SamMarlow <sam.marlow(at)roadrunner.com>
Subject: Main Tires
I just realized it is going to be difficult to add air to the mains, does anyone have a better way than removing the wheel pants? Sam Marlow Wiring ________________________________________________________________________________
From: "Carl Froehlich" <carl.froehlich(at)cox.net>
Subject: Main Tires
Date: Dec 31, 2006
I use 4 Wal-Mart valve stem extensions connected end to end (the metal kind work better than the plastic ones). Each wheel pant has a spring loaded SS door (ACS item) that is lined up with the valve stem. I put a white mark on the tire so that it points down, visible below the bottom of the wheel pant when the valve stem is lined up with the door. Put the now long valve extension through the door and screw onto the tire valve stem. Make sure you take the valve stem extension out before moving the plane. Carl Froehlich RV-8A (290 hrs) RV-10 (wings) -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com]On Behalf Of SamMarlow Sent: Sunday, December 31, 2006 2:18 PM Subject: RV10-List: Main Tires I just realized it is going to be difficult to add air to the mains, does anyone have a better way than removing the wheel pants? Sam Marlow Wiring ________________________________________________________________________________
From: "Marcus Cooper" <coop85(at)bellsouth.net>
Subject: Main Tires
Date: Dec 31, 2006
Carl, Here's a link to the part I think you are using: http://www.aircraftspruce.com/catalog/hapages/accessdoors.php Is this the right thing? Thanks, Marcus - also looking for a better way to check tire pressure. -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Carl Froehlich Sent: Sunday, December 31, 2006 2:53 PM Subject: RE: RV10-List: Main Tires I use 4 Wal-Mart valve stem extensions connected end to end (the metal kind work better than the plastic ones). Each wheel pant has a spring loaded SS door (ACS item) that is lined up with the valve stem. I put a white mark on the tire so that it points down, visible below the bottom of the wheel pant when the valve stem is lined up with the door. Put the now long valve extension through the door and screw onto the tire valve stem. Make sure you take the valve stem extension out before moving the plane. Carl Froehlich RV-8A (290 hrs) RV-10 (wings) ________________________________________________________________________________
From: "Dick Gurley" <rngurley(at)mindspring.com>
Subject: Newbie question about scratches
Date: Dec 31, 2006
I am currently working on my horizontal stabilizer forward spar. When I pulled the blue plastic off of the spar, I found some handling damage scratches from =BD to 3 thousands (.003) deep. They run both with and across the gain. What is the best way to polish these out? Thanks Dick Gurley Empanage ________________________________________________________________________________
From: "jdalton77" <jdalton77(at)comcast.net>
Subject: Re: Newbie question about scratches
Date: Dec 31, 2006
Dick, I would wait. If they're really bad you may want to smooth and prime, but for the most part you'll have so many scratches by the time you're done that you'll have to scothbrite and prime anyway. Jeff ----- Original Message ----- From: Dick Gurley To: rv10-list(at)matronics.com Sent: Sunday, December 31, 2006 9:08 PM Subject: RV10-List: Newbie question about scratches I am currently working on my horizontal stabilizer forward spar. When I pulled the blue plastic off of the spar, I found some handling damage scratches from =BD to 3 thousands (.003) deep. They run both with and across the gain. What is the best way to polish these out? Thanks Dick Gurley Empanage ________________________________________________________________________________
Date: Dec 31, 2006
From: "Jim Beyer" <fehdxl(at)gmail.com>
Subject: Re: Newbie question about scratches
Dick, If you don't already have a 6" Scotch-brite deburring wheel mounted on a bench-grinder, then you really should. It would smooth out those tooling marks in no time at all. Don't be shocked at the $55 sticker price -- it's worth every penny! Here's a link to what I'm talking about. *http://tinyurl.com/y9z62w* Also, the 1" x 1" abrasives mounted to a die-grinder is, IMNSHO, the only way to de-bur inside edges such as lightening holes. Just go the the next page from the link above. In the mean time, some 400 (or higher) grit wet/dry sandpaper will smoothin g it out fine. -Jim P.S. I think the other guys thought you were talking about scratches on th e outside of a skin...yeah, there will be lots of those. Don't wory about them until painting. On 12/31/06, Dick Gurley wrote: > > I am currently working on my horizontal stabilizer forward spar. When I > pulled the blue plastic off of the spar, I found some handling damage > scratches from =BD to 3 thousands (.003) deep. They run both with and ac ross > the gain. What is the best way to polish these out? > > > Thanks > > > Dick Gurley > > Empanage > > * > =========== =========== =========== > > * > > -- o=\o ________________________________________________________________________________
Subject: Re: Main Tires
From: "Jim & Julie Wade" <jwade(at)msdeltawireless.com>
Date: Jan 01, 2007
buy no leak tubes from Desser tire company, then you only have to air the tires once or twice a year. Jim 40383 70 hrs of flying fun Read this topic online here: http://forums.matronics.com/viewtopic.php?p=84844#84844 ________________________________________________________________________________
Subject: Re: Is D2A out of business?
From: "Mike@Crossbow" <msmith(at)xbow.com>
Date: Jan 02, 2007
Crossbow has issued a press release in regards to the recent events at D2A and we have extended our upgrade program through June of 2007 in order to ensure that all of the existing customers in the field have a chance to receive an updated NAV425EX. As we have stated before and have documented in detail on our website, the NAV425EX initially had several bugs. These bugs were very difficult to replicate in house, however after some time we did identify the problem and have been offering updated versions free of charge to our customers. The NAV425EX and its variants continue to be sold to multiple EFIS manufacturers and we do not have any bugs or performance related problems with these units. We have a large number of these units in the field that are performing very well. Crossbow was the first company to build an FAA certified MEMS based AHRS and continues to be a leader in the AHRS market. If anyone currently has a NAV425EX that they would like to have updated, please contact us directly at 408-965-3300 or via email at techsupport(at)xbow.com. Please provide the serial number of your unit and a return shipping address. Crossbow will ensure that we update your unit in a timely manner. Please also note that we strongly suggest that all customers update their GPS antenna to an external mount GPS antenna as well as noted on our service bulletin. We have found that the Antcom 2G15A-XS-1 (www.antcom.com) is a high performance, cost effective solution for most installations. -------- Michael Smith Application Engineer Inertial Systems Crossbow Technology msmith(at)xbow.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=84973#84973 ________________________________________________________________________________
Subject: Re: [LML] D2 Update
From: "Mike@Crossbow" <msmith(at)xbow.com>
Date: Jan 02, 2007
There are a lot of posts on this topic already, however I'd like to refer any customers to some of the other posts to make sure that everyone has the right information. http://forums.matronics.com/viewtopic.php?t 828&highlight=d2a In regards to Brent's original email, I think there is a lot of misinformation here but we do not intend to get into a shouting match over this since this does not benefit the customers. I will however make some key points. 1) "If Xbow can fix their own EFIS why can't they fix the NAV42X". The NAV425EX originally had some bugs in the system, however we resolved those issues last April and have been updating units since. This unit has been continuosly sold to other EFIS manufacturers since then and has proven to be a high performanc and reliable AHRS. We offered these fixes to D2A, however they chose to take another path. Please also note that Crossbow does not currently sell an EFIS. 2) Crossbow has extended our upgrade program through June of 2007 and will be working very closely with the panel builders to ensure the satisfaction of our customers. Crossbow will always support our customers and will do everything in our power to ensure that they are taken care of. -------- Michael Smith Application Engineer Inertial Systems Crossbow Technology msmith(at)xbow.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=84976#84976 ________________________________________________________________________________
From: "Dave Hertner" <effectus(at)rogers.com>
Subject: New Design Brake Pedals and Stainless Brake Lines
Date: Jan 02, 2007
RV-10 Listers, I have just completed my newly designed Brake Pedals and Teflon-cored braided stainless steel brake line system. I am considering offering this package up for sale. Brake Pedals I designed the brake pedals to eliminate a problem a number of RV pilots have shared with me. When coming in for a landing with a crosswind it is very easy to be applying the brake simultaneously with moderate rudder inputs. This leads to higher tire wear due to the application of brake at touchdown. In extreme cases the aircraft could veer unexpectedly upon touchdown. My design allows room for your toe and provides a separate pedal tread for rudder only application. When you are applying rudder the brake pedal is depressed OFF. You simply move your foot upward, placing your toe on the upper tread and the heal of your foot on the lower tread to apply the brakes. The brake pedal chassis are constructed from stainless steel so that there will be no di-electric issues in an area that sees moisture. The tabs are TIG welded and the assembly is screwed together using stainless steel hardware. The pedal treads are high quality rubber units that come from an automotive supplier. I have designed these brake pedals to exactly fit in place of Van's pedals and they align at the top when the bottom of the rudder hoops are aligned at the bottom. 3 bolts out, 3 bolts in. All you have to do is place the appropriate washers for proper spacing. Teflon-cored Braided Stainless Steel Brake Line System I also developed an upgrade to the Plastic brake line system that Vans provides with the kit. I have replaced the entire brake line system from the reservoir to the Matco Parking brake interface with the aluminium lines on the firewall. In this installation I have inverted the Matco master cylinders. This allows for a much neater installation and less clutter between your feet. I developed this system for a couple of reasons. First, I heard that there were some leakage issues with the plastic lines as well as some sponginess over time that has been attributed to the rubber lined braided hoses that Van's supplies. Secondly, there is aesthetics. I couldn't get over the fact that I am building an aircraft valued over $200,000 that has the same brake lines that are supplied with many ultralight kits. The footwell looks much more professional and much less cluttered. There are 3 photos below showing the entire system installed in my RV-10. I anticipate that the brake pedals are going to sell for $175.00 for one side and $300.00 for both sides. I have yet to receive the total


December 16, 2006 - January 02, 2007

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