RV-Archive.digest.vol-mm

March 06, 2002 - March 12, 2002



      
      
      
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From: "John Starn" <jhstarn(at)earthlink.net>
Subject: Re: Towing a RV6 fusalage?
Date: Mar 06, 2002
We, Gummibear & I, have towed the HRII rocket several times. We moved it from the original constuction garage to Hesperia Airport, then to the welding shop of our local exhaust guy (who's building a -6A), then to Tom's garage in Apple Valley and then to Apple Valley airport. The welder guy used a piece of "square" tubing that fit in the smaller tow hitch of the Grand Prix and the larger hitch on my Dodge Ram PU. He made and welded a 3" wide, 4"long, 1 1/2" deep box on the end of this 4' tube. Tube is 4' long so there is no conflict with the tail while turning. Bent the tube twice so the "box" was level & about 12" to 18" (GP vs Ram) off the ground. We towed with the tail wheel strapped into this box. The complete tail and engine were mounted. Must have towed at least 30 or so miles total without a problem. Ran slow with flashers and a chase vehicle. For run ups on the IO540 we tied the tail wheel down with a chain. I hope we exceeded 550# of pull. Can't speak for the -6 but the HRII tail section was and is just fine. Do Not Archive KABONG ----- Original Message ----- Subject: Re: RV-List: Towing a RV6 fusalage? > How far do you have to tow? I towed mine by the tail wheel spring. ________________________________________________________________________________
Date: Mar 06, 2002
Subject: Anodizing fuel caps?
From: czechsix(at)juno.com
Guys, Since my -8A is going to have a T-6A paint scheme, and the T-6A has red anodized fuel caps, I decided my fuel caps have gotta be red anodized too : ) Only problem is the fuel caps we get from Vans are some sort of cast aluminum, and the guys I've talked to who do custom anodizing say that cast aluminum often has other metals mixed in which may result in less than desirable results when anodizing (may be splotchy in appearance, turn black, or just not work at all). So, I'm wondering if anybody has tried anodizing one of Van's fuel caps, or do any of you metallurgy gurus out there know what kind of stuff is in these caps? Along the same line, does anybody know if there's another higher quality (i.e. machined aluminum vs. cast) fuel cap on the market that would fit into the RV tank filler neck? Eagerly awaiting ya'll's opinions.... --Mark Navratil Cedar Rapids, Iowa RV-8A finish kit stuff... ________________________________________________________________________________
From: ABAYMAN(at)aol.com
Date: Mar 06, 2002
Subject: Re: Vans tach sender
mark the tack setup i got from vans is a 3 part thing. the transducer which mounts on the rear of the case,,it is connected by a square cable to connect to the tack drive of the engine, to the transducer, and 4 wires go the the tack gauge. all seems to work perfectly together, and seems very accurate, although i did not check it against anything. hope this helps scott tampa ________________________________________________________________________________
From: "Jordan, Mel" <jordan_mel(at)ti.com>
Subject: Maintenance Schedule
Date: Mar 06, 2002
I think your idea is a good one. I would add the Vacuum Pump as some have a TBO 600 hours. Since your already doing the Mags at 500 hours, play it safe and do the Vac. Pump at the same time if you have one. Failure of the pump is a leading cause in IFR fatal accidents. Mel Jordan Tucson From: "Randall Henderson" <randallh(at)attbi.com> Subject: RV-List: Maintenance Schedule Someone recently mentioned the 500 hour TBO on Slick Mags. This reminded me of something that I've been thinking about since my focus has gone from "building" to "maintaining". And that is, a "maintenance schedule" that goes beyond the normal annual condition inspection. Kind of like the maintenance schedule for your car -- there's all of the regular 20K mile stuff which would be like our condition inspections, but also things like the timing belt at 60,000 miles which would be more like our magneto O/H. Has anyone worked up something like this? I'd like some suggestions for what to put on mine. I have the data from the C/S prop manual (lubricate every 6 months and at 100hr/condition inspection time, recommended O/H at 1000 hrs/60 or 72 months for aerobatic craft) the bit about the Slick Mags (500 hr internal inspection and service), and the engine recommended TBO. What else is there like that that would go on such a list? I know TBO for engine, prop, etc. are recommended, not mandatory. Be that as it may, I'd like to make up a comprehensive list for my plane of this kind of stuff. TIA Randall Henderson, RV-6 N6R (~300 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com>
Subject: F18 Pics
Date: Mar 06, 2002
My mail system is mis-formatting my email so Matronics is stripping out the folder. ________________________________________________________________________________
Date: Mar 06, 2002
From: "Scott Kuebler" <skuebler(at)cannondesign.com>
Subject: RV-6 / 6a kit for sale
RV-6 / 6a kit for sale. Empennage: Complete except for fiberglass tips. Includes electric elevator trim kit. All parts are alodined and primed with Marhyde primer. Wings & Phlogiston Spar: Both skeletons assembled. All skins drilled to both wings. Includes electric ailreon trim kit. ALL parts (assembled or not) are alodined and primed with Deft epoxy primer (Mil-P-23377G). Both kits are the pre-punched versions purchased in 1997 & 1998 by myself. Construction is excellent. Preview plans and Orndorff videos included for both kits. Priced to sell: $5000 If all items were purchased separately the price would be more than $6500 for unassembled kits. The reason for selling is that my wife and I just had our first child and I have an old house to finish rebuilding first. The tools are not for sale; I will be keeping them to guarantee that I will build another RV in the near future! Scott Kuebler Buffalo, NY 716-695-1987 home 716-510-0318 cell skuebler(at)cannondesign.com ________________________________________________________________________________
From: "John Warren" <jwdub(at)teleport.com>
Subject: Tach Checking
Date: Mar 06, 2002
Another interesting fact in checking an optical prop tach. An 8 foot fluorescent light will cut the observable rpm in half, or 1800 for a two blade prop. John Warren RV-6 in progress LaCenter WA ________________________________________________________________________________
From: "John Furey" <john(at)fureychrysler.com>
Subject: Tach/MP
Date: Mar 06, 2002
Has anyone out there had experience with the Technology Kitchen EPM tachometer/manifold pressure/% of power gauge? Also there was a web site on the list for an electronic attitude indicator from out on the west coast( not blue mountain) priced about $1800. Does anyone know what that site was? Thanks John RV6A ________________________________________________________________________________
From: "KostaLewis" <mikel(at)dimensional.com>
Subject: Re: Maintenance Schedule
Date: Mar 06, 2002
> Someone recently mentioned the 500 hour TBO on Slick Mags.......... OK: what is recommended to overhaul/maintain the mags and/or where does one get that information?? Mine are 575 hours and working............ Michael ________________________________________________________________________________
From: "Terry Watson" <terrywatson3(at)attbi.com>
Subject: Re: Tach/MP
Date: Mar 06, 2002
I think you are referring to Dynon Development, dynondevelopment.com. I don't think they have shipped anything yet. Terry ----- > Also there was a web site on the list for an electronic attitude > indicator from out on the west coast( not blue mountain) priced about > $1800. Does anyone know what that site was? ________________________________________________________________________________
Date: Mar 06, 2002
From: Dave Bristol <bj034(at)lafn.org>
Subject: Re: Pitot Static/Tansponder Check
There is no requirement for the encoder to be checked on a regular basis unless you are IFR. The transponder can be bench tested to comply. Ref: 91.411, 91.413, Appendix F of part 43. Dave RV_8 Pilot wrote: > > Larry - > > I didn't see any responses to your question, so I'll take a stab. > Transponder encoder checks are required basically when operating where > they're required equipment. In a mode C veil and above 10K'. It's required > (x-ponder use and 24 month check) by the FAR's. > > Reasoning? I'd imagine the feds just feel that if you're going to be "in > the system" squawking an altitude, they want it accurate. Makes sense to > me. You're in close proximity to airline and other IFR traffic in a mode C > veil and when above 10K'. > > Also, the check has to be done by a certified shop/tech. I looked into this > extensively and came to the conclusion that you can't self certify, even as > a homebuilder. > > I spent about $100 for my last check. The tech "tuned" my system while > checking it out. The performance improvement was noticable afterwards, > based on my lack of complaints and range from ATC facilities. Before, I'd > have problems with them "seeing" me occasionally. > > This basic x-ponder/encoder check is different than the pitot static system > check required if operating IFR. > > Bryan Jones -8 > Pearland, Texas > > >My question is why are transponder checks required? It's easy to know if > >it is working or not. ATC picks us up, they get the correct discrete > >code and the altitude checks. > > > >Why do we have to pay all the money to the radio shop, in my case to > >someone who doesn't know what they are doing, and in my case to someone > >who does even less than the functional check referred to above. > > Send and receive Hotmail on your mobile device: http://mobile.msn.com > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Maintenance Schedule
Date: Mar 06, 2002
The isn't a 500 hr. TBO on Slicks. There is, just like on a Bendix. a 500 hour inspection as well as a 1000 hour inspection which is listed in the master service manual. Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org Always looking for articles for the Experimenter ----- Original Message ----- From: "KostaLewis" <mikel(at)dimensional.com> Subject: Re: RV-List: Maintenance Schedule > Someone recently mentioned the 500 hour TBO on Slick Mags.......... OK: what is recommended to overhaul/maintain the mags and/or where does one get that information?? Mine are 575 hours and working............ Michael ________________________________________________________________________________
Date: Mar 06, 2002
From: Dave Bristol <bj034(at)lafn.org>
Subject: Re: Towing a RV6 fusalage?
If you pull it up the ramp by the tail remember that it's VERY nose heavy without the tail and wings and will go up on it's nose quite easily. Dave Rv6238(at)aol.com wrote: > > Time is near to move my 6 to the airport. In order to get the plane out of > the basement I will excavate a ramp and lay a 3/4" plywood floor or maybe > 2X12 "tracks" to roll the fuse up to ground level. The engine is installed > and the tail will be removed. The panel and instruments are also installed. I > estimate the weight to be around 550 lbs. I know this has been done before > [Terry, are you watching?] so I could use advise. I am thinking of towing the > fuse up the ramp with a 4WD or tractor. Question, will the tailwheel assembly > and rear bulkheads stand the stress? Or is it better to tow by the front? If > front is best how best to hook up the tow rope. Input needed! And perhaps a > little courage.Thanks guys. > Bill Griffin > Balto., MD > ________________________________________________________________________________
From: "kevin lane" <n3773(at)attbi.com>
Subject: Re: Hanger Sizes
Date: Mar 06, 2002
our T-hangar is, I believe, 39' wide. Using a winch and a ramp we have two -6a's straight in. The wings overlap and the wingtip of the plane on the ground actually fits between the other's wheelpant and underside of the wing. It's tight but saves us $118/mo. It is nice to have the plane up on the 24" ramp while working on wheel pants too. Another pair of RV's have copied our set-up. We winch the planes by the nose wheel bolts that hold on the wheel pant. Kevin ________________________________________________________________________________
Date: Mar 06, 2002
From: Bobby Hester <bhester(at)apex.net>
Subject: Re: IE capacitive fuel sender system
Dan Masys wrote: > > Bobby Hester wrote: > > > > > Anybody installing the IE capacitive system in the fuel tanks, did you > > install the external bracket outside the root rib that they talk about > > in the instructions? Has anyone installed the electronic interface > > module yet? Would like to see a picture of what this looks like. > > I have the electronic interface but haven't installed it. I made .032 3/4 > angle brackets from some leftover stiffener material. So you can see how big > (or tiny, as the case may be) the EI sender unit is, I put it up against the > bracket in the pictures available here: > > http://array.ucsd.edu/rv7a/FuelSender.html > > -Dan Masys > -7A N747DL reserved, fuse I guess since the IE Gauge is so cheap they cannot afford to put a BNC connector on the end of the wire. -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
From: "Nancy and Walter Shipley" <wshipley(at)esper.com>
Subject: Re: IO 360 Fuel Pump Plumbing
Date: Mar 06, 2002
I have an IO-360 180hp with a Bendix injector servo. In my case, fuel flow is from right to left, viewed from the rear. Walt Shipley RV8A N314TS ---------- > From: Henley <henley(at)seii.net> > To: rv-list(at)matronics.com > Subject: RV-List: IO 360 Fuel Pump Plumbing > Date: Wednesday, March 06, 2002 7:56 AM > > > Getting ready to hook up fuel lines to my engine and find that the inlet > and outlet on the engine driven fuel pump are not labeled. Can anyone > with an IO360 tell me looking at the pump on the rear of the engine, > does the fuel flow from left to right or vice versa. > > John Henley > > > > ________________________________________________________________________________
From: "John Burton" <jdburton(at)cox.net>
Subject: Flying around in an F18 without a canopy is bad. pix URL
Date: Mar 06, 2002
Per the message below, the url for the F-18 pis is: (that's right -- no www, no http, just type it in as presented). Thanks to Scott and to Don Gates for sending them -- ----- Original Message ----- From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com> Subject: RE: RV-List: flying around in an F18 without a canopy is bad.. > John, > The URL keeps getting stripped out when I send the email. Could you please > > Thanks! ________________________________________________________________________________
From: "William Davis" <rvpilot(at)mpinet.net>
Subject: Re: Tach/MP
Date: Mar 06, 2002
John, Have been using one for over 200 hrs. What do you want to know about it? Bill RV-8 Tiger-Kat ----- Original Message ----- From: "John Furey" <john(at)fureychrysler.com> Subject: RV-List: Tach/MP > > Has anyone out there had experience with the Technology Kitchen EPM > tachometer/manifold pressure/% of power gauge? > > Also there was a web site on the list for an electronic attitude > indicator from out on the west coast( not blue mountain) priced about > $1800. Does anyone know what that site was? > > Thanks > John RV6A > > > > > > ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: Re: IE capacitive fuel sender system
Date: Mar 06, 2002
The converter module has a little ring terminal on each of the two wires. EI has a capacitance sender unit that these work with. There are two tiny screws that attach the two terminals. The designer of Van's senders came up with a BNC type connection instead. So the little ring terminals are snipped off (unless one has devised a way to hook up the BNC by using the ring terminals). What I did was to cut off the ring terminals. Attach a piece of coax(about 2 1/2" long) to the mating BNC connecter as you normally would. Strip the insulation off for about an inch down to the shield and unwravel the shield and then twist it back together to make a pigtail. One of the converter wires attaches to the pigtail. Take off more insulation off down to the center conductor. The other converter wire attaches to the center conductor. I used butt splices on both wires. I used shrink wrap on the center connection and then larger shrink wrap over the whole mess to add protection. The BNC coax exits out of one end of the shrinkwrap and the long wires that connect to the guage exit out the other. There may be other ways to connect, but I like this the best. I know you are already thinking about which wire attaches to the center conductor. The answer is, it doesn't matter! Sorry, no pics, Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: "Bobby Hester" <bhester(at)apex.net> Subject: Re: RV-List: IE capacitive fuel sender system > > Dan Masys wrote: > > > > > Bobby Hester wrote: > > > > > > > > Anybody installing the IE capacitive system in the fuel tanks, did you > > > install the external bracket outside the root rib that they talk about > > > in the instructions? Has anyone installed the electronic interface > > > module yet? Would like to see a picture of what this looks like. > > > > I have the electronic interface but haven't installed it. I made .032 3/4 > > angle brackets from some leftover stiffener material. So you can see how big > > (or tiny, as the case may be) the EI sender unit is, I put it up against the > > bracket in the pictures available here: > > > > http://array.ucsd.edu/rv7a/FuelSender.html > > > > -Dan Masys > > -7A N747DL reserved, fuse > > I guess since the IE Gauge is so cheap they cannot afford to put a BNC connector > on the end of the wire. > > > -- > Surfing the Web from Hopkinsville, KY > Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ > RV7A Working on the wings :-) > > ________________________________________________________________________________
From: JTAnon(at)aol.com
Date: Mar 06, 2002
Subject: Pro Seal & Fuel Lube
Gents, Pro-Seal I have an RV 7A QB kit so my tanks are already done. I need a small amount of Proseal for various jobs like sealing the firewall, cover on the tank, etc. Two questions: How much do I really need? pint? quart? Aircraft Spruce lists a "Pro-seal type" tank sealant (PN 09-38510) Type B-2 (Mil spec 8802E) in a poly bag with nozzle that looks like a lot less messy alternative. Is this stuff the same as Pro-seal? Anybody used it? Fuel Lube The manual says to use Fuel Lube on gas and oil fittings. In Aircraft Spruce Fuel Lube is listed as $23 a pound. Right below it in the catalog is a product called Bakerseal in smaller quantities. Is this an equivalent product? John McDonnell (RV7A Fuse) ________________________________________________________________________________
From: "Robin Wessel" <robin.wessel(at)verizon.net>
Subject: Re: Pitot Static/Transponder Check
Date: Mar 06, 2002
I recently had the IFR and Transponder check done for $250 at a local avionics shop. Interestingly, for $250 they did not do any actual calibrations. Apparently adjustments cost extra. I found this out when after I got the cert and logbook stickers, the encoder was squawking 300 above altitude with ATC. I am not sure if it is shoddy workmanship with the avionics shop or what. After finding out that an actual "calibration" would cost additional beyond the standard pitot/static & correspondence cert. I proceeded to adjust the encoder myself (knowing that my altimeter was officially certified as reference). A friend of mine with a certified a/c experienced a similar situation when he had is IFR/TPX cert done at Pacific Coast Avionics. They charged him an additional $70 beyond the $250 to adjust the little screw in the altimeter so it would read airport elevation correctly. moral of the story: adjust your altimeter and encoder yourself before you get it certified because they will charge you for any adjustments. I was able to adjust my encoder easily because my Garmin GPS reports the gray code alt from the encoder. My understanding is that the FAR's allow a tolerance of +- 125 feet of encoder correspondence and the altimeter is 75 feet or less. With a little patience you can calibrate the encoder much better than an avionics shop is required to. robin wessel RV-6A flying http://robin.getbiz.net Tigard, OR ________________________________________________________________________________
Date: Mar 06, 2002
From: Jim Bean <jim-bean(at)att.net>
Subject: Magneto Swap
I am trying to figure out how to swap out the dual magneto on my engine. It's an IO360A1B6D that came out of a Cessna 177. The objective is to replace the dual magneto with a single unit to pair up with an electronic ignition. I contacted Bendix (TCM) and the tech rep told me the magneto to use and to get the driven gear from an IO360A1B engine. These are available, pricey, but the unknown seems to be placing the gear at the right depth. The tech rep thought that spacers would be required to position the gear. Anyway has anyone tried this and what was the result? TIA Jim Bean RV-8 ________________________________________________________________________________
Date: Mar 06, 2002
From: Jim Bean <jim-bean(at)att.net>
Subject: [Fwd: Magneto Swap]
Date: Wed, 06 Mar 2002 22:32:01 -0500 From: Jim Bean <jim-bean(at)att.net> Subject: Magneto Swap I am trying to figure out how to swap out the dual magneto on my engine. It's an IO360A1B6D that came out of a Cessna 177. The objective is to replace the dual magneto with a single unit to pair up with an electronic ignition. I contacted Bendix (TCM) and the tech rep told me the magneto to use and to get the driven gear from an IO360A1B engine. These are available, pricey, but the unknown seems to be placing the gear at the right depth. The tech rep thought that spacers would be required to position the gear. Anyway has anyone tried this and what was the result? TIA Jim Bean RV-8 ________________________________________________________________________________
From: "Michael J. Robbins" <kitfox(at)gte.net>
Subject: Re: Pro Seal & Fuel Lube
Date: Mar 06, 2002
John; Use TiteSeal. Mike Robbins RV8 ----- Original Message ----- From: <JTAnon(at)aol.com> > Fuel Lube > The manual says to use Fuel Lube on gas and oil fittings. > > John McDonnell (RV7A Fuse) ________________________________________________________________________________
From: "Bruce Gray" <bruce.gray(at)snet.net>
Subject: [Fwd: Magneto Swap]
Date: Mar 06, 2002
The best way is to swap out the accessory housing of the engine with an accessory housing from an IO-360 A1A, A1B, A1B6, or A1C engine. Bruce Glasair III -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Jim Bean Subject: RV-List: [Fwd: Magneto Swap] Date: Wed, 06 Mar 2002 22:32:01 -0500 From: Jim Bean <jim-bean(at)att.net> Subject: Magneto Swap I am trying to figure out how to swap out the dual magneto on my engine. It's an IO360A1B6D that came out of a Cessna 177. The objective is to replace the dual magneto with a single unit to pair up with an electronic ignition. I contacted Bendix (TCM) and the tech rep told me the magneto to use and to get the driven gear from an IO360A1B engine. These are available, pricey, but the unknown seems to be placing the gear at the right depth. The tech rep thought that spacers would be required to position the gear. Anyway has anyone tried this and what was the result? TIA Jim Bean RV-8 ________________________________________________________________________________
Date: Mar 06, 2002
From: Finn Lassen <finnlassen(at)netzero.net>
Subject: Re: Compaq Ipaq Cheap for Anywhere map buyers
Maybe - this is the monochrome - not color screen. Finn Donald Mei wrote: > > I just got this email from a "deals" oriented email list: > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and Mortar > OfficeDepot (i.e. the actual store, not the web site) This one is on > clearance at your local retail Office Depot store. They`re really running > out of stock though, and they`re not getting any more in. The SKU# for this > product is 858-251. Best of luck! > > If you are planning on doing anywhere map or icarus solid state efis any > time soon, this is a steal. This item is sold on most web sites for $399. > This item has just been EOl (end of life) according to a friend of mine who > works at compaq. It is for all intents and purposes "current product" and > is the same ipaq that you've heard all the good stuff about. > > Don Mei > RV-4 - N92CT > 3B9 - Chester, CT ---------------------------------------------------- Sign Up for NetZero Platinum Today Only $9.95 per month! http://my.netzero.net/s/signup?r=platinum&refcd=PT97 ________________________________________________________________________________
Date: Mar 06, 2002
From: Michael McGee <jmpcrftr(at)teleport.com>
Subject: Re: Pitot Static/Transponder Check
Okay Robin, I think this is a great topic for the Home Wing meeting. I'll bring my transponder to the April meeting and we can calibrate it before I take it in for it's bi-annual. M > >I recently had the IFR and Transponder check done for $250 at a local >avionics shop. Interestingly, for $250 they did not do any actual >calibrations. Apparently adjustments cost extra. I found this out when after >I got the cert and logbook stickers, the encoder was squawking 300 above >altitude with ATC. I am not sure if it is shoddy workmanship with the >avionics shop or what. After finding out that an actual "calibration" would >cost additional beyond the standard pitot/static & correspondence cert. I >proceeded to adjust the encoder myself (knowing that my altimeter was >officially certified as reference). A friend of mine with a certified a/c >experienced a similar situation when he had is IFR/TPX cert done at Pacific >Coast Avionics. They charged him an additional $70 beyond the $250 to adjust >the little screw in the altimeter so it would read airport elevation >correctly. > >moral of the story: adjust your altimeter and encoder yourself before you >get it certified because they will charge you for any adjustments. I was >able to adjust my encoder easily because my Garmin GPS reports the gray code >alt from the encoder. My understanding is that the FAR's allow a tolerance >of +- 125 feet of encoder correspondence and the altimeter is 75 feet or >less. With a little patience you can calibrate the encoder much better than >an avionics shop is required to. > >robin wessel >RV-6A flying >http://robin.getbiz.net >Tigard, OR > > Mike McGee, RV-4 N996RV, O320-E2G, Aurora, OR 13B in gestation mode ________________________________________________________________________________
From: "Daniel Estrada F." <dani_estrada(at)infosel.net.mx>
Subject:
Date: Mar 06, 2002
________________________________________________________________________________
From: "Daniel Estrada F." <dani_estrada(at)infosel.net.mx>
Subject: Need your help (not RV related)
Date: Mar 06, 2002
Hello, As some of you know, I had to quit building my RV7A. But now I am planning start next year a Professional Pilot Career and here is when I need your help and tips. I need you to tell me what of the following flight training schools is the best: Flight Safety (the best for me, but too expensive!) American Flyers ComAir Academy Phoenix East Aviation Tyler School of Aeronautics Or what school you recommend..?? Thanks and sorry for the not related RV question.. Daniel Estrada F Mexico City ex--RV-7A ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Mar 07, 2002
Subject: Re: Need your help (not RV related)
In a message dated 3/6/2002 9:04:46 PM Pacific Standard Time, dani_estrada(at)infosel.net.mx writes: > As some of you know, I had to quit building my RV7A. But now I am > planning start next year a Professional Pilot Career and here is when I > need your help and tips. I need you to tell me what of the following > flight training schools is the best: > > Flight Safety (the best for me, but too expensive!) > American Flyers > ComAir Academy > Phoenix East Aviation > Tyler School of Aeronautics > > Or what school you recommend..?? A buddy of mine (and maybe one of the 9/11 terrorists, although not concurrently) were trained at Embry-Riddle. -GV (N1GV) ________________________________________________________________________________
Date: Mar 07, 2002
From: Charlie Kuss <chaskuss(at)bellsouth.net>
Subject: Re: Gasket Sealant on Lycoming's
Whoops! Perhaps I should have been more specific in my instructions. ( I didn't recommend using it on both sides of the gasket) As Gary noted, you only apply adhesive between the valve cover (or other removable part) and the gasket. To easily remove difficult gaskets, use your right angle die grinder with the 2" Roloc ScotchBrite disks. Many years before I ever used one of these tools to de burr sheet aluminium, I was using it on vehicles to remove old gaskets and clean up gasket mating surfaces. Charlie Kuss >Be forwarned that when Gorrilla Snot is used as a gasket adhesive the >gasket will never come off without serious scraping or chemical soaking. >Do not applly Gorrilla Snot to both sides of the gasket, you'll tear the >cylinder from the crankase trying to get the valve cover off. 3M means >business when they call a product an adhesive. It is good stuff. > >Gary > > > Apply a thin layer of 3M super weatherstrip adhesive (aka Gorilla snot) to > > the valve cover side of the gasket. Set the gasket in the valve cover, > > then remove it for 1-3 minutes. This allows the adhesive to "tack up" (much > > like using contact cement) Reinstall the gasket in the valve cover. Quickly > > position the gasket in the cover so that all the bolt holes line up > > properly. (The adhesive becomes very sticky quickly). Leave the other > > gasket surface dry and install the cover. Install and tighten up the bolts > > using a nut driver. Torque to specs using a torque wrench. ________________________________________________________________________________
Date: Mar 07, 2002
From: Mike Thompson <grobdriver(at)yahoo.com>
Subject: Re: Flying around in an F18 without a canopy is bad. pix URL
I'd say hang a big OPPS! on that one. --- John Burton wrote: > > > Per the message below, the url for the F-18 pis is: > > > (that's right -- no www, no http, just type it in as presented). > > Thanks to Scott and to Don Gates for sending them -- ________________________________________________________________________________
From: "Mike Plecenik" <nanchang(at)earthlink.net>
Subject: Re: Compaq Ipaq Cheap for Anywhere map buyers
Date: Mar 07, 2002
From Amazon.c: (they're still asking over $500. new & over $300. used) Standard memory: 32 MB RAM, 16 MB ROM Maximum memory: Up to 64 MB with card Expansion slot: CompactFlash Display type: Color-reflective TFT LCD (indoor/outdoor) Display colors: 4,096 (12-bit) Display size: 2.26 by 3.02 inches Resolution: 240 by 320 pixels Display backlight: Yes, ambient-light sensor adjusts automatically Processor: 206 MHz Intel StrongARM SA-1110 32-bit RISC Operating system: Microsoft Windows for Pocket PCs PC compatible: Yes Mac compatible: No PC system requirements: 486 MHz processor or higher, Windows 98 or 2000 for USB synchronization, USB port, CD-ROM drive Handwriting recognition: Yes Keyboard: On-screen User controls: On/off, light, menu, speaker/5-way joystick, contacts, calendar Memo pad: Yes Address book: Yes Scheduler: Yes E-mail: Yes Web browser: Yes Security: Password protection Stereo: Yes Built-in speaker: Yes Headset jack: Yes (3.5mm stereo) Voice recorder: Yes MP3 playback: Yes Audible content playback: Yes AC adapter included: Yes Battery type: 950 mAh Lithium Polymer Batteries included: Yes Average battery life: 12 hours Serial port: Yes, with optional Compaq serial cradle USB: Yes Infrared: Yes Wireless: Yes Docking cradle: USB cradle included PC cable: Yes Other hardware: Two styli, vinyl slipcase, AC adapter Software: Pocket PC software: Pocket Word, Pocket Excel, Pocket Internet Explorer, Windows Media Player, Inbox, Microsoft Reader, File Explorer, Asset Viewer, Picture Viewer; Desktop software: Microsoft Active Sync 3.1, Microsoft Money for Pocket PC, Pocket Streets, Outlook 2000, Internet Explorer 5.0, Media Manager, Tscribe, Microsoft Reader e-book samples Width: 3.28 inches Height: 0.62 inches Depth: 5.11 inches Weight: 6.3 ounces Warranty, parts: 1 year Warranty, labor: 1 year > > Maybe - this is the monochrome - not color screen. > > Finn > > Donald Mei wrote: > > > > > I just got this email from a "deals" oriented email list: > > > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and Mortar > > OfficeDepot (i.e. the actual store, not the web site) This one is on > > clearance at your local retail Office Depot store. They`re really running > > out of stock though, and they`re not getting any more in. The SKU# for this > > product is 858-251. Best of luck! > > ________________________________________________________________________________
Date: Mar 07, 2002
From: philip condon <pcondon(at)mitre.org>
RV-List Digest Server
Subject: Re: RV-List Digest: Engine long-term storage trick
I am in the process of setting my O-540 Lycoming up for long term storage and needed to seal off the exhaust ports from ambient air (to keep moisture from harming the valve stem,face & seat ect..)I used the dryer plugs as most folks do and needed a cheap, quick way of sealing the exhaust ports on all the jugs. Off to the sports store to get 6 handball balls and two racketball balls. Jammed one of the racketball balls into the hollow crankshaft cavatity (after spraying LPS-2 in there) and jammed a (smaller) handball ball into the exhaust post. The rubber in the balls sealed the openings, and the color dosen't look all that bad either. 24 quarts of oil there so far too......hope there isn't much room left, that oil is expensive...... ________________________________________________________________________________
From: "Jordan, Mel" <jordan_mel(at)ti.com>
Subject: Flight Training
Date: Mar 07, 2002
GV None of the terrorists of 9/11 were trained at Embry-Riddle. However, First Officers David M. Charlebois on AA77 was a Riddle graduate. In the days following 9/11, when all the press were on a witch hunt to blame flight training for the acts of these fanatics, Embry-Riddle was incorrectly identified as having trained one of the terrorists. This was later proven not correct. The person Embry-Riddle trained that shared a similar name with one of the terrorists, is currently an airline captain. Mel Jordan From: Vanremog(at)aol.com Subject: Re: RV-List: Need your help (not RV related) In a message dated 3/6/2002 9:04:46 PM Pacific Standard Time, dani_estrada(at)infosel.net.mx writes: > As some of you know, I had to quit building my RV7A. But now I am > planning start next year a Professional Pilot Career and here is when I > need your help and tips. I need you to tell me what of the following > flight training schools is the best: > > Flight Safety (the best for me, but too expensive!) > American Flyers > ComAir Academy > Phoenix East Aviation > Tyler School of Aeronautics > > Or what school you recommend..?? A buddy of mine (and maybe one of the 9/11 terrorists, although not concurrently) were trained at Embry-Riddle. -GV (N1GV) ________________________________________________________________________________
Date: Mar 07, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: RV-List Digest: Engine long-term storage trick
philip condon wrote: > > 24 quarts of oil there so far too......hope there isn't much room left, that oil is expensive...... You did use the cheapest automotive oil you could find, didn't you? :-) No need to pour the good stuff in just to pickle the engine. Sam Buchanan "The RV Journal" http://thervjournal.com ________________________________________________________________________________
Date: Mar 07, 2002
From: Dan DeNeal <rv6apilot(at)yahoo.com>
Subject: Plumbing Woes?!?
Why is it so difficult to plumb the airspeed with the pito tube, the altimeter and vertical speed with the static. And then theirs the vacuum lines that need an airfilter for intake and vacuum regulator that leads to the vacuum pump. I understand the process!!! What I don't understand is why I can't make it work. The back of the airspeed requires 1/8" threads with a 1/4" barb to conect a hose that measures 1/4" ID which I think is 3/8"OD. But a 3/8"OD will not work for the T-Connectors that have 1/8" threads to screw into the altimeter and have 1/4"OD connectors! And then theirs the vacuum connections that require 1/4" threads with a 3/8" barb. Do you use plastic lines? I am so frustrated with this plumbing!!!! Dan DeNeal RV6a ________________________________________________________________________________
From: "C. Rabaut" <crabaut(at)coalinga.com>
Subject: Re: RV-List Digest: Engine long-term storage trick
Date: Mar 07, 2002
You mean I did not have to pay all that money for Shell "2F" oil??? ----- Original Message ----- From: Sam Buchanan <sbuc(at)hiwaay.net> Subject: Re: RV-List: Re: RV-List Digest: Engine long-term storage trick > > > philip condon wrote: > > > > > > 24 quarts of oil there so far too......hope there isn't much room left, that oil is expensive...... > > > You did use the cheapest automotive oil you could find, didn't you? :-) > > No need to pour the good stuff in just to pickle the engine. > > Sam Buchanan > "The RV Journal" http://thervjournal.com > > ________________________________________________________________________________
From: "CHUCK STRATMAN" <Pilot93434(at)kscable.com>
Subject: Cessna Master Switch
Date: Mar 07, 2002
Posters, I recived a real nice split master switch from ACS, however there is no wiring diagram with it. Does any one know where to find a good (labled) wire schematic for this switch or has one I can rent? This switch has 6 terminals, 2 singles and 2 doubled up. Chuck Stratman wiring N118JR ________________________________________________________________________________
From: "Tony Castellano" <tcastell(at)bestweb.net>
Subject: Re: [Fwd: Magneto Swap]
Date: Mar 07, 2002
I converted a Lycoming O360-A1F6D, which also came from a Cessna Cardinal, from the Dual Bendix mag to a single Slick mag (with impulse coupler). The gear from the Bendix mag fit the Slick mag perfectly. The only thing I had to do was turn down the diameter of the flat washer a small amount. I installed a Jeff Rose (Electroair) electronic ignition for the other set of plugs. Jeff offers a split gear as the pickup which is easily installed on the forward end of the crank. I discussed this previously on the list, so if you search the archives, you can get more detailed information. ie mag model numbers etc. Tony Castellano tcastell(at)bestweb.net Hopewell Junction, NY RV-6 N401TC ----- Original Message ----- From: "Jim Bean" <jim-bean(at)att.net> Subject: RV-List: [Fwd: Magneto Swap] > > > Date: Wed, 06 Mar 2002 22:32:01 -0500 > From: Jim Bean <jim-bean(at)att.net> > To: rv-list(at)matronics.com > Subject: Magneto Swap > > I am trying to figure out how to swap out the dual magneto on my engine. > It's an IO360A1B6D that came out of a Cessna 177. The objective is to > replace the dual magneto with a single unit to pair up with an > electronic ignition. I contacted Bendix (TCM) and the tech rep told me > the magneto to use and to get the driven gear from an IO360A1B engine. > These are available, pricey, but the unknown seems to be placing the > gear at the right depth. The tech rep thought that spacers would be > required to position the gear. > > Anyway has anyone tried this and what was the result? > > TIA Jim Bean > RV-8 > > ________________________________________________________________________________
From: "Bob Hasson" <hassonr(at)theriver.com>
Subject: Re: Pro Seal & Fuel Lube
Date: Mar 06, 2002
John, A lot of people use the term "pro seal" to describe all fuel tank sealants, just as some people refer to any soft drink as a "coke". In this case there are many companies manufacturing sealants, Coast Pro Seal Co. is just one of them. All fuel tank sealants are manufactured to a Military Specification (Mil Spec). A few Mil Spec fuel tank sealants are: Mil-S-8802, Mil-S-83318(1), Mil-S-8802D, Mil-S-83430, and PS 890. All of these Mil Specs will have additional numbers/letters that further define the sealant, an example of a complete Mil Spec is Mil-S-8802-B-2. The alpha following the base number (in this case "B") indicates the viscosity, type A sealants are thin and type B is much thicker. Normally type A sealants are applied with a brush and type B with a spachula, either type can be used in an injection gun. The last number in the sequence is the application time in hours, in this case 2 hours. All of these sealants are polysulfide type and cure time is based on a standard atmosphere, changes in humidity and temperature can increase, or decrease the cure time. There are hundreds of types of sealants used in the aero-space industry, however not all of them that look, smell, and taste like the fuel tank sealants listed above are fuel resistant! The Mil Spec for fuel tank sealants specifies that the product is "Sealing compound, integral fuel tanks and fuel cell cavities", as long as this description is on the container it should be safe to use as a fuel tank sealer. As for the "sem Kit", it IS a lot messy, but at a cost. It contains the curing compound (black stuff) in the tube which is mixed with the base compound (white stuff) when the plunger is extended. In other words it is designed to be mixed, used and the balance tossed. It is probably smarter to just go ahead and buy a pint of the PS 890 and mix what you need. If you keep the unmixed materials in a refrigerator (your beer frig, not with food products), it will last a long time. I hope this helps. Bob Hasson Tucson, AZ RV-6A 188 hours -----Original Message----- From: JTAnon(at)aol.com <JTAnon(at)aol.com> Date: Wednesday, March 06, 2002 8:48 PM Subject: RV-List: Pro Seal & Fuel Lube > >Gents, > >Pro-Seal >I have an RV 7A QB kit so my tanks are already done. I need a small amount >of Proseal for various jobs like sealing the firewall, cover on the tank, etc. > >Two questions: > >How much do I really need? pint? quart? > >Aircraft Spruce lists a "Pro-seal type" tank sealant (PN 09-38510) Type B-2 >(Mil spec 8802E) in a poly bag with nozzle that looks like a lot less messy >alternative. Is this stuff the same as Pro-seal? Anybody used it? > >Fuel Lube >The manual says to use Fuel Lube on gas and oil fittings. In Aircraft Spruce >Fuel Lube is listed as $23 a pound. Right below it in the catalog is a >product called Bakerseal in smaller quantities. Is this an equivalent >product? > >John McDonnell (RV7A Fuse) > > ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Cessna Master Switch
Date: Mar 07, 2002
> >Posters, >I recived a real nice split master switch from ACS, however there is no >wiring diagram with it. Does any one know where to find a good (labled) >wire schematic for this switch or has one I can rent? This switch has 6 >terminals, 2 singles and 2 doubled up. > >Chuck Stratman >wiring N118JR > > I have the same switch in my airplane. No schematic needed. It's just two independent rocker switches. Put an ohmmeter across the terminals to see what opens up and what closes when the switches are activated. The doubled up terminals are common to each other so you can hook up other wires to the same electrical point, such as ones that could go to an overvoltage relay, panel indicator, etc. Brian Denk RV8 N94BD 277 hrs. Send and receive Hotmail on your mobile device: http://mobile.msn.com ________________________________________________________________________________
Date: Mar 07, 2002
From: David Roseblade <davidagr(at)emirates.net.ae>
Subject: Static pickup for RV6
Listers, Van's sells a static port kit for the RV6, how essential is this? I only intend to fly VFR and therefore is a pickup in the cockpit sufficient? Your thoughts, experience and advise. David Roseblade RV6 Finishing kit Dubai, UAE ________________________________________________________________________________
Date: Mar 07, 2002
From: Finn Lassen <finnlassen(at)netzero.net>
Subject: Re: Compaq Ipaq Cheap for Anywhere map buyers
Mike, why are you quoting specs on the Color model? The 3135 or 3035 is monochrome! That's why the much lower price. The screen! Finn Mike Plecenik wrote: > > >From Amazon.c: (they're still asking over $500. new & over $300. used) > > Standard memory: 32 MB RAM, 16 MB ROM > Maximum memory: Up to 64 MB with card > Expansion slot: CompactFlash > Display type: Color-reflective TFT LCD (indoor/outdoor) > Display colors: 4,096 (12-bit) > Display size: 2.26 by 3.02 inches > Resolution: 240 by 320 pixels > Display backlight: Yes, ambient-light sensor adjusts automatically > Processor: 206 MHz Intel StrongARM SA-1110 32-bit RISC > Operating system: Microsoft Windows for Pocket PCs > PC compatible: Yes > Mac compatible: No > PC system requirements: 486 MHz processor or higher, Windows 98 or 2000 for > USB synchronization, USB port, CD-ROM drive > Handwriting recognition: Yes > Keyboard: On-screen > User controls: On/off, light, menu, speaker/5-way joystick, contacts, > calendar > Memo pad: Yes > Address book: Yes > Scheduler: Yes > E-mail: Yes > Web browser: Yes > Security: Password protection > Stereo: Yes > Built-in speaker: Yes > Headset jack: Yes (3.5mm stereo) > Voice recorder: Yes > MP3 playback: Yes > Audible content playback: Yes > AC adapter included: Yes > Battery type: 950 mAh Lithium Polymer > Batteries included: Yes > Average battery life: 12 hours > Serial port: Yes, with optional Compaq serial cradle > USB: Yes > Infrared: Yes > Wireless: Yes > Docking cradle: USB cradle included > PC cable: Yes > Other hardware: Two styli, vinyl slipcase, AC adapter > Software: Pocket PC software: Pocket Word, Pocket Excel, Pocket Internet > Explorer, Windows Media Player, Inbox, Microsoft Reader, File Explorer, > Asset Viewer, Picture Viewer; Desktop software: Microsoft Active Sync 3.1, > Microsoft Money for Pocket PC, Pocket Streets, Outlook 2000, Internet > Explorer 5.0, Media Manager, Tscribe, Microsoft Reader e-book samples > Width: 3.28 inches > Height: 0.62 inches > Depth: 5.11 inches > Weight: 6.3 ounces > Warranty, parts: 1 year > Warranty, labor: 1 year > > > > > Maybe - this is the monochrome - not color screen. > > > > Finn > > > > Donald Mei wrote: > > > > > > > > I just got this email from a "deals" oriented email list: > > > > > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and Mortar > > > OfficeDepot (i.e. the actual store, not the web site) This one is on > > > clearance at your local retail Office Depot store. They`re really > running > > > out of stock though, and they`re not getting any more in. The SKU# for > this > > > product is 858-251. Best of luck! > > > > ---------------------------------------------------- Sign Up for NetZero Platinum Today Only $9.95 per month! http://my.netzero.net/s/signup?r=platinum&refcd=PT97 ________________________________________________________________________________
From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com>
Subject: Compaq Ipaq Cheap for Anywhere map buyers
Date: Mar 07, 2002
Don Mei originally said that OfficeMax was selling the 3635 for that low price. 3635 is the color model, not the monochrome. I've never seen the monochrome model anywhere. Scott VanArtsdalen, MCSE, CCNA Network Administrator Union Safe Deposit Bank 209-946-5116 -----Original Message----- From: Finn Lassen [mailto:finnlassen(at)netzero.net] Subject: Re: RV-List: Compaq Ipaq Cheap for Anywhere map buyers Mike, why are you quoting specs on the Color model? The 3135 or 3035 is monochrome! That's why the much lower price. The screen! Finn Mike Plecenik wrote: > > >From Amazon.c: (they're still asking over $500. new & over $300. used) > > Standard memory: 32 MB RAM, 16 MB ROM > Maximum memory: Up to 64 MB with card > Expansion slot: CompactFlash > Display type: Color-reflective TFT LCD (indoor/outdoor) > Display colors: 4,096 (12-bit) > Display size: 2.26 by 3.02 inches > Resolution: 240 by 320 pixels > Display backlight: Yes, ambient-light sensor adjusts automatically > Processor: 206 MHz Intel StrongARM SA-1110 32-bit RISC > Operating system: Microsoft Windows for Pocket PCs > PC compatible: Yes > Mac compatible: No > PC system requirements: 486 MHz processor or higher, Windows 98 or 2000 for > USB synchronization, USB port, CD-ROM drive > Handwriting recognition: Yes > Keyboard: On-screen > User controls: On/off, light, menu, speaker/5-way joystick, contacts, > calendar > Memo pad: Yes > Address book: Yes > Scheduler: Yes > E-mail: Yes > Web browser: Yes > Security: Password protection > Stereo: Yes > Built-in speaker: Yes > Headset jack: Yes (3.5mm stereo) > Voice recorder: Yes > MP3 playback: Yes > Audible content playback: Yes > AC adapter included: Yes > Battery type: 950 mAh Lithium Polymer > Batteries included: Yes > Average battery life: 12 hours > Serial port: Yes, with optional Compaq serial cradle > USB: Yes > Infrared: Yes > Wireless: Yes > Docking cradle: USB cradle included > PC cable: Yes > Other hardware: Two styli, vinyl slipcase, AC adapter > Software: Pocket PC software: Pocket Word, Pocket Excel, Pocket Internet > Explorer, Windows Media Player, Inbox, Microsoft Reader, File Explorer, > Asset Viewer, Picture Viewer; Desktop software: Microsoft Active Sync 3.1, > Microsoft Money for Pocket PC, Pocket Streets, Outlook 2000, Internet > Explorer 5.0, Media Manager, Tscribe, Microsoft Reader e-book samples > Width: 3.28 inches > Height: 0.62 inches > Depth: 5.11 inches > Weight: 6.3 ounces > Warranty, parts: 1 year > Warranty, labor: 1 year > > > > > Maybe - this is the monochrome - not color screen. > > > > Finn > > > > Donald Mei wrote: > > > > > > > > I just got this email from a "deals" oriented email list: > > > > > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and Mortar > > > OfficeDepot (i.e. the actual store, not the web site) This one is on > > > clearance at your local retail Office Depot store. They`re really > running > > > out of stock though, and they`re not getting any more in. The SKU# for > this > > > product is 858-251. Best of luck! > > > > ---------------------------------------------------- Sign Up for NetZero Platinum Today Only $9.95 per month! http://my.netzero.net/s/signup?r=platinum&refcd=PT97 ________________________________________________________________________________
From: Gosh2Fly(at)aol.com
Date: Mar 07, 2002
Subject: Re: RV8-List: [Fwd: Magneto Swap]
________________________________________________________________________________
From: Gosh2Fly(at)aol.com
Date: Mar 07, 2002
Subject: Re: RV8-List: [Fwd: Magneto Swap]
jIM, I'am doing the same thing with a 0320-H2AD dual mag (D4RN-2021). It 's a harder problem than it appears to be. It will be a month or so to I can try this mag. It is a 1200 series mag (no part number ) right hand rotating mag with a shaft matched to the dual mag type. This was all done by a mag shop ( only mag. shop I could find that would help) Magneto E.R. (877)599-4859,Waylen Bruce. My advice is go with a dual electronic ignition with a battery backup. It's been done and Jeff Rose (Electroair) can do it. Ken ________________________________________________________________________________
From: "Bob Busick" <panamared1(at)brier.net>
Subject: Re: Plumbing Woes?!?
Date: Mar 07, 2002
You are correct, the plumbing is not designed to fit. I had Van's static system kit, by the time I finished fixing all of the leaks, there is nothing left on the plane from the original Van's kit. Not that his kit is bad, it just doesn't fit anything else in my system. I went to the local hardware store and bought about one of each of everything they had in plastic tubing and connectors, spices etc. Van's system leaked, hardware store system doesn't. Van's system does not fit connectors, hardware store does. I am sure someone has been able to make Van's system work, but not I. Bob > What I don't understand is why I can't make it work. > The back of the airspeed requires 1/8" threads with a > 1/4" barb to conect a hose that measures 1/4" ID which > I think is 3/8"OD. But a 3/8"OD will not work for the > T-Connectors that have 1/8" threads to screw into the > altimeter and have 1/4"OD connectors! > > And then theirs the vacuum connections that require > 1/4" threads with a 3/8" barb. Do you use plastic > lines? ________________________________________________________________________________
From: "Mike Plecenik" <nanchang(at)earthlink.net>
Subject: Re: Compaq Ipaq Cheap for Anywhere map buyers
Date: Mar 07, 2002
Because he said 3635. ----- Original Message ----- From: "Finn Lassen" <finnlassen(at)netzero.net> Subject: Re: RV-List: Compaq Ipaq Cheap for Anywhere map buyers > > Mike, why are you quoting specs on the Color model? The 3135 or 3035 is > monochrome! > > That's why the much lower price. The screen! > > Finn > > Mike Plecenik wrote: > > > > > >From Amazon.c: (they're still asking over $500. new & over $300. used) > > > > Standard memory: 32 MB RAM, 16 MB ROM > > Maximum memory: Up to 64 MB with card > > Expansion slot: CompactFlash > > Display type: Color-reflective TFT LCD (indoor/outdoor) > > Display colors: 4,096 (12-bit) > > Display size: 2.26 by 3.02 inches > > Resolution: 240 by 320 pixels > > Display backlight: Yes, ambient-light sensor adjusts automatically > > Processor: 206 MHz Intel StrongARM SA-1110 32-bit RISC > > Operating system: Microsoft Windows for Pocket PCs > > PC compatible: Yes > > Mac compatible: No > > PC system requirements: 486 MHz processor or higher, Windows 98 or 2000 for > > USB synchronization, USB port, CD-ROM drive > > Handwriting recognition: Yes > > Keyboard: On-screen > > User controls: On/off, light, menu, speaker/5-way joystick, contacts, > > calendar > > Memo pad: Yes > > Address book: Yes > > Scheduler: Yes > > E-mail: Yes > > Web browser: Yes > > Security: Password protection > > Stereo: Yes > > Built-in speaker: Yes > > Headset jack: Yes (3.5mm stereo) > > Voice recorder: Yes > > MP3 playback: Yes > > Audible content playback: Yes > > AC adapter included: Yes > > Battery type: 950 mAh Lithium Polymer > > Batteries included: Yes > > Average battery life: 12 hours > > Serial port: Yes, with optional Compaq serial cradle > > USB: Yes > > Infrared: Yes > > Wireless: Yes > > Docking cradle: USB cradle included > > PC cable: Yes > > Other hardware: Two styli, vinyl slipcase, AC adapter > > Software: Pocket PC software: Pocket Word, Pocket Excel, Pocket Internet > > Explorer, Windows Media Player, Inbox, Microsoft Reader, File Explorer, > > Asset Viewer, Picture Viewer; Desktop software: Microsoft Active Sync 3.1, > > Microsoft Money for Pocket PC, Pocket Streets, Outlook 2000, Internet > > Explorer 5.0, Media Manager, Tscribe, Microsoft Reader e-book samples > > Width: 3.28 inches > > Height: 0.62 inches > > Depth: 5.11 inches > > Weight: 6.3 ounces > > Warranty, parts: 1 year > > Warranty, labor: 1 year > > > > > > > > Maybe - this is the monochrome - not color screen. > > > > > > Finn > > > > > > Donald Mei wrote: > > > > > > > > > > > I just got this email from a "deals" oriented email list: > > > > > > > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and Mortar > > > > OfficeDepot (i.e. the actual store, not the web site) This one is on > > > > clearance at your local retail Office Depot store. They`re really > > running > > > > out of stock though, and they`re not getting any more in. The SKU# for > > this > > > > product is 858-251. Best of luck! > > > > > > > > ---------------------------------------------------- > Sign Up for NetZero Platinum Today > Only $9.95 per month! > http://my.netzero.net/s/signup?r=platinum&refcd=PT97 > > ________________________________________________________________________________
Date: Mar 07, 2002
From: "Owens, Laird" <Owens(at)aerovironment.com>
Subject: Static pickup for RV6
David, The pressure in the cabin is different then the static source outside, and would give you incorrect altitude indications if only sensing inside pressure. The other people flying in the system (be it IFR or VFR) expect you to be at the altitude your supposed to be at. I know I would appreciate it in case we ever fly near each other (althought I don't plan any trips to the UAE in my RV anytime soon). I'd recommend plumbing like Vans recommends. It's simple and adds very little weight. Regards, Laird 440 hrs RV-6 SoCal From: rv-list(at)matronics.com on Thu, Mar 7, 2002 10:23 AM Subject: RV-List: Static pickup for RV6 Listers, Van's sells a static port kit for the RV6, how essential is this? I only intend to fly VFR and therefore is a pickup in the cockpit sufficient? Your thoughts, experience and advise. David Roseblade RV6 Finishing kit Dubai, UAE ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: Static pickup for RV6
Date: Mar 07, 2002
It's easy to install, and cheap. Good insurance for an accurate altimiter and airspeed, even if you are flying VFR. (So do I). Personally, I like the Cleveland kit much better. Paul Besing RV-6A N197AB Arizona http://www.lacodeworks.com/besing First Flight 22 July 01 Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "David Roseblade" <davidagr(at)emirates.net.ae> Subject: RV-List: Static pickup for RV6 > > Listers, > > Van's sells a static port kit for the RV6, how essential is this? I only > intend to fly VFR and therefore is a pickup in the cockpit sufficient? > > Your thoughts, experience and advise. > > David Roseblade > RV6 Finishing kit > Dubai, UAE > > ________________________________________________________________________________
Date: Mar 07, 2002
From: Kevin Horton <khorton(at)cyberus.ca>
Subject: Static pickup for RV6
There is another down side to an in-cabin static port. The cabin pressure will change as you change the amount of outside air coming into or leaving the cabin. So if you open or close a vent, or change the setting of the cabin heat box, you'll affect the sensed static pressure. Most people seem to only think this is an issue with the altimeter, but the airspeed indicator uses static pressure too. So, if you want a consistent indicated airspeed for any given flight condition (e.g. at the stall), you need a consistent static pressure source. Granted, the errors in static pressure will be smaller at low speed, but it still seems like a good idea to have a static source that gives a consistent static pressure. Kevin Horton RV-8 (installing engine & electrics) Ottawa, Canada http://eccentrix.com/misc/rv8/rv8.html > >David, > >The pressure in the cabin is different then the static source >outside, and would give you incorrect altitude indications if only >sensing inside pressure. > >The other people flying in the system (be it IFR or VFR) expect you >to be at the altitude your supposed to be at. I know I would >appreciate it in case we ever fly near each other (althought I don't >plan any trips to the UAE in my RV anytime soon). > >I'd recommend plumbing like Vans recommends. It's simple and adds >very little weight. > >Regards, > >Laird 440 hrs >RV-6 SoCal >From: rv-list(at)matronics.com on Thu, Mar 7, 2002 10:23 AM >Subject: RV-List: Static pickup for RV6 >To: RV List > > >Listers, > >Van's sells a static port kit for the RV6, how essential is this? I only >intend to fly VFR and therefore is a pickup in the cockpit sufficient? > >Your thoughts, experience and advise. > >David Roseblade >RV6 Finishing kit >Dubai, UAE ________________________________________________________________________________
Date: Mar 07, 2002
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: Compaq Ipaq Cheap for Anywhere map buyers
If you want one, run, don't walk, to the phone & start calling Office Depots til you find one. It's the 3650 bundled with the 'cf' sleeve. I just bought the last one here in my hometown. Of course, it will be worth about $50 in 6 months when the 3rd generation models are released. :-) Finn Lassen wrote: > > > Mike, why are you quoting specs on the Color model? The 3135 or 3035 is > monochrome! > > That's why the much lower price. The screen! > > Finn > > Mike Plecenik wrote: > > > > > >From Amazon.c: (they're still asking over $500. new & over $300. used) > > > > Standard memory: 32 MB RAM, 16 MB ROM > > Maximum memory: Up to 64 MB with card > > Expansion slot: CompactFlash > > Display type: Color-reflective TFT LCD (indoor/outdoor) > > Display colors: 4,096 (12-bit) > > Display size: 2.26 by 3.02 inches > > Resolution: 240 by 320 pixels > > Display backlight: Yes, ambient-light sensor adjusts automatically > > Processor: 206 MHz Intel StrongARM SA-1110 32-bit RISC > > Operating system: Microsoft Windows for Pocket PCs > > PC compatible: Yes > > Mac compatible: No > > PC system requirements: 486 MHz processor or higher, Windows 98 or 2000 for > > USB synchronization, USB port, CD-ROM drive > > Handwriting recognition: Yes > > Keyboard: On-screen > > User controls: On/off, light, menu, speaker/5-way joystick, contacts, > > calendar > > Memo pad: Yes > > Address book: Yes > > Scheduler: Yes > > E-mail: Yes > > Web browser: Yes > > Security: Password protection > > Stereo: Yes > > Built-in speaker: Yes > > Headset jack: Yes (3.5mm stereo) > > Voice recorder: Yes > > MP3 playback: Yes > > Audible content playback: Yes > > AC adapter included: Yes > > Battery type: 950 mAh Lithium Polymer > > Batteries included: Yes > > Average battery life: 12 hours > > Serial port: Yes, with optional Compaq serial cradle > > USB: Yes > > Infrared: Yes > > Wireless: Yes > > Docking cradle: USB cradle included > > PC cable: Yes > > Other hardware: Two styli, vinyl slipcase, AC adapter > > Software: Pocket PC software: Pocket Word, Pocket Excel, Pocket Internet > > Explorer, Windows Media Player, Inbox, Microsoft Reader, File Explorer, > > Asset Viewer, Picture Viewer; Desktop software: Microsoft Active Sync 3.1, > > Microsoft Money for Pocket PC, Pocket Streets, Outlook 2000, Internet > > Explorer 5.0, Media Manager, Tscribe, Microsoft Reader e-book samples > > Width: 3.28 inches > > Height: 0.62 inches > > Depth: 5.11 inches > > Weight: 6.3 ounces > > Warranty, parts: 1 year > > Warranty, labor: 1 year > > > > > > > > Maybe - this is the monochrome - not color screen. > > > > > > Finn > > > > > > Donald Mei wrote: > > > > > > > > > > > I just got this email from a "deals" oriented email list: > > > > > > > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and Mortar > > > > OfficeDepot (i.e. the actual store, not the web site) This one is on > > > > clearance at your local retail Office Depot store. They`re really > > running > > > > out of stock though, and they`re not getting any more in. The SKU# for > > this > > > > product is 858-251. Best of luck! > > > > > > ________________________________________________________________________________
From: "Gordon or Marge Comfort" <gcomfo(at)tc3net.com>
Subject: Re: Plumbing Woes?!?
Date: Mar 07, 2002
----- Original Message ----- From: "Dan DeNeal" <rv6apilot(at)yahoo.com> Subject: RV-List: Plumbing Woes?!? > What I don't understand is why I can't make it work. > Dan DeNeal Dan: The nature of your difficulty is not quite clear to me but here are some things to consider: Most of the pitot/static instruments have 1/8" tapered pipe threads for their taps so several types of fittings may be used. Plastic fittings (thread to barb) are available and can work well with clear plastic tubing. To reduce the chance of leaks, the fittings should be of good quality and without flash or offset at the mold parting line. Tubing should have a smooth ID. Some tubing seems to have been extruded with worn dies so that there are longitudinal ridges either inside or out. To further minimise the chance of leaks an application of contact cement to the barb or threads can be applied and assembled wet, taking care not to place the cement where it can intrude into the airways. If instrument ports are so close together as to preclude elbow or tee fittings, a straight fitting and a freestanding tee or elbow may be used. When faced with the need to adapt from one diameter to another it is possible to find tubing that will insert snugly into a larger diameter and with the contact cement and a tie wrap or two you can have the security and the leak resistance you need. On my -4, I used a low pressure rubber hose from the vacuum pump to the regulator, only because of the heat behind the engine. All the rest was clear plastic tubing. The above applies to the larger fittings used with suction instruments too, if you have them. This is one way to do it (not the only way). Gordon Comfort N363GC ________________________________________________________________________________
Date: Mar 07, 2002
From: Bobby Hester <bhester(at)apex.net>
Subject: Re: IE capacitive fuel sender system
Jerry Calvert wrote: > > The converter module has a little ring terminal on each of the two wires. > EI has a capacitance sender unit that these work with. There are two tiny > screws that attach the two terminals. The designer of Van's senders came up > with a BNC type connection instead. So the little ring terminals are > snipped off (unless one has devised a way to hook up the BNC by using the > ring terminals). > > What I did was to cut off the ring terminals. Attach a piece of coax(about > 2 1/2" long) to the mating BNC connecter as you normally would. Strip the > insulation off for about an inch down to the shield and unwravel the shield > and then twist it back together to make a pigtail. One of the converter > wires attaches to the pigtail. Take off more insulation off down to the > center conductor. The other converter wire attaches to the center > conductor. I used butt splices on both wires. I used shrink wrap on the > center connection and then larger shrink wrap over the whole mess to add > protection. The BNC coax exits out of one end of the shrinkwrap and the > long wires that connect to the guage exit out the other. > > There may be other ways to connect, but I like this the best. I know you > are already thinking about which wire attaches to the center conductor. The > answer is, it doesn't matter! Thanks for the details! That will help a lot. -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
From: "Jim Bower" <rvbuilder(at)hotmail.com>
Subject: Re: Pro Seal & Fuel Lube
Date: Mar 08, 2002
John, I have used both ProSeal (the kind with two separate containers), and the B2 sealant, both from Aircraft Spruce. I mostly used the B2 on my tanks because it really was easier and less messy. You don't want to get that for small jobs, because once you mix it up in the tube, it's a done deal...you have to use it up or you've wasted it. I highly recommend you buy the smallest kit of Proseal you can get and keep it in a cool place. That stuff comes in real handy for lots of things. If you've watched George Orndorff's videos, he uses it for things like gluing the NACA air vents onto the fuselage sides. Proseal has a shelf life, but from what I've heard, when it gets old it just takes longer to set up. You won't be using it for anything really critical like your tanks anyhow. Go for it. Jim Bower RV-6A Wings (almost done) Send and receive Hotmail on your mobile device: http://mobile.msn.com ________________________________________________________________________________
From: "David Deffner" <deffner(at)glade.net>
Subject: canopy
Date: Mar 07, 2002
Could one you guys with a tilt up canopy on an RV6 measure the length from the front at base of windshield to the aft point of canopy. I would sure appreciate it. I am wanting to put a 6 canopy on my Emeraude with a raised turtle deck, which appears to be a little higher than the 6. Thanks, David ________________________________________________________________________________
Date: Mar 07, 2002
From: Finn Lassen <finnlassen(at)netzero.net>
Subject: Re: Compaq Ipaq Cheap for Anywhere map buyers
My sincere apologies. Sounds too incredible to be true. Especially as it lists on the Office Depot website (under same SKU#) at $599.99. Finn "Van Artsdalen, Scott" wrote: > > Don Mei originally said that OfficeMax was selling the 3635 for that low > price. 3635 is the color model, not the monochrome. I've never seen the > monochrome model anywhere. > > Scott VanArtsdalen, MCSE, CCNA > Network Administrator > Union Safe Deposit Bank > 209-946-5116 > > -----Original Message----- > From: Finn Lassen [mailto:finnlassen(at)netzero.net] > Sent: Thursday, March 07, 2002 10:09 AM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Compaq Ipaq Cheap for Anywhere map buyers > > > Mike, why are you quoting specs on the Color model? The 3135 or 3035 is > monochrome! > > That's why the much lower price. The screen! > > Finn > > Mike Plecenik wrote: > > > > > >From Amazon.c: (they're still asking over $500. new & over $300. used) > > > > Standard memory: 32 MB RAM, 16 MB ROM > > Maximum memory: Up to 64 MB with card > > Expansion slot: CompactFlash > > Display type: Color-reflective TFT LCD (indoor/outdoor) > > Display colors: 4,096 (12-bit) > > Display size: 2.26 by 3.02 inches > > Resolution: 240 by 320 pixels > > Display backlight: Yes, ambient-light sensor adjusts automatically > > Processor: 206 MHz Intel StrongARM SA-1110 32-bit RISC > > Operating system: Microsoft Windows for Pocket PCs > > PC compatible: Yes > > Mac compatible: No > > PC system requirements: 486 MHz processor or higher, Windows 98 or 2000 > for > > USB synchronization, USB port, CD-ROM drive > > Handwriting recognition: Yes > > Keyboard: On-screen > > User controls: On/off, light, menu, speaker/5-way joystick, contacts, > > calendar > > Memo pad: Yes > > Address book: Yes > > Scheduler: Yes > > E-mail: Yes > > Web browser: Yes > > Security: Password protection > > Stereo: Yes > > Built-in speaker: Yes > > Headset jack: Yes (3.5mm stereo) > > Voice recorder: Yes > > MP3 playback: Yes > > Audible content playback: Yes > > AC adapter included: Yes > > Battery type: 950 mAh Lithium Polymer > > Batteries included: Yes > > Average battery life: 12 hours > > Serial port: Yes, with optional Compaq serial cradle > > USB: Yes > > Infrared: Yes > > Wireless: Yes > > Docking cradle: USB cradle included > > PC cable: Yes > > Other hardware: Two styli, vinyl slipcase, AC adapter > > Software: Pocket PC software: Pocket Word, Pocket Excel, Pocket Internet > > Explorer, Windows Media Player, Inbox, Microsoft Reader, File Explorer, > > Asset Viewer, Picture Viewer; Desktop software: Microsoft Active Sync 3.1, > > Microsoft Money for Pocket PC, Pocket Streets, Outlook 2000, Internet > > Explorer 5.0, Media Manager, Tscribe, Microsoft Reader e-book samples > > Width: 3.28 inches > > Height: 0.62 inches > > Depth: 5.11 inches > > Weight: 6.3 ounces > > Warranty, parts: 1 year > > Warranty, labor: 1 year > > > > > > > > Maybe - this is the monochrome - not color screen. > > > > > > Finn > > > > > > Donald Mei wrote: > > > > > > > > > > > I just got this email from a "deals" oriented email list: > > > > > > > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and > Mortar > > > > OfficeDepot (i.e. the actual store, not the web site) This one is on > > > > clearance at your local retail Office Depot store. They`re really > > running > > > > out of stock though, and they`re not getting any more in. The SKU# > for > > this > > > > product is 858-251. Best of luck! > > > > > > > > ---------------------------------------------------- > Sign Up for NetZero Platinum Today > Only $9.95 per month! > http://my.netzero.net/s/signup?r=platinum&refcd=PT97 > ________________________________________________________________________________
Date: Mar 08, 2002
Subject: nosewheel fork
From: czechsix(at)juno.com
Training wheel guys, What type of grease / lubricant are you guys using where the nosewheel fork pivots on the nosegear leg? There's a zerk fitting but I don't see a callout for specific grease type. Would the Aeroshell #5 grease used for the wheel bearings work well for the nosewheel fork too? Also, does the fork need to be primed (ohmygosh, did I ask a *primer* question?). It's cold outside and I'm feeling lazy and don't want to prime anything right now.... --Mark Navratil Cedar Rapids, Iowa RV-8A finish kit stuff..... ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: nosewheel fork
Date: Mar 08, 2002
Mark, Shame on you for asking that pri**er question! Your punishment is that you now must Alumiprep Alodine and Pri**er your nose wheel fork. While your at it, be sure to use the most difficult and time consuming type of Pri**er sealer the industry has to offer. If it's really hard to use it's bound to be better, isn't it? Well at least that's what someone told me. {:-)!! I considered the environment that the fork will live and work in and epoxy pri**er sealed mine. For that same reason I will also paint it and the various parts including the wheel even though it will all be out of sight. I have not yet found the answer to lubing the fork. Jump in lister's what's best to use. Who knows Mark? maybe You have hit on another one of those entertaining topics that come to the surface from time to time here on the list. :) ! Keep up the good work, Jim in Kelowna (it's late) ----- Original Message ----- From: <czechsix(at)juno.com> Subject: RV-List: nosewheel fork > > Training wheel guys, > > What type of grease / lubricant are you guys using where the nosewheel > fork pivots on the nosegear leg? There's a zerk fitting but I don't see > a callout for specific grease type. Would the Aeroshell #5 grease used > for the wheel bearings work well for the nosewheel fork too? > > Also, does the fork need to be primed (ohmygosh, did I ask a *primer* > question?). It's cold outside and I'm feeling lazy and don't want to > prime anything right now.... > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A finish kit stuff..... > > ________________________________________________________________________________
From: "Jack Textor" <jack(at)IaJobs.com>
Subject: Torque Wrench Info
Date: Mar 08, 2002
Wanted the group to know the 1/4" 0-200 inch pound torque wrench I purchased from JC Whitney just passed a certification. The tolerance was 4%. Mine was within 1/4 of a percent. I was pleasantly surprised. Jack RV8, wings DSM ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: RV-6A upper gear leg fairings
Date: Mar 08, 2002
All you RV-6A builders ... I have upper gear leg fairings, but can't figure out how to hold them in place. I don't think that drilling holes in my fuel tanks for screws is a good idea. The plane is flying, so access to the fuselage isn't great. I saw somewhere once that these upper fairings could be held in place by using springs, but I can't see how that would work. Any ideas out there? Steve Soule Huntington, Vermont N227RV ________________________________________________________________________________
From: "Bob Waalkes" <waalkes(at)netnitco.net>
Subject: RV-4 Sale
Date: Mar 08, 2002
For Sale: RV-4 Project Wings Complete Tail Complete Control Surfaces Complete Fuse Bulkheads Complete Parts: Remainder of Fuse (ready to go into jig) Cowl Engine Mount Canopy Some Instruments Complete & Updated Manuals Videos Must Sell - New Baby..... $6,500 Bob Waalkes Fas-Pak, Inc. 411 Fairfield Ave. Michigan City, IN 46360 Phone: 219-874-7990 Phone: 888-247-9937 Fax: 219-874-7991 Email: waalkes(at)netnitco.net ________________________________________________________________________________
Date: Mar 08, 2002
Subject: Re: nose wheel fork
From: Denis Walsh <deniswalsh(at)earthlink.net>
Mark, There have been several reports over the years of "over lubricating" this item. Apparently the excess grease will ooze down onto the friction washers and give you the permanent shakes on landing roll out. Based on those reports, I have never used the zerk. Rather I slather a little #5 on the rubbing surfaces and on the leg at each annual or other removal. This has worked for me so far. On the other matter, I too felt lazy and had a case of primer burn out, just as you do now. My fork is unpainted. It now looks like crap. I highly recommend you not only prime it, but give it a real serious coat of two part epoxy primer and finish coat. That puppy is your lead dog into all the slush rain, mud, snow and crud you will ever go in to. Not only that, it has a nice wheel pant to keep it moist. Denis > From: czechsix(at)juno.com > Reply-To: rv-list(at)matronics.com > Date: Fri, 8 Mar 2002 02:11:43 -0600 > To: rv-list(at)matronics.com > Subject: RV-List: nosewheel fork > > > Training wheel guys, > > What type of grease / lubricant are you guys using where the nosewheel > fork pivots on the nosegear leg? There's a zerk fitting but I don't see > a callout for specific grease type. Would the Aeroshell #5 grease used > for the wheel bearings work well for the nosewheel fork too? > > Also, does the fork need to be primed (ohmygosh, did I ask a *primer* > question?). It's cold outside and I'm feeling lazy and don't want to > prime anything right now.... > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A finish kit stuff..... > > > > > > ________________________________________________________________________________
Date: Mar 08, 2002
Subject: Re: RV-6A upper gear leg fairings
From: Denis Walsh <deniswalsh(at)earthlink.net>
I had the same reservation about the fuel tank, and also avoided going into the main spar. The springs work good for the 6, not so easy on 6A. I used a couple of riv nuts where it was too tough to get to the other side for a plate nut. Also one plate nut in the wing fairing as I recall. Two or three screws seems to be enough. DLW > From: "Stephen J. Soule" <SSoule(at)pfclaw.com> > Reply-To: rv-list(at)matronics.com > Date: Fri, 8 Mar 2002 09:44:06 -0500 > To: "Rv-List (E-mail)" > Subject: RV-List: RV-6A upper gear leg fairings > > > All you RV-6A builders ... > > I have upper gear leg fairings, but can't figure out how to hold them in > place. I don't think that drilling holes in my fuel tanks for screws is a > good idea. The plane is flying, so access to the fuselage isn't great. I saw > somewhere once that these upper fairings could be held in place by using > springs, but I can't see how that would work. Any ideas out there? > > Steve Soule > Huntington, Vermont > N227RV > > > > > > ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: RV-6A upper gear leg fairings
Date: Mar 08, 2002
Pop rivets work great on a finished airplane. There shouldn't be any reason that you would need to take them off. Paul Besing RV-6A N197AB Arizona http://www.lacodeworks.com/besing First Flight 22 July 01 Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "Stephen J. Soule" <SSoule(at)pfclaw.com> Subject: RV-List: RV-6A upper gear leg fairings > > All you RV-6A builders ... > > I have upper gear leg fairings, but can't figure out how to hold them in > place. I don't think that drilling holes in my fuel tanks for screws is a > good idea. The plane is flying, so access to the fuselage isn't great. I saw > somewhere once that these upper fairings could be held in place by using > springs, but I can't see how that would work. Any ideas out there? > > Steve Soule > Huntington, Vermont > N227RV > > ________________________________________________________________________________
Date: Mar 08, 2002
From: "Gary Zilik" <zilik(at)bewellnet.com>
Subject: Re: RV-6A upper gear leg fairings
Steve, I used #6 screws into the belly skins. One in the front into the belly skin, one center inside through the belly skin and the third ouside rear into the belly skin/outside seat rib. The forward belly is thick enough to tap for the #6 screws. The rear attach is only the .032 skin so I made sure I had the outside seat rib also, this made .063 thickness(same as front belly skin) and tapped well. The inside center one went into the overlap the belly skins which is .063+.032, plenty thick. I figure if they ever strip out I can use rivnuts in place of the tapped hole. So far so good with 300 hrs. Use a manual screw driver to install the screws and just snug them up, I have never found them loose. I also countersunk the fairing and am not using any of the SS countersunk washers. Gary "Stephen J. Soule" wrote: > > > All you RV-6A builders ... > > I have upper gear leg fairings, but can't figure out how to hold them in > place. I don't think that drilling holes in my fuel tanks for screws is a > good idea. The plane is flying, so access to the fuselage isn't great. I saw > somewhere once that these upper fairings could be held in place by using > springs, but I can't see how that would work. Any ideas out there? > > Steve Soule > Huntington, Vermont > N227RV > ________________________________________________________________________________
Date: Mar 08, 2002
From: "Gary Zilik" <zilik(at)bewellnet.com>
Subject: Re: RV-6A upper gear leg fairings
The upper tang on my fairing broke so I had to remove the fairing for fixing. In my case the cuff has to be removed to remove the fairing. Granted pop rivets are easy to drill out but screws are easier. Gary Paul Besing wrote: > > > Pop rivets work great on a finished airplane. There shouldn't be any reason > that you would need to take them off. > > Paul Besing > RV-6A N197AB Arizona > http://www.lacodeworks.com/besing > First Flight 22 July 01 > Kitlog Pro Builder's Log Software > http://www.kitlog.com > > ----- Original Message ----- > From: "Stephen J. Soule" <SSoule(at)pfclaw.com> > To: "Rv-List (E-mail)" > Subject: RV-List: RV-6A upper gear leg fairings > > > > > All you RV-6A builders ... > > > > I have upper gear leg fairings, but can't figure out how to hold them in > > place. I don't think that drilling holes in my fuel tanks for screws is a > > good idea. The plane is flying, so access to the fuselage isn't great. I > saw > > somewhere once that these upper fairings could be held in place by using > > springs, but I can't see how that would work. Any ideas out there? > > > > Steve Soule > > Huntington, Vermont > > N227RV > > > > > ________________________________________________________________________________
Date: Mar 08, 2002
From: Larry Bowen <lcbowen(at)yahoo.com>
Subject: Re: Torque Wrench Info
Where is you take it to be certified? -Larry --- Jack Textor wrote: > > Wanted the group to know the 1/4" 0-200 inch pound torque wrench I purchased > from JC Whitney just passed a certification. The tolerance was 4%. Mine > was within 1/4 of a percent. I was pleasantly surprised. > Jack > RV8, wings > DSM > > > > > > > > ________________________________________________________________________________
From: "David Carter" <dcarter(at)datarecall.net>
Subject: RV-6 tip-up canopy - roll bar's F-632 length
Date: Mar 08, 2002
Looked in RV-list and RV-6 list archives - didn't find info on my problem, so request input of the list: I've built my roll bar assembly (F-631/632 brace) and have it sitting on fuelage, cleco'd thru top skin rivet holes into F-632 brace so it is flush with F-606 baggage wall/bulkhead (replaced interfering round head rivets in bulkhead with flush rivets and drilled recesses in top of shim and aft angle for top skin rivets and dimples to recess into). Problem: The fwd edge of roll bar is now 3/4 inch fwd of the fwd edge of the seat back brace. - Called and talked to Gus at Van's today to confirm that position is OK - it is not. He said front of roll bar has to be flush with front of seat back brace - so have to cut 3/4 inch off back of F-632 and re-drill aft angle and 2 little side angles. Gus promised he'd ask for a change to builder's manual to tell where the two ends of the roll bar are to be positioned, and put a note on Dwg 39 to reference Dwg 51 which shows roll bar aligned with the vertical side longeron that canopy latch is fastened to, which is his basis for saying roll cage and seat back should be aligned.) - I just exchanged a private e-mail with a builder who was at this point 10 months ago and he said he didn't have this problem. Anyone else have this same "F-632 is 3/4 inch too long" problem? - ( Gus said they've never had a builder report such a thing before. That's what they say every time I bring up a problem. Then I put it on the list and "everyone" says, "Yeah, I had that.") David Carter Nederland, Texas RV-6 QB 409-722-7259 ________________________________________________________________________________
From: "Jack Textor" <jack(at)IaJobs.com>
Subject: Torque Wrench Info
Date: Mar 08, 2002
Larry, A pilot/A&P friend sent it to Utah. I will get the specifics for the list. I have also had the Ia Air Guard check them in the past; they didn't charge me a thing. Jack Subject: Re: RV-List: Torque Wrench Info Where is you take it to be certified? -Larry > Wanted the group to know the 1/4" 0-200 inch pound torque wrench I purchased > from JC Whitney just passed a certification. The tolerance was 4%. Mine > was within 1/4 of a percent. I was pleasantly surprised. > Jack > RV8, wings > DSM ________________________________________________________________________________
Subject: Cessna wrinkle paint
Date: Mar 08, 2002
From: "Bob Japundza" <Bob.Japundza(at)realmed.com>
Hi Folks, Could anyone tell me a where I can get the grey wrinkle paint that Cessna uses on the panels of their new 172/182/206's? I'm sure it'd be three times the cost if I ordered it from Cessna. Bob Japundza RV-6 N244BJ O-360CS flying 275 hours building F1 ________________________________________________________________________________
Date: Mar 08, 2002
Subject: RV-6 tip-up canopy - roll bar's F-632 length
From: Don Jordan <dons6a(at)juno.com>
Dave: drw 32 shows it lines up with the 605. drwg 26 shows you put the 605G angle in there to carry the load of the 2- an 4 bolts ( drwg 39) later. They hold the two feeties to the 605. The tillt is called out I think about 2 7/8ths from the vertical. Now you can fix the length of the 632 brace. Note they ask for .032 shim under the skin. You got to fit the thickness of the plexi in there. You may want to lower that also. Will pointed this out & I think I used .040 & I was too close. Plan out your final rivet sequence in that area & GET THE PLASTIC OFF THE INSIDE before you nail the pllexi down. I like too never got that off. Don Jordan - N6DJ - 6A Arlington, Tx ****************************** writes: > > > Looked in RV-list and RV-6 list archives - didn't find info on my > problem, > so request input of the list: > > I've built my roll bar assembly (F-631/632 brace) and have it > sitting on > fuelage, cleco'd > thru top skin rivet holes into F-632 brace so it is flush with F-606 > baggage > wall/bulkhead (replaced interfering round head rivets in bulkhead > with flush > rivets and drilled recesses in top of shim and aft angle for top > skin rivets > and dimples to recess into). > > Problem: The fwd edge of roll bar is now 3/4 inch fwd of the fwd > edge of > the seat back > brace. > - Called and talked to Gus at Van's today to confirm that > position is > OK - it is not. He said front of roll bar has to be flush with > front of > seat back brace - so have to cut 3/4 inch off back of F-632 > and re-drill aft angle and 2 little side angles. Gus promised he'd > ask for > a change to builder's manual to tell where the two ends of the roll > bar are > to be positioned, and put a note on Dwg 39 to reference Dwg 51 which > shows > roll bar aligned with the vertical side longeron that canopy latch > is > fastened to, which is his basis for saying roll cage and seat back > should be > aligned.) > - I just exchanged a private e-mail with a builder who was at > this > point 10 months ago and he said he didn't have this problem. > > Anyone else have this same "F-632 is 3/4 inch too long" problem? > - ( Gus said they've never had a builder report such a thing > before. > That's what they say every time I bring up a problem. Then I put it > on the > list and "everyone" says, "Yeah, I had that.") > > David Carter > Nederland, Texas > RV-6 QB > 409-722-7259 > > ________________________________________________________________________________
From: "Bob Busick" <panamared1(at)brier.net>
Subject: Re: Gross Weight Determinations
Date: Mar 08, 2002
I checked the archives and I have seen that some people have set RV6/A gross weights at 1800-1950 lbs. Also it has been stated numerous times that the builder/manufacturer sets the gross weight. However, my FAA inspector when he saw my gross weight of 1800 he told me that I had to document from Vans the designed gross weight. I told him that it was 1600/1650 and he told me that he would only approve an 1800 gross weight if Van would put that in writing. Assuming that Van will not put this in writing, how do I get around this. I don't need an 1800 gross weight, but, it would be nice if I need it. Bob ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Gross Weight Determinations
Date: Mar 08, 2002
I think your inspector is wrong. That is why it is called an experimental. Cy Galley Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org ----- Original Message ----- From: "Bob Busick" <panamared1(at)brier.net> Subject: Re: RV-List: Gross Weight Determinations I checked the archives and I have seen that some people have set RV6/A gross weights at 1800-1950 lbs. Also it has been stated numerous times that the builder/manufacturer sets the gross weight. However, my FAA inspector when he saw my gross weight of 1800 he told me that I had to document from Vans the designed gross weight. I told him that it was 1600/1650 and he told me that he would only approve an 1800 gross weight if Van would put that in writing. Assuming that Van will not put this in writing, how do I get around this. I don't need an 1800 gross weight, but, it would be nice if I need it. Bob ________________________________________________________________________________
Date: Mar 08, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Gross Weight Determinations
Bob, you need to somehow explain to the misinformed DAR that you, not Vans, are the manufacturer of the airplane; as the manufacturer, you can set the GW anywhere you wish! What kind of gross weight would he require if you had substituted rocket wings for Vans wings, or used a Mustang II tail section, or...gasp....used a Subaru engine that Vans doesn't endorse?? If he balks at this, show him the registration application where you indicated the plane is a "Busick RV-6A". If he still balks......get a DAR that knows what he is doing......and let all the local builders know to avoid this turkey. Or.....do the paperwork for 1600.......and fly the plane at whatever weight you wish. ;-) Sam Buchanan (RV-6, been flown at 1600, been flown at 1675, been flown at 1725.......) "The RV Journal" http://thervjournal.com ===================== Bob Busick wrote: > > > I checked the archives and I have seen that some people have set RV6/A gross > weights at 1800-1950 lbs. Also it has been stated numerous times that the > builder/manufacturer sets the gross weight. > > However, my FAA inspector when he saw my gross weight of 1800 he told me > that I had to document from Vans the designed gross weight. I told him that > it was 1600/1650 and he told me that he would only approve an 1800 gross > weight if Van would put that in writing. > > Assuming that Van will not put this in writing, how do I get around this. > I don't need an 1800 gross weight, but, it would be nice if I need it. > > Bob > > _ ________________________________________________________________________________
From: "John Warren" <jwdub(at)teleport.com>
Subject: Gross Weight Determinations
Date: Mar 08, 2002
Van's manuals indicate a "recommended" gross weight because it is determined by the builder. However, don't forget that as the gross weight goes up the allowable G's goes down and whatever extra margin is built in for the landing gear and motor mount will be reduced as well. John Warren RV 6 N645W LaCenter WA ________________________________________________________________________________
From: "Garth Shearing" <garth(at)Islandnet.com>
Subject: Re: Gross Weight Determinations
Date: Mar 08, 2002
I'm in Canada where the regs a a little different, but if in the U.S. you can change the gross weight to anything, why is there a need for an inspection at all? Garth Shearing VariEze and 80% RV6A Victoria BC Canada | Bob, you need to somehow explain to the misinformed DAR that you, not | Vans, are the manufacturer of the airplane; as the manufacturer, you can | set the GW anywhere you wish! What kind of gross weight would he require | if you had substituted rocket wings for Vans wings, or used a Mustang II | tail section, or...gasp....used a Subaru engine that Vans doesn't | endorse?? | ________________________________________________________________________________
From: "Tom Gummo" <t.gummo(at)verizon.net>
Subject: Re: Cessna wrinkle paint
Date: Mar 08, 2002
I found a grey wrinkle paint at a auto paint store. Then painted it black. :-) Tom Apple Valley, CA ----- Original Message ----- From: "Bob Japundza" <Bob.Japundza(at)realmed.com> Subject: RV-List: Cessna wrinkle paint > > Hi Folks, > > Could anyone tell me a where I can get the grey wrinkle paint that > Cessna uses on the panels of their new 172/182/206's? I'm sure it'd be > three times the cost if I ordered it from Cessna. > > Bob Japundza > RV-6 N244BJ O-360CS flying 275 hours > building F1 > > > > > > ________________________________________________________________________________
From: ABAYMAN(at)aol.com
Date: Mar 08, 2002
Subject: Re: RV-6 interoir blank
listers if interested in color coordinating your interior before you do it by trail and error, you can copy this picture , paste into paint, and have a ball trying to decide what your interior will look like. go to the link below. its in the yahoo photo gallary under Scott R RV6 INT. i tried to make it look as real as i could. enjoy scott tampa http://photos.groups.yahoo.com/group/vansairforce/lst?& .dir=/Scott+Reviere%27RV-6A/RV6A+interior+blank&.src=gr&.view=t&.last=1 ________________________________________________________________________________
From: "Tom Gummo" <t.gummo(at)verizon.net>
Subject: Re: Gross Weight Determinations
Date: Mar 08, 2002
Pass his/her name to the EAA. They have a program to work with DARs. I am sure he is mistaken. You can set any thing you want. Tom Gummo Apple Valley, Ca ----- Original Message ----- From: "Bob Busick" <panamared1(at)brier.net> Subject: Re: RV-List: Gross Weight Determinations > > I checked the archives and I have seen that some people have set RV6/A gross > weights at 1800-1950 lbs. Also it has been stated numerous times that the > builder/manufacturer sets the gross weight. > > However, my FAA inspector when he saw my gross weight of 1800 he told me > that I had to document from Vans the designed gross weight. I told him that > it was 1600/1650 and he told me that he would only approve an 1800 gross > weight if Van would put that in writing. > > Assuming that Van will not put this in writing, how do I get around this. > I don't need an 1800 gross weight, but, it would be nice if I need it. > > Bob > > ________________________________________________________________________________
From: "Tim Lewis" <timrv6a(at)earthlink.net>
Date: Mar 08, 2002
Subject: Re: nosewheel fork
> What type of grease / lubricant are you guys using where the nosewheel > fork pivots on the nosegear leg? There's a zerk fitting but I don't > see a callout for specific grease type. Would the Aeroshell #5 grease > used for the wheel bearings work well for the nosewheel fork too? Light Plane Maintenance ran a pretty detailed grease article in June 2000. They eneded up recommended Aeroshell 6 for grease gun use and Aeroshell 5 for our wheels. I use Aeroshell 6 on the prop hub because it's required (can't mix grease in prop hubs). On the advice of a local experienced A&P, I simplified my life and just used Aeroshell 6 everywhere (prop hub, wheels, zerks for nose gear fork). That's worked fine for 320 hrs. No sign of excessive wear on the wheel bearings when I clean and inspect them at each annual. > Also, does the fork need to be primed (ohmygosh, did I ask a *primer* > question?). It's cold outside and I'm feeling lazy and don't want to > prime anything right now.... I recommend priming and painting. Mine has a good solid coat of Imron over epoxy primer, which helps protect it from the filth that accumulates under that nose gear fairing during the year. Tim ****** Tim Lewis -- HEF (Manassas, VA) RV-6A N47TD - First Flight 18 Dec 99 http://www.geocities.com/timrv6a ****** ________________________________________________________________________________
From: "Tom Gummo" <t.gummo(at)verizon.net>
Subject: Re: Gross Weight Determinations
Date: Mar 08, 2002
It is a money making program for FAA cronnies. My DAR spent two minutes at the plane and then asked for 350 dollars. Tom Gummo Apple Valley, CA ----- Original Message ----- From: "Garth Shearing" <garth(at)Islandnet.com> Subject: Re: RV-List: Gross Weight Determinations > > I'm in Canada where the regs a a little different, but if in the U.S. you > can change the gross weight to anything, why is there a need for an > inspection at all? > > Garth Shearing > VariEze and 80% RV6A > Victoria BC Canada > > | Bob, you need to somehow explain to the misinformed DAR that you, not > | Vans, are the manufacturer of the airplane; as the manufacturer, you can > | set the GW anywhere you wish! What kind of gross weight would he require > | if you had substituted rocket wings for Vans wings, or used a Mustang II > | tail section, or...gasp....used a Subaru engine that Vans doesn't > | endorse?? > | > > ________________________________________________________________________________
Date: Mar 08, 2002
From: old ogre <jollyd(at)ipns.com>
Subject: for sale RV8A
RV8A for sale...98-99% finished...just little things left to do...0320, 160hp..0smoh..new C/S prop..new upholstry...radio transpndr..$61,500.00 located oregon ________________________________________________________________________________
From: "Rob A" <racker(at)rmci.net>
Subject: Gross Weight Determinations
Date: Mar 08, 2002
> you can > set the GW anywhere you wish! Sort of it seems. Reading FAA Order 8130.2D (what the inspector uses to certify aircraft), you must base your operating weights/cg limits from kit manufacturer data (text of order below). However, the same order also states the FAA inspector is only to check that the c.g. and its fore and aft limits have been established, NOT the gross weight the builder has set. I guess the key is not to mention the word gross *anywhere*. Its not required on the data plate, and if you show the inspector you have done the calcs for all your intended mission profiles to prove the c.g. is within fore/aft limits, you have satisfied the FAA order requirement. > What kind of gross weight would he require > if you had substituted rocket wings for Vans wings, You would have to do all the calcs to determine the safe weights/cg limits (also covered in the order). > or...gasp....used a Subaru engine that Vans doesn't > endorse?? The airframe will only be stable in a certain c.g. range regardless of what's up front. I suspect you would still have to use the kit manufacturers data. If an inspector insists on gross weight data, maybe giving him a higher gross weight with a load factor limitation (based on Van's 6g's@1375lbs) would make things happy. Rob Acker (RV-6). ************************************************* FAA Order 8130.2D, Airworthiness Certification of Aircraft and Related Products, Par. 127, Subsection 2(f): Weight and Balance. (1) Prior to certification, the amateur builder should accurately weigh the aircraft in accordance with established weight and balance procedures to determine the aircraft's empty, gross, and most forward and aft center of gravity range, including the weight and balance for the initial flight tests in order to help reduce stall, spin, and other control related accidents. Such limits would be determined by the builder through calculations if the aircraft is self-designed, or as specified in the data for aircraft constructed from a kit or built from purchased plans. The completed weight and balance report, including load limits for crew, oil, fuel, and baggage, should be available in the aircraft along with the other applicable placards, listings, and markings required by 91.9. (2) Prior to certificating the aircraft, the FAA should verify that the weight and balance data is accurate for that aircraft; that the aircraft has been weighed correctly; and that the CG and its most forward and aft CG limits are established. ________________________________________________________________________________
From: "Craig Chipley" <craigchipley(at)hotmail.com>
Subject: RV-8A flight visibilty
Date: Mar 08, 2002
List, I am contemplating the RV-8A. Of those that are flying, how is the visiblity over the nose? Or total visibilty for that matter. Seems like a long nose compared to Van's other designs. I like the airplane. Just a few things left to figure out before the BIG PURCHASE!!. Thanks for the help, Craig ________________________________________________________________________________
From: JNice51355(at)aol.com
Date: Mar 08, 2002
Subject: Re: RV-4 Sale
In a message dated 3/8/02 7:21:00 AM Pacific Standard Time, Eric.J.Henson(at)chase.com writes: > OK, what's going on here? This is like the third baby-forced sale of an RV > in the last few months. Folks My wife has it together, folks. While building the RV, I acquired a Cherokee to fly. My wife has appropriately nicknamed this airplane BABY. Jim Nice WA State ________________________________________________________________________________
Date: Mar 08, 2002
From: Bobby Hester <bhester(at)apex.net>
Subject: Re: Torque Wrench Info
Jack Textor wrote: > > Larry, > A pilot/A&P friend sent it to Utah. I will get the specifics for the list. > I have also had the Ia Air Guard check them in the past; they didn't charge > me a thing. > Jack > > Subject: Re: RV-List: Torque Wrench Info > > Where is you take it to be certified? > > -Larry > > > Wanted the group to know the 1/4" 0-200 inch pound torque wrench I > purchased > > from JC Whitney just passed a certification. The tolerance was 4%. Mine > > was within 1/4 of a percent. I was pleasantly surprised. > > Jack > > RV8, wings > > DSM > Is that a 0-200 or a 20-200? I saw a 20-200 on there web site. -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
From: "AJ Yahya" <ajyahya(at)relay3.jaring.my>
Subject: TruTrak autopilot system
Date: Mar 09, 2002
I am considering TruTrak DigiFlight 100 with GPS steering for an RV-7A project which just started. I understand that the unit include: a.. Built-in Digital Slaved Directional Gyro a.. Digital Heading Selector This obviously will save me cost from buying a slaved DG if I considers a S-TEC system 20. Has anyone had any experience with the TruTrak system? AJ Yahya ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Mar 08, 2002
Subject: Re: TruTrak autopilot system
You might try Wayne Williams at : rwayne(at)gamewood.net E. Len Leggette, RV-8A Greensboro, N.C. N910LL (res) Hanger #23 INT ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)jetstream.net>
Subject: Safety and Operating Costs
Date: Mar 08, 2002
Regarding my post on March 3 on the subject of Shell W oil Randy Levold asked if I was including W 15-50 in it. To clear things up I was talking about the standard W series not the multiple viscosity. For the Lycoming's my practice has been to run W100 spring to fall and W80 through the colder months. As I have mentioned before I preheat for starting when the temperatures are below the freezing mark so I really have no need for the 15-50. In all honesty I would still preheat in the colder temperatures for starting even if running 15-50. On the 15-50 I would like to see some engines run to overhaul and see what the condition was on tear down. I have no doubt that is as advertised and the LW 16702 additive in it takes care of those who are running the H2AD's. This additive would be a real plus during the winter months when the engines sit idle for long periods. Here in Canada and I am sure it would be the same in the USA Shell added W100 Plus which also contains the LW16702 additive. This is my choice for the coming summer anyway. And for those just starting a new or overhauled engine just a reminder to go with Shell straight mineral oil not the W series until the oil consumption settles down. Avoid ground running and taxiing as much as possible. Eustace Bowhay Blind Bay, B.C. Wiring and instruments on the 6A. ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)jetstream.net>
Subject: Re: RV-6A upper gear leg fairings
Date: Mar 08, 2002
Hey guys, were did you get the fairings from? Eustace Bowhay ----- Original Message ----- From: "Stephen J. Soule" <SSoule(at)pfclaw.com> Subject: RV-List: RV-6A upper gear leg fairings > > All you RV-6A builders ... > > I have upper gear leg fairings, but can't figure out how to hold them in > place. I don't think that drilling holes in my fuel tanks for screws is a > good idea. The plane is flying, so access to the fuselage isn't great. I saw > somewhere once that these upper fairings could be held in place by using > springs, but I can't see how that would work. Any ideas out there? > > Steve Soule > Huntington, Vermont > N227RV > > ________________________________________________________________________________
From: "cmcgough" <rv6(at)ssc.net.au>
Subject: contact help
Date: Mar 09, 2002
Could someone give me the contact no of Alex Dominicis. His RV6 is in the calender under April and I need to know the colour of his paint. Chris and Susie VH-MUM ________________________________________________________________________________
Date: Mar 08, 2002
From: Ted Gauthier <tgauthier(at)comcast.net>
Subject: Slider/Tip up Photo's
I have been asked by several builders for photo's of the modification to my canopy which makes it a slider and a tip up so I have posted the photo's to the yahoo group photos in the Ted Gauthier file. You can obtain the plans from the original designer Rich Meske. If anyone still has questions, just drop me a note and I will do my best to explain what I did. Ted Gauthier RV 6, finishing Pontia, Michigan ________________________________________________________________________________
Date: Mar 08, 2002
From: Dan Masys <dmasys(at)cox.net>
Subject: Re: TruTrak autopilot system
AJ Yahya wrote: > > I am considering TruTrak DigiFlight 100 with GPS steering for an RV-7A > project which just started. I understand that the unit include: > > a.. Built-in Digital Slaved Directional Gyro > a.. Digital Heading Selector > > This obviously will save me cost from buying a slaved DG if I considers > a S-TEC system 20. > > Has anyone had any experience with the TruTrak system? Got the Digiflight 200 TruTrak. Haven't put it all together yet but have installed the roll servo in a -7A wing and have the pitch servo for the fuse. Quality seems to be very good and the pieces fit the -7 perfectly -- simple bolt-on that replaces current brackets. -Dan Masys -7A fuse ________________________________________________________________________________
Date: Mar 08, 2002
From: Chris Good <chrisjgood(at)yahoo.com>
Subject: Tilting slider canopy
Listers, Rich Meske has asked me to post a web page about his tilting slider canopy modification. The URL is: http://rv.supermatrix.com/misc/tilt-slider.html ==== Regards, Chris Good, http://www.rv.supermatrix.com West Bend, WI RV-6A N86CG, 328 hrs ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: compass
Date: Mar 08, 2002
Today's crayon-level question: What makes a compass an aviation compass? I picked up a Ritchie X-15 marine compass (http://www.ritchienavigation.com/ritchie.htm) that would look real nice in my panel, and the fact that it was $26 is a bonus. Any reason why it won't work? - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Gross Weight Determinations
Date: Mar 08, 2002
In the US, the job of the FAA/DAR is to ensure that the aircraft is amateur built (non-commercial), that it meets the requirements, and is airworthy. In the US there is no requirement for the DAR to ensure that your aircraft is built to any sort of specification given by the kit mfg.(I.E. Vans). As was stated earlier, you could put taylorcraft wings and a lancair tail on the thing if you wanted! A good example is the Harmon Rocket, Boyd's "Super Six", etc.... You are the kit mfg, Van's just supplies you with components and hardware. That being said, you must ultimately determine the performance variables for YOUR plane. I know things are differnt in other countries, but that's how it is in the US. Cheers, Stein Bruch, A&P RV6, Minneapolis. Waiting on Seats and Seat Belts, Paint and a Hangar. I'm in Canada where the regs a a little different, but if in the U.S. you can change the gross weight to anything, why is there a need for an inspection at all? Garth Shearing VariEze and 80% RV6A Victoria BC Canada ________________________________________________________________________________
Date: Mar 08, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: compass
Larry Bowen wrote: > > > Today's crayon-level question: > > What makes a compass an aviation compass? > > I picked up a Ritchie X-15 marine compass > (http://www.ritchienavigation.com/ritchie.htm) that would look real nice > in my panel, and the fact that it was $26 is a bonus. Any reason why it > won't work? > > - > Larry Bowen > Larry(at)BowenAero.com > http://BowenAero.com Per FAR 91.205 which calls out requirements for instruments: b) Visual-flight rules (day). For VFR flight during the day, the following instruments and equipment are required: (3) Magnetic direction indicator. The same holds true for night and IFR operations. So......is the marine compass a "Magnetic direction indicator"? :-) The DAR will probably want to see you attach a correction card near the unit, but any ol' compass is legal in our experimental planes as long as it can be reasonably swung. The only compass in my RV-6 is the electronic module in the RMI uEncoder. Sam Buchanan (RV-6) "The RV Journal" http://thervjournal.com ________________________________________________________________________________
From: "rodney.woodard" <rodney.woodard(at)attbi.com>
Subject: Re: Gross Weight Determinations
Date: Mar 08, 2002
>>>do the paperwork for 1600.......and fly the plane at whatever weight you wish. ;-)"<<< I wouldn't do this... The insurance folks can correct me if I'm wrong, but I'm guessing the insurance company won't be wild about paying a claim if you are intentionally operating the aircraft outside its limitations. For this reason, I would think it would be wise to set the gross weight high enough that you'd never bust the limitation. The other issue is that das-Fed could issue a violation for exceeding your chosen gross weight. I do agree that you are the manufacturer and should be able to set any gross weight you desire. I'm guessing that Sam was probably just poking fun when he said you could, "do the paperwork for 1600.......and fly the plane at whatever weight you wish. ;-)" and that's why he put the smiley in there. Best regards, Rod Woodard Northern Colorado RV-3 empennage in progress ----- Original Message ----- From: "Sam Buchanan" <sbuc(at)hiwaay.net> Subject: Re: RV-List: Gross Weight Determinations > > Bob, you need to somehow explain to the misinformed DAR that you, not > Vans, are the manufacturer of the airplane; as the manufacturer, you can > set the GW anywhere you wish! What kind of gross weight would he require > if you had substituted rocket wings for Vans wings, or used a Mustang II > tail section, or...gasp....used a Subaru engine that Vans doesn't > endorse?? > > If he balks at this, show him the registration application where you > indicated the plane is a "Busick RV-6A". > > If he still balks......get a DAR that knows what he is doing......and > let all the local builders know to avoid this turkey. > > Or.....do the paperwork for 1600.......and fly the plane at whatever > weight you wish. ;-) > > Sam Buchanan (RV-6, been flown at 1600, been flown at 1675, been flown > at 1725.......) > "The RV Journal" http://thervjournal.com > > ===================== > > Bob Busick wrote: > > > > > > I checked the archives and I have seen that some people have set RV6/A gross > > weights at 1800-1950 lbs. Also it has been stated numerous times that the > > builder/manufacturer sets the gross weight. > > > > However, my FAA inspector when he saw my gross weight of 1800 he told me > > that I had to document from Vans the designed gross weight. I told him that > > it was 1600/1650 and he told me that he would only approve an 1800 gross > > weight if Van would put that in writing. > > > > Assuming that Van will not put this in writing, how do I get around this. > > I don't need an 1800 gross weight, but, it would be nice if I need it. > > > > Bob > > > > _ > > ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: RV-6A upper gear leg fairings
Date: Mar 09, 2002
Team Rocket makes and sells a set of upper and lower gear leg intersection fairings. They fit the gear leg fairings that Team Rocket makes and sells. I believe they fit the pressure recovery wheel pants that Van sells. Check the Team Rocket web site to make sure. The products are high quality, well made items. I made my own lower gear leg fairings, but bought the uppers from Team Rocket. Steve Soule -----Original Message----- Hey guys, were did you get the fairings from? Eustace Bowhay ________________________________________________________________________________
From: "Jim Sears" <sears(at)searnet.com>
Subject: Re: Gross Weight Determinations
Date: Mar 09, 2002
> The basic idea behind inspections seems to be that the paper work is > done correctly. > Sometimes, I think Jerry is right on this one. I've seen some homebuilts I wouldn't even think of riding in. They got past their inspection, somehow. I can tell you that mine was given a very good inspection by my DAR. I thought he was a little pricey until I sat down and thought about the time he had in mine. It wasn't so pricey, anymore. When you go to fly-ins, see if you find those that look too dangerous to ride in. You're not going to find many of them that bad, thank goodness. However, that doesn't mean they're not there. Things can be hidden, like bad riveting, wiring, etc. I've seen wiring and plumbing so bad that I wonder that the owner hadn't had problems with leaks and shorts. Now, I'm not one who has looked at lots and lots of homebuilts. It's that a large percentage are that way. They look great on the outside; but, they're disasters on the inside. Some things need looking at by the professionals to be sure we have them right. I've personally looked at enough wiring and plumbing jobs while hanging around the airport that I was able to do a pretty decent job on mine. How many of you can say that and feel good about it? If not, have a pro look at it for you to be sure you're doing the right thing. That way, you don't have to worry about the DAR's looking at it. You'll know it's right. Uh, oh. I'm getting off the subject. :-) As for the weight limit, I had to set mine at 1800 to feel comfortable about it. I wanted enough room for insurance companies. I can easily fill mine to 1700 pounds with two standard passengers. Even though I can meet the standard weight, my passengers don't always do that. My DAR said nothing about my gross weight. He did check out my CG calculations that included one for a 300 pound passenger at full and empty tanks. One may think that's funny; but, I've taken up kids in the Young Eagles program that weighed more than that. That was in my Cheetah. I'd have to fly off some fuel before I felt safe to do it; but, I made sure that kid got the ride. Anyway, my DAR was satisfied and passed my airplane into the next phase of the adventure. Jim Sears in KY RV-6A N198JS EAA Tech Counselor ________________________________________________________________________________
From: "Jerry Carter" <jcarter8(at)midsouth.rr.com>
Subject: Re: RV8-List: RV-8A flight visibilty
Date: Mar 09, 2002
> --> RV8-List message posted by: "Craig Chipley" > > > List, I am contemplating the RV-8A. Of those that are flying, how is the > visiblity over the nose? Or total visibilty for that matter. Seems like a > long nose compared to Van's other designs. I like the airplane. Just a few > things left to figure out before the BIG PURCHASE!!. Thanks for the help, > Craig > > Well, a picture is worth...... see http://rv8asite.homestead.com/moreflying.html Jerry Carter RV-8A 99 hrs, 132 landings ________________________________________________________________________________
Date: Mar 09, 2002
Subject: RV-8A flight visibilty
From: czechsix(at)juno.com
Hi Craig, I'm not flying my own -8A yet nor have I soloed any -8 or -8A from the front seat in flight, but I've flown back seat in -8/A's and sat in the front seat of many on the ground making airplane noises, switching to guns, and dropping laser-guided weapons into caves in Afghanistan.... My conclusion has been that the visibility over the nose is excellent.....WAY better than any spam can you've ever been in. Yes the nose is fairly long relative to the size of the airplane, but it's a small airplane and the nose slopes down quite a bit and you sit up pretty high. Probly the biggest disadvantage would be in an -8 taildragger on the ground which would be the "worst-case" visibility-wise, but if you've already seen the light and are planning to join the ranks of us nosedragger training-wheel weenies, you don't have a thing to worry about. Jump on in, you'll love it! --Mark Navratil Cedar Rapids, Iowa RV-8A finish kit stuff....makin' airplane noises.... _______ From: "Craig Chipley" <craigchipley(at)hotmail.com> Subject: RV-List: RV-8A flight visibilty List, I am contemplating the RV-8A. Of those that are flying, how is the visiblity over the nose? Or total visibilty for that matter. Seems like a long nose compared to Van's other designs. I like the airplane. Just a few things left to figure out before the BIG PURCHASE!!. Thanks for the help, Craig ________________________________________________________________________________
Date: Mar 09, 2002
Subject: Re: Gross Weight Determinations
From: czechsix(at)juno.com
I've been watching the various discussions here for the past couple years on problems people run into with inspectors (like gross weight, engine AD compliance, etc. etc.). Seems to me that the problem is this: 1) One of the primary purposes of the inspection is to determine airworthiness (i.e. safety). 2) The inspection is a subjective evaluation on the part of the inspector. So, here's where the problems begin. It's true that because your RV is an Experimental you have a lot of leeway in the limitations you set for your aircraft, and what things you do to your airframe or engine.....that is to say the regs may not call out anywhere that an experimental aircraft has to follow the kit manufacturer's suggested gross weight or the engine manufacturers suggested service bulletins, AD's, etc. But when the inspector comes along he should be evaluating the aircraft from a safety perspective, so he might ask you to add an adel clamp here, a tiewrap there, reroute this or that hose, etc to ensure safety. Along the same lines he may feel very strongly that because Van's has an outstanding reputation as a kit producer/ designer, his recommended gross weight should be followed. Or likewise, if you're using a Lycosaur (even with an experimental data plate on it) the AD's should be complied with because they were intended to fix known safety problems (yeah I know some are pretty bogus but that's beside the point here). I'm not defending the FAA inspector or DAR in any way, just trying to clarify what I perceive as an ongoing thread/misunderstanding on this List regarding inspections. If an inspector refuses to sign off your airplane for something he considers a safety issue, it doesn't matter one bit whether he's "right" or "wrong" or whether the change he wants you to make is "required" for experimental aircraft. You're pretty much stuck.......so your options at that point are to use resources such as EAA, Vans, or other documentation to convince him otherwise, or to get a new inspector. --Mark Navratil Cedar Rapids, IA RV-8A finish kit stuff.... _______ From: "Bob Busick" <panamared1(at)brier.net> Subject: Re: RV-List: Gross Weight Determinations I checked the archives and I have seen that some people have set RV6/A gross weights at 1800-1950 lbs. Also it has been stated numerous times that the builder/manufacturer sets the gross weight. However, my FAA inspector when he saw my gross weight of 1800 he told me that I had to document from Vans the designed gross weight. I told him that it was 1600/1650 and he told me that he would only approve an 1800 gross weight if Van would put that in writing. Assuming that Van will not put this in writing, how do I get around this. I don't need an 1800 gross weight, but, it would be nice if I need it. Bob ________________________________________________________________________________
From: "Joe Larson" <jpl(at)showpage.org>
Subject: Gross Weight
Date: Mar 09, 2002
> > Assuming that Van will not put this in writing, how do I get around this. > I don't need an 1800 gross weight, but, it would be nice if I need it. Can anyone comment on how Van's set their initial gross weight, and what the implications would be for flying at a heavier weight? Obviously, we won't get the same climb performance, but our performance is aready well above what I'm used to flying... Comments? -Joe ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: Gross Weight Determinations
Date: Mar 09, 2002
One thing I haven't seen mentioned in this thread yet are the in-flight g-load limitations at weights greater than 1650, in the case of the 6 or 6A. One can extrapolate (within reason) what the limitations should be. Van's design numbers for the 6/6A are 1375 lbs +6g, and at 1650 the limit is +4.4. At 1800, this works out to be about +3.5 g's. This does not consider landing gear loads. I believe it is prudent to plan to burn 100lbs of fuel or so before landing, when the flight was initiated at something like 1800lbs. Alex Peterson Maple Grove, MN 6A N66AP flying 96 hours ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: compass
Date: Mar 09, 2002
OK. Thanks, Sam. So, there is nothing physically "special" about a aviation comapss. It's not gimbled different or dampened or whatever? Physically, Marine whiskey compass =? Aviation whiskey compass The only thing lacking on this model from Ritchie is a way to adjust it. I guess that's where the correction card comes into play ... - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > Larry Bowen wrote: > > > > > > Today's crayon-level question: > > > > What makes a compass an aviation compass? > > > > I picked up a Ritchie X-15 marine compass > > (http://www.ritchienavigation.com/ritchie.htm) that would look real > > nice in my panel, and the fact that it was $26 is a bonus. > Any reason > > why it won't work? > > > > - > > Larry Bowen > > Larry(at)BowenAero.com > > http://BowenAero.com > > > Per FAR 91.205 which calls out requirements for instruments: > > b) Visual-flight rules (day). For VFR flight during the day, > the following instruments and equipment are required: instruments snipped> > > (3) Magnetic direction indicator. > > > > The same holds true for night and IFR operations. > > So......is the marine compass a "Magnetic direction indicator"? :-) > > The DAR will probably want to see you attach a correction > card near the unit, but any ol' compass is legal in our > experimental planes as long as it can be reasonably swung. > > The only compass in my RV-6 is the electronic module in the > RMI uEncoder. > > Sam Buchanan (RV-6) > "The RV Journal" http://thervjournal.com > ________________________________________________________________________________
Date: Mar 09, 2002
Subject: Anodizing fuel caps
From: czechsix(at)juno.com
Guys, FYI for the archives, I did some more research on the fuel caps supplied by Vans (made by Usher) and was told that they can NOT be anodized.....they are a casting that includes other metals along with aluminum, and have a high silicon content. To get good results with anodizing you need a machined aluminum alloy. I've looked through some catalogs (Aircraft Spruce, etc...) and there are several other caps available that would work, but none of them look compatible with the Usher caps.....it would have to be fitted with their own filler necks when the tanks are assembled. So my fuel caps will have to be painted instead : ( As a side note, the guy I talked to who does the castings said that if you don't want the paint to chip off so easily, you need to etch/alodine the caps before paint. Apparently the surface of the caps is contaminated by the mold release stuff, and just wiping it with MEK or equivalent will not clean it well enough for a really good paint bond......it'll stick ok, but will be more prone to chipping or peeling off than a surface prepared with etch/alodine. --Mark Navratil Cedar Rapids, Iowa RV-8A finish kit stuff.... ________________________________________________________________________________
From: "Rob A" <racker(at)rmci.net>
Subject: Re: Gross Weight Determinations
Date: Mar 09, 2002
> that > is to say the regs may not call out anywhere that an experimental > aircraft has to follow the kit manufacturer's suggested gross weight... > One thing I haven't seen mentioned in this thread yet are the in-flight > g-load limitations at weights greater than 1650, I guess my post last night was missed. Spells out the FAA regs regarding the following of kit manufacturer gross weight, and possible satisfaction of variances through appropriate load limitation calculations. Not trying to nit pick, just trying to make sure Bob and the inspector have valid info in hand so he can set his gross weight set higher. Rob Acker (RV-6, registration paperwork). ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: Anodizing fuel caps
Date: Mar 09, 2002
How about chrome? Paul Besing RV-6A Sold http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: <czechsix(at)juno.com> Subject: RV-List: Anodizing fuel caps > > Guys, FYI for the archives, I did some more research on the fuel caps > supplied by Vans (made by Usher) and was told that they can NOT be > anodized.....they are a casting that includes other metals along with > aluminum, and have a high silicon content. To get good results with > anodizing you need a machined aluminum alloy. I've looked through some > catalogs (Aircraft Spruce, etc...) and there are several other caps > available that would work, but none of them look compatible with the > Usher caps.....it would have to be fitted with their own filler necks > when the tanks are assembled. So my fuel caps will have to be painted > instead : ( > > As a side note, the guy I talked to who does the castings said that if > you don't want the paint to chip off so easily, you need to etch/alodine > the caps before paint. Apparently the surface of the caps is > contaminated by the mold release stuff, and just wiping it with MEK or > equivalent will not clean it well enough for a really good paint > bond......it'll stick ok, but will be more prone to chipping or peeling > off than a surface prepared with etch/alodine. > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A finish kit stuff.... > > > > > > ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: Re: Gross Weight Determinations
Date: Mar 09, 2002
Does one, in fact, have the option to get another inspector? I had seen messages years back on this list to the effect that once an inspector finds a discrepancy, it must be fixed - there is no second opinion. Sort of like getting an annual and disagreeing with the IA's call on maintenance before the Return-to-Service sign-off is obtained. Once an IA says it's bad, it has to be fixed and you can't get a second opinion. The interpretations of DARs and FISDO inspectors vary so greatly between regions and individuals that there may be no simple answer to this one. It was because of concerns like these that I got to know my inspector well before he came out to see the plane. We discussed my project and I showed him my well-documented lab book (a/k/a builder's log). He gave me some head 's up advice on what he expected and all went well at inspection time. In our area, there are lots of builders and it is pretty easy to find out who the good guys are before they show up to inspect your plane. Dennis Persyk 6A N600DP 114 hours Gross wt 1800 lbs ----- Original Message ----- From: <czechsix(at)juno.com> Subject: RV-List: Re: Gross Weight Determinations > > I'm not defending the FAA inspector or DAR in any way, just trying to > clarify what I perceive as an ongoing thread/misunderstanding on this > List regarding inspections. If an inspector refuses to sign off your > airplane for something he considers a safety issue, it doesn't matter one > bit whether he's "right" or "wrong" or whether the change he wants you to > make is "required" for experimental aircraft. You're pretty much > stuck.......so your options at that point are to use resources such as > EAA, Vans, or other documentation to convince him otherwise, or to get a > new inspector. > > --Mark Navratil > Cedar Rapids, IA > RV-8A finish kit stuff.... ________________________________________________________________________________
From: "Steve Hurlbut" <hurlbut_steve(at)hotmail.com>
Subject: RV-7/9 Fuselage help
Date: Mar 09, 2002
Ok 10 hours is enough. I'm trying to clecoe the F711, F712, F779 to the fuselage assembly and I can get 1 side clecoed on but the other side holes are off by 1/4" (too low, the F779 needs to be pulled in tighter). Anybody just throw away the F779 piece of $%&# and try a non-prepunched one? I'm at the point where holes are being enlarged due to the stress on the clecoes. Suggestions would be much appreciated to help me out of the frusterating hole and back into the building enjoyment hole. Thankx Steve RV-7A Join the worlds largest e-mail service with MSN Hotmail. http://www.hotmail.com ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Gross Weight Determinations
Date: Mar 09, 2002
Check with the EAA 1-888-eaa-info. Earl lawrence can help. Cy Galley Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org ----- Original Message ----- From: "Dennis Persyk" <dpersyk(at)worldnet.att.net> Subject: Re: RV-List: Re: Gross Weight Determinations Does one, in fact, have the option to get another inspector? I had seen messages years back on this list to the effect that once an inspector finds a discrepancy, it must be fixed - there is no second opinion. Sort of like getting an annual and disagreeing with the IA's call on maintenance before the Return-to-Service sign-off is obtained. Once an IA says it's bad, it has to be fixed and you can't get a second opinion. The interpretations of DARs and FISDO inspectors vary so greatly between regions and individuals that there may be no simple answer to this one. It was because of concerns like these that I got to know my inspector well before he came out to see the plane. We discussed my project and I showed him my well-documented lab book (a/k/a builder's log). He gave me some head 's up advice on what he expected and all went well at inspection time. In our area, there are lots of builders and it is pretty easy to find out who the good guys are before they show up to inspect your plane. Dennis Persyk 6A N600DP 114 hours Gross wt 1800 lbs ----- Original Message ----- From: <czechsix(at)juno.com> Subject: RV-List: Re: Gross Weight Determinations > > I'm not defending the FAA inspector or DAR in any way, just trying to > clarify what I perceive as an ongoing thread/misunderstanding on this > List regarding inspections. If an inspector refuses to sign off your > airplane for something he considers a safety issue, it doesn't matter one > bit whether he's "right" or "wrong" or whether the change he wants you to > make is "required" for experimental aircraft. You're pretty much > stuck.......so your options at that point are to use resources such as > EAA, Vans, or other documentation to convince him otherwise, or to get a > new inspector. > > --Mark Navratil > Cedar Rapids, IA > RV-8A finish kit stuff.... ________________________________________________________________________________
Date: Mar 09, 2002
From: Rob Prior <rv7(at)b4.ca>
Subject: Re: Gross Weight Determinations
Which may be why the FAA is more than happy to allow Canadian homebuilts into the US, but TC is opposed to allowing US homebuilts into Canada. Our inspection process appears to be more stringent... Preclosing inspections on all structures, final inspection before first flight, etc. I've heard of final inspections taking all day up here. -RB4 Tom Gummo wrote: > >It is a money making program for FAA cronnies. >My DAR spent two minutes at the plane and then asked for 350 dollars. >Tom Gummo > ________________________________________________________________________________
From: "Bruce Gray" <bruce.gray(at)snet.net>
Subject: Gross Weight Determinations
Date: Mar 09, 2002
We can fly into Canada any time we want. But live there? Under that type of oppressive bureaucracy? No way! Bruce Glasair III -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Rob Prior Subject: Re: RV-List: Gross Weight Determinations Which may be why the FAA is more than happy to allow Canadian homebuilts into the US, but TC is opposed to allowing US homebuilts into Canada. Our inspection process appears to be more stringent... Preclosing inspections on all structures, final inspection before first flight, etc. I've heard of final inspections taking all day up here. -RB4 ________________________________________________________________________________
Date: Mar 09, 2002
From: Kevin Horton <khorton(at)cyberus.ca>
Subject: Canadian inspection requirements, was: Gross Weight Determinations
It would be interesting to figure out what percentage of US homebuilt accidents are caused by stuff that would have been picked up by a Canadian style inspection. I'm betting a more stringent inspection would have made a difference in only a very small percentage of accidents. There is a proposed amendment to the Canadian regulations that would allow a US homebuilt to be imported into Canada, as long as it has flown 50 hours. See: <http://www.tc.gc.ca/aviation/regserv/carac/carac/part5-m&m/npa/archive/2001/jun/English/2001050e.htm> This has been in the works for awhile - I have no idea when or if it will be approved. Kevin Horton > >Which may be why the FAA is more than happy to allow Canadian homebuilts >into the US, but TC is opposed to allowing US homebuilts into Canada. > Our inspection process appears to be more stringent... Preclosing >inspections on all structures, final inspection before first flight, >etc. I've heard of final inspections taking all day up here. > >-RB4 > >Tom Gummo wrote: > >> >>It is a money making program for FAA cronnies. >>My DAR spent two minutes at the plane and then asked for 350 dollars. > >Tom Gummo >> ________________________________________________________________________________
From: "Dave Stewart" <davestewart(at)globalserve.net>
Subject: Re: RV-7/9 Fuselage help
Date: Mar 09, 2002
Steve I agree, this area is frustrating, but hang in there. The tailcone is a brute due to it's thickness. Some things that helped me: 1) make sure the tailcone edges are vertical along the J-stringer rivet lines (mine wasn't due to springback during forming) & get these clecoes in first. 2) measure the center distance of flange rivet holes in the SKINS 3) assuming you've riveted the fore & aft bulkhead halves together, fiddle with the flanges 'till they match (?!) skin holes & follow skin angle 4) insert & cleco front half, then coax aft half (grind old #40 bit as drift pin) & cleco every hole. Don't know if this is best way but it got me there. Dave (90252) ----- Original Message ----- From: "Steve Hurlbut" <hurlbut_steve(at)hotmail.com> Subject: RV-List: RV-7/9 Fuselage help > > > Ok 10 hours is enough. > I'm trying to clecoe the F711, F712, F779 to the fuselage assembly and I can > get 1 side clecoed on but the other side holes are off by 1/4" (too low, the > F779 needs to be pulled in tighter). Anybody just throw away the F779 piece > of $%&# and try a non-prepunched one? I'm at the point where holes are being > enlarged due to the stress on the clecoes. > > Suggestions would be much appreciated to help me out of the frusterating > hole and back into the building enjoyment hole. > > Thankx > Steve > RV-7A > > > Join the worlds largest e-mail service with MSN Hotmail. > http://www.hotmail.com > > ________________________________________________________________________________
From: "Glenn & Judi" <dirtyrottenscoundrels(at)attbi.com>
Subject: RV-6 Swivel Tailwheel Breakout Force.
Date: Mar 09, 2002
Hi, Is there anyway to increase the breakout force on the RV-6 full swivel tailwheel? Thanks, Glenn Gordon N442E ________________________________________________________________________________
From: KBoatri144(at)aol.com
Date: Mar 09, 2002
Subject: Re: RV-6 Swivel Tailwheel Breakout Force.
In a message dated 3/9/02 4:18:53 PM Eastern Standard Time, dirtyrottenscoundrels(at)attbi.com writes: << Hi, Is there anyway to increase the breakout force on the RV-6 full swivel tailwheel? Thanks, Glenn Gordon N442E >> There is a small spring which forces the pawl (pin) in the locking mechanism into the slot. This provides the centering force. To increase the break-out force, replace the original spring with a stronger spring with identical diameter and identical (or slightly greater) length. The downside to increasing the break out force is that it will tend to increase the side loads applied to the tailspring and mount. That portion of the airframe may be strong enought to handle these loads, and then again, it may not be. I dunno... Kyle Boatright 0-320/Aymar Demuth RV-6 Slider Kennesaw, GA http://www.angelfire.com/my/rv6 ________________________________________________________________________________
From: "Edward Cole" <edwardmcole(at)attbi.com>
Subject: Panel Mount Compass for Sale
Date: Mar 09, 2002
Listers, I have a remote mount Ritchie M-2 Compass for sale. It has a black bezel and blue face with white lettering. West Marine features it for $149 and it sells for $ 201 at Advantage propeller This is brand new in the box for $100 plus shipping. Below is a description from the West Marine Web site. Description Convenient instrument panel mounting makes this advanced technology easy to install and use. You get highly accurate MagTronic readings and extra-large numerals on a high-visibility blue dial that's easy to read. Sensor is gimbaled to 45=BA pitch and roll. Features include automatic compensation, edge lighting and reverse polarity protection. Noncorroding remote sensor housing measures 4 1/8" x 2 15/16" x 4" and weighs only 24oz. Gauges fit standard panel knockouts and can be mounted at any angle. M-Series compasses include 20' cable and installation and compensation instructions. Repeaters include 20' cable. 2-year warranty. If interested, contact me off list at edwardmcole(at)attbi.com Ed Cole RV6A N2169D Flying RV6A N648RV Finishing ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: Anodizing fuel caps
Date: Mar 09, 2002
message posted by: "Paul Besing" > How about chrome? Anodizing? Paint? Chrome? Nahhh. Just take a polishing wheel to them and they shine up real nice. Randall Henderson, RV-6 N6R (~300 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
From: "rodney.woodard" <rodney.woodard(at)attbi.com>
Subject: Re: Gross Weight Determinations
Date: Mar 09, 2002
This is not correct. You always have the option of tugging your airplane across the ramp to a different IA. In an extreme case, you could probably get a ferry permit to fly the airplane to another airport and another IA. You are not held hostage. Don't get me wrong, MOST of the A&P's/IA's I've ever dealt with have been honest as the day is long and fine individuals. However, there's always one of anything lurking around ready to be the exception to the rule. A concrete example: I once had an IA refuse to sign off on an annual on a Cherokee 140 because he insisted that I comply with a Service Bulletin that was issued for the Saratoga and bigger Pipers. I refused. I was able to talk to his partner in the repair shop who was more reasonable, but I had already started the process to obtain a ferry permit to take my plane to a different airport and a different IA. It's easy to get into a p*ssing match over some of this stuff. One person says he carries a flashlight at night. The next person says he carries two. The next guy says he doesn't fly single engine aircraft at night. The next guy says he won't fly any aircraft at night. Etc., ad nauseum. Best regards, Rod Woodard ----- Original Message ----- From: "Dennis Persyk" <dpersyk(at)worldnet.att.net> Subject: Re: RV-List: Re: Gross Weight Determinations > (STUFF SNIPPED) > Once an IA says it's bad, it > has to be fixed and you can't get a second opinion. > ________________________________________________________________________________
From: "David Berryhill" <berryhill1911(at)hotmail.com>
Subject: Re: Anodizing fuel caps
Date: Mar 09, 2002
The original poster wanted to make them red, not shiny. Since you can't anodize them, how about a powder coat or just paint? Dave Berryhill > > How about chrome? > >Anodizing? Paint? Chrome? Nahhh. Just take a polishing wheel to them and >they shine up real nice. > >Randall Henderson, RV-6 N6R (~300 hrs) >Portland, OR >www.vanshomewing.org > MSN Photos is the easiest way to share and print your photos: http://photos.msn.com/support/worldwide.aspx ________________________________________________________________________________
Date: Mar 09, 2002
From: "J Andrews" <rv8a(at)lycos.com>
Subject: Re: RV-8A flight visibilty
Amazing! After years of flying Cessnas and Piper Warriors the 8A is a dream come true. First of all, the nose sits so far below the horizon my reference point for level flight is half way up the wind screen. I have to keep from just throwing my head back all the time and looking straight up at the sky. I'm still freaked at all times I see the moon in broad daylight. I flew my first formation flight two weeks ago and it was so easy to find my marks, even when passing under the lead the view is amazing. What a thrill. I can hardly wait to get good at it. It almost makes all that time I spent on the canopy worth it ;-) - Jim Andrews RV-8A (flying every weekend and loving every minute of it) -- On Fri, 08 Mar 2002 19:48:14 Craig Chipley wrote: > > >List, I am contemplating the RV-8A. Of those that are flying, how is the >visiblity over the nose? Or total visibilty for that matter. Seems like a >long nose compared to Van's other designs. I like the airplane. Just a few >things left to figure out before the BIG PURCHASE!!. Thanks for the help, >Craig > > 2,000,000,000 Web Pages--you only need 1. Save time with My Lycos. http://my.lycos.com ________________________________________________________________________________
Date: Mar 09, 2002
From: KAKlewin(at)aol.com
Subject: Carb Heat Muff/Accident...
Listers, Came upon the incident below while surfing the net...and it made me wonder if the design has been changed at all or if anyone one has come up with a better way to work the carb heat problem?? The long report basically said the 2" hose to the FAB is inadequate and a bad design? Just curious... Kurt in OKC, RV6AQB, Finishing.... On April 1, 1999, approximately 1700 mountain standard time, a Sly RV-6A homebuilt aircraft, N80287, owned and operated by the pilot, was substantially damaged after impacting terrain following a loss of engine power while in cruise flight near Payson, Utah. The airline transport rated pilot and one passenger were not injured. The local area personal flight was being operated under Title 14 CFR Part 91, and no flight plan was filed. The flight originated from the Spanish Fork-Springville Airport, Spanish Fork, Utah, at 1645. Visual meteorological conditions prevailed. According to the pilot, after being airborne for approximately 15 minutes, the aircraft's engine began to lose power. He stated that he applied carburetor heat and switched the fuel tanks, but observed no change in power. The loss of engine power was gradual, with no sudden stoppage, backfiring or surging. Unable to restore power to the engine, he initiated an emergency landing along a county road 6 miles south of the airport. During landing, he switched to another road to avoid power lines. Upon touchdown, the aircraft departed the side of the road and struck a fence post, damaging the nose gear, ailerons and rudder. At the request and in the presence of a Federal Aviation Administration (FAA) inspector, the engine was examined and test run at the Spanish Fork Flying Service on April 16, 1999. During the inspection, the fuel was clear and free of contaminates. The engine ran with and without the fuel pump turned on, and no discrepancies were noted. The pilot stated in his accident report that "other pilots at the scene agreed the conditions could cause carburetor icing." According to the FAA inspector present at the accident scene, weather conditions were partly cloudy and cold with calm wind. According to the inspector, "the conditions were a classic setup for carburetor icing." According to the Van's Aircraft construction and operating manual, one method of building the internal carburetor heat system is to "run a 2-inch air hose from a heat muff and position it to feed into the alternative air inlet of the carb[uretor] air box without being attached and closed." According to the FAA inspector who examined the aircraft following the accident, this is the method by which the pilot constructed the airplane. According to the inspector, the 2-inch hose is not large enough to adequately supply enough heat to the carburetor to sufficiently melt the ice. The aircraft was issued an airworthiness certificate by the FAA on August 24, 1995. ________________________________________________________________________________
From: JLINKJR(at)aol.com
Date: Mar 09, 2002
Subject: Re: TruTrak autopilot system
I have the digiflight 100 with GPSS. It is installed in the plane and I have had it powered up. It seems like it will be an excellent system and installation was a snap. There is so much info I could give but it would be best to hear it from the experts at tru-trak. The # is 501-751-0250 and ask for chuck. John Link rv-8 ________________________________________________________________________________
Date: Mar 09, 2002
From: Robert McCallum <robert.mccallum2(at)sympatico.ca>
Subject: Re: Carb Heat Muff/Accident...
KAKlewin(at)aol.com wrote: > > Listers, > > Came upon the incident below while surfing the net...and it made me wonder if the design has been changed at all or if anyone one has come up with a better way to work the carb heat problem?? The long report basically said the 2" hose to the FAB is inadequate and a bad design? Just curious... > > Kurt in OKC, RV6AQB, Finishing.... > Kurt; If you check the archives on this subject you will find that this topic came up not too long ago. The scary part of that discussion was the number of builders who felt that carburettor ice wasn't something that could affect them and therefore they weren't going to install (or didn't have) any provision for carb heat at all. That discussion also mentioned the adequacy/inadequacy of Van's design. The opinions were about as varied as the number of responders. As you can gather from the incident report you found, if you have a carb you NEED carb heat and when you need it you need lots of it. You may not need it often, but when you need it, you really need it. Bob McC ________________________________________________________________________________
From: "joe hine" <joehine(at)nbnet.nb.ca>
Subject: Re: Gross Weight Determinations
Date: Mar 09, 2002
I was going to fire off a flamer here, but I'll bite my tonge and just wonder why some people have to say things in a forum that has people from all over the world participating, that serves no purpose and pisses some of us off? Joe Hine Not native Canadian but CHOOSE to live here. > > We can fly into Canada any time we want. But live there? Under that type of > oppressive bureaucracy? No way! > > Bruce > Glasair III > ________________________________________________________________________________
From: JGSinger(at)aol.com
Date: Mar 09, 2002
Subject: RV-9A Quickbuild For Sale
A friend of mine needs to sell his RV-9A Quickbuild kit. He is not computer savvy so I told him I would put it on the list for him. Included is the following: Empenage: Completed with electric trim and light on bottom tip. Fiberglass tips not yet installed. Wings: Ready for ailerons and flaps. Control rod and final top skin not yet installed. Fuselage: Quickbuild - not touched. Flaps & Ailerons: Ready to install. Vans prepunched instrument panel. Two landing lights. Right & left step kits. All plans, documents & inventory sheets. Fiberglass kit w/ resin, etc. 6 Bench Grinder All Avery Tools: Squeezer sets Dimple dies Air line swivel 3X rivet gun Pin punches Scotchbrite pads and wheel Vixen file Rivet cutter 1/8 rivet set 3/4 flush set w/guard Back rivet set Micro-stop Countersinks Speed deburr tool Rivet gauges Cleco Pliers 12 steel rule Wiss snips R&L 10 #10 (3/16) Clecoes Avery hand squeezer Drill stop set 100 #40 (3/32) Clecoes Clamps 50 #30 (1/8) Clecoes Back rivet plate Bucking bars Drill bits This kit is set up for a tip-up canopy. Everything you need to start building the day you get it! He has $22,296.54 invested in everything. He is asking $18,000.00 for the whole thing. It is located in a hangar at Front Range Airport (FTG) which is located in Watkins, Colorado just east of Denver. If you are interested in owning a real nice RV-9A Quickbuild, his name is Jerry Lippert and he can be reached at (303) 751-1755. Thanks, John Singer RV-6A - Denver, CO Wheels, tires, wing gap seal, waiting on engine, etc . . . http://www.jgsinger.com/rv ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Re: TruTrak autopilot system
Date: Mar 09, 2002
Have you coupled it to a GPS? Which one? Was it difficult? In one of the many mental interations of my panel, I couple the trutrak to my garmin 295 (handheld) gps. But...the trutrak web site specfically does NOT recommend this, saying handhelds are not accurate enough. Sounds like some weak CYA talk to me...... - Larry Bowen RV-8 fuse Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of > JLINKJR(at)aol.com > Sent: Saturday, March 09, 2002 7:46 PM > To: rv-list(at)matronics.com > Subject: RV-List: Re: TruTrak autopilot system > > > > I have the digiflight 100 with GPSS. It is installed in the > plane and I have > had it powered up. It seems like it will be an excellent system and > installation was a snap. > There is so much info I could give but it would be best to > hear it from the > experts at tru-trak. The # is 501-751-0250 and ask for chuck. > > John Link > rv-8 > > > ========== > ========== > ========== > ========== > > > > > ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Mar 10, 2002
Subject: Re: Anodizing fuel caps
one last thing about anodizing, it fades in the sunlight. chris ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Mar 09, 2002
Subject: Re: Anodizing fuel caps
In a message dated 3/9/2002 7:22:28 AM Pacific Standard Time, czechsix(at)juno.com writes: > I did some more research on the fuel caps > supplied by Vans (made by Usher) and was told that they cannot be > anodized.....they are a casting that includes other metals along with > aluminum, and have a high silicon content. To get good results with > anodizing you need a machined aluminum alloy. Cast and welded aluminum pieces are notorious for not looking as good as machined plate when anodized, but not really for the reason you mentioned. All aluminum alloys contain other metals and silicon is one of the two principle alloying elements (with magnesium) in the popular 6XXX series aluminum, which anodize beautifully. Both the variations in the density and hardness of the cast material and the nonuniform oxide (a ceramic) layer that forms during the casting process are what interfere to varying degrees with the anodizing process. The dye that is used to provide coloring of the anodized surface and the subsequent sealing require a properly configured oxide matrix on the entire surface to fill to the same degree in order to look uniform to the eye. Incidentally these dyes look great when new but don't really standup well to UV exposure, so painting might be preferred. On the fuel cap you really only need a good looking top surface so, if you still want to anodize, it may help to grain (similar to a deep sanding in a single axis) just this surface to expose clean, fresh and more uniform metal first. -GV (N1GV) ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)new.rr.com>
Subject: F6101 and firewall weldment
Date: Mar 09, 2002
Fellow listers: I am working on fitting my diagonal longerons between the firewall and F604 on my 6A. I have been trying to trim the F6101 gusset so that the angle the longeron I am fitting works out with the predrilled holes in the firewall weldment. The very last hole in the aft end of the weldment is causing concern, because if I drill through it and the longeron, the hole will be right at the edge of the longeron. Poor edge distance to say the least. I do not see any reference in the plans regarding the location of the aft end of the diagonal longeron. I am concerned that if I trim the F6101 gusset enough to make that last weldment hole work, I will reduce the distance between the angled longeron and the bottom front longeron too much. I have measured this distance just as a starting point on the plans and it appears that as drawn, that distance should be about 8". There is no way that this measurement works out the way the firewall weldment is predrilled. Is this a concern??? Should I go have a few barley pops and chill out??? Thanks in advance gang. Regards, Jeff Orear RV6A fuse Peshtigo, WI ________________________________________________________________________________
Date: Mar 10, 2002
Subject: RV-8/A rear seat riser
From: czechsix(at)juno.com
I got some info from D.J. Lauritsen today regarding her seats for the -8A. There's a set of simple plans to build a seat "riser" for the back seat out of metal to reduce the thickness of cushion required (and save weight I assume?). Anyway, it shows an angled platform approx 17" X 12" made out of .032" alum, with one rib on each side made out of .025" alum. Just wondering, for you guys already flying with this configuration, have you found this design to be strong enough without any additional ribs or stiffeners in it? Seems like if a big bubba were to sit back there it might just cave in.....? Thanks, --Mark Navratil Cedar Rapids, Iowa RV-8A finish kit stuff....should be flying any year now.... ________________________________________________________________________________
From: "Jerry Carter" <jcarter8(at)midsouth.rr.com>
Subject: Re: RV-8/A rear seat riser
Date: Mar 10, 2002
> > I got some info from D.J. Lauritsen today regarding her seats for the > -8A. There's a set of simple plans to build a seat "riser" for the back > seat out of metal to reduce the thickness of cushion required (and save > weight I assume?). Anyway, it shows an angled platform approx 17" X 12" > made out of .032" alum, with one rib on each side made out of .025" alum. > Just wondering, for you guys already flying with this configuration, > have you found this design to be strong enough without any additional > ribs or stiffeners in it? Seems like if a big bubba were to sit back > there it might just cave in.....? > > Thanks, > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A finish kit stuff....should be flying any year now.... I don't know why you would need this. Becky Orndorff made my seats, and she just asked for a few measurements of the pilot and the passenger. My wife, who is about 5'4" sits on a cushion to raise her up and give her better visibility. But guys of average height like the height just fine. It seems like you would want the seat a little low for short people so that bigger folks wont cram their head against the canopy. Jerry Carter RV-8A ________________________________________________________________________________
From: WFACT01(at)aol.com
Date: Mar 10, 2002
Subject: Re: RV-8/A rear seat riser
MARK-You should have 4 ribs-also put 2 large lighting holes under the cushion for storage-TOM Thomas M. Whelan Whelan Farms Airport Post Office Box 426 249 Hard Hill Road North Bethlehem, CT 06751 PH 203-266-5300 FAX 203-266-5140 e-mail wfact01(at)aol.com EAA Chapter 1097, President RV-8 IO-540 LYC ________________________________________________________________________________
Date: Mar 10, 2002
Subject: fin wraps
From: "Robert Dickson" <bubba(at)coastalnet.com>
I'm ready to tie the cylinder baffle fin wraps together, using the safety wire and brake line method. My question is, do you cover the entire length of the safety wire between the wraps with the brake line? If that's so, then Van shorted me on brake line. I've got one piece of tube that's 20" long, which looks like it would be enough to do the two inner wraps with very little left over for the outer wraps. Am I missing something? Robert Dickson RV-6A, putting baffles on for the last time, I hope ________________________________________________________________________________
From: "Tim Lewis" <timrv6a(at)earthlink.net>
Date: Mar 10, 2002
Subject: Wobble Test (SB 388B)
Listers, It's nearing time for me to do the 400 hour exhaust valve guide clearance checks on my O-360. There appear to be two methods of accomplishing this. The first uses an ST-71 fixture and gage adapter with a dial indicator. I have no idea how much these cost. The second method of doing the test has you drop the exhaust valve into the cylinder and test exhaust valve guide clearance using a set of GO/NO-GO gages [if you don't like that spelling complain to Lycoming ; -) ]. For the O-360 the GO gage is .4985, and the NO-GO gage is .4995. I have no idea where to find these gages. I'm looking for advice on which method to use (fixture vs GO/NO-GO), and for likely sources and costs of the fixture and/or gages. Thanks, Tim Lewis ****** Tim Lewis -- HEF (Manassas, VA) RV-6A N47TD - First Flight 18 Dec 99 http://www.geocities.com/timrv6a ****** ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: RV-8/A rear seat riser
Date: Mar 10, 2002
> >I got some info from D.J. Lauritsen today regarding her seats for the >-8A. There's a set of simple plans to build a seat "riser" for the back >seat out of metal to reduce the thickness of cushion required (and save >weight I assume?). Anyway, it shows an angled platform approx 17" X 12" >made out of .032" alum, with one rib on each side made out of .025" alum. > Just wondering, for you guys already flying with this configuration, >have you found this design to be strong enough without any additional >ribs or stiffeners in it? Seems like if a big bubba were to sit back >there it might just cave in.....? > >Thanks, > >--Mark Navratil >Cedar Rapids, Iowa >RV-8A finish kit stuff....should be flying any year now.... > > Mark, I built the seat riser per plans, EXCEPT that I used only two ribs; one on each side. The inner two ribs were replaced with crosswise angles. I believe Randy Lervold did the same thing. I've had some mega bubbas sitting on it with no problems at all. By removed the two inner ribs, you have a very nice storage space available to you by removing the seat cushion, and lifting the pan up. This can be a very nice place to store things that are not usually needed...like some small survival goodies, a gun (you just never know), paperwork, etc. By pulling the two hinge pins that hold it to the floor, it can be removed for really tall pax. You just put the cushion flat on the floor. Brian Denk RV8 N94BD 279 hrs. MSN Photos is the easiest way to share and print your photos: http://photos.msn.com/support/worldwide.aspx ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Wobble Test (SB 388B)
Date: Mar 10, 2002
You used to be able to borrow the wobble valve jig from Lycoming. Don't know it you still can or not. Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh ----- Original Message ----- From: "Tim Lewis" <timrv6a(at)earthlink.net> Subject: RV-List: Wobble Test (SB 388B) Listers, It's nearing time for me to do the 400 hour exhaust valve guide clearance checks on my O-360. There appear to be two methods of accomplishing this. The first uses an ST-71 fixture and gage adapter with a dial indicator. I have no idea how much these cost. The second method of doing the test has you drop the exhaust valve into the cylinder and test exhaust valve guide clearance using a set of GO/NO-GO gages [if you don't like that spelling complain to Lycoming ; -) ]. For the O-360 the GO gage is .4985, and the NO-GO gage is .4995. I have no idea where to find these gages. I'm looking for advice on which method to use (fixture vs GO/NO-GO), and for likely sources and costs of the fixture and/or gages. Thanks, Tim Lewis ****** Tim Lewis -- HEF (Manassas, VA) RV-6A N47TD - First Flight 18 Dec 99 http://www.geocities.com/timrv6a ****** ________________________________________________________________________________
From: "Donald Mei" <don_mei(at)hotmail.com>
Subject: Gross weight
Date: Mar 10, 2002
I get the list in a summary form, so this may have already been said, if so, my apologies. You can make the gross weight anything you want. So long as during your test flying, you test fly the aircraft at that weight and determine that it handles correctly (I forget the exact term) I purchased my airplane but have gotten pretty familiar with the regs. One interesting aside. My RV-4 was built by a man who was a bit. . well large. (Bubbas in Vans terminology) He certified the airplane with a gross weight of 1700#. But, not being a stupid man, he stayed within Vans recommended CG specs. To keep within CG limits required balast. So, when I purchased my plane, it weighed 970# with 30 lbs of balast hung off the front of the engine to move the CG forward. He w&b shows it is withing envelope with a 200# pilot and a 200# passenger and 20 lbs of bagage. Since neither my fiance nor I weigh anywhere near #200, I remved the weights and reworked the w&b. The bottom line is this: Legal Perspective: if you test fly the aircraft at all ends of a given CG and GW envelope during your test phase, those are the legal limits. (You can even re-certify an aircraft for higher cg if you want) Common Sense Perspective: Stay within Vans CG limits, these planes get spooky when the aft limit is approached. Use Vans GW limit as a guide. If you fly out of a 5000 foot x 150 foot paved airport, only fly on nice days and are a model of smoothness, the excess power and control authority our RVs are blessed with can allow you to operate safely at well over Vans recommended gross. Just look at John Johanson. His plane's gross weight was 2040#. However, if you fly from a 800 foot grass field and are fond of bush pilot, full stall, drop it in type landings, then you had better pay attention to gross weight. Its all about your margin of safety and how much you need to feel comfortable. You make your decisions and take your chances. Don Mei MSN Photos is the easiest way to share and print your photos: http://photos.msn.com/support/worldwide.aspx ________________________________________________________________________________
Date: Mar 10, 2002
Subject: Re: Compaq Ipaq Cheap for Anywhere map buyers
From: "Glenn Bridges" <robwil(at)nlamerica.com>
dear scott, i live in central ga. but fly down to ssi frequently, and have been there on vacation many times. i will call you mon at the "bank". thanks for the response, glenn 478-275-0200 ---------- >From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com> >To: rv-list(at)matronics.com >Subject: RE: RV-List: Compaq Ipaq Cheap for Anywhere map buyers >Date: Thu, Mar 7, 2002, 1:52 PM > > >Don Mei originally said that OfficeMax was selling the 3635 for that low >price. 3635 is the color model, not the monochrome. I've never seen the >monochrome model anywhere. > >Scott VanArtsdalen, MCSE, CCNA >Network Administrator >Union Safe Deposit Bank >209-946-5116 > > -----Original Message----- >From: Finn Lassen [mailto:finnlassen(at)netzero.net] >Sent: Thursday, March 07, 2002 10:09 AM >To: rv-list(at)matronics.com >Subject: Re: RV-List: Compaq Ipaq Cheap for Anywhere map buyers > > >Mike, why are you quoting specs on the Color model? The 3135 or 3035 is >monochrome! > >That's why the much lower price. The screen! > >Finn > >Mike Plecenik wrote: > >> >> >From Amazon.c: (they're still asking over $500. new & over $300. used) >> >> Standard memory: 32 MB RAM, 16 MB ROM >> Maximum memory: Up to 64 MB with card >> Expansion slot: CompactFlash >> Display type: Color-reflective TFT LCD (indoor/outdoor) >> Display colors: 4,096 (12-bit) >> Display size: 2.26 by 3.02 inches >> Resolution: 240 by 320 pixels >> Display backlight: Yes, ambient-light sensor adjusts automatically >> Processor: 206 MHz Intel StrongARM SA-1110 32-bit RISC >> Operating system: Microsoft Windows for Pocket PCs >> PC compatible: Yes >> Mac compatible: No >> PC system requirements: 486 MHz processor or higher, Windows 98 or 2000 >for >> USB synchronization, USB port, CD-ROM drive >> Handwriting recognition: Yes >> Keyboard: On-screen >> User controls: On/off, light, menu, speaker/5-way joystick, contacts, >> calendar >> Memo pad: Yes >> Address book: Yes >> Scheduler: Yes >> E-mail: Yes >> Web browser: Yes >> Security: Password protection >> Stereo: Yes >> Built-in speaker: Yes >> Headset jack: Yes (3.5mm stereo) >> Voice recorder: Yes >> MP3 playback: Yes >> Audible content playback: Yes >> AC adapter included: Yes >> Battery type: 950 mAh Lithium Polymer >> Batteries included: Yes >> Average battery life: 12 hours >> Serial port: Yes, with optional Compaq serial cradle >> USB: Yes >> Infrared: Yes >> Wireless: Yes >> Docking cradle: USB cradle included >> PC cable: Yes >> Other hardware: Two styli, vinyl slipcase, AC adapter >> Software: Pocket PC software: Pocket Word, Pocket Excel, Pocket Internet >> Explorer, Windows Media Player, Inbox, Microsoft Reader, File Explorer, >> Asset Viewer, Picture Viewer; Desktop software: Microsoft Active Sync 3.1, >> Microsoft Money for Pocket PC, Pocket Streets, Outlook 2000, Internet >> Explorer 5.0, Media Manager, Tscribe, Microsoft Reader e-book samples >> Width: 3.28 inches >> Height: 0.62 inches >> Depth: 5.11 inches >> Weight: 6.3 ounces >> Warranty, parts: 1 year >> Warranty, labor: 1 year >> >> > >> > Maybe - this is the monochrome - not color screen. >> > >> > Finn >> > >> > Donald Mei wrote: >> > >> > > >> > > I just got this email from a "deals" oriented email list: >> > > >> > > OfficeDepot - Compaq iPaq 3635 PocketPC for $179.99 at Brick and >Mortar >> > > OfficeDepot (i.e. the actual store, not the web site) This one is on >> > > clearance at your local retail Office Depot store. They`re really >> running >> > > out of stock though, and they`re not getting any more in. The SKU# >for >> this >> > > product is 858-251. Best of luck! >> > > >> > >---------------------------------------------------- >Sign Up for NetZero Platinum Today >Only $9.95 per month! >http://my.netzero.net/s/signup?r=platinum&refcd=PT97 > > ________________________________________________________________________________
Date: Mar 10, 2002
From: Charles Brame <charleyb(at)earthlink.net>
Subject: Anodizing fuel caps
I'm not sure if chrome or nickel plating falls under the same guidelines as anodizing. Can Van's (Usher) fuel caps be chrome or nickel plated? Charlie Brame RV-6A QB N11CB (Res.) San Antonio ------------------------------------------ > Subject: RV-List: Anodizing fuel caps > From: czechsix(at)juno.com > > > Guys, FYI for the archives, I did some more research on the fuel caps > supplied by Vans (made by Usher) and was told that they can NOT be > anodized.....they are a casting that includes other metals along with > aluminum, and have a high silicon content. To get good results with > anodizing you need a machined aluminum alloy. I've looked through some > catalogs (Aircraft Spruce, etc...) and there are several other caps > available that would work, but none of them look compatible with the > Usher caps.....it would have to be fitted with their own filler necks > when the tanks are assembled. So my fuel caps will have to be painted > instead : ( > > As a side note, the guy I talked to who does the castings said that if > you don't want the paint to chip off so easily, you need to etch/alodine > the caps before paint. Apparently the surface of the caps is > contaminated by the mold release stuff, and just wiping it with MEK or > equivalent will not clean it well enough for a really good paint > bond......it'll stick ok, but will be more prone to chipping or peeling > off than a surface prepared with etch/alodine. > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A finish kit stuff.... > ________________________________________________________________________________
Date: Mar 10, 2002
From: emrath(at)comcast.net
Subject: Re: F6101 and firewall weldment
Jeff, not sure what your driving at exactly. I am building a -6A and my weldments were not predrilled. I followed Justice's notes on this. The F6101 does get trimmed quite a bit to follow the diagonal angle. I've looked at mine and you are correct, the last hole in the weldment is very close to the edge of the angle. See Justice on this, I believe his notes talked about this. The aft end of this angle, butts up against the F-604. My drawing shows a dimension of 8" from the bottom (top in the jig) of the F-604. Hope this helps. Marty in Brentwood TN ----- Original Message ----- From: "Jeff Orear" <jorear(at)new.rr.com> Subject: RV-List: F6101 and firewall weldment > > Fellow listers: > > I am working on fitting my diagonal longerons between the firewall and > F604 on my 6A. I have been trying to trim the F6101 gusset so that the > angle the longeron I am fitting works out with the predrilled holes in > the firewall weldment. The very last hole in the aft end of the > weldment is causing concern, because if I drill through it and the > longeron, the hole will be right at the edge of the longeron. Poor edge > distance to say the least. I do not see any reference in the plans > regarding the location of the aft end of the diagonal longeron. I am > concerned that if I trim the F6101 gusset enough to make that last > weldment hole work, I will reduce the distance between the angled > longeron and the bottom front longeron too much. I have measured this > distance just as a starting point on the plans and it appears that as > drawn, that distance should be about 8". There is no way that this > measurement works out the way the firewall weldment is predrilled. Is > this a concern??? Should I go have a few barley pops and chill out??? > Thanks in advance gang. > > > Regards, > > Jeff Orear > RV6A > fuse > Peshtigo, WI > > ________________________________________________________________________________
From: "Randy Lervold" <randy@rv-8.com>
Subject: Re: RV-8/A rear seat riser
Date: Mar 10, 2002
> I built the seat riser per plans, EXCEPT that I used only two ribs; one on > each side. The inner two ribs were replaced with crosswise angles. I > believe Randy Lervold did the same thing. I've had some mega bubbas sitting > on it with no problems at all. By removed the two inner ribs, you have a > very nice storage space available to you by removing the seat cushion, and > lifting the pan up. This can be a very nice place to store things that are > not usually needed...like some small survival goodies, a gun (you just never > know), paperwork, etc. > > By pulling the two hinge pins that hold it to the floor, it can be removed > for really tall pax. You just put the cushion flat on the floor. > > Brian Denk > RV8 N94BD > 279 hrs. Yep, leave out the two middle ribs and put in a couple of stiffeners, works great. And I think I made mine out of slightly thicker material than called for in DJ's plans to help compensate for eliminating the two center ribs. I thought I had a pic of mine on my web site but I guess not. I'll try to add one. BTW, one of the benefits of using the riser rather than just thicker cushions is that you build some angle into the seating surface. With plain cushions I would think there's a tendency for the seat bottom to slide forward. Randy Lervold RV-8 N558RL 151 hrs. www.rv-8.com ________________________________________________________________________________
From: "Joe Larson" <jpl(at)showpage.org>
Subject: Shelf age of pro-seal
Date: Mar 10, 2002
Okay, I have a supply of pro-seal that's been in my fridge for a few years. Any chance the stuff is still good? Anyone able to tell me how to test to see if it's any good? It's been opened and a modest amount used, but then it's been sealed and fridged ever since. I'm about to head back downstairs and finish prepping my tanks for riveting. I'd love to turn around and finish these suckers later this week. -Joe ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: Gross weight
Date: Mar 10, 2002
Agreed. On my trip to Monterey, we were close to aft limit with all of our bags. No matter your airspeed, it is virtually impossible to do a "flat" landing. Your nose is pitched way up. and the airplane doesn't fly too well at slow speeds. Van's airplanes are great machines, and are extremely easy to fly. However, when you are loaded close to aft CG limit, it can be very tricky to land one of these. (Especially with a lightweight starter and wood prop). Yes, you should test fly at all limits. However, I would wait to do the test flying for weight and balance till the end of your test flying period, so that you are completely familiar with your airplane's handling characteristics. I got to where I could grease my landings just about everytime. However, I was quite humbled when I flew with an aft CG limit. Paul Besing RV-6A Sold http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "Donald Mei" <don_mei(at)hotmail.com> Subject: RV-List: Gross weight > > I get the list in a summary form, so this may have already been said, if so, > my apologies. > > You can make the gross weight anything you want. So long as during your > test flying, you test fly the aircraft at that weight and determine that it > handles correctly (I forget the exact term) I purchased my airplane but > have gotten pretty familiar with the regs. One interesting aside. My RV-4 > was built by a man who was a bit. . well large. (Bubbas in Vans terminology) > He certified the airplane with a gross weight of 1700#. But, not being a > stupid man, he stayed within Vans recommended CG specs. To keep within CG > limits required balast. So, when I purchased my plane, it weighed 970# with > 30 lbs of balast hung off the front of the engine to move the CG forward. > He w&b shows it is withing envelope with a 200# pilot and a 200# passenger > and 20 lbs of bagage. Since neither my fiance nor I weigh anywhere near > #200, I remved the weights and reworked the w&b. > > The bottom line is this: > > Legal Perspective: if you test fly the aircraft at all ends of a given CG > and GW envelope during your test phase, those are the legal limits. (You > can even re-certify an aircraft for higher cg if you want) > > Common Sense Perspective: Stay within Vans CG limits, these planes get > spooky when the aft limit is approached. Use Vans GW limit as a guide. If > you fly out of a 5000 foot x 150 foot paved airport, only fly on nice days > and are a model of smoothness, the excess power and control authority our > RVs are blessed with can allow you to operate safely at well over Vans > recommended gross. Just look at John Johanson. His plane's gross weight > was 2040#. > > However, if you fly from a 800 foot grass field and are fond of bush pilot, > full stall, drop it in type landings, then you had better pay attention to > gross weight. > > Its all about your margin of safety and how much you need to feel > comfortable. You make your decisions and take your chances. > > Don Mei > > > MSN Photos is the easiest way to share and print your photos: > http://photos.msn.com/support/worldwide.aspx > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Shelf age of pro-seal
Date: Mar 10, 2002
Hi Joe, The Van's sealant that I have is fridge kept and still seems ok after Two years. I used it to seal the naca vents. Opinion: That said I would not trust it to seal tanks now. I don't think saving the cost of new sealant and the work required should things go wrong is worth the risk. Jim In Kelowna ----- Original Message ----- From: "Joe Larson" <jpl(at)showpage.org> Subject: RV-List: Shelf age of pro-seal > > Okay, I have a supply of pro-seal that's been in my fridge for a few years. Any > chance the stuff is still good? Anyone able to tell me how to test to see if it's > any good? > > It's been opened and a modest amount used, but then it's been sealed and > fridged ever since. > > I'm about to head back downstairs and finish prepping my tanks for riveting. > I'd love to turn around and finish these suckers later this week. > > -Joe > > ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: Shelf age of pro-seal
Date: Mar 10, 2002
This is my humble opinion so take it for what it's worth. But I'd say that if its been in your fridge the whole time then theres a good chance its still okay. Overall if it's still workable and relatively easy to mix and stir, then I doubt it's lost any significant sealing/adhesive properties. If its stiff enough that you have a hard time stirring/mixing it with the catalyst then I'd say it's old to use on your tanks. I have dug some pockets of "workable" stuff out of otherwise unworkable cans of proseal to do non-critical adhesive/sealant applications, and that still ends up working fine, but I wouldn't use it on the tanks unless the whole can was still nice and workable. Sometimes the top does skin over and if thats all that's bad then I'd say scrape off the top and go for it. Randall Henderson, RV-6 N6R (~300 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
From: "Joe Larson" <jpl(at)showpage.org>
Subject: Quality Construction
Date: Mar 10, 2002
Okay, there's been some discussion on building quality. I make mistakes. I suspect everyone does. The most glaring ones obviously need to be dealt with. I'm wondering when people decide to replace a part. When riveting skins, do you redo every rivet you're not happy with, or only if you have a few together. (I've sorta been using the theory that I'm likely to do as much damage drilling out one bad rivet to redo than the weakness implied by one or two bad rivets.) How much effort do people spend getting rivets in JUST the right spot (for those of use who have choices). Do you eyeball 3/8ths inches from the edge (or whatever), or do you take the other extreme -- measure it carefully, mark with a fine-tooth device, then center-punch it before drilling? Basically, I'm trying to decide just how careful I need to be to do a safe airplane. I'm not trying to win any builders awards, but I don't want the other RV guys to take a look and think, "Not flying in that one". -Joe ________________________________________________________________________________
From: "Joe Larson" <jpl(at)showpage.org>
Subject: Building tip: aligning ribs
Date: Mar 10, 2002
Well, this might be obvious to everyone else, but I'm on the end of my wings and finally figured out how to reduce my frustration on things like the fuel tanks. The problem: matching the center of ribs in stuff like the fuel tanks or the flaps with the pre-punched holes in the skins. The old method: use a sharpie to draw a line down the center of the rib flange. Sight through the skins then jockey the rib around until the line is centered, or at least centered within tolerances. The problem: trying to move the rib around while looking through the holes would drive me INSANE. I'd move the rib, look, move, look, move look, scream, run upstairs for a while, go back down, move the rib... You get the idea. The solution: I used the same sharpie to mark the insides of the skins. Mark alongside the line of holes on BOTH sides, 1/2 the width of the rib flange from the holes. You still need to eyeball through the skins, but the initial placement is always MUCH closer. Frustration is reduced dramatically. -J ________________________________________________________________________________
From: "Joe Larson" <jpl(at)showpage.org>
Subject: Duckworks Landing Lights: Lens Shape
Date: Mar 10, 2002
Okay, I've got my duckworks landing lights installed in both wings. And I'm not very happy with it. I'm going to have to redo the plexi lenses before I fly. The problem -- the precurved shape of the lens didn't match the shape of my wings. I don't care to wonder why too hard, but I choose to believe it's the lens that was out of shape, NOT my wing. I tried two solutions to this, with the second one tried in a few different ways. The first solution was force. No joy at all. You can't reach in from the back side, because you won't have access to the back once everything is installed. So the force you are allowed to apply is relatively small. So the next thing I tried -- I tossed the lens on a cookie sheet and threw it in the oven. I slowly increased the oven temperature until the lens started to sag. I let it bake like that for a couple of minutes, opening the oven to check to see how soft it was periodically. I found that sufficient temperature to make it mostly lie flat didn't heat it enough to make the part that was already pre-curved the most soften up. In the end, I had to reach temperatures very close to 400 degrees. I then took it out and as quickly as I could, dropped it over the nose of my leading edge. However, as it cooled, the edges lifted up, so I still didn't have the right shape. Repeated that a few times -- no joy. Tried heating even hotter, and it started sticking (badly) to the cookie sheet. Shut it all down for a day. Built a wing subsection that I can fit into the oven. Used particle board and some galvanized steel I had sitting around. Got the shape as close to wing shaped as I could, although the galvanized is a little hard to curl. It's close, but not perfect. I then tried the oven thing again, letting the lens soften and form around this structure I made. That got it closer to the shape needed, so I went ahead and finished the installation. However, once done, I'm still not very happy with the shape -- it just doesn't sit in there flat, and I have a gap sufficient to fill the entire area with water if I fly in the rain. NOT satisfied. If push came to shove, I could caulk it. But that's a pretty lazy solution. And I don't like the amount of local turbulence I'm going to have from a non-smooth leading edge. So I intend to try both lenses AGAIN. I'd love to hear suggestions. It seemed like I was work-hardening the plexi, so I was afraid to just keep trying with it -- I thought it might get brittle or something. What I'd love to do is hang a sheet of plexi over the REAL wing and nail it with a heat gun of some sort. Would that work? --- I'm also not happy with the double-sided-tape method of holding the aluminum strips on the inside of the lenses. That tape just doesn't hold. While monkeying around trying to get screws to start threading, stuff comes unstuck. I'm not happy about that, either. Does anyone have suggestions? --- The duckworks system seems like a good idea, but getting the lens to fit properly wasn't working for me. -Joe ________________________________________________________________________________
From: "Henley" <henley(at)seii.net>
Subject: RV6 For Sale
Date: Mar 10, 2002
Listners, My RV7 is nearing completion so guess it is time to sell my RV6. It is 160HP, Aymar-Demuth, slider, Orndorf interior, engine monitor, Elect aileron and elev trim, elect flaps, Navaid coupled to Lorance airmap,IFR equiped and much more. Completed 1998. 510 hrs TTAF and SMOH. $58,000. Can email pictures. John Henley, 850-609-3175 ________________________________________________________________________________
From: "LarryRobertHelming" <lhelming(at)sigecom.net>
Subject: RV7 Firewall Question
Date: Mar 10, 2002
There are four gussets (two each) named F601C and F601F that mount in corners of firewall shown on drawing 19; but, no parts are in kit and there are no instructions in building manual about fabricating them. Larry in Indiana, working on the Fuselage ________________________________________________________________________________
Date: Mar 10, 2002
From: gert <gert(at)execpc.com>
Subject: Re: RV-8/A rear seat riser
Hey Guys Question... do you have to remove this riser to get to the rear luggage department ?? Gert Randy Lervold wrote: > > > > I built the seat riser per plans, EXCEPT that I used only two ribs; one on > > each side. The inner two ribs were replaced with crosswise angles. I > > believe Randy Lervold did the same thing. I've had some mega bubbas > sitting > > on it with no problems at all. By removed the two inner ribs, you have a > > very nice storage space available to you by removing the seat cushion, and > > lifting the pan up. This can be a very nice place to store things that > are > > not usually needed...like some small survival goodies, a gun (you just > never > > know), paperwork, etc. > > > > By pulling the two hinge pins that hold it to the floor, it can be removed > > for really tall pax. You just put the cushion flat on the floor. > > > > Brian Denk > > RV8 N94BD > > 279 hrs. > > Yep, leave out the two middle ribs and put in a couple of stiffeners, works > great. And I think I made mine out of slightly thicker material than called > for in DJ's plans to help compensate for eliminating the two center ribs. I > thought I had a pic of mine on my web site but I guess not. I'll try to add > one. BTW, one of the benefits of using the riser rather than just thicker > cushions is that you build some angle into the seating surface. With plain > cushions I would think there's a tendency for the seat bottom to slide > forward. > > Randy Lervold > RV-8 N558RL 151 hrs. > www.rv-8.com > -- is subject to a download and archival fee in the amount of $500 ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: Duckworks Landing Lights: Lens Shape
Date: Mar 10, 2002
Did you try the "Duct tape handle" method of pulling the lens into the wing LE from the outside as mentioned in the instructions? Worked well for me and in fact for some reason it seems to work better than pushing it from the inside. (if you could get in there). Did you trim the lens so it only extends beyond the hole the minimum needed for the seal and attach strips? Any extra will make it stiffer and less able to form to the wing. I also ground/beveled the edges some since it did curl up just a bit at the edges. Smooth the edges though with very fine sandpaper as the stuff will crack at any stress risers if flexed. The double-sided tape seems to take some time to get a good bond. Rough up the surfaces and clean them first, then clamp the strips on overnight. If that fails, just use proseal. My best suggestion however is to call the man himself, Don "The Duck" Wentz. He's the one who makes the lenses including forming the bend in his oven (though I think he's now turned that over to his wife Janet.) They would have the best advice on how to make it fit your wing, and are good people and anxious for people to be satisfied with the product. Their number should be with the directions. If not drop me a line privately and I'll email it to you. Randall Henderson, RV-6 N6R (~300 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
Date: Mar 10, 2002
From: gert <gert(at)execpc.com>
Subject: Re: Duckworks Landing Lights: Lens Shape
Joe My lenses originally also did not fit very well either and had to heat them up too this is what I did..... I layed the lens inside the leading edge, before the leading edge was installed and used a heatgun to heat the plexi (lexan ??) material slowly till it was just soft/plyable enough to be pushed inside the leading edge curve, then I let it cool. The edges tend to curl if the material is heated too much (way too much in my experience) also, forming over the *outside* will get you close but will not result in a good fit when pushed in from the inside. this is because the *outside* of the plexi must conform to the *inside* of the leading edge, what you are doing is forming the *inside* of the plexi to the *outside* of the leading edge, the material thicknesses are working against you here. try using a heat gun and slowly pushing the plexi inside into the curve of the leading edge. this worked best for me but of course your mileage my differ, let me know if you have any questions. I used proseal to hold the strips against the plexi and did not use anything between the leading edge and the lens. I will put a thin layer of caulk or so on when I do final install. Gert Joe Larson wrote: > > > Okay, I've got my duckworks landing lights installed in both wings. And I'm > not very happy with it. I'm going to have to redo the plexi lenses before I > fly. > > The problem -- the precurved shape of the lens didn't match the shape of my > wings. I don't care to wonder why too hard, but I choose to believe it's the > lens that was out of shape, NOT my wing. > > I tried two solutions to this, with the second one tried in a few different ways. > > The first solution was force. No joy at all. You can't reach in from the back > side, because you won't have access to the back once everything is installed. > So the force you are allowed to apply is relatively small. > > So the next thing I tried -- I tossed the lens on a cookie sheet and threw it > in the oven. I slowly increased the oven temperature until the lens started to > sag. I let it bake like that for a couple of minutes, opening the oven to check > to see how soft it was periodically. I found that sufficient temperature to make > it mostly lie flat didn't heat it enough to make the part that was already pre-curved > the most soften up. > > In the end, I had to reach temperatures very close to 400 degrees. > > I then took it out and as quickly as I could, dropped it over the nose of my > leading edge. > > However, as it cooled, the edges lifted up, so I still didn't have the right shape. > > Repeated that a few times -- no joy. Tried heating even hotter, and > it started sticking (badly) to the cookie sheet. > > Shut it all down for a day. Built a wing subsection that I can fit into the oven. > Used particle board and some galvanized steel I had sitting around. Got the > shape as close to wing shaped as I could, although the galvanized is a little > hard to curl. It's close, but not perfect. > > I then tried the oven thing again, letting the lens soften and form around this > structure I made. > > That got it closer to the shape needed, so I went ahead and finished the > installation. However, once done, I'm still not very happy with the shape -- > it just doesn't sit in there flat, and I have a gap sufficient to fill the entire area > with water if I fly in the rain. NOT satisfied. > > If push came to shove, I could caulk it. But that's a pretty lazy solution. And I > don't like the amount of local turbulence I'm going to have from a non-smooth > leading edge. > > So I intend to try both lenses AGAIN. I'd love to hear suggestions. It seemed > like I was work-hardening the plexi, so I was afraid to just keep trying with > it -- I thought it might get brittle or something. > > What I'd love to do is hang a sheet of plexi over the REAL wing and nail it > with a heat gun of some sort. Would that work? > > --- > > I'm also not happy with the double-sided-tape method of holding the aluminum > strips on the inside of the lenses. That tape just doesn't hold. While monkeying > around trying to get screws to start threading, stuff comes unstuck. I'm not > happy about that, either. Does anyone have suggestions? > > --- > > The duckworks system seems like a good idea, but getting the lens to fit > properly wasn't working for me. > > -Joe > -- is subject to a download and archival fee in the amount of $500 ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: RV-8/A rear seat riser
Date: Mar 10, 2002
Are plans/illustrations for the seat riser on the web somewhere? - Larry Bowen RV-8 fuse Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Randy Lervold > Sent: Sunday, March 10, 2002 1:58 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: RV-8/A rear seat riser > > > > > I built the seat riser per plans, EXCEPT that I used only two ribs; > > one on each side. The inner two ribs were replaced with crosswise > > angles. I believe Randy Lervold did the same thing. I've had some > > mega bubbas > sitting > > on it with no problems at all. By removed the two inner ribs, you > > have a very nice storage space available to you by removing > the seat > > cushion, and lifting the pan up. This can be a very nice place to > > store things that > are > > not usually needed...like some small survival goodies, a > gun (you just > never > > know), paperwork, etc. > > > > By pulling the two hinge pins that hold it to the floor, it can be > > removed for really tall pax. You just put the cushion flat on the > > floor. > > > > Brian Denk > > RV8 N94BD > > 279 hrs. > > > Yep, leave out the two middle ribs and put in a couple of > stiffeners, works great. And I think I made mine out of > slightly thicker material than called for in DJ's plans to > help compensate for eliminating the two center ribs. I > thought I had a pic of mine on my web site but I guess not. > I'll try to add one. BTW, one of the benefits of using the > riser rather than just thicker cushions is that you build > some angle into the seating surface. With plain cushions I > would think there's a tendency for the seat bottom to slide forward. > > Randy Lervold > RV-8 N558RL 151 hrs. > www.rv-8.com > > > ========== > ========== > ========== > ========== > > > > > ________________________________________________________________________________
From: "Steve Hurlbut" <hurlbut_steve(at)hotmail.com>
Subject: Re: RV7 Firewall Question
Date: Mar 10, 2002
They are in the brown bags. #1981. Steve RV-7A >From: "LarryRobertHelming" <lhelming(at)sigecom.net> >Reply-To: rv-list(at)matronics.com >To: >Subject: RV-List: RV7 Firewall Question >Date: Sun, 10 Mar 2002 15:39:26 -0500 > > >There are four gussets (two each) named F601C and F601F that mount in >corners of firewall shown on drawing 19; but, no parts are in kit and >there are no instructions in building manual about fabricating them. > >Larry in Indiana, working on the Fuselage > > ________________________________________________________________________________
From: "Dana Overall" <bo124rs(at)hotmail.com>
Subject: RV flight sim
Date: Mar 10, 2002
I know the sim is not real flying but I still enjoy flying my Bonanza from the living room will it is in.................ugh...annual(man, I hate this time of year). Question from a newbee. Any sites out there that have an RV to play with?? I searched the archieves and found only one microsoft flight sim for a 6A and a 4 but the post was from 1999 and the URL is no longer good. Just looking for something to play with. Starting on my second homebuilt. Dana Overall Richmond, KY New 7? Builder MSN Photos is the easiest way to share and print your photos: http://photos.msn.com/support/worldwide.aspx ________________________________________________________________________________
From: JLINKJR(at)aol.com
Date: Mar 10, 2002
Subject: Re: TruTrak autopilot system
I have the digiflight 100 with GPSS coupled to a garmin 430. I have not flown yet and have only pwered up on the ground. Chuck at tru-trak is a decent guy and knows this system inside out. I bet he could tell you if with the combination listed before on the handheld hookup would work. ________________________________________________________________________________
From: "Haywire" <haywire(at)telus.net>
Subject: RV flight sim
Date: Mar 10, 2002
Try http://dkoelzer.murkworks.com/hangarx/ It works with FS98 & seems pretty real. There is a 6/6a, 8/8a & a Sonex TD/TG S. Todd Bartrim 13B rotary powered RV-9endurance (finish kit) C-FSTB (reserved) http://www3.telus.net/haywire/RV-9/C-FSTB.htm > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Dana Overall > Sent: March 10, 2002 4:38 PM > To: rv-list(at)matronics.com > Subject: RV-List: RV flight sim > > > I know the sim is not real flying but I still enjoy flying my > Bonanza from > the living room will it is in.................ugh...annual(man, I > hate this > time of year). > > Question from a newbee. Any sites out there that have an RV to play with?? > > I searched the archieves and found only one microsoft flight sim for a 6A > and a 4 but the post was from 1999 and the URL is no longer good. Just > looking for something to play with. > > Starting on my second homebuilt. > > Dana Overall > Richmond, KY > New 7? Builder > > > MSN Photos is the easiest way to share and print your photos: > http://photos.msn.com/support/worldwide.aspx > > ________________________________________________________________________________
From: "Bill VonDane" <n8vd(at)earthlink.net>
Subject: Shelf age of pro-seal
Date: Mar 10, 2002
Don't use it... If you don't know if it's any good, don't use it... Today I had to remove my tank end plates, and clean all the crap off them and the tanks, because the pro-seal I used to put them a couple of weeks ago never cured... If you think putting pro seal on is bad... Try taking off the crap that never sets up.... -Bill VonDane Colorado Springs, CO RV-8A - N8WV http://vondane.com/rv8a/ -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Joe Larson Subject: RV-List: Shelf age of pro-seal Okay, I have a supply of pro-seal that's been in my fridge for a few years. Any chance the stuff is still good? Anyone able to tell me how to test to see if it's any good? It's been opened and a modest amount used, but then it's been sealed and fridged ever since. I'm about to head back downstairs and finish prepping my tanks for riveting. I'd love to turn around and finish these suckers later this week. -Joe ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: RV-8/A rear seat riser
Date: Mar 11, 2002
>> >Hey Guys > >Question... > >do you have to remove this riser to get to the rear luggage department >?? > >Gert > > Seat back cushion yes, but the bottom cushion and riser, no. It depends on how thick your cushions are as well. YMMV. Brian Denk RV8 N94BD ________________________________________________________________________________
From: "LarryRobertHelming" <lhelming(at)sigecom.net>
Subject: Re: RV7 Firewall Question
Date: Mar 10, 2002
Thanks Steve. I had the info (after taking your advice) all along but in the excitement, after waiting a couple of weeks for the fuselage kit to arrive, I seem to have for a moment lost a builder's required instinct of looking everywhere for a part. You saved me some time, saved some frustration as well, and I thank you. Larry. ----- Original Message ----- From: "Steve Hurlbut" <hurlbut_steve(at)hotmail.com> Subject: Re: RV-List: RV7 Firewall Question > > They are in the brown bags. #1981. > > Steve > RV-7A > > > >From: "LarryRobertHelming" <lhelming(at)sigecom.net> > >Reply-To: rv-list(at)matronics.com > >To: > >Subject: RV-List: RV7 Firewall Question > >Date: Sun, 10 Mar 2002 15:39:26 -0500 > > > > > >There are four gussets (two each) named F601C and F601F that mount in > >corners of firewall shown on drawing 19; but, no parts are in kit and > >there are no instructions in building manual about fabricating them. > > > >Larry in Indiana, working on the Fuselage > > > > > > ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: RV-8/A rear seat riser:pic
Date: Mar 11, 2002
I found a pic of the rear seat riser on my web page at: http://geocities.com/CapeCanaveral/Hangar/9656/fuselage6.html It's only one pic, but hopefully worth a thousand words. Brian Denk RV8 N94BD MSN Photos is the easiest way to share and print your photos: http://photos.msn.com/support/worldwide.aspx ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Mar 10, 2002
Subject: Re: Cessna Master Switch
There is a schematic in the Tony Bingelis books under electrical. Len Leggette RV-8A N901LL (res) Greensboro, N.C. Hanger # 23 at INT ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: marine compass
Date: Mar 10, 2002
The marine compass may not have alitude compensating bellows for the inevitable bubble. W ________________________________________________________________________________
From: "Ross" <rmickey(at)ix.netcom.com>
Subject: Whelan Paower Supply on Ebay
Date: Mar 10, 2002
A frend of mine is selling two newly yellow tagged Whelan stobe power supplies on Ebay. These are the ones you put in the wingtips. Starting price is $200 for the two of them. http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&item=1711731716 Ross ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: marine compass
Date: Mar 11, 2002
How do I tell if it does? The rear of the compass body, where is looks like it was filled, has a thick rubber cover on it. How would it get a bubble, without also leaking? Thanks, - Larry Bowen RV-8 fuse and marine compass Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Wheeler North > Sent: Sunday, March 10, 2002 11:15 PM > To: 'RV-List Digest Server ' > Subject: RV-List: marine compass > > > > The marine compass may not have alitude compensating bellows > for the inevitable bubble. > > W > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Mar 11, 2002
Subject: Re: Anodizing fuel caps
In a message dated 3/10/2002 9:35:02 AM Pacific Standard Time, charleyb(at)earthlink.net writes: > I'm not sure if chrome or nickel plating falls under the same > guidelines as anodizing. Can Van's (Usher) fuel caps be chrome or > nickel plated? Electroless Nickel is a good finish for aluminum, although you need to ensure that it is a good plating shop that does mil-spec work. Electroless Ni throws so well that you can actually plate over scale and dirt, so lack of adhesion would be the chief concern if the article is not properly prepped first. If you want a matte chrome look with good adhesion, I would suggest graining, sanding or bead blasting lightly followed by electrolytic or electroless nickel plating. -GV (N1GV) ________________________________________________________________________________
Date: Mar 11, 2002
From: Jeff Point <jpoint(at)mindspring.com>
Subject: Re: RV flight sim
Flightsim.com has a great RV-6 and 6A for FS2K2. If you don't have 2K2 you need it. File names are rv6a_2k2.zip <http://www.flightsim.com/cgi/kdl/main/50/rv6a_2k2.zip?l7foR05G> and rv6_2k2.zip <http://www.flightsim.com/cgi/kdl/main/50/rv6_2k2.zip?l7foR05G> When I tried to use the older versions from 98 in 2K2 I had no end of trouble, but these two seem to work well. Jeff Point -6 fuselage Milwaukee WI Dana Overall wrote: >Question from a newbee. Any sites out there that have an RV to play with?? > > ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: Gear leg fairings
Date: Mar 11, 2002
Wayne, Go to the internet and find www.teamrocketaircraft.com ... once there, look in their catalog under "fiberglass." Steve Soule -----Original Message----- Hey guy's, I'm new to this site. Who's this "Team Rocket" your talking about. I'd be interested in those gear leg farings. Wayne ________________________________________________________________________________
From: "Glenn & Judi" <dirtyrottenscoundrels(at)attbi.com>
Subject: RV-6 Engine Idle Speed
Date: Mar 11, 2002
Hi, I am running a wood 3 blade prop with a harmonic dampener. Where should I have my idle set on a carb equipped, mag ignition, O-360-A1A? Since the prop doesn't have the inertia that a metal prop has, I thought it might make sense to increase the idle a little. How much? Thanks, Glenn Gordon N442E ________________________________________________________________________________
Subject: Re: RV-List Digest: 54 Msgs - 03/10/02
From: "Philip Chapman" <chapmanp(at)us.ibm.com>
Date: Mar 11, 2002
03/11/2002 08:33:33 AM Does anyone know where I can buy a race prop ?, I know all the standard wood prop manufacturers, but I am after a thin chord section race prop for a high reving 0-320 for handicap racing. Cheers Phil Chapman ________________________________________________________________________________
From: "John Furey" <john(at)fureychrysler.com>
Subject: Vision Micro System
Date: Mar 11, 2002
I"m looking for feedback on the merits of using the Vision Micro system in place of all the individual instruments. Some of my concerns are reliability and what happens if you need to replace just one of the functions. Your comments please. Best wishes, John Furey RV6A ________________________________________________________________________________
Date: Mar 11, 2002
From: Charlie Kuss <chaskuss(at)bellsouth.net>
Subject: Re: thread - rope - cable was gross weight
Don, You forgot to ask if you need to Alodine and prime the lead counterweights in the Rudder and Elevators! Thanks for the laugh. Charlie Kuss >snipped > >I was wonderring what kind of effect a nose wheel or tail wheel has on the >way primer sticks to the aircraft as it relates to CG and gross weight. So, >given my ignorance I have 3 questions for your really smart guys out there, >that includes you Boeing engineers: > >1)what is the best primer >2)Should I put the big wheel in the front or the little one in the back >3)What should the gross weight of my plane be. > >oh yeah,I almost forgot, one more > >4) I can get a great deal on an H2AD, should I buy it? (and how will that >one Extra large mag affect my CG and Gross weight. and do I need to prime >the magneto?? ) > >I think that the prime may have the most effect on my cg since it is prime. >If I do prime, I could always put balast in the tanks with the proseal. ?? > >Please advise. ________________________________________________________________________________
From: "Jim Norman" <jnorman(at)intermapsystems.com>
Subject: Vision Micro System
Date: Mar 11, 2002
John, Before you decide to go with a VM 1000, take a look at the IK-2000. We have hashed this out a bit several months ago, but this is a really cool unit with great features... I think it is the best engine monitor on the market...for less Canadian (or US) dollars than the VM 1000. See it here: http://www.i-ktechnologies.com Jim tampa -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of John Furey Subject: RV-List: Vision Micro System I"m looking for feedback on the merits of using the Vision Micro system in place of all the individual instruments. Some of my concerns are reliability and what happens if you need to replace just one of the functions. Your comments please. Best wishes, John Furey RV6A ________________________________________________________________________________
From: "Cole, Ed" <Ed_Cole(at)maximhq.com>
Subject: New starter For Sale
Date: Mar 11, 2002
Listers-- I have a brand new Electro Systems starter for sale. It is a 149 tooth model MZ4222 taken of a factory remanufactured IO360A1B6. Selling for $200 plus shipping This lists in ACS for $262 plus a $200 core charge. Please contact me off the list at edwardmcole(at)attbi.com or ed_cole(at)maximhq.com Thanks. Ed Cole RV6A N2169D Flying RV6A N648RV Finishing Maxim Home Page: http://www.maxim-ic.com Products Page: http://www.maxim-ic.com/MaximProducts/products.htm New Products: http://dbserv.maxim-ic.com/new_products.cfm Datasheets: http://dbserv.maxim-ic.com/l_datasheet3.cfm The information contained in this message is confidential and may be legally privileged. The message is intended solely for the addressee(s). If you are not the intended recipient, you are hereby notified that any use, dissemination, or reproduction is strictly prohibited and may be unlawful. If you are not the intended recipient, please contact the sender by return e-mail and destroy all copies of the original message. ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Vision Micro System
Date: Mar 11, 2002
Hi John, I too looked at virtually all of the engine monitors on the market. I have put them all on my website with a "review" page listing prices, functionaility, etc.. at http://www.steinair.com Regarding the VM-1000 unit, it is a very good unit but like Jim Norman, I personally believe that the best unit for the bucks is the I-K2000. The lead time for a VM is literally months. Some quick benefits of the IK (not to bring up a previous list argument) that I see are: Quick "one look" scan. All CHT's and EGT's in one glance. Everything normal is "in the green". Anything out of range is RED. The unit has multiple processors, and is much more fault tolerant than the VM. It also displays Alitude, Fuel Flow, Airspeed, Mode C, OAT, MP, Oil Press. Fuel Press, Oil Temp, Amps, Volts, RPM, % fuel remaining, and a few more added functions. The units can be separated for a tandem (RV-8) aircraft, and also fit nicely in a standard radio stack. Anyway, you can see more details on my website or send me a message offline. I'd be happy to discuss with you. Good Luck, Stein Bruch RV6, Minneapolis, Seats & Seatbelts. I"m looking for feedback on the merits of using the Vision Micro system in place of all the individual instruments. Some of my concerns are reliability and what happens if you need to replace just one of the functions. Your comments please. Best wishes, John Furey RV6A ________________________________________________________________________________
From: "Rick Jory" <rickjory(at)msn.com>
Subject: Re: Vision Micro System
Date: Mar 11, 2002
I went with the VM1000 (haven't flown yet) in that it takes up minimal space, relatively speaking, and was quite easy to plumb/wire (also relatively speaking). If one adds the EI gages together, the VM1000 is actually less expensive! Good luck. Rick Jory (RV8A) ----- Original Message ----- From: Jim Norman <jnorman(at)intermapsystems.com> Subject: RE: RV-List: Vision Micro System > > John, > Before you decide to go with a VM 1000, take a look at the IK-2000. We have > hashed this out a bit several months ago, but this is a really cool unit > with great features... I think it is the best engine monitor on the > market...for less Canadian (or US) dollars than the VM 1000. > > See it here: > http://www.i-ktechnologies.com > > Jim > tampa > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of John Furey > To: rv-list(at)matronics.com > Subject: RV-List: Vision Micro System > > > I"m looking for feedback on the merits of using the Vision Micro system > in place of all the individual instruments. Some of my concerns are > reliability and what happens if you need to replace just one of the > functions. Your comments please. > > Best wishes, > John Furey RV6A > > ________________________________________________________________________________
From: "Chuck Weyant" <chuck(at)chuckdirect.com>
Subject: Re: Duckworks Landing Lights: Lens Shape
Date: Mar 11, 2002
I had no problems. Followed the instructions to the T though. Chuck > Did you try the "Duct tape handle" method of pulling the lens into the wing > LE from the outside as mentioned in the instructions? Worked well for me and > in fact for some reason it seems to work better than pushing it from the > inside. (if you could get in there). > > Did you trim the lens so it only extends beyond the hole the minimum needed > for the seal and attach strips? Any extra will make it stiffer and less able > to form to the wing. I also ground/beveled the edges some since it did curl > up just a bit at the edges. Smooth the edges though with very fine sandpaper > as the stuff will crack at any stress risers if flexed. > > The double-sided tape seems to take some time to get a good bond. Rough up > the surfaces and clean them first, then clamp the strips on overnight. If > that fails, just use proseal. > > My best suggestion however is to call the man himself, Don "The Duck" Wentz. > He's the one who makes the lenses including forming the bend in his oven > (though I think he's now turned that over to his wife Janet.) They would > have the best advice on how to make it fit your wing, and are good people > and anxious for people to be satisfied with the product. > > Their number should be with the directions. If not drop me a line privately > and I'll email it to you. > > Randall Henderson, RV-6 N6R (~300 hrs) > Portland, OR > www.vanshomewing.org > > ________________________________________________________________________________
Date: Mar 11, 2002
From: Larry Bowen <lcbowen(at)yahoo.com>
Subject: Vision Micro System
Nice comparisons. Thanks. The ACS price is available now ($3250). It's my favorite, except for the price. The I-K 2000 looks awful busy to me. Larry RV-8 fuse http://BowenAero.com --- Stein Bruch wrote: > > Hi John, > > I too looked at virtually all of the engine monitors on the market. I have > put them all on my website with a "review" page listing prices, > functionaility, etc.. at http://www.steinair.com > > Regarding the VM-1000 unit, it is a very good unit but like Jim Norman, I > personally believe that the best unit for the bucks is the I-K2000. The > lead time for a VM is literally months. > > Some quick benefits of the IK (not to bring up a previous list argument) > that I see are: > > Quick "one look" scan. All CHT's and EGT's in one glance. > Everything normal is "in the green". Anything out of range is RED. > The unit has multiple processors, and is much more fault tolerant than the > VM. > It also displays Alitude, Fuel Flow, Airspeed, Mode C, OAT, MP, Oil Press. > Fuel Press, Oil Temp, Amps, Volts, RPM, % fuel remaining, and a few more > added functions. > > The units can be separated for a tandem (RV-8) aircraft, and also fit nicely > in a standard radio stack. > > Anyway, you can see more details on my website or send me a message > offline. I'd be happy to discuss with you. > > Good Luck, > Stein Bruch > RV6, Minneapolis, Seats & Seatbelts. > > > I"m looking for feedback on the merits of using the Vision Micro system > in place of all the individual instruments. Some of my concerns are > reliability and what happens if you need to replace just one of the > functions. Your comments please. > > Best wishes, > John Furey RV6A > > > > > > > > ________________________________________________________________________________
From: "Rhett Westerman" <rhettwesterman(at)hotmail.com>
Subject: Vision Micro System
Date: Mar 11, 2002
I do not see where the IK unit has an autotrack feature like the vision. That feature saved my XXX and kept me from having a dead stick. That feature alone makes the Vision the choice for me.... Rhett From: "Stein Bruch" <STEIN(at)STEINAIR.COM> Reply-To: rv-list(at)matronics.com To: Subject: RE: RV-List: Vision Micro System Date: Mon, 11 Mar 2002 11:35:16 -0600 -- RV-List message posted by: "Stein Bruch" Hi John, I too looked at virtually all of the engine monitors on the market. I have put them all on my website with a "review" page listing prices, functionaility, etc.. at http://www.steinair.com Regarding the VM-1000 unit, it is a very good unit but like Jim Norman, I personally believe that the best unit for the bucks is the I-K2000. The lead time for a VM is literally months. Some quick benefits of the IK (not to bring up a previous list argument) that I see are: Quick "one look" scan. All CHT's and EGT's in one glance. Everything normal is "in the green". Anything out of range is RED. The unit has multiple processors, and is much more fault tolerant than the VM. It also displays Alitude, Fuel Flow, Airspeed, Mode C, OAT, MP, Oil Press. Fuel Press, Oil Temp, Amps, Volts, RPM, % fuel remaining, and a few more added functions. The units can be separated for a tandem (RV-8) aircraft, and also fit nicely in a standard radio stack. Anyway, you can see more details on my website or send me a message offline. I'd be happy to discuss with you. Good Luck, Stein Bruch RV6, Minneapolis, Seats Seatbelts. -- RV-List message posted by: "John Furey" I"m looking for feedback on the merits of using the Vision Micro system in place of all the individual instruments. Some of my concerns are reliability and what happens if you need to replace just one of the functions. Your comments please. Best wishes, John Furey RV6A ________________________________________________________________________________
Date: Mar 11, 2002
From: "Owens, Laird" <Owens(at)aerovironment.com>
Subject: Vision Micro System
Looks like Van liked the IK-2000 enough to put it in the new RV-9 taildragger..... Laird SoCal --- Stein Bruch wrote: > > Hi John, > > I too looked at virtually all of the engine monitors on the market. I have > put them all on my website with a "review" page listing prices, > functionaility, etc.. at http://www.steinair.com > > Regarding the VM-1000 unit, it is a very good unit but like Jim Norman, I > personally believe that the best unit for the bucks is the I-K2000. The > lead time for a VM is literally months. > > Some quick benefits of the IK (not to bring up a previous list argument) > that I see are: > > Quick "one look" scan. All CHT's and EGT's in one glance. > Everything normal is "in the green". Anything out of range is RED. > The unit has multiple processors, and is much more fault tolerant than the > VM. > It also displays Alitude, Fuel Flow, Airspeed, Mode C, OAT, MP, Oil Press. > Fuel Press, Oil Temp, Amps, Volts, RPM, % fuel remaining, and a few more > added functions. > > The units can be separated for a tandem (RV-8) aircraft, and also fit nicely > in a standard radio stack. > > Anyway, you can see more details on my website or send me a message > offline. I'd be happy to discuss with you. > > Good Luck, > Stein Bruch > RV6, Minneapolis, Seats & Seatbelts. > > > I"m looking for feedback on the merits of using the Vision Micro system > in place of all the individual instruments. Some of my concerns are > reliability and what happens if you need to replace just one of the > functions. Your comments please. > > Best wishes, > John Furey RV6A > > > > > > > > ________________________________________________________________________________
Date: Mar 11, 2002
Subject: Re: Vision Micro System
From: <racker(at)rmci.net>
> >If one adds the EI gages together, the VM1000 is > actually less expensive! Flip side...less expensive until it breaks (like all the other all-in-one solutions). Ask me how I know :( Rob Acker (RV-6, all seperate gauges next project). ________________________________________________________________________________
From: "Jack Textor" <jack(at)IaJobs.com>
Subject: Torque Wrench Info
Date: Mar 11, 2002
Larry and others, The wrench is a 0-200 inch pound unit. It is not on-line that I could find. It was in a catalog I got months ago. Also, for calibration try: Western States Calibration, 105 West 2950 South, Salt Lake City, Utah 84115, phone 801-466-1700. Thanks, Jack > Larry, > A pilot/A&P friend sent it to Utah. I will get the specifics for the list. > I have also had the Ia Air Guard check them in the past; they didn't charge > me a thing. > Jack > > Subject: Re: RV-List: Torque Wrench Info > > Where is you take it to be certified? > > -Larry > > > Wanted the group to know the 1/4" 0-200 inch pound torque wrench I > purchased > > from JC Whitney just passed a certification. The tolerance was 4%. Mine > > was within 1/4 of a percent. I was pleasantly surprised. > > Jack > > RV8, wings > > DSM > Is that a 0-200 or a 20-200? I saw a 20-200 on there web site. -- ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Re: Hooker Harness - What Size?
Date: Mar 11, 2002
Norman, I got the narrow ones and they seem plenty wide. Especially since they have the pads. I did NOT spring for the rotary buckle. The standard one works very well and is easily removed with one hand. One suggestion. If you are putting in the crotch strap, you may want to have them shorten the strap length. I have a whole wad of strap that I either have to secure or I will cut it off. leaving a ragged edge. Ross Mickey ----- Original Message ----- From: "Norman" <nhunger(at)sprint.ca> > Looking at the 5 point hooker harness available from Team Rocket for > $312 USD, they are available in different widths. > Which one is best for an RV6A? > 1.75" or 2" or 3"? > Also, has anyone bucked up $499 for these belts with the rotary buckles? > Are they worth it? ________________________________________________________________________________
From: "Wentz, Don" <don.wentz(at)intel.com>
Subject: Duckworks Landing Lights: Lens Shape
Date: Mar 11, 2002
From: "Joe Larson" <jpl(at)showpage.org> Subject: RV-List: Duckworks Landing Lights: Lens Shape Joe, your post was fwded to me by a couple of RV-listers. I don't recall getting a call or email from you about your problems, but I'd like an opportunity to see if I can be of any help here. I'm copying it to the RVlist as informational in case you have raised questions for anyone else. Note my responses to your comments in the body of the text below. > Okay, I've got my duckworks landing lights installed in both wings. And I'm > not very happy with it. I'm going to have to redo the plexi lenses before I > fly. > > The problem -- the precurved shape of the lens didn't match the shape of my > wings. I don't care to wonder why too hard, but I choose to believe it's the > lens that was out of shape, NOT my wing. ---> Joe, unless you have a very early RV-4 or -6 wing, there is little chance that there would be a problem with the shape of your wing. The early wings had 'section bent' leading edges and indeed when Van's changed to 'rolling' the LE the shape changed some. This caused a re-shaping of our molds used for making the lenses, as we heard thru feedback that there was an increase in fitting problems. That was several years ago and we now get almost no complaints about fit of the lense. > > I tried two solutions to this, with the second one tried in a few different ways. > > The first solution was force. No joy at all. You can't reach in from the back > side, because you won't have access to the back once everything is installed. > So the force you are allowed to apply is relatively small. ---> Joe, the instructions describe a very good method of 'pulling' the lense into the wing LE for fit and drilling. I assume that you properly trimmed the lense as described in the instructions. I'm not saying that you will get a 'perfect' fit, but if you use the methods described you should get a very 'good' fit. > > So the next thing I tried -- I tossed the lens on a cookie sheet and threw it > in the oven. I slowly increased the oven temperature until the lens started to > sag. I let it bake like that for a couple of minutes, opening the oven to check > to see how soft it was periodically. I found that sufficient temperature to make > it mostly lie flat didn't heat it enough to make the part that was already pre-curved > the most soften up. > > In the end, I had to reach temperatures very close to 400 degrees. ---> Just FYI, we form the lenses at 280-300 deg F. > > I then took it out and as quickly as I could, dropped it over the nose of my > leading edge. > > However, as it cooled, the edges lifted up, so I still didn't have the right shape. > > Repeated that a few times -- no joy. Tried heating even hotter, and > it started sticking (badly) to the cookie sheet. > > Shut it all down for a day. Built a wing subsection that I can fit into the oven. > Used particle board and some galvanized steel I had sitting around. Got the > shape as close to wing shaped as I could, although the galvanized is a little > hard to curl. It's close, but not perfect. > > I then tried the oven thing again, letting the lens soften and form around this > structure I made. > > That got it closer to the shape needed, so I went ahead and finished the > installation. However, once done, I'm still not very happy with the shape -- > it just doesn't sit in there flat, and I have a gap sufficient to fill the > entire area with water if I fly in the rain. NOT satisfied. > ---> Joe, a couple of things. First, it is extremely difficult to make a satisfactory 'mold' of the wing shape. By eyeball you may think that you have it 'close', but once the lense is made you will find that it won't fit. Ask me how I know this ;-). Secondly, forming a lense over the OUTSIDE of the wing LE will make the curve WAY too big and the lense will never fit. The shape has to be molded to the inside curve of the wing, which is definitely more difficult than 'drape molding' on the outside. > If push came to shove, I could caulk it. But that's a pretty lazy solution. > And I don't like the amount of local turbulence I'm going to have from a > non-smooth leading edge. > > So I intend to try both lenses AGAIN. I'd love to hear suggestions. It seemed > like I was work-hardening the plexi, so I was afraid to just keep trying with > it -- I thought it might get brittle or something. > ---> Joe, you are correct, it definitely DOES work harden from repeated heating. > What I'd love to do is hang a sheet of plexi over the REAL wing and nail it > with a heat gun of some sort. Would that work? ---> No, for the reason described above. > I'm also not happy with the double-sided-tape method of holding the aluminum > strips on the inside of the lenses. That tape just doesn't hold. While > monkeying around trying to get screws to start threading, stuff comes unstuck. > I'm not happy about that, either. Does anyone have suggestions? > ---> Joe, I have to agree that the double sided tape is a marginal solution to this function. However, the numbers of cracked lenses that would occur if I were to recommend riveting that piece would be un-manageable. One option would be to use a very light weight countersunk aluminum 'pop' rivet to hold that rivet plate on. I may have some of these that I could give you. Since the lense should not have to be removed from the wing more than every few years, I hoped that the tape solution would be better than many broken lenses. > > --- > > The duckworks system seems like a good idea, but getting the lens to fit > properly wasn't working for me. > > -Joe ---> Joe, before you spend any more of your 'building' time trying to make lenses, why don't you give me your address and I'll send you 2 new plexi lenses. Try to install them using the methods described in the instructions. Take into account the location of the holes in the lense in relation to the now drilled and dimpled holes in the wing skin, drilling the lense just aft of center of the holes in the wings. You should be able to get a fit tight enough for the 1/16" grey foam tape supplied in the kit to seal out water. Very sorry for all of the extra time you have spent on this, please contact me if you need to discuss further. Don "The Duck" Wentz Duckworks RV-6 ________________________________________________________________________________
From: "Jim Norman" <jnorman(at)intermapsystems.com>
Subject: Vision Micro System
Date: Mar 11, 2002
The IK-2000 has 4 separate systems, each with its own power source... so if you lose some function, you don't loose them all. jim -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of racker(at)rmci.net Subject: Re: RV-List: Vision Micro System > >If one adds the EI gages together, the VM1000 is > actually less expensive! Flip side...less expensive until it breaks (like all the other all-in-one solutions). Ask me how I know :( Rob Acker (RV-6, all seperate gauges next project). ________________________________________________________________________________
Date: Mar 11, 2002
From: "John B. Abell" <jbabell(at)attbi.com>
Subject: Re: Vision Micro System
Hi John, I have the VM1000 instaled in my RV-6A along with the VM EC-100, fuel quantity system, OAT/CAT gauge, and chronometer. I have about 100 hours on my airplane and I love the VM stuff. It's very readable at all times, even in direct sunlight. Be careful of the VM fuel quantity system; it's a bitch to install. I haven't had any problems with any of it, but if you decide to install the VM1000, put the DPU in an accessible location. My guess is that most problems with the VM1000 would be transducer or wiring related. I think the rest of the components are very reliable. Good luck and best wishes, Jack Abell P.S. I haven't seen the IK whatever. John Furey wrote: > > I"m looking for feedback on the merits of using the Vision Micro system > in place of all the individual instruments. Some of my concerns are > reliability and what happens if you need to replace just one of the > functions. Your comments please. > > Best wishes, > John Furey RV6A > ________________________________________________________________________________
From: "Joe Larson" <jpl(at)showpage.org>
Subject: Duckworks System
Date: Mar 11, 2002
Okay, some people have gotten a misrepresentation of the problems I had. The problem isn't in the design of the system -- except for the double-sticky-tape thing My posting was getting long already, so I omitted some information. The second lens didn't fit because I'd goofed when I cut the skins. I cut it EXACTLY like the first one. Well, duh. It's supposed to be a mirror image. If I wanted to land inverted, it was cut to the right shape. That's why I had to reform the second lens in the first place. The first lens isn't a perfect fit, but I'd fly with it. Don gave me some tips about that, too. I like the Duckworks system. I think once installed, it looks nice, and it's a LOT easier than cutting up our wingtips and installing something out there. I don't like the double-sticky-tape method of holding the aluminum strips on. Don points out that trying to rivet the strips would crack the lens. I think using pro-seal is a much better choice. Don's email to me (which I believe he has cross-posted, but I get stuff in digest mode, so haven't received it yet) explained what I did wrong in trying to reform the lens. I draped it over the outside of my form, which gives me the wrong radius. Don and I will figure something out, and I expect to be happy by the time I'm done. So those of you considering the Duckworks system -- even though I had problems, they were basically of my own making. Granted, I would prefer a means of creating a lens that's actually flush with my wing skins, but that's impractical. I think it's a good system that can look nice if you exercise care and don't screw it up. -Joe ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: compass
Date: Mar 11, 2002
I'm not sure on a marine compass, I just know that the airpath avi compasses always seem to get a small bubble over time and that would place indue internal pressures at altitude, so there is a flexible bellows that compensates. A marine compass probably doesn't need this, unless you are going to do some significant surfing around Cape Horn. W ________________________________________________________________________________
Date: Mar 11, 2002
From: "Gary Zilik" <zilik(at)bewellnet.com>
Subject: Re: Duckworks System
If you take a close look at the RV-9A landing light cutout on the right wing (as I recall) you can see where Van's boys did the exact same thing. Cut the hole upside down. Close examination reveals the patch and I would bet that with a little more work it would not be visible. Gary Joe Larson wrote: > > The second lens didn't fit because I'd goofed when I cut the skins. I cut it > EXACTLY like the first one. Well, duh. It's supposed to be a mirror image. > If I wanted to land inverted, it was cut to the right shape. > ________________________________________________________________________________
From: "Doug Weiler" <dougweil(at)pressenter.com>
Subject: 8th Annual Twin Cities RV Forum
Date: Mar 11, 2002
Fellow Listers: The website detailing the Twin Cities RV Forum is up and running. Guest speakers will include George and Becki Orndorff, Jim Younkin (of autopilot fame), Paul Irlbeck, professional builder, brother Tom Irlbeck, former Navy Top Gun instructor plus others. Van's aircraft will be there. Plus we have relocated from Red Wing, MN to the Golden Wings Air Museum in Minneapolis. The website will be expanded as plans are confirmed. Here's the address: http://www.pressenter.com/~dougweil/RVforum/index.htm Thanks, Doug Weiler pres, MN Wing ________________________________________________________________________________
From: "Bob Busick" <panamared1(at)brier.net>
Subject: Re: RV9A with 89 Gallons of Fuel
Date: Mar 11, 2002
FYI When I did my fuel tank calibration and first fill up, we stoped at 60 gallons. I built the tanks per Vans plans, and when we stopped filling the tanks, there we no leaks nor were the tanks full. Airport manager assured me that there was nothing wrong with his finely tuned and calibrated fuel trucks? I never imagined this would happen, but I will never let someone fill my tanks without me watching. Bob > > Nope, no turbine for this plane. Even though I've increased it's ability to > carry fuel, my ability to fill those tanks is still quite limited. ________________________________________________________________________________
Date: Mar 11, 2002
From: Frank Dombroski <f_dombroski(at)yahoo.com>
Subject: Prop Gov Deals
I just purchased a Prop Gov from Southwest Aero, in WA state, 206-575-8732. The governor was freshly overhauled, looks like new, and was well less than half the price of a new gov. This is the Woodward #210195 converted to the same spec as the Woodward the Vans sold for the Lyc. IO/O 360. John is a great guy, and a pleasure to deal with. I highly reccomend him to all. Regards Frank Dombroski -8 finishing Fuse, on to the Canopy... --------------------------------- ________________________________________________________________________________
Date: Mar 11, 2002
From: Mark Schrimmer <mschrimmer(at)pacbell.net>
Subject: Re: Fuel Tank Builders
on 3/10/02 11:56 PM, RV-List Digest Server at rv-list-digest(at)matronics.com wrote: > The tanks, however, presented a whole different challenge. > Many, many rivets were bent over like nails Jim, I just went through this same problem last Saturday on my 9A tanks. Using my Avery rivet gauge, I determined that I should be using a rivet a half size longer than specified on the plans. This has been the case many times throughout the project, so I put in some 3-4s and when I shot and bucked them, they bent. A fellow builder (thanks Jerry) offered to shoot while I bucked and we still had the same problem. We finally decided to try some 3-3.5s as specified on the plans and these went in just fine. They definitely look undersized and are a little small according to my Avery gauge, but only one bent over. Anybody have any comments or suggestions? Mark Schrimmer Up to my elbows in Proseal ________________________________________________________________________________
Date: Mar 11, 2002
From: "Gary Zilik" <zilik(at)bewellnet.com>
Subject: Re: RV9A with 89 Gallons of Fuel
Yowsa, Van's spec sheet on the 9A shows 36 US Gallons as the fuel capacity. http://www.vansaircraft.com/public/rv-9spe.htm Gary Bob Busick wrote: > > > FYI > > When I did my fuel tank calibration and first fill up, we stoped at 60 > gallons. I built the tanks per Vans plans, and when we stopped filling the > tanks, there we no leaks nor were the tanks full. > > Airport manager assured me that there was nothing wrong with his finely > tuned and calibrated fuel trucks? I never imagined this would happen, but I > will never let someone fill my tanks without me watching. > > Bob > > > > > Nope, no turbine for this plane. Even though I've increased it's ability > to > > carry fuel, my ability to fill those tanks is still quite limited. > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Duckworks Landing Lights: Lens Shape
Date: Mar 11, 2002
Don, That is service beyond the call of duty! Great! Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org Always looking for articles for the Experimenter ----- Original Message ----- From: "Wentz, Don" <don.wentz(at)intel.com> Subject: RE: RV-List: Duckworks Landing Lights: Lens Shape From: "Joe Larson" <jpl(at)showpage.org> Subject: RV-List: Duckworks Landing Lights: Lens Shape Joe, your post was fwded to me by a couple of RV-listers. I don't recall getting a call or email from you about your problems, but I'd like an opportunity to see if I can be of any help here. I'm copying it to the RVlist as informational in case you have raised questions for anyone else. Note my responses to your comments in the body of the text below. > Okay, I've got my duckworks landing lights installed in both wings. And I'm > not very happy with it. I'm going to have to redo the plexi lenses before I > fly. > > The problem -- the precurved shape of the lens didn't match the shape of my > wings. I don't care to wonder why too hard, but I choose to believe it's the > lens that was out of shape, NOT my wing. ---> Joe, unless you have a very early RV-4 or -6 wing, there is little chance that there would be a problem with the shape of your wing. The early wings had 'section bent' leading edges and indeed when Van's changed to 'rolling' the LE the shape changed some. This caused a re-shaping of our molds used for making the lenses, as we heard thru feedback that there was an increase in fitting problems. That was several years ago and we now get almost no complaints about fit of the lense. > > I tried two solutions to this, with the second one tried in a few different ways. > > The first solution was force. No joy at all. You can't reach in from the back > side, because you won't have access to the back once everything is installed. > So the force you are allowed to apply is relatively small. ---> Joe, the instructions describe a very good method of 'pulling' the lense into the wing LE for fit and drilling. I assume that you properly trimmed the lense as described in the instructions. I'm not saying that you will get a 'perfect' fit, but if you use the methods described you should get a very 'good' fit. > > So the next thing I tried -- I tossed the lens on a cookie sheet and threw it > in the oven. I slowly increased the oven temperature until the lens started to > sag. I let it bake like that for a couple of minutes, opening the oven to check > to see how soft it was periodically. I found that sufficient temperature to make > it mostly lie flat didn't heat it enough to make the part that was already pre-curved > the most soften up. > > In the end, I had to reach temperatures very close to 400 degrees. ---> Just FYI, we form the lenses at 280-300 deg F. > > I then took it out and as quickly as I could, dropped it over the nose of my > leading edge. > > However, as it cooled, the edges lifted up, so I still didn't have the right shape. > > Repeated that a few times -- no joy. Tried heating even hotter, and > it started sticking (badly) to the cookie sheet. > > Shut it all down for a day. Built a wing subsection that I can fit into the oven. > Used particle board and some galvanized steel I had sitting around. Got the > shape as close to wing shaped as I could, although the galvanized is a little > hard to curl. It's close, but not perfect. > > I then tried the oven thing again, letting the lens soften and form around this > structure I made. > > That got it closer to the shape needed, so I went ahead and finished the > installation. However, once done, I'm still not very happy with the shape -- > it just doesn't sit in there flat, and I have a gap sufficient to fill the > entire area with water if I fly in the rain. NOT satisfied. > ---> Joe, a couple of things. First, it is extremely difficult to make a satisfactory 'mold' of the wing shape. By eyeball you may think that you have it 'close', but once the lense is made you will find that it won't fit. Ask me how I know this ;-). Secondly, forming a lense over the OUTSIDE of the wing LE will make the curve WAY too big and the lense will never fit. The shape has to be molded to the inside curve of the wing, which is definitely more difficult than 'drape molding' on the outside. > If push came to shove, I could caulk it. But that's a pretty lazy solution. > And I don't like the amount of local turbulence I'm going to have from a > non-smooth leading edge. > > So I intend to try both lenses AGAIN. I'd love to hear suggestions. It seemed > like I was work-hardening the plexi, so I was afraid to just keep trying with > it -- I thought it might get brittle or something. > ---> Joe, you are correct, it definitely DOES work harden from repeated heating. > What I'd love to do is hang a sheet of plexi over the REAL wing and nail it > with a heat gun of some sort. Would that work? ---> No, for the reason described above. > I'm also not happy with the double-sided-tape method of holding the aluminum > strips on the inside of the lenses. That tape just doesn't hold. While > monkeying around trying to get screws to start threading, stuff comes unstuck. > I'm not happy about that, either. Does anyone have suggestions? > ---> Joe, I have to agree that the double sided tape is a marginal solution to this function. However, the numbers of cracked lenses that would occur if I were to recommend riveting that piece would be un-manageable. One option would be to use a very light weight countersunk aluminum 'pop' rivet to hold that rivet plate on. I may have some of these that I could give you. Since the lense should not have to be removed from the wing more than every few years, I hoped that the tape solution would be better than many broken lenses. > > --- > > The duckworks system seems like a good idea, but getting the lens to fit > properly wasn't working for me. > > -Joe ---> Joe, before you spend any more of your 'building' time trying to make lenses, why don't you give me your address and I'll send you 2 new plexi lenses. Try to install them using the methods described in the instructions. Take into account the location of the holes in the lense in relation to the now drilled and dimpled holes in the wing skin, drilling the lense just aft of center of the holes in the wings. You should be able to get a fit tight enough for the 1/16" grey foam tape supplied in the kit to seal out water. Very sorry for all of the extra time you have spent on this, please contact me if you need to discuss further. Don "The Duck" Wentz Duckworks RV-6 ________________________________________________________________________________
From: "KostaLewis" <mikel(at)dimensional.com>
Subject: Re: Hooker Harness - What Size?
Date: Mar 11, 2002
> I got the narrow ones and they seem plenty wide. Especially since they have > the pads. One suggestion: if you are putting in the crotch strap, you may want to have them shorten the strap > length. I have a whole wad of strap that I either have to secure or I will cut it off. leaving a ragged edge. The other option, which I am looking at, is having the crotch strap made as a non-adjustable strap. Problem is, you don't really know how long it will need to be until you have the other belts in and adjusted. I find the only reason I adjust the crotch strap is to shorten it to take up the slack the fittings tend to make over time. That is the only thing I don't like about Hooker harneses: the fittings tend to "creap", not staying snug, as you wear them during a flight. I asked Mr. Hooker about that and he has a special spring loaded fitting that helps fight that but is more expensive than the regular fitting. It may be a problem with any belt set up. Michael ________________________________________________________________________________
From: "KostaLewis" <mikel(at)dimensional.com>
Subject: Re: filling the tanks
Date: Mar 11, 2002
> Airport manager assured me that there was nothing wrong with his finely > tuned and calibrated fuel trucks? I never imagined this would happen, but I > will never let someone fill my tanks without me watching. Maybe it's me, but I would never let anybody else but me fill my tanks. It's just a thing I have for several reasons. I know how much I am putting in: I am looking at the level in the tank. I have yet to scratch my paint with a fuel nozzle, spring or nozzle cap. The fuel is coming out of the 100LL tank, looking BLUE as I can see it come out of the nozzle. Suzie Q gets pissed if I let someone else fuel her and I tell the line person that. Have yet to have anyone refuse to let me fill her. Just keeps me more in touch with my airplane. Course, I have this routine I follow when I am on a fuel stop that keeps the fuel tanks caps on, the oil at the proper level and the oil access door closed, and the fuel sumps drained and smelling like Avgas and not Jet-A, the trim set for takeoff and the full swivel tail wheel in place before I get in the airplane. Michael RV-4 N232 Suzie Q ________________________________________________________________________________
From: N188rv(at)aol.com
Date: Mar 11, 2002
Subject: Re: RV8-List: RV-8A flight visibilty
Craig I have been flying my RV-8 for 3 months. The visibility is great over the nose. Wheel landing are a snap. Much better visibility than RV-6. Stan ________________________________________________________________________________
From: "TERRY BENZER" <TERRYBENZER(at)prodigy.net>
Subject: RV6/8 Trim tab
Date: Mar 11, 2002
Has anyone used pop/pull rivets to attach the trim tab spar to the bottom half of the skin? If so which rivet did you use? I maybe be able to backrivet it but my big hands keep me from using a bucking bar in there. I am thinking of purchasing a longeron yoke for my Avery squeezer, will I need it later or would it be $135 one time use? Thanks ________________________________________________________________________________
From: "Haywire" <haywire(at)telus.net>
Subject: RV9A with 89 Gallons of Fuel
Date: Mar 11, 2002
> > Yowsa, Van's spec sheet on the 9A shows 36 US Gallons as the fuel > capacity. > > http://www.vansaircraft.com/public/rv-9spe.htm > > Gary > WHAT??????!! only 36 gallons you say? Sheeet, ah new I shooda red the instrukshuns. Us dumb-ass Canucks shoolda stayed in skool, but I had to quit after pappy got et by a polar bare. I guess them there Oztrailians can't reed to well eether, esspeshally that Jon Johanson guy. ;-) ;-) S. Todd Bartrim 13B rotary powered RV-9endurance (finish kit) C-FSTB (reserved) http://www3.telus.net/haywire/RV-9/C-FSTB.htm ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Mar 11, 2002
Subject: Re: RV6/8 Trim tab
In a message dated 3/11/02 4:39:35 PM Pacific Standard Time, TERRYBENZER(at)prodigy.net writes: << I am thinking of purchasing a longeron yoke for my Avery squeezer, will I need it later or would it be $135 one time use? >> That yoke is one of the best tool investments I have made so far. The farther along I get the more I use it. Harry Crosby Pleasanton, California RV-6, finish kit stuff ________________________________________________________________________________
Date: Mar 11, 2002
From: George Kilpatrick <aeronut58(at)yahoo.com>
Subject: Lycoming starter ring gear: how to install?
I just got my O-360A4M back from major overhaul. The starter ring gear was removed by the rebuilder to secure the engine on its shipping pallet. My question is how to install the ring gear on the engine so that the timing marks are in correct alignment. It appears that it will mount in any of six orientations (corresponding to the six prop bolt holes). Any A&Ps out there who can help? George N888GK ________________________________________________________________________________
From: "Bill VonDane" <n8vd(at)earthlink.net>
Subject: Lycoming starter ring gear: how to install?
Date: Mar 11, 2002
George... The ring gear will only go on one way... One of the bushings has a larger diameter than the others... -Bill -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of George Kilpatrick Subject: RV-List: Lycoming starter ring gear: how to install? I just got my O-360A4M back from major overhaul. The starter ring gear was removed by the rebuilder to secure the engine on its shipping pallet. My question is how to install the ring gear on the engine so that the timing marks are in correct alignment. It appears that it will mount in any of six orientations (corresponding to the six prop bolt holes). Any A&Ps out there who can help? George N888GK ________________________________________________________________________________
From: "Ross A. Scroggs" <rscroggs(at)attbi.com>
Subject: Re: Lycoming starter ring gear: how to install?
Date: Mar 11, 2002
George, If you look closely at the starter gear you will see a small "O" next to one of the six large holes for the prop bolt bushings. This bushing hole will be slightly larger in diameter and will mesh with only one prop bushing on the crankshaft. This gear can only go on in one position, provided the ring gear is oriented with the alternator pulley side of the ring gear next to the crankcase. It's really almost fool proof. Ross Scroggs A&P RV-4 Flaps Conyers, Ga. ----- Original Message ----- From: George Kilpatrick <aeronut58(at)yahoo.com> Subject: RV-List: Lycoming starter ring gear: how to install? > > I just got my O-360A4M back from major overhaul. The > starter ring gear was removed by the rebuilder to > secure the engine on its shipping pallet. > > My question is how to install the ring gear on the > engine so that the timing marks are in correct > alignment. It appears that it will mount in any of > six orientations (corresponding to the six prop bolt > holes). > > Any A&Ps out there who can help? > > George > N888GK > > ________________________________________________________________________________
From: ABAYMAN(at)aol.com
Date: Mar 11, 2002
Subject: Re: RV6/8 Trim tab
terry once i broke down and bought the logeron yoke, i used it 99% of the time after that. it is more valuable than the 4 or 3 inch yokes. scott tampa ________________________________________________________________________________
From: "Bruce Gray" <bruce.gray(at)snet.net>
Subject: Lycoming starter ring gear: how to install?
Date: Mar 11, 2002
Unless his rebuilder didn't install the right bushings. Bruce -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Ross A. Scroggs Subject: Re: RV-List: Lycoming starter ring gear: how to install? George, If you look closely at the starter gear you will see a small "O" next to one of the six large holes for the prop bolt bushings. This bushing hole will be slightly larger in diameter and will mesh with only one prop bushing on the crankshaft. This gear can only go on in one position, provided the ring gear is oriented with the alternator pulley side of the ring gear next to the crankcase. It's really almost fool proof. Ross Scroggs A&P RV-4 Flaps Conyers, Ga. ________________________________________________________________________________
From: "John Starn" <jhstarn(at)earthlink.net>
Subject: Re: Lycoming starter ring gear: how to install?
Date: Mar 11, 2002
Right on Bill, AND make sure #1 cylinder is really at top dead center when setting the timing. It can be 180 degrees out and still "line up" with the timing marks. An IO540 can produce a very large, very loud fire ball out the exhaust and/or intake if attempting to start in the later condition. I have it on tape. KABONG ----- Original Message ----- From: Bill VonDane <n8vd(at)earthlink.net> Subject: RE: RV-List: Lycoming starter ring gear: how to install? > George... > The ring gear will only go on one way... One of the bushings has a > larger diameter than the others... > -Bill ________________________________________________________________________________
Date: Mar 11, 2002
From: Bobby Hester <bhester(at)apex.net>
Subject: Re: Vision Micro System
racker(at)rmci.net wrote: > > > > >If one adds the EI gages together, the VM1000 is > > actually less expensive! > > Flip side...less expensive until it breaks (like all the other all-in-one > solutions). Ask me how I know :( > > Rob Acker (RV-6, all seperate gauges next project). > Which one do you have (VM1000) and what broke? -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
Date: Mar 11, 2002
From: Jerry Springer <jsflyrv(at)earthlink.net>
Subject: Experimental aircraft myths
Those of you that get Sport Aviation from EAA well want to read the article on "Maintaining Your Homebuilt" written by Ron Alexander. It clears up some of the myths that have been around here for years about do or do we not have to remove the dataplate from a certified engine, WE DON'T according to this article. Another thing worth mentioning that we have discussed here before is that once an engine is installed on an experimental it no longer conforms to its original type design and is considered "experimental". The article in SA also talks about Airworthiness Directives, it say that the FAA does not issue ADs for homebuilt aircraft but does issue them for things like engines, props and magnetos that may be on our experimental. BUT this is what I found interesting because these things are installed on experimental airplanes they are no longer "certificated" and mandatory compliance is not necessary. This stuff has been discussed here so many time with so many different conclusions I thought it was interesting to see this view on these topics. Jerry Springer ________________________________________________________________________________
From: "Bruce Gray" <bruce.gray(at)snet.net>
Subject: Lycoming starter ring gear: how to install?
Date: Mar 11, 2002
Try this link, everything you ever wanted to know about propeller flange bushings. http://www.lycoming.textron.com/support/service_publications/service_instruc tions_recent/SI1098G.pdf Bruce -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of John Starn Subject: Re: RV-List: Lycoming starter ring gear: how to install? Right on Bill, AND make sure #1 cylinder is really at top dead center when setting the timing. It can be 180 degrees out and still "line up" with the timing marks. An IO540 can produce a very large, very loud fire ball out the exhaust and/or intake if attempting to start in the later condition. I have it on tape. KABONG ----- Original Message ----- From: Bill VonDane <n8vd(at)earthlink.net> Subject: RE: RV-List: Lycoming starter ring gear: how to install? ________________________________________________________________________________
Date: Mar 12, 2002
From: David Roseblade <davidagr(at)emirates.net.ae>
Subject: RV6 Tip up Canopy - forward weatherseal flange
Listers, I am at the point of installing the fwd fuse upper structure, a couple of thoughts that I need help with. I note that installation of the weatherseal flange to F668 has not really been addressed in full in the instructions - both Van's and others, my question is can it be fitted before the top skin/canopy or should I wait until all these things are available before fitting. Also instead of cutting slots and bending I propose to use a shrinker on the mating flange to get a good curve - has anyone else done this? I also propose to do the same for the instrument panel 3/4 x 3/4 .063" flange. Regards David Roseblade RV6 fuselage Dubai, UAE ________________________________________________________________________________
From: "Ross" <rmickey(at)ix.netcom.com>
Subject: Securing Empenage Fair
Date: Mar 11, 2002
I am finishing up my empenage fairing (did I mention that I HATE fiberglass???) and am wondering how to best finish the rear portion. My fairing wraps around the front of the horizonal stabilizer. It will not budge unless I splay the rear like two wings and shove forward. I remember that someone had an accident becasue the rear swrews came out and the elevator got caught by the fairing. What is the best way to secure this area? Most people seem to be using two screws. What about extending the alumium strip that forms the underside gap seal back to the rear of the vertical stabilizer and put the "wings" of the empanage fairing under this? Ross RV-6A ________________________________________________________________________________
Date: Mar 12, 2002
From: David Roseblade <davidagr(at)emirates.net.ae>
Subject: Re: Fuel Tank Builders
Jim, If you check the rivet specs, you will find there is quite a tolerance in width/height of the shop head, as long as you stay within these limits there will be no problems. Also the Jepperson Sheet Metal Manual makes reference to NOT using the normal formula on thin skins, but to use height 0.66 times the dia of the rivet and width 1.33 times the dia. This is contrary to normal guidelines of using 0.5 D and 1.5 D as the normal upset dimensions, this will avoid any skin distortion. My advice is if you use the shortest rivet that will meet the specs. You will also avoid any of those "nails". Throw away the gauge - it only causes concern, I use a vernier caliper if I think any of the rivets are a bit out of spec and find they are always in spec. See http://home.flash.net/~gila/rivet_spec/rivet_a.htm for rivet specs. Regards David Roseblade RV6 Fuse Dubai, UAE -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Mark Schrimmer Subject: RV-List: Re: Fuel Tank Builders on 3/10/02 11:56 PM, RV-List Digest Server at rv-list-digest(at)matronics.com wrote: > The tanks, however, presented a whole different challenge. > Many, many rivets were bent over like nails Jim, I just went through this same problem last Saturday on my 9A tanks. Using my Avery rivet gauge, I determined that I should be using a rivet a half size longer than specified on the plans. This has been the case many times throughout the project, so I put in some 3-4s and when I shot and bucked them, they bent. A fellow builder (thanks Jerry) offered to shoot while I bucked and we still had the same problem. We finally decided to try some 3-3.5s as specified on the plans and these went in just fine. They definitely look undersized and are a little small according to my Avery gauge, but only one bent over. Anybody have any comments or suggestions? Mark Schrimmer Up to my elbows in Proseal ________________________________________________________________________________
From: "Norman" <nhunger(at)sprint.ca>
Subject: Re: RV6 Tip up Canopy - forward weatherseal flange
Date: Mar 11, 2002
> I note that installation of the weatherseal flange to F668 has not really > been addressed in full in the instructions - both Van's and others, my > question is can it be fitted before the top skin/canopy or should I wait > until all these things are available before fitting. Also instead of cutting > slots and bending I propose to use a shrinker on the mating flange to get a > good curve - has anyone else done this? I did my weatherseal flange by the book then once it was installed, I used a modern autobody filler to seal the transition. I spent lots of time sanding and filling again, sanding and filling again,..... Looks very sharp. Norman Hunger RV6A Delta BC Canada ________________________________________________________________________________
Date: Mar 12, 2002
From: Lynn Clark <lclark(at)earthlink.net>
Subject: Subaru engine question
Hi, Well, I find I'm quite enamored with the EggenFellner Subaru engine. Seems like a slick way to go, but I have a dilemma. I live near Denver, so anticpate doing most of my flying at altitudes above 6500 MSL (most anything below that altitude around here is TPA). The dilemma is that I'm allegedly building an RV-7, and wonder if the 165 HP Subie engine is enough engine in that aircraft for these parts (assume it's supercharged). I'd originally planned on putting in a 180 HP Lycoming, so I'm thinking the supercharged Subie might be "close enough". One thing I would seriously consider doing is to sell my -7 emp and switch to a -9. I'd like to hear from folks who spend time flying at the higher altitudes as to their opinions of whether the supercharged 165 HP Subie engine would be a satisfatory engine in a -7 at these altitudes, or whether it would be a better choice in a -9. Van's says the -7 is designed for 150-200 HP engines, whereas the -9 is designed for a maximum 160 HP. So I assume from that, that the -9 would be a better choice to put a Subie engine in in this part of the country. Opinions? (And please, I'm not interested in the auto vs. lycosaur debate. ;-) -- Lynn Louisville, CO RV-7A empennage (allegedly) ________________________________________________________________________________
Date: Mar 12, 2002
From: ripsteel(at)edge.net (Mark Phillips)
Subject: Re: Fuel Tank Builders
I would suggest that once the "glue" sets, the structural value of the rivets is not as important as say, for other wing skins. Consider the bonding power of the pro-seal as not only making the structure leak-proof (hopefully!), but much stronger than rivets alone... shoot, there's been a lot of Yankees, Cheetahs, Tigers etc. flying for many years on glue-power alone! I would also suppose that a "smaller" shop head would be easier to seal over than one that is clinched over with a bent shank! DISCLAIMER: I have never built an airplane before... 8 ) From the PossumWorks in TN Mark -6A, ready to order the $5K box with the big bubble in it! > We finally decided to try some 3-3.5s as specified on > the plans and these went in just fine. They definitely look undersized and > are a little small according to my Avery gauge, but only one bent over. > > Anybody have any comments or suggestions? > > Mark Schrimmer > Up to my elbows in Proseal ________________________________________________________________________________
From: "Gordon or Marge Comfort" <gcomfo(at)tc3net.com>
Subject: Fin and Rudder loads--not RV related
Date: Mar 12, 2002
Listers: For all you aeronautical engineers out there: While perusing the website for the old NACA tech reports for the year 1946 I chanced upon report #838 titled "Consideration of dynamic loads on the vertical tail by the theory of flat yawing maneuvers." It seems that at that time it was recognized that alternating rudder inputs would result in increasing loads on the vertical surfaces and that with relatively small rudder deflections excessive loads could be reached. I would assume (always dangerous) that Airbus either knows about this or that the work was later refuted. I have had a couple of observations in this area. One time when flying a PIK 20B, while in unaccelerated flight at moderate speed, out of curiosity I pulsed the rudder quickly but not extremely, probably in a right/left/right/left sequence. The result surprised me initially in that the aft fuselage and tail started a resonant response that took a few cycles to damp out. The bird was fiberglas with a rather small tailboom and T-tail. I assumed that the behavior might be characteristic of the class of aircraft and resolved to be circumspect in my application of rudder. Years later when testing the RV-4 I did the same thing and surprisingly, got a similar response, albeit with less amplitude and quicker damping. Comments please. Gordon Comfort N363GC ________________________________________________________________________________
From: "Eric Newton" <enewton57(at)cableone.net>
Subject: Re: Securing Empenage Fair
Date: Mar 12, 2002
Ross, I used screws back there. Its really not a high visibility area and as you already pointed out, that is one place you don't want the fairing coming loose. Eric Newton - Long Beach, MS RV-6A N57ME (Flying - finishing up overhaul) www.ericsrv6a.com ----- Original Message ----- From: "Ross" <rmickey(at)ix.netcom.com> Subject: RV-List: Securing Empenage Fair > > I am finishing up my empenage fairing (did I mention that I HATE > fiberglass???) and am wondering how to best finish the rear portion. My > fairing wraps around the front of the horizonal stabilizer. It will not > budge unless I splay the rear like two wings and shove forward. I remember > that someone had an accident becasue the rear swrews came out and the > elevator got caught by the fairing. What is the best way to secure this > area? Most people seem to be using two screws. What about extending the > alumium strip that forms the underside gap seal back to the rear of the > vertical stabilizer and put the "wings" of the empanage fairing under this? > > Ross > RV-6A > > ________________________________________________________________________________
From: "Steve Hurlbut" <hurlbut_steve(at)hotmail.com>
Subject: Re: Subaru engine question
Date: Mar 12, 2002
At 8500 MSL a Supercharged Subaru produces the same hp as IO-360 180 hp. Both are about 150 hp at 8500 ft. The Subaru dry weight is a little heavier than the Lyc is I remember right. With the lighter prop (assuming composite prop vs metal prop on Lyc) I would say they are about the same (Eggenfellner clains the IO-360 is 40 lbs heavier but he take into account reduced fuel requirements which I don't agree with). 150 hp is plenty hp for a 1100 lb airplane at 8500 ft. Especailly an aerodynamically clean RV. It appears the 2 engines are be very similar in performance at this altitude. As you climb however the hp of the Subaru will be higher than the Lyc. Supercharged Sub will maintain 150 hp to 12500 ft and Lyc hp will fall off to 120 hp. I would definity go with the Subaru supercharged for flying out of a 6500 MSL strip. Steve RV-7A >From: Lynn Clark <lclark(at)earthlink.net> >Reply-To: rv-list(at)matronics.com >To: >Subject: RV-List: Subaru engine question >Date: Tue, 12 Mar 2002 03:01:26 -0700 (MST) > > >Hi, > >Well, I find I'm quite enamored with the EggenFellner Subaru engine. >Seems like a slick way to go, but I have a dilemma. I live near Denver, >so anticpate doing most of my flying at altitudes above 6500 MSL (most >anything below that altitude around here is TPA). The dilemma is that I'm >allegedly building an RV-7, and wonder if the 165 HP Subie engine is >enough engine in that aircraft for these parts (assume it's supercharged). >I'd originally planned on putting in a 180 HP Lycoming, so I'm thinking >the supercharged Subie might be "close enough". One thing I would >seriously consider doing is to sell my -7 emp and switch to a -9. > >I'd like to hear from folks who spend time flying at the higher altitudes >as to their opinions of whether the supercharged 165 HP Subie engine would >be a satisfatory engine in a -7 at these altitudes, or whether it would be >a better choice in a -9. Van's says the -7 is designed for 150-200 HP >engines, whereas the -9 is designed for a maximum 160 HP. So I assume >from that, that the -9 would be a better choice to put a Subie engine in >in this part of the country. > >Opinions? > >(And please, I'm not interested in the auto vs. lycosaur debate. ;-) > >-- Lynn >Louisville, CO >RV-7A empennage (allegedly) > > Send and receive Hotmail on your mobile device: http://mobile.msn.com ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: Re: RV-8A flight visibilty
Date: Mar 12, 2002
Craig, Visibility is great! Chuck & Dave Rowbotham RV-8A (Niantic, CT) >From: "Craig Chipley" <craigchipley(at)hotmail.com> >Reply-To: rv-list(at)matronics.com >To: rv8-list(at)matronics.com >Subject: RV-List: RV-8A flight visibilty >Date: Fri, 08 Mar 2002 19:48:14 -0600 > > >List, I am contemplating the RV-8A. Of those that are flying, how is the >visiblity over the nose? Or total visibilty for that matter. Seems like a >long nose compared to Van's other designs. I like the airplane. Just a few >things left to figure out before the BIG PURCHASE!!. Thanks for the help, >Craig > > Join the worlds largest e-mail service with MSN Hotmail. http://www.hotmail.com ________________________________________________________________________________
From: "Ollie Washburn" <skybolt-aviator(at)msn.com>
Subject: Re: Subaru engine question
Date: Mar 12, 2002
I would think that if the subie is supercharged it would have more power above 6500' than the Lyc. Ollie ________________________________________________________________________________
From: "Tommy Walker" <twsurveyor(at)msn.com>
Subject: Re: RV6 Tip up Canopy - forward weatherseal flange
Date: Mar 12, 2002
David, After having installed both flanges (weather seal & panel .063 flange) I don't think a shrinker will do enough "shrinking" to make the curves necessary. I went ahead and installed the weather seal flange before fitting the skins or installing the sub-panel. I also would advise NOT installing the sub panel and front skin until you have the canopy frame built and in place. The sub panel and the canopy frame have a kinda of "chicken or the egg" relationship! Good building, Tommy Walker 6A Tipper (Finishing) Ridgetop, TN ----- Original Message ----- From: David Roseblade Subject: RV-List: RV6 Tip up Canopy - forward weatherseal flange Listers, I am at the point of installing the fwd fuse upper structure, a couple of thoughts that I need help with. I note that installation of the weatherseal flange to F668 has not really been addressed in full in the instructions - both Van's and others, my question is can it be fitted before the top skin/canopy or should I wait until all these things are available before fitting. Also instead of cutting slots and bending I propose to use a shrinker on the mating flange to get a good curve - has anyone else done this? I also propose to do the same for the instrument panel 3/4 x 3/4 .063" flange. Regards David Roseblade RV6 fuselage Dubai, UAE ________________________________________________________________________________
From: "Mike Plecenik" <nanchang(at)earthlink.net>
Subject: Re: Subaru engine question
Date: Mar 12, 2002
Lynn - Another thing you might consider regarding which airplane to build is that the -9 has more wing area and a lighter wing loading than the -7. But, more important, the wing has a higher aspect ratio which will give better performance at the altitudes at which you're operating. This assumes you don't want to do aerobatics. (and I like "experimental" engines). - Mike > > Hi, > > Well, I find I'm quite enamored with the EggenFellner Subaru engine. > Seems like a slick way to go, but I have a dilemma. I live near Denver, > so anticpate doing most of my flying at altitudes above 6500 MSL (most > anything below that altitude around here is TPA). The dilemma is that I'm > allegedly building an RV-7, and wonder if the 165 HP Subie engine is > enough engine in that aircraft for these parts (assume it's supercharged). > I'd originally planned on putting in a 180 HP Lycoming, so I'm thinking > the supercharged Subie might be "close enough". One thing I would > seriously consider doing is to sell my -7 emp and switch to a -9. (snip) ________________________________________________________________________________
From: "Joe Larson" <jpl(at)showpage.org>
Subject: Rivet gun malfunction
Date: Mar 12, 2002
Another day, another question... I basically took several years off from building. Long story. Obviously I'm back at it, but I noticed something about my rivet gun the other day. If I press the gun tightly against the work surface and pull the trigger, it won't fire. If I back it off a little bit, THEN it can fire. Seems to me I used to hold it as tightly as I could against the surface to prevent a wide array of problems. Which would mean this new behavior is a malfunction. Anyone have clues how I can fix this? I have one of the guns from Avery. Note that I DO hand-oil my air tools with a couple of drops of oil at the start of a session. However, the rivet gun sat unused for 2 or 3 years. Thanks for the help. -Joe ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Rivet gun malfunction
Date: Mar 12, 2002
>> >Another day, another question... > >I basically took several years off from building. Long story. Obviously >I'm >back at it, but I noticed something about my rivet gun the other day. > >If I press the gun tightly against the work surface and pull the trigger, >it >won't fire. If I back it off a little bit, THEN it can fire. > >Seems to me I used to hold it as tightly as I could against the surface to >prevent a wide array of problems. Which would mean this new behavior >is a malfunction. > >Anyone have clues how I can fix this? I have one of the guns from Avery. > >Note that I DO hand-oil my air tools with a couple of drops of oil at >the start of a session. However, the rivet gun sat unused for 2 or 3 >years. > >Thanks for the help. > >-Joe > > I had an Avery gun that did basically the same thing. It would misfire randomly...just sorta go "phfffftt". I sent it to Bob Avery and he rebuilt the innards...for FREE...and sent it back. Your situation may just be a case of congealed oil or dirt in the mechanism. Maybe a solvent clean followed by a fresh oiling would do the trick. If not, send it off to Bob and I'm sure he'll take care of it for you. Brian Denk RV8 N94BD MSN Photos is the easiest way to share and print your photos: http://photos.msn.com/support/worldwide.aspx ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Subaru engine question
Date: Mar 12, 2002
> > > > > Hi, > > > > Well, I find I'm quite enamored with the EggenFellner Subaru engine. > > Seems like a slick way to go, but I have a dilemma. I live near Denver, > > so anticpate doing most of my flying at altitudes above 6500 MSL (most > > anything below that altitude around here is TPA). The dilemma is that >I'm > > allegedly building an RV-7, and wonder if the 165 HP Subie engine is > > enough engine in that aircraft for these parts (assume it's >supercharged). > > I'd originally planned on putting in a 180 HP Lycoming, so I'm thinking > > the supercharged Subie might be "close enough". One thing I would > > seriously consider doing is to sell my -7 emp and switch to a -9. >(snip) > I live in Albuquerque, and density altitude is also a big issue here. Field elevation is 5,380'. The current RV-6A that Eggenfellner is using as his show plane came from here..sort of. Homer Rogers built it in Canada, and sold it to Gary Seaton here in Albuquerque after I gave it my blessing. (GREAT airplane). My understanding is that after this year's fly-in season, Gary will get the airplane back. I should be able to get a flight or two in it with the Subie and will report what I find. I know this doesn't help you with your decision right now, but the expectations are that the airplane will have similar performance characteristics, with the turbo keeping the power up whereas the Lyc is pretty much outta poop right from the start. Brian Denk RV8 N94BD ________________________________________________________________________________
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
Subject: cheap and easy landing lights
Date: Mar 12, 2002
SNIP I like the Duckworks system. I think once installed, it looks nice, and it's a LOT easier than cutting up our wingtips and installing something out there. SNIP I'm sure the duckworks is nice, but if you have the RV-7 style wingtips that come with premolded lenses and follow the directions on my website you'll have a perfectly suitable landing light in each wingtip for less than $15 total cost. And if you decide you don't like them you can repair the hole in the wingtip in about 2 minutes. If you decide you don't like the duckwork hole in your wing skins... you're stuck. No flames intended... just sharing info. You can call me for advice, if needed. You can even buy a kit for this from Bill Von Dane if you like. It's all here... scroll clear to the bottom and look at the wingtip lights section. http://www.usi.edu/science/chemistry/vfrazier/Construction%20Notes%20for%20t he%20tail%20and%20wings.htm you may need to paste the long link back together in your browser. If that won't work click on the URL below and then go to the Wings and Tail section. Vince Frazier 812-985-7309 home 812-464-1839 work Stinson 108, NC97535 flying F-1H Rocket, N540VF reserved http://www.usi.edu/science/chemistry/vfrazier/page1.html ________________________________________________________________________________
From: skydog-8(at)attbi.com
Subject: Re: RV-8/A rear seat riser
Date: Mar 12, 2002
Randy, there ARE pictures on your web site. They are hideing under my name(the Randy Griffin part of your web site). Griff. > > > I built the seat riser per plans, EXCEPT that I used only two ribs; one on > > each side. The inner two ribs were replaced with crosswise angles. I > > believe Randy Lervold did the same thing. I've had some mega bubbas > sitting > > on it with no problems at all. By removed the two inner ribs, you have a > > very nice storage space available to you by removing the seat cushion, and > > lifting the pan up. This can be a very nice place to store things that > are > > not usually needed...like some small survival goodies, a gun (you just > never > > know), paperwork, etc. > > > > By pulling the two hinge pins that hold it to the floor, it can be removed > > for really tall pax. You just put the cushion flat on the floor. > > > > Brian Denk > > RV8 N94BD > > 279 hrs. > > > Yep, leave out the two middle ribs and put in a couple of stiffeners, works > great. And I think I made mine out of slightly thicker material than called > for in DJ's plans to help compensate for eliminating the two center ribs. I > thought I had a pic of mine on my web site but I guess not. I'll try to add > one. BTW, one of the benefits of using the riser rather than just thicker > cushions is that you build some angle into the seating surface. With plain > cushions I would think there's a tendency for the seat bottom to slide > forward. > > Randy Lervold > RV-8 N558RL 151 hrs. > www.rv-8.com > > > > > > ________________________________________________________________________________
From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com>
Subject: Rivet gun malfunction
Date: Mar 12, 2002
I sprayed some WD-40 into mine and ran it with the restrictor full open. Just let it pound on some wood for a while. Stopped only to spray some more WD-40 into it. I couldn't believe the amount of black gunk that came out. When it seemed to fire normally at the right pressure setting I oiled at it worked fine. Got that advice from some Ozzies. God love them Ozzies! Scott VanArtsdalen, MCSE, CCNA Network Administrator Union Safe Deposit Bank 209-946-5116 -----Original Message----- From: Brian Denk [mailto:akroguy(at)hotmail.com] Subject: Re: RV-List: Rivet gun malfunction >> >Another day, another question... > >I basically took several years off from building. Long story. Obviously >I'm >back at it, but I noticed something about my rivet gun the other day. > >If I press the gun tightly against the work surface and pull the trigger, >it >won't fire. If I back it off a little bit, THEN it can fire. > >Seems to me I used to hold it as tightly as I could against the surface to >prevent a wide array of problems. Which would mean this new behavior >is a malfunction. > >Anyone have clues how I can fix this? I have one of the guns from Avery. > >Note that I DO hand-oil my air tools with a couple of drops of oil at >the start of a session. However, the rivet gun sat unused for 2 or 3 >years. > >Thanks for the help. > >-Joe > > I had an Avery gun that did basically the same thing. It would misfire randomly...just sorta go "phfffftt". I sent it to Bob Avery and he rebuilt the innards...for FREE...and sent it back. Your situation may just be a case of congealed oil or dirt in the mechanism. Maybe a solvent clean followed by a fresh oiling would do the trick. If not, send it off to Bob and I'm sure he'll take care of it for you. Brian Denk RV8 N94BD MSN Photos is the easiest way to share and print your photos: http://photos.msn.com/support/worldwide.aspx ________________________________________________________________________________
From: "Charles Graves" <cgraves(at)secor.com>
Subject: Hartzell Propeller For Sale....
Date: Mar 12, 2002
Hartzell HC-C2YK-1BF Blades F7666A-2 (74") 205 hours since new Include Spinner (Fits Glasair I but may work for RV's?) $3500.00 Chuck Graves cgraves(at)secor.com ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Re: Hooker Harness - What Size?
Date: Mar 12, 2002
This will depend on how you secure the crotch strap to the fuse, how thick your seats are and how thick you are. Mine are installed just far enough aft of the control column that it won't interfere with it. I am at work now so I can't measure them but it seems like I only need about 4 inches of strap. I actually have the strap as short as I can get it. Hooker does a very beefy sewing job. The webbing threads through the hardware and is sewn together for ??inches. The double thickness webbing will not fit through the hardware. I have the two hardware ends as close as I can get them due to the double thickness of strap. What I would do is talk with the folks at Hooker and see if they would customize the crotch strap. In my opinion, the sewing does not have to be as beefy for the crotch strap as for the rest of the belts. If you can, sit in the plane with you seats in and measure the distance between where you are securing the end to the fuse and your lap. Have Hooker make the crotch belt so it adjusts 2-3 inches around this midpoint. Hope this isn't to confusing. Ross ----- Original Message ----- From: <czechsix(at)juno.com> Subject: Hooker Harness - What Size? > > > Hi Ross, what length do you recommend? Is this for the RV-6, or -8, or > what? > > Thanks, > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A finish kit stuff, thinking about Hooker harnessses.... > > _________________________________________________________________________ > _______ > From: "Ross Mickey" <rmickey(at)ix.netcom.com> > Subject: Re: RV-List: Hooker Harness - What Size? > > > Norman, > > I got the narrow ones and they seem plenty wide. Especially since they > have > the pads. I did NOT spring for the rotary buckle. The standard one > works > very well and is easily removed with one hand. One suggestion. If you > are > putting in the crotch strap, you may want to have them shorten the strap > length. I have a whole wad of strap that I either have to secure or I > will > cut it off. leaving a ragged edge. > > Ross Mickey > > > ----- Original Message ----- > From: "Norman" <nhunger(at)sprint.ca> > > Looking at the 5 point hooker harness available from Team Rocket for > > $312 USD, they are available in different widths. > > Which one is best for an RV6A? > > 1.75" or 2" or 3"? > > Also, has anyone bucked up $499 for these belts with the rotary > buckles? > > Are they worth it? > > > ________________________________________________________________ ________________________________________________________________________________
From: "Rick Jory" <rickjory(at)msn.com>
Subject: Re: Hooker Harness - What Size?
Date: Mar 12, 2002
A reminder that the following also sells 4 and 5 pt harnesses for the Van's series of aircraft. www.icdc.com/~morristec/ They utilize the "Schroth" restraint system used on the Airbus and other planes (many sailplanes use these). Part of this system is a harness webbing that slightly stretches under G forces to reduce injury, plus the "rotary" single point connect device (I believe team rocket offers this as an option). I haven't ordered my belts yet, so I can't suggest these over Hooker. Rick Jory RV8A ----- Original Message ----- From: Ross Mickey <rmickey(at)ix.netcom.com> Subject: RV-List: Re: Hooker Harness - What Size? > > This will depend on how you secure the crotch strap to the fuse, how thick > your seats are and how thick you are. Mine are installed just far enough > aft of the control column that it won't interfere with it. I am at work now > so I can't measure them but it seems like I only need about 4 inches of > strap. I actually have the strap as short as I can get it. Hooker does a > very beefy sewing job. The webbing threads through the hardware and is sewn > together for ??inches. The double thickness webbing will not fit through > the hardware. I have the two hardware ends as close as I can get them due > to the double thickness of strap. What I would do is talk with the folks at > Hooker and see if they would customize the crotch strap. In my opinion, the > sewing does not have to be as beefy for the crotch strap as for the rest of > the belts. If you can, sit in the plane with you seats in and measure the > distance between where you are securing the end to the fuse and your lap. > Have Hooker make the crotch belt so it adjusts 2-3 inches around this > midpoint. Hope this isn't to confusing. > > Ross > > > ----- Original Message ----- > From: <czechsix(at)juno.com> > To: > Subject: Hooker Harness - What Size? > > > > > > > > Hi Ross, what length do you recommend? Is this for the RV-6, or -8, or > > what? > > > > Thanks, > > > > --Mark Navratil > > Cedar Rapids, Iowa > > RV-8A finish kit stuff, thinking about Hooker harnessses.... > > > > > > _______ > > From: "Ross Mickey" <rmickey(at)ix.netcom.com> > > Subject: Re: RV-List: Hooker Harness - What Size? > > > > > > Norman, > > > > I got the narrow ones and they seem plenty wide. Especially since they > > have > > the pads. I did NOT spring for the rotary buckle. The standard one > > works > > very well and is easily removed with one hand. One suggestion. If you > > are > > putting in the crotch strap, you may want to have them shorten the strap > > length. I have a whole wad of strap that I either have to secure or I > > will > > cut it off. leaving a ragged edge. > > > > Ross Mickey > > > > > > ----- Original Message ----- > > From: "Norman" <nhunger(at)sprint.ca> > > > Looking at the 5 point hooker harness available from Team Rocket for > > > $312 USD, they are available in different widths. > > > Which one is best for an RV6A? > > > 1.75" or 2" or 3"? > > > Also, has anyone bucked up $499 for these belts with the rotary > > buckles? > > > Are they worth it? > > > > > > ________________________________________________________________ > > ________________________________________________________________________________
From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com>
Subject: Camloc part no's
Date: Mar 12, 2002
Dear Fellow RV-List'ers, After battling with the side hinges on my RV-4 cowling, I've decided to abandon the side hinges in favor of camlocs. I want to keep the hinge on the top and rear portions of the cowling. I called Skybolt and explained what I was trying to do. He said no problem, we'll sell you a kit for $300. I said that I don't need a whole kit, I just need enough camlocs to do the sides of my cowling and what are the part no's so I can order them from you. The salesman got very huffy and suspicious at this point. He spent the next minute or so explaining to me how he was not going to "give away" the contents of his kit just so I could go order them some place cheaper. His words and tone were very suspicious and accusatory. ??!! I find it odd too because I thought Skybolt manufactures their own camlocs... where else did he think I was going to find Skybolt camlocs. It's a shame, I would have preferred to use their camlocs. Now, he was willing to give me the part numbers if I supplied my credit card number immediately. I elected not to do so because I had other parts to order and I wanted to supply a complete list which I had not, as of that time, compiled. I politely thanked him for his time and hung up. I fully intended to order the camlocs from Skybolt but by the end of the conversation he was right, I will be ordering the camlocs somewhere else. Now, I'm not too up to date on my camloc lore, could someone please tell me what type of camlocs I should order? What parts will I need besides the camloc itself and the recepticle? Any special tools? Disclaimer: I understand that many of you have had very good experiences with Skybolt and I'm sure their product is very good. But my experience with Pete on the phone this morning turned me off of Skybolt. It is not my intent to defame or steer any customers away from Skybolt. I'm just relating my experience with the company. Original to RV-List(at)matronics.com Scott VanArtsdalen, MCSE, CCNA Network Administrator Union Safe Deposit Bank 209-946-5116 ________________________________________________________________________________
From: Zrxordeath(at)aol.com
Date: Mar 12, 2002
Subject: Re: Fin and Rudder loads--not RV related
From a rank amateur, Gordon, I am about as new to flying as you can get, having about 35 hours, and just finishing up my cross country solos. I discovered exactly the phenomenon you are describing while flying a Cessna 152. While cruising along one day, just messing around a little, to "see what would happen", I quickly deflected the rudder back and forth, a small amount. It felt really "weird", so I craned my neck around like an owl, and did it again (quick learner). I was shocked to see the whole empennage wagging around indepenent of the fuselage, and VERY quickly added this activity to the "Dont do" list. After landing, my buddy who runs the fuel truck, pulled up, to fill the plane, and I asked him about it. His eyes got a little wide, and he said he'd done the same thing, with the same result, and conclusion. I don't know the aerodynamics behind it, but it looked scary as hell, and I will remember this when I test fly my RV-7A, in a year or so. I imagine things like this can cause bad events to happen. Is this a form of flutter? Anyway, I will be doing a lot of reading, before I put on my "test pilot" hat. It served as a reminder that I definately dont know it all. Not by a long shot. Good luck all, Kyle Beckstrom RV7A Emp ________________________________________________________________________________
From: "Bob Busick" <panamared1(at)brier.net>
Subject: Re: Camloc part no's
Date: Mar 12, 2002
This is not the answer you wanted. But, I would recommend getting their catalog. This will give you the parts and pictures of the different type of camlocs. Yes, there are a lot of different variations, and it took me a few hours of studing the catalog before I decided what I needed (much of it comes down to your personal preference). The catalog also has a great "how to section" with pictures, and it is written just for the RV-4. However, an RV is an RV and a Camloc is a Camloc so the instructions will easily translate to the other RVs. Like most piecies of equipment, it does not come with instructions, that is why the catalog is important. Also you probably will want a couple of the camloc tools (I highly recommend the grommet tool), without them it can be a real pain! It is all in the catalog. Bob > > Dear Fellow RV-List'ers, > > After battling with the side hinges on my RV-4 cowling, I've decided to > abandon the side hinges in favor of camlocs. I want to keep the hinge on > the top and rear portions of the cowling. I called Skybolt and explained > what I was trying to do. He said no problem, we'll sell you a kit for $300. > I said that I don't need a whole kit, I just need enough camlocs to do the > sides of my cowling and what are the part no's so I can order them from you. > The salesman got very huffy and suspicious at this point. He spent the next > minute or so explaining to me how he was not going to "give away" the > contents of his kit just so I could go order them some place cheaper. His > words and tone were very suspicious and accusatory. ??!! I find it odd too > because I thought Skybolt manufactures their own camlocs... where else did > he think I was going to find Skybolt camlocs. It's a shame, I would have > preferred to use their camlocs. > > Now, he was willing to give me the part numbers if I supplied my credit card > number immediately. I elected not to do so because I had other parts to > order and I wanted to supply a complete list which I had not, as of that > time, compiled. I politely thanked him for his time and hung up. I fully > intended to order the camlocs from Skybolt but by the end of the > conversation he was right, I will be ordering the camlocs somewhere else. > > Now, I'm not too up to date on my camloc lore, could someone please tell me > what type of camlocs I should order? What parts will I need besides the > camloc itself and the recepticle? Any special tools? > > Disclaimer: I understand that many of you have had very good experiences > with Skybolt and I'm sure their product is very good. But my experience > with Pete on the phone this morning turned me off of Skybolt. It is not my > intent to defame or steer any customers away from Skybolt. I'm just > relating my experience with the company. > > Original to RV-List(at)matronics.com > > Scott VanArtsdalen, MCSE, CCNA > Network Administrator > Union Safe Deposit Bank > 209-946-5116 > > ________________________________________________________________________________
Date: Mar 12, 2002
From: Ken Balch <kbalch1(at)attbi.com>
Subject: A baffling question...
The little drawing that came with my baffle kit doesn't do a great job of depicting the layout of the seal material. I've managed to figure out everything but the proper orientation of the two pieces that span the small gap between the forward, horizontal baffles and the lower cowling inlets. It seems to make sense to rivet the material to the underside of the inlet and rest it on top of the baffle, but I can't recall ever seeing an RV with rivet heads inside the inlets. Can this be right, or am I missing something here? -- Regards, Ken Balch Ashland, MA RV-8 #81125 (N118KB) last 90% groups.yahoo.com/group/BostonRVBuilders/files/ ________________________________________________________________________________
From: "TERRY BENZER" <TERRYBENZER(at)prodigy.net>
Subject: Oil canning RV-8 elevator
Date: Mar 12, 2002
I am about to final rivet my left elevator and found that I now have oil canning only on the bottom half outboard of the trim tab. I have taken the skeleton out of the skin and put clecos in every hole with no change. Should I try tightening the trailing edge bend? Any other ideas would be appreciated Thanks ________________________________________________________________________________
Date: Mar 13, 2002
From: Dr Leo Davies <leo(at)icn.usyd.edu.au>
Subject: [Fwd: engine failure]
Date: Tue, 12 Mar 2002 17:32:51 +1100 From: Dr Leo Davies <leo(at)icn.usyd.edu.au> Subject: engine failure Dear List, I have had a couple of recent mid-life crises in my RV6. I thought I would share them with the list in the interests of preventing trouble for others. The most recent one was last weekend and went as follows. I was tooling along in my RV6A VH-LDX. She is an IFR aircraft and I was on an IFR plan but CAVOK at 8000 feet 55% cruise. The engine starts to run rough and then quits (that fast!). I look at the panel and see the H/L fuel pressure light blinking on my EI fuel management instrument. I check the fuel pressure and it is 0.0 (low). I change tanks and turn on the boost pump. The fuel pressure climbs and the engine re-starts. I am now about 8 seconds into my in-flight emergency. I am overhead a militiary airbase (runways dissapear over the horizons) so make a call telling them I am dropping in for a pre-cautionary landing. On the ten minute descent from 8000 feet (boost pump on all the time) I am wondering what happened. The wondering is accompanied by a slight fuel smell. On landing I turn off the boost pump and watch the pressure decay to zero again. By the time I taxi to the visitors parking lot I have decided that my 140 hour old 0-360 A-1-A has eaten its fuel pump and am mentally writing letters to Lycoming. Because I am due at a clinic 200 miles away I organize a rental car and head off. Three days later I am back with a mechanic to have a look at the problem. We take off the cowls and I hop in the front seat and turn on the master and the boost pump. The air around us is filled with a fine mist of aerosolized gasoline. Yikes..... So what happened? I have a priming system that taps off the gascolator to a solonoid and thence to the cylinders. I had always figured that a leak in this system would be a non-event because of the small quantity of fuel in the copper lines. Wrong.... The line between the gascolator and the solonoid had fractured. The engine pump was then sucking air through the gascolator and thus my engine failure. When I turned on the boost pump I solved the problem but at the expense of pouring fuel out of the gascolator into the engine compartment. I spent ten minutes or so on descent pumping fuel onto my left sided exhaust pipes. Someone smiled on me and I didn't catch fire. Why did the line fracture? I am not sure. I had an antivibration loop in the copper tube. I may have overflared the small gauge tubing or it may just have work hardened. Given the failure mode (unfriendly in the extreme) I am going to alter the system and use a flexible hose between the gascolator and the solonoid. A failure in a braided hose is likely to be much less unfriendly than in the copper which fractured clean through and left a serious orifice. If you are using this system I suggest you inspect the gascolator to solonoid connection and consider a change in materials. I welcome any alternative suggestions and in particular what I might have done wrong in manufacturing the copper tube link. Safe flying Leo Davies VH-LDX ________________________________________________________________________________
From: "Greg Young" <gyoung@cs-sol.com>
Subject: the Phoenix
Date: Mar 12, 2002
Eight months ago today, at about this time, I launched on the fateful first flight in my RV-6. Yesterday afternoon I got word that I was the successful bidder on the salvage. Hard to believe it took 8 months to resolve but I'll save my railings about the insurance company for a later time. I've fired off the check and should have the plane back in my hanger by the end of next week. So for all who asked, I'm now officially back in the RV building business and will be re/building the/a -6. After all, I've got an undamaged spinner and canopy. How could I not build another airplane around a canopy that could survive that crash? My current plan is to find an -6 (-6a?) project completed to the QB stage or beyond. There seem to be a lot of tail & wing projects available but not many with the fuselage so I am also considering building a new fuselage and picking up a tail/wing project. I have not completely dismissed a -7 but there's a part of me that wants to rebuild rather than build a new airplane. And I KNOW how strong the -6 is. But then again it might be fun to throw the -7 boxes in the air and have it come down assembled; } I may revise my plans when I get a good look at the wreckage and can inventory what, if any, structure is salvageable. If you know of any projects available, please let me know or pass my contact info (see below) to them. Finally, thank you to all of you for your thoughts, prayers and concerns over the last 8 months. It has meant a lot to me. An incident like this gives you a much deeper appreciation for the bond between all of us and just how special this community of RVers really is. I wish I was flying but under the circumstances I'm thrilled to be back as an active builder. Regards, Greg Young RV-6 N6GY ...Rebuilding! searching for Navion to fly gyoung@cs-sol.com Office/Cell: 281-376-0235 x123 Home: 281-376-2913 ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Mar 12, 2002
Subject: Intercom recommendations?
Hi all: I'm getting ready to order a bunch of avionics and having trouble deciding on an intercom. I'm going no frills (at least initially), with a single Icom A-200 com, a low end transponder, probably GTX 320A and no panel mount music system. Given that, and no obvious need for stereo, I'd sure appreciate hearing what intercoms some of you guys who are flying are using and are either happy or not satisfied with. Harry Crosby Pleasanton, California RV-6, wiring (just starting) ________________________________________________________________________________
Date: Mar 11, 2002
Subject: Camloc part no's
From: Don Jordan <dons6a(at)juno.com>
www.gen-aircraft-hardware.com You can get a free tech book which is great. call 888-247-2738 to get prices. Don Jordan - N6DJ - 6A Arlington, Tx ****************************** writes: > > > Dear Fellow RV-List'ers, > > After battling with the side hinges on my RV-4 cowling, I've decided > to > abandon the side hinges in favor of camlocs. I want to keep the > hinge on > the top and rear portions of the cowling. I called Skybolt and > explained > what I was trying to do. He said no problem, we'll sell you a kit > for $300. > I said that I don't need a whole kit, I just need enough camlocs to > do the > sides of my cowling and what are the part no's so I can order them > from you. > The salesman got very huffy and suspicious at this point. He spent > the next > minute or so explaining to me how he was not going to "give away" > the > contents of his kit just so I could go order them some place > cheaper. His > words and tone were very suspicious and accusatory. ??!! I find it > odd too > because I thought Skybolt manufactures their own camlocs... where > else did > he think I was going to find Skybolt camlocs. It's a shame, I would > have > preferred to use their camlocs. > > Now, he was willing to give me the part numbers if I supplied my > credit card > number immediately. I elected not to do so because I had other > parts to > order and I wanted to supply a complete list which I had not, as of > that > time, compiled. I politely thanked him for his time and hung up. I > fully > intended to order the camlocs from Skybolt but by the end of the > conversation he was right, I will be ordering the camlocs somewhere > else. > > Now, I'm not too up to date on my camloc lore, could someone please > tell me > what type of camlocs I should order? What parts will I need besides > the > camloc itself and the recepticle? Any special tools? > > Disclaimer: I understand that many of you have had very good > experiences > with Skybolt and I'm sure their product is very good. But my > experience > with Pete on the phone this morning turned me off of Skybolt. It is > not my > intent to defame or steer any customers away from Skybolt. I'm just > relating my experience with the company. > > Original to RV-List(at)matronics.com > > Scott VanArtsdalen, MCSE, CCNA > Network Administrator > Union Safe Deposit Bank > 209-946-5116 > > > > > messages. > > > > > > ________________________________________________________________________________
Date: Mar 12, 2002
Subject: Re: A baffling question...
From: Denis Walsh <deniswalsh(at)earthlink.net>
De Jaw Vous all over again!! This is exactly the same research, and conclusion I came to five years ago. I still very seldom see any one with it done that way, but that's the way I did it, and several others have been influenced by me to do it that way since. I used squeezed on universal head rivets with the heads up. Used a backing strip of .016 for the rubber so the rivets wouldn't pull through the rubber seal. Works fine and keeps cool. A gap of about .5 inch is needed. More and the rubber will flop. Less and you can't coax it around when putting the lower cowl on. Oh yeah, the rubber piece which you are going to rivet to the lower cowl inlet needs to curl up along the sides also :+). > From: Ken Balch <kbalch1(at)attbi.com> > Reply-To: rv-list(at)matronics.com > Date: Tue, 12 Mar 2002 16:10:19 -0500 > To: "rv-list(at)matronics.com" > Subject: RV-List: A baffling question... > > > The little drawing that came with my baffle kit doesn't do a great job > of depicting the layout of the seal material. I've managed to figure > out everything but the proper orientation of the two pieces that span > the small gap between the forward, horizontal baffles and the lower > cowling inlets. It seems to make sense to rivet the material to the > underside of the inlet and rest it on top of the baffle, but I can't > recall ever seeing an RV with rivet heads inside the inlets. Can this > be right, or am I missing something here? > > -- > Regards, > Ken Balch > Ashland, MA > RV-8 #81125 (N118KB) > last 90% > groups.yahoo.com/group/BostonRVBuilders/files/ > ________________________________________________________________________________
Date: Mar 13, 2002
From: Dr Leo Davies <leo(at)icn.usyd.edu.au>
Subject: Re: Engine Failure
> Dear List, >


March 06, 2002 - March 12, 2002

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