RV10-Archive.digest.vol-dd

March 04, 2008 - March 16, 2008



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Date: Mar 04, 2008
Subject: Re: Lower Cowl Mounts
From: "William Curtis" <wcurtis(at)nerv10.com>
Larry, Those bottom ones don't look like Camlocs, they look like screws with Tinnerman washers. I know Vic sold the plane but is he still on the list? William http://wcurtis.nerv10.com/ "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." -- Dr. Suess -------- Original Message -------- > > Vic used camlocs all the way around. You can see photos here: > <http://lrosen.nerv10.com/Construct/SunNFun_2006/Vic%20RV10/CamLocs/index.html> > > Larry Rosen > > William Curtis wrote: > > > > > >> Guys, > >> did anyone use camlocks for the bottom cowling mounts? > >> Michael > >> > > > > I am. Two per side on a 0.63 base. Four of each of the below: > > > > 244-16 Floting Receptacle 2.89 > > 4002-4 Camloc Stud 2.45 > > 4002-O Camloc Grommet 1.53 > > R4G Snap Rings 0.20 > > > > I used these on the horizontal sides of my Cardinal to replace the SouthCo fasteners and I like them a lot. Not enough however to use them in place of the hinges on the 10 except on the cowl bottom. > > > > The above prices are from Spruce, however if you go to OSH or Sun-N-Fun you can get them at the Aeromart for less. If you want to pay even more you can get the adjustable receptacle version but since the -4 stud will fit the thickness range of our cowling, I don't see any reason to use them. > > > > William > > http://wcurtis.nerv10.com/ > > "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." > > -- Dr. Suess ________________________________________________________________________________
From: John Ackerman <johnag5b(at)cableone.net>
Subject: Re: counter sinking canopy holes
Date: Mar 04, 2008
Greetings, Ron =46rom the Avery Catalog : "Special RV-10 countersink cutter for countersinking holes in cabin roof for seat belt anchor points. High speed 100=B0 3-flute precision ground 5/16" pilot X 5/8" body diameter X 1/4-28 threads." Part #C516 Avery Tools, L.P. 111 Aviator Dr Ft. Worth, Texas 76179 USA 1-800-652-8379 Marlys and John Ackerman 40458 - and the top is epoxied on today! On Mar 2, 2008, at 7:43 PM, McGANN, Ron wrote: > > > Forwarded second attempt from Patrick: > > Hi there John, could you please indicate the part number for the > countersink available from Avery as I would like to obtain one to be > sent downunder. > ________________________________________________________________________________
From: "DejaVu" <wvu(at)ameritel.net>
Subject: Re: Lower Cowl Mounts
Date: Mar 04, 2008
Hey who's using hinges for the lower cowl?! Don't do it. Actually, I'm chiming in late but seems like most folks are aware of this issue. Hinges were not a problem in my -6. They did not last past 5 hours in the -10. They eyelets broke one at a time. Just on the left side. I replaced that side with nutplates/screws then the other side started to break, one eyelet at a time. Eventually I fixed both sides. I made the plates out of the old instrument panel. Didn't need shims since the hinge halves lined up in the first place. I didn't want to patch up the existing holes on the cowl where the rivets used to be so I used six #8 nutplates/screws per side, with C/S washers. Very solid as you would imagine. Anh N591VU - flying ----- Original Message ----- From: "Deems Davis" <deemsdavis(at)cox.net> Sent: Monday, March 03, 2008 7:46 PM Subject: Re: RV10-List: Lower Cowl Mounts > > > Scott here's a link to 2 photos (click next to see the 2nd) > http://deemsrv10.com/album/Sec%2047%20Spinner%20and%20Cowling/slides/DSC04175.html > I've since trimmed the inside portion of the 'flange' so that it doesn't > stick out and interfere with the air exiting the lower cowl. (A John Cox > suggestion) > > Deems Davis # 406 > 'Its all done....Its just not put together' > http://deemsrv10.com/ > > Scott Schmidt wrote: >> >> Can someone point me to some photos. This is a modification I would like >> to make. I've already lost 2 eyelets. >> Scott Schmidt >> scottmschmidt(at)yahoo.com >> >> On Mar 3, 2008, at 12:30 PM, Rick Sked wrote: >> >> >> I made mine out of .063 aluminum, I think I used #8, three per side. >> >> Rick Sked >> 40185 >> ----- Original Message ----- >> From: "Tim Olson" <Tim(at)MyRV10.com> >> To: rv10-list(at)matronics.com >> Sent: Monday, March 3, 2008 8:33:55 AM (GMT-0800) America/Los_Angeles >> Subject: Re: RV10-List: Lower Cowl Mounts >> >> >> Not countersunk screws....round head screws. Yes, >> they're holding up great for people, and there are >> some now that I know personally (I'll let them speak up >> if they wish) who didn't install them until after they >> had issues with the hinges. But, there really are >> no problems with nutplates and screws...it's really >> secure. >> >> >> Tim Olson - RV-10 N104CD - Flying >> >> >> >> Vernon Smith wrote: >> Looking through some of the old postings, I found some discussion on >> replacing the lower cowl mounts with nutplates and screws. Are these >> modified mounts still holding up well during flight? Also were #10 >> countersunk screws and nut plates used? And finally what was the mounting >> plate made from? >> Thanks, >> >> Vern Smith (#324) >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> > > > ________________________________________________________________________________
Date: Mar 05, 2008
From: Larry Rosen <LarryRosen(at)comcast.net>
Subject: Re: Lower Cowl Mounts
Hate to say it, but William you are correct :-) . I took a look at the original photos and the bottom ones do not have the same markings on that as the camlocs on the sides. Larry William Curtis wrote: > > Larry, > > Those bottom ones don't look like Camlocs, they look like screws with Tinnerman washers. I know Vic sold the plane but is he still on the list? > > William > http://wcurtis.nerv10.com/ > "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." > -- Dr. Suess > > -------- Original Message -------- > >> >> Vic used camlocs all the way around. You can see photos here: >> <http://lrosen.nerv10.com/Construct/SunNFun_2006/Vic%20RV10/CamLocs/index.html> >> >> Larry Rosen >> >> William Curtis wrote: >> >>> >>> >>> >>>> Guys, >>>> did anyone use camlocks for the bottom cowling mounts? >>>> Michael >>>> >>>> >>> I am. Two per side on a 0.63 base. Four of each of the below: >>> >>> 244-16 Floting Receptacle 2.89 >>> 4002-4 Camloc Stud 2.45 >>> 4002-O Camloc Grommet 1.53 >>> R4G Snap Rings 0.20 >>> >>> I used these on the horizontal sides of my Cardinal to replace the SouthCo fasteners and I like them a lot. Not enough however to use them in place of the hinges on the 10 except on the cowl bottom. >>> >>> The above prices are from Spruce, however if you go to OSH or Sun-N-Fun you can get them at the Aeromart for less. If you want to pay even more you can get the adjustable receptacle version but since the -4 stud will fit the thickness range of our cowling, I don't see any reason to use them. >>> >>> William >>> http://wcurtis.nerv10.com/ >>> "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." >>> -- Dr. Suess >>> > > > ________________________________________________________________________________
From: Barry Marz <blalmarz(at)embarqmail.com>
Subject: Shoulder Harness Hardpoint
Date: Mar 05, 2008
I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com ________________________________________________________________________________
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Date: Mar 05, 2008
Subject: Shoulder Harness Hardpoint
I talked to my TC a while back about this subject and while he isn't a composite guy, he thought that it made more sense to make the hardpoint on the exterior or the cabin top. I planned to look into it more once I got to that point but this seems to be a good time to discuss. So what do the composite guys like Gary and Dave think? In adding a hard point for seatbelts to the canopy should it be from the inside or outside? Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz Sent: Wednesday, March 05, 2008 7:47 AM Subject: RV10-List: Shoulder Harness Hardpoint I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com ________________________________________________________________________________
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Date: Mar 05, 2008
Subject: Another lesson with windows
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From: "Bob Leffler" <rv(at)thelefflers.com>
Subject: Shoulder Harness Hardpoint
Date: Mar 05, 2008
If I recall what Dave Saylor did to his, when I took the class last month, I believe that he drilled about 1.5"-2.0" core from the inside, then filled with flox. Basically duplicating how the front belt attach points are constructed. Was your TC recommending you put a plate on top of the canopy? bob -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Wednesday, March 05, 2008 9:23 AM Subject: RE: RV10-List: Shoulder Harness Hardpoint I talked to my TC a while back about this subject and while he isn't a composite guy, he thought that it made more sense to make the hardpoint on the exterior or the cabin top. I planned to look into it more once I got to that point but this seems to be a good time to discuss. So what do the composite guys like Gary and Dave think? In adding a hard point for seatbelts to the canopy should it be from the inside or outside? Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz Sent: Wednesday, March 05, 2008 7:47 AM Subject: RV10-List: Shoulder Harness Hardpoint I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com __________ Information from ESET NOD32 Antivirus, version of virus signature database 2923 (20080305) __________ The message was checked by ESET NOD32 Antivirus. __________ Information from ESET NOD32 Antivirus, version of virus signature database 2923 (20080305) __________ The message was checked by ESET NOD32 Antivirus. ________________________________________________________________________________
Subject: Re: Another lesson with windows
From: "orchidman" <gary(at)wingscc.com>
Date: Mar 05, 2008
Printer (like in printing press) suppliers can supply 95%. You should be able to get a gallon for almost nothing. -------- Gary Blankenbiller RV10 - # 40674 Fuselage SB (N410GB reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=167808#167808 ________________________________________________________________________________
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Date: Mar 05, 2008
Subject: Shoulder Harness Hardpoint
The flox method is fairly common and the easiest way to go. The question is, do you drill it out from the outside or from the inside as most have done. Seems that you would retain more of the inherent strength of the structure against a pull out if it was done from the exterior. Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Bob Leffler Sent: Wednesday, March 05, 2008 8:59 AM Subject: RE: RV10-List: Shoulder Harness Hardpoint If I recall what Dave Saylor did to his, when I took the class last month, I believe that he drilled about 1.5"-2.0" core from the inside, then filled with flox. Basically duplicating how the front belt attach points are constructed. Was your TC recommending you put a plate on top of the canopy? bob -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Wednesday, March 05, 2008 9:23 AM Subject: RE: RV10-List: Shoulder Harness Hardpoint I talked to my TC a while back about this subject and while he isn't a composite guy, he thought that it made more sense to make the hardpoint on the exterior or the cabin top. I planned to look into it more once I got to that point but this seems to be a good time to discuss. So what do the composite guys like Gary and Dave think? In adding a hard point for seatbelts to the canopy should it be from the inside or outside? Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz Sent: Wednesday, March 05, 2008 7:47 AM Subject: RV10-List: Shoulder Harness Hardpoint I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com __________ Information from ESET NOD32 Antivirus, version of virus signature database 2923 (20080305) __________ The message was checked by ESET NOD32 Antivirus. __________ Information from ESET NOD32 Antivirus, version of virus signature database 2923 (20080305) __________ The message was checked by ESET NOD32 Antivirus. ________________________________________________________________________________
From: "gary" <speckter(at)comcast.net>
Subject: Shoulder Harness Hardpoint
Date: Mar 05, 2008
I think that we are missing the engineering that went into the design of the hard point built into the current structure. Typically the foam is removed in the area around the hole and filled with reinforcing material like chopped fiber or flox. This is the same thing that the Glasair folks do. This structure is sufficient to hold the shoulder harness. Additionally, fiberglass structures are meant to flex long before they break. Remember the wing on the Voyager during take off. By putting a metal washer on the outside of the structure you are creating a failure point at the outer edge. Think of it like this. If you took a one foot long tube and slid it over your fiberglass/graphite fishing rod and flexed it close to the failure point, it would fail prematurely at the end of the tube because it was not allowed to flex inside the tube. IMHO no additional structure is needed for the harness. Gary 40274 It is all together, now what? -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Wednesday, March 05, 2008 9:23 AM Subject: RE: RV10-List: Shoulder Harness Hardpoint I talked to my TC a while back about this subject and while he isn't a composite guy, he thought that it made more sense to make the hardpoint on the exterior or the cabin top. I planned to look into it more once I got to that point but this seems to be a good time to discuss. So what do the composite guys like Gary and Dave think? In adding a hard point for seatbelts to the canopy should it be from the inside or outside? Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz Sent: Wednesday, March 05, 2008 7:47 AM Subject: RV10-List: Shoulder Harness Hardpoint I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com ________________________________________________________________________________
From: "Marcus Cooper" <coop85(at)cableone.net>
Subject: Shoulder Harness Hardpoint
Date: Mar 05, 2008
FWIW I agree with Gary 100%. The area is already beefed up and if I remember correctly the points were solid glass with no foam. I was starting to wonder if folks were talking about additional points for a different harness system. Provided that's not the case, I think the structure is good to go as is. Marcus 40286 Just about to hit 250 hours and loving it. -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of gary Sent: Wednesday, March 05, 2008 3:41 PM Subject: RE: RV10-List: Shoulder Harness Hardpoint I think that we are missing the engineering that went into the design of the hard point built into the current structure. Typically the foam is removed in the area around the hole and filled with reinforcing material like chopped fiber or flox. This is the same thing that the Glasair folks do. This structure is sufficient to hold the shoulder harness. Additionally, fiberglass structures are meant to flex long before they break. Remember the wing on the Voyager during take off. By putting a metal washer on the outside of the structure you are creating a failure point at the outer edge. Think of it like this. If you took a one foot long tube and slid it over your fiberglass/graphite fishing rod and flexed it close to the failure point, it would fail prematurely at the end of the tube because it was not allowed to flex inside the tube. IMHO no additional structure is needed for the harness. Gary 40274 It is all together, now what? -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Wednesday, March 05, 2008 9:23 AM Subject: RE: RV10-List: Shoulder Harness Hardpoint I talked to my TC a while back about this subject and while he isn't a composite guy, he thought that it made more sense to make the hardpoint on the exterior or the cabin top. I planned to look into it more once I got to that point but this seems to be a good time to discuss. So what do the composite guys like Gary and Dave think? In adding a hard point for seatbelts to the canopy should it be from the inside or outside? Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz Sent: Wednesday, March 05, 2008 7:47 AM Subject: RV10-List: Shoulder Harness Hardpoint I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com ________________________________________________________________________________
Date: Mar 05, 2008
Subject: Shoulder Harness Hardpoint
From: "William Curtis" <wcurtis(at)nerv10.com>
The flox method may be common and while it is stronger than epoxy alone, if you read section 49, the Seats & Seat Belt section of the plans, the seat-belt hard-points are NOT filled with flox. According to page 49-02 "These hard points are a solid lay-up of glass (they contain no core material), and appear lighter than the surrounding area." If you want to make additional hard-points, to duplicate the hard-points for the front seats you should use lay-up of fiberglass NOT flox. I will be putting 3 Point harness in the rear and will use a Dremel to remove the core material and to then rebuild with layers of fiberglass. William http://wcurtis.nerv10.com/ "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." -- Dr. Suess -------- Original Message -------- > > The flox method is fairly common and the easiest way to go. The question is, do you drill it out from the outside or from the inside as most have done. Seems that you would retain more of the inherent strength of the structure against a pull out if it was done from the exterior. > > Michael > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Bob Leffler > Sent: Wednesday, March 05, 2008 8:59 AM > To: rv10-list(at)matronics.com > Subject: RE: RV10-List: Shoulder Harness Hardpoint > > > If I recall what Dave Saylor did to his, when I took the class last month, I > believe that he drilled about 1.5"-2.0" core from the inside, then filled > with flox. Basically duplicating how the front belt attach points are > constructed. > > Was your TC recommending you put a plate on top of the canopy? > > bob > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder > (Michael Sausen) > Sent: Wednesday, March 05, 2008 9:23 AM > To: rv10-list(at)matronics.com > Subject: RE: RV10-List: Shoulder Harness Hardpoint > > > > I talked to my TC a while back about this subject and while he isn't a > composite guy, he thought that it made more sense to make the hardpoint on > the exterior or the cabin top. I planned to look into it more once I got to > that point but this seems to be a good time to discuss. > > So what do the composite guys like Gary and Dave think? In adding a hard > point for seatbelts to the canopy should it be from the inside or outside? > > Michael > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz > Sent: Wednesday, March 05, 2008 7:47 AM > To: RV10-List Digest Server > Subject: RV10-List: Shoulder Harness Hardpoint > > > I am wondering if the hard-point for the shoulder harness connection > needs to be reinforced or have a washer added on top, so it will work > when needed. Any thoughts? > > Barry Marz > 18735 Baseleg AVE. > FT. Myers, Fl 33917 > 239-567-2271 > blalmarz(at)embarqmail.com ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: OSH
Date: Mar 05, 2008
We have decided to camp at OSH this year. Are any plans developing to get spots in Camp Scholler or park the 10s together in airplane camping? ________________________________________________________________________________
From: "Bob Leffler" <rv(at)thelefflers.com>
Subject: OSH
Date: Mar 05, 2008
Yes, there should be a large contingent of us there. Bob and Gary have already started talking about RV-10 HQ 2008. Hopefully they'll get there early and stake out our sites again this year. I'm sure there will also be a few in airplane parking. From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of David McNeill Sent: Wednesday, March 05, 2008 10:04 PM Subject: RV10-List: OSH We have decided to camp at OSH this year. Are any plans developing to get spots in Camp Scholler or park the 10s together in airplane camping? __________ Information from ESET NOD32 Antivirus, version of virus signature database 2925 (20080305) __________ The message was checked by ESET NOD32 Antivirus. ________________________________________________________________________________
Subject: OSH
Date: Mar 05, 2008
From: "Condrey, Bob (US SSA)" <bob.condrey(at)baesystems.com>
Gary and I plan on doing essentially the same thing as last year, only question is exactly what day we'll "claim our ground". The past couple of years we've gotten the sites on the Tuesday before opening weekend. For some reason last year there were a lot more people there early and combined with the 20 or so RV-10 spots, we wound up with the spread out a little. After we get into April I'll take a poll and then post exactly what we're doing. Bob _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of David McNeill Sent: Wednesday, March 05, 2008 7:04 PM Subject: RV10-List: OSH We have decided to camp at OSH this year. Are any plans developing to get spots in Camp Scholler or park the 10s together in airplane camping? ________________________________________________________________________________
From: neil <ncol(at)xtra.co.nz>
Subject: Re: OSH
Date: Mar 06, 2008
Hi Guys My wife & I are hoping to be at Osh for the first time this year. However, for weight reasons we are not able to bring any camping gear. We would love to stay on the field with everyone else, rather than a hotel miles away (probably fully booked by now anyhow). Does any one know how we could hire a tent or something for a couple of days? We plan on arriving on the Monday, but have to leave Thurs AM. I presume there is somewhere to wash, & I'm sure food won't be a problem. We are really looking forward to meeting so many of you that we have emailed / talked to over the last year or so. Neil & Sarah ZK-RVT On 6 Mar 2008, at 17:00, Bob Leffler wrote: > Yes, there should be a large contingent of us there.-- Bob and Gary > have already started talking about RV-10 HQ 2008.- Hopefully they=92ll > get there early and stake out our sites again this year.- I=92m sure > there will also be a few in airplane parking. > - > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of David > McNeill > Sent: Wednesday, March 05, 2008 10:04 PM > To: rv10-list(at)matronics.com > Subject: RV10-List: OSH > - > We- have decided to camp at OSH this year. Are any plans developing to > get spots in Camp Scholler or park the 10s together in airplane > camping? > - > - > http://www.matronics.com/Navigator?RV10-List > http://forums.matronics.com > http://www.matronics.com/contribution > - > > > __________ Information from ESET NOD32 Antivirus, version of virus > signature database 2925 (20080305) __________ > > The message was checked by ESET NOD32 Antivirus. > > > __________ Information from ESET NOD32 Antivirus, version of virus > signature database 2925 (20080305) __________ > > The message was checked by ESET NOD32 Antivirus. > > ________________________________________________________________________________
From: "Bob Leffler" <rv(at)thelefflers.com>
Subject: OSH
Date: Mar 06, 2008
I was able to rent a trailer from Van Boxtel. They will deliver it from Green Bay to Osh for an additional fee. http://www.vanboxtelrv.com/ Their RVs (4 wheel kind) are a little expensive ($1,700) for the week, but their tent campers and travel trailers were reasonable. From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of neil Sent: Thursday, March 06, 2008 1:31 AM Subject: Re: RV10-List: OSH Hi Guys My wife & I are hoping to be at Osh for the first time this year. However, for weight reasons we are not able to bring any camping gear. We would love to stay on the field with everyone else, rather than a hotel miles away (probably fully booked by now anyhow). Does any one know how we could hire a tent or something for a couple of days? We plan on arriving on the Monday, but have to leave Thurs AM. I presume there is somewhere to wash, & I'm sure food won't be a problem. We are really looking forward to meeting so many of you that we have emailed / talked to over the last year or so. Neil & Sarah ZK-RVT On 6 Mar 2008, at 17:00, Bob Leffler wrote: Yes, there should be a large contingent of us there. Bob and Gary have already started talking about RV-10 HQ 2008. Hopefully they'll get there early and stake out our sites again this year. I'm sure there will also be a few in airplane parking. From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of David McNeill Sent: Wednesday, March 05, 2008 10:04 PM Subject: RV10-List: OSH We have decided to camp at OSH this year. Are any plans developing to get spots in Camp Scholler or park the 10s together in airplane camping? http://www.matronics.com/Navigator?RV10-List http://forums.matronics.com http://www.matronics.com/contribution __________ Information from ESET NOD32 Antivirus, version of virus signature database 2925 (20080305) __________ The message was checked by ESET NOD32 Antivirus. __________ Information from ESET NOD32 Antivirus, version of virus signature database 2925 (20080305) __________ The message was checked by ESET NOD32 Antivirus. http://www.matronics.com/Navigator?RV10-List http://forums.matronics.com http://www.matronics.com/contribution ________________________________________________________________________________
Subject: Shoulder harnesses
Date: Mar 06, 2008
From: "Dawson-Townsend,Timothy" <tdawson-townsend(at)aurora.aero>
Remind me what the motivation is to create new hardpoints on the fiberglass for rear seat harnesses, instead of following the plans method? TDT 40025 Tim Dawson-Townsend tdt(at)aurora.aero 617-500-4812 (office) 617-905-4800 (mobile) ________________________________________________________________________________
Subject: Camping gear
Date: Mar 06, 2008
From: "Dawson-Townsend,Timothy" <tdawson-townsend(at)aurora.aero>
Neil & Sarah: One option would be to visit the Wal-Mart store near the field and buy yourselves a cheap tent for $50, and a couple sleeping pads and sheets for another $45. (Probably no need for sleeping bags in an Oshkosh summer!) Then just give them away to someone when it's time to leave . . . TDT 40025 Hi Guys My wife & I are hoping to be at Osh for the first time this year. However, for weight reasons we are not able to bring any camping gear. We would love to stay on the field with everyone else, rather than a hotel miles away (probably fully booked by now anyhow). Does any one know how we could hire a tent or something for a couple of days? We plan on arriving on the Monday, but have to leave Thurs AM. I presume there is somewhere to wash, & I'm sure food won't be a problem. We are really looking forward to meeting so many of you that we have emailed / talked to over the last year or so. Neil & Sarah ZK-RVT ________________________________________________________________________________
Subject: Camping gear
Date: Mar 06, 2008
From: "Phillips, Jack" <Jack.Phillips(at)cardinalhealth.com>
Or go to the UPS store on the field at OSH and ship them to your home. It might also be possible to ship comaping gear to OSH and pick it up when you arrive. I usually just ship it to a friend who lives within driving distance of OSH and he shows up with my gear and his and we camp together Jack Phillips # 610 Still waiting on the wing kit to arrive _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dawson-Townsend,Timothy Sent: Thursday, March 06, 2008 8:11 AM Subject: RV10-List: Camping gear Neil & Sarah: One option would be to visit the Wal-Mart store near the field and buy yourselves a cheap tent for $50, and a couple sleeping pads and sheets for another $45. (Probably no need for sleeping bags in an Oshkosh summer!) Then just give them away to someone when it's time to leave . . . TDT 40025 Hi Guys My wife & I are hoping to be at Osh for the first time this year. However, for weight reasons we are not able to bring any camping gear. We would love to stay on the field with everyone else, rather than a hotel miles away (probably fully booked by now anyhow). Does any one know how we could hire a tent or something for a couple of days? We plan on arriving on the Monday, but have to leave Thurs AM. I presume there is somewhere to wash, & I'm sure food won't be a problem. We are really looking forward to meeting so many of you that we have emailed / talked to over the last year or so. Neil & Sarah ZK-RVT _________________________________________________ This message is for the designated recipient only and may contain privilege d, proprietary or otherwise private information. If you have received it in error, please notify the sender immediately and delete the original. Any other use of the email by you is p rohibited. Dansk - Deutsch - Espanol - Francais - Italiano - Japanese - Nederlands - N orsk - Portuguese ________________________________________________________________________________
From: "Bob Leffler" <rv(at)thelefflers.com>
Subject: Shoulder harnesses
Date: Mar 06, 2008
For belts like: http://www.inertialbelts.com/ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dawson-Townsend,Timothy Sent: Thursday, March 06, 2008 8:08 AM Subject: RV10-List: Shoulder harnesses Remind me what the motivation is to create new hardpoints on the fiberglass for rear seat harnesses, instead of following the plans method? TDT 40025 Tim Dawson-Townsend tdt(at)aurora.aero 617-500-4812 (office) 617-905-4800 (mobile) ________________________________________________________________________________
From: GRANSCOTT(at)aol.com
Date: Mar 06, 2008
Subject: Re: Camping gear
I think "ZK" is a long way to ship any gear either way...when you get to KOSH, there are stores near by where you can go, buy a tent etc., heck you can even take the bus to the NE corner and get off and walk through the security fence...walk about two blocks to a strip mall, buy all you need including a cooler and carry cart etc., and load it on the bus and make the trip back to the camp ground or camp with a friend...the items you'll need are not very expensive. The weather is usually hot and muggy in years past there have been some interesting thunderstorms in the area. So don't camp in a low area...I've been going to KOSH off and on since the 70's...been hot, buggy, cold and wet--and that was just one day and enjoyed every second of being there. Visit EAA's web site and you'll be briefed on what's there. The stuff sold in the EAA stores is a bit expensive compared to local vendors but you don't need to go off site to get some staples...there are bathrooms and shower houses but you'll need your own kit. Don't leave anything valuable unattended as things have a way at walking at KOSH. They do have security, but this is a public event and they do not have security like an airport. I think it's a good safe place but when you're with the public you don't want to leave your valuables in a tent and wonder. My son had his I-Pod go missing a few years ago from our tent and the person left our rain fly open after robbing us only to have a huge thunderstorm fill our tent and camping gear, making for a soggy, wet night at Camp Stoller. The area is huge, you can easily walk several miles from one end to the other (they do have some transportation aides and buses) and with 100,000 or more people per day going in and out it's occasionally a bit crazy. I don't know how others feel, but the food on the grounds is just OK, some aircraft clubs have dinners--book in advance, one EAA chapter has a pancake breakfast, at the seaplane basin is a great fish fly--I believe you can get tickets a head of time--the fried Perch is outstanding. You'll have a great time, it's the best place to meet and talk aviation. Most don't make it to the EAA Museum but since it's your first time going--please make a point to go over to the museum...believe it or not the EAA HQ/Museum is not near the convention...you've got to go look for it. If you've involved in a local Chapter, and your president is not attending, they can name you as there rep and you can be named to attend several closed meeting for Chapter Presidents. But once again it needs to happen a head of time...and I'm sure the RV group will help you in anyway they can... Patrick **************It's Tax Time! Get tips, forms, and advice on AOL Money & Finance. (http://money.aol.com/tax?NCID=aolprf00030000000001) ________________________________________________________________________________
Subject: OSH
Date: Mar 06, 2008
From: John Jessen <n212pj(at)gmail.com>
I think this year may be my first trip to OSH, as well. If someone is starting a list, please add my name. Not sure who else will join me at this point. Also, not sure how I'm arriving, whether by land or air, but will be camping. John J 40328 ________________________________________________________________________________
Date: Mar 06, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: Lower Cowl Mounts
This is passed on from Vic as a reply... From: Vicsyracuse I read the archives, but don't have time to monitor the list. Sorry. But I saw your question. I used the skybolt fasteners top and sides, and 5 #8 screws with tinnerman washers on the bottom on both sides of the air exit area. I did my rv-6 this way, and am doing the RV-7 the same. I used .063 for the aluminum on the 10, but am using .050 on the 7. Vic -- Tim Olson - RV-10 N104CD - Flying William Curtis wrote: > >> Guys, >> did anyone use camlocks for the bottom cowling mounts? >> Michael > > I am. Two per side on a 0.63 base. Four of each of the below: > > 244-16 Floting Receptacle 2.89 > 4002-4 Camloc Stud 2.45 > 4002-O Camloc Grommet 1.53 > R4G Snap Rings 0.20 > > I used these on the horizontal sides of my Cardinal to replace the SouthCo fasteners and I like them a lot. Not enough however to use them in place of the hinges on the 10 except on the cowl bottom. > > The above prices are from Spruce, however if you go to OSH or Sun-N-Fun you can get them at the Aeromart for less. If you want to pay even more you can get the adjustable receptacle version but since the -4 stud will fit the thickness range of our cowling, I don't see any reason to use them. > > William > http://wcurtis.nerv10.com/ > "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." > -- Dr. Suess > ________________________________________________________________________________
Date: Mar 06, 2008
From: "Pascal" <rv10builder(at)verizon.net>
Subject: Re: Camping gear
or someone can let Neil borrow an extra one from last year that wasn't given away ;-) If I could find a way out there I would certainly bring a couple of tents (they are small enough) and let someone borrow or have it. Also consider many may think the same way and Walmart will be out of tents.. than what? I personally would not feel comfortable "winging it", but may be a non issue if one is there early.. I will say Walmart does have great tents. I have done better in rain with my Walmart than my Coleman ever did.. Pascal wish I could go but have no way to get there ;-( ----- Original Message ----- From: Dawson-Townsend,Timothy To: rv10-list(at)matronics.com Sent: Thursday, March 06, 2008 5:10 AM Subject: RV10-List: Camping gear Neil & Sarah: One option would be to visit the Wal-Mart store near the field and buy yourselves a cheap tent for $50, and a couple sleeping pads and sheets for another $45. (Probably no need for sleeping bags in an Oshkosh summer!) Then just give them away to someone when it's time to leave . . . TDT 40025 Hi Guys My wife & I are hoping to be at Osh for the first time this year. However, for weight reasons we are not able to bring any camping gear. We would love to stay on the field with everyone else, rather than a hotel miles away (probably fully booked by now anyhow). Does any one know how we could hire a tent or something for a couple of days? We plan on arriving on the Monday, but have to leave Thurs AM. I presume there is somewhere to wash, & I'm sure food won't be a problem. We are really looking forward to meeting so many of you that we have emailed / talked to over the last year or so. Neil & Sarah ZK-RVT ________________________________________________________________________________
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Date: Mar 06, 2008
Subject: Shoulder Harness Hardpoint
Yep, we are talking about adding additional hardpoints in the rear just forward of the rear bulkhead cover to support a different mounting point for the rear seat belts. In my caser the reason for not using the factory location back in the tailcone is twofold. The first reason is because I will probably be using David's Amsafe or similar retractable belts for at least the rear seat passengers. The second is my hat shelf project eliminated the ability to run back to the longeron points. So just so we are clear, we are not talking about the factory hardpoint in the top, we are talking about ADDING harpoints. You can see David's approach at the link below. I believe he worked with some pretty smart guys in developing his method so my question is more to help me understand the rationale behind doing the work on the inside rather than the outside. http://www.inertialbelts.com/ Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Marcus Cooper Sent: Wednesday, March 05, 2008 6:03 PM Subject: RE: RV10-List: Shoulder Harness Hardpoint FWIW I agree with Gary 100%. The area is already beefed up and if I remember correctly the points were solid glass with no foam. I was starting to wonder if folks were talking about additional points for a different harness system. Provided that's not the case, I think the structure is good to go as is. Marcus 40286 Just about to hit 250 hours and loving it. -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of gary Sent: Wednesday, March 05, 2008 3:41 PM Subject: RE: RV10-List: Shoulder Harness Hardpoint I think that we are missing the engineering that went into the design of the hard point built into the current structure. Typically the foam is removed in the area around the hole and filled with reinforcing material like chopped fiber or flox. This is the same thing that the Glasair folks do. This structure is sufficient to hold the shoulder harness. Additionally, fiberglass structures are meant to flex long before they break. Remember the wing on the Voyager during take off. By putting a metal washer on the outside of the structure you are creating a failure point at the outer edge. Think of it like this. If you took a one foot long tube and slid it over your fiberglass/graphite fishing rod and flexed it close to the failure point, it would fail prematurely at the end of the tube because it was not allowed to flex inside the tube. IMHO no additional structure is needed for the harness. Gary 40274 It is all together, now what? -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Wednesday, March 05, 2008 9:23 AM Subject: RE: RV10-List: Shoulder Harness Hardpoint I talked to my TC a while back about this subject and while he isn't a composite guy, he thought that it made more sense to make the hardpoint on the exterior or the cabin top. I planned to look into it more once I got to that point but this seems to be a good time to discuss. So what do the composite guys like Gary and Dave think? In adding a hard point for seatbelts to the canopy should it be from the inside or outside? Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz Sent: Wednesday, March 05, 2008 7:47 AM Subject: RV10-List: Shoulder Harness Hardpoint I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com ________________________________________________________________________________
Subject: Re: Camping gear
From: "johngoodman" <johngoodman(at)earthlink.net>
Date: Mar 06, 2008
> I don't know how others feel, but the food on the grounds is just OK, That's the truth! I finally gave up last year and drove out for every meal. John -------- #40572 QB Fuselage, wings finished N711JG reserved Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168071#168071 ________________________________________________________________________________
From: "gary" <speckter(at)comcast.net>
Subject: Shoulder Harness Hardpoint
Date: Mar 06, 2008
The approach David used looks sound to me. I think that he worked on the inside because it is more forgiving of the additional layers of glass he used to cover the hard points. The head liner will not show those additional layers he used to connect all the hard points. Gary 40274 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Thursday, March 06, 2008 12:19 PM Subject: RE: RV10-List: Shoulder Harness Hardpoint Yep, we are talking about adding additional hardpoints in the rear just forward of the rear bulkhead cover to support a different mounting point for the rear seat belts. In my caser the reason for not using the factory location back in the tailcone is twofold. The first reason is because I will probably be using David's Amsafe or similar retractable belts for at least the rear seat passengers. The second is my hat shelf project eliminated the ability to run back to the longeron points. So just so we are clear, we are not talking about the factory hardpoint in the top, we are talking about ADDING harpoints. You can see David's approach at the link below. I believe he worked with some pretty smart guys in developing his method so my question is more to help me understand the rationale behind doing the work on the inside rather than the outside. http://www.inertialbelts.com/ Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Marcus Cooper Sent: Wednesday, March 05, 2008 6:03 PM Subject: RE: RV10-List: Shoulder Harness Hardpoint FWIW I agree with Gary 100%. The area is already beefed up and if I remember correctly the points were solid glass with no foam. I was starting to wonder if folks were talking about additional points for a different harness system. Provided that's not the case, I think the structure is good to go as is. Marcus 40286 Just about to hit 250 hours and loving it. -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of gary Sent: Wednesday, March 05, 2008 3:41 PM Subject: RE: RV10-List: Shoulder Harness Hardpoint I think that we are missing the engineering that went into the design of the hard point built into the current structure. Typically the foam is removed in the area around the hole and filled with reinforcing material like chopped fiber or flox. This is the same thing that the Glasair folks do. This structure is sufficient to hold the shoulder harness. Additionally, fiberglass structures are meant to flex long before they break. Remember the wing on the Voyager during take off. By putting a metal washer on the outside of the structure you are creating a failure point at the outer edge. Think of it like this. If you took a one foot long tube and slid it over your fiberglass/graphite fishing rod and flexed it close to the failure point, it would fail prematurely at the end of the tube because it was not allowed to flex inside the tube. IMHO no additional structure is needed for the harness. Gary 40274 It is all together, now what? -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of RV Builder (Michael Sausen) Sent: Wednesday, March 05, 2008 9:23 AM Subject: RE: RV10-List: Shoulder Harness Hardpoint I talked to my TC a while back about this subject and while he isn't a composite guy, he thought that it made more sense to make the hardpoint on the exterior or the cabin top. I planned to look into it more once I got to that point but this seems to be a good time to discuss. So what do the composite guys like Gary and Dave think? In adding a hard point for seatbelts to the canopy should it be from the inside or outside? Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Barry Marz Sent: Wednesday, March 05, 2008 7:47 AM Subject: RV10-List: Shoulder Harness Hardpoint I am wondering if the hard-point for the shoulder harness connection needs to be reinforced or have a washer added on top, so it will work when needed. Any thoughts? Barry Marz 18735 Baseleg AVE. FT. Myers, Fl 33917 239-567-2271 blalmarz(at)embarqmail.com ________________________________________________________________________________
From: <rv(at)thelefflers.com>
Subject: Re: Camping gear
Date: Mar 06, 2008
I can tell you that thanks to Brenda, Susan, Andrea, and several other spouses that I can't remember their names, the folks at RV-10 HQ ate quite well most of the week. If you like corn, you were in heaven, thanks to Adrian. > > From: "johngoodman" <johngoodman(at)earthlink.net> > Date: 2008/03/06 Thu PM 02:08:20 EST > To: rv10-list(at)matronics.com > Subject: RV10-List: Re: Camping gear > > > > > I don't know how others feel, but the food on the grounds is just OK, > > > That's the truth! I finally gave up last year and drove out for every meal. > > John > > -------- > #40572 QB Fuselage, wings finished > N711JG reserved > ________________________________________________________________________________
From: "eagerlee" <eagerlee(at)comcast.net>
Subject: Re: Another lesson with windows
Date: Mar 06, 2008
I got 99% iso alcohol from Safeway Supermarket pharmacy shelves. Paul Hahn ________________________________________________________________________________
Subject: Lower Cowl Mounts
Date: Mar 07, 2008
From: "McGANN, Ron" <ron.mcgann(at)baesystems.com>
Has anyone tried stainless steel piano hinge on the lower cowl rather than the standard aluminium ones? If not, I will give it a try. Cheers, Ron Finshing the cowl -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of DejaVu Sent: Wednesday, 5 March 2008 2:14 PM Subject: Re: RV10-List: Lower Cowl Mounts Hey who's using hinges for the lower cowl?! Don't do it. Actually, I'm chiming in late but seems like most folks are aware of this issue. Hinges were not a problem in my -6. They did not last past 5 hours in the -10. They eyelets broke one at a time. Just on the left side. I replaced that side with nutplates/screws then the other side started to break, one eyelet at a time. Eventually I fixed both sides. I made the plates out of the old instrument panel. Didn't need shims since the hinge halves lined up in the first place. I didn't want to patch up the existing holes on the cowl where the rivets used to be so I used six #8 nutplates/screws per side, with C/S washers. Very solid as you would imagine. Anh N591VU - flying ----- Original Message ----- From: "Deems Davis" <deemsdavis(at)cox.net> Sent: Monday, March 03, 2008 7:46 PM Subject: Re: RV10-List: Lower Cowl Mounts > > > Scott here's a link to 2 photos (click next to see the 2nd) > http://deemsrv10.com/album/Sec%2047%20Spinner%20and%20Cowling/slides/DSC 04175.html > I've since trimmed the inside portion of the 'flange' so that it doesn't > stick out and interfere with the air exiting the lower cowl. (A John Cox > suggestion) > > Deems Davis # 406 > 'Its all done....Its just not put together' > http://deemsrv10.com/ > > Scott Schmidt wrote: >> >> Can someone point me to some photos. This is a modification I would like >> to make. I've already lost 2 eyelets. >> Scott Schmidt >> scottmschmidt(at)yahoo.com >> >> On Mar 3, 2008, at 12:30 PM, Rick Sked wrote: >> >> >> I made mine out of .063 aluminum, I think I used #8, three per side. >> >> Rick Sked >> 40185 >> ----- Original Message ----- >> From: "Tim Olson" <Tim(at)MyRV10.com> >> To: rv10-list(at)matronics.com >> Sent: Monday, March 3, 2008 8:33:55 AM (GMT-0800) America/Los_Angeles >> Subject: Re: RV10-List: Lower Cowl Mounts >> >> >> Not countersunk screws....round head screws. Yes, >> they're holding up great for people, and there are >> some now that I know personally (I'll let them speak up >> if they wish) who didn't install them until after they >> had issues with the hinges. But, there really are >> no problems with nutplates and screws...it's really >> secure. >> >> >> Tim Olson - RV-10 N104CD - Flying >> >> >> >> Vernon Smith wrote: >> Looking through some of the old postings, I found some discussion on >> replacing the lower cowl mounts with nutplates and screws. Are these >> modified mounts still holding up well during flight? Also were #10 >> countersunk screws and nut plates used? And finally what was the mounting >> plate made from? >> Thanks, >> >> Vern Smith (#324) >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> > > > "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." ________________________________________________________________________________
Subject: Re: Camping gear
Date: Mar 06, 2008
From: "John W. Cox" <johnwcox(at)pacificnw.com>
I for one found the friendliness of the group and the quality of food beyond question. I concur that the EAA provided vending choices "On Campus" to be only OK. So I concluded this comment was not the ladies of RV-10 HQ but rather the high priced, mediocre concessionaires. I too ate most breakfasts and most dinners off campus. The only consistent exception was a soft ice-cream cone each afternoon and a trip with friends to the trunk of my car where I had an iced stash of bottle water and YES, cold Wisconsin suds and other sundry Air Show watching food products. Those of you who rallied round the trunk know that I have dialed in OSH. Several of the EAA local chapters in our area chose to rendezvous each night at a quality restaurant around the greater OSH area. Often that locale can be far south as Fond du Lac or up into Appleton. The Warbird crowd I have been seen slumming with, tends to pillage the local restaurants around the UW-Oshkosh campus. We might just start a list of twenty of the best restaurants found. Each year the internet connection capability improves substantially. Why I can even remember when there was no McDonalds on the grounds. Years ago there used to be a Walmart right up the street. It is now closed but the next closest one is about 20 miles south of RV-10 Headquarters on the West side of State Highway 41 (which is right outside the front entrance). It is where that water, beer and sundry items are acquired. As Mike Sausen can tell you, I ship ahead all my clothing inside a large cooler. The cooler gets immediately converted upon touchdown in Wisconsin. Bob & Bob & Tim, I for one have appreciated your efforts... And you too Michael. John Cox #40600 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of rv(at)thelefflers.com Sent: Thursday, March 06, 2008 12:42 PM Subject: Re: RV10-List: Re: Camping gear I can tell you that thanks to Brenda, Susan, Andrea, and several other spouses that I can't remember their names, the folks at RV-10 HQ ate quite well most of the week. If you like corn, you were in heaven, thanks to Adrian. > > From: "johngoodman" <johngoodman(at)earthlink.net> > Date: 2008/03/06 Thu PM 02:08:20 EST > To: rv10-list(at)matronics.com > Subject: RV10-List: Re: Camping gear > > > > > I don't know how others feel, but the food on the grounds is just OK, > > > That's the truth! I finally gave up last year and drove out for every meal. > > John > > -------- > #40572 QB Fuselage, wings finished > N711JG reserved ________________________________________________________________________________
Subject: SJ Cowl, BA Prop and Spinner Issues
Date: Mar 06, 2008
From: "Robin Marks" <robin1(at)mrmoisture.com>
Dear list, My -10 build includes the SJ Cowl and a Hartzell BA prop. My understanding is that the James Cowl requires a 14" spinner. I know that Deems and others with the James Cowl are using different props that seem to ship with the spinner. Nice for them! I have sourced a Hartzell A-2297 metal spinner which Hartzell says is 13.9" x 17.6". I am not sure what I am more surprised about Hartzell not having a single photo, rendering or dimensional drawing / spec sheet on the spinner or that they want either side of $2,000 for the spinner. (Polished $2,073, unpolished $1,791). Geeeez Is there anyone out there using the James cowl/Hartzell BA combination that has solved this issue already? BTW I have contacted Whirl Wind, Aero Composites & UHS and none of them have, make or sell spinners for this application. Thanks, Robin RV-10 Plenum attached Cowl on its way Panel on its way Bankruptcy on its way ________________________________________________________________________________
From: "Carl Froehlich" <carl.froehlich(at)cox.net>
Subject: SJ Cowl, BA Prop and Spinner Issues
Date: Mar 06, 2008
I contacted Hartzell and they confirmed the A-2297 is the right spinner for the Van's BA Hartzell prop and the Sam James cowl. I purchased a new polished Hartzell A-2297 spinner for $885 from Mustang Aeronautics. The unpolished version is $785. Here is the contact information: Chris Tieman Mustang Aeronautics, Inc. 1470 Temple City Troy, MI 48084 (248) 649-6818 www.MustangAero.com Carl Froehlich RV-10 (wings) RV-8A (400 hrs) -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Robin Marks Sent: Thursday, March 06, 2008 6:50 PM Subject: RV10-List: SJ Cowl, BA Prop and Spinner Issues Dear list, My -10 build includes the SJ Cowl and a Hartzell BA prop. My understanding is that the James Cowl requires a 14" spinner. I know that Deems and others with the James Cowl are using different props that seem to ship with the spinner. Nice for them! I have sourced a Hartzell A-2297 metal spinner which Hartzell says is 13.9" x 17.6". I am not sure what I am more surprised about Hartzell not having a single photo, rendering or dimensional drawing / spec sheet on the spinner or that they want either side of $2,000 for the spinner. (Polished $2,073, unpolished $1,791). Geeeez Is there anyone out there using the James cowl/Hartzell BA combination that has solved this issue already? BTW I have contacted Whirl Wind, Aero Composites & UHS and none of them have, make or sell spinners for this application. Thanks, Robin RV-10 Plenum attached Cowl on its way Panel on its way Bankruptcy on its way ________________________________________________________________________________
Date: Mar 06, 2008
From: PJ Seipel <seipel(at)seznam.cz>
Subject: Re: SJ Cowl, BA Prop and Spinner Issues
Yeah, buy it from Mustang Aeronautics. I paid $885 + shipping for the polished version. Best price I could find. PJ Seipel RV-10 #40032 Carl Froehlich wrote: > > I contacted Hartzell and they confirmed the A-2297 is the right spinner for > the Van's BA Hartzell prop and the Sam James cowl. > > I purchased a new polished Hartzell A-2297 spinner for $885 from Mustang > Aeronautics. The unpolished version is $785. Here is the contact > information: > Chris Tieman > Mustang Aeronautics, Inc. > 1470 Temple City > Troy, MI 48084 > (248) 649-6818 > www.MustangAero.com > > Carl Froehlich > RV-10 (wings) > RV-8A (400 hrs) > > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Robin Marks > Sent: Thursday, March 06, 2008 6:50 PM > To: rv10-list(at)matronics.com > Subject: RV10-List: SJ Cowl, BA Prop and Spinner Issues > > > Dear list, > My -10 build includes the SJ Cowl and a Hartzell BA prop. My > understanding is that the James Cowl requires a 14" spinner. I know that > Deems and others with the James Cowl are using different props that seem > to ship with the spinner. Nice for them! > I have sourced a Hartzell A-2297 metal spinner which Hartzell > says is 13.9" x 17.6". I am not sure what I am more surprised about > Hartzell not having a single photo, rendering or dimensional drawing / > spec sheet on the spinner or that they want either side of $2,000 for > the spinner. (Polished $2,073, unpolished $1,791). Geeeez > Is there anyone out there using the James cowl/Hartzell BA > combination that has solved this issue already? > BTW I have contacted Whirl Wind, Aero Composites & UHS and none > of them have, make or sell spinners for this application. > > Thanks, > Robin > RV-10 > Plenum attached > Cowl on its way > Panel on its way > Bankruptcy on its way > > > ________________________________________________________________________________
From: "Rene" <rene(at)felker.com>
Subject: Death of Van's Kit 40322
Date: Mar 06, 2008
I am glade to announce that today kit 40322 died and in its place N423CF arose. Yes, first flight was today. Very exciting and a real milestone. Did not fly hands off, heavy left wing.......gives me something to work on. Rene' N423CF Flying 801-721-6080 ________________________________________________________________________________
Subject: SJ Cowl, BA Prop and Spinner Issues
Date: Mar 06, 2008
From: "Robin Marks" <robin1(at)mrmoisture.com>
His price has increased to $915.00 plus shipping for the polished which is still a heck of a lot better than $2,100.00 Thanks, Robin -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of PJ Seipel Sent: Thursday, March 06, 2008 5:56 PM Subject: Re: RV10-List: SJ Cowl, BA Prop and Spinner Issues Yeah, buy it from Mustang Aeronautics. I paid $885 + shipping for the polished version. Best price I could find. PJ Seipel RV-10 #40032 Carl Froehlich wrote: > > I contacted Hartzell and they confirmed the A-2297 is the right spinner for > the Van's BA Hartzell prop and the Sam James cowl. > > I purchased a new polished Hartzell A-2297 spinner for $885 from Mustang > Aeronautics. The unpolished version is $785. Here is the contact > information: > Chris Tieman > Mustang Aeronautics, Inc. > 1470 Temple City > Troy, MI 48084 > (248) 649-6818 > www.MustangAero.com > > Carl Froehlich > RV-10 (wings) > RV-8A (400 hrs) > > > -----Original Message----- > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Robin Marks > Sent: Thursday, March 06, 2008 6:50 PM > To: rv10-list(at)matronics.com > Subject: RV10-List: SJ Cowl, BA Prop and Spinner Issues > > > Dear list, > My -10 build includes the SJ Cowl and a Hartzell BA prop. My > understanding is that the James Cowl requires a 14" spinner. I know that > Deems and others with the James Cowl are using different props that seem > to ship with the spinner. Nice for them! > I have sourced a Hartzell A-2297 metal spinner which Hartzell > says is 13.9" x 17.6". I am not sure what I am more surprised about > Hartzell not having a single photo, rendering or dimensional drawing / > spec sheet on the spinner or that they want either side of $2,000 for > the spinner. (Polished $2,073, unpolished $1,791). Geeeez > Is there anyone out there using the James cowl/Hartzell BA > combination that has solved this issue already? > BTW I have contacted Whirl Wind, Aero Composites & UHS and none > of them have, make or sell spinners for this application. > > Thanks, > Robin > RV-10 > Plenum attached > Cowl on its way > Panel on its way > Bankruptcy on its way > > > ________________________________________________________________________________
From: Jesse Saint <jesse(at)saintaviation.com>
Subject: Re: Death of Van's Kit 40322
Date: Mar 06, 2008
Congratulations! Any pictures? Jesse Saint Saint Aviation, Inc. jesse(at)saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Mar 6, 2008, at 9:35 PM, Rene wrote: > > I am glade to announce that today kit 40322 died and in its place > N423CF > arose. > > Yes, first flight was today. Very exciting and a real milestone. > Did not > fly hands off, heavy left wing.......gives me something to work on. > > Rene' > N423CF Flying > 801-721-6080 > > ________________________________________________________________________________
Date: Mar 06, 2008
From: Robert Wright <flywrights(at)yahoo.com>
Subject: to Sun-N-Fun
Anyone going to Sun-N-Fun through coastal Georgia please stop by KLHW near Savannah and let's have lunch! http://airnav.com/airport/KLHW It's public use, though. NO PPR! If I get some interest I'll ask to see if the FBO will give some sort of fuel discount for Sun-N-Fun goers. If nothing else, we're having a fly-in 26 April. This is a new joint-use facility between the Army and the county based at the aged Wright Army Airfield. Rob Wright #392 Finish and FFWD as parts come in Be a better friend, newshound, and know-it-all with Yahoo! Mobile. Try it now. http://mobile.yahoo.com/;_ylt=Ahu06i62sR8HDtDypao8Wcj9tAcJ ________________________________________________________________________________
From: "Rene" <rene(at)felker.com>
Subject: Death of Van's Kit 40322
Date: Mar 06, 2008
This is my favorite picture. The ground crew did a great job at making sure everything was working right.....pictures, not so much. But I have not seen them all yet...... Rene' 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jesse Saint Sent: Thursday, March 06, 2008 8:16 PM Subject: Re: RV10-List: Death of Van's Kit 40322 Congratulations! Any pictures? Jesse Saint Saint Aviation, Inc. jesse(at)saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Mar 6, 2008, at 9:35 PM, Rene wrote: > > I am glade to announce that today kit 40322 died and in its place > N423CF > arose. > > Yes, first flight was today. Very exciting and a real milestone. > Did not > fly hands off, heavy left wing.......gives me something to work on. > > Rene' > N423CF Flying > 801-721-6080 > > ________________________________________________________________________________
From: "Rene" <rene(at)felker.com>
Subject: First FlightRigging Questions
Date: Mar 06, 2008
OK, need some opinions........ I was very excited about my first flight today, but did have a heavy wing and used a lot of nose down trim. It had me concerned. So tonight I went through the archives and I think I have it figured out.... Heavy wing, single pilot and.......only used right fuel tank during first flight. Not planning on switching tanks until the second flight. At the end of the flight I had a full left tank and ~ 15 gallons in the right tank. Can this type of in-balance lead to a very heavy left wing? Trim could not correct it. Elevator trim, needed to use a lot of nose down trim? At takeoff I added about 1 second, maybe two of trim. Also had almost full nose down trim during cruse. Is this normal? During transition training I don't remember using as much. After the flight, we went back over the elevator trim adjustment and it is per plans...35degrees. Rene' 801-721-6080 ________________________________________________________________________________
From: "Steven DiNieri" <capsteve(at)adelphia.net>
Subject: Re: Death of Van's Kit 40322
Date: Mar 07, 2008
awesome.. congrats.. steve ----- Original Message ----- From: "Rene" <rene(at)felker.com> Sent: Thursday, March 06, 2008 10:53 PM Subject: RE: RV10-List: Death of Van's Kit 40322 This is my favorite picture. The ground crew did a great job at making sure everything was working right.....pictures, not so much. But I have not seen them all yet...... Rene' 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jesse Saint Sent: Thursday, March 06, 2008 8:16 PM Subject: Re: RV10-List: Death of Van's Kit 40322 Congratulations! Any pictures? Jesse Saint Saint Aviation, Inc. jesse(at)saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Mar 6, 2008, at 9:35 PM, Rene wrote: > > I am glade to announce that today kit 40322 died and in its place > N423CF > arose. > > Yes, first flight was today. Very exciting and a real milestone. > Did not > fly hands off, heavy left wing.......gives me something to work on. > > Rene' > N423CF Flying > 801-721-6080 > > ________________________________________________________________________________
Subject: LoPresti Speed mods e-mail
From: "johngoodman" <johngoodman(at)earthlink.net>
Date: Mar 06, 2008
I have received an e-mail from LoPresti's web site that has absolutely locked up my mail program. It wants a user name and password that I don't even know. It won't let me get back to my inbox. A curse on his site!!!!!! John -------- #40572 QB Fuselage, wings finished N711JG reserved Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168196#168196 ________________________________________________________________________________
Date: Mar 07, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: First FlightRigging Questions
Rene', First, Congrats! Next, I disagree with Jesse depending on the stage of flight you're in, on the nose up/down trim. First, when you're solo in the 10, you have tons of power and climb, and when you hit the throttle you'll probably find that during certain stages of takeoff you'll be pushing on the stick quite a bit unless you're in trim. Out of the segmented LED, I usually have to take off with the 3rd to 4th from the bottom segment lit. So yeah, it's a bunch of nose-down trim during the takeoff roll. That plane has so darn much power that takeoffs are a bit amazing...the thing I remember most about the first takeoff is how unusual it was when I first left the ground. The plane accelerated sharply as soon as it left the pavement. The rolling resistance of the tires was very significant, and when they free up, you get a good kick in the a$$...it's way cool! But yeah, you'll be playing with the trim on takeoff a bit. Then, when it comes time to land, I'd agree more with Jesse....you'll be using quite a bit of nose up trim and be on the other end of the scale. If you have full trim deflection and it measures out correctly, I'd just say "fly it" and get some time in so you can get the feel. It will feel more natural over time. As for the heavy wing....yeah, fuel imbalance in the -10 can get you quite out of trim. The tanks are long and some fuel is far from the center axis. The trim should be able to take care of most of it. When I'm alone I notice it much more than when I'm hauling people around. If you've still got a wing low, I'd look at your aileron alignment, the shape and curvature of your wing tip trailing edges, and your flaps. Make sure your flaps are totally symmetrical, and that they're going all the way up to the stops. If your flaps are symmetrical and your ailerons are too, and the tips are nice, then aerodynamically you should be fine. Then the key may very well be just what Jesse mentioned... you may need to make sure your skid ball is centered. (Actually, check that first...it's easy) There are some cool tools you can use to center the skid ball if it's out to one side. They're called "feet". :) If you're like most -10s, you'll probably find that you'll need a wedge on the rudder if you don't have rudder trim....and the common side is the left side. Being out of rudder trim will make you hang a wing low. It's one reason I liked adding rudder trim to the plane...When you're flying long x/c you notice the little things....like a slight tilt to the horizon...and it drive you nuts. Rudder trim lets you get rid of that and make it perfect at any airspeed. So have at it and enjoy the plane. Watch for anything critical, but if it flies safely, get to know it and work through these issues systematically and you'll find in the end that you can make it fly perfect. Last night I had a beautiful night flight and flew into downtown St. Paul with all the lights, and it was just soooooo smooth...you're gonna love the plane! Tim Olson - RV-10 N104CD - Flying Jesse Saint wrote: > > With just a pilot and fuel you should be using more nose-up trim than > anything. If you are using nose-down, then something is wrong. This > may sound stupid and I certainly mean no offense, but are you sure that > you are trimming nose-down? Using most of (or at least a lot of) your > nose-up trim would be fairly normal in this condition. I would check > your trims and make sure you are getting your full deflection up on the > one trim tab that goes up while the other remains in the center. > > What trim do you have to offset the heavy wing? I just flew in a fairly > new RV-10 yesterday and it was flying one wing low until he trimmed the > ball into the center. That leveled it right up. > > > Jesse Saint > Saint Aviation, Inc. > jesse(at)saintaviation.com > Cell: 352-427-0285 > Fax: 815-377-3694 > > On Mar 7, 2008, at 12:01 AM, Rene wrote: > >> >> OK, need some opinions........ >> >> I was very excited about my first flight today, but did have a heavy wing >> and used a lot of nose down trim. It had me concerned. So tonight I >> went >> through the archives and I think I have it figured out.... >> >> Heavy wing, single pilot and.......only used right fuel tank during first >> flight. Not planning on switching tanks until the second flight. At the >> end of the flight I had a full left tank and ~ 15 gallons in the right >> tank. >> Can this type of in-balance lead to a very heavy left wing? Trim >> could not >> correct it. >> >> Elevator trim, needed to use a lot of nose down trim? At takeoff I added >> about 1 second, maybe two of trim. Also had almost full nose down trim >> during cruse. Is this normal? During transition training I don't >> remember >> using as much. >> >> After the flight, we went back over the elevator trim adjustment and >> it is >> per plans...35degrees. >> >> Rene' >> 801-721-6080 >> >> ________________________________________________________________________________
Subject: Death of Van's Kit 40322
Date: Mar 07, 2008
From: John Jessen <n212pj(at)gmail.com>
Beautiful sight. Congratulations! Now comes the dull part. Sorry that you have to fly instead of build. Poor guy! John J -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rene Sent: Thursday, March 06, 2008 7:53 PM Subject: RE: RV10-List: Death of Van's Kit 40322 This is my favorite picture. The ground crew did a great job at making sure everything was working right.....pictures, not so much. But I have not seen them all yet...... Rene' 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jesse Saint Sent: Thursday, March 06, 2008 8:16 PM Subject: Re: RV10-List: Death of Van's Kit 40322 Congratulations! Any pictures? Jesse Saint Saint Aviation, Inc. jesse(at)saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Mar 6, 2008, at 9:35 PM, Rene wrote: > > I am glade to announce that today kit 40322 died and in its place > N423CF arose. > > Yes, first flight was today. Very exciting and a real milestone. > Did not > fly hands off, heavy left wing.......gives me something to work on. > > Rene' > N423CF Flying > 801-721-6080 > > ________________________________________________________________________________
From: "Rene Felker" <rene(at)felker.com>
Subject: Death of Van's Kit 40322
Date: Mar 07, 2008
Ok, but y'all don't think the airplane is really "finished"? The second thing my wife said was.......you are going to do something with that ugly thing in the middle......the fiberglass console. I assured her that I would do something, just did not commit to what. Rene' Felker N423CF 40322 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Jessen Sent: Friday, March 07, 2008 8:22 AM Subject: RE: RV10-List: Death of Van's Kit 40322 Beautiful sight. Congratulations! Now comes the dull part. Sorry that you have to fly instead of build. Poor guy! John J -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rene Sent: Thursday, March 06, 2008 7:53 PM Subject: RE: RV10-List: Death of Van's Kit 40322 This is my favorite picture. The ground crew did a great job at making sure everything was working right.....pictures, not so much. But I have not seen them all yet...... Rene' 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jesse Saint Sent: Thursday, March 06, 2008 8:16 PM Subject: Re: RV10-List: Death of Van's Kit 40322 Congratulations! Any pictures? Jesse Saint Saint Aviation, Inc. jesse(at)saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Mar 6, 2008, at 9:35 PM, Rene wrote: > > I am glade to announce that today kit 40322 died and in its place > N423CF arose. > > Yes, first flight was today. Very exciting and a real milestone. > Did not > fly hands off, heavy left wing.......gives me something to work on. > > Rene' > N423CF Flying > 801-721-6080 > > ________________________________________________________________________________
Date: Mar 07, 2008
From: rsipp(at)earthlink.net
Subject: Re: Death of Van's Kit 40322
Way to go Rene. Let us know what the wing heavy cause was when you find it. Dick Sipp N110DV close do not archieve ________________________________________________________________________________
From: "sean(at)hangerg.com" <sean(at)hangerg.com>
Date: Mar 07, 2008
Subject: Lurking about
Ok, so here goes. I have been lurking about and I am getting ready to pull the trigger and purchase my RV10 kit from vans but I was wondering if any bigger induviduals can chime in. I am a fairly large guy 6 foot 1 and 235 pounds, how comfortable is the RV10 on longer trips. I currently have a cherokee 180 and the cabin room just isnt enough for my wife. So subsequently my wife doesnt like to fly longer trips becuase of comfort. So I am looking for input prior to calling vans and placing the order. I like the performance and the cabin seems like its much larger than the 180 I'm flying. Thanks for the help. Sean Garrison -------------------------------------------------------------------- mail2web.com Enhanced email for the mobile individual based on Microsoft Exchange - http://link.mail2web.com/Personal/EnhancedEmail ________________________________________________________________________________
From: "Albert Gardner" <ibspud(at)roadrunner.com>
Subject: Rudder Trim with Spring Bias
Date: Mar 07, 2008
The rudder trim system I have just installed seems to work very well. I used the same parts van uses for the aileron trim. I had already installed and wired in the LED trim indicator on my instrument panel and had a 5 wire cable run into the tail cone when I built the plane. I neglected to put a trim switch on the panel at the same time so I had to add that. (I can't remember why I didn't already have the switch installed - it sure would have made it simple then.) I made a pulley bracket that installs on top of F-1035 Battery/Bellcrank Mount and positions the pulley approximately between the rudder cables. (Later the elevator trim servo motor mount will install on top of this bracket and use the same screws.) I couldn't think of a neat way to attach to the rudder cables so I ran additional cables from the rudder trim servo back to the rudder horn and attached them there. Only had to drill 4 holes in the bottom skin to mount the trim servo and, if you don't count some missing skin and mild curses, installation was easy especially since I had already run the wires and the indicator was in place and wired. I picked up power and ground from the nearby flap switch. The pulley bracket is .032 with the edges bent up and a .032 doubler under the pulley. The springs span a 12" gap just like the aileron trim system does but I may add a bit more tension. I sort of holds the rudder from swinging easily on the ground but really doesn't function as a gust lock. Albert Gardner N991RV Yuma, AZ ________________________________________________________________________________
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Date: Mar 07, 2008
Subject: Lurking about
I think you will find it rather comfortable for a 4 place. There are a lot of us corn fed boys on the list and I have yet to hear anyone complain about long trips. I'm sure Tim will chime in here and he is another guy that is fairly big. The few times I have been up for flights I never noticed a comfort problem and I'm 6'2" and 260. I do have a lot of hanger time making airplane noises though. :) Michael -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of sean(at)hangerg.com Sent: Friday, March 07, 2008 10:37 AM Subject: RV10-List: Lurking about Ok, so here goes. I have been lurking about and I am getting ready to pull the trigger and purchase my RV10 kit from vans but I was wondering if any bigger induviduals can chime in. I am a fairly large guy 6 foot 1 and 235 pounds, how comfortable is the RV10 on longer trips. I currently have a cherokee 180 and the cabin room just isnt enough for my wife. So subsequently my wife doesnt like to fly longer trips becuase of comfort. So I am looking for input prior to calling vans and placing the order. I like the performance and the cabin seems like its much larger than the 180 I'm flying. Thanks for the help. Sean Garrison -------------------------------------------------------------------- mail2web.com - Enhanced email for the mobile individual based on Microsoft(r) Exchange - http://link.mail2web.com/Personal/EnhancedEmail ________________________________________________________________________________
Date: Mar 07, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: Lurking about
Sean, I'm currently pretty much identically sized as you....(wish I wasn't, 'cuz it ain't all muscle, but hey...I do what I can do) I can tell you that the RV-10 has considerably more capacity than what I take up. I am not at all large for that plane. You could be taller, wider or both, and probably be just fine. When my seats are cold, my head hits the top....until I warm it up and the foam conforms better. I could fix that with baked beans though. I've flown > 10hr days and found it more comfortable than 2 hours in the car. The standard Van's seats from oregon aero are exceedingly comfortable. You just won't be disappointed. Might want to go for a demo flight just to prove it to yourself. ;) Tim Olson - RV-10 N104CD - Flying sean(at)hangerg.com wrote: > > Ok, so here goes. I have been lurking about and I am getting ready to pull > the trigger and purchase my RV10 kit from vans but I was wondering if any > bigger induviduals can chime in. I am a fairly large guy 6 foot 1 and 235 > pounds, how comfortable is the RV10 on longer trips. I currently have a > cherokee 180 and the cabin room just isnt enough for my wife. So > subsequently my wife doesnt like to fly longer trips becuase of comfort. So > I am looking for input prior to calling vans and placing the order. I like > the performance and the cabin seems like its much larger than the 180 I'm > flying. > > Thanks for the help. > > Sean Garrison > ________________________________________________________________________________
Date: Mar 07, 2008
From: "Fred Williams, M.D." <drfred(at)suddenlinkmail.com>
Subject: Re: Lurking about
Go for it. You will love this airplane. I've ridden in the demonstrator and in my friends RV 10. Plenty of room. Enough for a center console if you want it. Take the plunge. Fred Williams 40515 sean(at)hangerg.com wrote: > > Ok, so here goes. I have been lurking about and I am getting ready to pull > the trigger and purchase my RV10 kit from vans but I was wondering if any > bigger induviduals can chime in. I am a fairly large guy 6 foot 1 and 235 > pounds, how comfortable is the RV10 on longer trips. I currently have a > cherokee 180 and the cabin room just isnt enough for my wife. So > subsequently my wife doesnt like to fly longer trips becuase of comfort. So > I am looking for input prior to calling vans and placing the order. I like > the performance and the cabin seems like its much larger than the 180 I'm > flying. > > Thanks for the help. > > Sean Garrison > > -------------------------------------------------------------------- > mail2web.com Enhanced email for the mobile individual based on Microsoft > Exchange - http://link.mail2web.com/Personal/EnhancedEmail > > > ________________________________________________________________________________
Date: Mar 07, 2008
From: Robert Wright <flywrights(at)yahoo.com>
Subject: Re: Lurking about
You'll fit. However, you may need to convince yourself of that and find a -10 to sit in. In fact, I'd be willing to say that you could fit two of yo u and two 180-lb guys in the plane and not be cramped.=0A=0ARob Wright=0A#3 92=0Afinish/ffwd=0A=0A=0A----- Original Message ----=0AFrom: "sean@hangerg. com" =0ATo: rv10-list(at)matronics.com=0ASent: Friday, March 7, 2008 11:37:00 AM=0ASubject: RV10-List: Lurking about=0A=0A--> RV10-List message posted by: "sean(at)hangerg.com" =0A=0AOk, so here goes. I have been lurking about and I am getting ready to pull=0Athe trigge r and purchase my RV10 kit from vans but I was wondering if any=0Abigger in duviduals can chime in. I am a fairly large guy 6 foot 1 and 235=0Apounds, how comfortable is the RV10 on longer trips. I currently have a=0Acherokee 180 and the cabin room just isnt enough for my wife. So=0Asubsequently my w ife doesnt like to fly longer trips becuase of comfort. So=0AI am looking f or input prior to calling vans and placing the order. I like=0Athe performa nce and the cabin seems like its much larger than the 180 I'm=0Aflying. =0A =0AThanks for the help.=0A=0ASean Garrison=0A=0A--------------------------- -----------------------------------------=0Amail2web.com ' Enhanced email for the mobile individual based on Microsoft=AE=0AExchange - http://link.m ==================0A=0A=0A _________ ___________________________________________________________________________ =0ABe a better friend, newshound, and =0Aknow-it-all with Yahoo! Mobile. T ry it now. http://mobile.yahoo.com/;_ylt=Ahu06i62sR8HDtDypao8Wcj9tAcJ =0A ________________________________________________________________________________
From: "Marvin Mixon" <mmixon(at)fastspot.net>
Subject:
Date: Mar 07, 2008
RV 10 tail kit for sale. $2,650. All parts completed except tail cone. Houston, TX area. Marvin ' 281-342-7802 3/6/2008 9:07 AM ________________________________________________________________________________
Subject: Re: OSH
From: "orchidman" <gary(at)wingscc.com>
Date: Mar 07, 2008
rv(at)thelefflers.com wrote: > I was able to rent a trailer from Van Boxtel. They will deliver it from Green Bay to Osh for an additional fee. http://www.vanboxtelrv.com/ (http://www.vanboxtelrv.com/)? Their RVs (4 wheel kind) are a little expensive ($1,700) for the week, but their tent campers and travel trailers were reasonable. > We just signed up for the last available 16' trailer (at least that is what I was told). We will pick it up as the delivery/set up fee was $400 big ones. Plan on arriving either Friday evening or Sat AM. and leaving Thursday but might stay until Fri early AM. Getting close [Mr. Green] -------- Gary Blankenbiller RV10 - # 40674 Fuselage SB (N410GB reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168283#168283 ________________________________________________________________________________
From: "Bob Leffler" <rv(at)thelefflers.com>
Subject: Lurking about
Date: Mar 07, 2008
Sean, I have a Cherokee 180 and my wife's #1 concern was legroom in the back seat. Here's a pic from the back of Dave Saylor's RV-10. I'm 6'2", 230lbs and as you can see there is plenty of room in the back seat. I can't remember if it was Dave Ward or John Goodman in the back seat with me, but it was a very comfortable ride. Nothing like a Cherokee. There was a good 6" between my knees and the back of the front seat. http://www.kitlog.com/photos/project_260/full/FP31012008A0002T.jpg bob -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of sean(at)hangerg.com Sent: Friday, March 07, 2008 8:37 AM Subject: RV10-List: Lurking about Ok, so here goes. I have been lurking about and I am getting ready to pull the trigger and purchase my RV10 kit from vans but I was wondering if any bigger induviduals can chime in. I am a fairly large guy 6 foot 1 and 235 pounds, how comfortable is the RV10 on longer trips. I currently have a cherokee 180 and the cabin room just isnt enough for my wife. So subsequently my wife doesnt like to fly longer trips becuase of comfort. So I am looking for input prior to calling vans and placing the order. I like the performance and the cabin seems like its much larger than the 180 I'm flying. Thanks for the help. Sean Garrison -------------------------------------------------------------------- mail2web.com - Enhanced email for the mobile individual based on Microsoft(r) Exchange - http://link.mail2web.com/Personal/EnhancedEmail __________ Information from ESET NOD32 Antivirus, version of virus signature database 2930 (20080307) __________ The message was checked by ESET NOD32 Antivirus. __________ Information from ESET NOD32 Antivirus, version of virus signature database 2930 (20080307) __________ The message was checked by ESET NOD32 Antivirus. ________________________________________________________________________________
Date: Mar 07, 2008
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: Lurking about
So how did you get taller John? :-D Is that airline work that elevating? John W. Cox wrote: > Bill is 6'4 and 285#, at the time I was over 6'2" and > 235#. I am north of that now. > > > ________________________________________________________________________________
Date: Mar 07, 2008
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: Lurking about
Folks don't believe it because of the low seating position, but even the oldest Mooneys are wider than both the Cherokee and the Bonanza. RV-10 has plenty of room. Bob Leffler wrote: > > Sean, > > I have a Cherokee 180 and my wife's #1 concern was legroom in the back seat. > Here's a pic from the back of Dave Saylor's RV-10. I'm 6'2", 230lbs and as > you can see there is plenty of room in the back seat. I can't remember if > it was Dave Ward or John Goodman in the back seat with me, but it was a very > comfortable ride. Nothing like a Cherokee. There was a good 6" between my > knees and the back of the front seat. > > http://www.kitlog.com/photos/project_260/full/FP31012008A0002T.jpg > > bob > > ________________________________________________________________________________
Subject: Lurking about
Date: Mar 07, 2008
From: "John W. Cox" <johnwcox(at)pacificnw.com>
Shrinking in height from ole age and the weight increase while trying to match Michael Sausen... at the same time eating Tim's Chili. I want an RV-10 figure like Rick Sked and Deems who are becoming only a wisp of there former selves last year. -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Friday, March 07, 2008 6:46 PM Subject: Re: RV10-List: Lurking about So how did you get taller John? :-D Is that airline work that elevating? John W. Cox wrote: > Bill is 6'4 and 285#, at the time I was over 6'2" and > 235#. I am north of that now. > > > ________________________________________________________________________________
From: "Russell Daves" <dav1111(at)erfwireless.net>
Subject: Re: Lurking about
Date: Mar 08, 2008
Sean, I'm 6', 260 heading towards 220. Mt time in the -10 was when I was almost 320...and I fit OK. You should not have any issues it is very roomy. The back even more so. Rick Sked 40185 I have read all the posts and guess I better put my two cents worth in as well. Since Rick Sked owned up to being a little heavy when he flew my -10 (I was in the left seat and Rick in the right) I will confess to being fat and happy as well At the time I was about 265 and am 5'10" tall. With Rick at 320 and me at 265 the front seats were a little crowded but I was not touching either the door or Rick's shoulder. Admittedly Rick and I were only doing a local flight but size wise it was a really good test. By the way on one local flight Rick was in the back seat and with me and a 180 lb guy up front the -10 at Las Vegas still performed like a winner. Bob K. (6'2" and 210), his wife and mine flew back from Las Vegas to El Paso along with full baggage and everybody was really happy with the room in the -10. Guys in front, girls in back. No, I wouldn't be dumb enough to post the weights of the wives!!! If I did my wife would see to it I lost all my excess weight running away. To give you a comparison, I owned three different C-182's, and the -10 is lots bigger inside than the C-182. Russ Daves N710RV - 190+ hours ________________________________________________________________________________
Date: Mar 08, 2008
From: Tim Lewis <timrvator(at)comcast.net>
Subject: Butyl inner tubes "just don't leak"
A February 2008 Aviation Consumer article on tires says" "...Until recently, tubes were manufactured from a natural rubber compound. Unfortunately, natural rubber is relatively porous and loses pressure more readily than synthetic materials. Therefore, your tires would lose pressure and go soft, too. Enter the butyl rubber tube, now largely the standard among all aircraft inner tube manufacturers. Since unused inner tubes are perfectly good for installation, were not saying you wont find a natural rubber tube out there on some shops shelf. Its perfectly serviceable, it just wont hold air as well. Goodyears Brown says the new butyl tubes, introduced some seven years ago, improve air retention by a factor of about 10. Steve Chlavin of Desser Tire, the GA industrys mega tire retailer, agrees, saying, "The new butyl leak-resistant tubes just dont leak."" It's fairly easy to add air to my RV-6A tires - the valve stems point out, so the tire can be aired through a small hole in the fairing. The situation is more challenging in a stock RV-10 (valve stems on the mains point toward the axle, for example). With this in mind, does anybody know whether the tires Vans shipped with the RV-10 kits are butyl or natural rubber? Tim -- Tim Lewis -- HEF (Manassas, VA) RV-6A N47TD -- 1000 hrs RV-10 #40059 under construction ________________________________________________________________________________
From: "Sean Garrison" <Sean(at)hangerg.com>
Subject: Re: Lurking about
Date: Mar 08, 2008
Thank you so much for all of the feedback it is very much appreciated. I guess I will have to get my backside into a 10 and take a flight either at Sun&Fun or with some fine individual that has a Florida. From the sounds of it I will have plenty of room. I do have one question though How much room loss will occur with interior work? Thanks All Sean Garrison From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Russell Daves Sent: Saturday, March 08, 2008 6:27 AM Subject: RV10-List: Re: Lurking about Sean, I'm 6', 260 heading towards 220. Mt time in the -10 was when I was almost 320...and I fit OK. You should not have any issues it is very roomy. The back even more so. Rick Sked 40185 I have read all the posts and guess I better put my two cents worth in as well. Since Rick Sked owned up to being a little heavy when he flew my -10 (I was in the left seat and Rick in the right) I will confess to being fat and happy as well At the time I was about 265 and am 5'10" tall. With Rick at 320 and me at 265 the front seats were a little crowded but I was not touching either the door or Rick's shoulder. Admittedly Rick and I were only doing a local flight but size wise it was a really good test. By the way on one local flight Rick was in the back seat and with me and a 180 lb guy up front the -10 at Las Vegas still performed like a winner. Bob K. (6'2" and 210), his wife and mine flew back from Las Vegas to El Paso along with full baggage and everybody was really happy with the room in the -10. Guys in front, girls in back. No, I wouldn't be dumb enough to post the weights of the wives!!! If I did my wife would see to it I lost all my excess weight running away. To give you a comparison, I owned three different C-182's, and the -10 is lots bigger inside than the C-182. Russ Daves N710RV - 190+ hours ________________________________________________________________________________
Date: Mar 08, 2008
From: Les Kearney <kearney(at)shaw.ca>
Subject: Brake Temperatures
Hi I was wondering if anyone has ever put temperature probes near the main brakes on the -10. I have read about a few cases where there have been brake overheating problems on various RV variations that have resulted in significant damage. It would seem that this should be a simple issue to monitor. Inquiring minds need to know.. Les Kearney #40643 C-GCWZ (reserved) ________________________________________________________________________________
From: "Jay Rowe" <jfrjr(at)roadrunner.com>
Subject: Power grid placements on AA panels
Date: Mar 08, 2008
Ahn, or anyone else with an Accuracy Avionics Panel for their 10: Where are you placing the primary and secondary power grids? Looks to me like the forward surface of the subpanel would be okay; a little hard to reach but doable. Also could the manifold pressure sensing unit go there as well? I also plan to put the door closure indicator relay units there too. All suggestions welcomed. Jay Rowe ________________________________________________________________________________
From: kilopapa(at)antelecom.net
Subject: Re: Lower Cowl Mounts
Date: Mar 08, 2008
Howdy, Is the problem at the firewall/cowl margin or between the top and bottom cowl halves? Is the hinge you replaced on the side or bottom of the lower cowl? Would you have any pics? Thanks, Kevin 40494 ----- Original Message Follows ----- From: "DejaVu" <wvu(at)ameritel.net> Subject: Re: RV10-List: Lower Cowl Mounts > >Hey who's using hinges for the lower cowl?! Don't do it. >Actually, I'm chiming in late but seems like most folks >are aware of this issue. Hinges were not a problem in my >-6. They did not last past 5 hours in the -10. They >eyelets broke one at a time. Just on the left side. I >replaced that side with nutplates/screws then the other >side started to break, one eyelet at a time. Eventually I >fixed both sides. I made the plates out of the old >instrument panel. Didn't need shims since the hinge halves >lined up in the first place. I didn't want to patch up >the existing holes on the cowl where the rivets used to be >so I used six #8 nutplates/screws per side, with C/S >washers. Very solid as you would imagine. Anh >N591VU - flying ________________________________________________________________________________
From: "Bob-tcw" <rnewman(at)tcwtech.com>
Subject: Re: Power grid placements on AA panels
Date: Mar 08, 2008
Jay, We are using the Acuracy Avoinics glass instrument panel and center console in our 10 and we are working out the details now. We have the version of the panel with the centered radio stack. We are using AFS 3500s on each side and a center stack of a GMX-200 mfd and 2 garmin 430w. I think the real challenge is the cutting and re-supporting of the three main instrument panel ribs. I'm just days away from posting the pictures of how we did it. When we are ready I'll add the pictures to the RV-10 section of our web site. We machined an aluminum arch out of billet 6061 aluminum with an L shaped profile to resupport the material that just has to be removed from the three ribs to accomidated the AFS glass panels. I think most of the power and ground buses will be attached to the forward sub panel. Additionally, I'm putting a small fuse block bus in the rear of the aircraft on my equipment rack I made behind the baggage area. I have pictures of that already up on our site. more to follow. Bob Newman TCW Technologies. www.tcwtech.com ----- Original Message ----- From: Jay Rowe To: RV10-list(at)matronics.com Sent: Saturday, March 08, 2008 3:26 PM Subject: RV10-List: Power grid placements on AA panels Ahn, or anyone else with an Accuracy Avionics Panel for their 10: Where are you placing the primary and secondary power grids? Looks to me like the forward surface of the subpanel would be okay; a little hard to reach but doable. Also could the manifold pressure sensing unit go there as well? I also plan to put the door closure indicator relay units there too. All suggestions welcomed. Jay Rowe ________________________________________________________________________________
From: "Rene" <rene(at)felker.com>
Subject: Power grid placements on AA panels
Date: Mar 08, 2008
This may be hard to explain and I got my panel from Stein. But here you go. I have three power buses, main, battery and e-bus. I took a little different route. I used a flat piece of AL about 4" by 6" and mounted my MP sensor, trim relays, a terminal board and a couple of other things. I used both sides. The I mounted that on the bottom of the subpanel, the flange, using the three bus terminals to hold it in place. So, if I need to work on anything on that piece, I just remove the three bus connections and the panel drops down. Because of a MP problem..I pushed the pin the wrong position in the connector...I have had to drop it once already and it worked pretty good. Sorry, no pictures. Rene' 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jay Rowe Sent: Saturday, March 08, 2008 1:27 PM Subject: RV10-List: Power grid placements on AA panels Ahn, or anyone else with an Accuracy Avionics Panel for their 10: Where are you placing the primary and secondary power grids? Looks to me like the forward surface of the subpanel would be okay; a little hard to reach but doable. Also could the manifold pressure sensing unit go there as well? I also plan to put the door closure indicator relay units there too. All suggestions welcomed. Jay Rowe <http://promos.hotbar.com/promos/promodll.dll?RunPromo&El=&SG=&RAND= 26220&pa rtner=seekmo> Upgrade Your Email - Click here! ________________________________________________________________________________
Date: Mar 08, 2008
From: Rick Sked <ricksked(at)embarqmail.com>
Subject: Re: Power grid placements on AA panels
Jay, I mounted the buss on the left forward rib. This left a short run from the buss to the starter relay and my main feed runs down the left side also. I mounte the rack using nutplases so if I have to remove it I can do do from underneath the panel...not fun but doable. I mounted the manifold pressure =C2-transducer on the right forward bulkhead facing the fiewall. Makes fo r a short run to the bulkhead adapter. I know you goiung to ask for pics bu t.....I have to find out where in my vast photos files they are. I have all kinds of pictures of that area but none of exactly what your looking for. Rick Sked 40185 ----- Original Message ----- From: "Jay Rowe" <jfrjr(at)roadrunner.com> Sent: Saturday, March 8, 2008 12:26:30 PM (GMT-0800) America/Los_Angeles Subject: RV10-List: Power grid placements on AA panels Ahn, or anyone else with an Accuracy Avionics Panel for their 10:=C2-=C2 - Where are=C2-you=C2-placing the primary and secondary power grids? =C2- Looks to me like the forward surface of the subpanel would be okay; =C2- a little hard to reach but doable.=C2- Also could the manifold pre ssure sensing unit go there as well?=C2- I also plan to put the door clos ure indicator relay units=C2-there too.=C2- All suggestions welcomed. =C2- Jay Rowe Upgrade Your Email - Click here! ________________________________________________________________________________
Date: Mar 08, 2008
From: Rick Sked <ricksked(at)embarqmail.com>
Subject: Re: Power grid placements on AA panels
Oh yeah,...mount the door relays to a piece of aluminum matched drilled and install nutplates=C2-to anywhere on the ribs or bulkheads. Attach the re lays to that little aluminum piece. Hook up the relay leads to the relays a nd intall it a one unit where you made your nutplates to hold it. It is way easier to slide the terminals on then mount the relays....trust me, I just hooked those up an hour ago. Rick Sked 40185 ----- Original Message ----- From: "Jay Rowe" <jfrjr(at)roadrunner.com> Sent: Saturday, March 8, 2008 12:26:30 PM (GMT-0800) America/Los_Angeles Subject: RV10-List: Power grid placements on AA panels Ahn, or anyone else with an Accuracy Avionics Panel for their 10:=C2-=C2 - Where are=C2-you=C2-placing the primary and secondary power grids? =C2- Looks to me like the forward surface of the subpanel would be okay; =C2- a little hard to reach but doable.=C2- Also could the manifold pre ssure sensing unit go there as well?=C2- I also plan to put the door clos ure indicator relay units=C2-there too.=C2- All suggestions welcomed. =C2- Jay Rowe Upgrade Your Email - Click here! ________________________________________________________________________________
Date: Mar 08, 2008
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: ShowPlanes Tail mod
Anyone considering Showplanes upper tailcone mod to change the rear fuselage profile? Seems like it would allow placement of an antenna or two under it. ________________________________________________________________________________
Subject: TT mounting specifications
From: "orchidman" <gary(at)wingscc.com>
Date: Mar 08, 2008
Does anyone have the specs for the TruTrak flat pack DigiFlight II? I have the servos but am trying to wait until later in getting the head. However this then creates another problem and this is planning the instrument panel. I know the panel cut out sizes but not what goes behind the panel. Is the housing wider then the front panel? How far back does it go and what extra clearance is needed? I have searched their site and can not find any sizing documents. -------- Gary Blankenbiller RV10 - # 40674 Fuselage SB (N410GB reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168521#168521 ________________________________________________________________________________
From: "FLAGSTONE" <flagstone(at)cox.net>
Subject: Re: TT mounting specifications
Date: Mar 08, 2008
Gary: This ref has the overall dimensions. If the flat pack dimensions are consistent with the standard model, the dimensions shown are for the case size. I happened to have my standard version out and I checked its dimensions. They agree to the site. http://www.trutrakflightsystems.com/instruments.htm Mark ----- Original Message ----- From: "orchidman" <gary(at)wingscc.com> Sent: Saturday, March 08, 2008 6:59 PM Subject: RV10-List: TT mounting specifications > > Does anyone have the specs for the TruTrak flat pack DigiFlight II? I have the servos but am trying to wait until later in getting the head. However this then creates another problem and this is planning the instrument panel. I know the panel cut out sizes but not what goes behind the panel. Is the housing wider then the front panel? How far back does it go and what extra clearance is needed? I have searched their site and can not find any sizing documents. > > -------- > Gary Blankenbiller > RV10 - # 40674 > Fuselage SB > (N410GB reserved) > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=168521#168521 > > ________________________________________________________________________________
From: "Chris" <toaster73(at)embarqmail.com>
Subject: Re: TT mounting specifications
Date: Mar 08, 2008
Was looking at this earlier today too. The depth is shown on the product page on the website as 5.5 inch, for flat pack or round. The cutout is in the install manual. Be nice if they had a 3 view somewhere. -Chris Lucas #40072 ----- Original Message ----- From: "orchidman" <gary(at)wingscc.com> Sent: Saturday, March 08, 2008 9:59 PM Subject: RV10-List: TT mounting specifications > > Does anyone have the specs for the TruTrak flat pack DigiFlight II? I > have the servos but am trying to wait until later in getting the head. > However this then creates another problem and this is planning the > instrument panel. I know the panel cut out sizes but not what goes behind > the panel. Is the housing wider then the front panel? How far back does > it go and what extra clearance is needed? I have searched their site and > can not find any sizing documents. > > -------- > Gary Blankenbiller > RV10 - # 40674 > Fuselage SB > (N410GB reserved) > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=168521#168521 > > > ________________________________________________________________________________
Date: Mar 08, 2008
From: Bill DeRouchey <billderou(at)yahoo.com>
Subject: Re: TT mounting specifications
Looks like you are getting this in pieces and unfortunately this is from memory. The front top & bottom are 3/8" above and below the cutout, add 1/2" for each side. Use 5.5" for depth but add 2.5" for DB-25 connector and pitot/static connections. Bill DeRouchey #40029, flying Chris wrote: Was looking at this earlier today too. The depth is shown on the product page on the website as 5.5 inch, for flat pack or round. The cutout is in the install manual. Be nice if they had a 3 view somewhere. -Chris Lucas #40072 ----- Original Message ----- From: "orchidman" Sent: Saturday, March 08, 2008 9:59 PM Subject: RV10-List: TT mounting specifications > > Does anyone have the specs for the TruTrak flat pack DigiFlight II? I > have the servos but am trying to wait until later in getting the head. > However this then creates another problem and this is planning the > instrument panel. I know the panel cut out sizes but not what goes behind > the panel. Is the housing wider then the front panel? How far back does > it go and what extra clearance is needed? I have searched their site and > can not find any sizing documents. > > -------- > Gary Blankenbiller > RV10 - # 40674 > Fuselage SB > (N410GB reserved) > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=168521#168521 > > > ________________________________________________________________________________
Date: Mar 09, 2008
From: "Doug Gee" <Doug.Gee@firestone-textiles.com>
Subject: Florida Builders
I have just flown my 172 from Ont Canada to KZPH for vacation. I am 90 percent sure I am going to build an RV10 as soon as I get some home reno projects out of the way. Just wondering if there are any central Florida builders up for a visit and a "few" questions? Thanks ________________________________________________________________________________
From: "Russell Daves" <dav1111(at)erfwireless.net>
Subject: Re: Lurking about
Date: Mar 09, 2008
How much room loss will occur with interior work? My previous posting was based on the finished interior work, not stripped down. If you climb into the back seat of an unfinished -10 without seats, carpet, or side panels installed you could fit two 6"10" 375 lb sumu wrestlers. Russ Daves ________________________________________________________________________________
Date: Mar 09, 2008
From: jimandlaura <jimandlaura(at)peoplepc.com>
Subject: Brake Temperatures Hi
Les, I can confirm this. Shortly after finishing my RV-6 I had a problem with my left brake not releasing all the way. This resulted in my brake heating up enough to cause my tube to leak. My left brake peddle had a little bit of friction that wasn't allowing the peddle to return to the forward position. This little bit, maybe 1/4"-3/8", of hang-up was keeping enough pressure on the brake to cause my leak. I tried cleaning up and lubricating the peddle, but it still would not return all the way. I ended up being able to put more tension on the springs in the brake calipers by inserting a couple washers. This worked very well and fixed the problem. Jim Riley #40191 Finishing From: Les Kearney <kearney(at)shaw.ca> Subject: Brake Temperatures Hi I was wondering if anyone has ever put temperature probes near the main brakes on the -10. I have read about a few cases where there have been brake overheating problems on various RV variations that have resulted in significant damage. It would seem that this should be a simple issue to monitor. Inquiring minds need to know.. Les Kearney #40643 C-GCWZ (reserved) ________________________________________ ________________________________________________________________________________
From: "Rene" <rene(at)felker.com>
Subject: Electric/Gas Tow Bars
Date: Mar 09, 2008
Any recommendations on Electric or Gas powered tow bars. Now that I am actually taking the completed..almost..in and out of the hanger I see a need for one. I can get the airplane out of the hanger no problem but getting it back in is a different story. I thought about putting a winch in the back of the hanger and just pulling it in, but the tow bar may be easier. Any recommendations for one that works well with the wheel pans on? Rene' 801-721-6080 ________________________________________________________________________________
Subject: Re: Rudder Trim with Spring Bias
From: "jkreidler" <jason.kreidler(at)regalbeloit.com>
Date: Mar 09, 2008
Albert, I really like this approach. I especially like the ease of installation, this is something that could be added after the fact without much headache at all. I had never thought of mounting the mechanism in the tail cone, I was always trying to 'wedge' it in the tunnel somewhere. Nice work! I do have some questions though. Are the springs initially stretched? In other words if the rudder placed at full deflection do both springs still have tension in them (one spring barely tensioned, and the other nearly fully extended)? What trim force do you think you are getting? I had sent an e-mail to Vans asking what input they thought would be required. They told me that a 5 to 10 pound force as measured at the bottom of the rudder pedal should take care of any 'normal' trim, 25 pounds could be required to compensate for takeoff forces. I have been crunching numbers on the torsion spring bias system that I had designed. I am having difficulty getting the required trim force without overloading the trim servo motor, or limiting the travel too much. A combination of the two systems may be just the ticket to realize the benefits of both. Again I really like the different approach, thanks for sharing. Jason Kreidler - #40617 4 Partner Build - Finishing Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168597#168597 ________________________________________________________________________________
Subject: Where did you mount the Lightspeed Plasma III box
From: "Michael Wellenzohn" <rv-10(at)wellenzohn.net>
Date: Mar 09, 2008
Hi, soon I'll come to the point where I will mount my Lightspeed Plasma III control box. I saw some pictures where it was mounted inside of the firewall. Where did you mount it? Best Regards Michael -------- RV-10 builder (engine, prop, finishing) #511 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168598#168598 ________________________________________________________________________________
From: "Marcus Cooper" <coop85(at)cableone.net>
Subject: Where did you mount the Lightspeed Plasma III box
Date: Mar 09, 2008
Michael, I mounted mine on the sub panel behind the instrument panel. I had read somewhere that the heat in the engine compartment might not be a good thing on the brain box so I wanted it behind the firewall. I could certainly be off on that thought. Seems to work just fine. Marcus 40286 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Michael Wellenzohn Sent: Sunday, March 09, 2008 1:40 PM Subject: RV10-List: Where did you mount the Lightspeed Plasma III box Hi, soon I'll come to the point where I will mount my Lightspeed Plasma III control box. I saw some pictures where it was mounted inside of the firewall. Where did you mount it? Best Regards Michael -------- RV-10 builder (engine, prop, finishing) #511 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168598#168598 ________________________________________________________________________________
From: "Carl Froehlich" <carl.froehlich(at)cox.net>
Subject: Where did you mount the Lightspeed Plasma III box
Date: Mar 09, 2008
I have dual Lightspeed II+ in my 8A. I would not consider mounting the CDI module on the firewall side of the engine if for no reason other than heat. These modules get hot by themselves. You might want to ask Klaus about heat issues with the Plasma III. Here is what his web site says: The PLASMA CDI module should be mounted in a clean and dry place on the cold side of the firewall. If space limitations require mounting on the engine side of the firewall, a protective metal cover should be used to protect the module from water/engine cleaning materials and heat. In this situation, the module should be oriented such that the connectors are to the sides of the plane. Air must be allowed to flow between the bottom of the module and the mounting surface. On 6-cylinder systems, cooling air should be supplied to the box via the cooling port on the 15-pin connector side of the ignition module. For 6-cyl. systems that do not have a cooling port, contact LSE for this modification. Cooling is not required for 4-cyl. systems. I would mount the modules in a cool spot and not on the back side of the firewall even if it is insulated. Use standoffs to allow for air to circulate behind the modules. Keep in mind you need to provide a blast tube for cooling. I would assume you could rig up a cooling fan instead if a blast tube was too hard. BTW - I got a note back from eMag the other day. They are progressing on their 6 cylinder ignition system but I did not get a target date for availability. I am hoping these are on the market as an alternative to Lightspeed when I'm ready for the engine. Carl Froehlich RV-8A (400 hrs) RV-10 (wings) -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Michael Wellenzohn Sent: Sunday, March 09, 2008 2:40 PM Subject: RV10-List: Where did you mount the Lightspeed Plasma III box Hi, soon I'll come to the point where I will mount my Lightspeed Plasma III control box. I saw some pictures where it was mounted inside of the firewall. Where did you mount it? Best Regards Michael -------- RV-10 builder (engine, prop, finishing) #511 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168598#168598 ________________________________________________________________________________
From: "Jay Rowe" <jfrjr(at)roadrunner.com>
Subject: Re: Power grid placements on AA panels
Date: Mar 09, 2008
Thanks Bob, Rick, and Rene. Great suggestions that I will (did) incorporate. Actually what I did today was fashion several alum. angle strips to run on the bottom of the three forward ribs then attached those to the ribs with large nutplates. Then riveted the power grids to the angled alum. with the grids facing downward. The result is they sit low enough in that forward subpanel space that they are easy to get to for attaching wires and such. And, if they have to be removed to replace fuses (or any other reason) they drop right down by removing the four large nutplate bolts. I also beefed up the ribs just a bit with several small pieces of angle stock. I also have enough room to mount the MAP box, the door indicator relays, and probably the Lightspeed box if I decide to keep it out of the engine compartment. And, by the way Bob, with my set up (two horizontal GRT screens and the cantened center radio stack I did not have to alter the anterior ribs at all). I did provide some additional support to the radio stack by running some angled stock from the stack up to the already reinforced center rib. Jay ----- Original Message ----- From: Bob-tcw To: rv10-list(at)matronics.com Sent: Saturday, March 08, 2008 5:13 PM Subject: Re: RV10-List: Power grid placements on AA panels Jay, We are using the Acuracy Avoinics glass instrument panel and center console in our 10 and we are working out the details now. We have the version of the panel with the centered radio stack. We are using AFS 3500s on each side and a center stack of a GMX-200 mfd and 2 garmin 430w. I think the real challenge is the cutting and re-supporting of the three main instrument panel ribs. I'm just days away from posting the pictures of how we did it. When we are ready I'll add the pictures to the RV-10 section of our web site. We machined an aluminum arch out of billet 6061 aluminum with an L shaped profile to resupport the material that just has to be removed from the three ribs to accomidated the AFS glass panels. I think most of the power and ground buses will be attached to the forward sub panel. Additionally, I'm putting a small fuse block bus in the rear of the aircraft on my equipment rack I made behind the baggage area. I have pictures of that already up on our site. more to follow. Bob Newman TCW Technologies. www.tcwtech.com ----- Original Message ----- From: Jay Rowe To: RV10-list(at)matronics.com Sent: Saturday, March 08, 2008 3:26 PM Subject: RV10-List: Power grid placements on AA panels Ahn, or anyone else with an Accuracy Avionics Panel for their 10: Where are you placing the primary and secondary power grids? Looks to me like the forward surface of the subpanel would be okay; a little hard to reach but doable. Also could the manifold pressure sensing unit go there as well? I also plan to put the door closure indicator relay units there too. All suggestions welcomed. Jay Rowe ------------------------------------------------------------------------- --- Checked by AVG. 3/7/2008 2:01 PM ________________________________________________________________________________
Date: Mar 09, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: Where did you mount the Lightspeed Plasma III box
While certainly not a proof of reliability, I had 320 hours of perfect operation with my Plasma III....with no cooling port on it. I recently took advantage of the winter downtime and sent it in for the cooling port and all additional updates that they could do. I haven't added blast cooling air yet, but plan to as soon as I care to lay under the panel again. ;) What I did was mount mine on the firewall, cabin side, upper area behind the pilots side of the firewall....way up on that top curved area that is largely wasted space. I mounted it and had stand-off rubber feet under it to ensure that it had an air gap between it and the firewall. Originally I mounted it with just screws and nuts, but getting to it was a bit of a pain because I had to have the wife turn the screws while I held the wrench. So, when it was out for the mods, I put nutplates on the box so that now I can just put it in place and screw it in. It's definitely not in the most accessible area for removal, but then again, it's something that you will rarely (hopefully) have to remove. Had I bought mine after the cooling port became standard, I would have not had reason to remove it. So it's kind of nice to use some of that wasted space. Plus, being high on the firewall leaves for nice short and easy to route RG-400 lines for the coil wires. Not the best way, perhaps, but it's served me very well. Having had so many hours without cooling ports, the heat issue thing isn't a major fear for me...but I do think it's best to go with any manufacturer recommendations for sure. Tim Olson - RV-10 N104CD - Flying Carl Froehlich wrote: > I have dual Lightspeed II+ in my 8A. I would not consider mounting the > CDI module on the firewall side of the engine if for no reason other > than heat. These modules get hot by themselves. You might want to ask > Klaus about heat issues with the Plasma III. Here is what his web site > says: > > > > > > The PLASMA CDI module should be mounted in a clean and dry place on the > cold side of the firewall. If space limitations require mounting on the > engine side of the firewall, a protective metal cover should be used to > protect the module from water/engine cleaning materials and heat. In > this situation, the module should be oriented such that the connectors > are to the sides of the plane. Air must be allowed to flow between the > bottom of the module and the mounting surface. On 6-cylinder systems, > cooling air should be supplied to the box via the cooling port on the > 15-pin connector side of the ignition module. For 6-cyl. systems that > do not have a cooling port, contact LSE for this modification. Cooling > is not required for 4-cyl. systems. > > > > > > I would mount the modules in a cool spot and not on the back side of the > firewall even if it is insulated. Use standoffs to allow for air to > circulate behind the modules. Keep in mind you need to provide a blast > tube for cooling. I would assume you could rig up a cooling fan instead > if a blast tube was too hard. > > > > BTW - I got a note back from eMag the other day. They are progressing > on their 6 cylinder ignition system but I did not get a target date for > availability. I am hoping these are on the market as an alternative to > Lightspeed when I'm ready for the engine. > > > > Carl Froehlich > > RV-8A (400 hrs) > > RV-10 (wings) > ________________________________________________________________________________
From: John Gonzalez <indigoonlatigo(at)msn.com>
Subject: tail light strobe combo
Date: Mar 09, 2008
Can someone explain what is required to hook up the wiring on this Whelen T ail light/strobe combo. Out of the base of the unit is the normal strobe wi res, red, black and white going to a 3 prong molex. There are also two othe r wires which are going to a two prong molex connector. These other two wir e are both blue. Can someone give me a heads up? Thanks, John G. 409 ________________________________________________________________________________
Date: Mar 09, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: tail light strobe combo
Well, the red/black/white hook up like all the other strobe pack strobes do...and the 2 other blue wires are the tail light and hence there is no + or - . Not much to it. Tim Olson - RV-10 N104CD - Flying John Gonzalez wrote: > Can someone explain what is required to hook up the wiring on this > Whelen Tail light/strobe combo. Out of the base of the unit is the > normal strobe wires, red, black and white going to a 3 prong molex. > There are also two other wires which are going to a two prong molex > connector. These other two wire are both blue. > > Can someone give me a heads up? > > Thanks, > > John G. 409 > ________________________________________________________________________________
Subject: RVator
From: "tganster" <tganster(at)mwwb.net>
Date: Mar 09, 2008
For those who might not be aware, the first electronic RVator news letter is now available at this link. http://doc.vansaircraft.com/RVator/Download_rvator.htm -------- Tom Ganster 40778 Tailcone Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168672#168672 ________________________________________________________________________________
Subject: Re: TT mounting specifications
From: "orchidman" <gary(at)wingscc.com>
Date: Mar 09, 2008
Thanks all. This is getting real close to having the real thing. I believe I can safely position the location of the cutout on the panel now. I have one of the face plates (thanks to Stein and crew). -------- Gary Blankenbiller RV10 - # 40674 Fuselage SB (N410GB reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168680#168680 ________________________________________________________________________________
Subject: Re: Lower Cowl Mounts
From: "tintopranch" <mark_sutherland(at)yahoo.com>
Date: Mar 09, 2008
I have 150 hrs on my RV10 and I am on my second left bottom hinge which as all ready lost one tab. I am not sure why it happens but I agree that the best idea is to go with screws and nut plates from the start. I will be changing my soon. -------- MARK SUTHERLAND RV-10 40292 Flying since June 07 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168698#168698 ________________________________________________________________________________
Date: Mar 09, 2008
From: Deems Davis <deemsdavis(at)cox.net>
Subject: RV10 missing in Texas
I just saw this posted on VAF "Folks, I am posting this after talking with Doug, with the sole purpose of letting people know what is going on. I propose that we keep the speculation to ZERO, but if you have any factual information, pass it on here. We don't know very much, except that Mark Ritter, of Lockhart, TX is the subject of a search tonight, He left Brenham a few minutes after 1230 this afternoon, headed home, and never showed up. Apparently there was a "ping" from his cell phone about 20 miles northwest of Brenham a few minutes after his departure, according to information I got from his friends out near his home field. He took off about two minutes ahead of me, but we were going opposite directions. We can only hope and pray that he turns up - I am certain that a full-up search will be going when daylight hits tomorrow. Paul Dye " Say some prayer for Mark Deems ________________________________________________________________________________
Date: Mar 09, 2008
From: Rick Sked <ricksked(at)embarqmail.com>
Subject: RV-10 missing in Texas
>From the Vansairforce site. Posted by Paul Dye. Folks, I am posting this after talking with Doug, with the sole purpose of letting people know what is going on. I propose that we keep the speculation to ZERO, but if you have any factual information, pass it on here. We don't know very much, except that Mark Ritter, of Lockhart, TX is the subject of a search tonight, He left Brenham a few minutes after 1230 this afternoon, headed home, and never showed up. Apparently there was a "ping" from his cell phone about 20 miles northwest of Brenham a few minutes after his departure, according to information I got from his friends out near his home field. He took off about two minutes ahead of me, but we were going opposite directions. We can only hope and pray that he turns up - I am certain that a full-up search will be going when daylight hits tomorrow. Paul ________________________________________________________________________________
From: "Russell Daves" <dav1111(at)erfwireless.net>
Subject: Re: Lower Cowl Mounts
Date: Mar 10, 2008
I have 150 hrs on my RV10 and I am on my second left bottom hinge which as all ready lost one tab. I am not sure why it happens but I agree that the best idea is to go with screws and nut plates from the start. I will be changing my soon. -------- MARK SUTHERLAND Instead of screws and nutplates you should consider the floating camlocks from SkyBolt which I installed. Russ Daves N710RV - 190+ hours ________________________________________________________________________________
Subject: Butyl inner tubes "just don't leak"
Date: Mar 10, 2008
From: "Condrey, Bob (US SSA)" <bob.condrey(at)baesystems.com>
As I recall the tubes for the mains are AirStops (butyl) but the nose is not. Bob #40105 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Tim Lewis Sent: Saturday, March 08, 2008 6:34 AM Subject: RV10-List: Butyl inner tubes "just don't leak" A February 2008 Aviation Consumer article on tires says" "...Until recently, tubes were manufactured from a natural rubber compound. Unfortunately, natural rubber is relatively porous and loses pressure more readily than synthetic materials. Therefore, your tires would lose pressure and go soft, too. Enter the butyl rubber tube, now largely the standard among all aircraft inner tube manufacturers. Since unused inner tubes are perfectly good for installation, we're not saying you won't find a natural rubber tube out there on some shop's shelf. It's perfectly serviceable, it just won't hold air as well. Goodyear's Brown says the new butyl tubes, introduced some seven years ago, improve air retention by a factor of about 10. Steve Chlavin of Desser Tire, the GA industry's mega tire retailer, agrees, saying, "The new butyl leak-resistant tubes just don't leak."" It's fairly easy to add air to my RV-6A tires - the valve stems point out, so the tire can be aired through a small hole in the fairing. The situation is more challenging in a stock RV-10 (valve stems on the mains point toward the axle, for example). With this in mind, does anybody know whether the tires Vans shipped with the RV-10 kits are butyl or natural rubber? Tim -- Tim Lewis -- HEF (Manassas, VA) RV-6A N47TD -- 1000 hrs RV-10 #40059 under construction ________________________________________________________________________________
From: Vernon Smith <planesmith(at)hotmail.com>
Subject: Lower Cowl Mounts
Date: Mar 10, 2008
I'm planning on doing a cross between the two ideas and using floating nutp lates: Two Lug Miniature Anchor Nuts Part No. Thread Size Price Buy MF5000-06 6-32 $1.09 MF5000-08 8-32 $0.91 MF5000-3(Manufactured Material Certification Available) 10-32 $0.79 Aircraft Spruce is one source. They are also known as MS21059. Vern Smith (#324) From: dav1111(at)erfwireless.netTo: rv10-list(at)matronics.comSubject: Re: RV10-L ist: Lower Cowl MountsDate: Mon, 10 Mar 2008 06:25:22 -0500 I have 150 hrs on my RV10 and I am on my second left bottom hinge which as all ready lost one tab. I am not sure why it happens but I agree that the best idea is to go with screws and nut plates from the start. I will be changing my soon. -------- MARK SUTHERLANDInst ead of screws and nutplates you should consider the floating camlocks from SkyBolt which I installed. Russ Daves N710RV - 190+ hours _________________________________________________________________ Climb to the top of the charts!-Play the word scramble challenge with sta r power. http://club.live.com/star_shuffle.aspx?icid=starshuffle_wlmailtextlink_ja n ________________________________________________________________________________
Subject: Re: RV-10 missing in Texas
From: "tintopranch" <mark_sutherland(at)yahoo.com>
Date: Mar 10, 2008
this was posted by Austin News Station KXAN... Mark and I have shared RV10 building tips with each other and I hope he is found safe.... Man Missing After Plane Disappears A 71-year-old man is missing after he flew a plane out of Brenham on Sunday, according to a Civil Air Patrol official. The missing man, Mark Ritter, had lunch in Brenham at 12:30 p.m. He said that he wasn't feeling well and was going to head back to his home in Lockhart. The RV10 experimental plane never made it to Lockhart. The last contact with the plane was at 2 p.m. Sunday, 10 miles east of Giddings, just south of 290. Civil Air Patrol Capt. Arthur Woodgate said officials are asking people to look in their backyards and if you have any information, call him at 512-858-1383. You could also call Cmdr. John Ureke at 832-643-5290. KXAN Austin News has a crew on the scene and will bring updates as soon as they become available. -------- MARK SUTHERLAND RV-10 40292 Flying since June 07 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=168809#168809 ________________________________________________________________________________
From: "Albert Gardner" <ibspud(at)roadrunner.com>
Subject: Re: Rudder Trim with Spring Bias
Date: Mar 10, 2008
I used drawing OP38-6 (Electric Trim System) for information on spacing the springs. I can't remember the un-stretched length of the spring but I left a 6" gap between the trim servo arm and the end of the cable from the rudder. The spring never goes slack but I was more worried about over stretching it. I trim full right rudder on take off and it seems to be about right depending on climb out speed and there seems to be adequate trim available for cruise and descent. I didn't measure the pedal force but I think I should have stretched the springs another 1/2" or so. I'm going to order a spring from Vans and see how far it will stretch without distortion. If I need more tension I'll add another spring inside of the one that's there. Albert Gardner Yuma, AZ -----Original Message----- Albert, I really like this approach. I especially like the ease of installation, this is something that could be added after the fact without much headache at all. I do have some questions though. Are the springs initially stretched. What trim force do you think you are getting? I had sent an e-mail to Vans asking what input they thought would be required. They told me that a 5 to 10 pound force as measured at the bottom of the rudder pedal should take care of any 'normal' trim, 25 pounds could be required to compensate for takeoff forces. Jason Kreidler - #40617 4 Partner Build - Finishing ________________________________________________________________________________
From: "Albert Gardner" <ibspud(at)roadrunner.com>
Subject: Lower Cowl Mounts
Date: Mar 10, 2008
I have used nutplates on my RV-9A (850 hrs) and on the RV-10 (68 hrs) and their strong point is reliability and expense. Albert Gardner Yuma, AZ -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Russell Daves I have 150 hrs on my RV10 and I am on my second left bottom hinge which as all ready lost one tab. I am not sure why it happens but I agree that the best idea is to go with screws and nut plates from the start. I will be changing my soon. MARK SUTHERLAND ________________________________________________________________________________
Date: Mar 10, 2008
From: "Pascal" <rv10builder(at)verizon.net>
Subject: Re: Rudder Trim with Spring Bias
Sure seems like another great option with a kit that already exists! My questions? Have you called Van's on this and spoken with Ken K? He might have some insight into the spring tightness and maybe even guidance on the way it is setup. Please do keep us updated on the testing and any changes made /results Thanks for sharing! Pascal ----- Original Message ----- From: "Albert Gardner" <ibspud(at)roadrunner.com> Sent: Monday, March 10, 2008 10:18 AM Subject: RE: RV10-List: Re: Rudder Trim with Spring Bias > > I used drawing OP38-6 (Electric Trim System) for information on spacing > the > springs. I can't remember the un-stretched length of the spring but I left > a > 6" gap between the trim servo arm and the end of the cable from the > rudder. > The spring never goes slack but I was more worried about over stretching > it. > I trim full right rudder on take off and it seems to be about right > depending on climb out speed and there seems to be adequate trim available > for cruise and descent. I didn't measure the pedal force but I think I > should have stretched the springs another 1/2" or so. I'm going to order a > spring from Vans and see how far it will stretch without distortion. If I > need more tension I'll add another spring inside of the one that's there. > Albert Gardner > Yuma, AZ > > -----Original Message----- > Albert, I really like this approach. I especially like the ease of > installation, this is something that could be added after the fact without > much headache at all. I do have some questions though. Are the springs > initially stretched. What trim force do you think you are getting? I had > sent an e-mail to Vans asking what input they thought would be required. > They told me that a 5 to 10 pound force as measured at the bottom of the > rudder pedal should take care of any 'normal' trim, 25 pounds could be > required to compensate for takeoff forces. > Jason Kreidler - #40617 > 4 Partner Build - Finishing > > > ________________________________________________________________________________
Subject: RV-10 missing in Texas
Date: Mar 10, 2008
From: "John W. Cox" <johnwcox(at)pacificnw.com>
This has only tangent connect to the search for Mark, however a similar incident happened here in Oregon several years ago. Robert McCann was departing with a series of Sunday morning pilots who would go for the $100 Ham and Egg breakfast - each and every weekend. He was not feeling well, was flying solo and was the final of 13 pilots to depart Point A. Few of those 13 filed flight plans back to Point B. Everyone knew the route and it was a large gaggle headed the same general direction. Once family members became concerned our aviation club of over 100 aircraft strong wanted to start an immediate air search. Turns out each County Sheriff has the final authority to activate a search or focus on more politically expedient issues. Confusion as to which of three potential counties (Marion, Clackamas or Washington) lead to some disconnect. Aviators were told to Stand Down. Timing was our perception that we would find Robert safe if we could just get involved. Much like the concerted efforts of finding Steve Fossett, little amounts of money or aircraft would change the outcome of a rescue which becomes a search and recovery. It fell into the hands of the leadership of the sheriff and the response of the CAP to close the chapter. My prayers are with clear skies, a strong cellphone battery and a filed flight plan to begin the extensive search. KXAN was reporting light rain this morning and the noon report did not update the story. Paul's report of 20 miles NW and looking at the Direct To course brings back those memories and a need for heighten prayers for a speedy and successful outcome. The issue of 121.5 and February 2009 should be on every builders minds along with your most effective prayers. John Cox -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rick Sked Sent: Sunday, March 09, 2008 8:37 PM Subject: RV10-List: RV-10 missing in Texas >From the Vansairforce site. Posted by Paul Dye. Folks, I am posting this after talking with Doug, with the sole purpose of letting people know what is going on. I propose that we keep the speculation to ZERO, but if you have any factual information, pass it on here. We don't know very much, except that Mark Ritter, of Lockhart, TX is the subject of a search tonight, He left Brenham a few minutes after 1230 this afternoon, headed home, and never showed up. Apparently there was a "ping" from his cell phone about 20 miles northwest of Brenham a few minutes after his departure, according to information I got from his friends out near his home field. He took off about two minutes ahead of me, but we were going opposite directions. We can only hope and pray that he turns up - I am certain that a full-up search will be going when daylight hits tomorrow. Paul ________________________________________________________________________________
Date: Mar 10, 2008
From: Scott Schmidt <scottmschmidt(at)yahoo.com>
Subject: Re: Rudder Trim with Spring Bias
Speaking of rudders and rudder trim I had a bad thing happen in Vegas last weekend. I flew down and on Friday for the Nascar race and parked my plane into the wind and installed my rudder lock. On Saturday a front came thro ugh, the winds reversed had gusts up to 50 knots and it broke my rudder lo ck that I made and caused the rudder to slam side to side and did some cosm etic damage to it. It sheared two of the three rivets on both rudder stops that are attached to the metal brackets on the HS spar. I could not believe it. I don=A2t think I=A2ll be able to fix it and make it look like new so I=A2ll probably be building a new one. (just priced it out last night, $40 0 for a new rudder) I want to add a nice electric rudder trim to it and thi s will give me a chance to do that. I will also be re-designing my rudder lock. It had a weak point in it, I knew it did but never thought there wou ld be enough force on it to break it. =0ALive and learn and luckily I can do some learning for the group. Make sure you use a rudder lock and yes, th ere can be 50 knot gusts when you would never predict it. At least the wea ther was great for the races with a good breeze and Kirby Chamblis flew his Edge 540 for the crowd before the race. =0A=0AI am looking into the "best practices" for rudder trim to adapt to my new rudder and like the idea pres ented in this thread. I am going to leave my wedge on my new rudder and ad d the rudder trim. That way it will very little deflection in cruise. =0A =0AScott Schmidt=0Ascottmschmidt(at)yahoo.com=0A=0A=0A----- Original Message ----=0AFrom: Pascal <rv10builder(at)verizon.net>=0ATo: rv10-list(at)matronics.com =0ASent: Monday, March 10, 2008 12:20:23 PM=0ASubject: Re: RV10-List: Re: R =0A=0ASure seems like another great option with a kit that already exists!=0AMy questions? Have you called Van's on this and spoken with Ken K? He might =0Ahave some insight into the spring tightness and maybe even guidance on the =0Away it is setup.=0APlease do keep us upda ted on the testing and any changes made /results=0AThanks for sharing!=0APa scal=0A----- Original Message ----- =0AFrom: "Albert Gardner" <ibspud@roadr unner.com>=0ATo: =0ASent: Monday, March 10, 2008 1 0:18 AM=0ASubject: RE: RV10-List: Re: Rudder Trim with Spring Bias=0A=0A=0A =0A>=0A> I used drawing OP38-6 (Electric Trim System) for information on sp acing =0A> the=0A> springs. I can't remember the un-stretched length of the spring but I left =0A> a=0A> 6" gap between the trim servo arm and the end of the cable from the =0A> rudder.=0A> The spring never goes slack but I w as more worried about over stretching =0A> it.=0A> I trim full right rudder on take off and it seems to be about right=0A> depending on climb out spee d and there seems to be adequate trim available=0A> for cruise and descent. I didn't measure the pedal force but I think I=0A> should have stretched t he springs another 1/2" or so. I'm going to order a=0A> spring from Vans an d see how far it will stretch without distortion. If I=0A> need more tensio n I'll add another spring inside of the one that's there.=0A> Albert Gardne r=0A> Yuma, AZ=0A>=0A> -----Original Message-----=0A> Albert, I really like this approach. I especially like the ease of=0A> installation, this is so mething that could be added after the fact without=0A> much headache at all . I do have some questions though. Are the springs=0A> initially stretched . What trim force do you think you are getting? I had=0A> sent an e-mail t o Vans asking what input they thought would be required.=0A> They told me t hat a 5 to 10 pound force as measured at the bottom of the=0A> rudder pedal should take care of any 'normal' trim, 25 pounds could be=0A> required to compensate for takeoff forces.=0A> Jason Kreidler - #40617=0A> 4 Partner Bu ======================0A=0A=0A=0A =0A=0A=0A ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: Stainless placard
Date: Mar 10, 2008
What kind of engraving/stamping was done for your tail placards? What kind of cost? Trying to avoid the $100+ placard that nobody ever reads and still comply with the requirement.. ________________________________________________________________________________
From: Jeff Carpenter <jeff(at)westcottpress.com>
Subject: Fuel Tank Corrosion
Date: Mar 10, 2008
When I made my tanks... last May and June... I taped off the areas of the skin that would be mated to the stiffeners and ribs with blue painters tape. I roughened up the surface with scotch brite, cleaned with aluma-prep and assembled with pro-seal. I left the baffle off of the tanks as I was debating the installation of capacitance senders instead of the floats. Over time (can't quite say how much) I pulled up the painters tape. So, I'm now ready to close up the tanks (with the floats) and find that the right tank has a light corrosion in it... primarily under the areas and at the edges of where the tape had been. I believe this is both from the adhesive on the tape as well as my failure to completely rinse the aluma-prep off in some areas. I can remove this with a whole lot of elbow grease and a scotch brite pad. It comes up a bit easier with aluma-prep and a scotch brite pad, but will then run in to the nooks and crannies of the tank and create a new problem somewhere else if I don't rinse quickly enough. Will the presence of fuel in the tank act as corrosion protection and keep this from progressing? Is this process something that stops when the corrosive agent (the aluma prep, or the tape) is removed or "used up," or is this a ball that once rolling won't stop? Jeff Carpenter 40304 Scoth brite Hell Awaiting your reply ________________________________________________________________________________
From: larryrosen(at)comcast.net
Subject: Re: Stainless placard
Date: Mar 10, 2008
$100 no way. Placards from Vans $2.75 for the plain jane one or $12.00 for the fancy vans airforce one. It will cost you more for shipping than the cost of the placard. From the Vans web store http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1205189344-220-669&browse=airframe&product=placards Then have aircraft engravers make engrave them for you. $26. They may be able to supply the placard also. http://www.engravers.net/aircraft/dataplate.htm Larry Rosen #356 -------------- Original message -------------- From: "David McNeill" <dlm46007(at)cox.net> What kind of engraving/stamping was done for your tail placards? What kind of cost? Trying to avoid the $100+ placard that nobody ever reads and still comply with the requirement..
$100 no way.
<DIV>Placards from Vans $2.75 for the plain jane one or $12.00 for the fancy vans airforce one. It will cost you more for shipping than the cost of the placard.  From the Vans web store <A href="http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1205189344-220-669&browse=airframe&product=placards">http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1205189344-220-669&browse=airframe&product=placards</A></DIV>
 
Then have aircraft engravers make engrave them for you.  $26.  They may be able to supply the placard also. http://www.engravers.net/aircraft/dataplate.htm
 
Larry Rosen
#356
 
What kind of engraving/stamping was done for your tail placards? What kind of cost? Trying to avoid the $100+ placard that nobody ever reads and still comply with the requirement..

      
      
      

      
      
      
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Date: Mar 10, 2008
From: Tim Lewis <timrvator(at)comcast.net>
Subject: Re: Electric/Gas Tow Bars
I bought the Tow Buddy. It's the one Wag Aero sells (http://www.ground-support.com/tow_buddy.html and http://store.wagaero.com/index.php?cPath=602_517). I've had it about 2 years, so far so good. I've used it with my RV-10 in the shop, and with my RV-6A out at the hangar. Works with my RV-10 and RV-6A just fine, but the grip width has to be adjusted to go from one to the other, as I recall. Back when I bought mine (Osh 06) they had the normal model and one with a higher power, higher current controller board. I bought that one. (I think they market them as the TB-2000 and TB-3000 now, but ask to be sure). I talked to several of the other manufacturers but couldn't get a clear answer on whether or not their products would work with an RV-10. The folks at Powertow were infuriating to deal with. Wag Aero's folks, on the other hand, put me directly in touch with the guy who knew everything about the Tow Buddy. They worked with me to be certain their unit would work for my needs. The pins they supplied worked with both the RV-10 and RV-6. My only "complaint" is the low key marketing (!) at Wag Aero. They had options (snow chains, the boosted power board) that they didn't even mention in their sales literature or catalog. When I asked I got "sure we have have snow chains... you want those?" and while discussing my concerns about getting my RV-10 up over a hangar lip, the gentleman happened to mention the boosted power option. Hope this helps. Tim -- Tim Lewis -- HEF (Manassas, VA) RV-6A N47TD -- 1000 hrs RV-10 #40059 under construction Rene wrote: > > Any recommendations on Electric or Gas powered tow bars. Now that I > am actually taking the completed....almost....in and out of the hanger > I see a need for one. I can get the airplane out of the hanger no > problem but getting it back in is a different story. I thought about > putting a winch in the back of the hanger and just pulling it in, but > the tow bar may be easier. > > > > Any recommendations for one that works well with the wheel pans on? > > > > Rene' > > 801-721-6080 > > > > > > * > > > * ________________________________________________________________________________
From: "Carl Froehlich" <carl.froehlich(at)cox.net>
Subject: Electric/Gas Tow Bars
Date: Mar 10, 2008
Another option is to use a standard lawn tractor. You need to rig a tow bar so that it connects to the tractor. Several people at the airpark go this route. Some do a tow point on the front of the tractor so that they are facing the airplane when towing. Looking at the price of powered tow bars you can just about buy a new lawn tractor and get some other use out of it. Carl Froehlich RV-8A (400 hrs) RV-10 (wings) _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Tim Lewis Sent: Monday, March 10, 2008 9:42 PM Subject: Re: RV10-List: Electric/Gas Tow Bars I bought the Tow Buddy. It's the one Wag Aero sells (http://www.ground-support.com/tow_buddy.html and http://store.wagaero.com/index.php?cPath=602_517). I've had it about 2 years, so far so good. I've used it with my RV-10 in the shop, and with my RV-6A out at the hangar. Works with my RV-10 and RV-6A just fine, but the grip width has to be adjusted to go from one to the other, as I recall. Back when I bought mine (Osh 06) they had the normal model and one with a higher power, higher current controller board. I bought that one. (I think they market them as the TB-2000 and TB-3000 now, but ask to be sure). I talked to several of the other manufacturers but couldn't get a clear answer on whether or not their products would work with an RV-10. The folks at Powertow were infuriating to deal with. Wag Aero's folks, on the other hand, put me directly in touch with the guy who knew everything about the Tow Buddy. They worked with me to be certain their unit would work for my needs. The pins they supplied worked with both the RV-10 and RV-6. My only "complaint" is the low key marketing (!) at Wag Aero. They had options (snow chains, the boosted power board) that they didn't even mention in their sales literature or catalog. When I asked I got "sure we have have snow chains... you want those?" and while discussing my concerns about getting my RV-10 up over a hangar lip, the gentleman happened to mention the boosted power option. Hope this helps. Tim -- Tim Lewis -- HEF (Manassas, VA) RV-6A N47TD -- 1000 hrs RV-10 #40059 under construction Rene wrote: Any recommendations on Electric or Gas powered tow bars. Now that I am actually taking the completed..almost..in and out of the hanger I see a need for one. I can get the airplane out of the hanger no problem but getting it back in is a different story. I thought about putting a winch in the back of the hanger and just pulling it in, but the tow bar may be easier. Any recommendations for one that works well with the wheel pans on? Rene' 801-721-6080 href="http://www.matronics.com/Navigator?RV10-List">http://www.matronics.com /Navigator?RV10-List href="http://forums.matronics.com">http://forums.matronics.com href="http://www.matronics.com/contribution">http://www.matronics.com/contri bution ________________________________________________________________________________
From: "Doerr, Ray R [NTK]" <Ray.R.Doerr(at)sprint.com>
Date: Mar 11, 2008
Subject: Florida Builders
How long are you going to be in Florida? I'm also originally from Ontario (Walkerton) but live in Kansas now. I will be leaving for Florida (Lakeland KLAL) on Sunday. If your still there, please give me a call. I should be arriving around dinner time on Sunday March 16th and leaving Sunday morning March 23rd. If any others in the area would like to get together, please let me know. Thank You Ray Doerr (913) 226-0106 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Doug Gee Sent: Sunday, March 09, 2008 6:59 AM Subject: RV10-List: Florida Builders I have just flown my 172 from Ont Canada to KZPH for vacation. I am 90 percent sure I am going to build an RV10 as soon as I get some home reno projects out of the way. Just wondering if there are any central Florida builders up for a visit and a "few" questions? Thanks ________________________________________________________________________________
Subject: 90 Degree Oil Filter Housing
From: "dmaib(at)mac.com" <dmaib(at)mac.com>
Date: Mar 11, 2008
Does anybody know if the 1.5 inch spacer for the Casper Labs 90 degree oil filter housing would be the right one for the IO-540 installation on the RV-10? Vans has three different sizes and they say that the 1.5 inch will fit most RV installations, but when I called and asked specifically about this installation, they did not have an answer. I would love to hear from anyone who has installed this adapter. I notice that this product as advertised in Spruce does not mention any spacers. Anybody know how to get in touch with Casper Labs? Google does not get me there. -------- David Maib RV-10 #40559 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169008#169008 ________________________________________________________________________________
Date: Mar 11, 2008
From: Rick Sked <ricksked(at)embarqmail.com>
Subject: Re: 90 Degree Oil Filter Housing
Thats the spacer I used...1.5" from B & C products heres the link, scroll to the bottom of the page. http://www.bandc.biz/cgi-bin/ez-catalog/cat_display.cgi?20X358218 Rick Sked 40185 ----- Original Message ----- From: dmaib(at)mac.com Sent: Tuesday, March 11, 2008 8:02:52 AM (GMT-0800) America/Los_Angeles Subject: RV10-List: 90 Degree Oil Filter Housing Does anybody know if the 1.5 inch spacer for the Casper Labs 90 degree oil filter housing would be the right one for the IO-540 installation on the RV-10? Vans has three different sizes and they say that the 1.5 inch will fit most RV installations, but when I called and asked specifically about this installation, they did not have an answer. I would love to hear from anyone who has installed this adapter. I notice that this product as advertised in Spruce does not mention any spacers. Anybody know how to get in touch with Casper Labs? Google does not get me there. -------- David Maib RV-10 #40559 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169008#169008 ________________________________________________________________________________
From: "Dave Saylor" <Dave(at)AirCraftersLLC.com>
Subject: 90 Degree Oil Filter Housing
Date: Mar 11, 2008
I'm not sure if Casper Labs is different but here is a B&C adapter with a 1.5" spacer on my -10. Dave Saylor AirCrafters LLC 140 Aviation Way Watsonville, CA 831-722-9141 831-750-0284 CL www.AirCraftersLLC.com -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of dmaib(at)mac.com Sent: Tuesday, March 11, 2008 8:03 AM Subject: RV10-List: 90 Degree Oil Filter Housing Does anybody know if the 1.5 inch spacer for the Casper Labs 90 degree oil filter housing would be the right one for the IO-540 installation on the RV-10? Vans has three different sizes and they say that the 1.5 inch will fit most RV installations, but when I called and asked specifically about this installation, they did not have an answer. I would love to hear from anyone who has installed this adapter. I notice that this product as advertised in Spruce does not mention any spacers. Anybody know how to get in touch with Casper Labs? Google does not get me there. -------- David Maib RV-10 #40559 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169008#169008 ________________________________________________________________________________
Subject: 90 Degree Oil Filter Housing
Date: Mar 11, 2008
From: "Condrey, Bob (US SSA)" <bob.condrey(at)baesystems.com>
Dave, What sort of tubing did you use on the crankcase vent line? Bob #40105 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dave Saylor Sent: Tuesday, March 11, 2008 12:42 PM Subject: RE: RV10-List: 90 Degree Oil Filter Housing I'm not sure if Casper Labs is different but here is a B&C adapter with a 1.5" spacer on my -10. Dave Saylor AirCrafters LLC 140 Aviation Way Watsonville, CA 831-722-9141 831-750-0284 CL www.AirCraftersLLC.com -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of dmaib(at)mac.com Sent: Tuesday, March 11, 2008 8:03 AM Subject: RV10-List: 90 Degree Oil Filter Housing Does anybody know if the 1.5 inch spacer for the Casper Labs 90 degree oil filter housing would be the right one for the IO-540 installation on the RV-10? Vans has three different sizes and they say that the 1.5 inch will fit most RV installations, but when I called and asked specifically about this installation, they did not have an answer. I would love to hear from anyone who has installed this adapter. I notice that this product as advertised in Spruce does not mention any spacers. Anybody know how to get in touch with Casper Labs? Google does not get me there. -------- David Maib RV-10 #40559 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169008#169008 ________________________________________________________________________________
Date: Mar 11, 2008
From: "bruce breckenridge" <bbreckenridge(at)gmail.com>
Subject: RE: RV-10 missing in Texas
http://www.keyetv.com/news/local/story.aspx?content_id=4faca74a-e114-4cec-86cd-dafba7fb2fe9 Mark & his aircraft have been found. Our prayers and condolences are with his family. Bruce & Becky Breckenridge 40018 ________________________________________________________________________________
Subject: Re: 90 Degree Oil Filter Housing
From: "dmaib(at)mac.com" <dmaib(at)mac.com>
Date: Mar 11, 2008
I have not done the crankcase vent line yet. The engine is hanging on the hoist in my hangar. Probably won't mount it for another couple of weeks. Thanks for the responses on the spacer. Sounds like the 1.5 is the right one. -------- David Maib RV-10 #40559 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169073#169073 ________________________________________________________________________________
Date: Mar 11, 2008
From: linn Walters <pitts_pilot(at)bellsouth.net>
Subject: Re: RE: RV-10 missing in Texas
bruce breckenridge wrote: > http://www.keyetv.com/news/local/story.aspx?content_id=4faca74a-e114-4cec-86cd-dafba7fb2fe9 > > Mark & his aircraft have been found. Our prayers and condolences are > with his family. Mine too. I think we can all take a little time here and reflect on this tragedy. He wasn't feeling well ...... yet flew home. Just like the sage advice 'friends don't let friends drive drunk', maybe his friends could have prevented the tragedy by offering him a ride home, or a place to stay. But then maybe they wouldn't have made any difference. We'll never know. We've lost a fellow aviator and a beautiful airplane ...... and that's a crying shame. Linn ...... :'( > > Bruce & Becky Breckenridge > 40018 > > ________________________________________________________________________________
From: "Dave Saylor" <Dave(at)AirCraftersLLC.com>
Subject: 90 Degree Oil Filter Housing
Date: Mar 11, 2008
I've used SCAT tube there on a couple installations. It seems to work nicely and it's much easier to manage. -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Condrey, Bob (US SSA) Sent: Tuesday, March 11, 2008 10:55 AM Subject: RE: RV10-List: 90 Degree Oil Filter Housing --> Dave, What sort of tubing did you use on the crankcase vent line? Bob #40105 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Dave Saylor Sent: Tuesday, March 11, 2008 12:42 PM Subject: RE: RV10-List: 90 Degree Oil Filter Housing I'm not sure if Casper Labs is different but here is a B&C adapter with a 1.5" spacer on my -10. Dave Saylor AirCrafters LLC 140 Aviation Way Watsonville, CA 831-722-9141 831-750-0284 CL www.AirCraftersLLC.com -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of dmaib(at)mac.com Sent: Tuesday, March 11, 2008 8:03 AM Subject: RV10-List: 90 Degree Oil Filter Housing Does anybody know if the 1.5 inch spacer for the Casper Labs 90 degree oil filter housing would be the right one for the IO-540 installation on the RV-10? Vans has three different sizes and they say that the 1.5 inch will fit most RV installations, but when I called and asked specifically about this installation, they did not have an answer. I would love to hear from anyone who has installed this adapter. I notice that this product as advertised in Spruce does not mention any spacers. Anybody know how to get in touch with Casper Labs? Google does not get me there. -------- David Maib RV-10 #40559 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169008#169008 ________________________________________________________________________________
Subject: Re: Stainless placard
From: "John Kirkland" <jskirkland(at)webpipe.net>
Date: Mar 11, 2008
I'm partial to the one EAA sells, better looking than plain-Jane. -------- RV-10 #40333 N540XP (reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169102#169102 ________________________________________________________________________________
From: "gary" <speckter(at)comcast.net>
Subject: RE: RV-10 missing in Texas
Date: Mar 11, 2008
Don't flame me on this but when I go I would prefer to go doing what I love, Flying Gary 40274 _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of linn Walters Sent: Tuesday, March 11, 2008 4:52 AM Subject: Re: RV10-List: RE: RV-10 missing in Texas bruce breckenridge wrote: http://www.keyetv.com/news/local/story.aspx?content_id=4faca74a-e114-4cec-86 cd-dafba7fb2fe9 Mark & his aircraft have been found. Our prayers and condolences are with his family. Mine too. I think we can all take a little time here and reflect on this tragedy. He wasn't feeling well ...... yet flew home. Just like the sage advice 'friends don't let friends drive drunk', maybe his friends could have prevented the tragedy by offering him a ride home, or a place to stay. But then maybe they wouldn't have made any difference. We'll never know. We've lost a fellow aviator and a beautiful airplane ...... and that's a crying shame. Linn ...... :'( Bruce & Becky Breckenridge 40018 ________________________________________________________________________________
From: Jeff Carpenter <jeff(at)westcottpress.com>
Subject: Fuel Tank Corrosion, with visual aid
Date: Mar 11, 2008
I asked this question over 24 hours ago and so far there have been no responses. With all that's going on with the list right now I'm going to repost the question, with the attached picture in the hopes I might get some feedback. Where's John Cox when you need him? When I made my tanks... last May and June... I taped off the areas of the skin that would be mated to the stiffeners and ribs with blue painters tape. I roughened up the surface with scotch brite, cleaned with aluma-prep and assembled with pro-seal. I left the baffle off of the tanks as I was debating the installation of capacitance senders instead of the floats. Over time (can't quite say how much) I pulled up the painters tape. So, I'm now ready to close up the tanks (with the floats) and find that the right tank has a light corrosion in it... primarily under the areas and at the edges of where the tape had been. I believe this is both from the adhesive on the tape as well as my failure to completely rinse the aluma-prep off in some areas. I can remove this with a whole lot of elbow grease and a scotch brite pad. It comes up a bit easier with aluma-prep and a scotch brite pad, but will then run in to the nooks and crannies of the tank and create a new problem somewhere else if I don't rinse quickly enough. Will the presence of fuel in the tank act as corrosion protection and keep this from progressing? Is this process something that stops when the corrosive agent (the aluma prep, or the tape) is removed or "used up," or is this a ball that once rolling won't stop? Jeff Carpenter 40304 Scoth brite Hell Awaiting your reply IMG_0257.JPG

      
      
      
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From: John Gonzalez <indigoonlatigo(at)msn.com>
Subject: Fuel Tank Corrosion, with visual aid
Date: Mar 11, 2008
I looked at your post yesterday and really thought about it. First, I am no t sure why this happened, chemically. I realize that Alodine not rinsed can cause corrosion, but I thought that acid removed corrosion. Are you sure t he acid didn't do something to the painters tape, which then made it chemic ally bind to the aluminum or alter the aluminum? When aluminum corrodes, does it not make aluminum oxide which is a white po wder which easily comes off. Certainly re application of alumi prep should remove it. As long as you rinse the alumprep and don't let it dry, why wou ld there be any problems. They put this stuff on the outside of a planes, n ooks and crannies and all before painting. My question, are you certain this is corrosion???? John G. (not a metalergist)> To: rv10-list(at)matronics.com> From: jeff@westco ttpress.com> Subject: RV10-List: Fuel Tank Corrosion, with visual aid> Date o and so far there have been no > responses. With all that's going on with the list right now I'm > going to repost the question, with the attached pi cture in the hopes > I might get some feedback. Where's John Cox when you n eed him?> > When I made my tanks... last May and June... I taped off the ar eas of > the skin that would be mated to the stiffeners and ribs with blue > painters tape. I roughened up the surface with scotch brite, cleaned > wi th aluma-prep and assembled with pro-seal. I left the baffle off > of the t anks as I was debating the installation of capacitance > senders instead of the floats. Over time (can't quite say how much) > I pulled up the painter s tape.> > So, I'm now ready to close up the tanks (with the floats) and fi nd > that the right tank has a light corrosion in it... primarily under > t he areas and at the edges of where the tape had been. I believe > this is b oth from the adhesive on the tape as well as my failure to > completely rin se the aluma-prep off in some areas. I can remove this > with a whole lot o f elbow grease and a scotch brite pad. It comes up > a bit easier with alum a-prep and a scotch brite pad, but will then > run in to the nooks and cran nies of the tank and create a new problem > somewhere else if I don't rinse quickly enough.> > Will the presence of fuel in the tank act as corrosion protection and > keep this from progressing? Is this process something that stops > when the corrosive agent (the aluma prep, or the tape) is removed or > "used up," or is this a ball that once rolling won't stop?> > > Jeff C arpenter> 40304> Scoth brite Hell> Awaiting your reply> > > > > ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: Re: Stainless placard
Date: Mar 11, 2008
Thanks. I found that the Centennial placard I received for the Glastar was unused so will use that one. -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Kirkland Sent: Tuesday, March 11, 2008 3:27 PM Subject: RV10-List: Re: Stainless placard --> I'm partial to the one EAA sells, better looking than plain-Jane. -------- RV-10 #40333 N540XP (reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169102#169102 ________________________________________________________________________________
From: "Bob-tcw" <rnewman(at)tcwtech.com>
Subject: Re: Fuel Tank Corrosion, with visual aid
Date: Mar 11, 2008
----- Original Message ----- From: "Jeff Carpenter" <jeff(at)westcottpress.com> Sent: Tuesday, March 11, 2008 8:01 PM Subject: RV10-List: Fuel Tank Corrosion, with visual aid >I asked this question over 24 hours ago and so far there have been no > responses. With all that's going on with the list right now I'm > going to repost the question, with the attached picture in the hopes > I might get some feedback. Where's John Cox when you need him? > > When I made my tanks... last May and June... I taped off the areas of > the skin that would be mated to the stiffeners and ribs with blue > painters tape. I roughened up the surface with scotch brite, cleaned > with aluma-prep and assembled with pro-seal. I left the baffle off > of the tanks as I was debating the installation of capacitance > senders instead of the floats. Over time (can't quite say how much) > I pulled up the painters tape. > > So, I'm now ready to close up the tanks (with the floats) and find > that the right tank has a light corrosion in it... primarily under > the areas and at the edges of where the tape had been. I believe > this is both from the adhesive on the tape as well as my failure to > completely rinse the aluma-prep off in some areas. I can remove this > with a whole lot of elbow grease and a scotch brite pad. It comes up > a bit easier with aluma-prep and a scotch brite pad, but will then > run in to the nooks and crannies of the tank and create a new problem > somewhere else if I don't rinse quickly enough. > > Will the presence of fuel in the tank act as corrosion protection and > keep this from progressing? Is this process something that stops > when the corrosive agent (the aluma prep, or the tape) is removed or > "used up," or is this a ball that once rolling won't stop? > > > Jeff Carpenter > 40304 > Scoth brite Hell > Awaiting your reply > > -------------------------------------------------------------------------------- > > IMG_0257.JPG > > >

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________________________________________________________________________________
From: "Bob-tcw" <rnewman(at)tcwtech.com>
Subject: Re: Fuel Tank Corrosion, with visual aid
Date: Mar 11, 2008
Jeff, I've had my wings in storage in my unheated hangar for a year now with some blue painters tape holding some of the blue protective film back in place. I'll try to get out to the hangar tomorrow and peel some tape back and report on any corrision due to blue tape alone. The outer skins were not treated with any chemicals (knowingly) Bob Newman TCW Technologies www.tcwtech.com ----- Original Message ----- From: "Jeff Carpenter" <jeff(at)westcottpress.com> Sent: Tuesday, March 11, 2008 8:01 PM Subject: RV10-List: Fuel Tank Corrosion, with visual aid >I asked this question over 24 hours ago and so far there have been no > responses. With all that's going on with the list right now I'm > going to repost the question, with the attached picture in the hopes > I might get some feedback. Where's John Cox when you need him? > > When I made my tanks... last May and June... I taped off the areas of > the skin that would be mated to the stiffeners and ribs with blue > painters tape. I roughened up the surface with scotch brite, cleaned > with aluma-prep and assembled with pro-seal. I left the baffle off > of the tanks as I was debating the installation of capacitance > senders instead of the floats. Over time (can't quite say how much) > I pulled up the painters tape. > > So, I'm now ready to close up the tanks (with the floats) and find > that the right tank has a light corrosion in it... primarily under > the areas and at the edges of where the tape had been. I believe > this is both from the adhesive on the tape as well as my failure to > completely rinse the aluma-prep off in some areas. I can remove this > with a whole lot of elbow grease and a scotch brite pad. It comes up > a bit easier with aluma-prep and a scotch brite pad, but will then > run in to the nooks and crannies of the tank and create a new problem > somewhere else if I don't rinse quickly enough. > > Will the presence of fuel in the tank act as corrosion protection and > keep this from progressing? Is this process something that stops > when the corrosive agent (the aluma prep, or the tape) is removed or > "used up," or is this a ball that once rolling won't stop? > > > Jeff Carpenter > 40304 > Scoth brite Hell > Awaiting your reply > > -------------------------------------------------------------------------------- > > IMG_0257.JPG > > >

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________________________________________________________________________________
Date: Mar 11, 2008
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: 90 Degree Oil Filter Housing
Anyone considered the 45 degree adapter ECI sells? On Tue, Mar 11, 2008 at 12:20 PM, dmaib(at)mac.com wrote: > > I have not done the crankcase vent line yet. The engine is hanging on the > hoist in my hangar. Probably won't mount it for another couple of weeks. > Thanks for the responses on the spacer. Sounds like the 1.5 is the right > one. > > -------- > David Maib > RV-10 #40559 > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=169073#169073 > > ________________________________________________________________________________
Subject: Re: RV-10 missing in Texas
From: "reubanks" <reubanks1(at)sbcglobal.net>
Date: Mar 11, 2008
I read the post below this evening and I cant help but comment on this. You have no idea what Marks friends did or didnt do on the day he left Brenham, or for that matter what exactly was wrong with Mark. It is very irresponsible to make a comment like the one below. Comments like that are hurtful at minimum. The best any of us can do at this point is pray for Marks family and friends. [/quote] Mine too. I think we can all take a little time here and reflect on this tragedy. He wasn't feeling well ...... yet flew home. Just like the sage advice 'friends don't let friends drive drunk', maybe his friends could have prevented the tragedy by offering him a ride home, or a place to stay. But then maybe they wouldn't have made any difference. We'll never know. We've lost a fellow aviator and a beautiful airplane ...... and that's a crying shame. Linn ...... :'( > > Bruce & Becky Breckenridge > 40018 > > > > > > > > > > [b] Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169134#169134 ________________________________________________________________________________
Subject: Fuel Tank Corrosion, with visual aid
Date: Mar 11, 2008
From: "John W. Cox" <johnwcox(at)pacificnw.com>
I'm undergoing knee surgery tomorrow and still a bit heavy hearted over the loss of a fellow member and what I ranked as one of the five prettiest RV-10s ever completed. Damn it! Aluma-prep uses acid to etch and make porous the Alclad finish. (and did you know there is a top side and bottom side finish with visible grain direction.) It is important in pursuit of a quality finish job that the substrate be clean before application of aluma-prep. It is important to neutralize the acid with de-ionized or distilled water. Think of the acid as only a catalyst. Once the reaction begins, you need to remediate and finish the process. The Alodine treatment is chromic acid which hardens the porous finish. The final step is to wash again with Non mineralized water. Often, builders use tap water and introduce contaminants into the chemistry. (Anyone watching all the pharmaceuticals being found in common tap water?) The porous characteristic aides in later primer or sealer application with long term adhesion. Remember that each side of the Alclad only has 5% pure aluminum to turn whitish with oxidation. (You do the math on 0.016 or 0.032 sheet stock). To sand, scotchbrite or acid etch it too much is to go right through to the copper hybrid under the pure aluminum. (It alodines differently). Most Structural Repair Manuals spell out replacement of base material when corrosion reaches 10% of original thickness. That is why as the builder, we need to create our own SRM and know the thickness of all materials we chose to use in assemblage. Just because it came from VANS does not justify guessing later. When corrosion is found, it must be 100% removed or just like a cavity, it just keeps feeding itself. If we have to remediate beyond 10%, its off for a new part(at the airlines). I don't think that is what you want to hear. We often use MEK with proper skin protection to remove contaminates and organics before re-alodining aluminum. Yes we do, re-alodine. Every exposed piece gets the treatment. One of the premises yet to be answered is how does "my beloved proseal" hold up to adulterated corn squeezing inside the fuel tank. I would love for the discussion to get elevated as to which components need to be replaced to embrace subsidizing American Farmers instead of importation of $110+ per barrel crude and amplify our balance of trade deficit to Third World Tycoons. How about our President opening the US strategic oil reserves to wipe out all of the US hedge fund investors who are making this situation worse by pumping up artificial demand. Fuel in the tank acts to reduce airborne oxidants but does not eliminate them. That is the old wives tale of keep tanks topped off. The ball will stop rolling when it is removed from the playing field. It doesn't stop on its own. Sorry. Study Intergranular and Exfoliation Corrosion. "http://aluminium.matter.org.uk/content/html/eng/default.asp?catid=180&p ageid=2144416690" Use at least a 5X loop or 10X loop to view the degree of corrosion remaining. John Cox 40600 Pegleg Hell in Portland -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Jeff Carpenter Sent: Tuesday, March 11, 2008 5:01 PM Subject: RV10-List: Fuel Tank Corrosion, with visual aid I asked this question over 24 hours ago and so far there have been no responses. With all that's going on with the list right now I'm going to repost the question, with the attached picture in the hopes I might get some feedback. Where's John Cox when you need him? Will the presence of fuel in the tank act as corrosion protection and keep this from progressing? Is this process something that stops when the corrosive agent (the aluma prep, or the tape) is removed or "used up," or is this a ball that once rolling won't stop? Jeff Carpenter 40304 Scoth brite Hell Awaiting your reply ________________________________________________________________________________
Date: Mar 11, 2008
From: "Pascal" <rv10builder(at)verizon.net>
Subject: Re: RV-10 missing in Texas
I think many of us are simply too upset to see yet another RV-10 builder lost in less than 6 months to bother with responding to Linn's comment and wasting time on this thread. I never met Mark, but I certainly have his plane as one of my desktop screensavers and remember his sharing the excitement when the plane came out of the paint shop.. I am saddened of his loss and could care less why he flew, I do care that we lost a fellow comrade and that seems to be all that is important to me. Hope we see some more postings from you reubanks. Pascal ----- Original Message ----- From: "reubanks" <reubanks1(at)sbcglobal.net> Sent: Tuesday, March 11, 2008 6:32 PM Subject: RV10-List: Re: RV-10 missing in Texas > > I read the post below this evening and I cant help but comment on this. > You have no idea what Marks friends did or didnt do on the day he left > Brenham, or for that matter what exactly was wrong with Mark. It is very > irresponsible to make a comment like the one below. Comments like that > are hurtful at minimum. The best any of us can do at this point is pray > for Marks family and friends. > > [/quote] Mine too. I think we can all take a little time here and reflect > on this tragedy. He wasn't feeling well ...... yet flew home. Just like > the sage advice 'friends don't let friends drive drunk', maybe his friends > could have prevented the tragedy by offering him a ride home, or a place > to stay. But then maybe they wouldn't have made any difference. We'll > never know. We've lost a fellow aviator and a beautiful airplane ...... > and that's a crying shame. > Linn ...... :'( > > >> >> Bruce & Becky Breckenridge >> 40018 >> >> > >> > >> > >> > >> [b] > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=169134#169134 > > > ________________________________________________________________________________
From: "Jay Rowe" <jfrjr(at)roadrunner.com>
Subject: traveling tool
Date: Mar 11, 2008
Deems and Barry M: The countersink cutter arrived safe and sound. Will do my work tomorrow AM and then get it in the mail to Barry in FL. Barry should know who is next on the list. Thanks to all. Jay ________________________________________________________________________________
Date: Mar 11, 2008
From: "Fred Williams, M.D." <drfred(at)suddenlinkmail.com>
Subject: Re: RV-10 missing in Texas
Fellow RV er's I want to send my condolences to the whole RV family who lost a good person yesterday. I had the pleasure of meeting Mark this last Christmas vacation. My daughter and I were flying the 152 between Paris and Corpus Christi. Brenham is about half way for us. We stopped in for lunch and Mark was there with his 10. He was kind enough to take the time and show my teenage daughter what a "real" RV 10 looks like (not the pieces in my shop). He answered a bunch of my questions and cleaned some drool off of his paint. He even took the time to answer a later email question from me. I only knew him for 30 minutes, but he seemed like a real gentleman. He will be missed. Fred Williams 40515 ________________________________________________________________________________
Date: Mar 11, 2008
From: linn Walters <pitts_pilot(at)bellsouth.net>
Subject: Re: RV-10 missing in Texas
reubanks wrote: > >I read the post below this evening and I cant help but comment on this. You have no idea what Marks friends did or didnt do on the day he left Brenham, > Yes, that is true. > or for that matter what exactly was wrong with Mark. > Again, true. > It is very irresponsible to make a comment like the one below. > I don't think so, and admitted that his friends may not have made any difference. > Comments like that are hurtful at minimum. > I apologize. It wasn't menat to be hurtful, and I do see your point. > The best any of us can do at this point is pray for Marks family and friends. > No, the best we can do is look out for our fellow friends and aviators. I don't know Mark ..... wish I did, but the bottom line (as posted here) is that he wasn't feeling well and flew off anyway. You're absolutely correct .... I don't know if what was bothering him had any bearing on the accident ..... but the point I was trying to make is that no matter what caused his accident, the decision to fly home was, in my mind, a poor one, and that we are our brothers' keepers. My post was meant only to remind folks of that fact, and not be, in any way, as chastizing. Again, I apologize for any hurt my comment caused. Linn > > [/quote] Mine too. I think we can all take a little time here and reflect on this tragedy. He wasn't feeling well ...... yet flew home. Just like the sage advice 'friends don't let friends drive drunk', maybe his friends could have prevented the tragedy by offering him a ride home, or a place to stay. But then maybe they wouldn't have made any difference. We'll never know. We've lost a fellow aviator and a beautiful airplane ...... and that's a crying shame. > Linn ...... :'( > > > > >> >> Bruce & Becky Breckenridge >> 40018 >> >> >> >>> >>> >>> >>> >> [b] >> >> > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=169134#169134 > > > > ________________________________________________________________________________
From: "bob.kaufmann" <bob.kaufmann(at)cox.net>
Subject: RE: RV-10 missing in Texas
Date: Mar 11, 2008
I offer my prayers and condolences for the family. I have lost way to many friends this year already, and although some of them were a little crusty I have a deep love for them. I please request that we all do the best that we can to help each other in love and fellowship and keep pounding rivets or twisting wires. Bob K Like Deems, its done just not all together yet. N104BK, someday. ________________________________________________________________________________
Date: Mar 11, 2008
From: Jerry Stark <jerry_stark(at)prodigy.net>
Subject: Mark Ritter
I met Mark a number years ago. He was an example of what EAA was about. He shared his building experiences, his goals, and his successes and his redoes. His work was meticulous. His enthusiasm was always present. Yes I am a lurker and social security keeps me from jumping on the "I got to build one". I have been lurking since day one of the forum. I did not know Mark that well. I flew to Lockhart a number of times. He was a little shy early in his build about posting ( My opinion ) but his work was very detailed. He opened up once he got flying (my opinion ). I stopped to see him in Lockhart a few times and after he was flying, he was usually flying to Brenham to eat lunch, he loved the blue bell icecream. I also remember his offer to Jesse Saint to take him to Texas BBQ if he came to Texas. He was a generous man and I am sorry not to be able to interact with again. God bless the survivors! his Family and friends. It was a torturous weekend. This forum is generally very informative. There are times when it becomes a " I got to talk to somebody" thing, but I so enjoy it. God Bless all of us; our time is temporary, make the most of it. Some one said " we aren't here for a long time, we are here for a good time." God Bless Mark and his family. May the rest of us enjoy his life as much as he did. ________________________________________________________________________________
From: Rob Kermanj <flysrv10(at)gmail.com>
Subject: Re: 90 Degree Oil Filter Housing
Date: Mar 12, 2008
I have one on mine with 310 hrs on the plane. What do you need to know? The breather tube has to be talked to in order to clear the filter. Otherwise, nothing else to worry about. I drain my oil overnight and have zero drip when I remove the filter the next day. Rob. On Mar 11, 2008, at 9:15 PM, Kelly McMullen wrote: > Anyone considered the 45 degree adapter ECI sells? > > On Tue, Mar 11, 2008 at 12:20 PM, dmaib(at)mac.com wrote: > > I have not done the crankcase vent line yet. The engine is hanging > on the hoist in my hangar. Probably won't mount it for another > couple of weeks. > Thanks for the responses on the spacer. Sounds like the 1.5 is the > right one. > > -------- > David Maib > RV-10 #40559 > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=169073#169073 > > ________________________________________________________________________________
Date: Mar 12, 2008
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: 90 Degree Oil Filter Housing
Great. Exactly what I wanted to know. Looks like the tach drive might be a bit tight. I gather there is no issue with the engine mount or cowling clearance. On Wed, Mar 12, 2008 at 4:29 AM, Rob Kermanj wrote: > I have one on mine with 310 hrs on the plane. What do you need to know? > > The breather tube has to be talked to in order to clear the filter. > Otherwise, nothing else to worry about. > > I drain my oil overnight and have zero drip when I remove the filter the > next day. > > Rob. > > > On Mar 11, 2008, at 9:15 PM, Kelly McMullen wrote: > > Anyone considered the 45 degree adapter ECI sells? > > On Tue, Mar 11, 2008 at 12:20 PM, dmaib(at)mac.com wrote: > > > > > I have not done the crankcase vent line yet. The engine is hanging on the > hoist in my hangar. Probably won't mount it for another couple of weeks. > > Thanks for the responses on the spacer. Sounds like the 1.5 is the right > one. > > > > -------- > > David Maib > > RV-10 #40559 > > > > > > > > > > Read this topic online here: > > > > http://forums.matronics.com/viewtopic.php?p=169073#169073 > > > > > > > > > > > > > > > > > > > > > > > > > href="http://www.matronics.com/Navigator?RV10-List">http://www.matronics.com/Navigator?RV10-List > href="http://forums.matronics.com">http://forums.matronics.com > href="http://www.matronics.com/contribution">http://www.matronics.com/contribution > > ________________________________________________________________________________
Date: Mar 12, 2008
From: curtis groote <cgroote1(at)yahoo.com>
Subject: Re: Electric/Gas Tows
Last summer I researched several aircraft tugs and winches. The -10 was too much for me to get out of the hangar let alone getting it back in up an incline. I didn't want an electric cord to deal with and wasn't enamored with starting a gas engine in the winter. Initially I thought about the Powertow EZ40 but after sending in measurements twice along with at least five subsequent phone calls and making no progress over a month's time, I decided to shop elsewhere. What I have now is an Aero-Tow E-200. Terry was extremely easy and pleasant to deal with and made the adaptors for the -10 without any fuss. The unit trickle charges so it's always ready and does what I need it to do. Never miss a thing. Make Yahoo your home page. http://www.yahoo.com/r/hs ________________________________________________________________________________
Subject: Re: Fuel Tank Corrosion, with visual aid
Date: Mar 12, 2008
From: nicholscatoauto(at)aol.com
While we are on the fuel tank topic John Cox brings up a good point about alcohol and its effects on proseal. I am about 4 weeks away from starting my fuel tanks and would really like to build the entire fuel system to accept a moderate amount of alcohol, say 10%.? Is anybody else taking a proactive approach to possibly using fuel with alcohol in it. Not that I would use it as a general rule but it would always be an option if needed. If anyone has any insight or thoughts fire away. Jeff Nichols 40648 -----Original Message----- From: John W. Cox <johnwcox(at)pacificnw.com> Sent: Tue, 11 Mar 2008 7:43 pm Subject: RE: RV10-List: Fuel Tank Corrosion, with visual aid One of the premises yet to be answered is how does "my beloved proseal" hold up to adulterated corn squeezing inside the fuel tank. I would love for the discussion to get elevated as to which components need to be replaced to embrace subsidizing American Farmers instead of importation of $110+ per barrel crude and amplify our balance of trade deficit to Third World Tycoons. ________________________________________________________________________________
From: Rob Kermanj <flysrv10(at)gmail.com>
Subject: Re: 90 Degree Oil Filter Housing
Date: Mar 12, 2008
The tach drive is indeed very close but I can't tell you how close, based on my memory. Of course, if you are using any kind of glass panel, you will not need the tach cable. If you need to know how close they are, I will have to look when I take the cowl off. Let me know. There are no issues with the mount or cowl. You will need the 1.5 inch spacer for the adopter. Rob On Mar 12, 2008, at 9:54 AM, Kelly McMullen wrote: > > Great. Exactly what I wanted to know. Looks like the tach drive might > be a bit tight. I gather there is no issue with the engine mount or > cowling clearance. > > On Wed, Mar 12, 2008 at 4:29 AM, Rob Kermanj > wrote: >> I have one on mine with 310 hrs on the plane. What do you need to >> know? >> >> The breather tube has to be talked to in order to clear the filter. >> Otherwise, nothing else to worry about. >> >> I drain my oil overnight and have zero drip when I remove the >> filter the >> next day. >> >> Rob. >> >> >> On Mar 11, 2008, at 9:15 PM, Kelly McMullen wrote: >> >> Anyone considered the 45 degree adapter ECI sells? >> >> On Tue, Mar 11, 2008 at 12:20 PM, dmaib(at)mac.com >> wrote: >> >>> >>> I have not done the crankcase vent line yet. The engine is hanging >>> on the >> hoist in my hangar. Probably won't mount it for another couple of >> weeks. >>> Thanks for the responses on the spacer. Sounds like the 1.5 is the >>> right >> one. >>> >>> -------- >>> David Maib >>> RV-10 #40559 >>> >>> >>> >>> >>> Read this topic online here: >>> >>> http://forums.matronics.com/viewtopic.php?p=169073#169073 >>> >>> >>> >>> >>> >>> >>> >>> >>> >>> >>> >> >> >> href="http://www.matronics.com/Navigator?RV10-List">http://www.matronics.com/Navigator?RV10-List >> href="http://forums.matronics.com">http://forums.matronics.com >> href="http://www.matronics.com/contribution">http://www.matronics.com/contribution >> >> >> >> >> >> >> >> > > ________________________________________________________________________________
Date: Mar 12, 2008
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: 90 Degree Oil Filter Housing
Thanks. That covers all I need to know. Rob Kermanj wrote: > > The tach drive is indeed very close but I can't tell you how close, > based on my memory. Of course, if you are using any kind of glass > panel, you will not need the tach cable. > > If you need to know how close they are, I will have to look when I > take the cowl off. Let me know. > > There are no issues with the mount or cowl. You will need the 1.5 > inch spacer for the adopter. > > Rob > > On Mar 12, 2008, at 9:54 AM, Kelly McMullen wrote: > >> >> Great. Exactly what I wanted to know. Looks like the tach drive might >> be a bit tight. I gather there is no issue with the engine mount or >> cowling clearance. >> >> On Wed, Mar 12, 2008 at 4:29 AM, Rob Kermanj wrote: >>> I have one on mine with 310 hrs on the plane. What do you need to >>> know? >>> >>> The breather tube has to be talked to in order to clear the filter. >>> Otherwise, nothing else to worry about. >>> >>> I drain my oil overnight and have zero drip when I remove the filter >>> the >>> next day. >>> >>> Rob. >>> >>> >>> On Mar 11, 2008, at 9:15 PM, Kelly McMullen wrote: >>> >>> Anyone considered the 45 degree adapter ECI sells? > ================================================ ________________________________________________________________________________
Date: Mar 12, 2008
From: "bruce breckenridge" <bbreckenridge(at)gmail.com>
Subject: Re: RV-10 missing in Texas
Thanks Chuck. It was actually Linn's comments, but our info was still danglin' at the bottom. I sorta thought the same thing: "uh-oh, what'd I say?!!" Bruce ________________________________________________________________________________
From: "Chris" <toaster73(at)embarqmail.com>
Subject: Infinity Grip...am I crazy?
Date: Mar 12, 2008
So I am trying (again) to decide what buttons to put on my grip. If I understand things correctly I can do the following: Trigger - PTT China Hat - Trim Top Right (use toggles w/ center off, mom - on up and down): frequency flip flop from standby on com1 (up) and com 2 (down) via SL30 and 430 Top Left (use toggles w/ center off, mom -on up and down): screen paging on GRT1 and GRT 2 via GRT Middle (NO 8632 push button) : Autopilot control wheel steering via trutrak Bottom pinky (NO 8632 push button) : swap com1 and com2 via GMA 340 Does this seem like a good setup or is it overkill with stuff I won't use? Also does it appear to all be doable? Thanks Chris Lucas #40072 electrics - cabin top - doors- overhead console - door locks - stick grips - panel - landing gear - engine mount ________________________________________________________________________________
From: John Gonzalez <indigoonlatigo(at)msn.com>
Subject: Infinity Grip...am I crazy?
Date: Mar 12, 2008
Make sure you have a heads up display with the directions on how to use the stick. While you at it, push forward--down, Pull Back --Up and side to sid e. Top of the list should read, Look out window and fly plane. can't help myself. John G. From: toaster73(at)embarqmail.comTo: rv10-list(at)matronics.comSubject: RV10-List : Infinity Grip...am I crazy?Date: Wed, 12 Mar 2008 14:53:57 -0400 So I am trying (again) to decide what buttons to put on my grip. If I unde rstand things correctly I can do the following: Trigger - PTT China Hat - Trim Top Right (use toggles w/ center off, mom - on up and down): frequency flip flop from standby on com1 (up) and com 2 (down) via SL30 and 430 Top Left (use toggles w/ center off, mom -on up and down): screen paging o n GRT1 and GRT 2 via GRT Middle (NO 8632 push button) : Autopilot control wheel steering via trutrak Bottom pinky (NO 8632 push button) : swap com1 and com2 via GMA 340 Does this seem like a good setup or is it overkill with stuff I won't use? Also does it appear to all be doable? Thanks Chris Lucas #40072 electrics - cabin top - doors- overhead console - door locks - stick grips - panel - landing gear - engine mount ________________________________________________________________________________
Date: Mar 12, 2008
From: Rick Sked <ricksked(at)embarqmail.com>
Subject: Re: Infinity Grip...am I crazy?
I used the top left and right buttons for the TT Autopilot control wheel st eering, pinky for AP disengage hat for trim, trigger for PTT. But then agai n I have the CH grip Rick Sked 40185 ----- Original Message ----- From: "Chris" <toaster73(at)embarqmail.com> Sent: Wednesday, March 12, 2008 11:53:57 AM (GMT-0800) America/Los_Angeles Subject: RV10-List: Infinity Grip...am I crazy? So I am trying (again) to decide what buttons to put on my grip.=C2- If I understand things correctly I can do the following: Trigger - PTT China Hat - Trim Top Right (use toggles w/ center off, mom - on up and down): frequency flip flop from standby on com1=C2-(up) and com 2 (down) via SL30 and 430 Top Left (use toggles w/ center off, mom -on up and down):=C2-=C2-scree n paging on GRT1 and GRT 2 via GRT Middle (NO 8632 push button)=C2-: Autopilot control wheel steering via tr utrak Bottom pinky (NO 8632 push button)=C2- : swap com1=C2-and com2 via GMA 340 Does this seem like a good setup or is it overkill with stuff I won't use? Also does it appear to all be doable? Thanks Chris Lucas #40072 electrics - cabin top - doors- overhead console - door locks - stick grips - panel - landing gear - engine mount ==== ======================= == ________________________________________________________________________________
From: GRANSCOTT(at)aol.com
Date: Mar 12, 2008
Subject: Re: RV-10 missing in Texas
A group that was over looked in this tragedy is the folks in Civil AirPatrol, AFRCC, and local law enforcement that completed an excellent search pattern, quickly finding this downed airman when weather permitted them to search...I know that they are not reading this site...but a big note of thanks for their volunteerism on the CAP folks and the professionalism of the others. It's just tragic that they we're not able to Mark alive. Patrick **************It's Tax Time! Get tips, forms, and advice on AOL Money & Finance. (http://money.aol.com/tax?NCID=aolprf00030000000001) ________________________________________________________________________________
Date: Mar 12, 2008
From: Rick Sked <ricksked(at)embarqmail.com>
Subject: Re: Infinity Grip...am I crazy?
I use push, houses get bigger, pull houses get smaller...for awhile, then t hey get bigger again. Rick Sked 40185 don not archive ----- Original Message ----- From: "John Gonzalez" <indigoonlatigo(at)msn.com> Sent: Wednesday, March 12, 2008 12:27:42 PM (GMT-0800) America/Los_Angeles Subject: RE: RV10-List: Infinity Grip...am I crazy? Make sure you have a heads up display with the directions on how to use the stick. While you at it, push forward--down, Pull Back --Up and side to sid e. Top of the list should read, Look out window and fly plane. =C2- can't help myself. =C2- John G. =C2- =C2- =C2- From: toaster73(at)embarqmail.com Subject: RV10-List: Infinity Grip...am I crazy? Date: Wed, 12 Mar 2008 14:53:57 -0400 So I am trying (again) to decide what buttons to put on my grip.=C2- If I understand things correctly I can do the following: Trigger - PTT China Hat - Trim Top Right (use toggles w/ center off, mom - on up and down): frequency flip flop from standby on com1=C2-(up) and com 2 (down) via SL30 and 430 Top Left (use toggles w/ center off, mom -on up and down):=C2-=C2-scree n paging on GRT1 and GRT 2 via GRT Middle (NO 8632 push button)=C2-: Autopilot control wheel steering via tr utrak Bottom pinky (NO 8632 push button)=C2- : swap com1=C2-and com2 via GMA 340 Does this seem like a good setup or is it overkill with stuff I won't use? Also does it appear to all be doable? Thanks Chris Lucas #40072 electrics - cabin top - doors- overhead console - door locks - stick grips - panel - landing gear - engine mount get=_blank>http://www.matronics.com/Navigator?RV10-List p://forums.matron == ==== ======================= == ________________________________________________________________________________
Subject: Infinity Grip...am I crazy?
Date: Mar 12, 2008
From: "Chris Johnston" <CJohnston(at)popsound.com>
Won't the CWS button also disengage the AP? I'm in the process of figuring out what should control what with my stick grip. cj -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rick Sked Sent: Wednesday, March 12, 2008 12:30 PM Subject: Re: RV10-List: Infinity Grip...am I crazy? I used the top left and right buttons for the TT Autopilot control wheel steering, pinky for AP disengage hat for trim, trigger for PTT. But then again I have the CH grip Rick Sked 40185 ----- Original Message ----- From: "Chris" <toaster73(at)embarqmail.com> Sent: Wednesday, March 12, 2008 11:53:57 AM (GMT-0800) America/Los_Angeles Subject: RV10-List: Infinity Grip...am I crazy? So I am trying (again) to decide what buttons to put on my grip. If I understand things correctly I can do the following: Trigger - PTT China Hat - Trim Top Right (use toggles w/ center off, mom - on up and down): frequency flip flop from standby on com1 (up) and com 2 (down) via SL30 and 430 Top Left (use toggles w/ center off, mom -on up and down): screen paging on GRT1 and GRT 2 via GRT Middle (NO 8632 push button) : Autopilot control wheel steering via trutrak Bottom pinky (NO 8632 push button) : swap com1 and com2 via GMA 340 Does this seem like a good setup or is it overkill with stuff I won't use? Also does it appear to all be doable? Thanks Chris Lucas #40072 electrics - cabin top - doors- overhead console - door locks - stick grips - panel - landing gear - engine mount ________________________________________________________________________________
Date: Mar 12, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: Infinity Grip...am I crazy?
Yeah, they're one in the same. Tim Olson - RV-10 N104CD - Flying Chris Johnston wrote: > Wont the CWS button also disengage the AP? Im in the process of > figuring out what should control what with my stick grip. > > > > cj ________________________________________________________________________________
From: "Chuck Weyant" <chuck(at)chuckdirect.com>
Subject: Performance of Hartzell Blended Airfoil
Date: Mar 12, 2008
I've got a chance to purchase a brand new Hartzell constant speed that's been in the box for four years for $4,500. Standard 80" blades. Van's has a new Hartzell prop with blended air foil type blades for $6,300. Anyone out there know if the difference in performance between the two is worth the additional $2,000? Chuck ________________________________________________________________________________
From: "Bob-tcw" <rnewman(at)tcwtech.com>
Subject: Re: Fuel Tank Corrosion
Date: Mar 12, 2008
Jeff, I visited my hangar today to inspect my wings that have beeen in storage. I had blue painters tape on a half a dozen places directly on the aluminum. About 3 or 4 of the locations were tape directly on aluminum that had the alclad buffed off. The other places had tape on undisturbed alclad. None of the places showed any sign of corrosion. I know that we can get some very humid conditions here, particularly when we have a very cold day, followed by a warm day. On many occasions I find my airplane completely covered in dew from the temperature swing through the dew point. This is particularly prevalent this time of year as we transition out of winter. Best regards, Bob Newman TCW Technologies www.tcwtech.com ________________________________________________________________________________
From: "Chuck Weyant" <chuck(at)chuckdirect.com>
Subject: Hartzell blended airfoil performance
Date: Mar 12, 2008
I've got a chance to purchase a brand new Hartzell constant speed that's been in the box for four years for $4,500. Standard 80" blades. Van's has a new Hartzell prop with blended air foil type blades for $6,300. Anyone out there know if the difference in performance between the two is worth the additional $2,000? Chuck ________________________________________________________________________________
Date: Mar 12, 2008
From: Robert Wright <flywrights(at)yahoo.com>
Subject: Door fit
All, I've been looking at the way my doors fit to the canopy and am wondering, "Since I did as good a job as I could, including clamping everything flush while the epoxy set, then why do I have a slight bulge on one door in relation to the canopy," and, "should everything look perfect as a result of trimming, or should I naturally be expecting to add some filler between the canopy and doors to make everything smooth and ready for paint?" Reading through other websites, they're written up to seem like masters of the fiberglass trimming, and once trimmed and glued they're ready for the paint booth after a coat of primer on. Thoughts and pointers? Rob Wright #392 starting on door hinges Looking for last minute shopping deals? ________________________________________________________________________________
Subject: Hartzell blended airfoil performance
Date: Mar 13, 2008
From: "Robin Marks" <robin1(at)mrmoisture.com>
Check, If my math is right it's $1,800 less, not $2,000. Yes I round everything too, round down on -10 costs for my wife and round up -10 performance for my friends. The BA is significantly faster while parked that the square tipped Hartzell. I THINK the TBO on the BA is 6 years. If that is the case for the boxed prop you are you 2 years from an OH? I don't know when the clock starts. I doubt the boxed prop is warranted anymore. If an OH is due in 2+/- years that makes the price difference even smaller. Baring any info suggesting the boxed prop is a better then the BA I would purchase the new, fully warranted BA. Think of it as second guess insurance. You know, how you may second guess your choice for the remainder of the time you own the -10. I have a non-BA Hartzell on my RV-6A and wish it was a brand spankin' new BA in its place. Robin -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Chuck Weyant Sent: Wednesday, March 12, 2008 8:06 PM Subject: RV10-List: Hartzell blended airfoil performance I've got a chance to purchase a brand new Hartzell constant speed that's been in the box for four years for $4,500. Standard 80" blades. Van's has a new Hartzell prop with blended air foil type blades for $6,300. Anyone out there know if the difference in performance between the two is worth the additional $2,000? Chuck ________________________________________________________________________________
Subject: Door fit
Date: Mar 13, 2008
From: "McGANN, Ron" <ron.mcgann(at)baesystems.com>
YMMV - but ". . . should I naturally be expecting to add some filler between the canopy and doors to make everything smooth and ready for paint?" is where I ended up. Especially after the door seals were installed. cheers, Ron 187 finishing ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Robert Wright Sent: Thursday, 13 March 2008 2:41 PM To: rv10-list(at)matronics.com Subject: RV10-List: Door fit All, I've been looking at the way my doors fit to the canopy and am wondering, "Since I did as good a job as I could, including clamping everything flush while the epoxy set, then why do I have a slight bulge on one door in relation to the canopy," and, "should everything look perfect as a result of trimming, or should I naturally be expecting to add some filler between the canopy and doors to make everything smooth and ready for paint?" Reading through other websites, they're written up to seem like masters of the fiberglass trimming, and once trimmed and glued they're ready for the paint booth after a coat of primer on. Thoughts and pointers? Rob Wright #392 starting on door hinges ________________________________ Be a better friend, newshound, and "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." ________________________________________________________________________________
Date: Mar 12, 2008
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: Door fit
Rob, My experience was certainly Not ' cut/glue/hang/ it was more like... cut/glue/hang/fill/sand/hang/fill/sand/hang/fill/sand.......... you get the picture. http://deemsrv10.com/cabinwindowslogindex.html I'm NO master of fiberglass / epoxy, the good news is you really don't have to be, other than it being messy and sticky, there's not too much you can do w/ fiberglass that can't be corrected if you goof up. In the end (I haven't installed door seals yet ....?) I'm happy with the fit of the doors to the cabin cover. But it took a LOT of additional work. A lot of it depends on you own taste and preferences, Van's fiberglass parts are not made with the same precision as the CNC metal parts. I'm sure that they all possess the required strength to do their respective functions. The additional work is really a mater of cosmetics and your personal preferences. Deems Davis # 406 'Its all done....Its just not put together' http://deemsrv10.com/ Robert Wright wrote: > All, > > I've been looking at the way my doors fit to the canopy and am > wondering, "Since I did as good a job as I could, including clamping > everything flush while the epoxy set, then why do I have a slight > bulge on one door in relation to the canopy," and, "should everything > look perfect as a result of trimming, or should I naturally be > expecting to add some filler between the canopy and doors to make > everything smooth and ready for paint?" > > Reading through other websites, they're written up to seem like > masters of the fiberglass trimming, and once trimmed and glued they're > ready for the paint booth after a coat of primer on. > > Thoughts and pointers? > * > > * ________________________________________________________________________________
From: "John Dunne" <acs(at)acspropeller.com.au>
Subject: Door fit
Date: Mar 13, 2008
Rob, I was very careful as well but in the end you could fit a small animal between the door and the canopy. I ended up fibreglassing my doors shut and then creating and molding the canopy to the door with a gentle transition. Finally I re-cut the original opening back through. Wasted a lot of time on this and agonized over it way too much and in the end it was simple enough to fix. I also removed the small animal so it didn't suffocate because the doors were now airtight. John 40315 Cowls. _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Robert Wright Sent: Thursday, 13 March 2008 2:11 PM Subject: RV10-List: Door fit All, I've been looking at the way my doors fit to the canopy and am wondering, "Since I did as good a job as I could, including clamping everything flush while the epoxy set, then why do I have a slight bulge on one door in relation to the canopy," and, "should everything look perfect as a result of trimming, or should I naturally be expecting to add some filler between the canopy and doors to make everything smooth and ready for paint?" Reading through other websites, they're written up to seem like masters of the fiberglass trimming, and once trimmed and glued they're ready for the paint booth after a coat of primer on. Thoughts and pointers? Rob Wright #392 starting on door hinges _____ Be a better friend, newshound, and ________________________________________________________________________________
From: "John Dunne" <acs(at)acspropeller.com.au>
Subject: Hartzell blended airfoil performance
Date: Mar 13, 2008
Hartzell service letter HC-SL-61-61Y extract only: " C. Calendar Limits (1) The effects of exposure to the environment over a period of time create a need for propeller overhaul regardless of flight time. Corrosion can create hidden defects in critical blade retention components; therefore, a 36, 60 or 72 calendar month limit between overhauls is specified. (2) Start date for calendar limit is when the propeller is first installed and run on an engine. Calendar limit is not interrupted by subsequent removal and/or storage " One thing to check is the full s/n of the hub unit. Make sure it has a "B" suffix e.g AU12345 B. There are some limiting AD's and SB's on the early model hubs when bolted to an O/IO-540. Other than that like Robin says it's significantly faster whilst parked. John 40315 cowls " -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Robin Marks Sent: Thursday, 13 March 2008 2:28 PM Subject: RE: RV10-List: Hartzell blended airfoil performance Check, If my math is right it's $1,800 less, not $2,000. Yes I round everything too, round down on -10 costs for my wife and round up -10 performance for my friends. The BA is significantly faster while parked that the square tipped Hartzell. I THINK the TBO on the BA is 6 years. If that is the case for the boxed prop you are you 2 years from an OH? I don't know when the clock starts. I doubt the boxed prop is warranted anymore. If an OH is due in 2+/- years that makes the price difference even smaller. Baring any info suggesting the boxed prop is a better then the BA I would purchase the new, fully warranted BA. Think of it as second guess insurance. You know, how you may second guess your choice for the remainder of the time you own the -10. I have a non-BA Hartzell on my RV-6A and wish it was a brand spankin' new BA in its place. Robin -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Chuck Weyant Sent: Wednesday, March 12, 2008 8:06 PM Subject: RV10-List: Hartzell blended airfoil performance I've got a chance to purchase a brand new Hartzell constant speed that's been in the box for four years for $4,500. Standard 80" blades. Van's has a new Hartzell prop with blended air foil type blades for $6,300. Anyone out there know if the difference in performance between the two is worth the additional $2,000? Chuck ________________________________________________________________________________
From: GRANSCOTT(at)aol.com
Date: Mar 13, 2008
Subject: Re: Hartzell blended airfoil performance
In a message dated 3/12/2008 11:32:19 PM Central Daylight Time, robin1(at)mrmoisture.com writes: I THINK the TBO on the BA is 6 years. Do you know for sure that this suggested TBO date will apply to your experimental aircraft? **************It's Tax Time! Get tips, forms, and advice on AOL Money & Finance. (http://money.aol.com/tax?NCID=aolprf00030000000001) ________________________________________________________________________________
From: Indran Chelvanayagam <dc71(at)netspace.net.au>
Subject: Re: Door fit
Date: Mar 13, 2008
Now we all come out of hiding... The gap between my first set of doors & the canopy was more than the allowable small animal. Have recently taken delivery of a new set of door shells. The local FG aeroplane guru will be supervising the second set over Easter - has already suggested many changes to the procedure in the Van's manual, such as clecoing the shells all the way around the perimeter; heat gun to remove any bending stress before joining; and totally ignoring the preformed dimples. As a side note, the new pink layups are better surface quality than the old green ones. Will post more info (&pics) when doors done. Indran #228 - soon to be a four door RV10 On 13/03/2008, at 3:55 PM, John Dunne wrote: > Rob, I was very careful as well but in the end you could fit a small > animal between the door and the canopy. > I ended up fibreglassing my doors shut and then creating and molding > the canopy to the door with a gentle transition. > Finally I re-cut the original opening back through. Wasted a lot of > time on this and agonized over it way too much and in the end it was > simple enough to fix. > I also removed the small animal so it didn=92t suffocate because the > doors were now airtight. > John 40315 Cowls. > > From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com > ] On Behalf Of Robert Wright > Sent: Thursday, 13 March 2008 2:11 PM > To: rv10-list(at)matronics.com > Subject: RV10-List: Door fit > > All, > > I've been looking at the way my doors fit to the canopy and am > wondering, "Since I did as good a job as I could, including clamping > everything flush while the epoxy set, then why do I have a slight > bulge on one door in relation to the canopy," and, "should > everything look perfect as a result of trimming, or should I > naturally be expecting to add some filler between the canopy and > doors to make everything smooth and ready for paint?" > > Reading through other websites, they're written up to seem like > masters of the fiberglass trimming, and once trimmed and glued > they're ready for the paint booth after a coat of primer on. > > Thoughts and pointers? > > > Rob Wright > #392 > starting on door hinges > > Be a better friend, newshound, and > > > - The RV10-List Email Forum - > - MATRONICS WEB FORUMS - > --> http://forums.matronics.com > - List Contribution Web Site - > -Matt Dralle, List Admin. > > ________________________________________________________________________________
From: "Doerr, Ray R [NTK]" <Ray.R.Doerr(at)sprint.com>
Date: Mar 13, 2008
Subject: Infinity Grip...am I crazy?
Here is what I have, and I love it. Red Trigger - PTT Hat (Up/Dn) - Elevator Trim Hat (Left/Right) - Ailron Trim Hat (Left/Right) while Blue Pinky switch is pressed for longer than .5 sec onds - Rudder Trim Top Toggle (Center Off) - Flaps Top Green Switch - Audio Panel Com Swap Black (Thumb) - AutoPilot Engage/Disengage Blue (Pinky) - Com Act/Stby Swap if pressed less than .5 second. I also have Transponder Ident wired, but I don't use it, it's j ust an easy to hit the ident on the unit when you change a squak code. Thank You Ray Doerr 40250 N519RV (352 hours on the Hobbs) ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server@m atronics.com] On Behalf Of Chris Sent: Wednesday, March 12, 2008 1:54 PM Subject: RV10-List: Infinity Grip...am I crazy? So I am trying (again) to decide what buttons to put on my grip. If I unde rstand things correctly I can do the following: Trigger - PTT China Hat - Trim Top Right (use toggles w/ center off, mom - on up and down): frequency flip flop from standby on com1 (up) and com 2 (down) via SL30 and 430 Top Left (use toggles w/ center off, mom -on up and down): screen paging o n GRT1 and GRT 2 via GRT Middle (NO 8632 push button) : Autopilot control wheel steering via trutrak Bottom pinky (NO 8632 push button) : swap com1 and com2 via GMA 340 Does this seem like a good setup or is it overkill with stuff I won't use? Also does it appear to all be doable? Thanks Chris Lucas #40072 electrics - cabin top - doors- overhead console - door locks - stick grips - panel - landing gear - engine mount ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: Hartzell blended airfoil performance
Date: Mar 13, 2008
FWIW I had a C177RG from 1976 with a McCauley on it. As a private owner there were no required overhauls. My prop was overhauled with first engine overhaul in 1984. Thereafter it was resealed twice due to a "spitting" of grease during operaton. Total time was about 3500 hours over 28 years when I sold the aircraft and no operational problems . _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of GRANSCOTT(at)aol.com Sent: Thursday, March 13, 2008 5:06 AM Subject: Re: RV10-List: Hartzell blended airfoil performance In a message dated 3/12/2008 11:32:19 PM Central Daylight Time, robin1(at)mrmoisture.com writes: I THINK the TBO on the BA is 6 years. Do you know for sure that this suggested TBO date will apply to your experimental aircraft? _____ It's Tax Time! Get <http://money.aol.com/tax?NCID=aolprf00030000000001> tips, forms and advice on AOL Money & Finance. ________________________________________________________________________________
From: "John Testement" <jwt(at)roadmapscoaching.com>
Subject: Door fit
Date: Mar 13, 2008
Rob, I spent countless hours getting the doors to fit well - and them countless more after the seals were installed. I even had the doors painted first, final installed seals and then filled/sanded the canopy before painting. As my partner is working on a second plane we are thinking of using a square rabbit in the canopy for the door edge to fit into instead of the 45 degree angle. This would avoid the thin door edge. Anyone else done this? John Testement HYPERLINK "mailto:jwt(at)roadmapscoaching.com"jwt(at)roadmapscoaching.com 40321 Richmond, VA Painting // All, I've been looking at the way my doors fit to the canopy and am wondering, "Since I did as good a job as I could, including clamping everything flush while the epoxy set, then why do I have a slight bulge on one door in relation to the canopy," and, "should everything look perfect as a result of trimming, or should I naturally be expecting to add some filler between the canopy and doors to make everything smooth and ready for paint?" Reading through other websites, they're written up to seem like masters of the fiberglass trimming, and once trimmed and glued they're ready for the paint booth after a coat of primer on. Thoughts and pointers? Checked by AVG. 1:27 PM ________________________________________________________________________________
Date: Mar 13, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: Hartzell blended airfoil performance
I'm not going to go too far out on a rant on this, but... "We don't need TSO'd equipment, we're experimental" "We don't need to meet that FAR 23 requirement, we're experimental" "That requirement doesn't apply to us, we're experimental" "We don't need to use Mil Spec parts, we're expermental" Those kind of things really get under my skin. Sure, there is truth and we get some good benefits being experimental, and sure there are lots of good examples of acceptable changes to what is common in certified planes. But, my stomach turns when I hear people go on proclaiming how we can build "better" planes than the certified world, and our planes are faster, more efficient, and "safer" than certified planes. For probably the vast majority of the builders, this simply won't be a true statement....because they decided to cut some corner and didn't hold themselves up to the same maintenance or construction standard as the certified plane was built to. This prop thing in particular?? Well, if I were buying a 4 year old prop that had sat in a box, I'd probably figure in the cost of having it inspected and having the o-rings replaced, unless it had been well sealed and packaged. It's probably going to be just fine and not need any of that. And I'm not even saying it needs an overhaul in 2 years...I'm just reminding everyone that most of the standards that people have to follow in the certified world are there because someone's blood was spilled.....and we can't really claim our planes to be safer or better than certifieds unless we hold ourselves to the same standards. This message doesn't necessarily directly apply to the issue we're discussing....it's more of a general comment. Still stinging a little from the loss of the 2nd RV-10 pilot out of only 125-ish flying. Wonder what the long term record will be, when we compare to the certified world. Tim Olson - RV-10 N104CD - Flying GRANSCOTT(at)aol.com wrote: > In a message dated 3/12/2008 11:32:19 PM Central Daylight Time, > robin1(at)mrmoisture.com writes: > > I THINK the TBO on the BA is 6 years. > > Do you know for sure that this suggested TBO date will apply to your > experimental aircraft? > ________________________________________________________________________________
Date: Mar 13, 2008
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: Hartzell blended airfoil performance
All valid points to ponder. There is a middle ground with props. It is generally referred to as a "inspect and reseal", same as any other inspect and repair as necessary. Cost is normally less than 1/2 price of an overhaul. For a prop that has been stored, it ensures no corrosion, good lube and good seals, and no metal needs removal. An overhaul requires metal removal, which shortens the life of the prop. Kelly Tim Olson wrote: > I'm not going to go too far out on a rant on this, but... > > "That requirement doesn't apply to us, we're experimental" > > For probably the vast majority of the builders, this simply won't be > a true > statement....because they decided to cut some corner and > didn't hold themselves up to the same maintenance or > construction standard as the certified plane was built to. > > This prop thing in particular?? Well, if I were buying a 4 year > old prop that had sat in a box, I'd probably figure in the > cost of having it inspected and having the o-rings replaced, > unless it had been well sealed and packaged. It's probably > going to be just fine and not need any of that. And I'm > not even saying it needs an overhaul in 2 years.... > > Tim Olson - RV-10 N104CD - Flying > ________________________________________________________________________________
Date: Mar 13, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: Hartzell blended airfoil performance
Yeah, I didn't mean to go off too much in relation to the prop. I know that if they're cared for, heck, it should last well in storage and be even better on the blade end than if it were being flown. Seals go bad though. It was more of a general thing....not so much this particular prop issue. I just think we owe it to GA in general to always try to do our best and not give any black eyes to our homebuilt category. Tim Olson - RV-10 N104CD - Flying Kelly McMullen wrote: > > All valid points to ponder. > There is a middle ground with props. It is generally referred to as a > "inspect and reseal", same as any other inspect and repair as necessary. > Cost is normally less than 1/2 price of an overhaul. For a prop that has > been stored, it ensures no corrosion, good lube and good seals, and no > metal needs removal. An overhaul requires metal removal, which shortens > the life of the prop. > Kelly > Tim Olson wrote: >> I'm not going to go too far out on a rant on this, but... >> >> "That requirement doesn't apply to us, we're experimental" >> >> For probably the vast majority of the builders, this simply won't be >> a true >> statement....because they decided to cut some corner and >> didn't hold themselves up to the same maintenance or >> construction standard as the certified plane was built to. >> >> This prop thing in particular?? Well, if I were buying a 4 year >> old prop that had sat in a box, I'd probably figure in the >> cost of having it inspected and having the o-rings replaced, >> unless it had been well sealed and packaged. It's probably >> going to be just fine and not need any of that. And I'm >> not even saying it needs an overhaul in 2 years.... >> >> Tim Olson - RV-10 N104CD - Flying >> ________________________________________________________________________________
From: neil <ncol(at)xtra.co.nz>
Subject: Re: Infinity Grip...am I crazy?
Date: Mar 14, 2008
As an option, we put one of the switches to use as a Trim Disconnect. Press once to disconnect, again to reconnect. That way, once in cruise, trimmed out & autopilot on, there are no worries about someone bumping the trim switch. Neil On 14 Mar 2008, at 1:42, Doerr, Ray R [NTK] wrote: > > ----------- Here is what I have, and I love it. > - > Red Trigger ' PTT > - > Hat -(Up/Dn) ' Elevator Trim > Hat -(Left/Right) ' Ailron Trim > Hat -(Left/Right) while Blue Pinky switch is pressed for longer than > .5 seconds ' Rudder Trim > - > Top Toggle (Center Off) ' Flaps > - > Top Green Switch ' Audio Panel Com Swap > Black (Thumb) ' AutoPilot Engage/Disengage > Blue (Pinky) ' Com Act/Stby Swap if pressed less than .5 second. > - > - > ----------- I also have Transponder Ident wired, but I don=92t use it, > it=92s just an easy to hit the ident on the unit when you change a squak > code. > - > - > > Thank You > Ray Doerr > 40250 N519RV (352 hours on the Hobbs) > > From: owner-rv10-list-server(at)matronics.com > [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Chris > Sent: Wednesday, March 12, 2008 1:54 PM > To: rv10-list(at)matronics.com > Subject: RV10-List: Infinity Grip...am I crazy? > - > So I am trying (again) to decide what buttons to put on my grip.- If I > understand things correctly I can do the following: > - > Trigger - PTT > - > China Hat - Trim > - > Top Right (use toggles w/ center off, mom - on up and down): frequency > flip flop from standby on com1-(up) and com 2 (down) via SL30 and 430 > - > Top Left (use toggles w/ center off, mom -on up and down):--screen > paging on GRT1 and GRT 2 via GRT > - > Middle (NO 8632 push button)-: Autopilot control wheel steering via > trutrak > - > Bottom pinky (NO 8632 push button)- : swap com1-and com2 via GMA 340 > - > Does this seem like a good setup or is it overkill with stuff I won't > use? Also does it appear to all be doable? > - > Thanks > Chris Lucas > #40072 > electrics - cabin top - doors- overhead console - door locks - stick > grips - panel - landing gear - engine mount > - > - > - > http://www.matronics.com/contribution > - > > ________________________________________________________________________________
Subject: Re: Door fit
From: "nick(at)nleonard.com" <nick(at)nleonard.com>
Date: Mar 13, 2008
Fitting the doors...certainly one of my favorite parts of the construction process. After countless hours of trying to get a decent fit just to get them to close (no seals yet), while the whole time my hangar mate (who's building an RV-8A) keeps coming over and saying that they are good enough, just move on. "Go look at a Cirrus and see the quality that they do" was his encouragement to stop "wasting" my time. So I did and it was an eye opener. I was absolutely amazed at not just the size of the gap, especially along the front and top edges, but the inconsistency of the gap. It was embarrassing to think that someone paid almost 1/2 million dollars for that kind of workmanship. So I know that I will have a lot more work to do when I add the seals and it will end up ten time better than the Cirrus. It doesn't have to be a paper thickness sized gap to be functional and attractive. Now, on to putting in the windows...I really am missing squeezing rivets! -------- Nick Leonard RV-10 (40015) Finish Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169583#169583 ________________________________________________________________________________
From: GRANSCOTT(at)aol.com
Date: Mar 13, 2008
Subject: Re: Hartzell blended airfoil performance
Tim, My point being a 91 operation does not need to follow the guideline of commercial operations...we don't do 100 hour inspections, nor are engine or prop TBO a mandatory requirement. I agree it's prudent to do good maintenance and be cautious/careful. You hear folks go on about engine TBO being xxxx hours, when in reality all engine manufacturers also place a time line on the engine for TBO along with hours and which ever occurs first is the TBO for many chapters of operations but not 91. Not buying a prop that's been boxed and if it's been kept in good condition because one believes that a TBO number may apply to an experimental or a part 91 operation does not make sense to me. You can walk down any airport and see props that have not been rebuilt or overhauled in decades and they are perfectly good props eventhough they are beyond TBO...then again some engines will not make it to TBO...ala the Lycoming Crank situation. I'm not meaning to imply that since it's an experimental to throw all good common sense to the wind...but at least look at the part logically for the mission and aircraft and not to put artifical limits in place that do not apply to the plane and operation. Heck go back to the person and explain your thinking, maybe they'll buy in and give you the prop for $3k... P **************It's Tax Time! Get tips, forms, and advice on AOL Money & Finance. (http://money.aol.com/tax?NCID=aolprf00030000000001) ________________________________________________________________________________
Subject: Re: Door fit
From: "jim berry" <jimberry(at)qwest.net>
Date: Mar 13, 2008
John, I did what you are considering, and really like the results. I did not like the fragility of a 45 degree edge on the doors, and found the inconsistent rolled edge on the canopy impossible to trim to. So I squared off the door edges using the double layer of masking tape method to trim the door edges about 1/16 inch inside the canopy edge. When fitting the doors I focused on getting the bottom edge of each door properly aligned with the fuselage skin, as this was an area I did not want to use flox or micro. There were spots where the door side edges stood proud of the canopy edge, but that was OK because I knew that some of the window edges were going to be proud of the canopy also. Once the windows were installed, the canopy surface was built up with a flox/micro mix to match the window and door surface and a new canopy edge was created to match the squared off door edge. The result is a solid door edge and a nice, consistant matching edge for the canopy door opening. Jim Berry 40482 N15JB(reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169622#169622 ________________________________________________________________________________
Subject: Re: Door fit
From: "orchidman" <gary(at)wingscc.com>
Date: Mar 13, 2008
jim berry wrote: > John, > The result is a solid door edge and a nice, consistant matching edge for the canopy door opening. Jim, any chance in seeing some pictures? -------- Gary Blankenbiller RV10 - # 40674 Fuselage SB (N410GB reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169632#169632 ________________________________________________________________________________
Subject: Re: Door fit
From: "jim berry" <jimberry(at)qwest.net>
Date: Mar 13, 2008
Gary, Sorry, I did not take any pics. Jim Berry 40482 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169649#169649 ________________________________________________________________________________
From: John Gonzalez <indigoonlatigo(at)msn.com>
Subject: Andair/FI Fitting
Date: Mar 13, 2008
Does anyone have an Andair valve and has installed the fuel system which Va n's sells. I am trying to figure out why I need to install this special AN fitting in the system. Where does it go and why is it needed? Seems like the exit port on the fuel system setup which is normally plugged back into the standard Van's fuel selector valve could simple be put right into the Andair valve return port. What am I missing? John G ________________________________________________________________________________
From: "gary" <speckter(at)comcast.net>
Subject: 3 view drawing
Date: Mar 13, 2008
Can anyone forward me a 3 view drawing? I tried to get it off of Van's site and I can't seem to make it work. Computer dummy that I am. I need it for the FAA inspection. Gary 40274 ________________________________________________________________________________
From: "Rene Felker" <rene(at)felker.com>
Subject: 3 view drawing
Date: Mar 13, 2008
I used a picture for my DAR inspection....The DAR also took pictures of other documentation...... Rene' Felker N423CF 40322 801-721-6080 -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of gary Sent: Thursday, March 13, 2008 3:00 PM Subject: RV10-List: 3 view drawing Can anyone forward me a 3 view drawing? I tried to get it off of Van's site and I can't seem to make it work. Computer dummy that I am. I need it for the FAA inspection. Gary 40274 ________________________________________________________________________________
Subject: Re: 3 view drawing
From: "jim berry" <jimberry(at)qwest.net>
Date: Mar 13, 2008
Gary, Go to www.myrv10.com/miscphotos/rv-drawings/linedrawing_rv10_3view.pdf. Jim Berry 40482 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169674#169674 ________________________________________________________________________________
Subject: Fuel Injector Servo SB
Date: Mar 14, 2008
From: "McGANN, Ron" <ron.mcgann(at)baesystems.com>
G'day all, There is a service bulletin on the Precision Airmotive series of Fuel Injectors requiring immediate attention. http://www.precisionairmotive.com/Publications/PEX-1.pdf refers. I have not checked the part number of the servo delivered with my new Lyco from Vans, but I'm pretty sure it is one of the affected items. I don't recall seeing any posts on this issue on the list, so I thought I would pass on the details. Apologies in advance if this is not relevant to the fuel injection servos we have on our 540's. Cheers, Ron -187 finishing (was going to install the servo tonight!) "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." ________________________________________________________________________________
Date: Mar 13, 2008
From: Deems Davis <deemsdavis(at)cox.net>
Subject: Re: Andair/FI Fitting
John, it's been a while since I did this, but I used the Andair valve and the standard Van's supplied fuel pump/filter kit. I don't recall a special fitting. (It may have something to do with which Andair valve you have/ordered as they are available with several different fitting configurations) here's a link to the photo album of that portion. http://deemsrv10.com/album/Sec%2037%20Fuel%20System/slides/DSC02794.html there's several additional photos, just follow the controls on the page. Deems Davis # 406 'Its all done....Its just not put together' http://deemsrv10.com/ John Gonzalez wrote: > Does anyone have an Andair valve and has installed the fuel system > which Van's sells. I am trying to figure out why I need to install > this special AN fitting in the system. Where does it go and why is it > needed? > > Seems like the exit port on the fuel system setup which is normally > plugged back into the standard Van's fuel selector valve could simple > be put right into the Andair valve return port. What am I missing? > > John G > > * > > > * ________________________________________________________________________________
Subject: Re: Andair/FI Fitting
From: "jim berry" <jimberry(at)qwest.net>
Date: Mar 13, 2008
If by "special AN fitting" you mean the swivel tee, it will make your line connections much easier. Jim Berry 40482 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169701#169701 ________________________________________________________________________________
From: "Chris" <toaster73(at)embarqmail.com>
Subject: Re: Infinity Grip...am I crazy?
Date: Mar 13, 2008
Well that sounds just as crazy as my possible plan. ;>) And you like it ok? and remember it all ok? So maybe I'll press forward and see what happens - possibly with yet another configuration before I actually order. Thanks to all for the replies on the set ups! -Chris #40072 ----- Original Message ----- From: Doerr, Ray R [NTK] To: rv10-list(at)matronics.com Sent: Thursday, March 13, 2008 8:42 AM Subject: RE: RV10-List: Infinity Grip...am I crazy? Here is what I have, and I love it. Red Trigger - PTT Hat (Up/Dn) - Elevator Trim Hat (Left/Right) - Ailron Trim Hat (Left/Right) while Blue Pinky switch is pressed for longer than .5 seconds - Rudder Trim Top Toggle (Center Off) - Flaps Top Green Switch - Audio Panel Com Swap Black (Thumb) - AutoPilot Engage/Disengage Blue (Pinky) - Com Act/Stby Swap if pressed less than .5 second. I also have Transponder Ident wired, but I don't use it, it's just an easy to hit the ident on the unit when you change a squak code. Thank You Ray Doerr 40250 N519RV (352 hours on the Hobbs) ------------------------------------------------------------------------- ----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Chris Sent: Wednesday, March 12, 2008 1:54 PM To: rv10-list(at)matronics.com Subject: RV10-List: Infinity Grip...am I crazy? So I am trying (again) to decide what buttons to put on my grip. If I understand things correctly I can do the following: Trigger - PTT China Hat - Trim Top Right (use toggles w/ center off, mom - on up and down): frequency flip flop from standby on com1 (up) and com 2 (down) via SL30 and 430 Top Left (use toggles w/ center off, mom -on up and down): screen paging on GRT1 and GRT 2 via GRT Middle (NO 8632 push button) : Autopilot control wheel steering via trutrak Bottom pinky (NO 8632 push button) : swap com1 and com2 via GMA 340 Does this seem like a good setup or is it overkill with stuff I won't use? Also does it appear to all be doable? Thanks Chris Lucas #40072 electrics - cabin top - doors- overhead console - door locks - stick grips - panel - landing gear - engine mount http://www.matronics.com/contribution ________________________________________________________________________________
From: "Chris" <toaster73(at)embarqmail.com>
Subject: Re: Door fit
Date: Mar 13, 2008
Robert, Someone wrote before that "the fit is right when you are tired of sanding and re-filling and sanding" perhaps that was Deems. I made a couple of mods to the process for initial fit. 1) I glued (with super glue) two strips of trimmed door glass to the outside of the door, fore and aft where the two protruding alignment tabs are. I match drilled through the tabs into the glued on piece. THen I cut the tabs off. That allowed the door to begin its journey into flush fit with the canopy. As I took the door on and off it would go pretty much right back to where it was every time. See photo. 2) After I got the fit pretty darn good I mixed a thick epoxy/flox and spread it over the door and cabin top at the joint until I had a nice surface together. I did this just in a couple of areas that were troublesome. This mixture would not flow at all and this was with hinges on but no door seal. I then lifted the door open slightly so it wouldn't all glue together. Yes, it did pull a little ridge of the mix up but not much if done careful. After it dried I just knocked of the ridge with the sanding block and I have a razor like fit. This is with a 45 degree style door. I also coated the 45 degree portion of the door with pure epoxy to give it durability. I'll revisit the fit with the door seals on, those just arrived . I am trying the ones from Aviation Tech Products. The alignment tabs supe glued on are easy to pop right off and then sand away the residue. Don't need much glue either just a couple drops. -Chris #40072 ----- Original Message ----- From: Robert Wright To: rv10-list(at)matronics.com Sent: Thursday, March 13, 2008 12:10 AM Subject: RV10-List: Door fit All, I've been looking at the way my doors fit to the canopy and am wondering, "Since I did as good a job as I could, including clamping everything flush while the epoxy set, then why do I have a slight bulge on one door in relation to the canopy," and, "should everything look perfect as a result of trimming, or should I naturally be expecting to add some filler between the canopy and doors to make everything smooth and ready for paint?" Reading through other websites, they're written up to seem like masters of the fiberglass trimming, and once trimmed and glued they're ready for the paint booth after a coat of primer on. Thoughts and pointers? Rob Wright #392 starting on door hinges ------------------------------------------------------------------------- ----- Be a better friend, newshound, and ________________________________________________________________________________
Subject: Fuel Injector Servo SB
Date: Mar 14, 2008
From: "McGANN, Ron" <ron.mcgann(at)baesystems.com>
Checked my injector servo at lunch time (straight out of the box, not yet installed). Although the plug was lockwired it was clearly loose. Since the only heat my engine has been exposed to is the test run conducted at the factory, shrinkage of the seal with heat is not the only problem here. I doubt the plug was properly torqued at the factory before delivery. check those servos!! cheers, Ron ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 8:55 AM To: rv10-list(at)matronics.com Subject: RV10-List: Fuel Injector Servo SB G'day all, There is a service bulletin on the Precision Airmotive series of Fuel Injectors requiring immediate attention. http://www.precisionairmotive.com/Publications/PEX-1.pdf <http://www.precisionairmotive.com/Publications/PEX-1.pdf> refers. I have not checked the part number of the servo delivered with my new Lyco from Vans, but I'm pretty sure it is one of the affected items. I don't recall seeing any posts on this issue on the list, so I thought I would pass on the details. Apologies in advance if this is not relevant to the fuel injection servos we have on our 540's. Cheers, Ron -187 finishing (was going to install the servo tonight!) "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." ________________________________________________________________________________
From: "John Dunne" <acs(at)acspropeller.com.au>
Subject: Fuel Injector Servo SB
Date: Mar 14, 2008
This is the FAA AD Ron is referring to in case some of you don't have the info through the mail yet.. I could say something with regards experimental and some earlier comments but I'll resist :-) John 40315. _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 2:17 PM Subject: RE: RV10-List: Fuel Injector Servo SB Checked my injector servo at lunch time (straight out of the box, not yet installed). Although the plug was lockwired it was clearly loose. Since the only heat my engine has been exposed to is the test run conducted at the factory, shrinkage of the seal with heat is not the only problem here. I doubt the plug was properly torqued at the factory before delivery. check those servos!! cheers, Ron _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 8:55 AM Subject: RV10-List: Fuel Injector Servo SB G'day all, There is a service bulletin on the Precision Airmotive series of Fuel Injectors requiring immediate attention. <http://www.precisionairmotive.com/Publications/PEX-1.pdf> http://www.precisionairmotive.com/Publications/PEX-1.pdf refers. I have not checked the part number of the servo delivered with my new Lyco from Vans, but I'm pretty sure it is one of the affected items. I don't recall seeing any posts on this issue on the list, so I thought I would pass on the details. Apologies in advance if this is not relevant to the fuel injection servos we have on our 540's. Cheers, Ron -187 finishing (was going to install the servo tonight!) "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." p://www.matronics.com/Navigator?RV10-List ics.com .matronics.com/contribution "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." ________________________________________________________________________________
From: "John Dunne" <acs(at)acspropeller.com.au>
Subject: Door fit
Date: Mar 14, 2008
Hi Indran, good to see you're still plugging away. I suppose I should clarify what I meant by "small animal" in case someone gets the idea it's O.K to have a gap the size of a beaver. My gap was more like 4 to 5mm at the worst spot. For what it's worth, the fit was good prior to the window installation. John 40315 _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Indran Chelvanayagam Sent: Thursday, 13 March 2008 10:44 PM Subject: Re: RV10-List: Door fit Now we all come out of hiding... The gap between my first set of doors & the canopy was more than the allowable small animal. Have recently taken delivery of a new set of door shells. The local FG aeroplane guru will be supervising the second set over Easter - has already suggested many changes to the procedure in the Van's manual, such as clecoing the shells all the way around the perimeter; heat gun to remove any bending stress before joining; and totally ignoring the preformed dimples. As a side note, the new pink layups are better surface quality than the old green ones. Will post more info (&pics) when doors done. Indran #228 - soon to be a four door RV10 On 13/03/2008, at 3:55 PM, John Dunne wrote: Rob, I was very careful as well but in the end you could fit a small animal between the door and the canopy. I ended up fibreglassing my doors shut and then creating and molding the canopy to the door with a gentle transition. Finally I re-cut the original opening back through. Wasted a lot of time on this and agonized over it way too much and in the end it was simple enough to fix. I also removed the small animal so it didn't suffocate because the doors were now airtight. John 40315 Cowls. _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Robert Wright Sent: Thursday, 13 March 2008 2:11 PM Subject: RV10-List: Door fit All, I've been looking at the way my doors fit to the canopy and am wondering, "Since I did as good a job as I could, including clamping everything flush while the epoxy set, then why do I have a slight bulge on one door in relation to the canopy," and, "should everything look perfect as a result of trimming, or should I naturally be expecting to add some filler between the canopy and doors to make everything smooth and ready for paint?" Reading through other websites, they're written up to seem like masters of the fiberglass trimming, and once trimmed and glued they're ready for the paint booth after a coat of primer on. Thoughts and pointers? Rob Wright #392 starting on door hinges _____ Be a better friend, newshound, and - The RV10-List Email Forum - ________________________________________________________________________________
From: Richard Reynolds <rvreynolds(at)macs.net>
Subject: Re: Door fit
Date: Mar 14, 2008
John, We put a 1/8 square rabbit in the canopy door frame. it made the door very easy to fit. Make it deep enough for the thickest part of the door. Be careful when trimming the canopy frame in way of the aluminum fuselage frame. Please note! After trimming the door to the factory scribe lines, take equal amounts off the forward and aft edges. The temptation is after getting one edge to fit, removing the remainder from the other edge. DON'T, because it makes the inside "jam" unequal. (Ask me how I know) Also, the top of the canopy door frame really does not need the rabbit, The top edge of the door WILL require a bevel to open properly! Richard Reynolds On Mar 13, 2008, at 8:54 AM, John Testement wrote: > Rob, > > I spent countless hours getting the doors to fit well - and them > countless more after the seals were installed. I even had the doors > painted first, final installed seals and then filled/sanded the > canopy before painting. As my partner is working on a second plane > we are thinking of using a square rabbit in the canopy for the door > edge to fit into instead of the 45 degree angle. This would avoid > the thin door edge. Anyone else done this? > > John Testement > jwt(at)roadmapscoaching.com > 40321 > Richmond, VA > Painting > > > // All, > > I've been looking at the way my doors fit to the canopy and am > wondering, "Since I did as good a job as I could, including > clamping everything flush while the epoxy set, then why do I have a > slight bulge on one door in relation to the canopy," and, "should > everything look perfect as a result of trimming, or should I > naturally be expecting to add some filler between the canopy and > doors to make everything smooth and ready for paint?" > > Reading through other websites, they're written up to seem like > masters of the fiberglass trimming, and once trimmed and glued > they're ready for the paint booth after a coat of primer on. > > Thoughts and pointers? > > > Checked by AVG. > 3/12/2008 1:27 PM > > ________________________________________________________________________________
Subject: Fuel Injector Servo SB/Emergency AD
Date: Mar 14, 2008
From: "Rhonda Bewley" <Rhonda(at)bpaengines.com>
You should also be aware that the Precision SB and Emergency AD apply not only to new certified RSA5 and RSA10 servos and the experimental Precision Silverhawk systems but also apply to any systems overhauled or repaired by in the field since August 1, 2006. So, even if you purchased an overhauled engine from a shop like mine, Lycon or countless others and it has a Bendix/Precision system on it, you need to comply with this AD for your own safety. Rhonda Barrett-Bewley Barrett Precision Engines, Inc. 2870-B N. Sheridan Rd. Tulsa, OK 74115 (918) 835-1089 phone (918) 835-1754 fax www.barrettprecisionengines.com <http://www.barrettprecisionengines.com/> ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Dunne Sent: Friday, March 14, 2008 1:07 AM Subject: RE: RV10-List: Fuel Injector Servo SB This is the FAA AD Ron is referring to in case some of you don't have the info through the mail yet.. I could say something with regards experimental and some earlier comments but I'll resist :-) John 40315. ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 2:17 PM Subject: RE: RV10-List: Fuel Injector Servo SB Checked my injector servo at lunch time (straight out of the box, not yet installed). Although the plug was lockwired it was clearly loose. Since the only heat my engine has been exposed to is the test run conducted at the factory, shrinkage of the seal with heat is not the only problem here. I doubt the plug was properly torqued at the factory before delivery. check those servos!! cheers, Ron ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 8:55 AM To: rv10-list(at)matronics.com Subject: RV10-List: Fuel Injector Servo SB G'day all, There is a service bulletin on the Precision Airmotive series of Fuel Injectors requiring immediate attention. http://www.precisionairmotive.com/Publications/PEX-1.pdf <http://www.precisionairmotive.com/Publications/PEX-1.pdf> refers. I have not checked the part number of the servo delivered with my new Lyco from Vans, but I'm pretty sure it is one of the affected items. I don't recall seeing any posts on this issue on the list, so I thought I would pass on the details. Apologies in advance if this is not relevant to the fuel injection servos we have on our 540's. Cheers, Ron -187 finishing (was going to install the servo tonight!) "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." p://www.matronics.com/Navigator?RV10-List ics.com .matronics.com/contribution "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." - The RV10-List Email Forum - Thank you for your generous support! --> http://www.matronics.com/contribution ________________________________________________________________________________
From: Rob Kermanj <flysrv10(at)gmail.com>
Subject: flight planning
Date: Mar 14, 2008
A great flight planning web site that I think you will appreciate. http://www.navmonster.com/ Rob Kermanj ________________________________________________________________________________
Date: Mar 14, 2008
From: Dave Lammers <davelammers(at)mchsi.com>
Subject: Re: Door fit
John, Did you do the window install with the door on, or off, the fuselage? If off, do you think that the post install fit issue could have been reduced if the install were made with the door on the fuselage? Thanks, Dave Lammers finishing John Dunne wrote: > Hi Indran, good to see you're still plugging away. > > I suppose I should clarify what I meant by "small animal" in case > someone gets the idea it's O.K to have a gap the size of a beaver. > > My gap was more like 4 to 5mm at the worst spot. > > For what it's worth, the fit was good prior to the window installation. > > John 40315 > > ________________________________________________________________________________
From: John Gonzalez <indigoonlatigo(at)msn.com>
Subject: Re: Andair/FI Fitting
Date: Mar 14, 2008
JIm, I do mean the Tee swivel. So if it makes connection easier, where does it m ake connection easier? WHere does it go? JOhn> Subject: RV10-List: Re: Andair/FI Fitting> From: jimberry(at)qwest.net> Date: Thu, 13 Mar 2008 16:36:58 -0700> To: rv10-list(at)matronics.com> > --> R V10-List message posted by: "jim berry" > > If by "spec ial AN fitting" you mean the swivel tee, it will make your line connections much easier.> > Jim Berry> 40482> > > > > Read this topic online here:> > http://forums.matronics.com/viewtopic.php?p=169701#169701> > > > > > > > ========================> > > ________________________________________________________________________________
From: "Doerr, Ray R [NTK]" <Ray.R.Doerr(at)sprint.com>
Date: Mar 14, 2008
Subject: Fuel Injector Servo SB/Emergency AD
As I understand it, if you had your before the August 1, 2006 date, it did not apply. Is this correct? Thank You Ray Doerr CDNI Principal Engineer Sprint PCS 16020 West 113th Street Lenexa, KS 66219 Mailstop KSLNXK0101 (913) 859-1414 (Office) (913) 226-0106 (Pcs) (913) 859-1234 (Fax) Ray.R.Doerr(at)sprint.com ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server@m atronics.com] On Behalf Of Rhonda Bewley Sent: Friday, March 14, 2008 8:04 AM Subject: RE: RV10-List: Fuel Injector Servo SB/Emergency AD You should also be aware that the Precision SB and Emergency AD apply not o nly to new certified RSA5 and RSA10 servos and the experimental Precision S ilverhawk systems but also apply to any systems overhauled or repaired by i n the field since August 1, 2006. So, even if you purchased an overhauled engine from a shop like mine, Lycon or countless others and it has a Bendix /Precision system on it, you need to comply with this AD for your own safet y. Rhonda Barrett-Bewley Barrett Precision Engines, Inc. 2870-B N. Sheridan Rd. Tulsa, OK 74115 (918) 835-1089 phone (918) 835-1754 fax www.barrettprecisionengines.com<http://www.barrettprecisionengines.com/> ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server@m atronics.com] On Behalf Of John Dunne Sent: Friday, March 14, 2008 1:07 AM Subject: RE: RV10-List: Fuel Injector Servo SB This is the FAA AD Ron is referring to in case some of you don't have the i nfo through the mail yet.. I could say something with regards experimental and some earlier comments b ut I'll resist :) John 40315. ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server@m atronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 2:17 PM Subject: RE: RV10-List: Fuel Injector Servo SB Checked my injector servo at lunch time (straight out of the box, not yet i nstalled). Although the plug was lockwired it was clearly loose. Since th e only heat my engine has been exposed to is the test run conducted at the factory, shrinkage of the seal with heat is not the only problem here. I d oubt the plug was properly torqued at the factory before delivery. check those servos!! cheers, Ron ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server@m atronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 8:55 AM Subject: RV10-List: Fuel Injector Servo SB G'day all, There is a service bulletin on the Precision Airmotive series of Fuel Injec tors requiring immediate attention. http://www.precisionairmotive.com/Publ ications/PEX-1.pdf refers. I have not checked the part number of the servo delivered with my new Lyco from Vans, but I'm pretty sure it is one of the affected items. I don't recall seeing any posts on this issue on the list, so I thought I w ould pass on the details. Apologies in advance if this is not relevant to the fuel injection servos we have on our 540's. Cheers, Ron -187 finishing (was going to install the servo tonight!) "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." p://www.matronics.com/Navigator?RV10-List ics.com .matronics.com/contribution "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." - The RV10-List Email Forum - Thank you for your generous support! --> http://www.matronics.com/contribution ________________________________________________________________________________
Subject: Fuel Injector Servo SB/Emergency AD
Date: Mar 14, 2008
From: "Rhonda Bewley" <Rhonda(at)bpaengines.com>
That's how I read it. Rhonda ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Doerr, Ray R [NTK] Sent: Friday, March 14, 2008 10:24 AM Subject: RE: RV10-List: Fuel Injector Servo SB/Emergency AD As I understand it, if you had your before the August 1, 2006 date, it did not apply. Is this correct? Thank You Ray Doerr CDNI Principal Engineer Sprint PCS 16020 West 113th Street Lenexa, KS 66219 Mailstop KSLNXK0101 (913) 859-1414 (Office) (913) 226-0106 (Pcs) (913) 859-1234 (Fax) Ray.R.Doerr(at)sprint.com ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Rhonda Bewley Sent: Friday, March 14, 2008 8:04 AM Subject: RE: RV10-List: Fuel Injector Servo SB/Emergency AD You should also be aware that the Precision SB and Emergency AD apply not only to new certified RSA5 and RSA10 servos and the experimental Precision Silverhawk systems but also apply to any systems overhauled or repaired by in the field since August 1, 2006. So, even if you purchased an overhauled engine from a shop like mine, Lycon or countless others and it has a Bendix/Precision system on it, you need to comply with this AD for your own safety. Rhonda Barrett-Bewley Barrett Precision Engines, Inc. 2870-B N. Sheridan Rd. Tulsa, OK 74115 (918) 835-1089 phone (918) 835-1754 fax www.barrettprecisionengines.com <http://www.barrettprecisionengines.com/> ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of John Dunne Sent: Friday, March 14, 2008 1:07 AM Subject: RE: RV10-List: Fuel Injector Servo SB This is the FAA AD Ron is referring to in case some of you don't have the info through the mail yet.. I could say something with regards experimental and some earlier comments but I'll resist :-) John 40315. ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 2:17 PM Subject: RE: RV10-List: Fuel Injector Servo SB Checked my injector servo at lunch time (straight out of the box, not yet installed). Although the plug was lockwired it was clearly loose. Since the only heat my engine has been exposed to is the test run conducted at the factory, shrinkage of the seal with heat is not the only problem here. I doubt the plug was properly torqued at the factory before delivery. check those servos!! cheers, Ron ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of McGANN, Ron Sent: Friday, 14 March 2008 8:55 AM To: rv10-list(at)matronics.com Subject: RV10-List: Fuel Injector Servo SB G'day all, There is a service bulletin on the Precision Airmotive series of Fuel Injectors requiring immediate attention. http://www.precisionairmotive.com/Publications/PEX-1.pdf <http://www.precisionairmotive.com/Publications/PEX-1.pdf> refers. I have not checked the part number of the servo delivered with my new Lyco from Vans, but I'm pretty sure it is one of the affected items. I don't recall seeing any posts on this issue on the list, so I thought I would pass on the details. Apologies in advance if this is not relevant to the fuel injection servos we have on our 540's. Cheers, Ron -187 finishing (was going to install the servo tonight!) "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." p://www.matronics.com/Navigator?RV10-List ics.com .matronics.com/contribution "Warning: The information contained in this email and any attached files is confidential to BAE Systems Australia. If you are not the intended recipient, any use, disclosure or copying of this email or any attachments is expressly prohibited. If you have received this email in error, please notify us immediately. VIRUS: Every care has been taken to ensure this email and its attachments are virus free, however, any loss or damage incurred in using this email is not the sender's responsibility. It is your responsibility to ensure virus checks are completed before installing any data sent in this email to your computer." - The RV10-List Email Forum - Thank you for your generous support! --> http://www.matronics.com/contribution http://www.matronics.com/contribution ________________________________________________________________________________
Subject: Re: Andair/FI Fitting
From: "jim berry" <jimberry(at)qwest.net>
Date: Mar 14, 2008
John, I believe most people are using the Andair valve with the built in 90 degree ports, because it makes plumbing the fuel lines easier. I used the swivel tee on the center(or outflow) port because there is not enough room for a standard tee to clear the other 2 ports during installation. If you spend some time trying to get all 3 lines installed to the Andair in the confined space of the tunnel I think you will find the extra cost of the swivel tee to be worth it. Jim Berry 40482 N15JB(reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169822#169822 ________________________________________________________________________________
Subject: Re: Door fit
From: "jim berry" <jimberry(at)qwest.net>
Date: Mar 14, 2008
I will be interested to hear how Richard created a 1/8 inch rabbet, but in the mean time I can suggest an alternative. If you trim the door edge square so that it sits slightly inside the curved portion of the canopy edge, the door edge can serve as a mold for creating the rabbet. The inner edge of the door should be just tangent to the radius of the canopy edge. Once you have the windows installed, apply 2 layers of release tape(packing tape) to the edge of the doors. You should have all door locking hardware installed and adjusted to final fit. Close the doors and lock them in place. Trowel on a mix of flox/micro to the canopy top so it fills the gap between the door edge and the canopy. After it cures, open the doors and remove the packing tape. You will be left with a rabbet that exactly matches your door edge, and should require very little clean up. Also, I would suggest installing the door windows with the doors mounted on the canopy. Jim Berry 40482 N15JB(reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=169828#169828 ________________________________________________________________________________
Date: Mar 14, 2008
From: Rick Sked <ricksked(at)embarqmail.com>
Subject: Re: Door fit
The gap the size of a BEAVER???=C2-=C2- :).......maybe you should have said Polecat.. ----- Original Message ----- From: "John Dunne" <acs(at)acspropeller.com.au> Sent: Thursday, March 13, 2008 11:37:46 PM (GMT-0800) America/Los_Angeles Subject: RE: RV10-List: Door fit Hi Indran, good to see you=99re still plugging away. I suppose I should clarify what I meant by =9Csmall animal=9D i n case someone gets the idea it=99s O.K to have a gap the size of a b eaver. My gap was more like 4 to 5mm at the worst spot. For what it=99s worth, the fit was good prior to the window installat ion. John 40315 From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server@m atronics.com] On Behalf Of Indran Chelvanayagam Sent: Thursday, 13 March 2008 10:44 PM Subject: Re: RV10-List: Door fit Now we all come out of hiding... The gap between my first set of doors & the canopy was more than the allowa ble small animal. Have recently taken delivery of a new set of door shells. The local FG aero plane guru will be supervising the second set over Easter - has already sug gested many changes to the procedure in the Van's manual, such as clecoing the shells all the way around the perimeter; heat gun to remove any bending stress before joining; and totally ignoring the preformed dimples. As a side note, the new pink layups are better surface quality than the old green ones.=C2- Will post more info (&pics) when doors done. Indran #228 - soon to be a four door RV10 On 13/03/2008, at 3:55 PM, John Dunne wrote: Rob, I was very careful as well but in the end you could fit a small animal between the door and the canopy. I ended up fibreglassing my doors shut and then creating and molding the ca nopy to the door with a gentle transition. Finally I re-cut the original opening back through. Wasted a lot of time on this and agonized over it way too much and in the end it was simple enough to fix. I also removed the small animal so it didn=99t suffocate because the doors were now airtight. John 40315 Cowls. From: =C2- owner-rv10-list-server(at)matronics.com =C2- [mailto: owner-rv1 0-list-server(at)matronics.com ] =C2- On Behalf Of =C2- Robert Wright Sent: =C2- Thursday, 13 March 2008 2:11 PM Subject: =C2- RV10-List: Door fit All, I've been looking at the way my doors fit to the canopy and am wondering, " Since I did as good a job as I could, including clamping everything flush w hile the epoxy set, then why do I have a slight bulge on one door in relati on to the canopy," and, "should everything look perfect as a result of trim ming, or should I naturally be expecting to add=C2-some filler between th e canopy and doors to make everything smooth and ready for paint?" Reading through other websites, they're written up to seem like masters of the fiberglass trimming, and once=C2-trimmed and glued=C2-they're ready for the paint booth=C2-after=C2-a coat of primer on. Thoughts and pointers? Rob Wright #392 starting on door hinges Be a better friend, newshound, and =C2- =C2- =C2-=C2-=C2-=C2- ===== ==== ======================= == ________________________________________________________________________________
Date: Mar 14, 2008
Subject: flight planning
From: "William Curtis" <wcurtis(at)nerv10.com>
Not sure how they can call themselves a GA planning site when you can't overlay your route on an actual aviation map (sectional, TAC, etc). Did I miss how to do this? The only options for the route maps are Street Map, Satellite, Hybrid and Terrain. I much prefer http://skyvector.com/ It will overlay your planned route on the actual current Sectional, TAC or IFR charts. William http://wcurtis.nerv10.com/ "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." -- Dr. Suess -------- Original Message -------- > > A great flight planning web site that I think you will appreciate. > > http://www.navmonster.com/ > > > Rob Kermanj ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: flight planning
Date: Mar 14, 2008
There is a free flight planning program (less the more detailed functions) from wwww.seattleavionics.com called voyager -----Original Message----- From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of William Curtis Sent: Friday, March 14, 2008 10:19 AM Subject: re: RV10-List: flight planning Not sure how they can call themselves a GA planning site when you can't overlay your route on an actual aviation map (sectional, TAC, etc). Did I miss how to do this? The only options for the route maps are Street Map, Satellite, Hybrid and Terrain. I much prefer http://skyvector.com/ It will overlay your planned route on the actual current Sectional, TAC or IFR charts. William http://wcurtis.nerv10.com/ "Be who you are and say what you feel because those who mind don't matter and those who matter don't mind." -- Dr. Suess -------- Original Message -------- > > A great flight planning web site that I think you will appreciate. > > http://www.navmonster.com/ > > > Rob Kermanj ________________________________________________________________________________
From: kilopapa(at)antelecom.net
Subject: Re: Door fit
Date: Mar 14, 2008
General door fitting questions: Are you installing the door seals prior to painting? If so, why? Is it necessary to have the seal installed during the door fitting process? If so, why? Thanks, Kevin 40494 ________________________________________________________________________________
From: kilopapa(at)antelecom.net
Subject: Re: Door fit
Date: Mar 14, 2008
Chris, Is the seal from ATP hollow? Will you be mounting it temporarily at this fitting check, assuming pre-paint? Is the choice of door seal necessary to know at the time of door fitting? Thanks, Kevin 40494 ------------------------------------------------------------------------------------------ ----- Original Message Follows ----- From: "Chris" <toaster73(at)embarqmail.com> Subject: Re: RV10-List: Door fit Date: Thu, 13 Mar 2008 22:01:35 -0400 .....and this was with hinges on but no door seal. .....I'll revisit the fit with the door seals on, those just arrived . I am trying the ones from Aviation Tech Products. -Chris >#40072 ________________________________________________________________________________
From: "John Dunne" <acs(at)acspropeller.com.au>
Subject: Re: Door fit
Date: Mar 15, 2008
Dave, I did the window install on the fuse. It was a very hot day if I recall (36C around 100F) and the weld-on went off very quickly...too quickly for my liking but my figuring on a hot day was the plexi was more pliable and less likely to suffer any cracks. I must admit, I came back a few days later and removed the doors and it wasn't until I re-installed them some weeks later that I actually noticed the problem. It had me a little perplexed as I'd think it unlikely the bowing would have been caused by the window install and curing process. My initial thoughts were that I didn't have the doors back in their exact position when re-installed but in the end I figured a few people were suffering a similar result albeit no-one was really openly discussing it and the finer finish work was my responsibility in any case. Like I previously stated I wasted far to much time on this and it only annoyed me because all the metal work up until that point was precise and a pleasure to work on. Once I got over the "take it from the box and fit it" mentality I started to enjoy the flexibility of the glass work and the ease with which you can fix mistakes. John 40315 ----- Original Message ----- From: Dave Lammers To: rv10-list(at)matronics.com Sent: Friday, March 14, 2008 11:38 PM Subject: Re: RV10-List: Door fit John, Did you do the window install with the door on, or off, the fuselage? If off, do you think that the post install fit issue could have been reduced if the install were made with the door on the fuselage? Thanks, Dave Lammers finishing John Dunne wrote: Hi Indran, good to see you're still plugging away. I suppose I should clarify what I meant by "small animal" in case someone gets the idea it's O.K to have a gap the size of a beaver. My gap was more like 4 to 5mm at the worst spot. For what it's worth, the fit was good prior to the window installation. John 40315 ________________________________________________________________________________
From: "Chuck Weyant" <chuck(at)chuckdirect.com>
Subject: Re: Door fit
Date: Mar 13, 2008
For what it's worth I think the door build is the worst part of buuilding this airplane. I've spent hours and stinking hours fitting, filling, cutting, on and on. Finally I get an acceptable fit, on go the seals, and nothing fits, or closes. Rip out the seals everything is fine. Don't know what I'm going to do at this point. Chuck ----- Original Message ----- From: "Deems Davis" <deemsdavis(at)cox.net> Sent: Wednesday, March 12, 2008 10:10 PM Subject: Re: RV10-List: Door fit > > Rob, My experience was certainly Not ' cut/glue/hang/ it was more like... > cut/glue/hang/fill/sand/hang/fill/sand/hang/fill/sand.......... you get > the picture. > http://deemsrv10.com/cabinwindowslogindex.html > > I'm NO master of fiberglass / epoxy, the good news is you really don't > have to be, other than it being messy and sticky, there's not too much you > can do w/ fiberglass that can't be corrected if you goof up. In the end > (I haven't installed door seals yet ....?) I'm happy with the fit of the > doors to the cabin cover. But it took a LOT of additional work. A lot of > it depends on you own taste and preferences, Van's fiberglass parts are > not made with the same precision as the CNC metal parts. I'm sure that > they all possess the required strength to do their respective functions. > The additional work is really a mater of cosmetics and your personal > preferences. > > > Deems Davis # 406 > 'Its all done....Its just not put together' > http://deemsrv10.com/ > > Robert Wright wrote: >> All, >> I've been looking at the way my doors fit to the canopy and am >> wondering, "Since I did as good a job as I could, including clamping >> everything flush while the epoxy set, then why do I have a slight bulge >> on one door in relation to the canopy," and, "should everything look >> perfect as a result of trimming, or should I naturally be expecting to >> add some filler between the canopy and doors to make everything smooth >> and ready for paint?" >> Reading through other websites, they're written up to seem like masters >> of the fiberglass trimming, and once trimmed and glued they're ready for >> the paint booth after a coat of primer on. >> Thoughts and pointers? >> * >> >> * > > > ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: window cleaning
Date: Mar 14, 2008
What cleaners and cloths are being used to clean the windows. Its about time to remove the protective coverings. ________________________________________________________________________________
From: "Chris" <toaster73(at)embarqmail.com>
Subject: Re: Door fit
Date: Mar 14, 2008
No its not hollow it is a neoprene of sorts made for pipers, so its more like a square cross section. Not unlike the home depot stuff...but better. I have not opened it yet, looks like there is some special adhesive with it too. I plan to use some carpet tape for a temporary type install to see how it will interfere with what I call the "preliminary" door fit I have achieved. Going into this I couldn't believe the seal wouldn't possibly change my fit so I am mentally prepared for more work once the seal is on. I think its a good idea to try a temporary fit of the seal because I think the trim of the cabin top and its variation will affect the seal and its compression or lack of compression etc. -Chris #40072 ----- Original Message ----- From: <kilopapa(at)antelecom.net> Sent: Friday, March 14, 2008 3:03 PM Subject: Re: RV10-List: Door fit > > Chris, > > Is the seal from ATP hollow? Will you be mounting it > temporarily at this fitting check, assuming pre-paint? Is > the choice of door seal necessary to know at the time of > door fitting? > > Thanks, > > Kevin > 40494 > ------------------------------------------------------------------------------------------ > > ----- Original Message Follows ----- > From: "Chris" <toaster73(at)embarqmail.com> > To: > Subject: Re: RV10-List: Door fit > Date: Thu, 13 Mar 2008 22:01:35 -0400 > > .....and this was with hinges on but no door seal. > > .....I'll revisit the fit with the door seals on, those just > arrived . I am trying the ones from Aviation Tech Products. > > -Chris >>#40072 > > > ________________________________________________________________________________
From: Rob Kermanj <flysrv10(at)gmail.com>
Subject: Re: window cleaning
Date: Mar 15, 2008
Use Lemon Pledge and terry cloth sold by Sam or any towel. Works great. Rob. On Mar 14, 2008, at 8:46 PM, David McNeill wrote: > What cleaners and cloths are being used to clean the windows. Its > about time to remove the protective coverings. > > ________________________________________________________________________________
Date: Mar 15, 2008
From: Tim Olson <Tim(at)MyRV10.com>
Subject: Re: window cleaning
While I never had problems with Pledge (pump ONLY NOT AEROSOL) on my last plane, I've now switched exclusively to Plexus for my RV-10... the windshield being so utterly painful to replace I figured it was worth a couple bucks more for the care. Try skygeek.com for pricing. I've also been exclusively using microfiber towels for the past 5 or 6 years...they're perfect for the job. Tim Olson - RV-10 N104CD - Flying Rob Kermanj wrote: > Use Lemon Pledge and terry cloth sold by Sam or any towel. Works great. > > Rob. > > On Mar 14, 2008, at 8:46 PM, David McNeill wrote: > >> What cleaners and cloths are being used to clean the windows. Its >> about time to remove the protective coverings. >> * >> >> * > ________________________________________________________________________________
Date: Mar 15, 2008
From: PJ Seipel <seipel(at)seznam.cz>
Subject: Re: window cleaning
You can get Plexus locally at any Honda or Harley Davidson motorcycle shop. Their pricing is fairly competitive with the online shops once you factor in shipping. PJ Seipel RV-10 #40032 Tim Olson wrote: > > While I never had problems with Pledge (pump ONLY NOT AEROSOL) on my > last plane, I've now switched exclusively to Plexus for my RV-10... > the windshield being so utterly painful to replace I figured it was > worth a couple bucks more for the care. Try skygeek.com for pricing. > I've also been exclusively using microfiber towels for the past 5 or 6 > years...they're perfect for the job. > > Tim Olson - RV-10 N104CD - Flying > > > Rob Kermanj wrote: >> Use Lemon Pledge and terry cloth sold by Sam or any towel. Works great. >> >> Rob. >> >> On Mar 14, 2008, at 8:46 PM, David McNeill wrote: >> >>> What cleaners and cloths are being used to clean the windows. Its >>> about time to remove the protective coverings. >>> * >>> >>> * >> > > ________________________________________________________________________________
Date: Mar 15, 2008
From: "Chase Snodgrass" <airplanedriver(at)gmail.com>
Subject: VS1016
Almost ready to rivet vertical stabilizer, and have a part leftover. LOL. Where does VS1016 fit???? Chase Snodgrass Presidio, TX http://flybigbend.com ________________________________________________________________________________
Date: Mar 15, 2008
From: Les Kearney <kearney(at)shaw.ca>
Subject: There was an old woman ....
Hi One of the things I have learned in building my -10 (some assembly still required), is there is a huge amount that I don't know. For example, as I was building my tail cone I ended up leaving some dents and dings in the cone that make me winch every time I look at it. Anyway, as I am coming close to where I have to attach the cone to the fuse (a step I have been avoiding for logistical reasons), I keep looking at the cone wondering what I should do about my less than perfect work. Last Monday, I rented a small van and took my cone out to my paint shop to get an opinion. He took one look at the "minor imperfections" and said they were nothing. To demonstrate he mixed up some aluminium filler filled one of the dents and then sanded it done so it was smooth as a baby's butt. He also showed me the before / after photos of a C&^%&%172 that had hail damage on the wings. Amazing. I now know what magic a good shop can do. The "outies" were what was bothering me the most. These he said were easily dealt with as well. I rapidly realized I was being a worry wart old woman.. (no offence to PC worry wart old women intended.) Serendipity being what it is, I was glad I went as he had a Glasair Sportsman in the shop for painting. It was an "11 day to taxi" with the windows not quite complete. I saw how the windows were Silpruf'd in with a "trench" around the perimeter. I believe the plan was to Silpruf the trench and use this as a trim ring around the window. I believe the upside to this was that it would be *easier* to replace a window. I have just received the Glasair Silpuf video so I look forward to seeing how this really works. Cheers Les Kearney #40643 ________________________________________________________________________________
Date: Mar 15, 2008
From: PJ Seipel <seipel(at)seznam.cz>
Subject: Re: VS1016
Take a look in section 11, page 5. PJ Seipel RV-10 #40032 Chase Snodgrass wrote: > > Almost ready to rivet vertical stabilizer, and have a part leftover. > LOL. Where does VS1016 fit???? > > Chase Snodgrass > Presidio, TX > http://flybigbend.com > > > ________________________________________________________________________________
Date: Mar 15, 2008
From: linn Walters <pitts_pilot(at)bellsouth.net>
Subject: Re: window cleaning
You can also get acrylic cleaners at good motorcycle shops ..... they have a worse problem than we do!!! I use copious amounts of water (hold the hose on the windshield) and my had to get the grit and big bug lumps off, then lay a wet towel over the windshield to soften the remaining bug bodies ...... wash with an old t-shirt ....the microfiber should work well here .... and then use an acrylic cleaner. I bought a bottle of LP AERO cleaner at Sun-n-Fun, but have used others from motorcycle and auto parts places with excellent results. Linn Tim Olson wrote: > > While I never had problems with Pledge (pump ONLY NOT AEROSOL) on my > last plane, I've now switched exclusively to Plexus for my RV-10... > the windshield being so utterly painful to replace I figured it was > worth a couple bucks more for the care. Try skygeek.com for pricing. > I've also been exclusively using microfiber towels for the past 5 or 6 > years...they're perfect for the job. > > Tim Olson - RV-10 N104CD - Flying ________________________________________________________________________________
From: John Gonzalez <indigoonlatigo(at)msn.com>
Subject: Re: Andair/FI Fitting
Date: Mar 15, 2008
Jim, I presume what you mean is with the tee fitting, I wouldn't have to run ret urn lines to each tank, and that the way you have it installed means that t he overflow fuel that is created when the pump is on just goes back to the supply line coming off the Andair valve. In my case I was originally going to install a different type of engine whi ch required fuel pumps running continiously, so I in fact have return lines already installed running back to the tank so as I understand it, I will n ot need this tee fitting. I will just run my overflow line to the upper ret urn port on my Andair valve and return the fuel to the tank it was pulled f rom. Is this correct? Thanks, JOhn G. 409 redesigning the Door fitting, perfect timing with the emails.> Subject: RV10-List: Re: Andair/FI Fitting> From: jimberry(at)qwest.net> Date: st message posted by: "jim berry" > > John,> > I believ e most people are using the Andair valve with the built in 90 degree ports, because it makes plumbing the fuel lines easier. I used the swivel tee on the center(or outflow) port because there is not enough room for a standard tee to clear the other 2 ports during installation. If you spend some time trying to get all 3 lines installed to the Andair in the confined space of the tunnel I think you will find the extra cost of the swivel tee to be wo rth it.> > Jim Berry> 40482> N15JB(reserved)> > > > > Read this topic onlin e here:> > http://forums.matronics.com/viewtopic.php?p=169822#169822> > > -======================== ==> > > ________________________________________________________________________________
From: "gary" <speckter(at)comcast.net>
Subject: Weight and B alance
Date: Mar 15, 2008
Does anyone have a good weight and balance spreadsheet. I couldn't find one in the search here or Vans airforce. Gary 40274 ________________________________________________________________________________
Subject: Re: Andair/FI Fitting
From: "jim berry" <jimberry(at)qwest.net>
Date: Mar 15, 2008
John, I think we may be talking about different things. See page 37-4, step 7. My comments assume one is using the Andair fuel valve with the built in 90 degree fittings. I believe most people are using this valve, as it provides easier routing of the fuel lines than the valve with 45 degree fittings shown in Van's drawings. The problem with using a standard AN826 tee on the center port is that the middle leg of the tee will not clear the right and left ports during installation. The swivel tee allows you to keep the middle leg in a fixed position while you tighten the female leg on to the center port of the Andair Valve. I also have a return(purge) line for my Airflow Performance injector, so I actually used 2 swivel tees on the center and right ports to make future maintenance easier. Jim Berry 40482 N15JB(reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=170079#170079 ________________________________________________________________________________
From: neil <ncol(at)xtra.co.nz>
Subject: What did I do wrong?
Date: Mar 16, 2008
________________________________________________________________________________
From: "Bob-tcw" <rnewman(at)tcwtech.com>
Subject: wing root fairing support, Bad Part???
Date: Mar 16, 2008
I'm working on Page 44-2, the wing root fairing supports F-1099EFG-L and F-1099EFG-R, I believe I have a bad part and could use some help identifying the good part. The part (F-1099EFG) has an L shaped angle with one flange being about .750" wide and the other .640" wide. The parts I received are NOT mirror images of each other. One part has the holes punched in the .750" flange, the other in the .640" flange. This effects the height of the support of the wing root fairing and pretty clearly one of these is wrong. Can anyone tell me which flange the holes should be punched in so I can tell Van's which one they need to send me and in the mean time fit up the good part I do have. My guess currently is the pre punched holes are on the .750 flange that mates up to the fuselage per steps 2 and 3 on page 44-2. Thanks for the help, Bob Newman TCW Technologies www.tcwtech.com ________________________________________________________________________________
Date: Mar 16, 2008
From: Les Kearney <kearney(at)shaw.ca>
Subject: Silpruf / Window Installation and other magic
Hi One the strength of Dave Saylor's recommendation and other comments, I purchased the AirlinkTech video on using Silpruf to set install windows. The video can be found at: http://tinyurl.com/2ndhr9 I watched the video last night and have a few comments, FWIW. First, a big negative - it's on a VHS tape not on a DVD. After that it was a very nice "how to" video. In short the process used is to mask the windows and then set them in place on small Silpruf standoffs that keep the windows flush with the canopy. A bead of Silpuf is used to install the windows. Screw on clecos are used to keep everything in pace while things dry. The video is very detailed and shows everything required, step by step. It explains how and why to mask the windows to get a nice sharp reveal. It also shows how to trim the windows for a perfect fit. A groove (about 1/8") is left between the windows and the canopy. After painting, Silpruf is used to fill the groove. Apparently Silpruf cannot be painted so you must pick a Silpuf colour that works with your pain scheme. At first blush there seems to be some obvious advantages to this method they being: * The Silpruf has a long working time so you don't have to play "beat the clock" when installing. * The Silpruf is non reactive so you can use normal masking tape to setup the "reveal" edges. You will have lots of time to get everything just right before you have to remove the masks. * The Silpruf is flexible so there won't be cracks in the paint / caulking around the windows * In the event that a window needs to be replaced. It would be a much easier job to remove & replace the window *I think*. * You are not glassing onto a window with all the associated issues with sanding etc. As someone mentioned in an earlier post, with windows you can't fix a screw up with an OOPS rivet. * Before curing and after, excess along the groove can be easily removed. A quick search shows that Silpruf is available in a wide choice of colours including: White, Black, Limestone, Light Grey, Aluminium, GreyDark, Grey, Precast White and Bronze. Right after I watched the video I checked the plans to see how the front window is installed. My recollection was there was no "joggle" at the bottom of the front windscreen. Using Silpruf on the front windscreen would, I think, require building a joggle and then trimming the window to fit. I just noticed that Dave noted this rework in one of his posts as well. The video is very detailed and shows everything required, step by step. It explains how and why to mask the windows to get a nice sharp reveal. It also shows how to trim the windows for a perfect fit. If you are contemplating using this method, get the video, it is well worth the cost. Anyway, I for one plan to use this method on the side windows. I still have a lot of time to contemplate the front windscreen... Cheers Les Kearney #40643 - moving from rivets to systems C-GCWZ ________________________________________________________________________________
From: "David McNeill" <dlm46007(at)cox.net>
Subject: wing root fairing support, Bad Part???
Date: Mar 16, 2008
you do have a bad part; I had one also the left one bad , right was OK. and Van's saw and shipped a new part the part was bent wrong and holes do not line up even when properly shaped. Also heights do not match top fairing. _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Bob-tcw Sent: Sunday, March 16, 2008 6:39 AM Subject: RV10-List: wing root fairing support, Bad Part??? I'm working on Page 44-2, the wing root fairing supports F-1099EFG-L and F-1099EFG-R, I believe I have a bad part and could use some help identifying the good part. The part (F-1099EFG) has an L shaped angle with one flange being about .750" wide and the other .640" wide. The parts I received are NOT mirror images of each other. One part has the holes punched in the .750" flange, the other in the .640" flange. This effects the height of the support of the wing root fairing and pretty clearly one of these is wrong. Can anyone tell me which flange the holes should be punched in so I can tell Van's which one they need to send me and in the mean time fit up the good part I do have. My guess currently is the pre punched holes are on the .750 flange that mates up to the fuselage per steps 2 and 3 on page 44-2. Thanks for the help, Bob Newman TCW Technologies www.tcwtech.com ________________________________________________________________________________
Date: Mar 16, 2008
From: Brian Rodgers <airphoto177(at)yahoo.com>
Subject: New to list
Any one from Long Island NY? I own a piper 235 pathfinder now and plan on building a RV10 in a few years. Just waiting to buy a house with a garage. In the mean time I am just doing my research. Thank you Brian Rodgers --------------------------------- Be a better friend, newshound, and know-it-all with Yahoo! Mobile. Try it now. ________________________________________________________________________________
From: Richard Reynolds <rvreynolds(at)macs.net>
Subject: Re: Door fit
Date: Mar 16, 2008
Apple-Mail-42--238489084 Apple-Mail-43--238489077-- ________________________________________________________________________________
From: "Chris" <toaster73(at)embarqmail.com>
Subject: Garmin Avionics stack question
Date: Mar 16, 2008
In planning my panel , I will have a garmin 430, sl30, gtx327, and gma 340, looking at the lengths of everything if I stack them in said order top to bottom I will be able to see the back of the tubes on each unit looking up from the floor. Would this be ok. I am not use to any particular order. Plus having the 430 on top puts its sreen up where I can see it. Just thought this arrangment might be handy down the road if I have maintenance issues looking working under/behind the panel. Thoughts?? Chris Lucas #40072 ________________________________________________________________________________
From: Jesse Saint <jesse(at)saintaviation.com>
Subject: Re: Garmin Avionics stack question
Date: Mar 16, 2008
First of all, I may recommend one of the PMA audio panels over the Garmin, but they are a little more expensive. Second, while it is true that the audio panel is shorter from front to back, the shape of the tray is very conducive to putting it at the top of the stack. With the way the wires come out of it, there won't be much (if anything) you can do on it from underneath the panel. The best way to access them, IMHO is to leave a little bit of a service loop in the back so you can pull the stack out of the panel and make any changes. The main thing I have seen the need to do from under the panel is to remove and replace antenna wires, which would work whether you put the 430 at the top or the 340 at the top. FWIW, working on your back under the panel is extremely uncomfortable and difficult. Planning a way to access things from the front, especially by making the panel in more than one piece so you can pull out one part at a time to work behind others, is my preferred way to install. Though possibly a little bit unconventional, I prefer to wire the radio stack instruments together and use aluminum angle to hold them together, and then use nutplates and screws to hold them to the instrument panel. I prefer this because it makes it a lot easier to remove the rest of the panel to allow work to be done on the radio stack or things/wires in the sub-panel area. As John Cox always says, part of the building process is thinking through and planning for the maintenance procedures, which is exactly what you are doing. In summary, planning a way to access things from the front would be my recommendation instead of planning to work on them from underneath. Jesse Saint Saint Aviation, Inc. jesse(at)saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Mar 16, 2008, at 9:48 PM, Chris wrote: > In planning my panel , I will have a garmin 430, sl30, gtx327, and > gma 340, looking at the lengths of everything if I stack them in > said order top to bottom I will be able to see the back of the tubes > on each unit looking up from the floor. Would this be ok. I am not > use to any particular order. Plus having the 430 on top puts its > sreen up where I can see it. Just thought this arrangment might be > handy down the road if I have maintenance issues looking working > under/behind the panel. Thoughts?? > > Chris Lucas > #40072 > > ________________________________________________________________________________
Subject: Garmin Avionics stack question
Date: Mar 17, 2008
From: "McGANN, Ron" <ron.mcgann(at)baesystems.com>
Hey Chris, I have the same stack as yourself. My layout has the 340 on top, 430, sl30 and the GTX-327. Here is what I found during install: 1. the 430 and the SL-30 extend beyond the subpanel and require a penetration. Subsequent routing of the 430/sl-30 loom to the 340/327 and panel instruments is a PITA. 2. although the 327 fits in the panel/subpanel gap, I still needed to install a 90deg BNC connector to the antenna. Had the 327 not been on the bottom, this would have been a pain. 3. I have the panel divided into Pilot/stack/copilot segments as suggested by Jesse and it works well. 4. I have a sufficiently large service loop to allow the stack segment to be brought forward for access to the connectors. 5. My power and EFIS/avionics (3xGRT and EIS, CDI, T&B, A/P etc) data looms are laid out on the aft side of the subpanel (ie facing the pilot) for easy access. Planning the panel wiring for ease of maintenance is something that takes time, but it is well worth it when you find that you omitted a connection during final checkout! cheers, Ron ________________________________ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Chris Sent: Monday, 17 March 2008 12:18 PM To: rv10-list(at)matronics.com Subject: RV10-List: Garmin Avionics stack question In planning my panel , I will have a garmin 430, sl30, gtx327,


March 04, 2008 - March 16, 2008

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