RV-List Digest Archive

Thu 07/22/04


Total Messages Posted: 30



Today's Message Index:
----------------------
 
     1. 03:07 AM - Re: New engine and prop... long... (Doug Gray)
     2. 03:23 AM - Re: WD-421 Aileron Bellcrank bushing (Jim Sears)
     3. 03:39 AM - Blue Mountain EFIS for sale on ebay (Kirk Hammersmith)
     4. 04:31 AM - Re: Blue Mountain EFIS for sale on ebay (Mickey Coggins)
     5. 05:56 AM - Re: WD-421 Aileron Bellcrank bushing (cgalley)
     6. 06:06 AM - Bahamas trip in November? (Garrett, Randy L (C4S))
     7. 06:29 AM - Re: RV7A Rudder... (George Neal E Capt AU/PC)
     8. 06:35 AM - RV10 (Ron Walker)
     9. 07:02 AM - Re: Bahamas trip in November? (Stewart, Michael (ISS Atlanta))
    10. 07:34 AM - Hotel room available for OSH (David Grover)
    11. 08:38 AM - Need help with brake lines (Jason Sneed)
    12. 09:50 AM - Re: RV10 (Jim Sears)
    13. 10:02 AM - Re: WD-421 Aileron Bellcrank bushing (Jim Sears)
    14. 10:04 AM - Paint Inquiry (rebibb@comcast.net)
    15. 11:21 AM - Re: WD-421 Aileron Bellcrank bushing (JusCash@aol.com)
    16. 12:06 PM - Re: Need help with brake lines (Tim Bryan)
    17. 12:59 PM - Re: WD-421 Aileron Bellcrank bushing (Dean)
    18. 01:32 PM - Avionics shop in New England? (Garrett, Randy L (C4S))
    19. 01:47 PM - Re: Pressure Trivia (was carrying pressurized cylinders) (Sebastian Trost)
    20. 04:28 PM - Re: Need help with brake lines (Mike Robertson)
    21. 04:33 PM - Camping in Vintage Camping in Oshkosh (Gert)
    22. 05:24 PM - Re: Pressure Trivia (was carrying pressurized cylinders) (Tedd McHenry)
    23. 06:01 PM - Fw: Firewall access through oil filler door (Ralph E. Capen)
    24. 06:25 PM - Re: Need help with brake lines (N223RV@aol.com)
    25. 06:51 PM - Re: Fw: Firewall access through oil filler door (linn walters)
    26. 07:07 PM - Re: Fw: Firewall access through oil filler door (Jeff Point)
    27. 07:46 PM - Re: Fw: Firewall access through oil filler door (Laird Owens)
    28. 09:15 PM - Re: Fw: Firewall access through oil filler door (Harvey Sigmon)
    29. 10:20 PM - Tach & Tune and Bank for sale (Jim Anglin)
    30. 11:31 PM - Re: Fw: Firewall access through oil filler door (Vanremog@aol.com)
 
 
 


Message 1


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    Time: 03:07:30 AM PST US
    From: Doug Gray <dgra1233@bigpond.net.au>
    Subject: Re: New engine and prop... long...
    --> RV-List message posted by: Doug Gray <dgra1233@bigpond.net.au> Yes, I say fuel up and go take some more measurements.... do not archive.. Dave Bristol wrote: > --> RV-List message posted by: Dave Bristol <bj034@lafn.org> > > Doug and Kevin, > > It seems to me that since GPS does not give "heading" information, that > data would have had to come from the DG or compass, both of which are a > little suspect accuracy wise. So I would think it more prudent to make > another test flight and get the "track" data from the GPS. Or maybe I'm > missing something? : > ) > > Thanks for a another great tool and all the really usable info you guys > give us on a regular basis! > > Dave Bristol > > > Doug Gray wrote: > > >>--> RV-List message posted by: Doug Gray <dgra1233@bigpond.net.au> >> >>Kevin, >> >>I agree, why not eliminate the error if we can. A GPS and the simple >>calculation provides a remarkably precise tool to make real performance >>assessment. >> >>To make use of Heading rather than the GPS track data the solution is to >>create a new cell that is the sum of the squares of the differences >>between the spreadsheet's Heading output cells and the actual headings >>recorded. >> >>Then, use the 'solver' tool to minimise this cell (ie zero since it is >>the sum of squares) while varying the three track input fields. >> >>It is a bit messy, but has rescued more than one flight data set. >> >>Note.. I believe some GPS manufacturers label the 'Track' data field as >>'Heading'. This does not help. >> >> >> >> >> > > > > > > > >


    Message 2


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    Time: 03:23:26 AM PST US
    From: Jim Sears <sears@searnet.com>
    Subject: Re: WD-421 Aileron Bellcrank bushing
    --> RV-List message posted by: Jim Sears <sears@searnet.com> > You're gonna want to replace that bolt you sanded ASAP! You most likely > removed the cad plating, and the bolt can now rust. The intent is not for > the bushing to rotate around the bolt -- rather the bellcrank rotates around > the bushing. To make this perfectly clear...the bolt & bushing should > remain STATIONARY with respect to the plane and each other. This is the > case for aileron bellcranks, control stick pivots, etc. > > (Note: I'm speaking in terms of RV-7 and RV-8 wings only...I can't speak for > the design on other models, but I presume they're similar.) Dan is correct; but, my controls don't work that way. When I was building Scooter, I approached my local A&Ps with IAs and discussed how the assembly is to be built. I could build it as Dan stated; or, I could build it making the bushing stationary and let it rotate about the bolt. The latter was the preferred method, by general concensus amongst us. The reason being is to let the bolt wear out before the assembly. It's easier to replace the bolt than it is to replace the weldment, if that still exists when the weldment wears out. Granted, we could be talking about years from now; but, I still liked the idea of replacing a bolt rather than the assembly. I installed my bushing with a very tight fit and let the bolt rotate within it. I also changed out the bolts so that I could use castellated nuts and cotter pins. I also installed washers at each end of the bushing for friction relief. So far, it's working quite well. I keep the bolt lubed with LPS-2, each year. There's very little friction there; so, the bolt should last well into this century. If not, I'll buy a bushing and bolt instead of an assembly. Much cheaper to fix, that way. Although I'm not advocating anyone's changing the way they're doing their assembly, I just wanted you to know that there is another way to approach the problem. I'm sure the cad plating is already gone on my bolts because of the rotation. I'm not planning on replacing them anytime soon, though. I'm also going to use the same method on my new -7A because it seems like the right thing to do for me. Now, to the original question. When the rubbing occurs, is the bolt tightened down or loose? I'm betting the bolts are straight. You could do a roll test on a very flat surface and watch for light under them as you roll them. A bent bolt will have light variances under them as they are rolled. Is it possible that when you tighten down the bolts that you may be bending the bushing ever so slightly? I can remember vaguely that mine did that until I changed my approach to the problem. I can't swear to that, though. It was a very long time ago. Jim Sears in KY RV-6A N198JS (Scooter) RV-7A #70317 (Finishing the tail. Wings awaitin') EAA Technical Counselor EAA Flight Advisor


    Message 3


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    Time: 03:39:48 AM PST US
    From: "Kirk Hammersmith" <kirk@direct2avionics.com>
    Subject: Blue Mountain EFIS for sale on ebay
    --> RV-List message posted by: "Kirk Hammersmith" <kirk@direct2avionics.com> For anyone interested in a BM EFIS or BM EFIS Lite, I came accross this on ebay. http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&rd1&item2485259014&category26436&sspagenameWDVW Kirk


    Message 4


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    Time: 04:31:56 AM PST US
    From: Mickey Coggins <mick-matronics@rv8.ch>
    Subject: Re: Blue Mountain EFIS for sale on ebay
    --> RV-List message posted by: Mickey Coggins <mick-matronics@rv8.ch> The = signs get removed for some reason, probably a Microsoft conspiracy. :-) Try this simplified URL: http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&item=2485259014 or search for item number 2485259014. Mickey >For anyone interested in a BM EFIS or BM EFIS Lite, I came accross this on ebay. > >http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&rd1&item2485259014&category26436&sspagenameWDVW > >Kirk -- Mickey Coggins http://www.rv8.ch/ #82007 QB Wings/Fuselage


    Message 5


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    Time: 05:56:02 AM PST US
    From: "cgalley" <cgalley@qcbc.org>
    Subject: Re: WD-421 Aileron Bellcrank bushing
    --> RV-List message posted by: "cgalley" <cgalley@qcbc.org> Let me take a different approach. When the bushing rotates on the bolt, the bolt assumes all the loadings. When the bushing does not rotate on the bolt, all loadings are taken by the bushing, Since the bushing is larger, it is stronger to let the fitting rotate about the bushing. That is the way Van and many others design pivots so they can use a bolt that is small for lightness but doesn't have the critical strength necessary. Cy Galley - Chair, Emergency Aircraft Repair Safety Programs Editor - TC EAA Sport Pilot ----- Original Message ----- From: "Jim Sears" <sears@searnet.com> Subject: Re: RV-List: WD-421 Aileron Bellcrank bushing > --> RV-List message posted by: Jim Sears <sears@searnet.com> > > > > You're gonna want to replace that bolt you sanded ASAP! You most likely > > removed the cad plating, and the bolt can now rust. The intent is not for > > the bushing to rotate around the bolt -- rather the bellcrank rotates > around > > the bushing. To make this perfectly clear...the bolt & bushing should > > remain STATIONARY with respect to the plane and each other. This is the > > case for aileron bellcranks, control stick pivots, etc. > > > > (Note: I'm speaking in terms of RV-7 and RV-8 wings only...I can't speak > for > > the design on other models, but I presume they're similar.) > > Dan is correct; but, my controls don't work that way. When I was building > Scooter, I approached my local A&Ps with IAs and discussed how the assembly > is to be built. I could build it as Dan stated; or, I could build it making > the bushing stationary and let it rotate about the bolt. The latter was the > preferred method, by general concensus amongst us. The reason being is to > let the bolt wear out before the assembly. It's easier to replace the bolt > than it is to replace the weldment, if that still exists when the weldment > wears out. Granted, we could be talking about years from now; but, I still > liked the idea of replacing a bolt rather than the assembly. I installed my > bushing with a very tight fit and let the bolt rotate within it. I also > changed out the bolts so that I could use castellated nuts and cotter pins. > I also installed washers at each end of the bushing for friction relief. So > far, it's working quite well. I keep the bolt lubed with LPS-2, each year. > There's very little friction there; so, the bolt should last well into this > century. If not, I'll buy a bushing and bolt instead of an assembly. Much > cheaper to fix, that way. > > Although I'm not advocating anyone's changing the way they're doing their > assembly, I just wanted you to know that there is another way to approach > the problem. I'm sure the cad plating is already gone on my bolts because > of the rotation. I'm not planning on replacing them anytime soon, though. > I'm also going to use the same method on my new -7A because it seems like > the right thing to do for me. > > Now, to the original question. When the rubbing occurs, is the bolt > tightened down or loose? I'm betting the bolts are straight. You could do > a roll test on a very flat surface and watch for light under them as you > roll them. A bent bolt will have light variances under them as they are > rolled. Is it possible that when you tighten down the bolts that you may be > bending the bushing ever so slightly? I can remember vaguely that mine did > that until I changed my approach to the problem. I can't swear to that, > though. It was a very long time ago. > > Jim Sears in KY > RV-6A N198JS (Scooter) > RV-7A #70317 (Finishing the tail. Wings awaitin') > EAA Technical Counselor > EAA Flight Advisor > >


    Message 6


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    Time: 06:06:56 AM PST US
    From: "Garrett, Randy L (C4S)" <Randy.L.Garrett@gdc4s.com>
    Subject: Bahamas trip in November?
    --> RV-List message posted by: "Garrett, Randy L (C4S)" <Randy.L.Garrett@gdc4s.com> John King (kingjohn@erols.com) is organizing a trip to the Bahamas in November. John has a Kitfox, but has opened this trip to RV's and other types as well. For a sample of John's excellent trip planning skills (and a really fun read), see http://www.sportflight.com/alaska/ I am planning to go. If anyone else is interested, please contact John by email. Randy RV-6A 380 hours


    Message 7


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    Time: 06:29:22 AM PST US
    From: George Neal E Capt AU/PC <Neal.George@maxwell.af.mil>
    Subject: RV7A Rudder...
    --> RV-List message posted by: George Neal E Capt AU/PC <Neal.George@MAXWELL.AF.MIL> Travis - I haven't yet mounted the bottom rudder tip on my -7; I'm waiting till the tail is mounted to make sure there isn't a gross mismatch in the tailcone-to-rudder intersection. Mine has a line scribed in the gelcoat. A call to Van's confirmed my suspicion that the scribed line is a trim-to mark. If you're burning to cut it now just to have something to do, trim to the scribe mark... Neal George, RV-7 N8ZG (wings) > I am having trouble visualizing what needs to get cut and where to cut it.


    Message 8


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    Time: 06:35:33 AM PST US
    From: "Ron Walker" <ron@walker.net>
    Subject: RV10
    --> RV-List message posted by: "Ron Walker" <ron@walker.net> Got my first look up close at an RV10 under construction. I've seen the factory demo one, but seeing the 'guts' really gives you a better understanding of it. Really sweet lookin even without the skins. These guys had the emp done, QB wings and were working on the fuse. They're really making progress and will have it in the air before ya know it. What *really* impressed me were the new plans! The way the instructions are printed along side of the assembly drawings now on legal size paper bound in a binder ! A very nice layout! They just keep getting better and better! Now if they could go back and retrofit the 7 plans to that format ;o) Wouldn't help me at all ... but there are plenty out there that WOULD benefit ! It was also cool seeing a 6A, 7A, 9A and 10 all in the same hangar space that's not at the Vans factory! Ron N520TX - 41 hrs and out of my Phase 1 prison cell !!!


    Message 9


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    Time: 07:02:41 AM PST US
    Subject: Bahamas trip in November?
    From: "Stewart, Michael (ISS Atlanta)" <mstewart@iss.net>
    --> RV-List message posted by: "Stewart, Michael (ISS Atlanta)" <mstewart@iss.net> Feel free to poke around the site I created for the flight of 15 RV's 3 months ago to the Bahamas and the Turks. It will probably have some useful info for newbees. This site was the central communications tool for the group. It was indeed a trip of a lifetime. Funny thing is we all are interested in headin for Alaska on our next adventure. Enjoy. Mike Stewart http://www.mstewart.net/teamrv/turkscaicos -----Original Message----- From: owner-rv-list-server@matronics.com [mailto:owner-rv-list-server@matronics.com] On Behalf Of Garrett, Randy L (C4S) Subject: RV-List: Bahamas trip in November? --> RV-List message posted by: "Garrett, Randy L (C4S)" <Randy.L.Garrett@gdc4s.com> John King (kingjohn@erols.com) is organizing a trip to the Bahamas in November. John has a Kitfox, but has opened this trip to RV's and other types as well. For a sample of John's excellent trip planning skills (and a really fun read), see http://www.sportflight.com/alaska/ I am planning to go. If anyone else is interested, please contact John by email. Randy RV-6A 380 hours == == == ==


    Message 10


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    Time: 07:34:16 AM PST US
    From: "David Grover" <grover@ev1.net>
    Subject: Hotel room available for OSH
    --> RV-List message posted by: "David Grover" <grover@ev1.net> I have reservation for a room at the Best Western in Ripon starting July 28 - Aug. 1st. that I am not going to be able to use. If anyone is interested in any or all of the days in the block that I have reserved please contact me off the list. David Grover grover@ev1.net


    Message 11


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    Time: 08:38:12 AM PST US
    From: Jason Sneed <n242ds@cox.net>
    Subject: Need help with brake lines
    --> RV-List message posted by: Jason Sneed <n242ds@cox.net> I have an RV-6 and I have had numerous problems with my brake lines. The builder used what looks like plastic (poly) brake lines down the gear leg fairing to the caliper. A couple times the caliper heated up and melted the plastic tube at the fitting and I lost all my fluid. Yesterday I did a fast no flap landing and my right brake pedal was very stiff after landing (probably due to the brake fluid being VERY hot) once stopped I mashed the brake and POP. At the very top of the gear leg fairing I have a pin hole in the plastic which leaked the fluid. I am getting pretty good at landing on a 2000 foot strip with no brakes but I do not think this is a good thing to brag about. Obviously I have to get rid of the plastic hose on both sides my questions are: 1. What type of hose to use? 2. I have woods stiffeners on my gear legs wrapped in glass, do I need to remove this to install the brake line? 3. Do I need to order pre-made hoses or can I make my own? 4. Is aluminum tubbing better that steel braided? or is there something better? 5. my brake lines basically are in the middle of the wood stiffeners. Any help would be great... Thanks, Jason Sneed Commercial Lending Officer First National Bank and Trust www.highland-parks.com/n242ds


    Message 12


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    Time: 09:50:05 AM PST US
    From: Jim Sears <sears@searnet.com>
    Subject: Re: RV10
    --> RV-List message posted by: Jim Sears <sears@searnet.com> > What *really* impressed me were the new plans! The way the instructions are > printed along side of the assembly drawings now on legal size paper bound in > a binder ! A very nice layout! They just keep getting better and better! Now > if they could go back and retrofit the 7 plans to that format ;o) Wouldn't > help me at all ... but there are plenty out there that WOULD benefit ! Like Ron, I do like the way they did it; but, I can attest to seeing some instructions that really need to be edited to make sense. A friend showed me one that I must have read at least three or four times and still didn't get much sense out of. As Dana says, we've become assemblers. :-) Even with some of the minor problems I'm having with the -7A, it sure beats all of the trial fitting I had to do with the -6A. Not having the mark and drill holes is nice, as well. Jim Sears in KY


    Message 13


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    Time: 10:02:31 AM PST US
    From: Jim Sears <sears@searnet.com>
    Subject: Re: WD-421 Aileron Bellcrank bushing
    --> RV-List message posted by: Jim Sears <sears@searnet.com> > Let me take a different approach. When the bushing rotates on the bolt, the > bolt assumes all the loadings. When the bushing does not rotate on the bolt, > all loadings are taken by the bushing, Since the bushing is larger, it is > stronger to let the fitting rotate about the bushing. That is the way Van > and many others design pivots so they can use a bolt that is small for > lightness but doesn't have the critical strength necessary. That's a good observation; but, it seems to me that the loads, which haven't been very heavy in my RV, would be in shear. If that's the case, wouldn't the shear loads be carried by the bolt, no matter how big or small it is and which of the two methods is used? I'm no engineer; so, I can't swear to it. I just know the method I used was the preferred method when I talked with my IA buddies. It made sense then and still does. I think we talked about shear, as well. It's been a long while ago, though. With the bolt rotating in the bushing, one might want to check the bolt for wear more often than when the assembly is rotating around the bushing. I don't think it rotates all that much, though. Unless one is beating the heck out of the end points of the stick throws, there is very little force on those bolts. Just how much force is required when one is flying by barely touching the stick with the fingertips? Even when the loads are heavier in the pattern, they aren't very much because we trim that out. Under aerobatic loads, one might see things load up a bit. Since I'm a big chicken, I've not experienced those loads in Scooter. :-) Jim Sears in KY RV-6A N198JS (Scooter)


    Message 14


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    Time: 10:04:59 AM PST US
    From: rebibb@comcast.net
    Subject: Paint Inquiry
    0.5 MIME_BOUND_NEXTPART Spam tool pattern in MIME boundary --> RV-List message posted by: rebibb@comcast.net Has anyone ever used National Paint Industries Uraglow Polyurethane Enamel? I'm thinkking using it on my RV and wanted to see if anyone has ever used or seen it being used. Thanks Has anyone ever used National Paint Industries Uraglow Polyurethane Enamel? I'm thinkking using it on my RV and wanted to see if anyone has ever used or seen it being used. Thanks


    Message 15


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    Time: 11:21:01 AM PST US
    From: JusCash@aol.com
    Subject: Re: WD-421 Aileron Bellcrank bushing
    --> RV-List message posted by: JusCash@aol.com Thanks Cy, that was the explanation I was going to send. The reason you gave was hashed out on the list a few years ago. Cash Copeland A&P RV-6 N46FC Hayward, Ca In a message dated 7/22/2004 5:57:11 AM Pacific Daylight Time, cgalley@qcbc.org writes: --> RV-List message posted by: "cgalley" <cgalley@qcbc.org> Let me take a different approach. When the bushing rotates on the bolt, the bolt assumes all the loadings. When the bushing does not rotate on the bolt, all loadings are taken by the bushing, Since the bushing is larger, it is stronger to let the fitting rotate about the bushing. That is the way Van and many others design pivots so they can use a bolt that is small for lightness but doesn't have the critical strength necessary. Cy Galley - Chair, Emergency Aircraft Repair Safety Programs Editor - TC EAA Sport Pilot ----- Original Message ----- From: "Jim Sears" <sears@searnet.com> Subject: Re: RV-List: WD-421 Aileron Bellcrank bushing > --> RV-List message posted by: Jim Sears <sears@searnet.com> > > > > You're gonna want to replace that bolt you sanded ASAP! You most likely > > removed the cad plating, and the bolt can now rust. The intent is not for > > the bushing to rotate around the bolt -- rather the bellcrank rotates > around > > the bushing. To make this perfectly clear...the bolt & bushing should > > remain STATIONARY with respect to the plane and each other. This is the > > case for aileron bellcranks, control stick pivots, etc. > > > > (Note: I'm speaking in terms of RV-7 and RV-8 wings only...I can't speak > for > > the design on other models, but I presume they're similar.) > > Dan is correct; but, my controls don't work that way. When I was building > Scooter, I approached my local A&Ps with IAs and discussed how the assembly > is to be built. I could build it as Dan stated; or, I could build it making > the bushing stationary and let it rotate about the bolt. The latter was the > preferred method, by general concensus amongst us. The reason being is to > let the bolt wear out before the assembly. It's easier to replace the bolt > than it is to replace the weldment, if that still exists when the weldment > wears out. Granted, we could be talking about years from now; but, I still > liked the idea of replacing a bolt rather than the assembly. I installed my > bushing with a very tight fit and let the bolt rotate within it. I also > changed out the bolts so that I could use castellated nuts and cotter pins. > I also installed washers at each end of the bushing for friction relief. So > far, it's working quite well. I keep the bolt lubed with LPS-2, each year. > There's very little friction there; so, the bolt should last well into this > century. If not, I'll buy a bushing and bolt instead of an assembly. Much > cheaper to fix, that way. > > Although I'm not advocating anyone's changing the way they're doing their > assembly, I just wanted you to know that there is another way to approach > the problem. I'm sure the cad plating is already gone on my bolts because > of the rotation. I'm not planning on replacing them anytime soon, though. > I'm also going to use the same method on my new -7A because it seems like > the right thing to do for me. > > Now, to the original question. When the rubbing occurs, is the bolt > tightened down or loose? I'm betting the bolts are straight. You could do > a roll test on a very flat surface and watch for light under them as you > roll them. A bent bolt will have light variances under them as they are > rolled. Is it possible that when you tighten down the bolts that you may be > bending the bushing ever so slightly? I can remember vaguely that mine did > that until I changed my approach to the problem. I can't swear to that, > though. It was a very long time ago. > > Jim Sears in KY > RV-6A N198JS (Scooter) > RV-7A #70317 (Finishing the tail. Wings awaitin') > EAA Technical Counselor > EAA Flight Advisor > >


    Message 16


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    Time: 12:06:19 PM PST US
    From: "Tim Bryan" <rv6flyer@improvementteam.com>
    Subject: Re: Need help with brake lines
    --> RV-List message posted by: "Tim Bryan" <rv6flyer@improvementteam.com> Jason, The plans call for soft aluminum tubing to the brakes from the firewall area You may be able to just replace a small section near and connecting to the brake caliper to eliminate the heat. Tim Bryan RV-6 N616TB -------Original Message------- From: rv-list@matronics.com Subject: RV-List: Need help with brake lines --> RV-List message posted by: Jason Sneed <n242ds@cox.net> I have an RV-6 and I have had numerous problems with my brake lines. The builder used what looks like plastic (poly) brake lines down the gear leg fairing to the caliper. A couple times the caliper heated up and melted the plastic tube at the fitting and I lost all my fluid. Yesterday I did a fast no flap landing and my right brake pedal was very stiff after landing (probably due to the brake fluid being VERY hot) once stopped I mashed the brake and POP. At the very top of the gear leg fairing I have a pin hole in the plastic which leaked the fluid. I am getting pretty good at landing on a 2000 foot strip with no brakes but I do not think this is a good thing to brag about. Obviously I have to get rid of the plastic hose on both sides my questions are: 1. What type of hose to use? 2. I have woods stiffeners on my gear legs wrapped in glass, do I need to remove this to install the brake line? 3. Do I need to order pre-made hoses or can I make my own? 4. Is aluminum tubbing better that steel braided? or is there something better? 5. my brake lines basically are in the middle of the wood stiffeners. Any help would be great... Thanks, Jason Sneed Commercial Lending Officer First National Bank and Trust www.highland-parks.com/n242ds


    Message 17


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    Time: 12:59:44 PM PST US
    From: "Dean" <dvanwinkle@royell.net>
    Subject: Re: WD-421 Aileron Bellcrank bushing
    --> RV-List message posted by: "Dean" <dvanwinkle@royell.net> Jim and Others Van's bellcrank designs, at least in the RV-9/9A, is that the bushing is slightly longer than the bellcrank tube so that the bellcrank rotates about the captured bushing. By design, the bolt is more than adequate to take out any induced shear loads. The only contribution that the bushing could make against shear loads would be slight from the clamping friction at each end supplied by the bolt pressure. The bushing is the sacrificial material in the rotating joint. The wear rate on the OD of the bushing will be less than it would be on the ID due to the larger surface area and lower unit surface pressures involved. This design allows for easy bushing replacement and precludes bolt rotation that could enlarge holes in the support brackets. Hope this adds a little clarity to the situation. Dean Van Winkle RV-9A Fuselage/Finish ----- Original Message ----- From: "Jim Sears" <sears@searnet.com> Subject: Re: RV-List: WD-421 Aileron Bellcrank bushing > --> RV-List message posted by: Jim Sears <sears@searnet.com> > > > > Let me take a different approach. When the bushing rotates on the bolt, > the > > bolt assumes all the loadings. When the bushing does not rotate on the > bolt, > > all loadings are taken by the bushing, Since the bushing is larger, it is > > stronger to let the fitting rotate about the bushing. That is the way Van > > and many others design pivots so they can use a bolt that is small for > > lightness but doesn't have the critical strength necessary. > > That's a good observation; but, it seems to me that the loads, which haven't > been very heavy in my RV, would be in shear. If that's the case, wouldn't > the shear loads be carried by the bolt, no matter how big or small it is and > which of the two methods is used? I'm no engineer; so, I can't swear to it. > I just know the method I used was the preferred method when I talked with my > IA buddies. It made sense then and still does. I think we talked about > shear, as well. It's been a long while ago, though. With the bolt rotating > in the bushing, one might want to check the bolt for wear more often than > when the assembly is rotating around the bushing. I don't think it rotates > all that much, though. Unless one is beating the heck out of the end points > of the stick throws, there is very little force on those bolts. Just how > much force is required when one is flying by barely touching the stick with > the fingertips? Even when the loads are heavier in the pattern, they > aren't very much because we trim that out. Under aerobatic loads, one might > see things load up a bit. Since I'm a big chicken, I've not experienced > those loads in Scooter. :-) > > Jim Sears in KY > RV-6A N198JS (Scooter) > >


    Message 18


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    Time: 01:32:53 PM PST US
    From: "Garrett, Randy L (C4S)" <Randy.L.Garrett@gdc4s.com>
    Subject: Avionics shop in New England?
    --> RV-List message posted by: "Garrett, Randy L (C4S)" <Randy.L.Garrett@gdc4s.com> It's time for me to get my biennial transponder check. Is there an avionics shop in the Boston / Providence area that anyone particularly recommends? Thanks, Randy RV-6A 380 hours


    Message 19


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    Time: 01:47:19 PM PST US
    Subject: Re: Pressure Trivia (was carrying pressurized cylinders)
    From: Sebastian Trost <sebastian.trost@sbcglobal.net>
    --> RV-List message posted by: Sebastian Trost <sebastian.trost@sbcglobal.net> I don't know what airliner you were flying, but the Boeing 737 baggage compartment is pressurized, as I think all other jets are. You do get to 8000' cabin altitude, which I have had pop open sunscreen tubes, but you get to the same altitude sitting in the cabin. That's why passengers with a head cold have ear pain on descent... Sebastian Trost RV-7A QB Tipup Just got finish kit Working on rollover bar


    Message 20


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    Time: 04:28:47 PM PST US
    From: "Mike Robertson" <mrobert569@hotmail.com>
    Subject: Need help with brake lines
    --> RV-List message posted by: "Mike Robertson" <mrobert569@hotmail.com> Jason, On all the current aircraft the brake lines from the fuselage to the brake calipers are aluminum. You may be able to snake the alum line through as you pull the poly line out from your gear legs. Mike Robertson >From: Jason Sneed <n242ds@cox.net> >Reply-To: rv-list@matronics.com >To: rv-list@matronics.com >Subject: RV-List: Need help with brake lines >Date: Thu, 22 Jul 2004 10:34:30 -0500 > >--> RV-List message posted by: Jason Sneed <n242ds@cox.net> > >I have an RV-6 and I have had numerous problems with my brake lines. >The builder used what looks like plastic (poly) brake lines down the >gear leg fairing to the caliper. A couple times the caliper heated up >and melted the plastic tube at the fitting and I lost all my fluid. >Yesterday I did a fast no flap landing and my right brake pedal was >very stiff after landing (probably due to the brake fluid being VERY >hot) once stopped I mashed the brake and POP. At the very top of the >gear leg fairing I have a pin hole in the plastic which leaked the >fluid. I am getting pretty good at landing on a 2000 foot strip with no >brakes but I do not think this is a good thing to brag about. > >Obviously I have to get rid of the plastic hose on both sides my >questions are: > >1. What type of hose to use? >2. I have woods stiffeners on my gear legs wrapped in glass, do I need >to remove this to install the brake line? >3. Do I need to order pre-made hoses or can I make my own? >4. Is aluminum tubbing better that steel braided? or is there something >better? >5. my brake lines basically are in the middle of the wood stiffeners. > >Any help would be great... > >Thanks, > >Jason Sneed >Commercial Lending Officer >First National Bank and Trust >www.highland-parks.com/n242ds > > Dont just search. Find. Check out the new MSN Search! http://search.msn.click-url.com/go/onm00200636ave/direct/01/


    Message 21


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    Time: 04:33:58 PM PST US
    From: Gert <gert@execpc.com>
    Subject: Camping in Vintage Camping in Oshkosh
    --> RV-List message posted by: Gert <gert@execpc.com> This is a heads up for all who would like to continue camping in the ORIGINAL showplane camping area by vintage planes. Antique/classic/vintage has informed us that as a general rule only vintage airplanes can camp in that area. homebuilds will have to go to the *NEW* homebuild area, west of the RV parking area. only *pre-approved* non-vintage airplanes will be allowed. At least that is what we, the 'north-point crew' have een told. Ya'all read my buddy Jeff's article in the RVator on signs, signals, etc. If not, please do. If you do NOT have a readable sign, and sticky notes in pencil behind the colored canopy do not count as a sign, count on being stopped at about *every* intersection. For those who are 'old timers' and have parked in the rv area before, know that the taxiway leading up to the RV area and now the new homebuilt/showplane camping is only a ONE_WAY taxiway. This means that if traffic is en-route on the taxi way we have to not only hold you but also *STAGE* you at the entry to the warbird area. This to prevent a mexican stand-off at the intersection with Papa 1. Read about the EAA PECKING ORDER in the RVator. Please, please, when we direct you in the throat of the warbird area by the trimoter, turn into the throat and make a 180 degree turn so you face south again. Unless you fly in nigerian warbird RV6 colors you won't be welcome in warbirds. Hopefully we will be able to accomoate you as soon as possible. Gert p.s. Did I mention yet to bring yer 8x11 sign..facing the orange vests...the one in the NOTAMs....For several years now, the FAA folks have joked with us about starting NOTAM checks, let's hope it stays a joke. Last year one of them stood at north point doing an informal count of lack of signs.....he left shaking his head in despair....I have seen the feds follow at least 2 airplanes to their parking spots for gross neglect of following hand signals, almost running over an orange vest in each instance did not help their course..., neither airplane was an RV of course, but....have a copy in the airplane.....ya never know... -- -- is subject to a download and archival fee in the amount of $500


    Message 22


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    Time: 05:24:36 PM PST US
    From: Tedd McHenry <tedd@vansairforce.org>
    Subject: Re: Pressure Trivia (was carrying pressurized cylinders)
    --> RV-List message posted by: Tedd McHenry <tedd@vansairforce.org> Sebastian: > I don't know what airliner you were flying, but the Boeing 737 baggage > compartment is pressurized, as I think all other jets are. It was a Canadair CT-114 trainer, and the baggage compartment (a glovebox-sized thing in the wing root) was definitely not pressurized. Tedd McHenry Surrey, BC, Canada DO NOT ARCHIVE


    Message 23


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    Time: 06:01:17 PM PST US
    From: "Ralph E. Capen" <recapen@earthlink.net>
    Subject: Fw: Firewall access through oil filler door
    --> RV-List message posted by: "Ralph E. Capen" <recapen@earthlink.net> Fellow listers, I'm thinking about mounting a battery charger connector on my firewall so that I can keep my battery charged as my AM/FM radio draws some current to keep the stations/clock.... I'm trying to determine what area on the firewall can be reached through the oil filler door so I can mount this thing before I close the forward top skin and work on my canopy Does anyone have a general idea of what can be reached? I'm hoping for an area above and to the right/left of where Van's firewall forward instructions tell you to put the brake fluid reservior. Thanks, Ralph Capen RV6AQB - N822AR on the gear - engine's real soon


    Message 24


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    Time: 06:25:20 PM PST US
    From: N223RV@aol.com
    Subject: Re: Need help with brake lines
    --> RV-List message posted by: N223RV@aol.com Go to Pegasus racing, they have some an4 stainless steel braided hose and fittings. Very easy to assemble and very flexible. E-mail me offline if you can't find the part numbers and I'll get the catalog from the hanger this weekend. -Mike Kraus N223RV RV-4 Flying N213RV RV-10 Empennage complete, working on Tailcone


    Message 25


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    Time: 06:51:06 PM PST US
    From: linn walters <lwalters2@cfl.rr.com>
    Subject: Re: Fw: Firewall access through oil filler door
    --> RV-List message posted by: linn walters <lwalters2@cfl.rr.com> Ralph E. Capen wrote: >--> RV-List message posted by: "Ralph E. Capen" <recapen@earthlink.net> > >Fellow listers, > >I'm thinking about mounting a battery charger connector on my firewall so that I can keep my battery charged as my AM/FM radio draws some current to keep the stations/clock.... > >I'm trying to determine what area on the firewall can be reached through the oil filler door so I can mount this thing before I close the forward top skin and work on my canopy > >Does anyone have a general idea of what can be reached? I'm hoping for an area above and to the right/left of where Van's firewall forward instructions tell you to put the brake fluid reservior. > >Thanks, >Ralph Capen >RV6AQB - N822AR on the gear - engine's real soon > Great idea Ralph, but instead of mounting it to the firewall, why not attach a pigtail to the engine mount with a ty-rap or some other type of clip? That way it would be easily accessible and the open oil door would vent the heat after a flight. Radio Shack has some nice molex polarized 2-pin connectors that are just made to order for this job. Just use the molex crimping tool. Linn > > > >


    Message 26


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    Time: 07:07:18 PM PST US
    From: Jeff Point <jpoint@mindspring.com>
    Subject: Re: Fw: Firewall access through oil filler door
    --> RV-List message posted by: Jeff Point <jpoint@mindspring.com> A 2-prong extension cord works well in this application too. The female end gets cut off and attached to the battery, and tie-wrapped to the mount. The male end can be used to connect to the charger with whatever kind of connector is called for. The male end/ charger adapter is part of my emergency tool kit. Jeff Point RV-6 Milwaukee WI >Great idea Ralph, but instead of mounting it to the firewall, why not >attach a pigtail to the engine mount with a ty-rap or some other type of >clip? That way it would be easily accessible and the open oil door >would vent the heat after a flight. Radio Shack has some nice molex >polarized 2-pin connectors that are just made to order for this job. >Just use the molex crimping tool. >Linn > > > >> >> >> >> > > > >


    Message 27


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    Time: 07:46:11 PM PST US
    From: Laird Owens <owens@aerovironment.com>
    Subject: Re: Fw: Firewall access through oil filler door
    --> RV-List message posted by: Laird Owens <owens@aerovironment.com> Ralph, I wanted to be able to do the same, but came up with a different way to do than putting it on the firewall. I have a 12V receptacle in the cockpit that's hooked straight to the E bus, which comes straight off the battery. I made an adapter from the male 12V plug for the battery tender. Works great to keep the battery topped off. YMMV, Laird RV-6 950 hrs SoCal On Jul 22, 2004, at 6:54 PM, linn walters wrote: > --> RV-List message posted by: linn walters <lwalters2@cfl.rr.com> > > Ralph E. Capen wrote: > >> --> RV-List message posted by: "Ralph E. Capen" >> <recapen@earthlink.net> >> >> Fellow listers, >> >> I'm thinking about mounting a battery charger connector on my >> firewall so that I can keep my battery charged as my AM/FM radio >> draws some current to keep the stations/clock.... >> >> I'm trying to determine what area on the firewall can be reached >> through the oil filler door so I can mount this thing before I close >> the forward top skin and work on my canopy >> >> Does anyone have a general idea of what can be reached? I'm hoping >> for an area above and to the right/left of where Van's firewall >> forward instructions tell you to put the brake fluid reservior. >> >> Thanks, >> Ralph Capen >> RV6AQB - N822AR on the gear - engine's real soon


    Message 28


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    Time: 09:15:28 PM PST US
    From: "Harvey Sigmon" <rv6hes@comcast.net>
    Subject: Re: Fw: Firewall access through oil filler door
    --> RV-List message posted by: "Harvey Sigmon" <rv6hes@comcast.net> Ralph: On my RV-6A I installed a external power receptacle system inside the oil door. What I did was at my airplane junkyard I removed the whole external power system from a piper Cherokee. Inside the door aft on the engine mount V I mounted the Receptacle Socket and on the opposite side of the firewall I mounted the relay to control the power. And the power feeds through the firewall to the battery bus. Inside the oil door I have a switch to control the external power Relay. I also carry with my tools a jumper cord to start the engine if the battery might be dead. I think Electric Bob has an schematic idea of how to do this, Works fine. Harvey Sigmon RV-6A N602RV ----- Original Message ----- From: "Ralph E. Capen" <recapen@earthlink.net> Subject: RV-List: Fw: Firewall access through oil filler door > --> RV-List message posted by: "Ralph E. Capen" <recapen@earthlink.net> > > Fellow listers, > > I'm thinking about mounting a battery charger connector on my firewall so that I can keep my battery charged as my AM/FM radio draws some current to keep the stations/clock.... > > I'm trying to determine what area on the firewall can be reached through the oil filler door so I can mount this thing before I close the forward top skin and work on my canopy > > Does anyone have a general idea of what can be reached? I'm hoping for an area above and to the right/left of where Van's firewall forward instructions tell you to put the brake fluid reservior. > > Thanks, > Ralph Capen > RV6AQB - N822AR on the gear - engine's real soon > >


    Message 29


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    Time: 10:20:35 PM PST US
    From: "Jim Anglin" <jlanglin44@earthlink.net>
    Subject: Tach & Tune and Bank for sale
    --> RV-List message posted by: "Jim Anglin" <jlanglin44@earthlink.net> I have in excellent condition a used Mitchell tach with 27" cable and a Bendix Turn and Bank that hasn't been used since I got this -4. I am getting rid of them because my tach drive seal is leaking and I don't want to tear the engine apart to fix it so I went with electric. I don't want to put on a vac. pump so the T & B has got to go. I can email pictures. Jim


    Message 30


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    Time: 11:31:22 PM PST US
    From: Vanremog@aol.com
    Subject: Re: Fw: Firewall access through oil filler door
    --> RV-List message posted by: Vanremog@aol.com In a message dated 7/22/2004 7:46:57 PM Pacific Daylight Time, owens@aerovironment.com writes: I have a 12V receptacle in the cockpit that's hooked straight to the E bus, which comes straight off the battery. I made an adapter from the male 12V plug for the battery tender. Works great to keep the battery topped off. ===================================== Also good for charging the cell phone overnight while airplane camping. Always connect your 12V receptacle (lighter socket) thru a circuit breaker (or fuse) directly to the battery bus and it can do double duty unattended. GV (RV-6A N1GV O-360-A1A C/S, flying 708 hrs)




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