RV10-List Digest Archive

Mon 08/04/08


Total Messages Posted: 34



Today's Message Index:
----------------------
 
     1. 03:47 AM - Re: Flap alignment (Lew Gallagher)
     2. 04:08 AM -  MT Prop Governor Follow-up Report (Wayne Edgerton)
     3. 06:05 AM - Re: OSH gathering (Sam Marlow)
     4. 06:35 AM - Re: Re: Flap alignment (Rene Felker)
     5. 06:37 AM - Asymmetrical trim noted at OSH (Tim Olson)
     6. 07:15 AM - Re: Re: Leak Proofing the Fuel Sender (Kelly McMullen)
     7. 07:31 AM - Re: Flap alignment (Jesse Saint)
     8. 07:41 AM - Re: Asymmetrical trim noted at OSH (John Gonzalez)
     9. 08:04 AM - Re: OSH gathering (Don McDonald)
    10. 08:33 AM - Re: N104BS is painted! (Robin Marks)
    11. 08:41 AM - Re: Asymmetrical trim noted at OSH (John Cox)
    12. 08:51 AM - Re: Re: Leak Proofing the Fuel Sender (John Cox)
    13. 10:03 AM - Re: Asymmetrical trim noted at OSH (linn Walters)
    14. 10:46 AM - Re: Flap alignment (Scott Schmidt)
    15. 11:14 AM - Constructive Feedback was Asymmetrical trim noted at OSH (Les Kearney)
    16. 12:10 PM - Re: Constructive Feedback was Asymmetrical trim noted at OSH (linn Walters)
    17. 01:34 PM - Re: Constructive Feedback was Asymmetrical trim noted at OSH (Robert Wright)
    18. 02:31 PM - Re: Constructive Feedback was Asymmetrical trim noted at OSH (pascal)
    19. 02:47 PM - PIREP: Tungsten Bucking Bar (Douglas, Brian S)
    20. 03:02 PM - Re: Flap alignment (Lew Gallagher)
    21. 03:38 PM - Re: Constructive Feedback was Asymmetrical trim noted at OSH (Kelly McMullen)
    22. 04:15 PM - Re: Constructive Feedback was Asymmetrical trim noted at OSH (John Cox)
    23. 04:54 PM - Center console (Les Kearney)
    24. 05:39 PM - Re: Center console (Bob Leffler)
    25. 06:11 PM - Re: Center console (Les Kearney)
    26. 06:48 PM - SMA Diesel (Dawson-Townsend,Timothy)
    27. 07:22 PM - Re: SMA Diesel (John Cox)
    28. 08:25 PM - Re: Constructive Feedback was Asymmetrical trim noted at OSH (Tim Olson)
    29. 08:26 PM - Re: Re: Flap alignment (Tim Olson)
    30. 08:29 PM - Re: new prroducts (David McNeill)
    31. 09:06 PM - Re: SMA Diesel (Dave Leikam)
    32. 09:34 PM - Re: SMA Diesel (Kelly McMullen)
    33. 09:53 PM - OSH RV-10 Nose Wheel Pants & Fairing (Robin Marks)
    34. 10:00 PM - Las Vegas Area 10 Builders (John Cumins)
 
 
 


Message 1


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    Time: 03:47:25 AM PST US
    Subject: Re: Flap alignment
    From: "Lew Gallagher" <lewgall@charter.net>
    Thanks Rene', So -3 degrees it is? Just where in the heck do they tell you that?! And the "stops" are just when the leading edge of the flap bumps the spar? I think that leaves a fair amount of inaccuracy -- I like the -3 degrees better. It shouldn't be too hard to make a quick jig. This seems like a fairly critical setting and I'm surprised I couldn't find it addressed in the plans. We'll probably give Van's a call, but they're 3 hrs. behind us and we want to get this nailed so we can get the wings back off today. Later, - Lew -------- non-pilot crazy about building NOW OFICIALLY BUILDER #40549 Engine and FF here, now cowl and baffels,waiting on prop. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=196377#196377


    Message 2


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    Time: 04:08:00 AM PST US
    From: "Wayne Edgerton" <wayne.e@grandecom.net>
    Subject: MT Prop Governor Follow-up Report
    I have the same issue with the MT prop governor, it was surging 100 to 200rpm in cruise, and I pulled it off yesterday to send back to MT. A little bit of a hassle when you have the fairings installed. I asked them about exchange and I got the impression that they might be willing to do that but if you send them your current governor, when you receive it back and install it, it will be set at the same max RPM as when you removed it, so you don't have to do all of the adjustments that was required initially. Wayne Edgerton N602WT 175 hours


    Message 3


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    Time: 06:05:35 AM PST US
    From: Sam Marlow <sam@fr8dog.net>
    Subject: Re: OSH gathering
    I thought everything went great, the timing worked for me. I enjoyed putting faces with names! Thanks for a great cookout. Sam Marlow #40157 gary wrote: > > Just got back from OSH and while it is fresh on my and your minds, we would > like some feedback. > > We started serving around 6pm (or tried to) when we had the group > gatherings, it was suggested that later would be better for some. Comments? > > Are there other changes which would make things better next year? > > We have a surplus in the kitty again this year which will allow us to pick > up an extra camp site like we did this year, Thanks all of you. > > Any other comments? > > A special thanks to Michael Sausen for dropping off a mower for us to use > and for the carport tent and the large grill. These made life better for > all. > > Gary Specketer > > >


    Message 4


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    Time: 06:35:01 AM PST US
    From: "Rene Felker" <rene@felker.com>
    Subject: Re: Flap alignment
    The plans have you bringing the flap up to the stop. I do not remember if they ref 3 degrees or if I got that number form the list. Either way, I used my digital level to determine the 3 degrees. Measured the angle of the top skin and made sure flap was 3 degrees reflex. When I originally set the aileron and wing tip, I had the wings in the vertical stands and just pulled the flap up to the stop, clamped the flap and aileron together and then went to work on the wing tips. I am also using the flap positioning system, but you know I have not checked to see if the first stop is really 0 degrees, I think I may the next time I am at the hanger. Rene' Felker RV-10 N423CF Flying 801-721-6080 -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Lew Gallagher Sent: Monday, August 04, 2008 4:44 AM Subject: RV10-List: Re: Flap alignment Thanks Rene', So -3 degrees it is? Just where in the heck do they tell you that?! And the "stops" are just when the leading edge of the flap bumps the spar? I think that leaves a fair amount of inaccuracy -- I like the -3 degrees better. It shouldn't be too hard to make a quick jig. This seems like a fairly critical setting and I'm surprised I couldn't find it addressed in the plans. We'll probably give Van's a call, but they're 3 hrs. behind us and we want to get this nailed so we can get the wings back off today. Later, - Lew -------- non-pilot crazy about building NOW OFICIALLY BUILDER #40549 Engine and FF here, now cowl and baffels,waiting on prop. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=196377#196377


    Message 5


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    Time: 06:37:10 AM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Asymmetrical trim noted at OSH
    Was talking to another RV-10 pilot at OSH just before I left and he told me he peeked at some of the RV-10's that flew in and looked for asymmetrical trim tab deployment. As we've discussed in the past, the tabs should be both neutral at the same time, but when they go up, only one goes up (the other does move up a tiny amount), and when they go down, they both should go down. You should never have a situation where one goes up and one goes down. Having only one tab move up may sound crazy, but that's how it's supposed to work, and keep in mind that this isn't strange at all....many planes and even the other RV's are built with only one trim tab on one side. But, what makes our case unique is that if the builder screws up the rigging, they can end up with the 2 tabs in opposite deflections.....and if you follow the plans, you will likely have a small misalignment. These observations were not made by me, but were brought to my attention: So what was observed was that N921AC has some asymmetrical trim, then another unpainted RV-10 had a worse condition of asymmetrical trim. But the one that took the prize was one of the build-for-customer RV-10's that was at the show.... from what I was told, that RV-10 had one trim tab that was approx. 10 degrees up, while the other tab was approx. 10 deg down. NOW, the interesting thing was, the person also noticed that it appeared that this particular RV-10 may have had a little compression deformity of that rear bulkhead noted in the SB. Perhaps next year at OSH we should have a gathering to specifically look at some noted areas of every RV-10 and self-group-check for any potential safety issues? This year I just looked at all the pretty planes. Pretty good turnout overall. -- Tim Olson - RV-10 N104CD - Flying do not archive


    Message 6


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    Time: 07:15:40 AM PST US
    From: "Kelly McMullen" <apilot2@gmail.com>
    Subject: Re: Leak Proofing the Fuel Sender
    Same reason you don't use steel wool on aluminum. It can initiate corrosion. Yes, steel scrapers will scratch the aluminum and can generate all the issues of deep scratches. Phenolic scrapers, or scrap plexiglass ground into a scraper works pretty well. I don't disagree with Dan using what he did for that purpose(getting to skins apart), IF you recognize that close inspection will be required and you may have to scrap a piece if it gets too scratched. On way of reducing risk is to select stainless steel putty knife, to minimize the corrosion aspect. Of course John is giving you the airline point of view, where tanks frequently need attention, and costs are much higher, as are risks, along with the maximum level of regulation/oversight. Different standards, different needs...but the physics of steel and aluminum remain the same. On Sun, Aug 3, 2008 at 9:58 PM, John Ackerman <johnag5b@cableone.net> wrote: > > John, what is the reason given for no metallic scrapers? Crack initiation? > Accidental cuts and gouges? > What do you do if you need something very thin as Dan did (see below)? > John Ackerman 40458 > > > On Aug 3, 2008, at 5:25 PM, John Cox wrote: > >> >> Not to attract contrarian comments but the use of metallic scrapers on >> aluminum might be best avoided. We regularly complete such tasks with the >> use of MEK and plastic scrapers (and barrier gloves). Razor blades and putty >> knifes are a quick way to be pointed to the door on air carrier aircraft. >> Your family members deserve no less. >> >>> . Removing the side with the cork gasket was much easier, since the cork >>> is soft and a putty knife can be slipped in between the pieces and the cover >>> plate pried away and popped loose without much difficulty. The ProSeal only >>> side was quite a bit more difficult to break loose, ! >>> and required sliding a single edge razor blade between the bonded >>> surfaces most of the way around the circumference of the cover plate. >>> However, when it came loose it was somewhat easier to clean up using a >>> razor blade as a scraper combined with MEK. >>> >>> So the decision to use a gasket or not really comes down to ease of >>> future maintenance. Either way keeps the fuel in the tank. >>> >>> Hope this helps, >>> -Dan Masys >>> RV-10 N104LD back from OSH >>> RV-7A N747DL >


    Message 7


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    Time: 07:31:33 AM PST US
    From: Jesse Saint <jesse@saintaviation.com>
    Subject: Re: Flap alignment
    Lew, The best way I have seen to get the flaps correctly rigged is to have them installed on the plane and to raise them to the point that the bottom of the flap is flush with the bottom of the fuselage. Also, both flaps should reach this point at the same time. If it possible for one to reach this point early and put extra strain on the flap rod while the motor reaches full up. If this happens, when you drop the flaps the plane will want to roll because one flap will deploy more than the other. BTW, you will have to file down the end of the flap to remove any clearance issues with the side of the fuselage, and don't forget that there will be paint added, so leave a little room for paint, while not leaving a big gaping hole. The length on all of the pushrods can vary a little based on different components in the system. On the flaps, if you don't have them drilled and bolted with the exact dimensions as the plans call for, this can change the length of the pushrod. It's best to get it close and then install it and adjust for full retraction and deployment of the flaps and then snug up the jam nuts and mark which one is right and left for reinstallation after the wings go back on, unless (of course) you are rigging them with the final wing installation. Also something I have seen in the Aileron rigging. It is not uncommon, from what I have seen, to have the pushrod that connects to the aileron itself to have clearance issues with the aileron attach hinge when in full down. Make sure you don't have that issue when rigging. Jesse Saint Saint Aviation, Inc. jesse@saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Aug 3, 2008, at 9:47 PM, Lew Gallagher wrote: > > OK, we aligned the flaps, ailerons, wingtips today. Obviously > everything starts with the flaps in the raised position. But there > are adjustments on the flaps, so how do you know what the correct > raised position is? The instructions for length of the connecting > rods are a start, but how do you know when it's perfect? > > Not being a pilot, I just stuck a straight edge on the upper surface > of the wing and adjusted the flaps to be on that same plane to get > started. But now at home on the computer, I thought I'd better > check since I thought I remembered reading about slight up angle on > trailing edge for both ailerons for speed, etc. > > I've searched the archives and Tim's site, and sure enough, I found > a reference by Tim to a -3 degree in the up position of the flaps. > > Can someone confirm this for us? With the flaps/ailerons on the > same plane as the upper wing surface, I have both trailing ends of > the wingtips about 1/4 inch above the ailerons. I'm ready to > reshape the wingtip ends tomorrow, but they would be close to being > right if there is "up" built into the flap/aileron position. > > The wingtips are also slightly less than 1/4 inch too short -- as > opposed to the early ones that were too long. Is that a problem? > It wouldn't take much to add resin/flox to lengthen them a bit. > Heck, everything else is coming together so fine, I might as well > make that right too -- I just need to know what "right" is! > > Later, - Lew > > -------- > non-pilot > crazy about building > NOW OFICIALLY BUILDER #40549 > Engine and FF here, now cowl and baffels,waiting on prop. > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=196346#196346 > >


    Message 8


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    Time: 07:41:25 AM PST US
    From: John Gonzalez <indigoonlatigo@msn.com>
    Subject: Asymmetrical trim noted at OSH
    Did anyone get the tail number of the unpainter 10 with the compression mar ks near the bulkhead so that the owner could be informed of what was happen ing in case they are not aware of it on their own or not on this list? John G. > Date: Mon=2C 4 Aug 2008 08:34:22 -0500> From: Tim@MyRV10.com> To: rv10-list@matronics.com> Subject: RV10-List: Asymmetrical trim noted at OS king to another RV-10 pilot at OSH just before I left and> he told me he pe eked at some of the RV-10's that flew in and looked> for asymmetrical trim tab deployment. As we've discussed in> the past=2C the tabs should be both neutral at the same time=2C but> when they go up=2C only one goes up (the o ther does move up a> tiny amount)=2C and when they go down=2C they both sho uld go down.> You should never have a situation where one goes up and one> goes down.> > Having only one tab move up may sound crazy=2C but that's how > it's supposed to work=2C and keep in mind that this isn't> strange at all ....many planes and even the other RV's> are built with only one trim tab o n one side. But=2C what makes> our case unique is that if the builder screw s up the rigging=2C> they can end up with the 2 tabs in opposite deflection s.....and> if you follow the plans=2C you will likely have a small misalign ment.> > These observations were not made by me=2C but were brought> to my attention:> So what was observed was that N921AC has some asymmetrical trim =2C> then another unpainted RV-10 had a worse condition of> asymmetrical tr im. But the one that took the prize was one> of the build-for-customer RV-1 0's that was at the show....> from what I was told=2C that RV-10 had one tr im tab that was> approx. 10 degrees up=2C while the other tab was approx. 1 0 deg> down. NOW=2C the interesting thing was=2C the person also> noticed t hat it appeared that this particular RV-10 may> have had a little compressi on deformity of that rear> bulkhead noted in the SB.> > Perhaps next year a t OSH we should have a gathering to> specifically look at some noted areas of every RV-10> and self-group-check for any potential safety issues?> This year I just looked at all the pretty planes.> Pretty good turnout overall. ========================> > >


    Message 9


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    Time: 08:04:57 AM PST US
    From: Don McDonald <building_partner@yahoo.com>
    Subject: Re: OSH gathering
    Unfortunately, we were unable to get by and see you guys.- We did manage to drive through on Sunday, but couldn't remember the-location.... that b eing said, how about a nice large flag with RV 10 HHQ on it?--Did manag e to go to Van's dinner, but there were simply tooooo many-RV'ers there t o actually find anybody..... we were a couple of months from having the 10 flying, so next year our 10 will be there. Don & Kim McDonald #40636- Finishing the Finishing-- --- On Sun, 8/3/08, gary <speckter@comcast.net> wrote: From: gary <speckter@comcast.net> Subject: RV10-List: OSH gathering <speckter@comcast.net> Just got back from OSH and while it is fresh on my and your minds, we would like some feedback. We started serving around 6pm (or tried to) when we had the group gatherings, it was suggested that later would be better for some. Comments ? Are there other changes which would make things better next year? We have a surplus in the kitty again this year which will allow us to pick up an extra camp site like we did this year, Thanks all of you. Any other comments? A special thanks to Michael Sausen for dropping off a mower for us to use and for the carport tent and the large grill. These made life better for all. Gary Specketer =0A=0A=0A


    Message 10


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    Time: 08:33:59 AM PST US
    Subject: N104BS is painted!
    From: "Robin Marks" <robin1@mrmoisture.com>
    Sharp paint scheme. I really like the wheel pants. Robin Do Not Archive -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of rv10builder Sent: Friday, August 01, 2008 3:44 PM Subject: RV10-List: N104BS is painted! Just brought home my airplane today from GLO Custom. I'm really happy with the quality of their work! Brian Sutherland Nashville, TN N104BS 59.5 hours (and no, I haven't completed the SB yet! >:o )


    Message 11


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    Time: 08:41:05 AM PST US
    Subject: Asymmetrical trim noted at OSH
    From: "John Cox" <johnwcox@pacificnw.com>
    I second the comment of a pretty good turn-out and a good group of product representation entries. Kelly would be a good candidate as one of those potential observers. Each plane should be able to OPT out of the review if desired. As an EAA Tech, I would be happy to assist the team. Keeping rates low is a result of frequent Pilot Proficiency and regular maintenance. Knowing what to look for, how to correct it and pending issues beginning to arise saves everyone a lot of money and a loss of friends. By Opting out we can avoid some of the non-productive criticism that does not advance safety "One Iota". I spent this year getting training on becoming a Warbird Judge and how the scoring system works at OSH. The plastic plane crowd has publically conceded that the pursuit of million dollar kits has given the bulk of the market to VANS and the RV-10 is becoming the pre-eminent X-Cntry cruiser. John Cox Do not Archive -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Tim Olson Sent: Monday, August 04, 2008 6:34 AM Subject: RV10-List: Asymmetrical trim noted at OSH Was talking to another RV-10 pilot at OSH just before I left and he told me he peeked at some of the RV-10's that flew in and looked for asymmetrical trim tab deployment. As we've discussed in the past, the tabs should be both neutral at the same time, but when they go up, only one goes up (the other does move up a tiny amount), and when they go down, they both should go down. You should never have a situation where one goes up and one goes down. Having only one tab move up may sound crazy, but that's how it's supposed to work, and keep in mind that this isn't strange at all....many planes and even the other RV's are built with only one trim tab on one side. But, what makes our case unique is that if the builder screws up the rigging, they can end up with the 2 tabs in opposite deflections.....and if you follow the plans, you will likely have a small misalignment. These observations were not made by me, but were brought to my attention: So what was observed was that N921AC has some asymmetrical trim, then another unpainted RV-10 had a worse condition of asymmetrical trim. But the one that took the prize was one of the build-for-customer RV-10's that was at the show.... from what I was told, that RV-10 had one trim tab that was approx. 10 degrees up, while the other tab was approx. 10 deg down. NOW, the interesting thing was, the person also noticed that it appeared that this particular RV-10 may have had a little compression deformity of that rear bulkhead noted in the SB. Perhaps next year at OSH we should have a gathering to specifically look at some noted areas of every RV-10 and self-group-check for any potential safety issues? This year I just looked at all the pretty planes. Pretty good turnout overall. -- Tim Olson - RV-10 N104CD - Flying do not archive


    Message 12


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    Time: 08:51:53 AM PST US
    Subject: Re: Leak Proofing the Fuel Sender
    From: "John Cox" <johnwcox@pacificnw.com>
    Let me add that we sneak Skin Knives into some applications (also a terminable offence). Blending of scratches requires a 10:1 or 15:1 taper (depending on the SRM = Structural Repair Manual). You all have written one to effect repairs, haven't you? it is amazing how deep a scratch goes when force is used. Remember that the Alclad pure coating is not very thick. Five percent on each side for a total of 10 percent coating. So 0.032" means 0.0016" on each surface. On the RV-12 using 0.020 skin it is even more critical. Just hand force used on a tool can permanently stretch the skin - forever. "Skin knives" and "thread taps" are two ways to get quickly busted. We use them, on the sly and with high degree of situational awareness and desire for job security. John - back to GRAVES tonight after two weeks with real aviators. -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Kelly McMullen Sent: Monday, August 04, 2008 7:13 AM Subject: Re: RV10-List: Re: Leak Proofing the Fuel Sender Same reason you don't use steel wool on aluminum. It can initiate corrosion. Yes, steel scrapers will scratch the aluminum and can generate all the issues of deep scratches. Phenolic scrapers, or scrap plexiglass ground into a scraper works pretty well. I don't disagree with Dan using what he did for that purpose(getting to skins apart), IF you recognize that close inspection will be required and you may have to scrap a piece if it gets too scratched. On way of reducing risk is to select stainless steel putty knife, to minimize the corrosion aspect. Of course John is giving you the airline point of view, where tanks frequently need attention, and costs are much higher, as are risks, along with the maximum level of regulation/oversight. Different standards, different needs...but the physics of steel and aluminum remain the same. On Sun, Aug 3, 2008 at 9:58 PM, John Ackerman <johnag5b@cableone.net> wrote: > > John, what is the reason given for no metallic scrapers? Crack initiation? > Accidental cuts and gouges? > What do you do if you need something very thin as Dan did (see below)? > John Ackerman 40458 > > > On Aug 3, 2008, at 5:25 PM, John Cox wrote: > >> >> Not to attract contrarian comments but the use of metallic scrapers on >> aluminum might be best avoided. We regularly complete such tasks with the >> use of MEK and plastic scrapers (and barrier gloves). Razor blades and putty >> knifes are a quick way to be pointed to the door on air carrier aircraft. >> Your family members deserve no less. >> >>> . Removing the side with the cork gasket was much easier, since the cork >>> is soft and a putty knife can be slipped in between the pieces and the cover >>> plate pried away and popped loose without much difficulty. The ProSeal only >>> side was quite a bit more difficult to break loose, ! >>> and required sliding a single edge razor blade between the bonded >>> surfaces most of the way around the circumference of the cover plate. >>> However, when it came loose it was somewhat easier to clean up using a >>> razor blade as a scraper combined with MEK. >>> >>> So the decision to use a gasket or not really comes down to ease of >>> future maintenance. Either way keeps the fuel in the tank. >>> >>> Hope this helps, >>> -Dan Masys >>> RV-10 N104LD back from OSH >>> RV-7A N747DL >


    Message 13


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    Time: 10:03:10 AM PST US
    From: linn Walters <pitts_pilot@bellsouth.net>
    Subject: Re: Asymmetrical trim noted at OSH
    John Cox wrote: > > I second the comment of a pretty good turn-out and a good group of > product representation entries. > > Kelly would be a good candidate as one of those potential observers. > Each plane should be able to OPT out of the review if desired. Why (and how) would they do that??? Kinda defeats the purpose of increasing your knowledge (I didn't know that!!! :-P ) and everyone is going to see the same thing anyway. This group isn't full of sharks waiting for the chance to bite a head off, and if the 'anomaly' is so bad ..... shouldn't the owner be informed???? > As an EAA Tech, I would be happy to assist the team. > > Keeping rates low is a result of frequent Pilot Proficiency and regular > maintenance. Knowing what to look for, how to correct it and pending > issues beginning to arise saves everyone a lot of money and a loss of > friends. By Opting out we can avoid some of the non-productive > criticism that does not advance safety "One Iota". I spent this year > getting training on becoming a Warbird Judge and how the scoring system > works at OSH. > We'll always get some flames here and there ...... but as a group function I don't think that'll happen. The information could be presented on a written sheet rather than having a public hanging. > The plastic plane crowd has publically conceded that the pursuit of > million dollar kits has given the bulk of the market to VANS and the > RV-10 is becoming the pre-eminent X-Cntry cruiser. > As it should be. My favorite is the Grumman line ..... and the RV-10 is everything the Grumman AA-5s want to be. Plus, we can customize our birds and they can't!!! :-) Our Grumman Gang is a great group to get info from (for the Grummans), and the experience level is high ..... hence the info is excellent. We still have some biting emails, but if there are sensitive owners out there, they just consider the source and move on. The more we take care of our brethren, the better we get as a group, and that will result in better insurance rates and may even result in some flight cost savings. I don't mind taking flak .... builders are an opinionated lot ..... but I'd hate to miss that little nugget of info that helps me out. Linn .... my opinion do not archive > John Cox > Do not Archive > > -----Original Message----- > From: owner-rv10-list-server@matronics.com > [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Tim Olson > Sent: Monday, August 04, 2008 6:34 AM > To: rv10-list@matronics.com > Subject: RV10-List: Asymmetrical trim noted at OSH > > > Was talking to another RV-10 pilot at OSH just before I left and > he told me he peeked at some of the RV-10's that flew in and looked > for asymmetrical trim tab deployment. As we've discussed in > the past, the tabs should be both neutral at the same time, but > when they go up, only one goes up (the other does move up a > tiny amount), and when they go down, they both should go down. > You should never have a situation where one goes up and one > goes down. > > Having only one tab move up may sound crazy, but that's how > it's supposed to work, and keep in mind that this isn't > strange at all....many planes and even the other RV's > are built with only one trim tab on one side. But, what makes > our case unique is that if the builder screws up the rigging, > they can end up with the 2 tabs in opposite deflections.....and > if you follow the plans, you will likely have a small misalignment. > > These observations were not made by me, but were brought > to my attention: > So what was observed was that N921AC has some asymmetrical trim, > then another unpainted RV-10 had a worse condition of > asymmetrical trim. But the one that took the prize was one > of the build-for-customer RV-10's that was at the show.... > from what I was told, that RV-10 had one trim tab that was > approx. 10 degrees up, while the other tab was approx. 10 deg > down. NOW, the interesting thing was, the person also > noticed that it appeared that this particular RV-10 may > have had a little compression deformity of that rear > bulkhead noted in the SB. > > Perhaps next year at OSH we should have a gathering to > specifically look at some noted areas of every RV-10 > and self-group-check for any potential safety issues? > This year I just looked at all the pretty planes. > Pretty good turnout overall. > >


    Message 14


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    Time: 10:46:26 AM PST US
    From: Scott Schmidt <scottmschmidt@yahoo.com>
    Subject: Re: Flap alignment
    Here is a picture of Van's flap in the up position. http://scottandranae.smugmug.com/gallery/1100252_iPQ2t#53383949_nGRvz-A-LB Scott Schmidt scottmschmidt@yahoo.com ----- Original Message ---- From: Jesse Saint <jesse@saintaviation.com> Sent: Tuesday, August 5, 2008 7:28:44 AM Subject: Re: RV10-List: Flap alignment Lew, The best way I have seen to get the flaps correctly rigged is to have them installed on the plane and to raise them to the point that the bottom of the flap is flush with the bottom of the fuselage. Also, both flaps should reach this point at the same time. If it possible for one to reach this point early and put extra strain on the flap rod while the motor reaches full up. If this happens, when you drop the flaps the plane will want to roll because one flap will deploy more than the other. BTW, you will have to file down the end of the flap to remove any clearance issues with the side of the fuselage, and don't forget that there will be paint added, so leave a little room for paint, while not leaving a big gaping hole. The length on all of the pushrods can vary a little based on different components in the system. On the flaps, if you don't have them drilled and bolted with the exact dimensions as the plans call for, this can change the length of the pushrod. It's best to get it close and then install it and adjust for full retraction and deployment of the flaps and then snug up the jam nuts and mark which one is right and left for reinstallation after the wings go back on, unless (of course) you are rigging them with the final wing installation. Also something I have seen in the Aileron rigging. It is not uncommon, from what I have seen, to have the pushrod that connects to the aileron itself to have clearance issues with the aileron attach hinge when in full down. Make sure you don't have that issue when rigging. Jesse Saint Saint Aviation, Inc. jesse@saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Aug 3, 2008, at 9:47 PM, Lew Gallagher wrote: > > OK, we aligned the flaps, ailerons, wingtips today. Obviously > everything starts with the flaps in the raised position. But there > are adjustments on the flaps, so how do you know what the correct > raised position is? The instructions for length of the connecting > rods are a start, but how do you know when it's perfect? > > Not being a pilot, I just stuck a straight edge on the upper surface > of the wing and adjusted the flaps to be on that same plane to get > started. But now at home on the computer, I thought I'd better > check since I thought I remembered reading about slight up angle on > trailing edge for both ailerons for speed, etc. > > I've searched the archives and Tim's site, and sure enough, I found > a reference by Tim to a -3 degree in the up position of the flaps. > > Can someone confirm this for us? With the flaps/ailerons on the > same plane as the upper wing surface, I have both trailing ends of > the wingtips about 1/4 inch above the ailerons. I'm ready to > reshape the wingtip ends tomorrow, but they would be close to being > right if there is "up" built into the flap/aileron position. > > The wingtips are also slightly less than 1/4 inch too short -- as > opposed to the early ones that were too long. Is that a problem? > It wouldn't take much to add resin/flox to lengthen them a bit. > Heck, everything else is coming together so fine, I might as well > make that right too -- I just need to know what "right" is! > > Later, - Lew > > -------- > non-pilot > crazy about building > NOW OFICIALLY BUILDER #40549 > Engine and FF here, now cowl and baffels,waiting on prop. > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=196346#196346 > >


    Message 15


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    Time: 11:14:09 AM PST US
    From: "Les Kearney" <kearney@shaw.ca>
    Subject: Asymmetrical trim noted at OSH
    Linn Your post about "opting out" is a good segway into a topic that I wanted to raise with the group. Over my build process, this list has been my support group in a very real sense. There are few builders where I am so I have had to learn as a go along and call on the list when I run into problems. To that end, I find it easier and easier to admit my mistakes and get help. While at KOSH, I spoke with another builder who recognized my name from my "Oh sh*t" posts. As a builder he was only lurking as he found the list a bit intimidating. As a group, I believe that we need to encourage more builders to raise their issues and problems so that they can move forward in the knowledge that they are not alone in turning aluminum into scrap. If you read the list over time, it is easy to get the impression that not many "mistakes" are raised and therefore everyone is doing everything exactly right. While on the surface, having a "group inspection" of a/c at KOSH may sound like a good idea, I am not sure I would appreciate an uninvited critique of my workmanship. I suspect the process would all too easily evolve into a beauty contest. I understand that anyone can look at any a/c at KOSH and form their own opinions. This is fair dinkum. However, I don't think a "group inspection" would be such a great idea as it might offend the mere mortals on the list who are not building a show plane. Perhaps a better approach would be to identify a few recognized knowledgeable builders who can offer to review a/c one on one if asked. This respects the individual builders while making a very worthwhile service available in an informal and non-threatening manner. Just my $0.02 Cheers Les "some assembly required" Kearney #40643 -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of linn Walters Sent: August-04-08 10:58 AM Subject: Re: RV10-List: Asymmetrical trim noted at OSH John Cox wrote: > > I second the comment of a pretty good turn-out and a good group of > product representation entries. > > Kelly would be a good candidate as one of those potential observers. > Each plane should be able to OPT out of the review if desired. Why (and how) would they do that??? Kinda defeats the purpose of increasing your knowledge (I didn't know that!!! :-P ) and everyone is going to see the same thing anyway. This group isn't full of sharks waiting for the chance to bite a head off, and if the 'anomaly' is so bad ..... shouldn't the owner be informed???? > As an EAA Tech, I would be happy to assist the team. > > Keeping rates low is a result of frequent Pilot Proficiency and regular > maintenance. Knowing what to look for, how to correct it and pending > issues beginning to arise saves everyone a lot of money and a loss of > friends. By Opting out we can avoid some of the non-productive > criticism that does not advance safety "One Iota". I spent this year > getting training on becoming a Warbird Judge and how the scoring system > works at OSH. > We'll always get some flames here and there ...... but as a group function I don't think that'll happen. The information could be presented on a written sheet rather than having a public hanging. > The plastic plane crowd has publically conceded that the pursuit of > million dollar kits has given the bulk of the market to VANS and the > RV-10 is becoming the pre-eminent X-Cntry cruiser. > As it should be. My favorite is the Grumman line ..... and the RV-10 is everything the Grumman AA-5s want to be. Plus, we can customize our birds and they can't!!! :-) Our Grumman Gang is a great group to get info from (for the Grummans), and the experience level is high ..... hence the info is excellent. We still have some biting emails, but if there are sensitive owners out there, they just consider the source and move on. The more we take care of our brethren, the better we get as a group, and that will result in better insurance rates and may even result in some flight cost savings. I don't mind taking flak .... builders are an opinionated lot ..... but I'd hate to miss that little nugget of info that helps me out. Linn .... my opinion do not archive


    Message 16


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    Time: 12:10:06 PM PST US
    From: linn Walters <pitts_pilot@bellsouth.net>
    Subject: Re: Asymmetrical trim noted at
    OSH Les Kearney wrote: > > Linn > > Your post about "opting out" is a good segway into a topic that I wanted to > raise with the group. > > Over my build process, this list has been my support group in a very real > sense. There are few builders where I am so I have had to learn as a go > along and call on the list when I run into problems. To that end, I find it > easier and easier to admit my mistakes and get help. > They say confession is good for the soul! > While at KOSH, I spoke with another builder who recognized my name from my > "Oh sh*t" posts. As a builder he was only lurking as he found the list a bit > intimidating. As a group, I believe that we need to encourage more builders > to raise their issues and problems so that they can move forward in the > knowledge that they are not alone in turning aluminum into scrap. If you > read the list over time, it is easy to get the impression that not many > "mistakes" are raised and therefore everyone is doing everything exactly > right. > We all make mistakes. It's how we handle them that makes the difference. I'll admit to welding up the elevator horn holes twice because I wasn't satisfied. I ended up drilling the holes for the pushrod starting with 1/8" and working my way up to the #12 .... in three steps. Much, much easier although it took much, much longer. I'm now a satisfied camper. > While on the surface, having a "group inspection" of a/c at KOSH may sound > like a good idea, I am not sure I would appreciate an uninvited critique of > my workmanship. I suspect the process would all too easily evolve into a > beauty contest. I understand that anyone can look at any a/c at KOSH and > form their own opinions. This is fair dinkum. However, I don't think a > "group inspection" would be such a great idea as it might offend the mere > mortals on the list who are not building a show plane. > I see your point. There are no perfect airplanes out there .... whether we build them or a factory does. When I built my Pitts, it was rough compared to those who have built many. I was (and still am) really proud of my accomplishment. About the only thing I'm learning about with the RV-10 is the riveting .... and I'm getting the same education everyone else is. However, I don't get anal about a 'slightly imperfect' rivet. I'm not building my airplane for awards .... I'm going to fly the dickens out of it. My RV-10 isn't going to sit in the hangar like antique cars sit in garages. It's the consensus of a group that I look for. Like I said, we're an opinionated group, and the lone pair of eyes can do more 'damage' to your building reputation by running his mouth. He may be ignorant of the truth. The group opinion should be far more constructive. It's the experience of those looking that's important. > Perhaps a better approach would be to identify a few recognized > knowledgeable builders who can offer to review a/c one on one if asked. This > respects the individual builders while making a very worthwhile service > available in an informal and non-threatening manner. > Another good point. However, when do you see the recognized knowledgeable builders without a group??? ;-) > Just my $0.02 > And I appreciate your comments. I find this to be a really great group, and don't want 'fear of criticism' to cause anyone not to participate. Linn ..... will be part of the flying group someday > Cheers > > Les "some assembly required" Kearney > #40643


    Message 17


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    Time: 01:34:32 PM PST US
    From: Robert Wright <flywrights@yahoo.com>
    Subject: Re: Asymmetrical trim noted at OSH
    how about everybody come to my airport and inspect my airplane before the a irworthiness inspector does?- That'd be great!=0Ai should be careful for what I wish!=0ARob Wright=0A#392=0Awindshield fairing and spinner=0A=0A=0A =0A----- Original Message ----=0AFrom: Les Kearney <kearney@shaw.ca>=0ATo: rv10-list@matronics.com=0ASent: Monday, August 4, 2008 2:10:42 PM=0ASubject : Constructive Feedback was RV10-List: Asymmetrical trim noted at OSH=0A=0A =0A=0AYour post about "opting out" is a good segway into a topic that I wan ted to=0Araise with the group.=0A=0AOver my build process, this list has be en my support group in a very real=0Asense. There are few builders where I am so I have had to learn as a go=0Aalong and call on the list when I run i nto problems. To that end, I find it=0Aeasier and easier to admit my mistak es and get help. =0A=0AWhile at KOSH, I spoke with another builder who reco gnized my name from my=0A"Oh sh*t" posts. As a builder he was only lurking as he found the list a bit=0Aintimidating. As a group, I believe that we ne ed to encourage more builders=0Ato raise their issues and problems so that they can move forward in the=0Aknowledge that they are not alone in turning aluminum into scrap. If you=0Aread the list over time, it is easy to get t he impression that not many=0A"mistakes" are raised and therefore everyone is doing everything exactly=0Aright. =0A=0AWhile on the surface, having a " group inspection" of a/c at KOSH may sound=0Alike a good idea, I am not sur e I would appreciate an uninvited critique of=0Amy workmanship. I suspect t he process would all too easily evolve into a=0Abeauty contest. I understan d that anyone can look at any a/c at KOSH and=0Aform their own opinions. Th is is fair dinkum. However, I don't think a=0A"group inspection" would be s uch a great idea as it might offend the mere=0Amortals on the list who are not building a show plane.=0A=0APerhaps a better approach would be to ident ify a few recognized=0Aknowledgeable builders who can offer to review a/c o ne on one if asked. This=0Arespects the individual builders while making a very worthwhile service=0Aavailable in an informal and non-threatening mann er.=0A=0AJust my $0.02=0A=0ACheers=0A=0ALes "some assembly required" Kearne y=0A#40643=0A=0A-----Original Message-----=0AFrom: owner-rv10-list-server@m atronics.com=0A[mailto:owner-rv10-list-server@matronics.com] On Behalf Of l inn Walters=0ASent: August-04-08 10:58 AM=0ATo: rv10-list@matronics.com=0AS ubject: Re: RV10-List: Asymmetrical trim noted at OSH=0A=0A--> RV10-List me ssage posted by: linn Walters <pitts_pilot@bellsouth.net>=0A=0AJohn Cox wro >=0A>=0A> I second the comment of a pretty good turn-out and a good group o f=0A> product representation entries.=0A>=0A> Kelly would be a good candida te as one of those potential observers.=0A> Each plane should be able to OP T out of the review if desired.=0AWhy (and how) would they do that???- Ki nda defeats the purpose of =0Aincreasing your knowledge (I didn't know that !!! :-P ) and everyone is =0Agoing to see the same thing anyway.- This gr oup isn't full of sharks =0Awaiting for the chance to bite a head off, and if the 'anomaly' is so =0Abad ..... shouldn't the owner be informed????=0A> - As an EAA Tech, I would be happy to assist the team.=0A>=0A> Keeping ra tes low is a result of frequent Pilot Proficiency and regular=0A> maintenan ce.- Knowing what to look for, how to correct it and pending=0A> issues b eginning to arise saves everyone a lot of money and a loss of=0A> friends. - By Opting out we can avoid some of the non-productive=0A> criticism tha t does not advance safety "One Iota".- I spent this year=0A> getting trai ning on becoming a Warbird Judge and how the scoring system=0A> works at OS H.=0A>- =0AWe'll always get some flames here and there ...... but as a gr oup =0Afunction I don't think that'll happen.- The information could be =0Apresented on a written sheet rather than having a public hanging.=0A> Th e plastic plane crowd has publically conceded that the pursuit of=0A> milli on dollar kits has given the bulk of the market to VANS and the=0A> RV-10 i s becoming the pre-eminent X-Cntry cruiser.=0A>- =0AAs it should be.- M y favorite is the Grumman line ..... and the RV-10 is =0Aeverything the Gru mman AA-5s want to be.- Plus, we can customize our =0Abirds and they can' t!!! :-)=0A=0AOur Grumman Gang is a great group to get info from (for the G rummans), =0Aand the experience level is high ..... hence the info is excel lent.- We =0Astill have some biting emails, but if there are sensitive ow ners out =0Athere, they just consider the source and move on.=0A=0AThe more we take care of our brethren, the better we get as a group, and =0Athat wi ll result in better insurance rates and may even result in some =0Aflight c ost savings.- I don't mind taking flak .... builders are an =0Aopinionate d lot ..... but I'd hate to miss that little nugget of info =0Athat helps m ===================0A=0A=0A


    Message 18


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    Time: 02:31:43 PM PST US
    From: "pascal" <pascal@rv10builder.net>
    Subject: Re: Asymmetrical trim noted at OSH
    Les; My problem is I read too much about the building process so I don't recall where I read this but the group inspection idea is one I read and always thought was a great idea. . I have had many come by and look for all my shortfalls, my TC is a very knowledgeable RV pilot and I always dread what he will say about my building, I listen carefully to every comment, I ask questions and in the end am very happy for the feedback I received which usually is far more optimistic than I held my building skills to be. The important thing to remember is that we can take advice or leave it but one needs to consider what is raised and seriously determine if it applies. The good thing about a group (and this one is a great one) is that one can say they messed up and get feedback, which I usually take as positive and not harsh, Tim and a few others have made "gotchas" as a link to show how it is common for us to have issues with steps and sections. Section 29 was a breeze, the fuel tank sealing was a breeze, not because I am good, but because I was given a gotcha to avoid and hence was able to take the plans and adjust it to others issues so I would not have the same issue. If one looks at all the great sites out there Tim's, Deems, William Curtis, etc they have had many issues and they mention them and what they needed to do to repair the issue, I have looked at all these sites, Mike Rowe's and initially John Jensen to see what they did so I can work off of that as a starting point. Basically I think there is quite a lot out there to see what others have done before us and sitting in front of a computer I have more courage to ask a question and run than have someone look me in the face and say "you have got to be kidding.." which I jest because usually the responses come back quickly and allows one to think through options to repair the issue. Pascal -------------------------------------------------- From: "Les Kearney" <kearney@shaw.ca> Sent: Monday, August 04, 2008 11:10 AM Subject: Constructive Feedback was RV10-List: Asymmetrical trim noted at OSH > > Linn > > Your post about "opting out" is a good segway into a topic that I wanted > to > raise with the group. > > Over my build process, this list has been my support group in a very real > sense. There are few builders where I am so I have had to learn as a go > along and call on the list when I run into problems. To that end, I find > it > easier and easier to admit my mistakes and get help. > > While at KOSH, I spoke with another builder who recognized my name from my > "Oh sh*t" posts. As a builder he was only lurking as he found the list a > bit > intimidating. As a group, I believe that we need to encourage more > builders > to raise their issues and problems so that they can move forward in the > knowledge that they are not alone in turning aluminum into scrap. If you > read the list over time, it is easy to get the impression that not many > "mistakes" are raised and therefore everyone is doing everything exactly > right. > > While on the surface, having a "group inspection" of a/c at KOSH may sound > like a good idea, I am not sure I would appreciate an uninvited critique > of > my workmanship. I suspect the process would all too easily evolve into a > beauty contest. I understand that anyone can look at any a/c at KOSH and > form their own opinions. This is fair dinkum. However, I don't think a > "group inspection" would be such a great idea as it might offend the mere > mortals on the list who are not building a show plane. > > Perhaps a better approach would be to identify a few recognized > knowledgeable builders who can offer to review a/c one on one if asked. > This > respects the individual builders while making a very worthwhile service > available in an informal and non-threatening manner. > > Just my $0.02 > > Cheers > > Les "some assembly required" Kearney > #40643 > > -----Original Message----- > From: owner-rv10-list-server@matronics.com > [mailto:owner-rv10-list-server@matronics.com] On Behalf Of linn Walters > Sent: August-04-08 10:58 AM > To: rv10-list@matronics.com > Subject: Re: RV10-List: Asymmetrical trim noted at OSH > > > John Cox wrote: >> >> I second the comment of a pretty good turn-out and a good group of >> product representation entries. >> >> Kelly would be a good candidate as one of those potential observers. >> Each plane should be able to OPT out of the review if desired. > Why (and how) would they do that??? Kinda defeats the purpose of > increasing your knowledge (I didn't know that!!! :-P ) and everyone is > going to see the same thing anyway. This group isn't full of sharks > waiting for the chance to bite a head off, and if the 'anomaly' is so > bad ..... shouldn't the owner be informed???? >> As an EAA Tech, I would be happy to assist the team. >> >> Keeping rates low is a result of frequent Pilot Proficiency and regular >> maintenance. Knowing what to look for, how to correct it and pending >> issues beginning to arise saves everyone a lot of money and a loss of >> friends. By Opting out we can avoid some of the non-productive >> criticism that does not advance safety "One Iota". I spent this year >> getting training on becoming a Warbird Judge and how the scoring system >> works at OSH. >> > We'll always get some flames here and there ...... but as a group > function I don't think that'll happen. The information could be > presented on a written sheet rather than having a public hanging. >> The plastic plane crowd has publically conceded that the pursuit of >> million dollar kits has given the bulk of the market to VANS and the >> RV-10 is becoming the pre-eminent X-Cntry cruiser. >> > As it should be. My favorite is the Grumman line ..... and the RV-10 is > everything the Grumman AA-5s want to be. Plus, we can customize our > birds and they can't!!! :-) > > Our Grumman Gang is a great group to get info from (for the Grummans), > and the experience level is high ..... hence the info is excellent. We > still have some biting emails, but if there are sensitive owners out > there, they just consider the source and move on. > > The more we take care of our brethren, the better we get as a group, and > that will result in better insurance rates and may even result in some > flight cost savings. I don't mind taking flak .... builders are an > opinionated lot ..... but I'd hate to miss that little nugget of info > that helps me out. > Linn .... my opinion > do not archive > > >


    Message 19


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    Time: 02:47:27 PM PST US
    Subject: PIREP: Tungsten Bucking Bar
    From: "Douglas, Brian S" <brian-douglas@uiowa.edu>
    My wife and I stopped by the Cleaveland truck during OSH to say hi to Mike and of course browse the tool selection. After some glowing praise of the tungsten bucking bars ("rivets practically melt with these things") we decided to buy one and see what the hoopla is all about. Well, after driving 30-ish rivets last night (many in very tight quarters) I have to say I'm really impressed. The bar is so small it's hard to imagine many spots on the plane that you couldn't get it lined up on a rivet and yet it has the same mass of bars 4-5 times its size. It's early but my initial impression is that this is a must have tool, particularly for a new builder who doesn't already have a bunch of money invested in regular steel bars. Just my $.02 -Brian Iowa City, IA #40497


    Message 20


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    Time: 03:02:52 PM PST US
    Subject: Re: Flap alignment
    From: "Lew Gallagher" <lewgall@charter.net>
    DONE! Thanks for your timely responses. I made a -3 degree jig and went with that. Miraculously, when I adjusted the ailerons to the new flap position, the wing tips were dead on! Unbelievable, made my day. We started early while it was still cool and had the new adjustments made, all push rod locknuts tightened and safety painted, then disassembled and wings off and back in the garage by the time Van's opened up (12 noon our time). And none too soon since it hit 98 today. So we didn't bother to check with Van's. Scott and Jessie, thanks for the tip of looking at the corner relative to the fuse bottom edge. I did go ahead and trim the inner edge of the flaps to give a good clearance. And with the -3 degree setting, the corner is just a bit lower than the edge -- close enough since I don't want to mess with the great wingtip alignment. Later, - Lew -------- non-pilot crazy about building NOW OFICIALLY BUILDER #40549 Engine and FF here, now cowl and baffels,waiting on prop. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=196492#196492


    Message 21


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    Time: 03:38:55 PM PST US
    From: Kelly McMullen <kellym@aviating.com>
    Subject: Re: Asymmetrical trim noted at
    OSH Les, et al, I don't know if Canada has them, but this is one of the functions of the EAA Tech Counselor program. Perhaps there aren't too many tech counselors who are RV-10 builders yet...but John C and myself are. I'm not far enough into my project to offer much -10 specific advise, yet..but perhaps there are others who are. Anyone who has built a plane such as the RV-10 can apply to the EAA for designation as a Tech Counselor. I would encourage some of you that are flying to consider this, and it is a good way to both meet new builders and volunteer a little time to advise them. More information is available on the EAA web site. Most EAA chapters will have several, and some have even built an RV before. 8-) Project visits are done one on one, a written report is given to the builder, and a copy goes to EAA. It is one effort to reduce failures during the test fly-off period. Les Kearney wrote: > > Linn > > Your post about "opting out" is a good segway into a topic that I wanted to > raise with the group. > > Over my build process, this list has been my support group in a very real > sense. There are few builders where I am so I have had to learn as a go > along and call on the list when I run into problems. To that end, I find it > easier and easier to admit my mistakes and get help. > > While at KOSH, I spoke with another builder who recognized my name from my > "Oh sh*t" posts. As a builder he was only lurking as he found the list a bit > intimidating. As a group, I believe that we need to encourage more builders > to raise their issues and problems so that they can move forward in the > knowledge that they are not alone in turning aluminum into scrap. If you > read the list over time, it is easy to get the impression that not many > "mistakes" are raised and therefore everyone is doing everything exactly > right. > > While on the surface, having a "group inspection" of a/c at KOSH may sound > like a good idea, I am not sure I would appreciate an uninvited critique of > my workmanship. I suspect the process would all too easily evolve into a > beauty contest. I understand that anyone can look at any a/c at KOSH and > form their own opinions. This is fair dinkum. However, I don't think a > "group inspection" would be such a great idea as it might offend the mere > mortals on the list who are not building a show plane. > > Perhaps a better approach would be to identify a few recognized > knowledgeable builders who can offer to review a/c one on one if asked. This > respects the individual builders while making a very worthwhile service > available in an informal and non-threatening manner. > > Just my $0.02 > > Cheers > > Les "some assembly required" Kearney > #40643 > >


    Message 22


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    Time: 04:15:06 PM PST US
    Subject: Asymmetrical trim noted at OSH
    From: "John Cox" <johnwcox@pacificnw.com>
    Which airport? The DAR program involves non FAA personnel in the awarding of Airworthiness Certificates and the submission of application for a Repairman's Certificate. There was quite a discussion about DARs who are knowingly signing off multiple builds by the same builder for hire during the second 51% meeting at Osh. The first meeting on the 51% was by the FED about the rule change, in reality a policy change which "Is not about Safety". You may have a DAR who is just right for you. We had a great Airworthiness Inspector who moved from Hillsboro to Spokane and we lost a valued resource locally. "Das Fed" John Cox From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Robert Wright Sent: Monday, August 04, 2008 1:31 PM Subject: Re: Constructive Feedback was RV10-List: Asymmetrical trim noted at OSH how about everybody come to my airport and inspect my airplane before the airworthiness inspector does? That'd be great! i should be careful for what I wish! Rob Wright #392 windshield fairing and spinner ----- Original Message ---- From: Les Kearney <kearney@shaw.ca> Sent: Monday, August 4, 2008 2:10:42 PM Subject: Constructive Feedback was RV10-List: Asymmetrical trim noted at OSH Linn Your post about "opting out" is a good segway into a topic that I wanted to raise with the group. Over my build process, this list has been my support group in a very real sense. There are few builders where I am so I have had to learn as a go along and call on the list when I run into problems. To that end, I find it easier and easier to admit my mistakes and get help. While at KOSH, I spoke with another builder who recognized my name from my "Oh sh*t" posts. As a builder he was only lurking as he found the list a bit intimidating. As a group, I believe that we need to encourage more builders to raise their issues and problems so that they can move forward in the knowledge that they are not alone in turning aluminum into scrap. If you read the list over time, it is easy to get the impression that not many "mistakes" are raised and therefore everyone is doing everything exactly right. While on the surface, having a "group inspection" of a/c at KOSH may sound like a good idea, I am not sure I would appreciate an uninvited critique of my workmanship. I suspect the process would all too easily evolve into a beauty contest. I understand that anyone can look at any a/c at KOSH and form their own opinions. This is fair dinkum. However, I don't think a "group inspection" would be such a great idea as it might offend the mere mortals on the list who are not building a show plane. Perhaps a better approach would be to identify a few recognized knowledgeable builders who can offer to review a/c one on one if asked. This respects the individual builders while making a very worthwhile service available in an informal and non-threatening manner. Just my $0.02 Cheers Les "some assembly required" Kearney #40643 -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of linn Walters Sent: August-04-08 10:58 AM Subject: Re: RV10-List: Asymmetrical trim noted at OSH <pitts_pilot@bellsouth.net> John Cox wrote: > > I second the comment of a pretty good turn-out and a good group of > product representation entries. > > Kelly would be a good candidate as one of those potential observers. > Each plane should be able to OPT out of the review if desired. Why (and how) would they do that??? Kinda defeats the purpose of increasing your knowledge (I didn't know that!!! :-P ) and everyone is going to see the same thing anyway. This group isn't full of sharks waiting for the chance to bite a head off, and if the 'anomaly' is so bad ..... shouldn't the owner be informed???? > As an EAA Tech, I would be happy to assist the team. > > Keeping rates low is a result of frequent Pilot Proficiency and regular > maintenance. Knowing what to look for, how to correct it and pending > issues beginning to arise saves everyone a lot of money and a loss of > friends. By Opting out we can avoid some of the non-productive > criticism that does not advance safety "One Iota". I spent this year > getting training on becoming a Warbird Judge and how the scoring system > works at OSH. > We'll always get some flames here and there ...... but as a group function I don't think that'll happen. The information could be presented on a written sheet rather than having a public hanging. > The plastic plane crowd has publically conceded that the pursuit of > million dollar kits has given the bulk of the market to VANS and the > RV-10 is becoming the pre-eminent X-Cntry cruiser. > As it should be. My favorite is the Grumman line ..... and the RV-10 is everything the Grumman AA-5s want to be. Plus, we can customize our birds and they can't!!! :-) Our Grumman Gang is a great group to get info from (for the Grummans), and the experience level is high ..... hence the info is excellent. We still have some biting emails, but if there are sensitive owners out there, they just consider the source and move on. The more we take care of our brethren, the better we get as a group, and that will result in better insurance rates and may even result in some flight cost savings. I don't mind taking flak .... builders are an opinionated lot ..... but I'd hate to miss that little nugget of info that helps me out. Linn .... my opinion do not 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D


    Message 23


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    Time: 04:54:27 PM PST US
    From: "Les Kearney" <kearney@shaw.ca>
    Subject: Center console
    Hi Does anyone have a source for a center console similar to the ones sold by Accuracy Avionics? I don't need a panel, just the center console along with a storage box. I have fabbed an aluminum one but I really like the look of the ones I saw at KOSH. Inquiring minds need to know Les Kearney #40643


    Message 24


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    Time: 05:39:37 PM PST US
    From: "Bob Leffler" <rv@thelefflers.com>
    Subject: Center console
    Stein had one in his booth made out of aluminum. It looked pretty nice. $1,000 was a little too stiff for my budget. I like what Greg Hale did with his panel and console. http://www.nwacaptain.com/panel.html http://www.nwacaptain.com/console.html I asked, but he doesn't have copies of his plans anymore. When I get to this stage, I think I may take the time to build molds. It shouldn't be too hard to duplicate. It may take some time, but it will save some $$$. -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Les Kearney Sent: Monday, August 04, 2008 7:51 PM Subject: RV10-List: Center console Hi Does anyone have a source for a center console similar to the ones sold by Accuracy Avionics? I don't need a panel, just the center console along with a storage box. I have fabbed an aluminum one but I really like the look of the ones I saw at KOSH. Inquiring minds need to know Les Kearney #40643


    Message 25


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    Time: 06:11:29 PM PST US
    From: "Les Kearney" <kearney@shaw.ca>
    Subject: Center console
    Hi Bob I have seen Greg's site before. It was what got me thinking about a center console. I would like mine to be a little less elaborate however as I don't want to divide my panel in thirds. Greg's is pretty nice looking though.. Cheers Les -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Bob Leffler Sent: August-04-08 6:39 PM Subject: RE: RV10-List: Center console Stein had one in his booth made out of aluminum. It looked pretty nice. $1,000 was a little too stiff for my budget. I like what Greg Hale did with his panel and console. http://www.nwacaptain.com/panel.html http://www.nwacaptain.com/console.html I asked, but he doesn't have copies of his plans anymore. When I get to this stage, I think I may take the time to build molds. It shouldn't be too hard to duplicate. It may take some time, but it will save some $$$. -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Les Kearney Sent: Monday, August 04, 2008 7:51 PM Subject: RV10-List: Center console Hi Does anyone have a source for a center console similar to the ones sold by Accuracy Avionics? I don't need a panel, just the center console along with a storage box. I have fabbed an aluminum one but I really like the look of the ones I saw at KOSH. Inquiring minds need to know Les Kearney #40643


    Message 26


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    Time: 06:48:26 PM PST US
    Subject: SMA Diesel
    From: "Dawson-Townsend,Timothy" <tdawson-townsend@aurora.aero>
    Chatting with the SMA Diesel guys at Fond du Lac waiting for Friday's rain shower to blow through . . . They hinted that they have been talking a little with Van's about engineering an installation of the SMA diesel for the RV-10. This is a change from a few years ago when they weren't interested in the homebuilt market. Obviously Van's is conservative when it comes to engines, and SMA is, too. They want to make sure any installation is pretty well wrung out. The engine has essentially been around for at least 6 years now, so they think they have a pretty mature design. It is in their interest, obviously, but they hinted that the end of 100LL is going to accelerate now that some have picked it up as an environmental issue. (i.e. lead pollution) Anyway, for those of you that are in the early stages of building, if you want a certified diesel with a large company behind it for support, it might behoove you to let Van's know about your interest in the SMA diesel. The more folks that mention it to Van's, the more motivation they have to support SMA and perhaps even setup some OEM pricing like they have on Lycomonings. Cheers, TDT Tim Dawson-Townsend Aurora Flight Sciences tdt@aurora.aero 617-500-4812 (office) 617-905-4800 (mobile)


    Message 27


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    Time: 07:22:24 PM PST US
    Subject: SMA Diesel
    From: "John Cox" <johnwcox@pacificnw.com>
    I look forward to SMAs success in convincing VAN to consider a second engine option other than the Lycoming IO-540. I will say prayers and wish them luck for our brethren over the pond that have a hard time with 100LL avgas. I am adding Rob Hickman's 3 blade composite Hartzell to those prayers as well. I was just getting all excited about the Lycoming TEO-540-A ie2 engine having about the same chance. I was also sorry to hear that John Delamarter is no longer with Thunderbolt. Let's start posting about all the new vendor products to get things rolling again. John Cox From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Dawson-Townsend,Timothy Sent: Monday, August 04, 2008 6:45 PM Subject: RV10-List: SMA Diesel Chatting with the SMA Diesel guys at Fond du Lac waiting for Friday's rain shower to blow through . . . They hinted that they have been talking a little with Van's about engineering an installation of the SMA diesel for the RV-10. This is a change from a few years ago when they weren't interested in the homebuilt market. Obviously Van's is conservative when it comes to engines, and SMA is, too. They want to make sure any installation is pretty well wrung out. The engine has essentially been around for at least 6 years now, so they think they have a pretty mature design. It is in their interest, obviously, but they hinted that the end of 100LL is going to accelerate now that some have picked it up as an environmental issue. (i.e. lead pollution) Anyway, for those of you that are in the early stages of building, if you want a certified diesel with a large company behind it for support, it might behoove you to let Van's know about your interest in the SMA diesel. The more folks that mention it to Van's, the more motivation they have to support SMA and perhaps even setup some OEM pricing like they have on Lycomonings. Cheers, TDT Tim Dawson-Townsend Aurora Flight Sciences tdt@aurora.aero 617-500-4812 (office) 617-905-4800 (mobile)


    Message 28


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    Time: 08:25:00 PM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Re: Asymmetrical trim noted at
    OSH Pascal, I like the way you took my intention for that suggestion. Those who know me and know my plane know that I'm just another builder...who's had many of things go wrong along the way. Plenty of mistakes to point out. My plane isn't a showplane at all, but just another RV-10....one that gets flown for what it was designed. I'm not for beauty contests, but think it's great for those coming after me in the build to learn from the mistakes that I and many others have made. I certainly can pick on some planes and show some repetitive examples...but it's never out of poking fun at people...it's either about keeping them safe (i.e. the suggestion of checking peoples trim tabs or flap alignments....both of which are things that I've seen wrong on other RV-10's), or helping other builders avoid cosmetic mistakes. There were many RV-10's on the field this OSH. I saw some fairly average ones with nice blending on their elevator horns, where the fairings were smoothly transitioned to the aluminum. I saw a spectacularly finished RV-10 that lacked the smoothness in that area. Showing these things can help other builders make their planes better. Another perfect example is the seam of the upper forward fuse to the lower forward fuse, just forward of the windshield. I filled that seam well on the aft corners of the windscreen. It looks wonderful. However, it looks cosmetically hideous that I didn't think of filling that seam all the way forward. I'm constantly aware of that on my plane. Funny thing is, there were some absolutely otherwise spectacular planes there that did the same thing. Wouldn't it be nice to have someone point that out to you BEFORE you get that far along?? I know I sure which I had an RV-10 counselor to show me some tips in person. So nope, this isn't about picking on anyones plane, but I think that as a group, there's a lot that could be taught, and learned, by traveling from plane to plane. Can I do it on a one-on-one basis? Sure. But, to tell you the truth, I'm just not interested in that repetition over and over doing one-on-ones...it's inefficient to do it that way at OSH. We all just need to be grown up enough to be willing to share, willing to learn, and have both our positives and negatives pointed out. Heck, start with me...there's a lot of mileage you can have by critiquing the trailing edge of at least one of my doors and how well it blends with the fuselage. ;) Next year for OSH, if you're an RV-10 builder, try to come for the first 3 or 4 days of the show and we'll figure something out to do with that time that will benefit you. I learned this year though that if you're not there for the Sunday-Wed time early in the week, you're going to miss a lot of potential stuff...so come early, stay late, if at all possible. Tim Olson - RV-10 N104CD - Flying do not archive pascal wrote: > > Les; > My problem is I read too much about the building process so I don't > recall where I read this but the group inspection idea is one I read and > always thought was a great idea. . I have had many come by and look for > all my shortfalls, my TC is a very knowledgeable RV pilot and I always > dread what he will say about my building, I listen carefully to every > comment, I ask questions and in the end am very happy for the feedback I > received which usually is far more optimistic than I held my building > skills to be. > The important thing to remember is that we can take advice or leave it > but one needs to consider what is raised and seriously determine if it > applies. > > The good thing about a group (and this one is a great one) is that one > can say they messed up and get feedback, which I usually take as > positive and not harsh, Tim and a few others have made "gotchas" as a > link to show how it is common for us to have issues with steps and > sections. Section 29 was a breeze, the fuel tank sealing was a breeze, > not because I am good, but because I was given a gotcha to avoid and > hence was able to take the plans and adjust it to others issues so I > would not have the same issue. > If one looks at all the great sites out there Tim's, Deems, William > Curtis, etc they have had many issues and they mention them and what > they needed to do to repair the issue, I have looked at all these sites, > Mike Rowe's and initially John Jensen to see what they did so I can work > off of that as a starting point. > Basically I think there is quite a lot out there to see what others have > done before us and sitting in front of a computer I have more courage to > ask a question and run than have someone look me in the face and say > "you have got to be kidding.." which I jest because usually the > responses come back quickly and allows one to think through options to > repair the issue. > Pascal > > -------------------------------------------------- > From: "Les Kearney" <kearney@shaw.ca> > Sent: Monday, August 04, 2008 11:10 AM > To: <rv10-list@matronics.com> > Subject: Constructive Feedback was RV10-List: Asymmetrical trim noted > at OSH > >> >> Linn >> >> Your post about "opting out" is a good segway into a topic that I >> wanted to >> raise with the group. >> >> Over my build process, this list has been my support group in a very real >> sense. There are few builders where I am so I have had to learn as a go >> along and call on the list when I run into problems. To that end, I >> find it >> easier and easier to admit my mistakes and get help. >> >> While at KOSH, I spoke with another builder who recognized my name >> from my >> "Oh sh*t" posts. As a builder he was only lurking as he found the list >> a bit >> intimidating. As a group, I believe that we need to encourage more >> builders >> to raise their issues and problems so that they can move forward in the >> knowledge that they are not alone in turning aluminum into scrap. If you >> read the list over time, it is easy to get the impression that not many >> "mistakes" are raised and therefore everyone is doing everything exactly >> right. >> >> While on the surface, having a "group inspection" of a/c at KOSH may >> sound >> like a good idea, I am not sure I would appreciate an uninvited >> critique of >> my workmanship. I suspect the process would all too easily evolve into a >> beauty contest. I understand that anyone can look at any a/c at KOSH and >> form their own opinions. This is fair dinkum. However, I don't think a >> "group inspection" would be such a great idea as it might offend the mere >> mortals on the list who are not building a show plane. >> >> Perhaps a better approach would be to identify a few recognized >> knowledgeable builders who can offer to review a/c one on one if >> asked. This >> respects the individual builders while making a very worthwhile service >> available in an informal and non-threatening manner. >> >> Just my $0.02 >> >> Cheers >> >> Les "some assembly required" Kearney >> #40643 >> >> -----Original Message----- >> From: owner-rv10-list-server@matronics.com >> [mailto:owner-rv10-list-server@matronics.com] On Behalf Of linn Walters >> Sent: August-04-08 10:58 AM >> To: rv10-list@matronics.com >> Subject: Re: RV10-List: Asymmetrical trim noted at OSH >> >> >> John Cox wrote: >>> >>> I second the comment of a pretty good turn-out and a good group of >>> product representation entries. >>> >>> Kelly would be a good candidate as one of those potential observers. >>> Each plane should be able to OPT out of the review if desired. >> Why (and how) would they do that??? Kinda defeats the purpose of >> increasing your knowledge (I didn't know that!!! :-P ) and everyone is >> going to see the same thing anyway. This group isn't full of sharks >> waiting for the chance to bite a head off, and if the 'anomaly' is so >> bad ..... shouldn't the owner be informed???? >>> As an EAA Tech, I would be happy to assist the team. >>> >>> Keeping rates low is a result of frequent Pilot Proficiency and regular >>> maintenance. Knowing what to look for, how to correct it and pending >>> issues beginning to arise saves everyone a lot of money and a loss of >>> friends. By Opting out we can avoid some of the non-productive >>> criticism that does not advance safety "One Iota". I spent this year >>> getting training on becoming a Warbird Judge and how the scoring system >>> works at OSH. >>> >> We'll always get some flames here and there ...... but as a group >> function I don't think that'll happen. The information could be >> presented on a written sheet rather than having a public hanging. >>> The plastic plane crowd has publically conceded that the pursuit of >>> million dollar kits has given the bulk of the market to VANS and the >>> RV-10 is becoming the pre-eminent X-Cntry cruiser. >>> >> As it should be. My favorite is the Grumman line ..... and the RV-10 is >> everything the Grumman AA-5s want to be. Plus, we can customize our >> birds and they can't!!! :-) >> >> Our Grumman Gang is a great group to get info from (for the Grummans), >> and the experience level is high ..... hence the info is excellent. We >> still have some biting emails, but if there are sensitive owners out >> there, they just consider the source and move on. >> >> The more we take care of our brethren, the better we get as a group, and >> that will result in better insurance rates and may even result in some >> flight cost savings. I don't mind taking flak .... builders are an >> opinionated lot ..... but I'd hate to miss that little nugget of info >> that helps me out. >> Linn .... my opinion >> do not archive >> >> >> >> >> >> > > > >


    Message 29


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    Time: 08:26:48 PM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Re: Flap alignment
    Did you find that the flap was basically bottomed out on the spar when you were at -3 degrees? As far as I remember, the alignment process starts with the flaps tight against the rear spar...and that's about where the -3 is...and everything aligns to that. If your flaps though are below the fuselage when they're all the way at -3, you're almost definitely looking at drooped flaps...and it'll cost you a couple kts at best. So how close is your jig-measured -3 degress to the flaps bottoming out? Tim Olson - RV-10 N104CD - Flying do not archive Lew Gallagher wrote: > <lewgall@charter.net> > > DONE! Thanks for your timely responses. I made a -3 degree jig and > went with that. Miraculously, when I adjusted the ailerons to the > new flap position, the wing tips were dead on! Unbelievable, made my > day. > > We started early while it was still cool and had the new adjustments > made, all push rod locknuts tightened and safety painted, then > disassembled and wings off and back in the garage by the time Van's > opened up (12 noon our time). And none too soon since it hit 98 > today. So we didn't bother to check with Van's. > > Scott and Jessie, thanks for the tip of looking at the corner > relative to the fuse bottom edge. I did go ahead and trim the inner > edge of the flaps to give a good clearance. And with the -3 degree > setting, the corner is just a bit lower than the edge -- close enough > since I don't want to mess with the great wingtip alignment. > > Later, - Lew > > -------- non-pilot crazy about building NOW OFICIALLY BUILDER #40549 > Engine and FF here, now cowl and baffels,waiting on prop. > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=196492#196492 > > > > > > > > http://www.matronics.com/Navigator?RV10-List > > >


    Message 30


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    Time: 08:29:56 PM PST US
    From: "David McNeill" <dlm46007@cox.net>
    Subject: new prroducts
    Apparently the new PMAG for the IO540 is going to be tested on an RV10 starting directly after Oshkosh 2008. _____ From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of John Cox Sent: Monday, August 04, 2008 7:19 PM Subject: RE: RV10-List: SMA Diesel I look forward to SMAs success in convincing VAN to consider a second engine option other than the Lycoming IO-540. I will say prayers and wish them luck for our brethren over the pond that have a hard time with 100LL avgas. I am adding Rob Hickman's 3 blade composite Hartzell to those prayers as well. I was just getting all excited about the Lycoming TEO-540-A ie2 engine having about the same chance. I was also sorry to hear that John Delamarter is no longer with Thunderbolt. Let's start posting about all the new vendor products to get things rolling again. John Cox From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Dawson-Townsend,Timothy Sent: Monday, August 04, 2008 6:45 PM Subject: RV10-List: SMA Diesel Chatting with the SMA Diesel guys at Fond du Lac waiting for Friday's rain shower to blow through . . . They hinted that they have been talking a little with Van's about engineering an installation of the SMA diesel for the RV-10. This is a change from a few years ago when they weren't interested in the homebuilt market. Obviously Van's is conservative when it comes to engines, and SMA is, too. They want to make sure any installation is pretty well wrung out. The engine has essentially been around for at least 6 years now, so they think they have a pretty mature design. It is in their interest, obviously, but they hinted that the end of 100LL is going to accelerate now that some have picked it up as an environmental issue. (i.e. lead pollution) Anyway, for those of you that are in the early stages of building, if you want a certified diesel with a large company behind it for support, it might behoove you to let Van's know about your interest in the SMA diesel. The more folks that mention it to Van's, the more motivation they have to support SMA and perhaps even setup some OEM pricing like they have on Lycomonings. Cheers, TDT Tim Dawson-Townsend Aurora Flight Sciences tdt@aurora.aero 617-500-4812 (office) 617-905-4800 (mobile) http://www.matronics.com/Navigator?RV10-List http://forums.matronics.com http://www.matronics.com/contribution


    Message 31


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    Time: 09:06:35 PM PST US
    From: "Dave Leikam" <daveleikam@wi.rr.com>
    Subject: Re: SMA Diesel
    I was told by a rep at SMA that the retro-fit cost for a C182 is north of 100k. Dave Leikam RV-10 #40496 N89DA (Reserved) Muskego, WI ----- Original Message ----- From: Dawson-Townsend,Timothy To: rv10-list@matronics.com Sent: Monday, August 04, 2008 8:45 PM Subject: RV10-List: SMA Diesel Chatting with the SMA Diesel guys at Fond du Lac waiting for Friday's rain shower to blow through . . . They hinted that they have been talking a little with Van's about engineering an installation of the SMA diesel for the RV-10. This is a change from a few years ago when they weren't interested in the homebuilt market. Obviously Van's is conservative when it comes to engines, and SMA is, too. They want to make sure any installation is pretty well wrung out. The engine has essentially been around for at least 6 years now, so they think they have a pretty mature design. It is in their interest, obviously, but they hinted that the end of 100LL is going to accelerate now that some have picked it up as an environmental issue. (i.e. lead pollution) Anyway, for those of you that are in the early stages of building, if you want a certified diesel with a large company behind it for support, it might behoove you to let Van's know about your interest in the SMA diesel. The more folks that mention it to Van's, the more motivation they have to support SMA and perhaps even setup some OEM pricing like they have on Lycomonings. Cheers, TDT Tim Dawson-Townsend Aurora Flight Sciences tdt@aurora.aero 617-500-4812 (office) 617-905-4800 (mobile)


    Message 32


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    Time: 09:34:14 PM PST US
    From: "Kelly McMullen" <apilot2@gmail.com>
    Subject: Re: SMA Diesel
    Aside from cost issues...that package is designed to replace a 230 hp O-470, which weigh as much as an IO-550. There would have to be some serious effort to resolve W& B issues. Also, IIRC it needs a fair amount of cooling air for the radiator...not very streamlined. On Mon, Aug 4, 2008 at 9:03 PM, Dave Leikam <daveleikam@wi.rr.com> wrote: > I was told by a rep at SMA that the retro-fit cost for a C182 is north of > 100k. > > Dave Leikam > RV-10 #40496 > N89DA (Reserved) > Muskego, WI > >


    Message 33


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    Time: 09:53:38 PM PST US
    Subject: OSH RV-10 Nose Wheel Pants & Fairing
    From: "Robin Marks" <robin1@mrmoisture.com>
    Thanks everyone at OSH that made this year special. I neglected to photograph a mostly white -10 (from North or South Dakota) on the flight line that had some spectacular yet subtle fiberglass work. I am specifically referring to the Nose Wheel Pants and Leg Fairing. This builder changed the geometry of the leg fairing as it intersected the wheel pants giving the transition a flat surface for the wheel to pivot vs. the standard Vans look. The builder also built up the leading edge of the Nose Wheel Pant for a smooth transition to the Leg Fairing. If anyone took a picture that assembly would you please forward me a copy? Thanks, Robin Do Not Archive Robin@PaintTheWeb.com


    Message 34


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    Time: 10:00:29 PM PST US
    From: "John Cumins" <jcumins@jcis.net>
    Subject: Las Vegas Area 10 Builders
    Any 10 builders in the Las Vegas area, I will be in Las Vegas for 4 days and will have free time to visit to talk flying, building ect. Please contact me 707-479-5895 cell John G. Cumins President JC'S Interactive Systems 2499 B1 Martin Rd Fairfield Ca 94533 707-425-7100 707-425-7576 Fax Your Total Technology Solution Provider




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