RV10-List Digest Archive

Mon 11/27/06


Total Messages Posted: 53



Today's Message Index:
----------------------
 
     0. 12:37 AM - List of Contributors Coming Soon - Make Sure You're Listed! (Matt Dralle)
     1. 12:26 AM - Flowscan installation (McGANN, Ron)
     2. 12:33 AM - Re: Low Left Door Problem (Chris , Susie Darcy)
     3. 12:40 AM - Re: wheel bearings (Chris , Susie Darcy)
     4. 03:39 AM - Re: insurance (Russell Daves)
     5. 04:17 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (Link McGarity)
     6. 04:57 AM - Re: Updating numbers (Indran Chelvanayagam)
     7. 06:02 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (Maule Driver)
     8. 06:06 AM - Re: wheel bearings (Rick)
     9. 06:42 AM - Jack Stand (Jesse Saint)
    10. 07:01 AM - Re: Jack Stand (Rene Felker)
    11. 07:16 AM - Re: RV-10 cabin door locks (Tom Deutsch)
    12. 07:21 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (Brian Douglas)
    13. 07:21 AM - Re: Jack Stand (Rob Kermanj)
    14. 07:24 AM - Re: Jack Stand (Mark Ritter)
    15. 07:47 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (Link McGarity)
    16. 07:49 AM - Re: Jack Stand (Michael Schipper)
    17. 08:09 AM - Re: Jack Stand (Doerr, Ray R [NTK])
    18. 08:13 AM - Re: Jack Stand (Tim Olson)
    19. 08:39 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in (johngoodman)
    20. 08:42 AM - Seatbelts (Niko)
    21. 08:58 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (John W. Cox)
    22. 09:11 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (John Jessen)
    23. 09:22 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (Link McGarity)
    24. 09:34 AM - Re: Jack Stand (Michael Schipper)
    25. 10:16 AM - Re: Wing leading edge questions (RV Builder (Michael Sausen))
    26. 10:22 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (Niko)
    27. 10:37 AM - transponder antenna placement (Chris Johnston)
    28. 10:46 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (John W. Cox)
    29. 10:48 AM - Re: Jack Stand (Michael Schipper)
    30. 10:54 AM - Re: transponder antenna placement (Rick)
    31. 11:10 AM - Re: transponder antenna placement (John Gonzalez)
    32. 11:14 AM - Re: Jack Stand (Jesse Saint)
    33. 11:18 AM - Re: transponder antenna placement (Jesse Saint)
    34. 11:28 AM - Re: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 (MauleDriver)
    35. 11:30 AM - Re: transponder antenna placement (bcondrey)
    36. 11:33 AM - Re: transponder antenna placement (John W. Cox)
    37. 11:39 AM - Re: transponder antenna placement (Chris Johnston)
    38. 11:44 AM - Re: Jack Stand (Kelly McMullen)
    39. 12:10 PM - Re: transponder antenna placement (David McNeill)
    40. 12:18 PM - Re: transponder antenna placement (Tim Olson)
    41. 12:20 PM - Re: transponder antenna placement (Tim Olson)
    42. 12:22 PM - Re: Jack Stand (Tim Olson)
    43. 12:26 PM - Re: transponder antenna placement (Rick)
    44. 12:34 PM - Re: transponder antenna placement (Rick)
    45. 12:59 PM - Re: Re: transponder antenna placement (RV Builder (Michael Sausen))
    46. 01:02 PM - Re: transponder antenna placement (David McNeill)
    47. 01:22 PM - Re: Re: transponder antenna placement (John Gonzalez)
    48. 01:24 PM - Re: transponder antenna placement (Rick)
    49. 01:49 PM - Re: transponder antenna placement (Bill DeRouchey)
    50. 01:49 PM - Re: Re: transponder antenna placement (John W. Cox)
    51. 05:51 PM - truemap and motion m1300 outdoor tablet PC (ivo welch)
    52. 06:45 PM - Re: transponder antenna placement (linn Walters)
 
 
 


Message 0


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    Time: 12:37:08 AM PST US
    From: Matt Dralle <dralle@matronics.com>
    Subject: List of Contributors Coming Soon - Make Sure You're Listed!
    Dear Listers, The List of Contributors (LOC) is just around the corner! On December 1st I post a list of everyone that so generously made a Contribution to support the Lists. Its my way of publicly thanking everyone that took a minute to show their appreciation for the Lists. As a number of people have pointed out in their Contribution comments, the List seems at least as valuable of a building/flying/recreating tool as a typical your magazine subscription! And how interactive is a magazine, after all? :-) Won't you take minute and assure that your name is on the upcoming LOC? Tell others that you appreciate the Lists. Making a Contribution to support the Lists is fast and easy using your Visa, MasterCard, or Paypal account: http://www.matronics.com/contribution Or, by droping a personal check in the mail to: Matronics / Matt Dralle PO Box 347 Livermore CA 94551-0347 USA (Please include your email address on the check!) I would like to thank everyone that has so generously made a Contribution thus far during this year's List Fund Raiser! Remember that its YOUR support that keeps these Lists running and improving! Don't forget to include a little comment about how the Lists have helped you! Thank you! Matt Dralle Matronics Email List Administrator


    Message 1


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    Time: 12:26:19 AM PST US
    Subject: Flowscan installation
    From: "McGANN, Ron" <ron.mcgann@baesystems.com>
    G'day all, I am installing the flowscan sender at the moment. The sender mount holes appear to be sized for an AN4 bolt, while the fuselage attach bracket has nutplates for AN3. What's the go here - remove the mount and install nutplates for AN4, or insert a bushing into the sender? I received zero documentation from GRT on the floscan - is this normal? cheers, Ron 187 finishing


    Message 2


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    Time: 12:33:45 AM PST US
    From: "Chris , Susie Darcy" <VHMUM@bigpond.com>
    Subject: Re: Low Left Door Problem
    Zack I had no problem on either door with my finishing kit about a year old. I think maybe some people might not be putting the bracket on the canopy top far enough inboard??? Not sure otherwise regards Chris 388


    Message 3


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    Time: 12:40:46 AM PST US
    From: "Chris , Susie Darcy" <VHMUM@bigpond.com>
    Subject: Re: wheel bearings
    Main wheels looked greased to me but not the training wheel! Chris 388


    Message 4


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    Time: 03:39:54 AM PST US
    From: "Russell Daves" <dav1111@cox.net>
    Subject: Re: insurance
    In July 2006 I insured with NationAir (underwritten by AIG). $3710.00 for $200,000 hull coverage. I am a 1500+ PVT INST rated pilot with in excess of 300 hours RV-6A time and in excess of 1000+ High Performance time. I hope Bob and Rick get their mutual insurance pool set up and going before my renewal next year. Russ Daves N710RV 75 hours and counting


    Message 5


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    Time: 04:17:15 AM PST US
    From: Link McGarity <wv4i@bellsouth.net>
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 F1010 appears okay. F1012B flange NOT pre drilled/punched. Link McGarity #622 tailcone


    Message 6


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    Time: 04:57:07 AM PST US
    From: "Indran Chelvanayagam" <dc71@netspace.net.au>
    Subject: Updating numbers
    Ken Scott said 660-ish when he showed me around the Van's factory on Wed. Indran _____ From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of John Jessen Sent: Monday, 27 November 2006 10:11 AM Subject: RV10-List: Updating numbers Doing a web site update and repair session. Anyone know what we are up to as far as kits shipped? Someone with a recent delivery, what's your builder number? Thanks, John Jessen #40328 (buildus interruptus time is web site building and repair time) Do not archive


    Message 7


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    Time: 06:02:50 AM PST US
    From: Maule Driver <MauleDriver@nc.rr.com>
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 Thanks for taking the time to give me the big pic. I did go in and read the archives - that helps. Bill Watson - gotta prime! John W. Cox wrote: > >This subject was extensively posted when John Hilger received not one >but three defectively formed items in a row. They (the responses) should >all be in the archive. The posts at that time was "forgetaboutit", sand >it, stop drill it or do the correct action. > >Require that the defective part is replaced with one which is correctly >formed. Vans is great at that. You are the QC on all components >installed. > > > >


    Message 8


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    Time: 06:06:44 AM PST US
    From: Rick <ricksked@earthlink.net>
    Subject: Re: wheel bearings
    Sean, My mains were greased but I repacked them just cuz...peace of mind I guess. The nose wheel was not packed at all. Rick S. 40185


    Message 9


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    Time: 06:42:16 AM PST US
    From: "Jesse Saint" <jesse@itecusa.org>
    Subject: Jack Stand
    Has anybody come up with a good way to jack up the mains on the -10 without taking the axle nut off and using something like Avery sells? For most cases that works fine, but it would be nice to have another good way to do it. Do not archive Jesse Saint I-TEC, Inc. HYPERLINK "mailto:jesse@itecusa.org"jesse@itecusa.org HYPERLINK "http://www.itecusa.org"www.itecusa.org W: 352-465-4545 C: 352-427-0285 -- 4:00 AM


    Message 10


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    Time: 07:01:59 AM PST US
    From: "Rene Felker" <rene@felker.com>
    Subject: Jack Stand
    I saw something on vans air force, it was a bar and cable device. I have not seen it in use, but looked like it would work. Rene' Felker _____ From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Jesse Saint Sent: Monday, November 27, 2006 7:41 AM Subject: RV10-List: Jack Stand Has anybody come up with a good way to jack up the mains on the -10 without taking the axle nut off and using something like Avery sells? For most cases that works fine, but it would be nice to have another good way to do it. Do not archive Jesse Saint I-TEC, Inc. jesse@itecusa.org www.itecusa.org W: 352-465-4545 C: 352-427-0285 -- 11/27/2006 4:00 AM


    Message 11


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    Time: 07:16:17 AM PST US
    Subject: RV-10 cabin door locks
    From: "Tom Deutsch" <deutscht@rhwhotels.com>
    Grump, could you take a photo of your door lock install and post? Tom Deutsch, #40545 finishing ________________________________ From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of GenGrumpy@aol.com Sent: Saturday, November 25, 2006 12:14 PM Subject: RV10-List: RV-10 cabin door locks I used the same type of locks on my doors as Tim Olsen did, except I did not put the lock into the door latch mechanism like Tim did. I simply mounted the lock separately in the bottom of the door with the lock's arm swinging down into a cut out in the door frame rail, very similar to the baggage door lock assy. Seems to work great so far. grumpy #40404 33 hrs towards the 40 hr flyoff!!


    Message 12


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    Time: 07:21:22 AM PST US
    From: "Brian Douglas" <bsponcil@belinblank.org>
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 I have the same problem on both counts. I ground/buffed the crack out of the F-1010 this weekend but have decided that all rationality aside, it's going to drive me crazy to install it like that so I'm just going to pay to have a new one shipped. What's another $30 right? -Brian #40497 Iowa City, IA ----- Original Message ----- From: "MauleDriver" <MauleDriver@nc.rr.com> Sent: Sunday, November 26, 2006 7:12 PM Subject: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 > > During initial assembly of tailcone, I noticed that F-1012B was not > pre-punched for the skin. The plans shows both A & B as pre-punched. It > will be very easy to match drill the bulkhead using the skin punches and > relying on the A bulkhead for alignment. But I am curious whether others > have encountered the same thing. > > I also noticed a very small tear in the thin flange around the central > hole in bulkhead F-1010. It appears to have resulted from the forming of > the flange. It would seem to be subject to enlarging if the area is > stressed. Would a stop hole be called for? Or grinding the tear out? Or > a new part? I will be going to Vans with this. > > Link to photos of tear: > http://www.mykitlog.com/users/display_log.php?user=MauleDriver&project=224&category=0&log=23464&row=4 > > Bill Watson "MauleDriver" > The QB Fuse and Wing arrived last week (9 weeks early) - here we Gooooooo! > > >


    Message 13


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    Time: 07:21:46 AM PST US
    From: Rob Kermanj <flysrv10@gmail.com>
    Subject: Re: Jack Stand
    I use a Harbor Freight 24" bottle jack. I grinded the top of the piston to match an adopter (purchased form van or Avery) to fit the jack. This adopter is 1/2 sphere and screws into the wing tie-down with the eyebolt removed. I had to make a wooden base for the bottle jack for stability. It kinda looks like the jacks you see at FBO repair shops and lifts the wing. Sorry I cannot be much more specific about the adopter. At my age.....memory does not serve me well. If you decide to go this route and need a picture of the adopter, I will happy to supply you with one. do not archive Rob Kermanj On Nov 27, 2006, at 10:00 AM, Rene Felker wrote: > I saw something on vans air force, it was a bar and cable device. > I have not seen it in use, but looked like it would work. > > > Rene' Felker > > From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list- > server@matronics.com] On Behalf Of Jesse Saint > Sent: Monday, November 27, 2006 7:41 AM > To: rv10-list@matronics.com > Subject: RV10-List: Jack Stand > > > Has anybody come up with a good way to jack up the mains on the -10 > without taking the axle nut off and using something like Avery > sells? For most cases that works fine, but it would be nice to > have another good way to do it. > > > Do not archive > > > Jesse Saint > > I-TEC, Inc. > > jesse@itecusa.org > > www.itecusa.org > > W: 352-465-4545 > > C: 352-427-0285 > > > -- > 11/27/2006 4:00 AM > > > www.aeroelectric.com > www.buildersbooks.com > www.kitlog.com > www.homebuilthelp.com > http://www.matronics.com/contribution > http://www.matronics.com/Navigator?RV10-List > > ============================================================ _- > http://www.matronics.com/Navigator?RV10-List_- > =========================================================== >


    Message 14


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    Time: 07:24:41 AM PST US
    From: "Mark Ritter" <mritter509@msn.com>
    Subject: Jack Stand
    Jesse, I borrowed a couple of jack stands from the hangar next door and jacked the wings up at the tie down points. Worked well to get the mains off the ground while fitting the wheel and gear leg fairings. Alex DeDominicis sells a jack for the RV-10. Mark (N410MR) >From: "Jesse Saint" <jesse@itecusa.org> >To: <rv10-list@matronics.com> >Subject: RV10-List: Jack Stand >Date: Mon, 27 Nov 2006 09:41:14 -0500 > >Has anybody come up with a good way to jack up the mains on the -10 without >taking the axle nut off and using something like Avery sells? For most >cases that works fine, but it would be nice to have another good way to do >it. > > >Do not archive > > >Jesse Saint > >I-TEC, Inc. > >HYPERLINK "mailto:jesse@itecusa.org"jesse@itecusa.org > >HYPERLINK "http://www.itecusa.org"www.itecusa.org > >W: 352-465-4545 > >C: 352-427-0285 > > >-- >4:00 AM > _________________________________________________________________ Fixing up the home? Live Search can help


    Message 15


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    Time: 07:47:38 AM PST US
    From: Link McGarity <wv4i@bellsouth.net>
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 Found the F-1010 crack previous discussion and Van's answer. No hits on F-1012B lack of flange holes. Link McGarity #40622 do not archive


    Message 16


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    Time: 07:49:36 AM PST US
    From: Michael Schipper <mike@learningplanet.com>
    Subject: Re: Jack Stand


    Message 17


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    Time: 08:09:37 AM PST US
    Subject: Jack Stand
    From: "Doerr, Ray R [NTK]" <Ray.R.Doerr@sprint.com>
    I just jacked mine up this past weekend to rotate the tires on the rims because the outer tread on the tires was almost completely wore off while the rest of the treads were almost new. I borrowed a set of jack stands that they use for certified birds like Piper Arrows and was going to jack it up using a bolt in the tie down ring, but I was worried that with the span of these on the 10 it may not be able to handle the force. So I used the stands under the center section spars on the fuse with a =BD" board between the jack stands and the center section spars. This worked great. Once the plane is painted I would just make sure to have foam or something on the board to ensure not to scratch the paint. Thank You Ray Doerr 40250 ________________________________ From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Jesse Saint Sent: Monday, November 27, 2006 8:41 AM Subject: RV10-List: Jack Stand Has anybody come up with a good way to jack up the mains on the -10 without taking the axle nut off and using something like Avery sells? For most cases that works fine, but it would be nice to have another good way to do it. Do not archive Jesse Saint I-TEC, Inc. jesse@itecusa.org www.itecusa.org W: 352-465-4545 C: 352-427-0285 -- 11/27/2006 4:00 AM


    Message 18


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    Time: 08:13:03 AM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Re: Jack Stand
    I built these: http://www.myrv10.com/tips/generaltips.html (see about 1/2 way down) If someone's gonna own an RV-10 long term, they may as well prepare by having the tools. Just used them last week so I could replace my brakes, and I swapped the tires on the rims from side to side (keeps the same rotation), but I had to jack up both wheels at the same time. Tim Olson - RV-10 N104CD - Flying do not archive Mark Ritter wrote: > > Jesse, > > I borrowed a couple of jack stands from the hangar next door and jacked > the wings up at the tie down points. Worked well to get the mains off > the ground while fitting the wheel and gear leg fairings. Alex > DeDominicis sells a jack for the RV-10. > > Mark (N410MR) > > > >> From: "Jesse Saint" <jesse@itecusa.org> >> To: <rv10-list@matronics.com> >> Subject: RV10-List: Jack Stand >> Date: Mon, 27 Nov 2006 09:41:14 -0500 >> >> Has anybody come up with a good way to jack up the mains on the -10 >> without >> taking the axle nut off and using something like Avery sells? For most >> cases that works fine, but it would be nice to have another good way >> to do >> it. >> >> >> >> Do not archive >> >> >> >> Jesse Saint >> >> I-TEC, Inc. >> >> HYPERLINK "mailto:jesse@itecusa.org"jesse@itecusa.org >> >> HYPERLINK "http://www.itecusa.org"www.itecusa.org >> >> W: 352-465-4545 >> >> C: 352-427-0285 >> >> >> >> >> -- >> 4:00 AM >> > > _________________________________________________________________ > Fixing up the home? Live Search can help > > > >


    Message 19


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    Time: 08:39:24 AM PST US
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in
    From: "johngoodman" <johngoodman@earthlink.net>
    I happen to be at that exact spot in building, as well. My F-1012B also does not have pre-punched flanges, but it looks easy to match drill. As far as the F-1010 crack, mine has two gaps in the flange of the hole. It appears that it was worked on. I'll check with Vans.... John wv4i(at)bellsouth.net wrote: > Found the F-1010 crack previous discussion and Van's answer. No hits on > F-1012B lack of flange holes. > > Link McGarity > #40622 > > do not archive -------- #40572 Empennage - Starting tailcone. N711JG reserved Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77341#77341


    Message 20


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    Time: 08:42:06 AM PST US
    From: Niko <owl40188@yahoo.com>
    Subject: Seatbelts
    I am getting ready to order my seatbelts from Hooker Harness and I was wond ering what everyone else has been ordering. The standard sport belts or th e airline style ones. Any recommendations?=0A=0Athanks=0ANiko=0A40188


    Message 21


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    Time: 08:58:16 AM PST US
    Subject: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010
    From: "John W. Cox" <johnwcox@pacificnw.com>
    For the rest of you with this repetitive issue. Inspect all formed parts and inform VANS within the prescribed time of receipt. A defective formed part should be replaced at no additional purchase cost to the Builder/Manufacturer. Shipping is another matter. This aircraft has made a 125 million dollar economic impact to worldwide aviation, already. It will only take a few defective parts working in harmony to have a precipitous impact on insurance rates for the remaining builder/manufacturers left with the project. They(VANS) may have to resort to an RMA process and improved QC (internal) process which is good for all concerned. Complacency or willingness to install such parts is not a good thing. Ask your surviving spouses attorney. $30 here, 100 there, if you see all the rejected canopies you begin to get a picture of many builders actually doing a "Receipt Inspection". John Cox the Turbanator #40600 as before DO NOT ARCHIVE for litigation reasons -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Brian Douglas Sent: Monday, November 27, 2006 7:21 AM Subject: Re: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 <bsponcil@belinblank.org> I have the same problem on both counts. I ground/buffed the crack out of the F-1010 this weekend but have decided that all rationality aside, it's going to drive me crazy to install it like that so I'm just going to pay to have a new one shipped. What's another $30 right? -Brian #40497 Iowa City, IA ----- Original Message ----- From: "MauleDriver" <MauleDriver@nc.rr.com> Sent: Sunday, November 26, 2006 7:12 PM Subject: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 > > During initial assembly of tailcone, I noticed that F-1012B was not > pre-punched for the skin. The plans shows both A & B as pre-punched. It > will be very easy to match drill the bulkhead using the skin punches and > relying on the A bulkhead for alignment. But I am curious whether others > have encountered the same thing. > > I also noticed a very small tear in the thin flange around the central > hole in bulkhead F-1010. It appears to have resulted from the forming of > the flange. It would seem to be subject to enlarging if the area is > stressed. Would a stop hole be called for? Or grinding the tear out? Or > a new part? I will be going to Vans with this. > > Link to photos of tear: > http://www.mykitlog.com/users/display_log.php?user=MauleDriver&project=2 24&category=0&log=23464&row=4 > > Bill Watson "MauleDriver" > The QB Fuse and Wing arrived last week (9 weeks early) - here we Gooooooo! > > >


    Message 22


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    Time: 09:11:58 AM PST US
    From: "John Jessen" <jjessen@rcn.com>
    Subject: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 They should replace it for gratis. Give it a try. John Jessen #40328 Do not archive -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Brian Douglas Sent: Monday, November 27, 2006 10:21 AM Subject: Re: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 --> <bsponcil@belinblank.org> I have the same problem on both counts. I ground/buffed the crack out of the F-1010 this weekend but have decided that all rationality aside, it's going to drive me crazy to install it like that so I'm just going to pay to have a new one shipped. What's another $30 right? -Brian #40497 Iowa City, IA ----- Original Message ----- From: "MauleDriver" <MauleDriver@nc.rr.com> Sent: Sunday, November 26, 2006 7:12 PM Subject: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 > > During initial assembly of tailcone, I noticed that F-1012B was not > pre-punched for the skin. The plans shows both A & B as pre-punched. > It will be very easy to match drill the bulkhead using the skin > punches and relying on the A bulkhead for alignment. But I am curious > whether others have encountered the same thing. > > I also noticed a very small tear in the thin flange around the central > hole in bulkhead F-1010. It appears to have resulted from the forming > of the flange. It would seem to be subject to enlarging if the area > is stressed. Would a stop hole be called for? Or grinding the tear > out? Or a new part? I will be going to Vans with this. > > Link to photos of tear: > http://www.mykitlog.com/users/display_log.php?user=MauleDriver&project > =224&category=0&log=23464&row=4 > > Bill Watson "MauleDriver" > The QB Fuse and Wing arrived last week (9 weeks early) - here we Gooooooo! > > > -- 4:00 AM -- 4:00 AM


    Message 23


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    Time: 09:22:42 AM PST US
    From: Link McGarity <wv4i@bellsouth.net>
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 Talked to Van's this am re F-1012B flange. It is intentionally not PRE-drilled/punched so as to accommodate some variance in hole/skin alignment. Link McGarity #40622 tailcone do not archive


    Message 24


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    Time: 09:34:51 AM PST US
    From: Michael Schipper <mike@learningplanet.com>
    Subject: Re: Jack Stand


    Message 25


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    Time: 10:16:07 AM PST US
    Subject: Wing leading edge questions
    From: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net>
    The AoA's are generally much better at showing stall information (when was the last time you saw a jet with a stall tab). Because I am going with the AoA Pro, I for one didn't see the point of putting the old mechanical tab out there. Michael Sausen -10 #352 Fuselage -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Jae Chang Sent: Sunday, November 26, 2006 7:57 AM Subject: RE: RV10-List: Wing leading edge questions --> <jc-matronics_rv10@jline.com> Hi Eric... I finished my leading edges not that long ago. Instead of ordering/installing any of the accessories, I left the outer rib clecoed, so I could order and install accessories some time later. With the stall warning gizmo, I had not even considered not installing it, since it's such a useful thing to have. Are people just forgoing the mechnical stall indicator, for the AOA, or replacing it with something better? Jae -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Eric_Kallio Sent: Saturday, November 25, 2006 7:34 AM Subject: RV10-List: Wing leading edge questions I am getting ready to start the leading edges of my wings and plunk down some more money for accessories. I intend on purchasing the Gretz 1000 heated pitot, the Duckworks HID landing lights, and the AFS AOA. After reviewing the archives several of you had said that you were putting the light and the AOA on the last bay. Any feedback on how that worked out as far as space and ease of maintenace for the future? I was also looking at simply closing the stall horn holes and not installing it, as others have done. Does any body flying think that is something I should still install? Finally any other tips or gotchas out there. I have been all over Tim's and Deems's sites...pretty much live on those, and Mike Howe's also. Thanks for your feedback. Eric Kallio #40518 SB wings Read this topic online here: http://forums.matronics.com/viewtopic.php?p=76864#76864


    Message 26


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    Time: 10:22:49 AM PST US
    From: Niko <owl40188@yahoo.com>
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 I had mine replaced by Vans at no charge. I did not have to send in the or iginal one. I just sent them pictures of the cracks. No cost to me at all . I would not accept them with cracks. Although you might only see one cr ack in the region there might be another area ready to crack after a few lo ad cycles. Whether you need the strength or not, a part with a crack and a stop hole is not as strong as the original part without any cracks. =0A=0A Niko=0A40188=0A=0A=0A----- Original Message ----=0AFrom: John Jessen <jjess en@rcn.com>=0ATo: rv10-list@matronics.com=0ASent: Monday, November 27, 2006 12:02:19 PM=0ASubject: RE: RV10-List: 2 Tailcone Questions: F-1012B came u hn Jessen" <jjessen@rcn.com>=0A=0AThey should replace it for gratis. Give it a try. =0A=0AJohn Jessen #40328=0A=0ADo not archive=0A=0A=0A=0A-----Ori ginal Message-----=0AFrom: owner-rv10-list-server@matronics.com=0A[mailto:o wner-rv10-list-server@matronics.com] On Behalf Of Brian Douglas=0ASent: Mon day, November 27, 2006 10:21 AM=0ATo: rv10-list@matronics.com=0ASubject: Re : RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small=0Atear in il@belinblank.org>=0A=0AI have the same problem on both counts. I ground/b uffed the crack out of=0Athe F-1010 this weekend but have decided that all rationality aside, it's=0Agoing to drive me crazy to install it like that s o I'm just going to pay to=0Ahave a new one shipped. What's another $30 ri ght?=0A=0A=0A-Brian=0A=0A#40497=0AIowa City, IA=0A=0A----- Original Message -----=0AFrom: "MauleDriver" <MauleDriver@nc.rr.com>=0ATo: <rv10-list@matro nics.com>=0ASent: Sunday, November 26, 2006 7:12 PM=0ASubject: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear=0Ain F-1010=0A=0A =0A>=0A> During initial assembly of tailcone, I noticed that F-1012B was no t =0A> pre-punched for the skin. The plans shows both A & B as pre-punche d. =0A> It will be very easy to match drill the bulkhead using the skin =0A> punches and relying on the A bulkhead for alignment. But I am curious =0A> whether others have encountered the same thing.=0A>=0A> I also notice d a very small tear in the thin flange around the central =0A> hole in bulk head F-1010. It appears to have resulted from the forming =0A> of the flan ge. It would seem to be subject to enlarging if the area =0A> is stressed. Would a stop hole be called for? Or grinding the tear =0A> out? Or a ne w part? I will be going to Vans with this.=0A>=0A> Link to photos of tear: =0A> http://www.mykitlog.com/users/display_log.php?user=MauleDriver&proje ct=0A> =224&category=0&log=23464&row=4=0A>=0A> Bill Watson "MauleDr iver"=0A> The QB Fuse and Wing arrived last week (9 weeks early) - here we Gooooooo!=0A>=0A>=0A>=0A>=0A>=0A>=0A>=0A>=0A>=0A> =0A=0A=0A=0A=0A=0A--=0A4: ===========


    Message 27


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    Time: 10:37:48 AM PST US
    Subject: transponder antenna placement
    From: "Chris Johnston" <CJohnston@popsound.com>
    Hey all - I was perusing the archives looking for info on the transponder antenna placement, and I ran across mentions of microwaves cooking private parts. Really? Come on... really? I'm looking at spots to mount the antenna, and under the pilot / copilot seats seems like the best bet for me. The tunnel is out, because I made a false floor that goes from the firewall to the spar and I don't want any penetrations there. I was thinking the transponder antenna under the copilot and the avidyne/ryan traffic antenna under the pilot seat. I've already got comms under the rear passenger seats, and navs in the wingtips. Is the transponder really going to do a number on me or my copilot under the seats? Inquiring minds want to know... cj #40410 fuse www.perfectlygoodairplane.net


    Message 28


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    Time: 10:46:36 AM PST US
    Subject: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010
    From: "John W. Cox" <johnwcox@pacificnw.com>
    Removing the obvious (the visible crack) does not remove the adjacent induced stress which is yet to propagate. Many who have stop drilled learn that lesson with time on their airframe after a perceived patch was signed off. You are only cheating the inevitable. Metal has memory, it does not forget. You are not going to fool it into long term submission. We resort to Eddy Current and Ultrasonic more often that people know with our air carrier aircraft. The use of polarizing lens while watching the bending, drilling or cutting of Plexiglas/acrylic panel is a real eye opener if you can excuse the pun. The stresses can go wild. You can watch with dazzling amazement at the exact moment just before the crack destroys the final piece. Replacing it with one (F-1010)that has not been manipulated or masked is the "No brainer". You can consider it the Golden Panel too. Dip it in alodine like Tim did and then tell stories about it in hangars, years from now. John Cox #40600 -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of John Jessen Sent: Monday, November 27, 2006 9:02 AM Subject: RE: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 They should replace it for gratis. Give it a try. John Jessen #40328 Do not archive -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Brian Douglas Sent: Monday, November 27, 2006 10:21 AM Subject: Re: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 --> <bsponcil@belinblank.org> I have the same problem on both counts. I ground/buffed the crack out of the F-1010 this weekend but have decided that all rationality aside, it's going to drive me crazy to install it like that so I'm just going to pay to have a new one shipped. What's another $30 right? -Brian #40497 Iowa City, IA ----- Original Message ----- From: "MauleDriver" <MauleDriver@nc.rr.com> Sent: Sunday, November 26, 2006 7:12 PM Subject: RV10-List: 2 Tailcone Questions: F-1012B came unpunched, small tear in F-1010 > > During initial assembly of tailcone, I noticed that F-1012B was not > pre-punched for the skin. The plans shows both A & B as pre-punched. > It will be very easy to match drill the bulkhead using the skin > punches and relying on the A bulkhead for alignment. But I am curious > whether others have encountered the same thing. > > I also noticed a very small tear in the thin flange around the central > hole in bulkhead F-1010. It appears to have resulted from the forming > of the flange. It would seem to be subject to enlarging if the area > is stressed. Would a stop hole be called for? Or grinding the tear > out? Or a new part? I will be going to Vans with this. > > Link to photos of tear: > http://www.mykitlog.com/users/display_log.php?user=MauleDriver&project > =224&category=0&log=23464&row=4 > > Bill Watson "MauleDriver" > The QB Fuse and Wing arrived last week (9 weeks early) - here we Gooooooo! > > > -- 4:00 AM -- 4:00 AM


    Message 29


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    Time: 10:48:22 AM PST US
    From: Michael Schipper <mike@learningplanet.com>
    Subject: Re: Jack Stand
    On the -9A I use an ATV/Motorcycle jack that I bought at Harbor Freight. I made a wooden "truss" to take up the space between the jack and the plane. By placing it directly under the main spar I can lift the entire plane with just a pump of the lever. I normally only raise it about an inch or so. http://www.my9a.com/img/flying/fairings/f18.jpg Regards, Mike Schipper RV-10 #40576 - Wings www.rvten.com From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list- server@matronics.com] On Behalf Of Jesse Saint Sent: Monday, November 27, 2006 7:41 AM Subject: RV10-List: Jack Stand Has anybody come up with a good way to jack up the mains on the -10 without taking the axle nut off and using something like Avery sells? For most cases that works fine, but it would be nice to have another good way to do it.


    Message 30


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    Time: 10:54:13 AM PST US
    From: Rick <ricksked@earthlink.net>
    Subject: Re: transponder antenna placement
    Chris, I have heard both....that it is harmful microwave energy from William Curtis who's electronic knowledge I trust and that it's bunk. I mounted mine on the bottom right side between the battery and the right sidewall behind the baggage bulkhead. It's outta the way, it is a long coax run but at least it's not near the nads, rumor or not ;) Rick S. 40185


    Message 31


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    Time: 11:10:14 AM PST US
    From: "John Gonzalez" <indigoonlatigo@msn.com>
    Subject: transponder antenna placement
    How do you like 'em- sunny side up, over easy, hard boiled or poached. Scrambled is not an option. Seriously, what kind of material would be needed to stop the radiation? Inquiring organs want to know. John G. Do Not Archive >From: "Chris Johnston" <CJohnston@popsound.com> >To: <rv10-list@matronics.com> >Subject: RV10-List: transponder antenna placement >Date: Mon, 27 Nov 2006 10:36:33 -0800 > > >Hey all - > >I was perusing the archives looking for info on the transponder antenna >placement, and I ran across mentions of microwaves cooking private >parts. Really? Come on... really? I'm looking at spots to mount the >antenna, and under the pilot / copilot seats seems like the best bet for >me. The tunnel is out, because I made a false floor that goes from the >firewall to the spar and I don't want any penetrations there. I was >thinking the transponder antenna under the copilot and the avidyne/ryan >traffic antenna under the pilot seat. I've already got comms under the >rear passenger seats, and navs in the wingtips. Is the transponder >really going to do a number on me or my copilot under the seats? >Inquiring minds want to know... > >cj >#40410 >fuse >www.perfectlygoodairplane.net > >


    Message 32


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    Time: 11:14:20 AM PST US
    From: "Jesse Saint" <jesse@itecusa.org>
    Subject: Jack Stand
    Thanks for all the input. I hope this has helped others as well. I talked to Van=92s and they confirmed that the tie-down support is the preferred place to jack from, so we will do something like Tim has done. Jesse Saint I-TEC, Inc. HYPERLINK "mailto:jesse@itecusa.org"jesse@itecusa.org HYPERLINK "http://www.itecusa.org"www.itecusa.org W: 352-465-4545 C: 352-427-0285 _____ From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Michael Schipper Sent: Monday, November 27, 2006 1:46 PM Subject: Re: RV10-List: Jack Stand On the -9A I use an ATV/Motorcycle jack that I bought at Harbor Freight. I made a wooden "truss" to take up the space between the jack and the plane. By placing it directly under the main spar I can lift the entire plane with just a pump of the lever. I normally only raise it about an inch or so. HYPERLINK "http://www.my9a.com/img/flying/fairings/f18.jpg"http://www.my9a.com/img/ fly ing/fairings/f18.jpg Regards, Mike Schipper RV-10 #40576 - Wings www.rvten.com From: HYPERLINK "mailto:owner-rv10-list-server@matronics.com"owner-rv10-list-server@matro nic s.com [HYPERLINK "mailto:owner-rv10-list-server@matronics.com"mailto:owner-rv10-list-serve r@m atronics.com] On Behalf Of Jesse Saint Sent: Monday, November 27, 2006 7:41 AM Subject: RV10-List: Jack Stand Has anybody come up with a good way to jack up the mains on the -10 without taking the axle nut off and using something like Avery sells? For most cases that works fine, but it would be nice to have another good way to do it. "http://www.aeroelectric.com"www.aeroelectric.com "http://www.buildersbooks.com"www.buildersbooks.com "http://www.kitlog.com"www.kitlog.com "http://www.homebuilthelp.com"www.homebuilthelp.com "http://www.matronics.com/contribution"http://www.matronics.com/contribut ion "http://www.matronics.com/Navigator?RV10-List"http://www.matronics.com/Na vig ator?RV10-List 11/27/2006 4:00 AM -- 11/27/2006 4:00 AM


    Message 33


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    Time: 11:18:34 AM PST US
    From: "Jesse Saint" <jesse@itecusa.org>
    Subject: transponder antenna placement
    I can't speak to the sperm-count effect of the Transponder antenna, but if you're out of the baby-making stage, then that might not matter anyway. Let's go ahead and get the do not archive tag here. I put mine on the tunnel just aft of the firewall, which allows for a very short wiring run and keeps it away from the other cables and antennas. I have the comms under the pilot and copilot. The main thing I would recommend, if you are comfortable putting it under your seat, would be that you have at least 30-36 inches between it and the comms, which shouldn't be a big problem. Also, I understand that it is a good idea to keep the cable run separate from your other antennas. Jesse Saint I-TEC, Inc. jesse@itecusa.org www.itecusa.org W: 352-465-4545 C: 352-427-0285 -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Chris Johnston Sent: Monday, November 27, 2006 1:37 PM Subject: RV10-List: transponder antenna placement Hey all - I was perusing the archives looking for info on the transponder antenna placement, and I ran across mentions of microwaves cooking private parts. Really? Come on... really? I'm looking at spots to mount the antenna, and under the pilot / copilot seats seems like the best bet for me. The tunnel is out, because I made a false floor that goes from the firewall to the spar and I don't want any penetrations there. I was thinking the transponder antenna under the copilot and the avidyne/ryan traffic antenna under the pilot seat. I've already got comms under the rear passenger seats, and navs in the wingtips. Is the transponder really going to do a number on me or my copilot under the seats? Inquiring minds want to know... cj #40410 fuse www.perfectlygoodairplane.net -- 4:00 AM -- 4:00 AM


    Message 34


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    Time: 11:28:24 AM PST US
    From: MauleDriver <MauleDriver@nc.rr.com>
    Subject: Re: 2 Tailcone Questions: F-1012B came unpunched, small tear
    in F-1010 Not sure I follow the thinking here. Removing the visible tear simply removes the tear which could represent a focal point for local stresses. It is the most likely place for any stresses to manifest themselves in further tearing. Without the tear, I'm thinking there is no focal point and no tear to propogate. Whatever stresses exist in the piece remain. Just because there isn't a tear in a replacement part doesn't mean there isn't the same set of stresses in the part. They just didn't result in a tear. If you are saying that the tear induces stress and the metal remembers, I guess I don't understand that. In any case, the tear needs to be removed or possibly stop drilled. But doing either compromises the original intended strength of the piece so I agree it should be replaced. Bill Watson John W. Cox wrote: > > Removing the obvious (the visible crack) does not remove the adjacent > induced stress which is yet to propagate. Many who have stop drilled > learn that lesson with time on their airframe after a perceived patch > was signed off. You are only cheating the inevitable. Metal has memory, > it does not forget. You are not going to fool it into long term > submission. We resort to Eddy Current and Ultrasonic more often that > people know with our air carrier aircraft. > >


    Message 35


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    Time: 11:30:31 AM PST US
    Subject: Re: transponder antenna placement
    From: "bcondrey" <bob.condrey@baesystems.com>
    Chris, Below is from an exchange on this subject on the AeroElectric list - short version is that there isn't an issue. Bob ----------------------------------------------------------------------------- Message: #10129 Date: Mar 10, 2003 From: "Robert L. Nuckolls, III" Subject: Re: defending the "familiy jewels" . . . > >A transponder antenna that close to your passengers "private parts" >might not be the best thing to do. The radiation may do some damage. > >Rino A hangar myth. Folks have looked at the peak output power rating of a transponder (100 to 250W) and tried to make a connection between a desire to make one's airplane visible to a distant radar receiver and cooking meat. When you buy a microwave, it too is rated in the hundreds of watts . . . but CONTINUOUS duty. A good 700W microwave will boil a cup of water in about 2 minutes. (Remember the traveler's immersion heaters in the hardware store? They're 300W heaters and take about 4 minutes to boil a cup of water). If you measure the current draw of this machine, it will be on the order of 8-9 amps or 1000W total input. Your transponder draws about 1.5 amps while being interrogated for a total input power of 18W. The output comes in the form of a series of 0.5 uSec pulses in respond to an interrogation that represent a string of binary numbers representing either your squawk code (mode A) or altitude (mode C). Assuming you are interrogated once per second (quite often) your average output power for a 250W transponder is on the order of 250W x 20 pulses x 0.0000005 seconds/1 second or 2.5 milliwatts per second. This isn't going even going to warm up much less cook anything. Another fallacy of the myth concerns body parts most sensitive to microwave radiation . . . turns out that your eyes are the most vulnerable . . . but the story isn't nearly so interesting to really macho pilots. None the less, there are folks who have armor-shielded their seat bottoms in deference to this myth. The story was REALLY popular about 15 years ago in the heyday of the Long-Ezs Here's a post I did on a canard pusher list server about 5 years ago: > Location away from the pilot/co-pilot is also >recommended but over ten feet requires a different cable. Yes?? I was >thinking about locating it aft of the pilot in the baggage area. Is that >distance safe? A totally bogus recommendation. A few years back, someone observed that their transponder was rated for 200 watts output . . . 1/3rd that of the family microwave. Our hero was immediately concerned for preservation of the family jewels and proceeded to line the bottom of his composite seat pan with aluminum foil. What he failed to understand was that his RF coffee warmer and popcorn popper was rated in continuous watts while the transponder was in peak watts. The average power output from a transponder is less than 1 watt . . . BTW, the eyes are about 100 times more sensitive to the effects of microwave heating than are any deep organs . . . you'll go blind you quit making babies. Bob . . . Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77381#77381


    Message 36


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    Time: 11:33:32 AM PST US
    Subject: transponder antenna placement
    From: "John W. Cox" <johnwcox@pacificnw.com>
    This goes along with the original scientific studies used in 1983, when cell phones were first sold that said everyone was going to get brain tumors on the side closest the antenna on your hand-held. I think it led to a lot of brain dead teenagers but no tumorous growths in their adult life - yet. However, there are a lot of EA-6B Naval Aviators that swear their love life was curtailed by the errant electrons bouncing off the gold electroplated canopies from all that jamming they did for Uncle Sammy. Rick I would think the Air Force used similar stories on the girls in your day. Just don't forget about Blue Nads from those forward NACA ducts. John Cox 40600 -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Rick Sent: Monday, November 27, 2006 10:53 AM Subject: Re: RV10-List: transponder antenna placement Chris, I have heard both....that it is harmful microwave energy from William Curtis who's electronic knowledge I trust and that it's bunk. I mounted mine on the bottom right side between the battery and the right sidewall behind the baggage bulkhead. It's outta the way, it is a long coax run but at least it's not near the nads, rumor or not ;) Rick S. 40185


    Message 37


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    Time: 11:39:35 AM PST US
    Subject: transponder antenna placement
    From: "Chris Johnston" <CJohnston@popsound.com>
    Does the placement of the transponder antenna need to be as far forward as possible, or am I making that up? I feel like I read that or heard that somewhere. If I can put the antenna behind the bulkhead I'd love it! is there a good argument (besides longer coax run) against putting the antenna back there? cj #40410 fuse www.perfectlygoodairplane.net do not archive -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Rick Sent: Monday, November 27, 2006 10:53 AM Subject: Re: RV10-List: transponder antenna placement Chris, I have heard both....that it is harmful microwave energy from William Curtis who's electronic knowledge I trust and that it's bunk. I mounted mine on the bottom right side between the battery and the right sidewall behind the baggage bulkhead. It's outta the way, it is a long coax run but at least it's not near the nads, rumor or not ;) Rick S. 40185


    Message 38


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    Time: 11:44:00 AM PST US
    From: "Kelly McMullen" <apilot2@gmail.com>
    Subject: Re: Jack Stand
    I don't know if the -10 uses standard threaded tie-down anchors or not, but Mooney and I believe some other aircraft have threaded jackpoints that are installed in place of the tie-down rings whenever jacking is necessary. The underside of the jackpoint is milled conical so that it mates right up with a standard aircraft jack, while allowing relative freedom to pivot on the point while leveling or just jacking one side. On 11/27/06, Jesse Saint <jesse@itecusa.org> wrote: > > > Thanks for all the input. I hope this has helped others as well. I talked > to Van's and they confirmed that the tie-down support is the preferred place > to jack from, so we will do something like Tim has done. >


    Message 39


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    Time: 12:10:35 PM PST US
    From: "David McNeill" <dlm46007@cox.net>
    Subject: Re: transponder antenna placement
    Why worry? I have been flying light airplanes for thirty plus years and 4000 hours with the transponder antenna just below my seat. I had three healthy children in my 20s and two healthy children in my 50s , the last at 55. ----- Original Message ----- From: "John Gonzalez" <indigoonlatigo@msn.com> Sent: Monday, November 27, 2006 12:09 PM Subject: RE: RV10-List: transponder antenna placement > > How do you like 'em- sunny side up, over easy, hard boiled or poached. > Scrambled is not an option. > > Seriously, what kind of material would be needed to stop the radiation? > > Inquiring organs want to know. > > John G. > > Do Not Archive > > >>From: "Chris Johnston" <CJohnston@popsound.com> >>To: <rv10-list@matronics.com> >>Subject: RV10-List: transponder antenna placement >>Date: Mon, 27 Nov 2006 10:36:33 -0800 >> >> >>Hey all - >> >>I was perusing the archives looking for info on the transponder antenna >>placement, and I ran across mentions of microwaves cooking private >>parts. Really? Come on... really? I'm looking at spots to mount the >>antenna, and under the pilot / copilot seats seems like the best bet for >>me. The tunnel is out, because I made a false floor that goes from the >>firewall to the spar and I don't want any penetrations there. I was >>thinking the transponder antenna under the copilot and the avidyne/ryan >>traffic antenna under the pilot seat. I've already got comms under the >>rear passenger seats, and navs in the wingtips. Is the transponder >>really going to do a number on me or my copilot under the seats? >>Inquiring minds want to know... >> >>cj >>#40410 >>fuse >>www.perfectlygoodairplane.net >> >> >> >> >> >> > > >


    Message 40


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    Time: 12:18:16 PM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Re: transponder antenna placement
    If your com's are under the rear seats, having these antennas so close may not be a good thing. I'm no expert, but I do think they want 30+ inches or something like that, so the more the better. The other suggestion of under the tail seems OK though, despite the long cable run. I opted to keep that cable short and put it in the tunnel. Not sure if you could just do a penetration in your false floor and grommet it to seal it up, but if you can find a way to get it there, it's not a bad spot. Don't put it way up right by the exhaust though....leave it back a little. Tim Olson - RV-10 N104CD - Flying do not archive Chris Johnston wrote: > > Hey all - > > I was perusing the archives looking for info on the transponder antenna > placement, and I ran across mentions of microwaves cooking private > parts. Really? Come on... really? I'm looking at spots to mount the > antenna, and under the pilot / copilot seats seems like the best bet for > me. The tunnel is out, because I made a false floor that goes from the > firewall to the spar and I don't want any penetrations there. I was > thinking the transponder antenna under the copilot and the avidyne/ryan > traffic antenna under the pilot seat. I've already got comms under the > rear passenger seats, and navs in the wingtips. Is the transponder > really going to do a number on me or my copilot under the seats? > Inquiring minds want to know... > > cj > #40410 > fuse > www.perfectlygoodairplane.net >


    Message 41


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    Time: 12:20:51 PM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Re: transponder antenna placement
    I think you're making it up. On my old certified plane it was back behind the step area, under the tail. Tim Olson - RV-10 N104CD - Flying do not archive Chris Johnston wrote: > > Does the placement of the transponder antenna need to be as far forward > as possible, or am I making that up? I feel like I read that or heard > that somewhere. If I can put the antenna behind the bulkhead I'd love > it! is there a good argument (besides longer coax run) against putting > the antenna back there? > > cj > #40410 > fuse > www.perfectlygoodairplane.net > > > > > do not archive > -----Original Message----- > From: owner-rv10-list-server@matronics.com > [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Rick > Sent: Monday, November 27, 2006 10:53 AM > To: rv10-list@matronics.com > Subject: Re: RV10-List: transponder antenna placement > > > Chris, > > I have heard both....that it is harmful microwave energy from William > Curtis who's electronic knowledge I trust and that it's bunk. I mounted > mine on the bottom right side between the battery and the right sidewall > behind the baggage bulkhead. It's outta the way, it is a long coax run > but at least it's not near the nads, rumor or not ;) > > Rick S. > 40185 > > > > > > > > > >


    Message 42


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    Time: 12:22:45 PM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Re: Jack Stand
    It is threaded. Handy spot. As far as handling the load of the plane, if the plane can't lift itself by the wings, and handle that 1G, I'd be a bit worried about how it would handle 4G's. Tim Olson - RV-10 N104CD - Flying do not archive Kelly McMullen wrote: > > I don't know if the -10 uses standard threaded tie-down anchors or > not, but Mooney and I believe some other aircraft have threaded > jackpoints that are installed in place of the tie-down rings whenever > jacking is necessary. The underside of the jackpoint is milled conical > so that it mates right up with a standard aircraft jack, while > allowing relative freedom to pivot on the point while leveling or just > jacking one side. > > On 11/27/06, Jesse Saint <jesse@itecusa.org> wrote: >> >> >> >> Thanks for all the input. I hope this has helped others as well. I >> talked >> to Van's and they confirmed that the tie-down support is the preferred >> place >> to jack from, so we will do something like Tim has done. >>


    Message 43


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    Time: 12:26:38 PM PST US
    From: Rick <ricksked@earthlink.net>
    Subject: transponder antenna placement
    Well many a night we did radar ops checks and had to actually transmit, I never did trust those cones set out in front. I saw a guy throw a wad of steel wool out in front and watched it burst into flames...yeah I know not so smart in a slightly explosive enviroment but that convinced me that those invisible radio waves really could do some damage if they were powerful enough. That was almost as exciting as throwing a cement brick into an F-100 afterburner and watcing the force of full AB throw the brick a good 400 feet. The noise and vibrations off that AB was enough to make you feel sick to your stomach. All BTW you could not "see" Some truth to the term that what you can't see CAN hurt you. Of couse that leads to why there is an eye patch on the stick of the Victor alert birds..... Rick S. 40185 do not archive


    Message 44


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    Time: 12:34:20 PM PST US
    From: Rick <ricksked@earthlink.net>
    Subject: Re: transponder antenna placement
    lol....but how many Tails do they have David!! :) Rick S. 40185 do not archive


    Message 45


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    Time: 12:59:50 PM PST US
    Subject: Re: transponder antenna placement
    From: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net>
    Sounds like a good episode of Mythbusters. Adam can put his nads in a microwave and Jamie can sit on a transponder antenna while being regularly interrogated or pushing ident. ROFLMAO! Seriously though, I don't think anyone has ever done a serious study on this. In reality any potential health issues are probably pretty small. You probably get more rads from the solar radiation at 15,000 feet than from the transponder. I still wouldn't put it right under my seat though. The biggest issue in placement is keeping the antenna lead as short as possible. Michael Sausen -10 #352 fuselage -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of bcondrey Sent: Monday, November 27, 2006 1:30 PM Subject: RV10-List: Re: transponder antenna placement Chris, Below is from an exchange on this subject on the AeroElectric list - short version is that there isn't an issue. Bob ------------------------------------------------------------------------ ----- Message: #10129 Date: Mar 10, 2003 From: "Robert L. Nuckolls, III" Subject: Re: defending the "familiy jewels" . . . > >A transponder antenna that close to your passengers "private parts" >might not be the best thing to do. The radiation may do some damage. > >Rino A hangar myth. Folks have looked at the peak output power rating of a transponder (100 to 250W) and tried to make a connection between a desire to make one's airplane visible to a distant radar receiver and cooking meat. When you buy a microwave, it too is rated in the hundreds of watts . . . but CONTINUOUS duty. A good 700W microwave will boil a cup of water in about 2 minutes. (Remember the traveler's immersion heaters in the hardware store? They're 300W heaters and take about 4 minutes to boil a cup of water). If you measure the current draw of this machine, it will be on the order of 8-9 amps or 1000W total input. Your transponder draws about 1.5 amps while being interrogated for a total input power of 18W. The output comes in the form of a series of 0.5 uSec pulses in respond to an interrogation that represent a string of binary numbers representing either your squawk code (mode A) or altitude (mode C). Assuming you are interrogated once per second (quite often) your average output power for a 250W transponder is on the order of 250W x 20 pulses x 0.0000005 seconds/1 second or 2.5 milliwatts per second. This isn't going even going to warm up much less cook anything. Another fallacy of the myth concerns body parts most sensitive to microwave radiation . . . turns out that your eyes are the most vulnerable . . . but the story isn't nearly so interesting to really macho pilots. None the less, there are folks who have armor-shielded their seat bottoms in deference to this myth. The story was REALLY popular about 15 years ago in the heyday of the Long-Ezs Here's a post I did on a canard pusher list server about 5 years ago: > Location away from the pilot/co-pilot is also >recommended but over ten feet requires a different cable. Yes?? I was >thinking about locating it aft of the pilot in the baggage area. Is that >distance safe? A totally bogus recommendation. A few years back, someone observed that their transponder was rated for 200 watts output . . . 1/3rd that of the family microwave. Our hero was immediately concerned for preservation of the family jewels and proceeded to line the bottom of his composite seat pan with aluminum foil. What he failed to understand was that his RF coffee warmer and popcorn popper was rated in continuous watts while the transponder was in peak watts. The average power output from a transponder is less than 1 watt . . . BTW, the eyes are about 100 times more sensitive to the effects of microwave heating than are any deep organs . . . you'll go blind you quit making babies. Bob . . . Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77381#77381


    Message 46


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    Time: 01:02:47 PM PST US
    From: "David McNeill" <dlm46007@cox.net>
    Subject: Re: transponder antenna placement
    Since we met when I visited your garage you will have to judge for yourself ----- Original Message ----- From: "Rick" <ricksked@earthlink.net> Sent: Monday, November 27, 2006 1:33 PM Subject: Re: RV10-List: transponder antenna placement > > lol....but how many Tails do they have David!! :) > > Rick S. > 40185 > > do not archive > > > > >


    Message 47


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    Time: 01:22:45 PM PST US
    From: "John Gonzalez" <indigoonlatigo@msn.com>
    Subject: Re: transponder antenna placement
    Under the seat however, the moicrowaves would be going through several layers of metal to find your privates, unless your a low hanger. DO not archive >From: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net> >To: <rv10-list@matronics.com> >Subject: RE: RV10-List: Re: transponder antenna placement >Date: Mon, 27 Nov 2006 14:59:20 -0600 > ><rvbuilder@sausen.net> > >Sounds like a good episode of Mythbusters. Adam can put his nads in a >microwave and Jamie can sit on a transponder antenna while being >regularly interrogated or pushing ident. ROFLMAO! > >Seriously though, I don't think anyone has ever done a serious study on >this. In reality any potential health issues are probably pretty small. >You probably get more rads from the solar radiation at 15,000 feet than >from the transponder. I still wouldn't put it right under my seat >though. The biggest issue in placement is keeping the antenna lead as >short as possible. > >Michael Sausen >-10 #352 fuselage > >-----Original Message----- >From: owner-rv10-list-server@matronics.com >[mailto:owner-rv10-list-server@matronics.com] On Behalf Of bcondrey >Sent: Monday, November 27, 2006 1:30 PM >To: rv10-list@matronics.com >Subject: RV10-List: Re: transponder antenna placement > > >Chris, > >Below is from an exchange on this subject on the AeroElectric list - >short version is that there isn't an issue. > >Bob > >------------------------------------------------------------------------ >----- > >Message: #10129 Date: Mar 10, 2003 From: "Robert L. Nuckolls, III" >Subject: Re: defending the "familiy jewels" . . . > > > > > >A transponder antenna that close to your passengers "private parts" > >might not be the best thing to do. The radiation may do some damage. > > > >Rino > > A hangar myth. Folks have looked at the > peak output power rating of a transponder (100 to 250W) > and tried to make a connection between a desire to > make one's airplane visible to a distant radar receiver > and cooking meat. > > When you buy a microwave, it too is rated in the > hundreds of watts . . . but CONTINUOUS duty. A > good 700W microwave will boil a cup of water in > about 2 minutes. (Remember the traveler's immersion > heaters in the hardware store? They're 300W heaters > and take about 4 minutes to boil a cup of water). > If you measure the current draw of this machine, > it will be on the order of 8-9 amps or 1000W total > input. > > Your transponder draws about 1.5 amps while being > interrogated for a total input power of 18W. The > output comes in the form of a series of 0.5 uSec > pulses in respond to an interrogation that represent > a string of binary numbers representing either your > squawk code (mode A) or altitude (mode C). Assuming > you are interrogated once per second (quite often) > your average output power for a 250W transponder > is on the order of 250W x 20 pulses x 0.0000005 > seconds/1 second or 2.5 milliwatts per second. > This isn't going even going to warm up much less cook > anything. > > Another fallacy of the myth concerns body parts > most sensitive to microwave radiation . . . turns > out that your eyes are the most vulnerable . . . > but the story isn't nearly so interesting to > really macho pilots. None the less, there are > folks who have armor-shielded their seat bottoms > in deference to this myth. The story was REALLY > popular about 15 years ago in the heyday of > the Long-Ezs > > Here's a post I did on a canard pusher list > server about 5 years ago: > > > Location away from the pilot/co-pilot is also >recommended but over >ten feet requires a different cable. Yes?? I was >thinking about >locating it aft of the pilot in the baggage area. Is that >distance >safe? > > A totally bogus recommendation. A few years back, someone observed > that their transponder was rated for 200 watts output . . . 1/3rd > that of the family microwave. Our hero was immediately concerned for > preservation of the family jewels and proceeded to line the bottom > of his composite seat pan with aluminum foil. What he failed to > understand was that his RF coffee warmer and popcorn popper was > rated in continuous watts while the transponder was in peak watts. > The average power output from a transponder is less than 1 watt . . . > BTW, the eyes are about 100 times more sensitive to the effects of > microwave heating than are any deep organs . . . you'll go blind > you quit making babies. > > Bob . . . > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=77381#77381 > >


    Message 48


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    Time: 01:24:01 PM PST US
    From: Rick <ricksked@earthlink.net>
    Subject: Re: transponder antenna placement
    I knew that!! I didn't take notice though. ;) Rick S. do not archive


    Message 49


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    Time: 01:49:34 PM PST US
    From: Bill DeRouchey <billderou@yahoo.com>
    Subject: transponder antenna placement
    The antenna placement recommendations from Garmin are: 1. place antenna 3 feet (physical measurement) from transponder unit 2. cable no longer than 8.8 feet of RG-400 (to handle the high power) 3. 30 inches (physical measurement) from any com antenna 4. Try to maximize distance from landing gear leg when placing under the seat to minimize holes in pattern. Mine is too close but it works correctly. Bill DeRouchey billderou@yahoo.com Flying with a few pit stops "John W. Cox" <johnwcox@pacificnw.com> wrote: This goes along with the original scientific studies used in 1983, when cell phones were first sold that said everyone was going to get brain tumors on the side closest the antenna on your hand-held. I think it led to a lot of brain dead teenagers but no tumorous growths in their adult life - yet. However, there are a lot of EA-6B Naval Aviators that swear their love life was curtailed by the errant electrons bouncing off the gold electroplated canopies from all that jamming they did for Uncle Sammy. Rick I would think the Air Force used similar stories on the girls in your day. Just don't forget about Blue Nads from those forward NACA ducts. John Cox 40600 -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Rick Sent: Monday, November 27, 2006 10:53 AM Subject: Re: RV10-List: transponder antenna placement Chris, I have heard both....that it is harmful microwave energy from William Curtis who's electronic knowledge I trust and that it's bunk. I mounted mine on the bottom right side between the battery and the right sidewall behind the baggage bulkhead. It's outta the way, it is a long coax run but at least it's not near the nads, rumor or not ;) Rick S. 40185 ---------------------------------


    Message 50


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    Time: 01:49:35 PM PST US
    Subject: Re: transponder antenna placement
    From: "John W. Cox" <johnwcox@pacificnw.com>
    "Rads on the Nads". A new section for Tim on the RV U site. Leave it to Michael to get us all ROFLMAO. John Cox 40600 Do not Archive -----Original Message----- From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Monday, November 27, 2006 12:59 PM Subject: RE: RV10-List: Re: transponder antenna placement <rvbuilder@sausen.net> Sounds like a good episode of Mythbusters. Adam can put his nads in a microwave and Jamie can sit on a transponder antenna while being regularly interrogated or pushing ident. ROFLMAO! Seriously though, I don't think anyone has ever done a serious study on this. In reality any potential health issues are probably pretty small. You probably get more rads from the solar radiation at 15,000 feet than from the transponder. I still wouldn't put it right under my seat though. The biggest issue in placement is keeping the antenna lead as short as possible. Michael Sausen -10 #352 fuselage


    Message 51


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    Time: 05:51:19 PM PST US
    From: ivo welch <ivowel@gmail.com>
    Subject: truemap and motion m1300 outdoor tablet PC
    dear RV-ers. About 3 years ago, I purchased a license for truemap software. It was never used. It cost $595, and I presume that because it was never activated, the folks there will be kind enough to transfer this to anyone who wants to use it. (if not, I will take it back and refund the money.) I also purchased a Motion M1300 tablet PC, *with outdoor display*. the m1300 is almost the same thing as what they now sell as their LE 1600 tablet, though the latter has bluetood tech, and a fingerprint reader. the outdoor display is a *big* deal. w/o it, they are cheap. the tablet was also barely used, plus I have some accessories, like the extra keyboard---because I never ended up using the truemap software. finally, I have two USB GPS receivers. (they make sense, because a wireless consumes more power.) alas, I don't need the system any more. I may list it on ebay in a week or so. if you would like to purchase it, please drop me an email. not the smartest purchase I ever made... regards, /ivo


    Message 52


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    Time: 06:45:59 PM PST US
    From: linn Walters <pitts_pilot@bellsouth.net>
    Subject: Re: transponder antenna placement
    Not having to do any testing myself ... ;-) ..... I'll side with bunk! First of all, the energy just isn't there, and the average energy is way lower than that so ..... make your own assessment. Lets face it .... microwave ovens work on the resonant frequency of water molecules. I haven't a clue what that frequency really is, but the transponder frequency probably isn't anywhere close. I'd liken it to the cell phone/tumor thingy. Linn do not archive .... because I just may be blowing smoke! Rick wrote: > >Chris, > >I have heard both....that it is harmful microwave energy from William Curtis who's electronic knowledge I trust and that it's bunk. I mounted mine on the bottom right side between the battery and the right sidewall behind the baggage bulkhead. It's outta the way, it is a long coax run but at least it's not near the nads, rumor or not ;) > >Rick S. >40185 > > > >




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