RV-Archive.digest.vol-bn

June 06, 1996 - June 17, 1996



      >on?  One of the reasons to leave the skin off is for better access to the
      >back of the panel on a slider-equipped -6, right?
      
      Didn't anybody point out the option mentioned in the plans and construction 
      manual of making the panel removable? I found this very handy and it avoided the
      problems mentioned.
      
      FKJ
      
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Subject: Re: Top fwd fuse skin
Date: Jun 06, 1996
From: aol.com!EBundy2620(at)matronics.com
4.1) (8.7.4/8.7.3) with SMTP id QAA05049 for ; Thu ________________________________________________________________________________
Date: Jun 06, 1996
From: "Elon Ormsby" <Elon.Ormsby(at)quickmail.llnl.gov>
Subject: GPS
REGARDING GPS Weather or not selective availability (SA) is turned on or off is irrelevant for commercial use. From the very beginning all research and systems proposed for commercial use of GPS were designed to do an end-run around the degraded SA frequency. The speed of the official development taking place scares even the bureaucratic FAA. All of you know that you can use current certified IFR GPS in-route with accuracy incredibly better that VOR's (with SA turned-on). So what is the big deal - precision approach capability is just around the corner. Before you condemn the gov't take note: WAAS (Wide Area Augmentation System) is going to be the USA system. The FAA has just canceled the $475 million contract awarded to Wilcox electric and awarded a new contract to Wilcox's subcontractor, Hughes. Now get this, the reason cited was that Wilcox failed to meet milestones. Within 4 months of the award the FAA warned them they were slipping. In 6 months they sent a letter and within 8 months they canceled the order and awarded it to Hughes. That is unheard of in the government and is a example of their new freedom from Federal Acquisition Regulations. Hughes is expected to make up for lost time with initial deployment in 1998. FAA has canceled all development of MLS (microwave Landing System) with efforts directed toward GPS. The European Joint Aviation Authority has certified a Litton GPS/INS for the airbus A340/A330 for sole, in-route use, without the aid of terrestrial nav aids. It is a non-precision approach to 250 ft. This was a joint JAA & FAA effort. Honeywell has demonstrated its SLS-2000 in Europe. It was done in a company Citation with autopilot coupled approaches. It is accurate to within 5ft horizontally and 6ft vertically. The FAA will shift from "positive control" to free flight in the future. They are funding research on Cockpit Display Traffic Information (CDTI). It is proposed as an inexpensive means of insuring separation of general aviation aircraft (an absolute must for commercial free flight). None of the above cares about SA! Your big worry is who is going to pay for it. No one knows the true cost of the GPS system because it is budgeted in a air force black program. (rumors are it is $1 billion per year). The entire world is using it but only US taxpayers are paying for it. The current scheme is to surcharge each GPS unit that is sold (and maybe even the Dbase updates!). For sure you know the air force is going to move costs to the FAA who will then move those costs to the users. So while everyone is paying for it now - you (the user) will most likely be paying $300-400 more per unit when you buy one. But at least that car-moving-map in Japan will have antied-up. -Elon ________________________________________________________________________________
Subject: Re: GPS SELECTIVE AVAILABILITY
Date: Jun 06, 1996
From: Mike Kukulski <kukulski(at)indirect.com>
Response to my earlier posting: > >Ummmm.... Guys... let us think about the claim that higher accuracy gps >systems threaten the security of the USA.... While I may be to blame for bringing up the subject of military concerns over disabling GPS SA, I certainly didn't expect the subject to blossom into a debate over the issue. That discussion belongs on an armchair general's newsgroup, not the RV-List. Let's get back to buildin', flyin', and talkin' RVs!! Mike Kukulski (kukulski(at)indorect.com) RV-4 N96MK (wings fairings, flap linkages, fuellines, etc..) ________________________________________________________________________________
From: Michael Angiulo <mikeang(at)MICROSOFT.com>
Subject: Air Compressor deal, Drill press advice needed
Date: Jun 06, 1996
I totally agree. I have this behemoth in my house now and use headphones whenever it runs. Anyone who can suggest a way for me to make this thing quieter (I've enen contemplated burying it) please let me know. Where do you find oiled/belted compressors? I checked Sears, the Price Club, and large Eagle hardware before settling on this nightmare. ---------- From: ROBERT BUSICK[SMTP:nmsu.edu!rbusick(at)matronics.com] Sent: Thursday, June 06, 1996 3:49 PM Subject: Re: RV-List: Air Compressor deal, Drill press advice needed IMHO even if Sam's gave me the aircompressor free I would not take it. I have an oil free one and it make so much noise I am about to toss it. I definately plan on getting a quiet oilbath type. Costs more, but it is either that or quit building. My motto, buy expensive now, to save later. Bob Busick RV-6 rbusick(at)nmsu.edu On Thu, 6 Jun 1996, Tim Lewis wrote: > I found a pretty good deal at Sams (the Wal Mart warehouse), and I've > noticed that Sams often stocks the same "deals" in several locations. > Here in San Antonio they have a Coleman 4.5 hp, 25 gal air > compressor/tank, 9cfm @ 40 psi, 7.2 cfm @ 90 psi, w/ built in regulator > for $199. It's oil free, direct drive type. > > I'm looking for advice on a drill press: > > 1. 14" bench mount, 210-3700rpm, 3/4 hp from Harbor Freight, $200 > (has a "free oiler", whatever that is) > 2. 13" floor mount, 195-3630rmp, 3/4 hp from Harbo Freight, $230 > ("dry table, no oiler needed" whatever that means) > 3. 15" bench mount, 250-3100 rpm, 1 hp from Sears, $300 > > I'm inclined to go with the $200 unit from Harbor Freight. What's an > oiler? Any advice from the group on drill presses? > > Tim Lewis > Buying tools, waitin' fer the kit > ________________________________________________________________________________
Date: Jun 06, 1996
From: bill garrett <bgarrett(at)fast.net>
Subject: Re: RE: Service Charge
>Nice to know I was wrong on this one. Seems that Van's policy now is >to wear the merchant fee themselves. Good one Van's. I doubt that this is really true. More likely we're all paying for those who choose to charge the kits. My impression is that Van has always watched his profit margins carefully and tried to give as much bang for the buck as possible. I'd bet that some of this year's price increase is to cover his costs of accepting credit cards! He may not even be able to tell us exactly how much it is, but he has a bottom line and what he spends he must recover (plus a few sheckels to keep avgas in the RV's). Bill ________________________________________________________________________________
Date: Jun 06, 1996
From: ammeterj(at)ammeterj.seanet.com (John Ammeter)
Subject: Re: Arlington AirFair
At 03:37 PM 6/6/96 GMT, xxxx(at)xxxx.xxx.gov wrote: >John, > >I'm one of the lurkers on the RV-list who will soon reveal my true >identity (picking up RV-6 empennage kit on 6/21). > >I'd like some specifics on the Arlington AirFair. What are the >dates and some of the items on the agenda. > >Thanks, > >Xxxx > In deference to your request to remain anonymous I've deleted your true identity. However, I think my reply is of interest to many others besides yourself. The Arlington Airfair is held July 10-14 at Arlington Airport. Arlington Airport is about 40 miles north of Seattle. It is a former military field (from the Big One, WWII). It, during the airfair, will have one runway, 16/34. That runway is about 60 feet wide by 5000 feet long and surrounded by flat fields. Arlington is THE premier airport in Western Washington for First Flights. As an uncontrolled field, we're able to taxi test, do run-ups or whatever without contacting the Tower (ain't got one). During the Airfair there will be talks by aviation authors, aircraft fly-bys, homebuilders workshops, evening programs, exhibits, forums, special guest speakers, camping, showers, complete food service (don't forget the RV Picnic on Saturday afternoon), free shuttle to downtown street fair on Sat/Sun, etc. For more information you can 'surf' to 'http://www.nweaa.org/nweaa/' or email the airfair office at 'office(at)nweaa.org'. Again, be sure to register at the Puget Sound RVators Hospitality Tent next to the RV aircraft parking. If any RV builders or would be builders are driving into the Airfair we are offering admission tickets at the same price that pilots flying in to the Airfair will pay. This is a significant savings (50% to 66%). I will have tickets available shortly. The cost will be $5.00 for one day (sorry, Saturday only) and $10.00 for the entire week. I can mail them to you if you include a self addressed envelope with your payment (make check payable to Puget Sound RVators). John Ammeter ammeterj(at)ammeterj.seanet.com Seattle WA, USA RV-6 N16JA Flying 5 years ________________________________________________________________________________
From: jpl(at)showpg.mn.org (Joe Larson)
Subject: Trim Tab
Date: Jun 06, 1996
Folks -- I now have a trim tab! How we can get such a sense of satisfaction from such a minor accomplishment.... I have some general notes for people who follow. First, to all who told me the size of my rivet puller hole was too large and suggested methods of fixing, thanks! The 4 pulled rivets I just did look great. Turns out my puller had a 2-hole head, and the larger of the two was in place. I swapped, it worked great. Next, I have a minor problem in my trim tab. I'm not really going to worry about fixing it, but I thought I would warn people. When riveting the hinge to the elevator, the hinge bent slightly here and there due to the pressure of the rivets. This causes some difficulty in inserting the hinge pin (it's now REALLY tight), and some minor binding when I flop the trim tab back and forth. I recommend other people try to avoid this. Unless someone else has already solved the problem, I would recommend you insert the hinge pin. You are squeezing these rivets with the trim tab removed (and half the hinge is already riveted to the trim tab), but if you re-insert the pin, maybe it'll be stiff enough that it won't bend (or won't bend as much). If anyone has a good idea of how to fix mine, I'll take suggestions. Otherwise I won't worry about it. -Joe -- Joe Larson jpl(at)showpg.mn.org 612-591-1037 Showpage Software, Inc. http://www.wavefront.com/~showpg 6121 St. Croix Ave. N. Golden Valley, Mn 55422 Future RV-6A pilot. ________________________________________________________________________________
From: BPattonsoa(at)aol.com
Date: Jun 06, 1996
Subject: Re: GPS SELECTIVE AVAILABILITY(joke)
Who needs a GPS to deliver a small nuclear warhead. UPS is cheaper, faster, and much more accurate. B Patton ________________________________________________________________________________
From: JamesCone(at)aol.com
Date: Jun 06, 1996
Subject: Re: Top fwd fuse skin
To avoid the trouble of bucking rivets that were hard to get to after I installed all of my radios and instruments, I just popped in a few more pop rivets (Avex structural kind available from Van's) and filled the holes. Pop, pop, pop....I am after all, a charter member of Popaholics Anonymous, as any of my newsletter subscribers will attest to. Jim Cone jamescone(at)aol.com ________________________________________________________________________________
Date: Jun 06, 1996
From: Fred Hiatt <hiatt001(at)gold.tc.umn.edu>
Subject: Re: Air Compressor deal, Drill press advice needed
Tim Lewis wrote: > > I found a pretty good deal at Sams (the Wal Mart warehouse), and I've > noticed that Sams often stocks the same "deals" in several locations. > Here in San Antonio they have a Coleman 4.5 hp, 25 gal air > compressor/tank, 9cfm @ 40 psi, 7.2 cfm @ 90 psi, w/ built in regulator > for $199. It's oil free, direct drive type. > > I'm looking for advice on a drill press: > > 1. 14" bench mount, 210-3700rpm, 3/4 hp from Harbor Freight, $200 > (has a "free oiler", whatever that is) > 2. 13" floor mount, 195-3630rmp, 3/4 hp from Harbo Freight, $230 > ("dry table, no oiler needed" whatever that means) > 3. 15" bench mount, 250-3100 rpm, 1 hp from Sears, $300 > > I'm inclined to go with the $200 unit from Harbor Freight. What's an > oiler? Any advice from the group on drill presses? > > Tim Lewis > Buying tools, waitin' fer the kit Tim, I can't comment about the harbor frieght drill press, my drill press is a 1950's vintage Sears table mount. It's so heavy I can't lift it alone.(don't build them like they used to). However try to get one that has some beef (read heavy). You didn't ask about a bandsaw-- by all means get a good one. Mine is a 12" Delta, and it is a real mans tool (argh, argh). I use it constantly, not only on the RV metal but for countless other jobs. Good luck. Fred Hiatt ________________________________________________________________________________
Date: Jun 06, 1996
From: barnhart(at)a.crl.com (Dave Barnhart)
Subject: Re: F-625 Rib
>O.K. I have been following the fuselage construction manual found on >Hovan's page. So far everything has been going great. Even the part >where he stated that the F625 rib is too wide for the F-606 bulkhead. >I would like to here what alternatives others came up with to remedy the >problem. I found that mine were off in both dimensions (length and height). I split them *diagonally*, then spliced them back together. Whether is would have been easier to make two new flanges is a tossup. Best Regards, Dave Barnhart rv-6 sn 23744 ________________________________________________________________________________
From: WCannon313(at)aol.com
Date: Jun 06, 1996
Subject: Re: Top fwd fuse skin
Ed I left the top skin off of my -6 until the very very end and had no problem, You will be glad you did so when you are hooking everything up. Walt Cannon First engine start today!!!!!!!!!!!!! ________________________________________________________________________________
Date: Jun 04, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: fuslge side skins
> My concern is that some of the cowling hinges attach here and I don't want to > weaken the F601B by c-sinking it - but I also don't like the idea of c-sinking > the F670 skins... The F-601B firewall is .062 -- plenty thick to machine c-sink for 3/32 rivets. The skin is only .032. I know which one I'M going to countersink.... Randall Henderson randall(at)edt.com RV-6 ________________________________________________________________________________
Date: Jun 04, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Bair RV-6 in Sport Aviation.
> Couple that with the > gummint letting us have the industrial strength GPS signal soon and it's > going to be a whole new world, soon. Anyone know if there is a timeline for this yet, or is it still "probably soon"....? Randall Henderson randall(at)edt.com RV-6 ________________________________________________________________________________
Date: Jun 03, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: GPS
>... I have > just recently received a new King KLX-100 GPS/Comm and the jury is still out. I > am a little disappointed in the fact that both special use airspace and > intersections were removed from the data base. I'm surprised to hear that (no special use airspace). Do you know if they offer a version that _does_ have special use airspace? I find that to be one of the most useful features of the moving map type GPS units. No way I'd pay the money they're asking for it if it didn't have that. Randall Henderson randall(at)edt.com RV-6 ________________________________________________________________________________
From: WCannon313(at)aol.com
Date: Jun 06, 1996
Subject: Re: Electric Flap Installation
Fred I used the technique you mentioned of having two pins go from the center outward - simple, strong, and works like a charm. Walt Cannon ________________________________________________________________________________
Date: Jun 06, 1996
From: Cleaveland Tool and Material <clevtool(at)tdsi.net>
Subject: Cleaveland 800 number
I understand that I made a typo... our 800# really is 1-800-368-1822. Please re-update your catalogs. Sorry for the confusion, Mike ________________________________________________________________________________
From: frankv(at)pec.co.nz
Date: Jun 07, 1996
Subject: Re: Top fwd fuse skin
In <960606224533_129638391(at)emout17.mail.aol.com>, on 06 June 96 at 10:45 PM, aol.com!JamesCone(at)matronics.com said: >To avoid the trouble of bucking rivets that were hard to get to after >I installed all of my radios and instruments, I just popped in a few >more pop rivets (Avex structural kind available from Van's) and >filled the holes. I'm a long way from this part, but it occurs to me that it might be worth replacing the rivets with screws, so that access to instruments for maintenance is less of a chore. Or would the hassles of preventing leaks and/or fixing instruments damaged by leaks be greater than the hassle of occasionally crawling under the dash? -- -------------------------------------------------------------------- frankv(at)pec.co.nz | "Knowledge=Power=Energy=Matter=Mass; Frank van der Hulst | A good bookshop is just a genteel Software Engineer | Black Hole that knows how to read". PEC(NZ) Ltd (Cardax), Marton | Terry Pratchett, "Guards! Guards!" http://www.pec.co.nz/~frankv/ | -------------------------------------------------------------------- ________________________________________________________________________________
Date: Jun 06, 1996
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Air Compressor deal, Drill press advice needed
>Where do you find oiled/belted compressors? I checked Sears, the Price >Club, and large Eagle hardware before settling on this nightmare. > I bought mine at Home Depot, Cambell Hausfield 4.5hp 20 gal, $327. Harbor Freight has 'em too. Rob Acker (r.acker(at)ix.netcom.com) Rancho Santa Margarita, CA ________________________________________________________________________________
Date: Jun 06, 1996
From: Curt Reimer <Curt_Reimer(at)MBnet.MB.CA>
Subject: Re: Air Compressor deal, Drill press advice needed
On Thu, 6 Jun 1996, Tim Lewis wrote: > 1. 14" bench mount, 210-3700rpm, 3/4 hp from Harbor Freight, $200 > (has a "free oiler", whatever that is) > 2. 13" floor mount, 195-3630rmp, 3/4 hp from Harbo Freight, $230 > ("dry table, no oiler needed" whatever that means) > 3. 15" bench mount, 250-3100 rpm, 1 hp from Sears, $300 > > I'm inclined to go with the $200 unit from Harbor Freight. What's an > oiler? Any advice from the group on drill presses? I'd get the floor mount. I have no idea what the oiler is, but I bought a cheap floor mount and am glad I did. 3/4 hp is lots, but it sure is nice to be able to crank down the table when I need to, or just swing it out of the way. Plus, it doesn't take up any bench space, and the shavings fall on the floor, not on my bench. I have a grinder mounted on my main workbench and the bench top is constantly covered with aluminum dust. I should really build a stand for it. The speed ranges are adequate on all of them that you listed. Curt Reimer ________________________________________________________________________________
Date: Jun 07, 1996
From: Curt Reimer <Curt_Reimer(at)MBnet.MB.CA>
Subject: Re: Suburu RV-6 Update
On Thu, 6 Jun 1996 MikeT(at)aol.com wrote: > I visited NSI this am to check on the progress of the RV-6 Suburu prototype. > prices as of now are: 160hp $16,950, 180hp $18,450 and 200hp $19,950 adding > their prop with the package adds $2550. The packages include mount, wiring, Considering they cost virtually as much as a Lyc. and have no safety or reliability record behind them, and havn't even flown on an RV yet (!), I don't think I'll be sending NSI a deposit anytime soon. Of course, if the first 20 engines run like swiss clocks for 2000 hours and really are cheap to rebuild (i.e. I don't have to virtually replace the entire engine) I'll change my mind. Assuming NSI actually sells 20 engines at that price! Curt Reimer ________________________________________________________________________________
From: WStucklen(at)aol.com
Date: Jun 07, 1996
Subject: Re: Top fwd fuse skin
> I agree that it is best to leave this skin off until the last possible >moment. I looked at a RV-6 the other day and the builder was going to save >riveting this skin until the very last moment, like, even after the >instrument panel was installed. I pointed out that he probably wouldn't >like trying to rivet around his radio stack, gyros, wiring, plumbing, canopy >release mechanism, etc. Bob Skinner RV-6 > > Bob: I had no problem riviting the front top skin even after all the radios were installed. The stack (less actual radio) can be easily riveted around. I had my 15 Year old do the bucking: Small hands, very nimble.... I wouldn't ever consider putting my 200+ Lbs frame down under there to do that job! ( Though I've been there many a time since ..) When this riveting was done, few of the mechanical instruments were in the panel as I didn't want to shake them up during the riveting process. Just my $.02 worth..... Fred Stucklen RV-6A N925RV (Installing optional electric flaps.. Should be flying today..) wstucklen(at)aol.com ________________________________________________________________________________
From: WStucklen(at)aol.com
Date: Jun 07, 1996
Subject: Re: Top fwd fuse skin
>Fred, > >Did you use the proseal between the skins or as a fillet at the joint after >riveting. I remember some talk a month or so ago about the possibility of >weaking joints if used between the skins. > >Ross Mickey Ross: I used it between the skins ans have not had any signs of a weakened structure. From day one, I planned an IFR aircraft that would be seeing weather, and this sealant method seems to have held up to those expectations. I've not had an leaks (tiltup canopy) even in level 4 rain. Just be sure to close all potential water leak areas, especially the the bending radius relief slos in the F-668 bulkhead, and its drip edge. Fred Stucklen RV-6A N925RV wstucklen(at)aol.com ________________________________________________________________________________
From: jperri(at)interserv.com
Date: Jun 07, 1996
Subject: Re: GPS
All their other units have the special-use airspace. That's why I was surprised when this one didn't. When I called and talked to their GPS reps. their answer was that it was for VFR use only. Sound like a liability issue. He also would not comment if they would add this back in to the data base latter. I am not letting up I going to fax a letter about several user issues to their Customer Service department. I will advise. JMP ________________________________________________________________________________
From: EBundy2620(at)aol.com
Date: Jun 07, 1996
Subject: Re: Top fwd fuse skin
>moment. I looked at a RV-6 the other day and the builder was going to save >riveting this skin until the very last moment, like, even after the >instrument panel was installed. I pointed out that he probably wouldn't >like trying to rivet around his radio stack, gyros, wiring, plumbing, canopy >release mechanism, etc. Bob Skinner RV-6 Well, that's kind of what I had in mind too. With the sliding canopy, the instrument panel is pretty much fixed (it's strucural with the top skin according to Ken at Van's) once installed. So if you don't install the panel goodies first, you get to do all of it laying on your back under the panel. I'm just concerned about the riveting vibration attacking the avionics and gauges. Everything's a comprimise... Ed Bundy ebundy2620(at)aol.com ________________________________________________________________________________
Date: Jun 07, 1996
From: James Kelley <72466.1355(at)CompuServe.COM>
Subject: RE: Service Charge (chatter)
> > My RV-8 empennage order form doesn't mention any 4% service charge for > credit > card. I'd like to know if this is for real. > > > > Steve Johnson > > spjohnson(at)mmm.com > >Nice to know I was wrong on this one. Seems that Van's policy now is >to wear the merchant fee themselves. Good one Van's. A local (Atlanta) radio consumer advocate had a represenitive from MasterCard on his talk show some time back. He stated that it was against MC terms and conditions for a business to add a surcharge for using MC. He did not answer about other cards. He did state that their is no problem if a business offered a discount, for paying cash instead of using MC. I guess someone could have complained and caused a problem for Van's, I don't really know. IMHO: Van's could add x% to the price of the kit and give a x% cash discount. That would help take the CCCs out of the loop. James Kelley 72466.1355(at)compuserve.com ________________________________________________________________________________
Date: Jun 07, 1996
From: Phil Arter <arter(at)ncar.ucar.edu>
Subject: RV-8 HS-405 Ribs
Well, I found a mistake I had already made when drilling the HS-405 ribs to the front spar assy. Referring to the detail in the upper rt corner of dwg 3PP that says "middle and root ribs", and shows 3 rivets in the flange that attaches to the front spar, I put holes in the center of the HS-405 root rib flanges & spars. Then, after talking to Mike Angiulo about skin clearance around the HS-814, I noticed on the detail of the HS-404 rib cutout that it shows 2 rivets between the HS-810 and 814. If there is room, I will put 3 rivets between the spar splices, otherwise just 2, and leave the center hole I drilled by mistake empty. HS skeleton in jig & trued up. Phil arter(at)ncar.ucar.edu ________________________________________________________________________________
Date: Jun 07, 1996
From: "Gene Gottschalk ((301) 286-0708)" <geneg(at)rattler.gsfc.nasa.gov>
Subject: Re: Fuel Flop Tube
All, That's my opinion as well. It doesn't cost much, it's easy to do while in construction, and say, it make an otherwise boring 2nd tank construction more interesting. Also gives you the opportunity to make as yet unmade mistakes and improves Van's economy! -Gene, RV6a, fuse in jig >IMO, even if you don't plan on having an inverted fuel system, I would >install one flop tube. The reason is that you might one day decide that you >want an inverted system and the modification of the fuel tank would be a pain >in the @$$ once the plane is together and flying. > >Gary Corde >RV-6 N211GC > > ________________________________________________________________________________
Date: Jun 07, 1996
From: Harry Paine <HPair(at)ix8.ix.netcom.com>
To all I'm sorry but I'm getting tired of reading some of the stuff I see being asked. I've been in aircraft 25 years and have either built, repaired, rebuilt aircraft by all major aircraft companies. 1. If you guys are worried about that top fuselage skin .. screw the sucker on with nut plates spaces properly to carry the structural load..... its done all the time on factory built A/C. and would be a heck of alot easier When not if something goes wrong on the instrument panel, thats what I plan on doing when I get there.. I hate getting upside down under an inst panel if I know I don't have to. 2. As for pro seal weaking a joint that is fillet sealed???? I don't know where in the %^&*( that came from) but if thats true then every kerosene queen that anybody on this list has flown on has weakened joints.. because thats how there put together. Trust me when you have to repair a bonded joint its a $%^&*( because that joint is so strong with all rivets, bolts, hi locks, jobolts, removed its still strong, and takes a lot of prying to get apart. All majors require that most joints be fay sealed with a product similiar to pro seal only better and easier to use... it just costs 3 - 4x more. Which brings me to another question if I could show you guys how to do the both tanks in two - three days..... but had to pay say $100.00 - $150.00 using the same stuff that boeing or Mac DAC uses on their commercial A/c would any of you put up that kind of money? If so I could arrange to get some... please contact me personally, not on the list. later Harry Paine HPair(at)ix.netcom.com ________________________________________________________________________________
From: "Bob Newman" <bn(at)poseidon.crosslink.net>
Date: Jun 07, 1996
Subject: RV-6/8 Will I be comfortable?
I'm in the serious information gathering stage of a potential RV-6 or maybe an RV-8 project. A primary concern for me is seating comfort. I am 6' 3" tall, 175 lbs, 34" pants inseam. I tried on the factory prototype RV-6, and while I liked it, I found the seat back angle to be far too bolt upright for my taste. Leg room to the rudder pedals was tight, as was clearance from my head to the canopy. The airshow crowd prevented a more extended look, but the factory representative said all of this could be easily adjusted to suit my needs during construction. I tried on the the RV-8 at Sun-N-Fun and found it to be better. The adjustable rudder pedals allowed adequate leg room at the most forward position. Canopy clearance was excellent. However, the seat was still too bolt upright for me. My wife did not like the tandem seating as well as the side by side RV-6, and I really like the quick build kit for the RV-6. I would appreciate advice and comments, particularly from other tall builders that may have been through this already. Specific questions: 1. Can the seat back angle on the RV-6 or 8 be changed? Would that interfere with the rear seating on the RV-8? 2. Can I get adequate headroom in the RV-6 with thinner cushions, etc, and still have a comfortable seat? 3. Is it possible to move the rudder pedals forward or the seat back on the RV-6 for more leg room? 4. Should a tall guy like me build the RV-6 quick build, or wait (maybe 2 years??) for and RV-8 quick build kit? Bob Newman Warrenton, VA bn(at)crosslink.net I want to build one... ________________________________________________________________________________
Date: Jun 07, 1996
From: Kelli Lewis/Michael Kosta <mikel(at)dimensional.com>
Subject: Re: Air Compressor deal, Drill press advice needed
IMHO even if Sam's gave me the aircompressor free I would not take it. I have an oil free one and it make so much noise I am about to toss it. I definately plan on getting a quiet oilbath type. Costs more, but it is either that or quit building. My motto, buy expensive now, to save later. Bob Busick RV-6 rbusick(at)nmsu.edu On Thu, 6 Jun 1996, Tim Lewis wrote: > I found a pretty good deal at Sams (the Wal Mart warehouse), and I've > noticed that Sams often stocks the same "deals" in several locations. > Here in San Antonio they have a Coleman 4.5 hp, 25 gal air > compressor/tank, 9cfm @ 40 psi, 7.2 cfm @ 90 psi, w/ built in regulator > for $199. It's oil free, direct drive type. > > I'm looking for advice on a drill press: > > 1. 14" bench mount, 210-3700rpm, 3/4 hp from Harbor Freight, $200 > (has a "free oiler", whatever that is) > 2. 13" floor mount, 195-3630rmp, 3/4 hp from Harbo Freight, $230 > ("dry table, no oiler needed" whatever that means) > 3. 15" bench mount, 250-3100 rpm, 1 hp from Sears, $300 > > I'm inclined to go with the $200 unit from Harbor Freight. What's an > oiler? Any advice from the group on drill presses? > > Tim Lewis > Buying tools, waitin' fer the kit > ________________________________________________________________________________
Date: Jun 07, 1996
From: Kelli Lewis/Michael Kosta <mikel(at)dimensional.com>
Subject: Re: Air Compressor deal, Drill press advice needed
>IMHO even if Sam's gave me the aircompressor free I would not take it. I >have an oil free one and it make so much noise I am about to toss it. I >definately plan on getting a quiet oilbath type. Costs more, but it is >either that or quit building. My motto, buy expensive now, to save later. > >Bob Busick >RV-6 >rbusick(at)nmsu.edu Well, yes but the fact is the oil free compressors do work for not too much money. Mine is an Ingersol-Rand that has been doing its job for 5 years without problems. Yes, it still scares the bejebers out of me every time it starts up but I stuffed it under one of my work benches and used a fuselage packing crate top to make a door for it to live behind. Cut the noise in half and (maybe) would protect things if the tank someday decides to blow. I suppose someday I may get an oilbath type or mount an oil bath compressor on this tank. Michael Kosta RV-4 Fly By July mikel(at)dimensional.com ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: Fuel Flop Tube
Date: Jun 07, 1996
Well, to drag this on, please be advised that a flop tube has more complexity and therefore has more chance for proplems down the road. Here is why: The fixed aluminum tube will not (or should not) move if properly installed. Once it is installed it should never have a problem. The flop tube has some form of a flexable fuel line inside the tank. These can harden with age and cause problems. Things like the Pitts use to use a hose that they found was hardening with age. They have changed to the yellow tygon fuel hose. Hopefully that will last longer, but how knows. Second, you have a large metal end on the flop tube. That thing bangs around inside the tank. On aerobatic aircraft, you will find small aluminum flakes in your fuel strainer. This is from the flop tube hitting the tank and chipping away at the aluminum. Most have an O ring on the end to help prevent this but sometimes the O ring comes off. The flop tube requires some guides inside the tank so it does not get hung up on something. If it does not return to the bottom of the tank, well then your usable fuel can decrease a lot. The purpose of this message is to point out that everything has tradeoffs. Don't make it any more complex than you really require as you will have to maintain that complexity over the years. You have to weight the alternatives and do what you feel is correct for your needs and aircraft. Herman > All, > > That's my opinion as well. It doesn't cost much, it's easy to do while in > construction, and say, it make an otherwise boring 2nd tank construction > more interesting. Also gives you the opportunity to make as yet unmade > mistakes and improves Van's economy! > > -Gene, RV6a, fuse in jig > > >IMO, even if you don't plan on having an inverted fuel system, I would > >install one flop tube. The reason is that you might one day decide that you > >want an inverted system and the modification of the fuel tank would be a pain > >in the @$$ once the plane is together and flying. > > > >Gary Corde > >RV-6 N211GC > > > > Herman Dierks, Dept. E54S, AWSD, Austin, Texas mail: dierks(at)austin.ibm.com ________________________________________________________________________________
Date: Jun 07, 1996
From: Kelli Lewis/Michael Kosta <mikel(at)dimensional.com>
Subject: Re: Air Compressor deal, Drill press advice needed
IMHO even if Sam's gave me the aircompressor free I would not take it. I have an oil free one and it make so much noise I am about to toss it. I definately plan on getting a quiet oilbath type. Costs more, but it is either that or quit building. My motto, buy expensive now, to save later. Bob Busick RV-6 rbusick(at)nmsu.edu On Thu, 6 Jun 1996, Tim Lewis wrote: > I found a pretty good deal at Sams (the Wal Mart warehouse), and I've > noticed that Sams often stocks the same "deals" in several locations. > Here in San Antonio they have a Coleman 4.5 hp, 25 gal air > compressor/tank, 9cfm @ 40 psi, 7.2 cfm @ 90 psi, w/ built in regulator > for $199. It's oil free, direct drive type. > > I'm looking for advice on a drill press: > > 1. 14" bench mount, 210-3700rpm, 3/4 hp from Harbor Freight, $200 > (has a "free oiler", whatever that is) > 2. 13" floor mount, 195-3630rmp, 3/4 hp from Harbo Freight, $230 > ("dry table, no oiler needed" whatever that means) > 3. 15" bench mount, 250-3100 rpm, 1 hp from Sears, $300 > > I'm inclined to go with the $200 unit from Harbor Freight. What's an > oiler? Any advice from the group on drill presses? > > Tim Lewis > Buying tools, waitin' fer the kit > ________________________________________________________________________________
Date: Jun 07, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Top fwd fuse skin
Rob Lee said: > Also, I have the 2" sub panel on the bottom of the Instrument panel (which I > highly recommend), for switches / controls / fuel gauges and breakers etc - > which obviously reduces access room to some extent. Can you elaborate on why you recommend this? More space for switches/gauges, removable for better access, or what? The reason I ask is because I am trying to do all I can to maximize knee/leg room (like eliminate the center console), so I don't want add a sub-panel if I can help it. Randall Henderson randall(at)edt.com RV-6 ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 07, 1996
Subject: Re:
>To all >I'm sorry but I'm getting tired of reading some of the stuff I see being >asked. I've been in aircraft 25 years and have either built, repaired, >rebuilt aircraft by all major aircraft companies. >SNIP>>>>>>>>> >later Harry Paine >HPair(at)ix.netcom.com > Hey Harry.....Chill out a little. Most of the people on this list haven't worked on aircraft for 25 years and are here to learn. I'm flying a 4 that I built and I wasn't born knowing how to do it. I learned just like you did from people that have gone before me. I find some questions basic but one stupid question is better that one stupid mistake. I'm sure there are alot of people on this list that could use your experience. Regards: Rusty Gossard N47RG RV-4 Flying ________________________________________________________________________________
Date: Jun 07, 1996
From: "R. BUSICK" <rbusick(at)nmsu.edu>
Subject: Re: Arlington AirFair
John What is your address, so I can order tickets. Thanks Bob Busick RV-6 rbusick(at)nmsu.edu > > Again, be sure to register at the Puget Sound RVators Hospitality Tent next > to the RV aircraft parking. If any RV builders or would be builders are > driving into the Airfair we are offering admission tickets at the same price > that pilots flying in to the Airfair will pay. This is a significant > savings (50% to 66%). > > I will have tickets available shortly. The cost will be $5.00 for one day > (sorry, Saturday only) and $10.00 for the entire week. I can mail them to > you if you include a self addressed envelope with your payment (make check > payable to Puget Sound RVators). > > John Ammeter > ammeterj(at)ammeterj.seanet.com > Seattle WA, USA > RV-6 N16JA > Flying 5 years > > ________________________________________________________________________________
From: Ken.Hitchmough(at)IRAP.NRC.CA
Date: Jun 07, 1996
Subject: FUEL PUMP FOR INJECTED ENGINES
Posting-Date: Fri, 07 Jun 1996 14:20:00 -0500 (EST) Importance: normal A1-Type: MAIL Hop-Count: 2 For those of you contemplating putting fuel injection on your RV, here is a snippet of info that could save you some bucks and time. The Welden high pressure pump is NOT self priming! I learned this at my cost by destroying one that ran dry for 30secs only! My pump was mounted on the firewall and was thus not wet at the inlet. These pumps apparently blow quite well but can't suck to save their life. The obvious position for the pump is right down on the fuselage wall at the tank level. I opted to put it on the firewall for two reasons: 1. I didn't want high pressure lines in the cockpit 2. I wanted to be able to pressurize the system from either tank My solution to the problem is to put a facet pump just after the selector valve, this will supply a head of fuel to the high pressure pump. (If anyone sees a major flaw in this please yell!) I know the thought of having an aux pump for the aux pump seems a bit ridiculous but it does seem like the simplest solution. It also saves having to put a high pressure gascolator in the system (a gascolator is mandatory I believe here in Canada) I'll see how it does this weekend when I install it and have another go at my fuel flow test. Ken RV6A ________________________________________________________________________________
Date: Jun 07, 1996
From: ammeterj(at)ammeterj.seanet.com (John Ammeter)
Subject: Ticket to Arlington
>Return-Path: >Date: Fri, 07 Jun 1996 08:22:38 -0600 (MDT) >From: Bob Stobart <stobart(at)fiber.uwyo.edu> >Subject: Ticket to Arlington >To: ammeterj(at)ammeterj.seanet.com >X-UIDL: 49b5c36dee61016b48d18a4b3a6be213 > >Would you send me your address as I would like to purchase a ticket to the >show. In your message you didn't provide your street address. > >Thanks! > >Bob Stobart > > I should have proofed that email----- It is difficult to send mail without an address. so--for a ticket(s) to Arlington Airfair Send stamped self-addressed envelope to: John Ammeter 3233 NE 95th St Seattle WA 98115 $5.00 for Saturday only, $10.00 for all week. Make check payable to Puget Sound RVators. John Ammeter ammeterj(at)ammeterj.seanet.com Seattle WA, USA RV-6 N16JA Flying 5 years ________________________________________________________________________________
Date: Jun 07, 1996
From: Curt Reimer <Curt_Reimer(at)MBnet.MB.CA>
Subject: Re: Fuel Flop Tube
On Fri, 7 Jun 1996, Gene Gottschalk ((301) 286-0708) wrote: > All, > > That's my opinion as well. It doesn't cost much, it's easy to do while in > construction, and say, it make an otherwise boring 2nd tank construction > more interesting. Also gives you the opportunity to make as yet unmade > mistakes and improves Van's economy! I put one in just for the heck of it. My question is: did anyone adapt a filter screen of some kind to the tube? The stock tube just has a 1/4" or so hole in the end; looks like it could suck up lots of gunk into the fuel lines. Curt Reimer ________________________________________________________________________________
Date: Jun 07, 1996
From: Curt Reimer <Curt_Reimer(at)MBnet.MB.CA>
Subject: Re: your mail
On Fri, 7 Jun 1996, Harry Paine wrote: > To all > I'm sorry but I'm getting tired of reading some of the stuff I see being > asked. I've been in aircraft 25 years and have either built, repaired, > rebuilt aircraft by all major aircraft companies. > 2. As for pro seal weaking a joint that is fillet sealed???? I don't know > where in the %^&*( that came from) but if thats true then every kerosene > queen that anybody on this list has flown on has weakened joints.. because > thats how there put together. Trust me when you have to repair a bonded > joint its a $%^&*( because that joint is so strong with all rivets, bolts, > hi locks, jobolts, removed its still strong, and takes a lot of prying to > get apart. All majors require that most joints be fay sealed with a product > similiar to pro seal only better and easier to use... it just costs 3 - 4x > more. I recall seeing the video on building the 777 jet, where they even used sealer between the main spar flanges and the web! The big question here is quality control. If the builder gobs too much sealer on the faying surfaces, it just might result in a weaker joint. It might also be the case that those commercial aircraft are designed from the beginning to use the sealer, and compensate by using more rivets, bigger parts, whatever. Just a thought. My own empirical testing tends to agree with Harry. A 1" square joint glued together with ProSeal only (NO rivet) seemed to be much stronger and more rigid than a single 3/32 rivet through the same sized parts. I have no data to support this however. Curt Reimer ________________________________________________________________________________
Date: Jun 07, 1996
From: bcos(at)ix.netcom.com (William Costello )
Subject: Re: Air Compressor deal, Drill press advice needed
Hi Folks, Cheez, how many times is this bloody air compressor message going to bounce around? I have a Sears oil-less and it is noisy, but I can live with it in a walled off area with a louvered door. After all, this building stuff is not going to last forever! I hope! Best Regards, -- Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 Building RV-6 or 6A | Reserved N97WC ________________________________________________________________________________
Date: Jun 07, 1996
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: RV-6/8 Will I be comfortable?
>I am 6' 3" tall, 175 lbs, 34" pants inseam. I tried on the factory Hello Bob, I'm 6'4", 220, 36" inseam. RV-6 Quickbuild kit on order. I've tried on both the RV-6 and RV-8. The -8 is the better fit...but SBS seating has become important to me. The following is information I gathered directly from Van's and/or my trip to Sun'n'Fun. >1. Can the seat back angle on the RV-6 or 8 be changed? Would that >interfere with the rear seating on the RV-8? If you build the RV-6 with sliding canopy, the fuselage brace that the top seat back rests on can be moved back up to 3". This is in addition to the standard seat back angle adjustment. >2. Can I get adequate headroom in the RV-6 with thinner cushions, >etc, and still have a comfortable seat? I don't know if you have experienced this, but sometimes when I am trying a car on for size, I may fit but its a little tight (head brushing headliner, etc.). After fifteen minutes of driving I forget all about that. I seem to "stretch" when trying something on for size, then go into more relaxed mode when I forget about trying to fit in it. Anyhew...The seat pan can be lowered about 1" in the center portion. Seems your torso may be longer than mine (jeez...I already need 39.5" seated torso room). >3. Is it possible to move the rudder pedals forward or the seat >back on the RV-6 for more leg room? >From the posts here on the list, it seems some forward pedal displacement is possible. I will wait till I get to the "sitting" stage of fuselage construction; then start moving pedals, seats, and canopies around so I fit. Of course, to assure the selection of a comfortable seating position, I will be spending many hours in the garage making airplane noises (and coming up with an inflight relief system) . >4. Should a tall guy like me build the RV-6 quick build, or wait >(maybe 2 years??) for and RV-8 quick build kit? Do you want SBS or tandem? Good luck! Rob Acker (r.acker(at)ix.netcom.com) Rancho Santa Margarita, CA / RV-6Q / N164RA reserved ________________________________________________________________________________
From: PFPA(at)aol.com
Date: Jun 07, 1996
Subject: Re: GPS SELECTIVE AVAILABILITY(joke, not really)
If a nuke is ever detonated on US soil it will likely be delivered in a suitcase, not on top of an ICBM. And, if this is the case I don't think the owner will really care whether his bomb goes off on baggage carousel #s one, two, or three. I would be willing to bet that the same congress people pushing this selective GPS issue are also the ones promoting this new push for "star wars". And, who by coincidence are the major employers and political contributers in their districts? ...Raytheon, Marrietta, McDonald-Douglas, etc.... Corporate welfare for mega organizations who lack the guts to compete in the civilian marketplace. Follow the money folks. Now, back to my spray booth, unless some of you think its time for me to change the filters in my mask. Andy Gold ________________________________________________________________________________
Date: Jun 07, 1996
From: Kelli Lewis/Michael Kosta <mikel(at)dimensional.com>
Subject: Re:
>>To all >>I'm sorry but I'm getting tired of reading some of the stuff I see being >>asked. I've been in aircraft 25 years and have either built, repaired, >>rebuilt aircraft by all major aircraft companies. >>SNIP>>>>>>>>> >>later Harry Paine >>HPair(at)ix.netcom.com >> >Hey Harry.....Chill out a little. Most of the people on this list haven't >worked on aircraft for 25 years and are here to learn. I'm flying a 4 that >I built and I wasn't born knowing how to do it. I learned just like you did >from people that have gone before me. I find some questions basic but one >stupid question is better that one stupid mistake. > >I'm sure there are alot of people on this list that could use your experience. > >Regards: >Rusty Gossard >N47RG RV-4 Flying > > Thanks Rusty: you said what I was thinking. I had the opportunity to work as an aircraft mechanic for 6 years which REALLY helped in trying to figure out what was what and how things might be put together...but EVERYONE (Harry) will have questions as the project progresses. I enjoy having builders drop in and see what progress has taken place. And they usually have a question about the part of the project they are presently working on (remember building the TAIL SECTION?). Happy to help out. Sadly, however, not many flyers drop in to see what is going on. Guess they are TOO BUSY flying. Hope that isn't universal. Keep asking: the only stupid question is one that doesn't get asked. Michael Kosta RV-4 Fly By July mikel(at)dimensional.com ________________________________________________________________________________
From: JFLEISC(at)aol.com
Date: Jun 07, 1996
Subject: Re: Suburu RV-6 Update
automotive powered planes offer some interesting cost, power, and fuel advantages. however, someday (be it unlikly) you may want to sell your plane. there are a lot of nonbuilder, nonA+P, pilots like me out there. when i bought my first auto powered plane i had great problems finding an A+P to do annuals. later when i went to sell it, many potential buyers turned it down for the same reason. any thing i saved i lost later. On to other things; i have a machinist friend helping me build a smoke system for my O-360 powered RV-4. can anyone tell me an economical and redily available smoke medium and corosponding flow rate? jim ________________________________________________________________________________
Date: Jun 07, 1996
From: "Elon Ormsby" <Elon.Ormsby(at)quickmail.llnl.gov>
Subject: big bucks
REGARDING big bucks Andy you forgot a few when you said: --------------------------- "... who by coincidence are the major employers and political contributors in their districts? ...Raytheon, Marrietta, McDonald-Douglas, etc.... Corporate welfare for mega organizations who lack the guts to compete in the civilian marketplace. ---------------------------- How about...... Hughes (for the WAAS-GPS system you will fly the rest of your life) Alcoa (the stuff your riveting) Dow Chemical (the windshield your looking through) Textron (that 320/360 making all the noise) Allied Signal (King Avionics for that 121.5 stuff) 3M (for the filter you definitely need to change) Don't forget Cutter labs so your kids don't get polio. And what a rip-off Intel is. Van's using their pentium for structural analysis of the -3 wing problem and the -6 &-8 punched skins are done on CNC. All megabuck companies that you derive no benefit from. Of course you could move to Australia and "import" your quality of life - what's a little shipping charge anyway! -Elon ________________________________________________________________________________
From: KennyCobb(at)aol.com
Date: Jun 07, 1996
Subject: Re: big bucks
Very well stated Elon I agree 100%, these industries contribute technology to GA that pioneer aviators could have never imagined. Ken Crabtree Bakersfield, CA ________________________________________________________________________________
Date: Jun 07, 1996
From: Frank Smidler <smidler(at)dcwi.com>
Subject: Re: Top fwd fuse skin
Frank K Justice wrote: > Didn't anybody point out the option mentioned in the plans and construction > manual of making the panel removable? I found this very handy and it avoided the > problems mentioned. > > FKJ > Frank, I'm planning to make my panel removeable and I'm at the point of deciding how I'm going to do it. I'd be very interested in your method for consideration. Frank Smidler RV-6 fuselage out of jig smidler(at)dcwi.com ________________________________________________________________________________
Date: Jun 08, 1996
From: Rion Bourgeois <RION(at)worldnet.att.net>
Subject: Re: RV-6/8 Will I be comfortable?
>I'm in the serious information gathering stage of a potential RV-6 or >maybe an RV-8 project. A primary concern for me is seating comfort. I >am 6' 3" tall, 175 lbs, 34" pants inseam. I tried on the factory >prototype RV-6, and while I liked it, I found the seat back angle to be >far too bolt upright for my taste. Leg room to the rudder pedals >was tight, as was clearance from my head to the canopy. The airshow >crowd prevented a more extended look, but the factory representative >said all of this could be easily adjusted to suit my needs during >construction. I tried on the the RV-8 at Sun-N-Fun and found it to >be better. The adjustable rudder pedals allowed adequate leg room at >the most forward position. Canopy clearance was excellent. However, >the seat was still too bolt upright for me. My wife did not like >the tandem seating as well as the side by side RV-6, and I really >like the quick build kit for the RV-6. I would appreciate advice >and comments, particularly from other tall builders that may have >been through this already. Specific questions: > >1. Can the seat back angle on the RV-6 or 8 be changed? Would that >interfere with the rear seating on the RV-8? > >2. Can I get adequate headroom in the RV-6 with thinner cushions, >etc, and still have a comfortable seat? > >3. Is it possible to move the rudder pedals forward or the seat >back on the RV-6 for more leg room? > >4. Should a tall guy like me build the RV-6 quick build, or wait >(maybe 2 years??) for and RV-8 quick build kit? > >Bob Newman >Warrenton, VA >bn(at)crosslink.net >I want to build one... I suggest you talk to Tom Green at Van's. He is at least 6'3" tall, and is quite comfortable in his RV-6. I have seen the quick build kits out at Van's, and the workmanship is very good. Buy the RV-6 quick build kit now, and if you decide you have to have an RV-8, and IF they produce an RV-8 quick build kit, sell your -6 and buy an -8. ________________________________________________________________________________
Date: Jun 07, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: RV-6/8 Will I be comfortable?
>I'm in the serious information gathering stage of a potential RV-6 or >maybe an RV-8 project. A primary concern for me is seating comfort. I >am 6' 3" tall, 175 lbs, 34" pants inseam. I tried on the factory >prototype RV-6, and while I liked it, I found the seat back angle to be >far too bolt upright for my taste. Leg room to the rudder pedals >was tight, as was clearance from my head to the canopy. The airshow >crowd prevented a more extended look, but the factory representative >said all of this could be easily adjusted to suit my needs during >construction. I tried on the the RV-8 at Sun-N-Fun and found it to >be better. The adjustable rudder pedals allowed adequate leg room at >the most forward position. Canopy clearance was excellent. However, >the seat was still too bolt upright for me. My wife did not like >the tandem seating as well as the side by side RV-6, and I really >like the quick build kit for the RV-6. I would appreciate advice >and comments, particularly from other tall builders that may have >been through this already. Specific questions: > >1. Can the seat back angle on the RV-6 or 8 be changed? Would that >interfere with the rear seating on the RV-8? > >2. Can I get adequate headroom in the RV-6 with thinner cushions, >etc, and still have a comfortable seat? > >3. Is it possible to move the rudder pedals forward or the seat >back on the RV-6 for more leg room? > >4. Should a tall guy like me build the RV-6 quick build, or wait >(maybe 2 years??) for and RV-8 quick build kit? > >Bob Newman >Warrenton, VA >bn(at)crosslink.net >I want to build one... Bob, I'm 6' 3 1/2", 200 lbs. and 35" inseam. I have plenty of room in my tilt canopy, RV-6. I have the floor mounted rudders so can't comment on suspended pedals. I have taken out the "seat angle adjuster" on the top portion of the seat backs and just let the seat back rest on the cross piece to give me a more comfortable recline angle. My seat cushions are 3" Temperfoam with 1" of medium density foam on top and the seat back is 1" of Sunmate with a 1" of medium density foam overlay. I end up with 1 1/2 to 2 inch space between headset and canopy. If you could poll most passengers, I think that most would prefer side by side seating. If this is what your wife prefers, I'd definately go with the side by side. She let you build the airplane, right. Time to stock pile goodwill. If you really want an eight, you can build that next. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 07, 1996
From: kightdm(at)carol.net (Danny Kight)
Subject: Re: User Fees, Thank You Randall
Randall, Thanks for the nudge to get me off top dead center. I, too, got the letter from AOPA urging response on the user fee issue, but with three daughters, a pregnant wife, a new house, and recent move, there is precious little free time. (Worst of all are my RV-6 wing and fuse crates buried under moving boxes in the garage!) I had intended to write my congressman earlier, but kept putting it off until I read your post yesterday. My letter goes in the mail tomorrow. Thanks for the boost, Danny Kight kightdm(at)carol.net Anderson, SC RV-6 empennage completed, trying to get the new house livable so I can start on the wings. >All: > >I just finished my letter to my gummint representative. I am presenting >it here in the hopes that it will inspire others to write their letters. >Feel free to plagarize at will. > >Make yourself heard. We need to send a clear message so they will stop >trying to push this user fee crap on us once and for all. > >The text original AOPA legislative alert follows the letter. > >Randall Henderson >randall(at)edt.com > >---- > >June 6, 1996 > >The Honorable Mark O. Hatfield >U.S. Senate >Washington, DC 20510 > >Senator Hatfield: > >I am writing to urge you to do all you can to make sure that the tax on >airline tickets, which expired on January 1, is reinstated as soon as >possible. I am very concerned that if this does not happen soon, the >Aviation Trust Fund, which General Aviation users have been dutifully >paying into through fuel taxes for many years, will go bankrupt, and >the factions that want to impose direct user fees on general aviation >will win. Then we will be saddled with a hugely burdensome and >inefficient user fee scheme after all. > >General Aviation organizations, as well as individual pilots and >aircraft owners, are virtually unanimous in their opposition to user >fees. Proponents of user fees argue that General Aviation users are not >paying their fair share for the facilities they use. I strongly >disagree. The primary reason the FAA/ATC system is as complex as it is >is because of the air carriers, and the primary reason GA aircraft USE >the system is so that they won't be in conflict with said air carriers' >operations. It is only just that the air carriers should bear the major >burden for the FAA and ATC system in the first place. > >The bankruptcy of the Aviation Trust Fund would be a huge tragedy. I >find it ironic that the word "Trust" is in the name, as we as pilots >and aircraft owners have "trusted" for a long time that the money we >pay will be used wisely. But now, suddenly, it is being drained for no >good reason, and I fear that if it runs out it will be used against us >in an effort to impose a new, additional, bureaucracy-heavy fee >structure on General Aviation. I do not believe I am exaggerating when >I say if that occurs, it is almost certain to kill the General Aviation >industry, and then user fees won't do any good, since there won't be >anyone there to pay them. > >Sincerely, > >Randall Henderson > >---- > >------------- Begin Included Message ------------- > >AOPA Legislative Action >500 E Street SW, Suite 290 >Washington, DC 20024 > > >Dear Randall W. Henderson: > >Our war against user fees has reached a pivotal battle. AOPA >Legislative Action urgently needs your help to win it! > >You may have heard that the tax on airline tickets, which provides >most of the FAA's funding through the Aviation Trust Fund, expired >on January 1. Along with fuel taxes general aviation pays, and taxes >on cargo and other fuels, the ticket tax was the source of 70 >percent of FAA's funding. For a while, the surplus in the trust fund >is keeping FAA running, but the balance will run out by the end >of the year. > >The ticket tax was caught in the same fight over the federal budget >that shut the federal government down several times and caused >Congress to finish the 1996 budget seven months late. But that >fight is over now. Why hasn't congress reinstated the tax? > >Insiders in Washington know why. Certain key members of Congress >want to choke the FAA so that Congress will impose USER FEES for air >traffic control and other services. > >We all know that Congress doesn't do much until there's a chrisis. >Look at the accident in Cheyenne, Wyoming last month involving >Jessica Dubroff. Younger and younger children have been involved in >record-setting attempts for a decade now, but Congress only reacted >after disaster struck. And I'm afraid the same thing could happen >to the Aviation Trust Fund -- with terrible results. > >Unless we stir them to action, we fear Congress will let the Trust >Fund go to the verge of bankruptcy. Then legislators will wake up >in October - right before an election - and realize they must do >something, ANYTHING, to ensure that the safety of the traveling >public isn't compromised by a lack of funding. And in the climate of >chrisis, politicians will stamped toward any idea to fund aviation. > >And the quickest and easiest way to do it will be user fees -- _that_ >_you_ _will_ _have_ _to_ _pay_. > >It won't matter that user fees would devastate general aviation, >cost too much to collect, terribly disrupt the aviation industry, >and hand the FAA a blank check to spend all it wants. All our >arguments against user fees, which have been quite successful in >holding them back so far, will be swept away in the mad rush to >DO SOMETHING. > >By ignoring the expired ticket tax and holding the Aviation Trust >Fund hostage, user fee proponents are staging a last-ditch attempt >to force a discredited idea down the throats of aviation users. >These people are willing to let the trust fund go bankrupt just >to push their agenda. > >As a pilot and a taxpayer, you have the right to tell your >representatives in Congress how important it is to reinstate the >excise taxes that feed the Trust Fund now. We need to preserve >the existing system of taxes, not bankrupt the airway system just to >impose a draconian user fee scheme. This is the message Congress >needs to hear: Save the Aviation Trust Fund from Bankruptcy. >Restore the ticket tax before the FAA runs out of money! And no >new user fees! > >Anyone who cares very much about the future of general aviation, >I know I can depend on you to speak up. It's even more important >that you act today, because your senator, Mark O. Hatfield, is >Chairman of the Senate Transportation Appropriations Subcommittee. >Please contact Senator Hatfield today and urge him to act to save >the Trust Fund. You can write to him at: > >The Honorable Mark O. Hatfield >U.S. Senate >Washington, DC 20510. > >(Or whoever your senator(s) is/are if you do not live in Oregon) > >Thank you for your help. To say that the future of general aviation >depends on you now is no exaggeration. > >Sincerely, > >Phil Boyer >President >AOPA Leglislative Action > >=========================================================================== > >You can find more information about the issue of user fees and >the Trust Fund on the web at >http://www.aopa.org/whatsnew/aopala.htm > >You can find the names/addresses of your Senators at >http://www.senate.gov/ > >Randall Henderson >randall(at)edt.com >------------- End Included Message ------------- > > > > ________________________________________________________________________________
Date: Jun 08, 1996
From: "J.JB" <101351.2343(at)CompuServe.COM>
Subject: French "reseau du sport de l'air"
from : Jean LeBorgne RV6 builder Dear friends of the light aviation, The French association of aircraft homebuilders, the "Reseau du sport de l'air",needs your HELP, to promote his Web site ! The "WEB D'Or" contest, managed by the Canadian site " France .com" is just OPEN for your votes ! Our Site is registered in the category "Associations", and sure, if our "score" is good, it will be much visited, of worldwide "netsurfers" ! What a chance to show our small homebuilt planes ! TO VOTE RSAir, two solutions : 1 - you visit our site, click on the "web d'or" (golden Web) logo : then fill up the Vote form, GO TO : http://ourworld.compuserve.com/homepages/RSAIR It would be nice to Sign the guestbook, and read the registre ! 2 - call directly the vote form, at the adress : http://www.france.com/cgi-bin/france/vv.pl?sid=1151 Then, you will receive an Email, to confirm your vote : only return the message code at the adress : vote(at)www.france.com IT IS WORTHY TO PARTICIPATE AT THIS CONTEST ! Nothing to win , but to become famous !............ Thank you for the "Reseau du Sport de l'Air" , always 100% homebuilt Aviation ! Just BUILT'N FLY ! Chers amis de la petite aviation, L'Association francaise des constructeurs amateurs d'aeronefs, votre " Reseau du Sport de l'Air" a besoin de votre aide pour faire connaitre son site WEB ! Le grand concours du "WEB D'Or" , propose par nos amis canadiens, viens d'etre ouvert a vos votes ! Nous sommes inscrits dans la rubrique "Associations", et il est sur que si nous faisons un bon "score", notre site sera beaucoup visite, de "netsurfeurs" du monde entier ! Quelle promotion pour nos petits avions ! POUR VOTER RSAir, deux solutions : 1 - visiter le site, et clicquer sur le logo "web d'or", pour voir apparaitre le bulletin de vote : rendez vous a : http://ourworld.compuserve.com/homepages/RSAIR et profitez en pour signer le livre d'or, et consulter la liste des signataires ! 2 - appeller directement le bulletin de vote a l'adresse : http://www.france.com/cgi-bin/france/vv.pl?sid=1151 Vous recevrez un peu plus tard un message vous demandant de CONFIRMER votre vote : Retournez un courrier , contenant uniquement le code du message, a l'adresse : vote(at)www.france.com CA VAUT LE COUP DE PARTICIPER A CE CONCOURS ! Il n'y a rien a gagner, sauf a etre CONNU ................................... MERCI pour le Reseau du Sport de l'Air, toujours 100% Aviation Amateur ! ________________________________________________________________________________
Date: Jun 08, 1996
From: joehine(at)mi.net (joehine)
Subject: Re: big bucks
>REGARDING big bucks > >Of course you could move to Australia and "import" your quality of life - >what's a little shipping charge anyway! >-Elon > Elon, no offence intended but some of us who live in small nations and not the U.S. actually like it that way and consider the occasional shipping charge worth it. I don't want to get a patriotic shouting match going here but that attitude of some americans that the rest of the world is some how inferior is very annoying. The US has its major advantages and major disadvantages just like any other country including mine. Just had to get that off my chest. :-] Joe joehine(at)mi.net Comp. 9, Site 8, RR#4 506-452-1072 Home Fredericton, NB 506-452-3495 Work Canada, E3B 4X5 Nobody on their death bed ever said "I wish I'd spent more time at work" ________________________________________________________________________________
From: glepore(at)direct.ca (Guido Lepore)
Subject: Re: Top fwd fuse skin
Unsubscibe ________________________________________________________________________________
From: BrabstonD(at)aol.com
Date: Jun 08, 1996
Subject: Preserving Engines
I have an O 320 that was reoverhauled in 1989. It has not been run since then. When I got it, about two years ago, I planned to have my airplane flying in about 18 months. ha ha. I have it mounted in a stand nose down. I've been turning it every few months and spraying WD40 in the spark plug holes. Now I realize it will be a long time before that engine ever gets "fired up." What should I do to preserve it until then? Doug Brabston ________________________________________________________________________________
Date: Jun 08, 1996
From: barnhart(at)a.crl.com (Dave Barnhart)
Subject: Re: Preserving Engines
>I have an O 320 that was reoverhauled in 1989. It has not been run since >then. When I got it, about two years ago, I planned to have my airplane >flying in about 18 months. ha ha. I have it mounted in a stand nose down. > I've been turning it every few months and spraying WD40 in the spark plug >holes. Now I realize it will be a long time before that engine ever gets >"fired up." What should I do to preserve it until then? Get a copy of Lycoming Service Instruction SL180A, "Engine Preservation for Active and Stored Aircraft". One of Tony Bengelis' books also has some good advice on this subject. Best Regards, Dave Barnhart rv-6 sn 23744 ________________________________________________________________________________
Date: Jun 08, 1996
From: Boris Robinson <smbr(at)inetw.net>
Subject: Re: Preserving Engines
>I have an O 320 that was reoverhauled in 1989. It has not been run since >then. When I got it, about two years ago, I planned to have my airplane >flying in about 18 months. ha ha. I have it mounted in a stand nose down. > I've been turning it every few months and spraying WD40 in the spark plug >holes. Now I realize it will be a long time before that engine ever gets >"fired up." What should I do to preserve it until then? > >Doug Brabston > Doug, I live 1000' from the ocean in S. Florida (90% humidity is normal). Don George, from who I bought my engine, installed moisture plugs and told me to spray CRC or LPS in the cylinders every 2 to 3 weeks. These are much better than wd-40, which does not displace water as well and can dry in a few weeks and actually attract it. When I bought some CRC the other day spray COSMOLINE was strongly recomended (haven't used yet). This is not as good as the Lycoming pickling procedure, but an alternative. Bye the way, when Don was telling me about keeping the rust away he also stressed that my engine was HOT. I've attached a ground wire to each mag, but I turn the crank backward anyway. He told me about a customer that was recently turning a new engine through with a srew diver and it 'popped' once and sent the screw driver into the side wall, where it was left as a reminder. Good luck, Boris N51BR ________________________________________________________________________________
Date: Jun 08, 1996
From: sarg314(at)AZStarNet.com (Tom Sargent)
Subject: Re: GPS
> >> I use the EC-10X day and night in all kinds of weather. >> > > So how is the display in direct Sunlight? > > >Fred Stucklen RV-6A N925RV >(Installing optional electric flaps) >wstucklen(at)aol.com I've got an ec10-x that I've used about 4 times now. (It was Purchased last december - I'm not sure it's EXACTLY the same model referred to above.) It works great. It has a pretty standard looking (albeit hi resolution) LCD display. Very visible in sunlight. It's backlit for night use with 4 adjustable light levels. I haven't flown with it at night (but I have tried navigating my car with it at night!). There's a few areas where I think the control scheme is a little illogical, but nothing major. I wouldn't go crosscountry without it. I'm sure GPS is regularly saving lives by keeping inexperienced pilots (like me) from getting lost and running out of gas. --- Tom Sargent, Tucson, AZ, sarg314(at)azstarnet.com ________________________________________________________________________________
Date: Jun 08, 1996
From: "Timothy W. Whitman" <71610.2013(at)CompuServe.COM>
Subject: Bottom Hole
I've just assembled the flaps to the fuse and wings of my 6A, and find a 1 inch by 1 3/4 inch gap aft of the fuse bottom skin where it overlaps the wing bottom skin. Is this normal? What covers it? Also, how far up into the side of the fuse did others need to cut to clear the rod end attached to the flap? Tim Whitman Hamilton, MA ________________________________________________________________________________
Date: Jun 08, 1996
From: martin <ember@carib-link.net>
Subject: Re: big bucks
joehine wrote: > > >REGARDING big bucks > > > >Of course you could move to Australia and "import" your quality of life - > >what's a little shipping charge anyway! > >-Elon > > > > Elon, no offence intended but some of us who live in small nations and not > the U.S. actually like it that way and consider the occasional shipping > charge worth it. > > I don't want to get a patriotic shouting match going here but that attitude > of some americans that the rest of the world is some how inferior is very > annoying. The US has its major advantages and major disadvantages just like > any other country including mine. > As a resident of an even smaller country (Trinidad)I feel that I have to join in and support ! I don't think that Americans realise just how offensive their assumption that everything American is necessarily better can be. Too many don't even know where Trinidad is ! Regards, Martin Only the young die good. ________________________________________________________________________________
Date: Jun 08, 1996
Subject: Re: Bottom Hole
From: haipilot(at)usa.pipeline.com (Hai Pilot)
I'm really sorry about the dress code crap. Lisa and Charlie have gotten onto this little critical campaign about peoples dress. Can you imagine these two deciding to be the arbitors of other peoples lives? Lisa wrote up this little Dress Code paragraph and put it in the Kol, with my approval. I figured this way she would be satisfied and let it go away. Instead they are now going around to congregants telling them that their dresses are to short, their sleeves are not long enough, the boys should be in pants not shorts, etc. You are not the first to be insulted like this recently. I guess I need to put a stop it. One thing I suggest, is for you to call the president, Leo Plotkin, who is a reasonable enough fellow, and just tell him that you are upset at this intrusion. State it just like you did to me, that you try so hard just to get them here, and that in fact their dress style is just fine, and that if this happens to you again, you are liable to lose your temper and tell these people to go to hell. Also, I understand what you are saying about feeling yuked up, trying so hard not and then looking even better than normal due to the extra effort. I do it regularly. Don't worry - nobody really fits in, and if they do, it is only for a little while. I love you so much, it feels good. ________________________________________________________________________________
Date: Jun 08, 1996
From: jcimino(at)jcimino.microserve.com (Jim Cimino)
Subject: HS FRONT SPAR QUESTION
There's been a lot of talk about hs front spars. Van's manual says to pilot drill the holes and then the drawing says that some of these holes should be drilled in the assembly with the fuselage. What is the correct method and is it OK to pilot drill all the holes. Jim Cimino RV-8 sn#80039 ________________________________________________________________________________
Date: Jun 08, 1996
From: joehine(at)mi.net (joehine)
Subject: Re: Preserving Engines
>>I have an O 320 that was reoverhauled in 1989. It has not been run since >>then. When I got it, about two years ago, I planned to have my airplane >>flying in about 18 months. ha ha. I have it mounted in a stand nose down. >> I've been turning it every few months and spraying WD40 in the spark plug >>holes. Now I realize it will be a long time before that engine ever gets >>"fired up." What should I do to preserve it until then? >> >>Doug Brabston >> I was a sun and fun a few years ago and I overheard someone asking a person on the lycoming booth the same question and the response was. "plug all the holes and fill it up with oil, everything, the cylinders, the crankcase, everything". The guy went on to say that storing it on a stand like you have was the way to store it when it was full of oil. I don't know if this is completely out to lunch, but that was the response !! Joe joehine(at)mi.net Comp. 9, Site 8, RR#4 506-452-1072 Home Fredericton, NB 506-452-3495 Work Canada, E3B 4X5 Nobody on their death bed has ever been heard to say "Geeze,I wish I'd spent more time at work" ________________________________________________________________________________
From: EBundy2620(at)aol.com
Date: Jun 08, 1996
Subject: Re: No Subject
>I'm sorry but I'm getting tired of reading some of the stuff I see being >asked. I've been in aircraft 25 years and have either built, repaired, >rebuilt aircraft by all major aircraft companies. >1. If you guys are worried about that top fuselage skin .. screw the >2. As for pro seal weaking a joint that is fillet sealed???? I don't know >where in the %^&*( that came from) but if thats true then every kerosene Harry, I can see how some of this may be boring to you but that IS what this list is for. Most of us haven't been repairing aircraft for 25 years. I don't think most of us have ever even used a pneumatic rivet gun until we started our project. To try and scare people away from asking a "stupid" question (it's only stupid to those who know the answer and forget that they didn't know it at one time) is detrimental to what this list is about: building a quality, safe aircraft. If you're tired of reading about a certain subject, you can skip past it. I have found that even subjects with which I'm familiar still hold valuable information somtimes. Cheers, Ed Bundy ebundy2620(at)aol.com ________________________________________________________________________________
Date: Jun 08, 1996
From: Rick Osgood <74774.54(at)CompuServe.COM>
Subject: RV dress code
Also, I understand what you are saying about feeling yuked up, trying so hard not and then looking even better than normal due to the extra effort. I do it regularly. Don't worry - nobody really fits in, and if they do, it is only for a little while. I love you so much, it feels good. We all love you too........ Rick in MN ________________________________________________________________________________
Date: Jun 08, 1996
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: big bucks
>> As a resident of an even smaller country (Trinidad)I feel that >I have to join in and support ! I don't think that Americans realise just >how offensive their assumption that everything American is necessarily better >can be. Too many don't even know where Trinidad is ! Making false assumptions about Americans is not associated with building and flying RV's. Let's all get back to RV's! Rob Acker (r.acker(at)ix.netcom.com) Rancho Santa Margarita, CA / RV-6Q builder / N164RA reserved ________________________________________________________________________________
Date: Jun 09, 1996
From: Dan Ahearn <ahearns(at)ix.netcom.com>
Subject: Re: big bucks
This could get ugly..... Back to RV's Dan >joehine wrote: >> >> >REGARDING big bucks >> > >> >Of course you could move to Australia and "import" your quality of life - >> >what's a little shipping charge anyway! >> >-Elon >> > >> >> Elon, no offence intended but some of us who live in small nations and not >> the U.S. actually like it that way and consider the occasional shipping >> charge worth it. >> >> I don't want to get a patriotic shouting match going here but that attitude >> of some americans that the rest of the world is some how inferior is very >> annoying. The US has its major advantages and major disadvantages just like >> any other country including mine. >> As a resident of an even smaller country (Trinidad)I feel that >I have to join in and support ! I don't think that Americans realise just >how offensive their assumption that everything American is necessarily better >can be. Too many don't even know where Trinidad is ! > > Regards, > Martin > > > Only the young die good. > > ________________________________________________________________________________
Date: Jun 08, 1996
From: Fred Hiatt <hiatt001(at)gold.tc.umn.edu>
Subject: Re: Preserving Engines
aol.com!BrabstonD(at)matronics.com wrote: > > I have an O 320 that was reoverhauled in 1989. It has not been run since > then. When I got it, about two years ago, I planned to have my airplane > flying in about 18 months. ha ha. I have it mounted in a stand nose down. > I've been turning it every few months and spraying WD40 in the spark plug > holes. Now I realize it will be a long time before that engine ever gets > "fired up." What should I do to preserve it until then? > > Doug Brabston Doug, I'm sure you will get all sorts of answers to your question, so I will add my interpretation. This is a culmination of recommendations from a lot of different sources, no guarantees included. Remove all accessories, seal them in plastic bags (heavy) with silica jell inside. Make sealing covers out of plywood and gasket material. Heat a mixture of mineral oil + 25% Marvel Mystery oil to about 150 F. Spray this in every hole you can find, accosasionaly turning the engine on the crank a few degrees. Load up the crankcase with as much of the mixture as will fit. Put silica jell plugs in all spark plug holes. Put the covers+gasket material on all accessory holes. Get about 2-4 pounds of silica jell in bags (cloth). Prepare heavy plastic sheet to enclose the entire engine. Place the silica jell bags in the plastic enclosure and seal it tightly. Make it a practice to look at the silica jell in the bags and the plugs every two weeks to see if any of it is turning pink. If, it does turn pink, remove it, bake it out in an oven till it's blue again and reseal better than you did the time before. Good luck, Fred Hiatt ________________________________________________________________________________
Date: Jun 09, 1996
From: bcos(at)ix.netcom.com (William Costello )
Subject: Preserving engines
Hi Folks, There was a question about preserving an engine that won't be used for a couple of years. Tony Bingelis in his book, Firewall Forward, has a section titled Coping with that uninstalled Engine, which runs from page 44 through page 52. He gives specific recommendations for short term, medium term, and long term storage (which he calls flyable storage, temporary storage, and indefinite storage), complete with pictures and diagrams. He gives alternatives to what I guess is the official 'pickling' where you fill it with cosmoline or something (would probably be best to get this from Lycoming). He talks about using an antirust additive to the oil called MIL-C-6529, dehydrator spark plug replacements, and silica gel bags. I think Tony's books are outstanding and, if you go to Oshkosh this summer, you can buy them and avoid the exhorbitant shipping and handling charges. Hope this helps, -- Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 Building RV-6 or 6A | Reserved N97WC ________________________________________________________________________________
Date: Jun 09, 1996
From: Harold Sutphin <hsutphin(at)magicnet.net>
Subject: Re: Fuel Flop Tube
This came up a while back, check the RV List archive or some past issues of the RVator...The large slots are preferred at that point in the fuel system. Let the next in line filter catch the stuff. The flop tube would be TOO easy to clog if it used a finer mesh or similar setup. Harold RV-6A > On Fri, 7 Jun 1996, Gene Gottschalk ((301) 286-0708) wrote: > I put one in just for the heck of it. My question is: did anyone adapt a > filter screen of some kind to the tube? The stock tube just has a 1/4" or > so hole in the end; looks like it could suck up lots of gunk into the > fuel lines. > > Curt Reimer ________________________________________________________________________________
Date: Jun 09, 1996
From: Phil Arter <arter(at)ncar.ucar.edu>
Subject: Re: HS FRONT SPAR QUESTION
Jim, I believe you are talking about the 3/16" holes for mounting the HS to the fuselage. I had already drilled them to #30 as part of the hole pattern in the spar splice channels. While I'm confident they are in the right places, I am going to wait to enlarge them to 3/16" until final assembly. There are corresponding holes in the VS that should stay totaly blank, so they can be match drilled along with whatever part they attach to in the fuselage, to the ones in the HS. I figure the ones in the HS will become the "masters". It is a bit of a handicap for us RV-8 builders not having a set of preview plans so we know what the rest of the airplane looks like. Phil (#80005 working on VS) arter(at)ncar.ucar.edu >There's been a lot of talk about hs front spars. Van's manual says to pilot >drill the holes and then the drawing says that some of these holes should be >drilled in the assembly with the fuselage. What is the correct method and >is it OK to pilot drill all the holes. > >Jim Cimino >RV-8 sn#80039 > > > ________________________________________________________________________________
From: Rvbildr(at)aol.com
Date: Jun 09, 1996
Subject: Re: RV dress code
We can't see you here on the RV list so don't sweat it! ________________________________________________________________________________
Date: Jun 09, 1996
From: Betty Blanton <75472.372(at)CompuServe.COM>
Subject: Strobe Power Supply
RV-List, Has anyone mounted their strobe power supply under the baggage floor on an RV-6? If so what did you use for a mount, etc.? I'm thinking of putting mine, a standard Whelen, under the baggage floor directly behind the F-605 bulkhead and using nutplates on that section of flooring. Thanks, Stan Blanton 75472.372@compuserve RV-6 fuselage skeleton ________________________________________________________________________________
From: OrndorffG(at)aol.com
Date: Jun 09, 1996
Subject: Re: Ormdorff Addr
To get to George and Becki use "orndorffg(at)aol.com" ________________________________________________________________________________
From: SportAV8R(at)aol.com
Date: Jun 09, 1996
Subject: Re: RV-6/8 Will I be comfortable?
Bob S: I'm at the point of having to decide on upholstery options for my 6A. I've heard George Orndorf say the temperfoam takes too long to soften comfortably on cold days and to use high-density polyfoam from a fabric store. What's been your experience? What about the rest of the gang- what are you sitting on and how do you like it? Bill Boyd SportAV8R(at)aol.com ________________________________________________________________________________
From: SportAV8R(at)aol.com
Date: Jun 09, 1996
Subject: Re: Strobe Power Supply
The ps will likely fit under the baggage floor, but unless you have a heavy engine/prop/accessory combination, you might want to consider as forward a location as you can get to preserve cg range. I have nut-plated my whelen supply to the firewall on the pax side in the upper triangle section formed by the stiffeners. I hope it will not prove to be in the way of anything. If it is, I will move it later. Everyone tells me the 6A suffers from a tendency toward tail-heaviness. With electric trim and a tail position light and vertical stab strobe head already installed on mine, I didn't want to take the chance. At the rate I'm trudging through the instrument panel design/layout process, it will be a long time before I find out how the cg came out! Waiting for finishing kit, which will probably arrive before I'm ready for it... Bill Boyd western VA ________________________________________________________________________________
Date: Jun 09, 1996
From: billphil(at)ix.netcom.com (William Phillips )
Subject: Re: Fwd: Re: Small Talk From the OMABP (long)
Another week went by at the Old Mens Airplane Building Project. Its so hot here now that even with an evaporative cooler in the hangar we still cant work past about noon. It was 106 yesterday. We are going to have to scrap the Carter 4 barrel carburetor. It just wont tune. Weve ordered a Holly 2-barrel 500 cfm and the leaning kit for it too. In spite of that we did fly 3 times this week and even this morning. For those of you who like number crunching the takeoff roll 0 to 70 mph was just a tad under 9 seconds with a gross weight of 1450lb. We climbed to 3500 msl from 2000 and ran racetrack patterns over the airport for 25 minutes. The coolant temperature began to climb past 210 F so we backed off power from 23 inches to 17. It stabilized but didnt come down. We were always able to attain a temperature split of about 20 degrees between engine and radiator output. At the hangar we pulled and read the plugs. The outer cylinders were running leaner than the middle ones,as usual, but they were too lean. Without boring everyone, by going into the minute details of this carburetor I will just have to say that its highly modified at this point and the metering rods on the primary jets we too lean when running at 17 inches of manifold pressure. With the springs were running they dont transition to the richer setting until 19 inches. The secondary barrels are set up richer but never kicked in at the low manifold pressure. So we ran the engine too lean. You might ask why the EGT didnt show it. Well its broken and weve ordered a new one but like everything else at the OMABP its slow in coming. And like a bunch of kids, we wanted to fly our toy airplane. The airplane itself is a dream to fly. Weve had it up to 170 mph for stability testing and its as straight as a lawn dart. Weve tried full control deflections at various speeds and looked for any signs of flutter but see none. Today we indicated 70 mph on approach with 20 degrees of flaps, touched down at about 60 and the nose came through at about 55. Jess was flying and did a perfect job as usual. I mounted a Sony Hi-8 video camera in the baggage compartment and recorded all the temperatures, fuel flow/pressure, oil temp/pressure, voltage and all the flight data. It was just more routine than anything. Just puttin a little time on the system. This week well change carburetors and get the EGT going again. And, we need to rework some baffling under the cowling to move more air through the radiator. Maybe by next weekend I can pass on some positive data on speeds and rates of climb. Best Wishes to all and have a good WeekBill Phillips ________________________________________________________________________________
From: "David Drew" <noeldrew(at)iafrica.com>
Date: Jun 09, 1996
Subject: Re: Jon Johansen
I have been informed that Jon Johansen is expected in Durban, South Africa late in June and I look forward to meeting and helping him when he passes through. I believe he is planning a route from Perth Australia via the Cocos Islands with an awful lot of Indian Ocean between there and Durban. If any of the Australian listers can provide more details I would appreciate them. I have the only RV flying in South Africa which is a RV6 first flown in May last year with an 0-320 D2A and the Sensenich metal prop. It is inspiration for the dozen other builders and envy of all others pilots. 75 hours and no problems from day one. Thanks Van. Noel Drew noeldrew(at)iafrica.com ________________________________________________________________________________
From: frankv(at)pec.co.nz
Date: Jun 10, 1996
Subject: Re: RV-6/8 Will I be comfortable?
>>I am 6' 3" tall, 175 lbs, 34" pants inseam. I tried on the factory >>2. Can I get adequate headroom in the RV-6 with thinner cushions, >>etc, and still have a comfortable seat? >I don't know if you have experienced this, but sometimes when I am >trying a car on for size, I may fit but its a little tight (head >brushing headliner, etc.). After fifteen minutes of driving I forget >all about that. I seem to "stretch" when trying something on for >size, then go into more relaxed mode when I forget about trying to >fit in it. I'm 6'1", and had a ride in a -6 a few months ago. It had been built by a short guy for himself & his wife. I found that my head was hitting the canopy unless I sat in a slightly contorted position. An important point I'll make is that you should wear a headset when you're trying a plane out for size. My $0.02 worth. Frank. -- -------------------------------------------------------------------- frankv(at)pec.co.nz | "Knowledge=Power=Energy=Matter=Mass; Frank van der Hulst | A good bookshop is just a genteel Software Engineer | Black Hole that knows how to read". PEC(NZ) Ltd (Cardax), Marton | Terry Pratchett, "Guards! Guards!" http://www.pec.co.nz/~frankv/ | -------------------------------------------------------------------- ________________________________________________________________________________
Date: Jun 09, 1996
From: bcos(at)ix.netcom.com (William Costello )
Subject: Boone Fly-in Question
Hi Folks, Well, I couldn't make the Boone IA fly-in yesterday. We at Chapter 260 here in Lansing (near Chicago) had our pancake breakfast today. Had a good turnout for the way it was -- about a 300 ft ceiling in fog all day and, of course, not a plane flying. Dick Gross had his RV-6 there for Young Eagle flights, but no dice. It was fun to see the look on Dick's face when a young guy demonstrating a radio control helicopter inverted it and flew about 30 ft over Dick's plane on the ramp! My heart skipped a beat and I find it amazing we didn't have to administer CPR to Dick. I would very much appreciate a report of the Boone fly-in and especially anything new and exciting. If you don't think it is appropriate for the list, please send it to me privately. All responses welcome. Best regards, -- Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 Building RV-6 or 6A | Reserved N97WC ________________________________________________________________________________
Date: Jun 09, 1996
From: rdunn(at)ionet.net (Ron Dunn)
Subject: Re: HS FRONT SPAR QUESTION
>There's been a lot of talk about hs front spars. Van's manual says to pilot >drill the holes and then the drawing says that some of these holes should be >drilled in the assembly with the fuselage. What is the correct method and >is it OK to pilot drill all the holes. > >Jim Cimino >RV-8 sn#80039 > > Jim, I called Van's on that issue, after I had pilot drilled the holes. Ken Scott told me that there was no problem as the 3/16 assembly holes would correct any uncentered holes. I also put that question on the net a couple of weeks ago. All respondents (private) assured me that it was OK. I just finished driving the 120 #4 rivets in the rear spar last night! Good luck, Ron Ron Dunn #80078 RV-8 > HS in jig Broken Arrow, OK ________________________________________________________________________________
Date: Jun 09, 1996
From: john henley <j.henley(at)worldnet.att.net>
Subject: Bulkhead cutouts for J-channels
In attempting to fit the J-channels on the fuselage bulkheads, I find that some of the cutouts are such that the channels fit in ok, but others are missing the enlarged part of the cutout that allow the "curl on the bottom of the J" to fit. I either have to notch the channel or enlarge the cutout in the bulkheads. I can't find this addressed by Vans or Justice. I figure I am supposed to enlarge the bulkhead cutouts but then I am doubtful because why wouldn't Vans make them all the same unless the channels are supposed to be notched? Any help will be appreciated. John Henley, RV6 ________________________________________________________________________________
Date: Jun 09, 1996
From: Jack Haviland <jgh(at)iavbbs.com>
Subject: Michigan Wing FlyIn
The Michigan Wing of Van's Air Force will meet at Dalton Airport (about 10 miles NW of Flint International) on Sunday June 23, 1996 at noon. Lunch is a "bring a dish to pass" potluck. Their are numerous experimental category planes (including an outstanding RV-6) based at the field and anyone interested is invited. http://members.tripod.com/~6Alady/rvmi.html includes a map for those who elect to drive. Please feel free to send an email directly to us if you need more information. Jack & Katy Haviland ________________________________________________________________________________
Date: Jun 09, 1996
From: bcos(at)ix.netcom.com (William Costello )
Subject: Re: RV-6/8 Will I be comfortable?
Hi Folks, Regarding the personal height capability of the RV-6, I don't think the guys at the factory are giving you a snow job when they say you have the ability to build the seats so that you will fit very nicely if you are up to about 6' 4". I am just under 6' 3" with relatively short legs (about 21" inseam), so a lot of my height is in my back. I fit very comfortably in Dick Gross' RV-6, complete with a headset. He has the tilt-up canopy. I have heard that the new sliding canopy has even more head room potential. So I suspect the bottom line is, if you are 6' 3" or under, you can build either a -6 or an -8 so that you will be comfortable. For me, if my wife expressed a preference for the -6, that would really lean my in that direction. (Which she has; I am building the -6, but I prefer it to the -4 or -8 anyway.) But different strokes for different folks. Best regards, -- Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 Building RV-6 or 6A | Reserved N97WC ________________________________________________________________________________
Subject: Re: HS FRONT SPAR QUESTION
Date: Jun 09, 1996
From: Mike Kukulski <kukulski(at)indirect.com>
Previously written: >There's been a lot of talk about hs front spars. Van's manual says to pilot >drill the holes and then the drawing says that some of these holes should be >drilled in the assembly with the fuselage. What is the correct method and >is it OK to pilot drill all the holes. I can't speak for a RV-6 or RV-8 as I haven't seen their plans, but in the RV-4, the four holes for the bolts that attached the rear spar to the fuselage were pilot drilled on my airplane, and then matchdrilled to final size in assembly. If these are the holes in question, then follow Van's instructions - pilot drill them when building the stab and drill them to final size in assembly!! Mike Kukulski (kukulski(at)indorect.com) RV-4 N96MK (left wing flaps links, root fairings, etc.) ________________________________________________________________________________
Subject: My Dad Can Beat Up Your Dad
Date: Jun 09, 1996
From: Mike Kukulski <kukulski(at)indirect.com>
Let's knock this off. It's the "RV-List", remember?!! Talk backroom politics elsewhere. Recent thread: >>Of course you could move to Australia and "import" your quality of life - >> >what's a little shipping charge anyway! >> >-Elon >> > >> >> Elon, no offence intended but some of us who live in small nations and not >> the U.S. actually like it that way and consider the occasional shipping >> charge worth it. >> >> I don't want to get a patriotic shouting match going here but that attitude >> of some americans that the rest of the world is some how inferior is very >> annoying. The US has its major advantages and major disadvantages just like >> any other country including mine. >> As a resident of an even smaller country (Trinidad)I feel that >I have to join in and support ! I don't think that Americans realise >just >how offensive their assumption that everything American is necessarily >better >can be. Too many don't even know where Trinidad is ! Mike Kukulski (kukulski(at)indirect.com) RV-4 N96MK ________________________________________________________________________________
Date: Jun 09, 1996
From: Greg Puckett <71155.2336(at)CompuServe.COM>
Rod Woodard
Subject: HS Skin Rivet Selection
Hello everyone, I am now getting ready to skin the top side of the HS of my RV-8 and I have a couple concerns. First, the rivet the plans call for is an AN426AD3-3.5, using that rivet the protruding shank length beyond the dimple is .133" (about .010 shy of the minimun 1.5*D to get a good shop head) I'm sure I'll just use the -4 rivets and hope I dont bent over too many. Are they maybe thinking that you are going to countersink the skin and not dimple as the instructions say? Second, I dimpled the skin with cleaveland dies and a C-frame tool and many of the rivets don't set 100% flush, I plan on just countersinking slightly those holes to get a flush rivet, Does anyone see a problem with that? I know it all kind-of sounds picky but I really dont want to screw this thing up at this point. Nervous in Colorado, Greg Puckett RV-8 80081 71155.2336(at)compuserve.com ________________________________________________________________________________
Date: Jun 09, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: RV-6/8 Will I be comfortable?
>Bob S: I'm at the point of having to decide on upholstery options for my 6A. > I've heard George Orndorf say the temperfoam takes too long to soften >comfortably on cold days and to use high-density polyfoam from a fabric >store. What's been your experience? What about the rest of the gang- what >are you sitting on and how do you like it? > >Bill Boyd >SportAV8R(at)aol.com Bill, Yes, I agree with George. I flew the 40 hours off my six in March of 95 and it was cold. After 5-6 hours, my rear was sore. I flew with the 3 layer Temperfoam in a pillow case so there was not much material to lessen heat transfer. Temperfoam needs some heat to conform and I don't think the bottom layer (most dense) could ever be affected. (I think this material is made of old concrete park benches) I solved the comfort problem by putting a 1 inch layer of medium density, generic foam over the Temperfoam. I put a 1 inch layer of the same material over the 1 inch of Sunmate that I used for the seat back. I had the opportunity to talk with Jim Fix, Lincoln, NE prop guru and Temperfoam/Sunmate dealer a few days ago when he re-pitched my Sensenich prop for me. I relayed the above opinion to him and told him that I was thinking of using less dense Temperfoam or Sunmate for the seat cushions on my next RV. He was surprised about my comments on lack of comfort but discouraged the idea of usiing any foam other than the three layer Temperfoam. His basis for this was mainly from a safety standpoint as he had knowledge of mishaps where the surviviors of high G crashes credited the Temperfoam for saving their lives. I really feel that he was sincere in his beliefs and was not telling me this just to sell Temperfoam. In other words, I don't believe money would motivate him to tell anything but the truth. I haven't checked Jim's current prices, but I'd bet that his prices are better than Aircraft Spruce. After talking to Jim, I'll probably use the Temperfoam in the next RV. By the way, I just got back from the Boone RV fly-in and saw a lot of DJ's seats. They are nice but are quite pricey. I'd sure look in to George and Becki's options for seats. I had mine done at a local car/boat/plane upholsetery shop. I supplied the two 3-layer Temperfoam seat cushions and two one inch Sunmate seat backs and the shop supplied the one inch generic, medium density foam and the covering. They charged me a total of $165.00. This included two black vinyl stick booties as well. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 09, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Strobe Power Supply
>Has anyone mounted their strobe power supply under the baggage floor on an RV-6? >If so what did you use for a mount, etc.? >I'm thinking of putting mine, a standard Whelen, under the baggage floor >directly behind the F-605 bulkhead and using nutplates on that section of >flooring. > >Thanks, >Stan Blanton Stan, If you're not using a constant speed, you might want to consider mounting the power supply farther forward, maybe on the firewall. I mounted my single power supply for the vert. stab. single strobe behind the baggage compartment. This was a mistake as I needed more weight forward. I was planning on doing this on the six I'm building now. I'd be interested in hearing from other builders who used the single unit in the cockpit that are firing wing tip strobes. Any radio interference problems? Did you use shielded wire out to the strobes? How about wire routing? Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 09, 1996
From: jcimino(at)jcimino.microserve.com (Jim Cimino)
Subject: HS-802 question
Anyone else building an RV-8 have HS-602 instead of HS-802. The plans and manuals call for HS-802 and Van's sent HS-602's. Is this correct. I assume it is. Jim Cimino RV-8 sn#80039 working on HS front spar. ________________________________________________________________________________
Date: Jun 09, 1996
From: Pat McClung <pmc123(at)airmail.net>
Subject: Re: RV-6/8 Will I be comfortable?
aol.com!SportAV8R(at)matronics.com wrote: > > Bob S: I'm at the point of having to decide on upholstery options for my 6A. > I've heard George Orndorf say the temperfoam takes too long to soften > comfortably on cold days and to use high-density polyfoam from a fabric > store. What's been your experience? What about the rest of the gang- what > are you sitting on and how do you like it? > > Bill Boyd > SportAV8R(at)aol.com I have seats from DJ Lauritson with temperfoam and both ends smile when I sit down, either hot or cold weather!!! I have temperfoam in a open cockpit biplane also--IT IS WORTH TWICE THE MONEY IT COSTS. Just plan on an hour and numbness sets in with the cheap stuff. 4 to 5 hrs still comfortable on temperfoam-- That has been MY experience---Now let's see the screen lite up with the usual dissenters out there---always a minority voice isn't there(and usually loud). ________________________________________________________________________________
From: Michael Angiulo <mikeang(at)MICROSOFT.com>
Subject: HS Skin Rivet Selection
Date: Jun 09, 1996
I bought a whole bag of "4" length rivets because the dimpled skin/ribs are too thick for 3.5's as you found out. None bent over in riveting. As for countersinking the holes - bad idea I think to countersink a dimpled hole. You don't want to weaken these joints for some minimal cosmetic gain. Besides during the flush riveting I found that the heads formed slightly or the hole gave slightly as the finished result is far smoother than it was when I just put the rivet in the hole and felt across the surface. -Mike ---------- From: Greg Puckett[SMTP:CompuServe.COM!71155.2336(at)matronics.com] Sent: Sunday, June 09, 1996 4:23 PM Subject: RV-List: HS Skin Rivet Selection Hello everyone, I am now getting ready to skin the top side of the HS of my RV-8 and I have a couple concerns. First, the rivet the plans call for is an AN426AD3-3.5, using that rivet the protruding shank length beyond the dimple is .133" (about .01 0 shy of the minimun 1.5*D to get a good shop head) I'm sure I'll just use the -4 rivets and hope I dont bent over too many. Are they maybe thinking that you are going to countersink the skin and not dimple as the instructions say? Second, I dimpled the skin with cleaveland dies and a C-frame tool and many of the rivets don't set 100% flush, I plan on just countersinking slightly those holes to get a flush rivet, Does anyone see a problem with that? I know it all kind-of sounds picky but I really dont want to screw this thing up at this point. Nervous in Colorado, Greg Puckett RV-8 80081 71155.2336(at)compuserve.com ________________________________________________________________________________
From: Michael Angiulo <mikeang(at)MICROSOFT.com>
Subject: HS-802 question
Date: Jun 09, 1996
Absolutely correct. They're the same part. ---------- From: jcimino.microserve.com!jcimino(at)matronics.com[SMTP:jcimino.microserve.com!jcimino(at)matronics.com] Sent: Sunday, June 09, 1996 5:18 PM Subject: RV-List: HS-802 question Anyone else building an RV-8 have HS-602 instead of HS-802. The plans and manuals call for HS-802 and Van's sent HS-602's. Is this correct. I assume it is. Jim Cimino RV-8 sn#80039 working on HS front spar. ________________________________________________________________________________
Date: Jun 09, 1996
From: chester razer <crazer(at)egyptian.net>
Subject: Re: Bulkhead cutouts for J-channels
John, been there done that. Either modify the bulkhead or notch the channel or both. Don't know that it matters. Important thing is that the channel fits with little to no rubbing chet razer: riveting fuse skins ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 09, 1996
Subject: Re: Strobe Power Supply
I'd be interested in >hearing from other builders who used the single unit in the cockpit that are >firing wing tip strobes. Any radio interference problems? Did you use >shielded wire out to the strobes? How about wire routing? >Bob Skinner RV-6 BSkinner(at)ltec.net > Bob: I have the power supply in the baggage area of my 4 firing tip and tail strobes. The cables were the supplied ones from whelan and were grounded at the power pack. I did go thru terminal blocks inside the fuselage at the wing roots. I have no strobe noise in the radios. Regards: Rusty Gossard N47RG RV-4 Flying ________________________________________________________________________________
Date: Jun 09, 1996
From: Phil Arter <arter(at)ncar.ucar.edu>
Subject: Re: HS-802 question
Jim, Somewhere on the drawing it explains that by reworking the HS-602s, they become HS-802s. Phil >Anyone else building an RV-8 have HS-602 instead of HS-802. The plans and >manuals call for HS-802 and Van's sent HS-602's. Is this correct. I assume >it is. > >Jim Cimino >RV-8 sn#80039 >working on HS front spar. > > > ________________________________________________________________________________
Date: Jun 09, 1996
From: Rick Osgood <74774.54(at)CompuServe.COM>
Subject: RV6A wing ribs
I am looking for the correct spacing of rivets on the first four ribs on the 6A. I noted from George O's tape that the spacing is different but I can not locate it on the drawings. This would be front and rear spar attach points. Thanks to all. Rick 74774.54@compuserve,com ________________________________________________________________________________
Date: Jun 09, 1996
From: Ted French <french(at)computime.bc.ca>
Subject: Re: Strobe Power Supply
Bob Skinner wrote: > > >Has anyone mounted their strobe power supply under the baggage floor on an > RV-6? > >If so what did you use for a mount, etc.? > >I'm thinking of putting mine, a standard Whelen, under the baggage floor > >directly behind the F-605 bulkhead and using nutplates on that section of > >flooring. > > > >Thanks, > >Stan Blanton > > Stan, If you're not using a constant speed, you might want to consider > mounting the power supply farther forward, maybe on the firewall. I mounted > my single power supply for the vert. stab. single strobe behind the baggage > compartment. This was a mistake as I needed more weight forward. I was > planning on doing this on the six I'm building now. I'd be interested in > hearing from other builders who used the single unit in the cockpit that are > firing wing tip strobes. Any radio interference problems? Did you use > shielded wire out to the strobes? How about wire routing? > Bob Skinner RV-6 BSkinner(at)ltec.net Bob I installed the Wheelan power supply with the wingtip strobes (The comet-flash, I think its called) I have had no interference at all with my comm. I used shielded wire for the runs to the wingtips. My 6A is done and I'm just in the process of taxi testing. First flight should by Tues or Wed. Ted French RV-6A C-FXCS ________________________________________________________________________________
Date: Jun 09, 1996
From: blfogerty <bfogerty(at)ionet.net>
Subject: RV list addition
Please add my name to the RV Internet list, as above. I am 25% through on a RV6A, and need all the info and encouragement I can get. Thanks, Barry Fogerty ________________________________________________________________________________
From: JamesCone(at)aol.com
Date: Jun 09, 1996
Subject: Re: Top fwd fuse skin
You write: I'm a long way from this part, but it occurs to me that it might be worth replacing the rivets with screws, so that access to instruments for maintenance is less of a chore. Or would the hassles of preventing leaks and/or fixing instruments damaged by leaks be greater than the hassle of occasionally crawling under the dash? -- There are too many screws to do it this way. Just make the instrument panel removable and that will help a lot if you have to work on things behind the panel. Jim Cone jamescone(at)aol.com ________________________________________________________________________________
Date: Jun 09, 1996
From: kightdm(at)carol.net (Danny Kight)
Subject: Re: Greenville, SC Young Eagles
Bill Costello wrote: >Well, I couldn't make the Boone IA fly-in yesterday. We at Chapter 260 >here in Lansing (near Chicago) had our pancake breakfast today. Had a >good turnout for the way it was -- about a 300 ft ceiling in fog all >day and, of course, not a plane flying. Bill, Sorry to hear about your bad weather yesterday. You can celebrate vicariously with me on our FANTASTIC Young Eagles rally yesterday in Greenville, SC. We don't have a final count on the kids flown yet, but we think it is just over 400! (We stopped counting after about 300). We had 17 aircraft flying, including a Lake amphibian, Jetranger helicopter, Beech Baron, a Husky, Thorp T-18, and lots of 172s, 182s, and misc. Pipers. (Alas, no RVs. Sigh...) The line to get on the planes usually lasted about 2 hours, and people stayed in line even during a few short showers. Last year, we only had about 50 Young Eagles. Why the 8-fold increase? A couple of reasons: This year we had the Confederate Airforce's B-29, B-24, and B-25 on display throughout the week. The local media gave this a fair amount of attention, and we used this to our advantage. We also got the newspapers excited about the Young Eagles program, and they interviewed several of the pilots in our chapter, in addition to spreading the word of "free airplane rides on Saturday". My Sonerai was down for maintenance, so I ran the ground school instead of flying. My voice is hoarse from talking to hundreds of kids and their parents about the wonderful world of sport aviation and how they can be a part of it. Man, what a day!! Danny Kight kightdm(at)carol.net EAA Chapter 249 V.P. & Young Eagle Coordinator Sonerai IILT -flying RV-6 empennage done, hope to hang a wing spar in the jig in a couple of weeks! ________________________________________________________________________________
Date: Jun 09, 1996
From: barnhart(at)a.crl.com (Dave Barnhart)
Subject: Re: Strobe Power Supply
>Has anyone mounted their strobe power supply under the baggage floor on an >RV-6? >If so what did you use for a mount, etc.? >I'm thinking of putting mine, a standard Whelen, under the baggage floor >directly behind the F-605 bulkhead and using nutplates on that section of >flooring. Just a couple of days ago, I was laying on my back under my fuselage jig, starting to think about wiring. I too am probably going to put the Whelen supplu under the baggage floor right behing F605. I'll probably actually mount it to the belly skin rather than the bottom side of the floor. I'll rivet a doubler in place, drill four holes, and snap some tinnermans over the mounting holes in the Whelen supply. I think this is a good location for three reasons: 1. All the wiring to the strobes is behind the spar, so why try to route three big cables past the spar. Instead, with the power supplu under the baggage floor, all that needs to get routed is power and ground. 2. Some strobe power supplies make noise (not the RF kind, the kind of noise you can hear). putting the supply under the floor will help deaden the noise if it exists. 3. I'm trying to keep the strobe wiring isolated as much as possible from the Comm wiring. Best Regards, Dave Barnhart fuselage ready to rivet switching to IO320 overhaul mode ________________________________________________________________________________
Date: Jun 09, 1996
From: barnhart(at)a.crl.com (Dave Barnhart)
Subject: Re: Bulkhead cutouts for J-channels
John Henley wrote: >In attempting to fit the J-channels on the fuselage bulkheads, I find that >some of the cutouts are such that the channels fit in ok, but others are >missing the enlarged part of the cutout that allow the "curl on the bottom >of the J" to fit. Notch the bulkheads to fit the J-channels. The other thing to watch out for is that the bottom-most (top-most in the jig) j-channels may not fit far enough outboard to meet at the intersection of the bottom skin and the side skins. Be sure to trial-fit your skins before drilling the bottom j-channels to the bulkheads. Best Regards, Dave Barnhart rv-6 sn 23744 ready to rivet fuselage skins but switching to io320 overhaul mode ________________________________________________________________________________
Date: Jun 09, 1996
From: ammeterj(at)seanet.com (John Ammeter)
Subject: Re: RV-6/8 Will I be comfortable?
>Hi Folks, > >Regarding the personal height capability of the RV-6, I don't think the >guys at the factory are giving you a snow job when they say you have >the ability to build the seats so that you will fit very nicely if you >are up to about 6' 4". I am just under 6' 3" with relatively short >legs (about 21" inseam), so a lot of my height is in my back. I fit >very comfortably in Dick Gross' RV-6, complete with a headset. He has >the tilt-up canopy. I have heard that the new sliding canopy has even >more head room potential. > >Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 >Building RV-6 or 6A | Reserved N97WC > > Bill, Are you SURE that your inseam is 21"?? I thought I had a long torso at 5'11" and an inseam of 29". Must be difficult to find pants off the rack. John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA RV-6 N16JA Flying 5 years ________________________________________________________________________________
From: LWFL69A(at)prodigy.com ( MICHAEL T PIA)
Date: Jun 09, 1996
Subject: Message from Ralph
Ralph, Karl told me you had an account again. Welcome back. Tuesday and Wednesday are no good so maybe either Monday or Thursday. Call me tommorow night and we'll see whats going on. Mike ________________________________________________________________________________
Date: Jun 10, 1996
From: Royce Craven <roycec(at)ozemail.com.au>
Subject: Engines
I have just heard a rumor that Lycoming has developed an electronic ignition. Anyone know anything about this?? Any detail of the system and the cost? Royce Craven Melbourne Oz roycec(at)ozemail.com.au ________________________________________________________________________________
Date: Jun 10, 1996
From: boatright thomas reginald <trboatri(at)ux1.cso.uiuc.edu>
Subject: RV:list, airplane financing
hello all, I have been a lister since the begining. Mostly I just read the posts and learn. I am currently building an RV-4 (tail, wings, are done); fuselage is begun. I am planning on buying a Pitts S2-B as trainer & time builder untill I get the RV-4 done. Does anyone have any info as to the best place to seek financing in such an endevor? Thanks to all in advance Thomas R. Boatright trboatri(at)ux1.cso.edu.uiuc ________________________________________________________________________________
From: TMRV6(at)aol.com
Date: Jun 10, 1996
Subject: Re: Strobe Power Supply
(Bob Skinner) writes: >.I would like to hear from people that mounted their power pack on the firewall w/wingtip strobes. I have my power pack mounted to the firewall (high & left of center). Strobe wires are Whelen shielded running behind and under the battery box. I built a channel (cover) for wires that I ran next to the center left floor stiffener. Wires then proceed up and over the main spar into conduits that empty into the seat ribs, then through grommets into the wing. Yeah I know, strobe wires close to fuel lines..... All wires in this area double protected with plastic spiral wrap. (same type of wrap used in protecting fiber optic cable). I have no strobe noise in my com. Just turned 50 hours on the tach. First flight was on March 10, 1996. I hope this helps a little.. Todd ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 10, 1996
Subject: Re: Strobe Power Supply
SNIP>>>>>>> >2. Some strobe power supplies make noise (not the RF kind, the kind of >noise you can hear). putting the supply under the floor will help deaden >the noise if it exists. > >Best Regards, >Dave Barnhart >fuselage ready to rivet >switching to IO320 overhaul mode Dave: I don't think you will hear the power pack whine unless you shut the engine down and listen real hard.:) Regards: Rusty Gossard N47RG RV-4 Flying ________________________________________________________________________________
From: WStucklen(at)aol.com
Date: Jun 10, 1996
Subject: Re: Electric Flaps
<< 'm about to order the fuse and am trying to decide whether or not to order the electric flap. I'm curious - after 700 hours, what prompted you to go to the electric flap?? >> Over the last 700+ Hrs of flying my RV-6A, I've found it most uncomfortable to pull up the flap handle. I'm not the narrowest guy around (223 Lbs) and with another guy of similar width in the right seat, somebody has to move their arm in order for the flap handle to be lifted. And at an overall hieght of 5'11", the flap handle needed to be lifted almost to my armpit for full flaps. Couple that with an airspeed between 80-100 Mph, and that flap handle is a handful to pull. The electric flaps have solved all those problems. Flew it for the first time last Friday with no noticeble trim problems. Also tested them at 40 degrees, 100Mph just to be sure everything would work OK. Sure is a lot easier toggling that switch! In my RV-6A, I've tried to avoid running the strobe wires along side of radio antenna wires. Only the tail strobe shielded wire runs next to a Comm antenna wire, and I've not seen or heard any strobe power supply related noises in that radio....... Fred Stucklen RV-6A N925RV wstucklen(at)aol.com ________________________________________________________________________________
Date: Jun 10, 1996
From: bcos(at)ix.netcom.com (William Costello )
Subject: Re: RV-6/8 Will I be comfortable?
You wrote: > > >Bill, > >Are you SURE that your inseam is 21"?? I thought I had a long torso at >5'11" and an inseam of 29". Must be difficult to find pants off the rack. > >John Ammeter >ammeterj(at)seanet.com >3233 NE 95th St >Seattle WA, 98115 USA >RV-6 N16JA >Flying 5 years > > Oops! Glad I fly better than I type. Make that 31". Sorry 'bout that! Bill -- Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 Building RV-6 or 6A | Reserved N97WC ________________________________________________________________________________
Date: Jun 10, 1996
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: RV list addition
>Please add my name to the RV Internet list, as above. I am 25% through on a >RV6A, and need all the info and encouragement I can get. > >Thanks, >Barry Fogerty > > Barry, You need to send e-mail to rv-list-request(at)matronics.com, and include the word SUBSCRIBE in the message body. Rob Acker (r.acker(at)ix.netcom.com) Rancho Santa Margarita, CA / RV-6Q / N164RA reserved ________________________________________________________________________________
Date: Jun 10, 1996
From: RELOSVCS!WESTREG!EHENSON(at)cldwell.attmail.com (Henson, Eric)
Subject: Re: big bucks
THANKS ROB, you said it much more tactfully than I might have. (as the gung-ho jar-head puts his bayonet back in his scabert) Where in the plans does it talk about Americas shortcomings? (Sorry could'nt resist) Eric Henson Dana Point, CA >>>>>>>>>>>>>>>>>>>>>> Reply Seperator <<<<<<<<<<<<<<<<<<<<<<<<<<<<< Making false assumptions about Americans is not associated with building and flying RV's. Let's all get back to RV's! Rob Acker (r.acker(at)ix.netcom.com) Rancho Santa Margarita, CA / RV-6Q builder / N164RA reserved ________________________________________________________________________________
Date: Jun 10, 1996
From: csanchez(at)BayNetworks.com (Cheryl Sanchez)
Subject: Re:
>To all >I'm sorry but I'm getting tired of reading some of the stuff I see being >asked. I've been in aircraft 25 years and have either built, repaired, >rebuilt aircraft by all major aircraft companies. >SNIP>>>>>>>>> >later Harry Paine >HPair(at)ix.netcom.com > Now I consider myself to be reasonably intelligent and reasonably educated. I have a degree in electrical engineering and I've studied bio- chemistry, Russian and some medicine. I have a private pilot's license and an instrument rating. But when I started out building all I knew about building an airplane was that I was in love with the idea and had to give it a try. At the beginning, I had trouble drilling holes in my practices pieces of aluminum because I didn't know you had to punch the metal. Now? I can tell you all about priming, air compressors, dimpling vs. machine countersinking, fiberglassing, wiring, how the manifold pressure line works, etc. While that knowledge came from a number of sources, much of it came from this list. The recent comments from people about avionics and gps units has been very helpfull to me as I am about to buy. I am grateful that I live in a country where it is legal and affordable to build an airplane. I also hope the stupid politicians don't screw up the valuable resource that the internet is. So let's keep the info flowing. Cheryl Sanchez csanchez(at)world.std.com ________________________________________________________________________________
Date: Jun 10, 1996
From: Frank K Justice <Frank_K_Justice(at)ccm.ssd.intel.com>
Subject: Re: Bulkhead cutouts for J-channels
Text item: >In attempting to fit the J-channels on the fuselage bulkheads, I find that >some of the cutouts are such that the channels fit in ok, but others are >missing the enlarged part of the cutout that allow the "curl on the bottom >of the J" to fit. >I either have to notch the channel or enlarge the cutout in the bulkheads. I >can't find this addressed by Vans or Justice. I figure I am supposed to >enlarge the bulkhead cutouts but then I am doubtful because why wouldn't >Vans make them all the same unless the channels are supposed to be notched? >Any help will be appreciated. Sorry about that. Enlarge the slot in the bulkhead to accomodate the curl in the J-channel. FKJ Text item: External Message Header The following mail header is for administrative use and may be ignored unless there are problems. ***IF THERE ARE PROBLEMS SAVE THESE HEADERS***. Subject: RV-List: Bulkhead cutouts for J-channels From: john henley <worldnet.att.net!j.henley(at)matronics.com> Date: Sun, 9 Jun 1996 22:20:08 GMT 4.1) (8.7.4/8.7.3) with SMTP id QAA03768 for ; Sun ________________________________________________________________________________
Date: Jun 10, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Fuel Flop Tube
> > That's my opinion as well. It doesn't cost much, it's easy to do while in > > construction, and say, it make an otherwise boring 2nd tank construction > > more interesting. Also gives you the opportunity to make as yet unmade > > mistakes and improves Van's economy! I chose NOT to put a flop tube in for the following reasons: - It doesn't do you much good without fuel injection and inverted oil. I don't plan on ever doing those, so why bother? - More complexity = more potential failure points - Less accurate fuel readings -- the fuel sender goes in a different bay, or has to be some other kind of sender (e.g. more complexity, cost, etc.) - More work/expense/weight. - Those tanks were a pain in the a** as it was. I'm not saying other people shouldn't put one in if they feel it's right for them, just offering "food for thought" for people who might be on the fence about it. In my case, the "might as well, just in case" equation just didn't add up. Randall Henderson randall(at)edt.com RV-6 ________________________________________________________________________________
Date: Jun 10, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: User Fees, Thank You Randall
Dan: You're welcome. I know how easy it is to just sit on your butt and hope "the other guy" will do something, I've done it myself too many times. But I know if we end up with user fees and I DIDN'T write my letter -- well, I'd sure wish I had. I wish AOPA would start collecting e-mail addresses so they could send these "alerts" out to us that way. E-mail has the advantage that you're already sitting at your computer, so it's a small step to go ahead and compose that letter and press the "print" button. Randall Henderson randall(at)edt.com RV-6 > Randall, > > Thanks for the nudge to get me off top dead center. I, too, got the letter > from AOPA urging response on the user fee issue, but with three daughters, a > pregnant wife, a new house, and recent move, there is precious little free > time. (Worst of all are my RV-6 wing and fuse crates buried under moving > boxes in the garage!) > > I had intended to write my congressman earlier, but kept putting it off > until I read your post yesterday. My letter goes in the mail tomorrow. > > Thanks for the boost, > > Danny Kight kightdm(at)carol.net > Anderson, SC > > RV-6 empennage completed, trying to get the new house livable so I can start > on the wings. ________________________________________________________________________________
Date: Jun 10, 1996
From: twg(at)blink.ho.att.com (Tom Goeddel(x5278))
Subject: Re: HS Skin Rivet Selection
>> I am now getting ready to skin the top side of the HS of my RV-8 and I have a >> couple concerns. First, the rivet the plans call for is an AN426AD3-3.5, using >> that rivet the protruding shank length beyond the dimple is .133" (about .010 >> shy of the minimun 1.5*D to get a good shop head) I'm sure I'll just use the -4 >> rivets and hope I dont bent over too many. Are they maybe thinking that you are Just one point... There is a range of acceptable rivet lengths before driving - between 1d and 1.5d. The 1.5d number is the max before you become more likely to have problems with bending; it is also the recommended length. The closer you can get to 1.5d the better. Practically, you can get away with a little over 1.5d but not much because of the bending problem. At the other end, 1d is a bare minimum - if you do everything exactly right there should be enough material to get an acceptable shop head. If my calculations are right, yours are coming in at about 1.4d. That should be fine - you'll still have some margin in forming the shop head. Try a few on scrap just to be sure. If you were closer to the 1d end of the scale, I'd be more inclined to bump up to the next size, but not at 1.4d. Good luck! Tom Goeddel RV-6a t.goeddel@bell-labs.com ________________________________________________________________________________
Date: Jun 10, 1996
From: wigmore(at)lancelot.chs.lane.edu (Jack Wigmore)
Subject: 6 tail and wing kit for sale
SAVE TIME AND MONEY? Buy my completed RV6/6A empenage kit (excellent) and untouched wing kit ( not pre-punched) for $4000 USD total Price. Located in Eugene Oregon. Contact J. Wigmore (541) 935-2639 or wigmore(at)lancelot.chs.lane.edu ________________________________________________________________________________
From: Greg Bordelon <greg(at)brokersys.com>
Subject: Faying compound
Date: Jun 10, 1996
Is anyone on the list using a faying compound on any of the metal to metal joints. If so, what type, cost, supplier, phone number, details etc.. I've used Black Bear "Par Al Ketone" in the past but ACF 50 dissolves it and washes it away slowly. I tried to get some chromatic paste from a supplier last week but they said the EPA or someone had it banned and removed. Help? Greg Bordelon Houston Texas Squeezing rivets with my new Avery hand squeezer....wow, I like this tool! ________________________________________________________________________________
Date: Jun 11, 1996
From: John Morrissey <John.Morrissey(at)its.csiro.au>
Subject: Re: French "reseau du sport de l'air"
Hey Guys! This is a cute site!! Lots of pictures of Jodel Homebuilts. I own a Jodel D11 - This is an Australian variant on the French design. As us Jodel owners say "Bent wings are best!!" ---At least its a cheap fun thing to fly until I get my RV4 in the air! :-) John >http://ourworld.compuserve.com/homepages/RSAIR > > --------------------------------------------------------------------------- John Morrissey CSIRO ITS Communications Section Phone:- 06 2766811 Fax:- 06 2766617 Mobile:- 018 628804 Email:- John.Morrissey(at)its.csiro.au CSIRO ---- AUSTRALIA'S SCIENCE, AUSTRALIA'S FUTURE! --------------------------------------------------------------------------- ________________________________________________________________________________
From: Michael Angiulo <mikeang(at)MICROSOFT.com>
Subject: Safety reminders
Date: Jun 10, 1996
Not just power tools, but all the corrosive chemicals as well. I have a pair of "well etched" glasses which were a result of a nice mist of alumaprep (pure acid etch) misting into my face when the wind changed. If it melts glass I'm sure my eyeballs would have liked it none too much... -Mike ---------- From: Richard Chandler[SMTP:Claris.COM!mauser(at)matronics.com] Sent: Monday, June 10, 1996 2:58 PM Subject: RV-List: Safety reminders > Bye the way, when Don was telling me about keeping the rust away he > also stressed that my engine was HOT. I've attached a ground wire to > each mag, but I turn the crank backward anyway. He told me about > a customer that was recently turning a new engine through with a > srew diver and it 'popped' once and sent the screw driver into the > side wall, where it was left as a reminder. That reminds me of one of my personal safety reminders. If anyone comes to my apartment, they'll find half of a Dremel cut-off wheel embedded in my ceiling. I left it there as a reminder to always wear safety glasses when working with power tools. (And yes, I was wearing them when it happened. My previous reminder was a small nick in the old glasses, right in front of my eye.) Let's be careful out there. Those power tools are just waiting for the moment we become cavalier about them. Flesh is so much easier to work than wood or metal. -- "Wait a minute, you expect us innocent children to climb up dangerous scaffolding and paint naked people all over a church? We'll do it!!" -- Yakko Warner, Animaniacs "Yeah, I've got ADD, you wanna make something of.... oooh, cool. Look!" ________________________________________________________________________________
From: DerFlieger(at)aol.com
Date: Jun 10, 1996
Subject: Re: Strobe Power Supply
Bob, A related matter to some of your questions: I mounted my wet compass in the center top of the instrument panel on my 6, just to the left of the radio stack. Used non-magnetic stainless for the canopy release handle. The compass error was too large to adjust out. What I found was that the DC power wires feeding my strobe unit ________________________________________________________________________________
Date: Jun 10, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Sensenich prop update (long)
Fellow RVer's: I've put some time on the new Sensenich prop installation and have the following comments. I have a 150 hp Lycoming in my RV-6 and so went with the recommended 70" diameter/77" pitch. At full throttle at 7,500' (density altitude of 8,500'), leaned for best power, the engine turned at 2470 rpms. The true calibrated airspeed was 178 mph. This is within 2-3 mph that I got with my Props Inc. prop. I wanted to increase rpms closer to the 2,600 redline so as to increase take off and climb performance and possibly increase cruise a little. We reduced pitch a little over 2" making the prop a strong 74" pitch. This increased the cruise, full throttle at 7,500' rpms to 2,560 with a manifold pressure of 23", a gain of 90 rpms for just over 2" pitch reduction. Cruise speed remained the same but take off and climb seemed to improve somewhat. I did notice that at mag check rpms of 1,700 I had to put more pressure on the brakes to stop forward movement. I believe the Sensenich is probably more efficient than the Props Inc. (or any other wood prop) due to the airfoil shape covering more of the blade area. The Sensenich does not run a smooth as the wood props I have tried. My Props Inc. ran much smoother after dynamic balancing and I will dynamically balance any prop I have on my airplane, I really beleive in it. I will have the Sensenich dynamically balanced within the next week or so and will report any improvement. We put the Sensenich on a friends 150 hp RV-4 whose Lycoming has the flat (conical) mounts. He has been flying a dynamiclly balanced Prince prop (I've had this one on my RV and it is the smoothest so far). He said the Sensenich about shook him out of the cockpit. He didn't know if the needles were going to stay on his gauges or not. When we re-pitched the Sen., we checked everything that could be checked and the prop static balanced perfectly and the blades were in track, etc. This might be a consideration for those of you who are using flat mounts. Bottom line? I don't know. I like the looks of the multi laminate props (Warnke, Props Inc., Performance props (?)) and the smoothness. Also, the price is right. In the event of a prop strike, less damage to the engine. Downside: Having to check torque on a regular basis and having to reduce rpms through rain. Sensenich advantages: rain durability (and general resistance to the elements), not having to check torque often, more flywheel effect, lower idle setting therby reducing landing distance somewhat, the ability to easily re-pitch and not having to worry about changing prop contour around the spinner cutout as you would on a wood prop that is really "re-carved" instead of re-pitched. If I can get the engine to run a little smoother, I'll probably keep the Sensenich. If not, I don't know which one I would choose to keep on my plane. Also, I'll know a little more after flying the Sensenich at full gross at high density altitude. Side note. I waited until most RVs took off for home at Boone and watched them leave. You could tell the difference between the lower powered, fixed pitched props and the RVs with big engines and/or constant speed props. I gave a couple of rides and the guy that was with me was able to compare engine sound and take offs bwtween my RV-6 and others and thought that mine compared to other RVs i.e., the fixed pitched planes didn't sound like they were developing much power because of the lower rpms. I've been chasing perceived low power output on my engine and it now appears that maybe other 150 hp/fixed pitched RV-6's are performing about the same as mine. I guess the bottom line is: if you want breath-taking T.O. and climb you're going to have to build a lite airplane and put a constant speed prop on it. I felt that my climb rate was inferior to those rates reported by some other similarly equipped RV-6's. When comparing, I think it's important to know at what weight and what density altitude the climb tests are done. I got great ROC at Sun & Fun and when it's cold here and the wind is blowing but at full gross at a density altitude of 5,000 to 8,000 feet my rate of climb is around 700 fpm. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 10, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: HS Skin Rivet Selection
> > ...the rivet the plans call for is an AN426AD3-3.5, using > that rivet the protruding shank length beyond the dimple is .133" (about .010 > shy of the minimun 1.5*D to get a good shop head) I'm sure I'll just use the -4 > rivets and hope I dont bent over too many. The important thing here is not the length before driving, but the rivet dimensions AFTER being driven. The 1.5*D is just a somewhat conservative "rule of thumb" -- rivets will smash down more or less depending on how big the hole is, whether it's dimpled or machine c-sunk, etc. Get a set of rivet gauges from Avery, and/or check the dimensions as per the MIL-SPEC or A/C (using practice pieces) -- it's not necessary (or even desirable) to go strictly by the 1.5d rule. After a short time you should be able to get a feel for just how much rivet should be sticking through by eyeballing it. Randall Henderson randall(at)edt.com RV-6 ________________________________________________________________________________
Date: Jun 10, 1996
From: Boris Robinson <smbr(at)inetw.net>
Subject: Re: RV:list, airplane financing
> Try NAFCO at 1 800 999-4515, fax 941 646-1671. I financed my -4 kit and engine. > hello all, > I have been a lister since the begining. Mostly I just read the > posts and learn. I am currently building an RV-4 (tail, wings, > are done); fuselage is begun. > I am planning on buying a Pitts S2-B as trainer & time > builder untill I get the RV-4 done. Does anyone have any info > as to the best place to seek financing in such an endevor? > > > > Thanks to all in advance > > Thomas R. Boatright > trboatri(at)ux1.cso.edu.uiuc > > ________________________________________________________________________________
Date: Jun 10, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Strobe Power Supply
>Bob, > >A related matter to some of your questions: I mounted my wet compass in the >center top of the instrument panel on my 6, just to the left of the radio >stack. Used non-magnetic stainless for the canopy release handle. The >compass error was too large to adjust out. >What I found was that the DC power wires feeding my strobe unit Uh Oh, the rest of your message disappeared. Please send again. Bob ________________________________________________________________________________
From: Rvbildr(at)aol.com
Date: Jun 10, 1996
Subject: Re: RV:list, airplane financing
Try George Hill, Pitts dealer, at Eagle Air in Hampton, Ga. His phone # at home is 770-228-1918 and dealership # is 770-707-1111. Mal rvbildr(at)juno.com ________________________________________________________________________________
From: Richard Olson <rolson(at)Capital.Net>
Date: Jun 11, 1996
Subject: Re: Preserving Engines
I have exactly the same question about long term storage of engines. I have a used O-320 I am storing on a stand in a dry basement. I made the stand to mount the engine as on the airplane and did as the Lycoming rep reportedly said and filled it with oil. I am not sure how much is staying in the cylinders - it will run out the valves and out the intake or exhaust. Just last week I poured Marvel Mystery Oil into the cylinders, blew it around with an air line and rotated the crank. I think this should keep the top in pretty good shape. My consern is the cam shaft. I don't know if there is any way to flood the area with oil and I am conserned about it pitting. Even if I wind up overhauling the engine, this would be an expensive thing to add to the bill. I was considering cleaning out the cylinders and reducing the oil to normal levels and cranking the engine with the plugs out to see if I could get enough oil pressure to lubricate the cam. Would like to hear what others think and comments on my conserns. Are there other things going on that are as bad that I haven't even thought of? Thanks for raising the question. Rich Olson - Saratoga Springs, NY - Just received 6A Tail Kit so I have a long time to preserve! ________________________________________________________________________________
From: WStucklen(at)aol.com
Date: Jun 11, 1996
Subject: Re: Sensenich prop
> **** SNIP ***** > I got great ROC at Sun & Fun and when it's cold here and the wind >is blowing but at full gross at a density altitude of 5,000 to 8,000 feet my >rate of climb is around 700 fpm. >Bob Skinner RV-6 BSkinner(at)ltec.net > > Bob: Ever think about upgrading your engine to 160 Hp? 10 Hp more in a light plane does make a noticable difference....... Fred Stucklen RV-6A N925RV wstucklen(at)aol.com ________________________________________________________________________________
From: DerFlieger(at)aol.com
Date: Jun 11, 1996
Subject: Re: Strobe Power Supply
>>Bob, >> >>A related matter to some of your questions: I mounted my wet compass in the >>center top of the instrument panel on my 6, just to the left of the radio >>stack. Used non-magnetic stainless for the canopy release handle. The >>compass error was too large to adjust out. >>What I found was that the DC power wires feeding my strobe unit > > >Uh Oh, the rest of your message disappeared. Please send again. Bob > Here's the rest! The DC power wires were causing the large compass error, even when I moved them several inches away. I replaced them with shielded wire which solved the problem. BTW, my power supply is behind the baggage bulkhead since I have 180/CS. Jim Stugart ________________________________________________________________________________
From: DerFlieger(at)aol.com
Date: Jun 11, 1996
Subject: Belly Vibrations
Flying my friend's 6A we have noticed something pertinent to the "smoking rivet" topic, though I am reluctant to get this one started again!. His plane has NO interior including the floor. It's a 160 with Sterba prop, and a Vetterman crossover exhaust. By placing your feet at strategic locations on the floor you can either start or stop a huge drumming vibration in the floor. With no interior the noise and vibration is very evident, and surely must be instrumental in the loose rivets problem. To me this floor design is not stiff enough regardless of the size and number of rivets used. I suspect the real fix is to have more stiffeners and more closely spaced. We do not however see any smoking rivets, but there are less than 200 hours on the airplane. Jim Stugart ________________________________________________________________________________
Date: Jun 11, 1996
From: "Richard E Steffens" <resteffe(at)dpcmail.dukepower.com>
Subject: Props-rpm
I've been reading with interest the stuff on the Sensenich vs wood props, Bob Skinner's trials especially. If I read you correctly Bob, you are now undecided trying to decide on smoothness vs slight performance increase and higher cost. I am rebuilding a HIO-360 for my -6. It has conical mounts and gets it's rated 180 hp at 2900 rpm. I had considered getting a new cam to get the rpm down to 2700 so I could use a metal prop. However, perhaps the wood props might be better and I could keep my 2900 rpm cam. Will the wood props perform well at around 2900 rpm? How about the Catto or other three-bladed types (lower tip speed and looks cool)? Auybody else turning their prop a little faster? Other considerations - engine wear, fuel burn, etc??? Dick Steffens RV-6 North Carolina resteffe(at)dpcmail.dukepower.com ________________________________________________________________________________
Date: Jun 11, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: Faying compound
Greg, please enlighten me. What is a 'faying compound'? I learned a lot of things I had not known when building the plane, but this is something that got completely by me. Have I left something out that I should have put in? Are my joints going to swell and become arthritic?:<) John D >Is anyone on the list using a faying compound on any of the metal to metal >joints. >Greg Bordelon > > > John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
Date: Jun 11, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: RV-6/8 Will I be comfortable?
Pat, I disagree because I agree with you. I've got DJL seats and have found them to be very comfortable summer and winter. The longest flight I've had is 3:00, and it wasn't my butt that was hurting, seems my bladder isn't as large as it use to be! Comparing DJL seats (with the temper foam or what ever it is that cost extra) and the seats we had in the F-4s, the DJL wins with a smiling 'moon'. Wish I had had them on those 6 to 14 hour missions in the F-4, but I guess nothing would have been comfortable for that length of time. >> Bob S: I'm at the point of having to decide on upholstery options for my 6A. >> I've heard George Orndorf say the temperfoam takes too long to soften >> comfortably on cold days and to use high-density polyfoam from a fabric >> store. What's been your experience? What about the rest of the gang- what >> are you sitting on and how do you like it? >> Bill Boyd >> SportAV8R(at)aol.com >I have seats from DJ Lauritson with temperfoam and both ends smile when >I sit down, either hot or cold weather!!! I have temperfoam in a open >cockpit biplane also--IT IS WORTH TWICE THE MONEY IT COSTS. Just plan >on an hour and numbness sets in with the cheap stuff. 4 to 5 hrs still >comfortable on temperfoam-- >That has been MY experience---Now let's see the screen lite up with the >usual dissenters out there---always a minority voice isn't there(and >usually loud). > John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: Preserving Engines
Date: Jun 11, 1996
If you are concerned about the cam (and lifter), store the Lyc, upside down on its back. The cam is in the top of the case so if you store it upside down (on an old car tire) then the oil will cover the cam and lifters. Herman > I have exactly the same question about long term storage of engines. I > have a used O-320 I am storing on a stand in a dry basement. I made the > stand to mount the engine as on the airplane and did as the Lycoming rep > reportedly said and filled it with oil. I am not sure how much is staying > in the cylinders - it will run out the valves and out the intake or > exhaust. Just last week I poured Marvel Mystery Oil into the cylinders, > blew it around with an air line and rotated the crank. I think this > should keep the top in pretty good shape. > > My consern is the cam shaft. I don't know if there is any way to > flood the area with oil and I am conserned about it pitting. Even if I > wind up overhauling the engine, this would be an expensive thing to add > to the bill. I was considering cleaning out the cylinders and reducing > the oil to normal levels and cranking the engine with the plugs out to > see if I could get enough oil pressure to lubricate the cam. > > Would like to hear what others think and comments on my conserns. Are > there other things going on that are as bad that I haven't even thought > of? Thanks for raising the question. > > Rich Olson - Saratoga Springs, NY - Just received 6A Tail Kit so I have a > long time to preserve! > > -- -------------------------------------------------------- *NOTICE for internet mail*: Any ideas or thoughts expressed here are my own and are independent of my employer. Herman Dierks, Dept. E54S, AWSD, Austin, Texas mail: dierks(at)austin.ibm.com ________________________________________________________________________________
From: walsh(at)cpeedy.ENET.dec.com
Date: Jun 11, 1996
Subject: Pedal kits (chatter)
I was thumbing through the June Sport Aviation last night (while the Veriprime was drying) and showed my wife the little kiddie pedal kits in the back. They had a picture of a Gee Bee and my wife said "GET IT!!!" Has anybody built one of these kits? The company is Aviation Products in Cedar Rapids, IA. There's no phone # and they want $20 for plans. My almost 3 year old daughter would love this and I am now on the hook. Thanks for your indulgence in this only slightly related topic. John ________________________________________________________________________________
Date: Jun 11, 1996
From: Harry Paine <HPair(at)ix2.ix.netcom.com>
Subject: c214 squeezer for sale
I have a rebuilt CP 214 for sale standard yoke 1 1/2" with 2 flush sets and #40 #30 #20 cupped sets. price $250.00 COD. The last ones I had for sale went in two days. If you need one this is a terrific deal. First email gets it please contact me at HPair(at)ix.netcom.com harry Paine ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Jun 11, 1996
Subject: of carb jetting & hot cylinders
I started this chain some time ago and I now have some updates that I thought might be of interest to you fellow listers. As a quick recap, my RV-6 was plagued with a lean running engine (rich EGT's in the 1450 to 1600 range with the ability of only leaning it about 40 degrees) caused by the MA-4-SPA 10-5135 carb. In addition to this problem I had cylinder temps that were all over the place. The #2 cylinder was 310 & #3 was 470 in cruise. On take-off #3 would hit red line if I didn't step climb. I thought that the above problems were related to one another and to some degree (pun intended) they were. I tried all of the voodoo fixes (like the chicken wire on the carb throat) before getting real serious. BTW, don't do the chicken wire thing. It lowered my rpm by 100 rpm and also gives forming ice a place to collect on. I spoke with Van's, Consolidated Fuel and Mark Freeman(?last name) of RV-list fame about the possibility of drilling out my carb jet. The fix almost sounded too simple. After removing my carb (for the 100th time) I split it in half and removed the fuel riser. The jet is found at the bottom of the fuel riser. Mine measured out at a #42 drill bit size so I drilled it out to a #39. On start-up I knew that I did the right thing because it ran great on the ground. In the air I was able to lean out the engine about 80 to 100 degrees. I also noticed that my cold cylinders were running hotter and my hot cylinders were running colder (about 30 degrees in both directions). So I figured that if drilling the jet a little was good, drilling it more must be better. Guess what, I was RIGHT for a change. I drilled the jet out to a #37. Now rich EGT's are 1250 to 1280 and lean EGT's are 1420 to 1460. CHT's changed about 10 degrees in both directions but the hot cylinder was still to hot at 430 in cruise. It was time to look for different problems. I found that the exit area on the lower cowl was all cluttered with exhaust brackets and other unnecessary stuff. Cleaned up and enlarged, I lowered the #3 cylinder to 410 in cruise. As luck would have it, Rob Lee (another lister) was up in NJ from TX on a business trip and I invited him to go flying. Rob has an RV-6A that had the same jet problem. And as luck would have it, the weather sucked on the day we got together. BUT, as luck would have it, Rob and I started poking around my aircraft and Rob discovered that I forgot to complete my front baffle by installing the rubber seal. I don't know how many people looked at this aircraft and nobody picked-up on this. It took someone all the way from Texas to find this problem. Thanks Rob (and thanks for finding my rubber seal material for me - from across the room no less!). Well with that fixed I found another 10 degrees. So at cruise I get the following (by cruise I mean 8000' and full throttle): Cylinder # Rich EGT Lean EGT CHT 1 1250 1420 340 2 1250 1420 370 3 1280 1460 400 4 1280 1440 350 On take-off and climb (on a 80 degree day) #3 stays about 430 which is OK. RPM spread between rich and lean is about 25 rpm. On the down side, the engine runs very rich at low power settings and requires mixture control on the ground. I didn't loose or gain any speed in the process which surprised me. At 2720 RPM I show about 195 mph +/- 3mph. I can finnally take-off and climb like an RV should however. I still think that my engine runs about 30 degrees to hot and I will continue to look for additional ways to cool it down. What temps are the other -6's running...I'd really like to know. Anyway, for now I'll leave it alone and just enjoy flying it. Gary Corde RV-6 N211GC ________________________________________________________________________________
Date: Jun 11, 1996
From: Harry Paine <HPair(at)ix3.ix.netcom.com>
Subject: Re: RV-6/8 Will I be comfortable?
>aol.com!SportAV8R(at)matronics.com wrote: >> >> Bob S: I'm at the point of having to decide on upholstery options for my 6A. >> I've heard George Orndorf say the temperfoam takes too long to soften >> comfortably on cold days and to use high-density polyfoam from a fabric >> store. What's been your experience? What about the rest of the gang- what >> are you sitting on and how do you like it? >> >> Bill Boyd >> SportAV8R(at)aol.com > > >I have seats from DJ Lauritson with temperfoam and both ends smile when >I sit down, either hot or cold weather!!! I have temperfoam in a open >cockpit biplane also--IT IS WORTH TWICE THE MONEY IT COSTS. Just plan >on an hour and numbness sets in with the cheap stuff. 4 to 5 hrs still >comfortable on temperfoam-- > >That has been MY experience---Now let's see the screen lite up with the >usual dissenters out there---always a minority voice isn't there(and >usually loud). > >MY butts been on it for ten years and couldn't be happier, now if I could just get my back to cooperate! HP ________________________________________________________________________________
Date: Jun 11, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Sensenich Re-Pitch
Fellow RVer's, If any of you have the Sensenich CM prop and would like to have it re-pitched, Jim Fix of Fix Prop Shop, Lincoln, Nebraska will re-pitch it for $ 80.00. You pay for shiping and insurance, both ways. His phone number is: 402-470-2346. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Jun 11, 1996
Subject: Re: Strobe Power Supply
For what it's worth, I put my power pack strobe under the baggage floor which is removable. I put my ELT behind (but close) to the baggage wall. My CG is fine. No problems with the radios. Gary Corde RV-6 N211GC ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Jun 11, 1996
Subject: Re: RV:list, airplane financing
Call Bobby Thomas at Citizens National Bank in Laurel, MD. He is RV friendly as he has built/flys an RV-4. Real good guy. Sorry, I don't have is number on me but he should be in the book. Gary Corde RV-6 N211GC ________________________________________________________________________________
From: dougweil(at)pressenter.com (Doug Weiler)
Subject: Re: RV:list, airplane financing
Date: Jun 11, 1996
> > > > hello all, > I have been a lister since the begining. Mostly I just read the > posts and learn. I am currently building an RV-4 (tail, wings, > are done); fuselage is begun. > I am planning on buying a Pitts S2-B as trainer & time > builder untill I get the RV-4 done. Does anyone have any info > as to the best place to seek financing in such an endevor? > > > > Thanks to all in advance > > Thomas R. Boatright > trboatri(at)ux1.cso.edu.uiuc > Try Greentree Financial in St. Paul, MN. They are actively financing homebuilts and other "exotic" flying machines. Their number is 1-800-851-1367. Doug Weiler, MN Wing ________________________________________________________________________________
From: dougweil(at)pressenter.com (Doug Weiler)
Subject: Re: Boone Fly-in Question
Date: Jun 11, 1996
The Boone flyin was a major success. Weather was perfect for the first time in several years. 30 RVs were on the field with about 150 in attendance. I flew my 180 down with 6 Rvs from the local MN area. (of course they beat me by 30 minutes!!). We had a great pig roast. Several workshops were on hand (fuel tanks, riveting, etc). Lots of partially completed components also on display. Many nice RVs were there, but I was floored by the beautiful RV-4 by Lyle Hefer of Dubuque, IA. Lyle built a beautiful -6 several years ago, and his -4 was even better. It had a sliding canopy of his own design that really changed the looks of the -4 (and for the better). He had a custom bubble blown and the mechanism is ingenious (you roll it back with a little crank like a P-51). Lyle modified the fuselage to move the instrument panel forward and the front seat back slightly. I sat in it and and was most comfortable. It felt better than any -4 I've been in. Footwells for the rear passenger and ingenious "hanging" rear rudder pedals that were both simpler and better looking than Van's design. His RV had the tall gear and was powered by a 180 with a C/S. His cruise is 205 mph!!! Lyle master is a master in in the machine shop and many items he made himself (rudder pedals, tailwheel, etc). If I can only convince him to tell me his secret of this canopy design. It's great!!!!! Doug Weiler, MN Wing ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: Pedal kits (chatter)
Date: Jun 11, 1996
I built a pair of the X29/X15 jets that they offer. Their plans and designs are first rate. I think it came with about 18 pages of detailed steps to build the plane. The plans are full-size so you just cut them out and transfer to the plywood. The jets were designed to use 1 sheet of plywood. I had to buy a router (wanted one anyway). They offer other kits for the welded components, wheels, decals, etc. I used these as I wanted to minimize the time it took. I built the two jets in about 4 or 5 weekends, including full paint and decals. Showed them at the Kerville flyin twice. One made the Pacific Flyer newspaper with my son 'flying' it. I think they cost about $225.00 each with all the material, paint, etc. This company offers about a dozen types of planes from Pitts, P51, etc. all very good designs. He usually shows them at Oshkosh by the main entrance by the control tower. Herman > I was thumbing through the June Sport Aviation last night (while the > Veriprime was drying) and showed my wife the little kiddie pedal kits in > the back. They had a picture of a Gee Bee and my wife said "GET IT!!!" > > Has anybody built one of these kits? The company is Aviation Products in > Cedar Rapids, IA. There's no phone # and they want $20 for plans. > > My almost 3 year old daughter would love this and I am now on the hook. > Thanks for your indulgence in this only slightly related topic. > > John > -- -------------------------------------------------------- *NOTICE for internet mail*: Any ideas or thoughts expressed here are my own and are independent of my employer. Herman Dierks, Dept. E54S, AWSD, Austin, Texas mail: dierks(at)austin.ibm.com ________________________________________________________________________________
From: david_fried(at)smtpgwy.dehavilland.ca
Date: Jun 11, 1996
Subject: Sensenich Re-Pitch
The blade twist distribution from root to tip is a factor in propeller performance. The pitch on a controllable propeller is changed by rotating the blade about a bearing at the root, preserving the twist distribution and changing the angle of attack for each spanwise station an equal amount. I imagine that the re-pitching process does not take place at the root of the blade as there is an awful lot of metal there. The posting below says that the job can be done inexpensively, which makes me think that it is not a lengthy process. Does any body know how this is done? Where does the blade deformation take place? David Fried DF-6 C-____ dfried(at)dehavilland.ca ______________________________ Forward Header __________________________________ Subject: RV-List: Sensenich Re-Pitch Date: 6/11/96 12:13 PM Fellow RVer's, If any of you have the Sensenich CM prop and would like to have it re-pitched, Jim Fix of Fix Prop Shop, Lincoln, Nebraska will re-pitch it for $ 80.00. You pay for shiping and insurance, both ways. His phone number is: 402-470-2346. Bob Skinner RV-6 BSkinner(at)ltec.net >From owner-rv-list(at)matronics.com Date: Tue, 11 Jun 1996 10:10:58 -0500 From: Bob Skinner <ltec.net!BSkinner(at)matronics.com> Subject: RV-List: Sensenich Re-Pitch ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: of carb jetting & hot cylinders
Date: Jun 11, 1996
Gary, you did not say what engine/HP you have. Can you post that info? I have the same carb model number on my O320-E2D and have somewhat similar problem of too lean a mixture. I just got off the phone with Precision Airmotive (The Marvel carb mfg.). They have a Ventrui Hotline (1-800-838-8181). He said one of the main problems is mechanics that set the one piece venturi in the carb and drive it down too far. It is suppose to stop with the 3 feet where the carb halves meet. I plan to check this first. He said to also check the bowl vent for blockage and the main jet for blockage, and the intake tubes for air leaks. I don't think I have any of those problems. He also told me to make sure I had venturi part number 46-F10. There are several models that are close to the same. You can not see the part number however unless the venturi is removed as it is stamped on the outside of the venturi. Herman > I started this chain some time ago and I now have some updates that I thought > might be of interest to you fellow listers. > > As a quick recap, my RV-6 was plagued with a lean running engine (rich EGT's > in the 1450 to 1600 range with the ability of only leaning it about 40 > degrees) caused by the MA-4-SPA 10-5135 carb. In addition to this problem I > had cylinder temps that were all over the place. The #2 cylinder was 310 & #3 > was 470 in cruise. On take-off #3 would hit red line if I didn't step climb. > I thought that the above problems were related to one another and to some > degree (pun intended) they were. > > I tried all of the voodoo fixes (like the chicken wire on the carb throat) > before getting real serious. BTW, don't do the chicken wire thing. It > lowered my rpm by 100 rpm and also gives forming ice a place to collect on. > > I spoke with Van's, Consolidated Fuel and Mark Freeman(?last name) of RV-list > fame about the possibility of drilling out my carb jet. The fix almost > sounded too simple. After removing my carb (for the 100th time) I split it > in half and removed the fuel riser. The jet is found at the bottom of the > fuel riser. Mine measured out at a #42 drill bit size so I drilled it out to > a #39. On start-up I knew that I did the right thing because it ran great on > the ground. In the air I was able to lean out the engine about 80 to 100 > degrees. I also noticed that my cold cylinders were running hotter and my > hot cylinders were running colder (about 30 degrees in both directions). So I > figured that if drilling the jet a little was good, drilling it more must be > better. Guess what, I was RIGHT for a change. > > I drilled the jet out to a #37. Now rich EGT's are 1250 to 1280 and lean > EGT's are 1420 to 1460. CHT's changed about 10 degrees in both directions > but the hot cylinder was still to hot at 430 in cruise. It was time to look > for different problems. I found that the exit area on the lower cowl was all > cluttered with exhaust brackets and other unnecessary stuff. Cleaned up and > enlarged, I lowered the #3 cylinder to 410 in cruise. > > As luck would have it, Rob Lee (another lister) was up in NJ from TX on a > business trip and I invited him to go flying. Rob has an RV-6A that had the > same jet problem. And as luck would have it, the weather sucked on the day we > got together. BUT, as luck would have it, Rob and I started poking around my > aircraft and Rob discovered that I forgot to complete my front baffle by > installing the rubber seal. I don't know how many people looked at this > aircraft and nobody picked-up on this. It took someone all the way from > Texas to find this problem. Thanks Rob (and thanks for finding my rubber seal > material for me - from across the room no less!). Well with that fixed I > found another 10 degrees. So at cruise I get the following (by cruise I mean > 8000' and full throttle): > > Cylinder # Rich EGT Lean EGT CHT > 1 1250 1420 340 > 2 1250 1420 370 > 3 1280 1460 400 > 4 1280 1440 350 > > On take-off and climb (on a 80 degree day) #3 stays about 430 which is OK. > RPM spread between rich and lean is about 25 rpm. On the down side, the > engine runs very rich at low power settings and requires mixture control on > the ground. I didn't loose or gain any speed in the process which surprised > me. At 2720 RPM I show about 195 mph +/- 3mph. I can finnally take-off and > climb like an RV should however. I still think that my engine runs about 30 > degrees to hot and I will continue to look for additional ways to cool it > down. > > What temps are the other -6's running...I'd really like to know. Anyway, for > now I'll leave it alone and just enjoy flying it. > > Gary Corde > RV-6 N211GC > -- -------------------------------------------------------- *NOTICE for internet mail*: Any ideas or thoughts expressed here are my own and are independent of my employer. Herman Dierks, Dept. E54S, AWSD, Austin, Texas AIX Network Performance Measurement/Analysis phone: TL 678-2831 outside: (512) 838-2831 MS: 9530 fax: 512-838-1801 mail: dierks(at)austin.ibm.com ________________________________________________________________________________
Date: Jun 11, 1996
From: bcos(at)ix.netcom.com (William Costello )
Subject: Re: RV:list, airplane financing
You wrote: > >Call Bobby Thomas at Citizens National Bank in Laurel, MD. He is RV friendly >as he has built/flys an RV-4. Real good guy. > >Sorry, I don't have is number on me but he should be in the book. > >Gary Corde >RV-6 N211GC > Phone number is 410-792-7626. I have a call in for him. Thanks Gary. -- Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 Building RV-6 or 6A | Reserved N97WC ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 11, 1996
Subject: Re: Gascolators
This may have been discussed before but it is probably like the wheel landing/three point debate: the discussion is ongoing. So-> To Gascolate or Not to Gascolate: that is the question. The argument is that gascolators is 1930's tractor technology. How many do you see on cars these days? There is debate in this neck of the forest whether we need them (appologies to our Canadian brethren as they are required). I know some who have put the inline glass filters under the floorbords with little windows to see what is happening in the filters. There is one for each tank. This makes all kinds of sense as, when the sloshing compound decides to come unstuck it won't jam up the entire system (as it would if a gascolator was used). There is argument also that the lowest point in the fuel system on the RV-s is the tanks anyway and a gascolator isn't much good for trapping water. WELL: I have one on the -4 because "that's the way we've always done it" but now I wonder if I have the best system. Whaddya think? Michael Kosta RV-4 232SQ Fly By July (or August, something, I don't know) ________________________________________________________________________________
Subject: Re: Preserving Engines
Date: Jun 11, 1996
From: "Calin Brabandt" <cwbraban(at)ichips.intel.com>
Herman Dierks has a good point: > If you are concerned about the cam (and lifter), store the Lyc, upside down > on its back. The cam is in the top of the case so if you store it upside > down (on an old car tire) then the oil will cover the cam and lifters. I stored my Lyc upside down. I removed the spark plugs and filled each cylinder with Stitts storage oil. Then I replaced the bottom set of plugs (top set when the engine's upside down) with dessicant plugs, just to be sure but I don't think there's any air in there at all. I also replaced the crankcase oil with Stitts storage oil. With the engine upside-down, you can fill it up to a level in the sump (covering all moving parts) using about four gallons including the cylinders mentioned above. The oil can't run out of the cylinders because the oil level is above the cylinders. I think I paid about $25 / gallon for the oil so the total price of storage was a little over $100 with the plugs. Cal ________________________________________________________________________________
Date: Jun 11, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Sensenich prop
>Bob: > Ever think about upgrading your engine to 160 Hp? 10 Hp more in a light >plane does make a noticable difference....... > >Fred Stucklen RV-6A N925RV Hi Fred, Yes, I've thought about it. I really messed up. I overhauled the engine several years ago and at the time thought that I would use auto fuel. I had been using auto fuel with no problems for years in my 1948 Cessna 170 and my 90 hp Super Cub. Eventually, I came to the conclusion that I didn't want to use auto fuel in the RV, so I should have put in the higher compression pistons. I really hesitate to tear into the engine now as it uses no oil, compression is good, etc. If I ever have any cylinder problems, I'll probably convert to 160 hp, but for now will leave things as they are. Thanks, Bob Skinner ________________________________________________________________________________
Date: Jun 11, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Belly Vibrations
>Flying my friend's 6A we have noticed something pertinent to the "smoking >rivet" topic, though I am reluctant to get this one started again!. His >plane has NO interior including the floor. It's a 160 with Sterba prop, and >a Vetterman crossover exhaust. By placing your feet at strategic locations >on the floor you can either start or stop a huge drumming vibration in the >floor. With no interior the noise and vibration is very evident, and surely >must be instrumental in the loose rivets problem. To me this floor design is >not stiff enough regardless of the size and number of rivets used. I >suspect the real fix is to have more stiffeners and more closely spaced. We >do not however see any smoking rivets, but there are less than 200 hours on >the airplane. > >Jim Stugart Jim, does your friend's exhaust system have the turn downs on it? After I installed turn downs on my Vetterman SS cross-over, vibration dropped a little and noise dropped alot. I agree that more stiffners might help the problem. Thanks for your comments on strobes. Bob Skinner ________________________________________________________________________________
Date: Jun 11, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Props-rpm
> I've been reading with interest the stuff on the Sensenich vs wood > props, Bob Skinner's trials especially. If I read you correctly Bob, > you are now undecided trying to decide on smoothness vs slight > performance increase and higher cost. I am rebuilding a HIO-360 for my -6. It has conical mounts and gets > it's rated 180 hp at 2900 rpm. I had considered getting a new cam to > get the rpm down to 2700 so I could use a metal prop. However, perhaps > the wood props might be better and I could keep my 2900 rpm cam.> > Will the wood props perform well at around 2900 rpm?> > How about the Catto or other three-bladed types (lower tip speed and > looks cool)?> > Auybody else turning their prop a little faster?> > Other considerations - engine wear, fuel burn, etc??? > > Dick Steffens RV-6 North Carolina > resteffe(at)dpcmail.dukepower.com Dick, My guess is that I'll keep the metal prop. I'm pretty sure that this prop will benifit from a dynamic balance job. The metal prop seems to provide more thrust even though the take off rpms are lower that with the wood. Not having to check torque and being able to blast through rain are other advantages. As far as I know, the testing is not done on the prop that Sensenich has designed for the 180 hp. It's possible that there won't be any redline restriction on this prop. It would be interesting to get comments from other builders who have conical mounts and are running the metal prop. I wouldn't base my selection on just my say so. The RV-4 that we put the Sen. on might have had some trait in the engine/airframe that caused excessive vibration, I don't know. I do know that the engine in this RV ran very, very smoothly with the wood prop. I would think that it would be more cost-effective to reduce rpms through prop pitch changes than to have to purchase a new cam, especially if you were not going to split the case, anyway. This would drop the horse power, though. I'm sure there are others on the list who know this engine and could give you better advice, than I. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 11, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Belly Vibrations
I've had the guys from Van's over a few times looking over my fuselage and they were talking about this very issue, and recommended an .040 aluminum sub-floor over the stiffeners, attached to the stiffeners somehow, with insulation underneath. Mike Seager is doing something similar on his current RV-6. He replaced the two outer stiffeners with 3/4" deep by 1 1/2" wide "U" channels, (custom made) and intends to pop-rivet the sub-floor directly to those. ______ | | ---+ +--- My intention is to use 3/4" angle screw/nut-plated or riveted to the existing channel, and use nut plates/screws to screw the subfloor to those pieces. +--- || ---+ Randall Henderson RV-6 ________________________________________________________________________________
From: "Jeff Davis" <jdavis1(at)ford.com>
Date: Jun 11, 1996
Subject: Need Instructions on how to change E-Mail Address
I have changed E-Mail address - What is the process to update the list?? Tail underway - Starting to skin.... -- ******************************************************************************** Jeffrey S. Davis Ford Motor Company Supervisor - Performance Luxury Chassis Engineering (313)845-8114 Fax (313)317-4960 ******************************************************************************** ________________________________________________________________________________
Date: Jun 11, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Sensenich Re-Pitch
The blade twist distribution from root to tip is a factor in propeller > performance. > I imagine that the re-pitching process does not take place at > the root of the blade as there is an awful lot of metal there. > The posting below says that the job can be done inexpensively, which > makes me think that it is not a lengthy process. Does any body know > how this is done? Where does the blade deformation take place? > > David Fried David, You are correct. The re-pitching starts at around 20 inches or so from the hub, I believe. I was there when Jim Fix re-pitched my prop but don't remember the station numbers. There were about 4 stations marked along the prop. For each station there is a template that matches the prop at that station. The template is placed on a---I don't know what you call it--- a protractor kind of thing with degrees marked on it that is placed on a very flat metal table. The prop is clamped down at the hub. Then, they take a padded "U" shaped tool the width of the prop blade and with an arm about six feet long and slide it into postion at the appropriate station and put some weight on it. Jim draped his leg on the arm and really put some weight on it. The pitch is checked and more bending is done, if needed. As he progresses outward, different "U" tools with shorter arms are used. When re-pitching is done, he checks track and balance. Jim didn't have to do much bending and it only took one or two shots for him to get it right. He's been doing this a long time. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
From: rwoodard(at)lawyernet.com
Date: Jun 11, 1996
Subject: Wiring Grommets
I apologize if this same basic message appears more than once. I think I lost the first one in cyberspace... A couple of us RV-8 builders are to the point where we need to install elastic grommets in the VS and HS ribs to provide for lighting, communication and navigation antenna and wires. We've found AN931 Elastic Grommets for sale on page 102 of the most recent AS catalog. Can anyone give advice as to which grommets we need and how many? Assume that we're installing every electronic/avionics gadget known to man including the newly-released electric, turbo-charged, inverted sliding canopy option. :-o) Thanks in advance for the answers, Greg Puckett and Rod Woodard RV-8, #'s 80081 and 80033 Aurora and Loveland, Colorado 71155.2336(at)Compuserve.com RWoodard(at)lawyernet.com P.S. To Colorado RV-builders: I spoke with Van's this afternoon. They are "for sure" going to bring the RV-8 and "probably" an RV-6 to the Longmont fly-in on June 29-30. We'll see ya all there! And remember... the line for RV-8 rides forms behind me! [rww] ________________________________________________________________________________
From: rmickey(at)ix.netcom.com
Date: Jun 11, 1996
Subject: Re: Need Instructions on how to change E-Mail Address
>I have changed E-Mail address - What is the process to update the list?? > >Tail underway - Starting to skin.... > >-- >*************************************************************************** ***** > Jeffrey S. Davis > Ford Motor Company > Supervisor - Performance Luxury Chassis Engineering > (313)845-8114 Fax (313)317-4960 >*************************************************************************** ***** > > Send a message from your old email address to rv-list-request(at)matronics.com put unsubscribe in the body of the message Then from your new email address do the same but put subscribe in the body. Also, try to remember to turn off your signature, or make a small one, when sending messages as they clog the archives. Ross Mickey ________________________________________________________________________________
From: rwoodard(at)lawyernet.com
Date: Jun 11, 1996
Subject: Wire grommets
Several of us building RV-8's are at a point where we need to install grommets to provide for lighting, communication and navigation wiring. What size should we be considering? And approximately how many will we need for the entire project so that we can order them all at once. We've found AN931 elastic grommets on page 102 of the most current AS catalog. Can anyone out there suggest which sizes we should order and install. Assume we'll be installing every electronic/avionics option known to man including the optional electric sliding canopy. Thanks in advance for the help. Greg Puckett and Rod Woodard RV-8, #'s 80081 and 80033 Aurora and Loveland, Colorado P.S. To all the other Colorado RV-builders: I just talked to Van's and they are "for sure" bringing the RV-8 and "probably" a -6 to the June 29-30 Longmont Fly-In. See ya all there! The line forms behind me! [rww] ________________________________________________________________________________
Date: Jun 11, 1996
From: paulried(at)Interpath.com
Subject: Pedal kits (chatter)
>I was thumbing through the June Sport Aviation last night (while the >Veriprime was drying) and showed my wife the little kiddie pedal kits in >the back. They had a picture of a Gee Bee and my wife said "GET IT!!!" > >Has anybody built one of these kits? The company is Aviation Products in >Cedar Rapids, IA. There's no phone # and they want $20 for plans. > >My almost 3 year old daughter would love this and I am now on the hook. >Thanks for your indulgence in this only slightly related topic. > >John > John: There is a company called Wings & Wheels, P.O. Box 1510, Jacksonville, OR 97530 phone # 503-878-1473 fax # 503 -878-1461 that offers what they call and RV-Sport. You can just get the plans or you can get a kit that has ABS cowling, wheel pants, and a windshield. It is a tail dragger that looks just like an RV-3. I built one for my kids and they love it, but it takes up a whole lot of space in the garage! You need to pull one of the cars out to get it past. Paul Riedlinger paulried(at)interpath.com Empennage almost done....wing kit set to ship June 26th! ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: Gascolators
Date: Jun 11, 1996
I guess they are getting a bit outdated, however I put one on my RV4. I think the main value is that it could hold a lot of water if needed. If you stopped for fuel and got some bad fuel (with water in it) the gascolator may save you. How many of you drain your sumps after you fill up at the pumps (on a XC lets say). I never have. This can happen. I know of one FBO that had underground tanks and they had a lot of water leak into the tank after some heavy rain. The FBO was not aware that this had happened. There was so much water that it filled the filter on the truck. Luckly, the line person noticed that the filler spout was not cold as it normally was on fueling a plane and they got to checking and they had pumped almost pure water into the plane. Not even a gascolator would have helped this screw up. However, you get the point. These small inline filters will not trap the water. Herman > This may have been discussed before but it is probably like the wheel > landing/three point debate: the discussion is ongoing. So-> > > To Gascolate or Not to Gascolate: that is the question. > > The argument is that gascolators is 1930's tractor technology. How many do > you see on cars these days? There is debate in this neck of the forest > whether we need them (appologies to our Canadian brethren as they are > required). I know some who have put the inline glass filters under the > floorbords with little windows to see what is happening in the filters. > There is one for each tank. This makes all kinds of sense as, when the > sloshing compound decides to come unstuck it won't jam up the entire system > (as it would if a gascolator was used). There is argument also that the > lowest point in the fuel system on the RV-s is the tanks anyway and a > gascolator isn't much good for trapping water. > > WELL: I have one on the -4 because "that's the way we've always done it" but > now I wonder if I have the best system. > > Whaddya think? > > Michael Kosta > RV-4 232SQ > Fly By July (or August, something, I don't know) Herman Dierks, Dept. E54S, AWSD, Austin, Texas mail: dierks(at)austin.ibm.com ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: RV:list, airplane financing
Date: Jun 11, 1996
AOPA also finances AC. If you are a member of AOPA, you should have received junk mail on this. I think EAA also has someone that will do financing. I used Bank1 locally here to finance a plane. Our credit union will also do it. Many of these places have the usual red tape. At Bank1, all they wanted to see was some comparable listings from trade-a-plane. They did not need to see the logs or the plane. Nice and easy, but that may have just been the person we dealt with. The message is, check your local banks, as many are eager to finance and some have a person that handles the aircraft loans. > You wrote: > > > >Call Bobby Thomas at Citizens National Bank in Laurel, MD. He is RV > friendly > >as he has built/flys an RV-4. Real good guy. > > > >Sorry, I don't have is number on me but he should be in the book. > > > >Gary Corde > >RV-6 N211GC > > > Phone number is 410-792-7626. I have a call in for him. Thanks Gary. > -- > > Bill Costello | bcos(at)ix.netcom.com | Chicago | 312-445-1246 > Building RV-6 or 6A | Reserved N97WC > > Herman Dierks, Dept. E54S, AWSD, Austin, Texas mail: dierks(at)austin.ibm.com ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 11, 1996
Subject: Re: Gascolators
SNIP>>>>>>>>> >To Gascolate or Not to Gascolate: that is the question. SNIP>>>>>>>>>>>> >Whaddya think? > >Michael Kosta >RV-4 232SQ Michael: I too puzzeld over this question 2 1/2 years ago when I was building. I put it in and have never found anything other than gas in it in the 200 hours I've been flying my 4. I would want some form of filtration in the system if it wasn't there so I guess the screen serves the purpose. I have given some thought to the potential problem of a chunck of slosh comming loose and blocking the fuel system at the tank switch but I have not seen any loose crud in the tanks when I sump them. So.......I fly it the way most everybody does with the gascolator. One of the guys I hangar with elected not to use one, but has one large in line filter after the tank selector. It's a high pressure injected installation. We'll see how that works out as far as how much of a pain it is to inspect. Regards: Rusty Gossard N47RG RV-4 Flying ________________________________________________________________________________
Date: Jun 11, 1996
From: Dan Boudro <dboudro(at)nmia.com>
Subject: Re: Gascolators
I've got one because: - that's the way we've always done it - same reason I have an O320 - it makes me turn the fuel pump on, walk around, and check the gascolator. I once noticed fuel pouring out from under the cowl, when I turned the fuel pump off the flow stopped! It was a hose which was leaking severely at a connector. - its on my checklist forever IMHO, you don't really need one but I'd install one anyway. Some logic here, hu? (engineer) :-) Dan Boudro RV-4 N9167Z Albuquerque, NM dboudro(at)nmia.com ________________________________________________________________________________
From: Michael Angiulo <mikeang(at)MICROSOFT.com>
Subject: Wiring Grommets
Date: Jun 11, 1996
Here's what I did: I asked Van's who suggested that grommets aren't as good as just running the wire through a polished hole in the rib and then using silicon all around it to completely secure the wire. I didn't like that answer. A local mechanic then told me to just go buy some automotive grommets, drill a hole or two and put them in the center rib. The end ribs are easy to drill and fit once you know what you're going to be routing. I used some grommets which looked like they would fit normal coax cable (pencil thickness), figuring I wouldn't have anything bigger than that in the tail anyway. I put two of them along the centerline of the center rib. One I just put in the back by reaming the ?" tooling hole to size and the other I just drilled about 3" farther forward. I hope this works! -Mike Getting good at drilling out rivets ---------- From: lawyernet.com!rwoodard(at)matronics.com[SMTP:lawyernet.com!rwoodard(at)matronics. com] Sent: Tuesday, June 11, 1996 1:39 PM Subject: RV-List: Wiring Grommets I apologize if this same basic message appears more than once. I think I lost the first one in cyberspace... A couple of us RV-8 builders are to the point where we need to install elastic grommets in the VS and HS ribs to provide for lighting, communication and navigation antenna and wires. We've found AN931 Elastic Grommets for sale on page 102 of the most recent AS catalog. Can anyone give advice as to which grommets we need and how many? Assume that we're installing every electronic/avionics gadget known to man including the newly-released electric, turbo-charged, inverted sliding canopy option. :-o) Thanks in advance for the answers, Greg Puckett and Rod Woodard RV-8, #'s 80081 and 80033 Aurora and Loveland, Colorado 71155.2336(at)Compuserve.com RWoodard(at)lawyernet.com P.S. To Colorado RV-builders: I spoke with Van's this afternoon. They are "for sure" going to bring the RV-8 and "probably" an RV-6 to the Longmont fly-in on June 29-30. We'll see ya all there! And remember... the line for RV-8 rides forms behind me! [rww] ________________________________________________________________________________
From: MIKE_PARKINSON@HP-Australia-om1.om.hp.com
Date: Jun 12, 1996
Subject: Re: Faying compound
Hi, I had not questioned this issue before, but in my 9 years in the airforce we were always required to use faying compound between riveted joints. What is it? well - we used a yellow chromate type paste. I guess its a bit like gasket cement on cars, but its never supposed to harden. The maintenance manuals I have for military aircraft all require the use of a faying compound. I have not been using it on my RV6, although I am now wondering whether I would be better off using it? Regards Mike Parkinson RV6 HS ______________________________ Reply Separator _________________________________ Subject: Re: RV-List: Faying compound HP-Singapore,mimegw1 Date: 11/6/96 11:33 PM Greg, please enlighten me. What is a 'faying compound'? I learned a lot of things I had not known when building the plane, but this is something that got completely by me. Have I left something out that I should have put in? Are my joints going to swell and become arthritic?:<) John D >Is anyone on the list using a faying compound on any of the metal to metal >joints. >Greg Bordelon > > > John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
Date: Jun 11, 1996
From: Phil Arter <arter(at)ncar.ucar.edu>
Subject: Preserving Engines
If you store your engine upside down and filled with oil, and especially if you fill the cylinders with oil, you should tag it so you remember to drain the cylinders before inadvertantly trying to turn it over with the starter or prop. With a hydraulic lock in the cylinders it is possible to damage a connecting rod. Phil ________________________________________________________________________________
Date: Jun 11, 1996
From: "Richard Chandler" <mauser(at)Claris.COM>
Subject: Re: Preserving Engines
> I stored my Lyc upside down. I removed the spark plugs and filled > each cylinder with Stitts storage oil. Then I replaced the bottom set > of plugs (top set when the engine's upside down) with dessicant > plugs, just to be sure but I don't think there's any air in there at > all. > > I also replaced the crankcase oil with Stitts storage oil. With > the engine upside-down, you can fill it up to a level in the > sump (covering all moving parts) using about four gallons including > the cylinders mentioned above. The oil can't run out of the > cylinders because the oil level is above the cylinders. > > I think I paid about $25 / gallon for the oil so the total price > of storage was a little over $100 with the plugs. Couldn't you do the same thing with something cheaper, like Kerosene? (I used to have a friend who kept his guns, with the grips removed, in a 5 gallon bucket of Kero. He never had to clean them. Just fish them out, wipe 'em down and oil them before he went shooting, and dump them back in when he was done. Hoppes No. 9 is mainly Kerosene anyway.) -- "Wait a minute, you expect us innocent children to climb up dangerous scaffolding and paint naked people all over a church? We'll do it!!" -- Yakko Warner, Animaniacs "Yeah, I've got ADD, you wanna make something of.... oooh, cool. Look!" ________________________________________________________________________________
Date: Jun 11, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: of carb jetting & hot cylinders
Gary; For what it's worth, I have an 0-320 e2d, have a single probe on the #4 cly (left rear) and I get 290-315 cht and 1300-1475 egt. The egt is located 1 1/2 in below the flange. The instruct. for the egt probe suggested that location. I was advised later (by a guru) that I should have put it further downstream so as not to 'burn' it out too soon. The cht is probe type. I always considered this cht to be low, but doesn't seem to have effected anything, unless it was the glazing of the cly walls and resulting low comp at 125 hours. Don't know what caused that. John D >What temps are the other -6's running...I'd really like to know. Anyway, for >now I'll leave it alone and just enjoy flying it. > >Gary Corde >RV-6 N211GC > John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
Date: Jun 11, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: Gascolators
Michael; Since you asked. I had the gascolater because 'that's the way it's done'. It didn't make sense to me at the time except that it was a strainer or filter. I had some vapor lock problems with mine when using auto fuel. I first shielded and blast tubed the gascolater. It apparently helped. Then I thought about the slosh compound coming off, what it would do to the smallest diameter in the fuel line- the elect boost pump. So I put an inline see through auto type fuel filter in the lines from the tank to the fuel selector, thinking that if the stuff comes loose, it would take an awful lot to stop up the pleats in the filter, plus I could switch to the other tank if so. The only thing, most of the auto fuel filters will sort of turn to mush if they get water in them. So I check mine (in addition to tank drain) before each flight, they are just forward of the main wing spar, behind my heels on the left side, same location on the rt side. I plan to change them out each yearly or 100 hours. Cost about 3.50 per. As for water, I try to refuel before I let the plane sit over night. When I went through AF fly training, at basic and advanced, they drilled into us that the main source of water was condensation within the tank when it wasn't full, like an over night cool down with the tanks only partially full. The gascolater we were told was located in the lowest position of the fuel system and served as a filter and settlement bowl. In the RV6, I think I now have a filter in line, and a settlement bowl, in the lowest part of the fuel system, the shape of the wing tank. So I have the service of a gascolater without the gascolater which apparently was a heat sink as well when it was in the engine compartment. Incidentally, the local FBO says I should have it for the water that may form in the lines from the selector to the carb. We have a difference of opinion regarding that. When I asked him what would collect it that formed from the gascolator to the carb, he said it won't form there!! So, to answer your question, I don't have a gascolator anymore, and haven't had any more vapor problems either. So, it's your call as you know. But the above is my shadetree reasoning. John D John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
Date: Jun 11, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: Sensenich Re-Pitch
David; The pitch change takes place outside of a certain dist from the hub. The Sensinich home page has info regarding this. I don't remember the exact dist but it says something like 'no repitch should occur with in xxx dist of the hub, where the thickness is xxx inches. Rather than give you what my bad memory has, you can down load it from the horses mouth. John D John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
From: rmickey(at)ix.netcom.com
Date: Jun 11, 1996
Subject: Exhaust Turndowns
> >Jim, does your friend's exhaust system have the turn downs on it? After I >installed turn downs on my Vetterman SS cross-over, vibration dropped a >little and noise dropped alot. I agree that more stiffners might help the >problem. Thanks for your comments on strobes. Bob Skinner > > I mentioned the use of turndowns on the exhaust at our last builders meeting and the response was one of hesitation. The concern is that the turndown will cause a significant upward thrust on the end of the exhaust placing a tourque on the exhaust pipes. Is this a concern or are the exhaust pipes secured in such a way as to compensate for this? I remember a past post noting that turndowns were not availible for some engine/exhaust combinations. Is this true? ---------------------------------------------------------------------------- ------------------------------------- ---------------------------------------------------------------------------- ------------------------------------- Ross Mickey Phone: 541-342-1892 2300 Oakmont Way #205 Fax: 541-342-5492 Eugene, Oregon 97401 email: rmickey(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 11, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: Belly Vibrations
Bob; Could I bother you for an elaboration on these turn down tubes? Are they like the exhaust ext we use to put on our hot rods, chrome etc? Or are they something that is welded on etc.? John D >Jim, does your friend's exhaust system have the turn downs on it? After I >installed turn downs on my Vetterman SS cross-over, vibration dropped a >little and noise dropped alot. I agree that more stiffners might help the >problem. Thanks for your comments on strobes. Bob Skinner > > John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
From: jpl(at)showpg.mn.org (Joe Larson)
Subject: Re: Gascolators (displaying my ignorance)
Date: Jun 11, 1996
Well, time to display my utter ignorance of the fuel system. What's a gascolator? I'm assuming it's some sort of filter. For a more complete answer, how about listing the parts of the fuel system, beginning with the fuel tank, in order. Thanks. -J -- Joe Larson jpl(at)showpg.mn.org 612-591-1037 Showpage Software, Inc. http://www.wavefront.com/~showpg 6121 St. Croix Ave. N. Wings shipped last Friday. Golden Valley, Mn 55422 Future RV-6A pilot. ________________________________________________________________________________
Date: Jun 12, 1996
From: Finn Egil H|yer Grimnes <f.e.h.grimnes(at)fys.uio.no>
Subject: New member of the list
I am hoping to build an rv6 in time, in that respect I am wondering if any of you have heard anyting about putting a Volvo engine in a rv? There are these swedish guys who have put the 6cylinder version of a 960Volvo engine in a Piper Pony, it has been running for some time now pulling gliders with a 4 bladed prop and silencer, nice and quiet! I recently heard that someone has put a Volvo engine in an rv, probably the 5 cylinder version of the same engine, but that's all I have heard. Finn Egil Grimnes ________________________________________________________________________________
From: Rvbildr(at)aol.com
Date: Jun 12, 1996
Subject: Re: Belly Vibrations
Do you think adding some 3/4x3/4 angle in between the existing stiffeners would be a good idea? It couldn't weigh that much. Mal rvbildr(at)juno.com ________________________________________________________________________________
Date: Jun 12, 1996
From: Pat McClung <pmc123(at)airmail.net>
Subject: Re: Belly Vibrations
John Darby wrote: > > Bob; > Could I bother you for an elaboration on these turn down tubes? Are they > like the exhaust ext we use to put on our hot rods, chrome etc? Or are they > something that is welded on etc.? > John D > > >Jim, does your friend's exhaust system have the turn downs on it? After I > >installed turn downs on my Vetterman SS cross-over, vibration dropped a > >little and noise dropped alot. I agree that more stiffners might help the > >problem. Thanks for your comments on strobes. Bob Skinner > > > > > John Darby RV6 N61764 flying > johnd@our-town.com The turn downs are about 4" long, made of the same material as the exhaust with about 30 degree angle. I welded mine in 4 place around perimeter--They fit over the exhaust tail pipes and fastening is dealers choice. ________________________________________________________________________________
Date: Jun 12, 1996
From: Pat McClung <pmc123(at)airmail.net>
Subject: Re: Exhaust Turndowns
ix.netcom.com!rmickey(at)matronics.com wrote: > > > > > >Jim, does your friend's exhaust system have the turn downs on it? After I > >installed turn downs on my Vetterman SS cross-over, vibration dropped a > >little and noise dropped alot. I agree that more stiffners might help the > >problem. Thanks for your comments on strobes. Bob Skinner > > > > > > I mentioned the use of turndowns on the exhaust at our last builders meeting > and the response was one of hesitation. The concern is that the turndown > will cause a significant upward thrust on the end of the exhaust placing a > tourque on the exhaust pipes. Is this a concern or are the exhaust pipes > secured in such a way as to compensate for this? > I remember a past post noting that turndowns were not availible for some > engine/exhaust combinations. Is this true? > > ---------------------------------------------------------------------------- > ------------------------------------- > ---------------------------------------------------------------------------- > ------------------------------------- > Ross Mickey Phone: 541-342-1892 > 2300 Oakmont Way #205 Fax: 541-342-5492 > Eugene, Oregon 97401 email: rmickey(at)ix.netcom.com I have the vetterman exhaust crossover with the turn downs and get the vibration in the floor--not severe but you hear it if you lift both feet off the floor at the same time--I plan to try some of the sound deadning foam with the aluminum backing, and carpet over that. It seems slight enough that it is not noticable except when feet are lifted so hope it will work--report later. ________________________________________________________________________________
Date: Jun 12, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Belly Vibrations
>Bob; >Could I bother you for an elaboration on these turn down tubes? Are they >like the exhaust ext we use to put on our hot rods, chrome etc? Or are they >something that is welded on etc.? >John D John, They are stainless and they are welded on. I saw Larry Vetterman at Boone and he said that he has been shipping new cross-overs with the turn downs already bent. The reason he didn't originally put the turn downs on was so you had a lot more latitude on positioning the pipes because of the ball joint. I assume that with the turn downs already bent in the pipes that the range of positioning (so when you're done, the turn downs point straight down) is somewhat limited but I don't forsee that being a problem on a new installation. On a retrofit, as my installation was, having "weld-on" turn downs might be an advantage because of easier retrofitting to existing mounting (to engine) hardware. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 12, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Exhaust Turndowns
>I mentioned the use of turndowns on the exhaust at our last builders meeting >and the response was one of hesitation. The concern is that the turndown >will cause a significant upward thrust on the end of the exhaust placing a >tourque on the exhaust pipes. Is this a concern or are the exhaust pipes >secured in such a way as to compensate for this? >I remember a past post noting that turndowns were not availible for some >engine/exhaust combinations. Is this true? --------------------------------- >Ross Mickey Phone: 541-342-1892 Ross, The pipes (at least mine) are secured in such a way that this shouldn't be a concern. Let me tell ya, there is a BIG difference in noise level. With out the turn downs, I don't think even a Bose headset would quiet things down enough. Before I installed the turn downs, I was wearing ear plugs under my Telex 4000 ANR and it was still loud. Also, exhaust pulses from straight pipes might contribute to belly pan vibration and loose rivets. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
From: jpl(at)showpg.mn.org (Joe Larson)
Subject: Re: Sensenich Re-Pitch
Date: Jun 12, 1996
Gang -- If I remember correctly, Van's is very concerned about the safety of repitched props. The original manufacturer did NOT design them to be repitched, so the likelihood of cracking goes up. Please -- talk to an expert before you do this -- someone who ISN'T involved in the repitching business. We don't want any props breaking. Note that just because one person flew for 300 hours on a repitched prop doesn't mean the next person who tries it will be so lucky. Maybe I'm mistaken, but I'm pretty sure Van's opinion is Don't Do It. Maybe that's changed. -Joe -- Joe Larson jpl(at)showpg.mn.org 612-591-1037 Showpage Software, Inc. http://www.wavefront.com/~showpg 6121 St. Croix Ave. N. Golden Valley, Mn 55422 Future RV-6A pilot. ________________________________________________________________________________
From: jpl(at)showpg.mn.org (Joe Larson)
Subject: Engine oil consumption
Date: Jun 12, 1996
> I really hesitate to tear into the engine now as it > uses no oil, compression is good, etc. > Thanks, Bob Skinner Okay. Here I am possibly mis-remembering something I just read. And maybe your term "no oil" meant "the right amount of oil". A recent Kitplanes, if I'm not mistaken, had an article about engine oil usage. I got the impression the engine is supposed to consume a small amount of oil or it's not being lubricated properly. The rings might be too tight and wearing badly. Can someone more knowledgeable comment? -Joe -- Joe Larson jpl(at)showpg.mn.org 612-591-1037 Showpage Software, Inc. http://www.wavefront.com/~showpg 6121 St. Croix Ave. N. Golden Valley, Mn 55422 Future RV-6A pilot. ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Jun 12, 1996
Subject: Re: of carb jetting and CHT's
There was a post asking what engine that I have in my aircraft. I have a 160 HP 0-320 turning a three bladed Performance prop. Gary Corde RV-6 N211GC ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Jun 12, 1996
Subject: Re: Exhaust Turndowns
Larry Vetterman sells the turn downs for his exhaust system for $25 (including shipping) for the pair. The are SS. As far as the downturns putting pressure on the exhaust system, the tail pipes are secured by brackets and the ball joint (on the cross-over system) is made to move freely so I would not worry about cracks. Gary Corde RV-6 N211GC ________________________________________________________________________________
Date: Jun 12, 1996
From: "Dan and Myrna Toupal" <DMToupal(at)msn.com>
Subject: My Dad Can Beat Up Your Dad
---------- From: owner-rv-list(at)matronics.com on behalf of Mike Kukulski Sent: Sunday, June 09, 1996 9:00 AM Subject: RV-List: My Dad Can Beat Up Your Dad Can't we all just get along . . . Recent thread: >>Of course you could move to Australia and "import" your quality of life - >> >what's a little shipping charge anyway! >> >-Elon >> > >> >> Elon, no offence intended but some of us who live in small nations and not >> the U.S. actually like it that way and consider the occasional shipping >> charge worth it. >> >> I don't want to get a patriotic shouting match going here but that attitude >> of some americans that the rest of the world is some how inferior is very >> annoying. The US has its major advantages and major disadvantages just like >> any other country including mine. >> As a resident of an even smaller country (Trinidad)I feel that >I have to join in and support ! I don't think that Americans realise >just >how offensive their assumption that everything American is necessarily >better >can be. Too many don't even know where Trinidad is ! Mike Kukulski (kukulski(at)indirect.com) RV-4 N96MK ________________________________________________________________________________
From: rmickey(at)ix.netcom.com
Date: Jun 12, 1996
Subject: Re: Faying compound
>Hi, > >I had not questioned this issue before, but in my 9 years in the airforce >we were always required to use faying compound between riveted joints. What >is it? well - we used a yellow chromate type paste. I guess its a bit like >gasket cement on cars, but its never supposed to harden. > >The maintenance manuals I have for military aircraft all require the use of >a faying compound. > >I have not been using it on my RV6, although I am now wondering whether I >would be better off using it? > >Regards >Mike Parkinson >RV6 HS Mike, I would like to put something between the firewall and fuselage skins just to seal it better from the engine compartment. Tom at Vans said to use proseal. I mentioned this on the list a while back and their were some who didn't think it was a good idea, concerns with weakening the joint. If you know of another product available to us civilian types, please let me know. Ross Mickey rmickey(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 12, 1996
From: Ron Caldwell <74504.1365(at)CompuServe.COM>
Subject: Wing Jig and Brackets
HooRay: My RV6A Empennage is all completed and I'm ready to get started on my Wing Kit (which is scheduled to be delivered any day now). I plan to build both wings at the same time. I will installed two more vertical 4x4 posts about 4 foot apart from my existing tail jig. What size angle iron for the brackets are required? 1/8'' or 1/4" or greater thickness? My empennage jig vertical posts are 109" apart. Is this distance OK? Any other suggestions for the Wing Jigs that I should consider. Thanks in advance for you help. Ron Caldwell RV6A (Tail Completed) 74504.1365(at)compuserve.com ________________________________________________________________________________
Date: Jun 12, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Engine oil consumption
>Okay. Here I am possibly mis-remembering something I just read. And maybe >your term "no oil" meant "the right amount of oil". A recent Kitplanes, if >I'm not mistaken, had an article about engine oil usage. I got the impression >the engine is supposed to consume a small amount of oil or it's not being >lubricated properly. The rings might be too tight and wearing badly. > >Can someone more knowledgeable comment? > >-Joe Sorry, Joe. Poor wording on my part. More properly stated: Engine oil consumption is OK. My O-320 burns 1 quart/16-18 hours. I read the same article, can't remember where. It said that really low oil consumption is not something to brag about as it is an indication that the cylinders are not receiving the proper amount of oil and therfore cylinder life would be reduced. BTW, the Lycoming manual says the maximum oil consumption at 75% power for O-320-E&A engines is .37 qts/hour. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 12, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Sensenich Re-Pitch
>If I remember correctly, Van's is very concerned about the safety of >repitched props. The original manufacturer did NOT design them to be >repitched, so the likelihood of cracking goes up. > >Please -- talk to an expert before you do this -- someone who ISN'T >involved in the repitching business. We don't want any props breaking. >Note that just because one person flew for 300 hours on a repitched >prop doesn't mean the next person who tries it will be so lucky. > >Maybe I'm mistaken, but I'm pretty sure Van's opinion is Don't Do It. >Maybe that's changed. > >-Joe Joe, You are correct when the above applies to factory props designed for Cherokees, Cesnas, etc. when they have been cut down (below minimum diameter as specified by the manufacture) and re-pitched. I wouldn't touch one of these props with a 10 foot pole. The Sensenich prop designed for the RV can be re-pitched as, I assume most fixed pitch metal props can be, as long as you stay within the limits set by the manufacturer. There are limits on the amount of re-pitching that can be done, even on this prop. Also, there is a minimum diameter on the CM70 prop which I believe is 68". Sensenich has the appropriate data (stations, maximum amount of pitche that can be removed or added, etc.) and templates available and the prop shop had all of this material. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Subject: Re: Preserving Engines
Date: Jun 12, 1996
From: "Calin Brabandt" <cwbraban(at)ichips.intel.com>
Regarding engine storage, Richard Chandler inquires: > > I think I paid about $25 / gallon for the oil so the total price > > of storage was a little over $100 with the plugs. > > Couldn't you do the same thing with something cheaper, like Kerosene? Engine oil would have been much cheaper too, but considering that I'm risking the better part of $20K, I decided the storage oil money wasn't significant. The stuff is designed for this application. I was concerned that if there were any air pockets, the oil would eventually shed or run off. If you're absolutely sure no bubbles are in there, anything that doesn't attack seals would probably be okay, but this stuff is supposed to really cling! Also, it doesn't wear out and I'm sure I can drain it and sell it to recoup at least some of my investment when I'm nearly ready to fly. Cal ________________________________________________________________________________
From: "David Drew" <noeldrew(at)iafrica.com>
Date: Jun 12, 1996
Subject: Re: Belly Vibrations
> Date: Tue, 11 Jun 1996 13:37:27 -0700 > From: edt.com!randall(at)matronics.com (Randall Henderson) > To: rv-list(at)matronics.com > Subject: Re: RV-List: Belly Vibrations > Reply-to: rv-list(at)matronics.com > I've had the guys from Van's over a few times looking over my fuselage > and they were talking about this very issue, and recommended an .040 > aluminum sub-floor over the stiffeners, attached to the stiffeners > somehow, with insulation underneath. > > Mike Seager is doing something similar on his current RV-6. He replaced > the two outer stiffeners with 3/4" deep by 1 1/2" wide "U" channels, > (custom made) and intends to pop-rivet the sub-floor directly to those. > ______ ________________________________________________________________________________
Date: Jun 12, 1996
From: Phil Arter <arter(at)ncar.ucar.edu>
Subject: Re: Faying compound
> >Mike, > >I would like to put something between the firewall and fuselage skins just >to seal it better from the engine compartment. Tom at Vans said to use >proseal. I mentioned this on the list a while back and their were some who >didn't think it was a good idea, concerns with weakening the joint. If you >know of another product available to us civilian types, please let me know. > > >Ross Mickey >rmickey(at)ix.netcom.com > > Ross, The warning about indiscriminantly using Proseal on joints was mine and seems to have led to some confusion for which I am sorry. What I meant was: When diverging from the plans, especially in the area of joints in the primary structure, it would be a good idea to consult with Van's first, because there may be some effect that isn't forseen. I don't know if a Prosealed joint is stronger or weaker than one without it. If Tom said the firewall would be an appropriate place to use Proseal, then go for it. Phil arter(at)ncar.ucar.edu ________________________________________________________________________________
Date: Jun 12, 1996
From: Ron Caldwell <74504.1365(at)CompuServe.COM>
Subject: Porterville CA Fly-In
This weekend is the Porterville CA Fly-in (June 14-15). Van's will be there with his RV4 and RV8. He's on the Airshow schedule to perform aerobatics in his RV4. I will be flying from Salt Lake in my Cherokee to attend the Fly-In. Is anyone else from the RV-List planning to attend?? I would like to meet up with you and chatt about our RV building experiences. Ron Caldwell RV6A Ready to Start the Wings 74504.1365(at)compuserve.com ________________________________________________________________________________
From: rmickey(at)ix.netcom.com
Date: Jun 12, 1996
Subject: Re: Belly Vibrations
>Do you think adding some 3/4x3/4 angle in between the existing stiffeners >would be a good idea? It couldn't weigh that much. >Mal rvbildr(at)juno.com > We had this discussion on the List in March. It started with Pter saying he was installing toolboxes under your knees. I am attaching to the bottom of this the parts of the thread I saved. You can also look at the archices for more. I am going to install a piece of angle on each of the two centermost stiffeners from the top of the spar to about 7" in front of the spar. Ross Mickey rmickey(at)ix.netcom.com > Peter, > > This sounds like a good idea. Could you share some specifics? What is a > "triangular section"? Between which floor stiffeners? Will it tie into the > firewalll? Will the top of the box be a hinged lid flush with the floor? > When you say "bolted to the spar" are you going to use the existing holes > throuh the spar and use longer bolts? > > Much thanks> Ross, The idea came from Bill Benedict who said others had done it, although I got no details from him. I plan to make triangular "ribs" which have a flange bolted top and bottom to the spar with longer bolts, with the lower side of the web rivetted to the vertical web of the floor stiffener to a distance about 7 inches forward of the spar, and with a flange on the sloping side (hypotenuse) which is about parallel to your lower leg when you are seated. The toolbox therefore sits under your knees/calves in an otherwise dead space. the floor stiffeners are cantilevered forward which really stiffens up the floor. Access will be by hinged panel on the sloping face. The "ribs" will have the biggest possible lightening holes and the stored tools wrapped in foam. BTW, Gil Alexander pointed out there are brackets holding the stiffeners to the spar. Anyone else miss them???? Peter Bennett > Thanks for the description. I called Bill today to get some more details, > and he couldn't remember any. I did mention to him that I was interested > in installing this toolbox to stiffen up the belly pan to try to change the > resonence frequency. He said he didn't think this would do much as the > vibration is mainly "under your feet" and stiffening back near the spar may > not do much. > I DISAGREE. I STARTED BY TRYING TO GET A SUPPORT INTO THE MIDDLE OF THE DRUMMING AREA. I DISCUSSED WITH LEO DAVIES A LATERAL STIFFENER FROM LONGERONS TO CENTRE. HE HAS GONE AHEAD AND DONE THIS AS HE INDICATED IN A RECENT POST. I CONTINUED EXPERIMENTING AND FOUND THAT A PIECE OF .063 ANGLE FROM THE TOP OF THE SPAR TO A POINT 7 - 8 INCHES FORWARD ON THE STIFFENER MAKES ONE HELLUVA DIFFERENCE. NOW THAT I HAVE FOUND F699, THE PIECE OF ANGLE MAKES A RIGID TRIANGLE WITH SPAR AND STIFFENER AND THE NEED FOR THE TOOLBOX BULKHEADS OR RIBS IS ELIMINATED. > I am building a 6A. The gear leg takes up the space under the outside knee > which precludes putting a box between the outside longeron and first > stiffener. That leaves the options of > 1) building two, 7 inch wide toolboxes between the middle stifeners and the > one to the ouside, or 2) building one 8 inch wide toolbox between the middel > two stiffeners or > 3) building one 22 inch wide toolbox spanning all four floor stiffeners > > If you are building a 6, you would also have the options associated with > using the 7 inch space between the longeron and first floor stiffener. > Which option are you leaning towards? > I INTEND TO HAVE TWO BOXES STARTING AT THE LONGERONS AND LEAVING 8" BETWEEN THEIR INNER ENDS. CHECK THE ROOM NEEDED TO WITHDRAW THE BATTERY BOX COVER. > You mentioned "The "ribs" will have the biggest possible lightening holes > and the stored tools wrapped in foam." Does this refer to the inside ribs > (if you will have any) or the outside ribs which form the outside of the box? > INSIDE RIBS, EXCEPT NOW THEY ARE NOT NEEDED. > Do you plan on running a 3/4" or 1" angle width wise spanning between the > longerons or between the stiffeners at the "nose" of the toolbox? > HAVEN'T THOUGHT THIS THROUGH YET, I'D LIKE TO PUT SOMETHING THERE TO TAKE PIANO HINGE SO THE WHOLE FRONT CAN OPEN AND BE REMOVED. > Thanks for your thoughts. Peter Bennett ________________________________________________________________________________
Date: Jun 13, 1996
From: John Morrissey <John.Morrissey(at)its.csiro.au>
Subject: Re: New member of the list (Chatter - humor)
Oh my God NO!! not a Volvo in the air!!! Having been run over twice by Volvo drivers (who have a particullarly bad reputation for poor driving here in Australia1) The thought of a sky full of Volvo drivers fills me with terror!! :-) An RV with a crash crumple zone?? Welcome to the list!! How much did the installation cost?? how many hours has it run?? what sort of problems have they encountered with the engine? John Morrissey > >I am hoping to build an rv6 in time, in that respect I am wondering if any >of you have heard anyting about putting a Volvo engine in a rv? > >There are these swedish guys who have put the 6cylinder version of a >960Volvo engine in a Piper Pony, it has been running for some time now >pulling gliders with a 4 bladed prop and silencer, nice and quiet! > >I recently heard that someone has put a Volvo engine in an rv, probably >the 5 cylinder version of the same engine, but that's all I have heard. > >Finn Egil Grimnes > > > ________________________________________________________________________________
From: Mickey Baker <mbaker(at)gate.net>
Subject: Re: c214 squeezer for sale
Date: Jun 12, 1996
I'll take it, but will not be back in town until the 21st, so you might want to delay mailing it a few days. Mickey Baker Sage Research Corporation 2652 NE 3rd Street Pompano Beach, FL 33062 Phone 305 785-2354 > > I have a rebuilt CP 214 for sale standard yoke 1 1/2" with 2 flush sets and > #40 #30 #20 cupped sets. price $250.00 COD. The last ones I had for sale > went in two days. If you need one this is a terrific deal. First email gets > it please contact me at HPair(at)ix.netcom.com > harry Paine > ________________________________________________________________________________
From: WStucklen(at)aol.com
Date: Jun 12, 1996
Subject: Re: Belly Vibrations
> *** SNIP *** >My intention is to use 3/4" angle screw/nut-plated or riveted to the >existing channel, and use nut plates/screws to screw the subfloor to >those pieces. > >Randall Henderson >RV-6 Randall: I,ve done this in my aircrarft, including the installation of 1/2" closed cell foam rubber between the top floor skin and the original belly skin. I also have a rug on top. The noise level is down conserably. Take-off and cruise cockpit noise levels are no worst than most other Piper or Cessna models. I have the Tolle exhaust system with the turned down ends and that helps. I did measure the noise levels at about 95 dB at one time, but that was way back when I was doing the 40 hr test period. I still have a few belly rivets that are smoking and need to be fixed soon. Except for the occational roll, I don't do aerobatics, so the majority of the stresses are from normal flying. The additional cockpit top floor and insulation may have kept this to a minimum. Fred Stucklen RV-6A N925RV (realy like the electric flaps!) wstucklen(at)aol.com ________________________________________________________________________________
Date: Jun 12, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Faying compound
I used some high-temp RTV gasket material I got at an auto parts store to seal around the firewall recess and edges. But after riveting, I found the stuff came off pretty easily. Apparently what I had wasn't quite the same as the "high-temp RTV" that most people use, which seems to stick better. I scraped off as much as I could around the joints and out of the seams, then smeared pro-seal all in there best I could. Now I wish I had just gone with something I KNOW will stick in the first place. Proseal is pretty heat resistant anyway as I recall, even though it's not advertised as "high-temp". And it's mainly there to keep exhaust gasses out of the cockpit, not to protect you from a real fire. Randall ________________________________________________________________________________
From: BARNES_ERIC(at)Tandem.COM
Date: Jun 12, 1996
Subject: Homebuilt Marker Beacon/Smoke System
A couple people had asked for infor on the following, and I just got around to digging last night... Homebuilt Marker Beacon - Sept. '93 KITPLANES pg.46 For the Smoke System, January '96 Kitplanes had an article on the "Dawn Patrol" (Dick Starks), which highlighted the set-up they installed. Hope this helps. Eric Barnes_Eric(at)tandem.com ________________________________________________________________________________
Date: Jun 12, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: User Fees
I'm curious as to how effective it is to post things about political issues such as the recent "AOPA Alert" regarding the Aviation Trust fund and User Fees. If you saw my posting, and wrote to your senator as a result, could you drop me a _private_ e-mail please? Thanks. Randall Henderson randall(at)edt.com ________________________________________________________________________________
From: DMusgrave(at)swri.edu
Date: Jun 12, 1996
Subject: Wiring Grommets
charset=US-ASCII lawyernet.com!rwoodard(at)matronics.com Wrote: | A couple of us RV-8 builders are to the point where we need to install | elastic grommets in the VS and HS ribs to provide for lighting, | communication and navigation antenna and wires. We've found AN931 | Elastic Grommets for sale on page 102 of the most recent AS catalog. | Can anyone give advice as to which grommets we need and how many? I just received short form catalog 26 from micro plastics, Flippin, AR 72634 (501) 453-2261. They make every kind and size of grommet for this application. You have to buy a jillion, but they only cost pennies apiece. Check it out! Dave Musgrave ________________________________________________________________________________
From: Terryg(at)SceptreCal.CCMAIL.CompuServe.COM
Date: Jun 12, 1996
Subject: FW: VS Tip Attach
'Listers -- due to some unfortunate trimming errors, I have wound up with a VS skin that is a little short on the top. More precisely, I have wound up with the skin extending past the tip rib by about 1/4 to 5/16", instead of the designated 1/2". In thinking about this for a while, I've come up with a couple of ideas. 1) The rivets attaching the VS tip are shown a 1/4" back from the top of the VS. I can still do that with mine, although I'll end up nicking the edge of the flange of the tip rib. Also, I'll have to modify the flange a little on the tip itself. 2) I can attach a nut plate behind each of the two tooling holes in the tip rib, and again, with a few minor changes to the tip itself, screw the tip on with two bolts into these nutplates. I'll have to make sure that they can seal though, so that they don't permit water to enter the VS. Of the two, I'm leaning toward the latter. Looks like I'm going to want to get that tip off, anyway, as there may well be antennae/strobe stuff in there that I want to get at. Any thoughts on the above, or the situation in general, I would most appreciate! Cheers... Terry in Calgary "Skinning VS" ________________________________________________________________________________
From: BrabstonD(at)aol.com
Date: Jun 12, 1996
Subject: RV6 Wing Spars
Most of you have probably been here, but for you guys just starting your wings, this may be worth while. I prepared the 1/8th and 1/4 inch flange strips according to instructions. Then I primed all those parts with epoxy primer--per instructions. Then I tried to assemble the parts according to instructions. When I put the flange strips together and tried to "S-L-I-D-E" those 3/8, 1/4, and 3/16 inch bolts into the holes to align everything I discovered that the bolts would not fit. After a lot of reading and studying, I concluded that the first 18 holes, starting with the first 1/4 inch bold, are underdrilled and tapped for a "close tollerance fit." When I primed the spar strips, I got primer in the holes and the primer made the holes too small for the bolds to fit. To solve the problem I have spent hours using 400 grit sand paper wrapped around approperatly sized round objects to get the primer out without enlarging the holes. If I had it to do other, I would roll up pieces of paper and stick them in the holes before I started priming. Maybe someone has a better solution--or am I the only one that had this problem. By the way, I've heard that it is a good idea to paint the bolts with primer and dirve them in wet when you get ready to install the wings. Anyone know about that? ________________________________________________________________________________
Date: Jun 12, 1996
From: "Richard Chandler" <mauser(at)Claris.COM>
Subject: Re: New member of the list (Chatter - humor)
> An RV with a crash crumple zone?? As an aside, on rec.motorcycles Volvo drivers have a similar rep. But one of the more interesting comments I've read about crumple zones was from a guy who got broadsided on his old Range Rover. It was to the effect that Range Rover engineers had found the perfect location for crumple zones - on the other guy's car. The accident totalled the other guy, but an hour with a hammer could pound out the dents in the Rover. -- "Wait a minute, you expect us innocent children to climb up dangerous scaffolding and paint naked people all over a church? We'll do it!!" -- Yakko Warner, Animaniacs "Yeah, I've got ADD, you wanna make something of.... oooh, cool. Look!" ________________________________________________________________________________
Date: Jun 12, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: RV6 Wing Spars
>objects to get the primer out without enlarging the holes. If I had it to do >other, I would roll up pieces of paper and stick them in the holes before I >started priming. Maybe someone has a better solution--or am I the only one >that had this problem. By the way, I've heard that it is a good idea to >paint the bolts with primer and dirve them in wet when you get ready to >install the wings. Anyone know about that? Considering that the holes drilled for the close tolerance bolts provide a tight enough fit to rub some cad plating off of the bolts, I wouldn't think that primer would stay on the bolts when inserted. I used Boeshield T-9 corrosion protectant (ACS) on my close tolerance bolts as it was recommended by a mechanic I have high regard for, however, it probably didn't stick to the bolt any better than the primer. It made me feel better, anyway. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
From: dralle (Matt G. Dralle 510-606-1001)
Date: Jun 12, 1996
Subject: Compuserve Members...
[RV-Listers: Below is a message I just emailed to Compuserve regarding their Internet emailer. I'm sure it'll hit their bit bucket before anyone there cares, but maybe something will be done. If you are a subscriber to Compuserve, please send them a message similar to mine asking that they modify their mailer. I sent my message to: "POSTMASTER(at)CompuServe.COM" and "support(at)compuserve.com" - Matt] ------------------------------------------------------------------------------ Compuserve Sys Admins: I run an Internet Email List with over 500 subscribers. Traffic on this list is over 30 messages per day. Below is a copy of one of the messages along with a message from the Compuserve Mailer. Note that this error message went to *ALL* 500 members of the List and was appened to the 21Mb archive file. People, *NO BODY* on the List cares that this person's mail box is full, and the huge archive file *really* doesn't need this crap making it that much larger. There a number of things to note here: 1) The "From " (note the lack of a ':') line is "owner-rv-list@...". Traditional mailers are suppose to use this address to send errors to, not the "From:" line. 2) Note the "Errors-To:" line address. Why are you sending errors back to the 'from' address when there is an Errors-To line??? 3) Note the "Precedence: bulk" line. If the precedence is "bulk" people, it means that its from an email list or something of similar nature and you *NEVER* send informational errors back. With 500 people on the List, I get a *LOT* of pissed-off-email when one of your addresses fills everyones email box with these 'mail box full' messages. Please fix your mailer. The Internet is too crowed and clogged already. Please don't dog it down more with these useless and unnecessary messages. Please respond. Matt Dralle Matronics dralle(at)matronics.com >-------------- >Your message could not be delivered for the following reason: > >Mailbox 70224.624 is currently full. >Please resend your message at a later time. > >--- Returned message --- > >From owner-rv-list(at)matronics.com >Received: from netcomsv.netcom.com (uucp9.netcom.com [163.179.3.9]) by arl-img-1.compuserve.com (8.6.10/5.950515) >Received: from matronics.com by netcomsv.netcom.com with UUCP (8.6.12/SMI-4.1) >Received: by matronics.com (4.1/SMI-4.1) >Errors-To: bounces(at)matronics.com >Date: Wed, 12 Jun 1996 16:33:03 -0700 >From: randall(at)edt.com (Randall Henderson) >Message-Id: <199606122333.QAA03829(at)amelia.edt.com> >To: rv-list(at)matronics.com >Subject: Re: RV-List: Faying compound >Mime-Version: 1.0 >Content-Type: text/plain; charset=us-ascii >Content-Transfer-Encoding: 7bit >Content-Md5: bE0ybaBu8+BCbYiwUW+y9g== >Sender: owner-rv-list(at)matronics.com >Precedence: bulk >Reply-To: rv-list(at)matronics.com > >I used some high-temp RTV gasket material I got at an auto parts store >to seal around the firewall recess and edges. But after riveting, I >found the stuff came off pretty easily. Apparently what I had wasn't >quite the same as the "high-temp RTV" that most people use, which seems >to stick better. I scraped off as much as I could around the joints and >out of the seams, then smeared pro-seal all in there best I could. > >Now I wish I had just gone with something I KNOW will stick in the first >place. Proseal is pretty heat resistant anyway as I recall, even though >it's not advertised as "high-temp". And it's mainly there to keep exhaust >gasses out of the cockpit, not to protect you from a real fire. > >Randall > >-------------- -- Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94550 510-606-1001 Voice | 510-606-6281 FAX | dralle(at)matronics.com Email http://www.matronics.com/ W.W.W. | Featuring Products For Aircraft ________________________________________________________________________________
From: jpl(at)showpg.mn.org (Joe Larson)
Subject: A suggestion for the elevators
Date: Jun 12, 1996
I was just fitting my elevators to my HS so that I could weigh the amount of load I needed in the counterbalance. (I didn't have the *slightest* intention of setting up the tail feathers on the desk, setting a chair in front facing away, and making vroom-vroom, rat-a-tat-tat noises! No, not me!) I discovered a slight fitting problem that I want to warn people about so they don't have this problem. As you can figure out, the counterbalance arms will bind if they are angled into the HS at all. Well, one of mine is pretty good, but the other one is too tight. Sigh. The only way I can fix it now is to remove some material, or build it again. (I'm going to remove the material). A method to avoid this problem -- after you've drilled the elevator skin to the skeleton, but before you have drilled the holes into the tip ribs, clamp the tip ribs and skin with cleco side clamps, take it all out of the jig, and fit it to the HS. You'll probably find that the skins are in the way a little bit, as you haven't formed the leading edge bend yet, but should be able to find some method of making sure everything matches. I was extremely careful to get things square. Obviously not *quite* careful enough. You only have to be off a degree or so to have a problem. Another suggestion -- when you are making your elevator skeleton, don't be too tight when locating the holes for the rod ends. The tips of the elevators must extend past the tips of the HS, but everything just has to be close at the middle. Don't be *too* sloppy, of course, but I've got about a 16th on the good end, and I think I would be happier with twice that. -Joe -- Joe Larson jpl(at)showpg.mn.org 612-591-1037 Showpage Software, Inc. http://www.wavefront.com/~showpg 6121 St. Croix Ave. N. Golden Valley, Mn 55422 Future RV-6A pilot. ________________________________________________________________________________
From: EBundy2620(at)aol.com
Date: Jun 12, 1996
Subject: Fuel primer solenoid
A while back someone mentioned an electric fuel primer solenoid. Can someone give me a contact to obtain one of these? Thanks, Ed Bundy (hooking up engine guts) ebundy2620(at)aol.com ________________________________________________________________________________
Date: Jun 12, 1996
From: Curt Reimer <Curt_Reimer(at)MBnet.MB.CA>
Subject: Re: Faying compound
On Wed, 12 Jun 1996, Phil Arter wrote: > The warning about indiscriminantly using Proseal on joints was mine and > seems to have led to some confusion for which I am sorry. > > What I meant was: When diverging from the plans, especially in the area of > joints in the primary structure, it would be a good idea to consult with > Van's first, because there may be some effect that isn't forseen. I don't > know if a Prosealed joint is stronger or weaker than one without it. > > If Tom said the firewall would be an appropriate place to use Proseal, then > go for it. Bear in mind that you don't have to put it on the faying surfaces. I deliberatly didn't and just plan to run a bead of it to seal the joints after they are riveted. Then you have a sealed firewall and no worries. Curt Reimer ________________________________________________________________________________
Date: Jun 12, 1996
From: Curt Reimer <Curt_Reimer(at)MBnet.MB.CA>
Subject: Re: RV6 Wing Spars
On Wed, 12 Jun 1996 BrabstonD(at)aol.com wrote: > holes too small for the bolds to fit. To solve the problem I have spent > hours using 400 grit sand paper wrapped around approperatly sized round > objects to get the primer out without enlarging the holes. If I had it to do > other, I would roll up pieces of paper and stick them in the holes before I > started priming. Maybe someone has a better solution--or am I the only one > that had this problem. By the way, I've heard that it is a good idea to > paint the bolts with primer and dirve them in wet when you get ready to > install the wings. Anyone know about that? I had the same problem and had to ream out the holes after the spar was assembled. The rolled up paper idea is a really good one. I learned my lesson. On most other parts, getting primer in the holes is no big deal because you can just run a drill bit through them later, but with machined or close tolerence holes, an ounce of prevention is worth a pound of cure! I agree with the "install bolts wet with primer" idea. I think this is standard practice, so I do it. But, I don't use epoxy primer for this, although I use it everywhere else. I just use zinc chromate out of a can. I think with epoxy, you'd have a heck of a time ever getting the bolts out again. Curt Reimer ________________________________________________________________________________
Date: Jun 12, 1996
From: Curt Reimer <Curt_Reimer(at)MBnet.MB.CA>
Subject: Re: Gascolators
> > The argument is that gascolators is 1930's tractor technology. How many do > > you see on cars these days? There is debate in this neck of the forest > > whether we need them (appologies to our Canadian brethren as they are > > required). I know some who have put the inline glass filters under the So it's 1930s technology. So what? Is there a better, more modern way of removing water from your fuel? If so what is it? If not, what the heck is wrong with 1930s technology? Aluminum monococque airframe design (like RVs use) is also 1930s technology. So what? If it works, it works. Curt Reimer Disgruntled Canadian Who Has to Use a Gascolator Anyway ________________________________________________________________________________
Date: Jun 12, 1996
From: Jeremy <jbenedic(at)hood.uofport.edu>
Subject: Merced/Bakersfield RV Report
Just in case anybody wanted to know, there were quite a few RV's at the Merced Fly-In last weekend. My best count was 43, although a few more could have slipped by. I only know of one who was an rv-lister though. At Bakersfield, there were RV's everywhere, on the ground and in the air. Unfortunately, it was too HOT to actually go out and count the number of airplanes, but a rough glance showed between 40 and 50. And if you really want to know, at Merced: RV-3: 2 RV-4: 20 RV-6: 18 RV-6A: 2 RV-8: 1 And if you really, really want to know, at Merced: RV-3 RV-4 RV-6 RV-6A RV-8 ------ ------ ------ ------ ------ N13KE N32KL N91CK N567RV N118RV unknown N320TD N4246 N164RS N444ED N181R N320A N826B N426RC N66RV N77GR N906GS N9180T N974JS N22954 N14JA N835B N146RV no-N # N946DP N186RR N695LS N4WJ N64DR [HR]N67CW N595BP N504JT N1KJ N44TK N6HJ [HR]N280HR N164CE N22KP N419D N98GB N49ZZ N344H N888TH ----------------------------------------------------------------------- | name://Jeremy Benedict | PP-ASEL (1994) [R/E: TD] | | email://jbenedic(at)uofport.edu | Logged:C-150,RV-4,-6,-6A,-6B,-6T| | http://www.uofport.edu/~jbenedic | TT: 188.2 hrs TT-RV: 95.2 hrs | | voice://503.240.1062 | | ----------------------------------------------------------------------- ________________________________________________________________________________
Date: Jun 12, 1996
From: Jerry Springer <jerryflyrv(at)village.yvv.com>
Subject: Re: A suggestion for the elevators
Joe Larson wrote: > *snip* > > I discovered a slight fitting problem that I want to warn people about so > they don't have this problem. As you can figure out, the counterbalance > arms will bind if they are angled into the HS at all. Well, one of mine is > pretty good, but the other one is too tight. Sigh. The only way I can fix > it now is to remove some material, or build it again. (I'm going to remove > the material). > > A method to avoid this problem -- after you've drilled the elevator skin to > the skeleton, but before you have drilled the holes into the tip ribs, clamp > the tip ribs and skin with cleco side clamps, take it all out of the jig, > and fit it to the HS. You'll probably find that the skins are in the way a > little bit, as you haven't formed the leading edge bend yet, but should be > able to find some method of making sure everything matches. > > I was extremely careful to get things square. Obviously not *quite* careful > enough. You only have to be off a degree or so to have a problem. > > Another suggestion -- when you are making your elevator skeleton, don't be > too tight when locating the holes for the rod ends. The tips of the elevators > must extend past the tips of the HS, but everything just has to be close at > the middle. Don't be *too* sloppy, of course, but I've got about a 16th on > the good end, and I think I would be happier with twice that. > > -Joe > > -- > Joe Larson jpl(at)showpg.mn.org 612-591-1037 > Showpage Software, Inc. http://www.wavefront.com/~showpg > 6121 St. Croix Ave. N. > Golden Valley, Mn 55422 Future RV-6A pilot. Along the same line as Joe's post, when I flew to Merced this last Weekend I stopped at Willows, CA for fuel and there was a Piper PA-28 fueling up, when he taxied out to take off he could not move the elevator because the heat had expanded his elevators to the point that they were binding on the HS so he taxied back in and was working the surfaces over with a file to get clearence, something to think about when setting your elevator to HS clearence on the outboard ends. I think 1/8 to 1/4" is not to much. I had not seen this before and found it interesting. Temp on the ramp was about 100 degrees. Jerry Springer RV-6 first flight July 14, 1989 :-) jerryflyrv(at)village.yvv.com ________________________________________________________________________________
Date: Jun 12, 1996
From: Harry Paine <HPair(at)ix3.ix.netcom.com>
Subject: Re: c214 squeezer for sale
>I'll take it, but will not be back in town until the 21st, so you might want >to delay mailing it a few days. > >Mickey Baker >Sage Research Corporation >2652 NE 3rd Street >Pompano Beach, FL 33062 > >Phone 305 785-2354 > > >Mickey sorry you were caller # 7 However I might have some more in the future and if you would still be interested in the next couple of months let me know. Thanks Harry Paine > >> > > > ________________________________________________________________________________
From: Mlfred(at)aol.com
Date: Jun 13, 1996
Subject: Your address?
Harry Would you send me your snail-mail address? Rgds Mark ________________________________________________________________________________
Date: Jun 13, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Fuel primer solenoid
>A while back someone mentioned an electric fuel primer solenoid. Can someone >give me a contact to obtain one of these? >Thanks, >Ed Bundy (hooking up engine guts) Ed, Aircraft Spruce, page 135, 95-96 catalog, $35.50. Bob Skinner ________________________________________________________________________________
Date: Jun 13, 1996
From: "Robert L. Nuckolls, III" <72770.552(at)CompuServe.COM>
Subject: Fuel primer solenoid
---------- Forwarded Message ---------- From: INTERNET:EBundy2620(at)aol.com\ RE: RV-List: Fuel primer solenoid A while back someone mentioned an electric fuel primer solenoid. Can someone give me a contact to obtain one of these? Ed, I seem to recall that Aircraft Spruce has one in their latest catalog. I loaned mine out so I can't look for you right now. If you have trouble finding it, let me know. By the way, I got this sad looking fragment of an envelope back in the mail yesterday with your mailing lable on it. Post Office appologized and offered to look for the rest of the package if I would just fill out five forms in triplicate and . . . . . well . . . it wasn't that bad. The upshot is that I think some mail sorting machine ate you book. Glad we got the envelope back or we'd never know about until you hollered . . . a nice new one is in today's mail. Bob . . . AeroElectric Connection ________________________________________________________________________________
Date: Jun 13, 1996
From: PatK(at)gnn.com (Patrick Kelley)
Subject: Re: Wing Jig and Brackets
You wrote: >What size angle iron for the brackets are required? 1/8'' or 1/4" or greater >thickness? My empennage jig vertical posts are 109" apart. Is this >distance OK? Any other suggestions for the Wing Jigs that I should >consider. Thanks in advance for you help. You have plenty of time before you need the wing jig; the spars will be built off of it. After pulling my spars out of the box, I had a good idea of the weight and added a 'jigger factor' for the rest of the wing structure. I then went to the hardware store and got some of the steel angle for shelving (the kind with holes already drilled; looks kinda like erector set beams). For the spar supports, I cut them long enough to extend past both sides of the jig - I store the long stock on the back side. The rear spar supports are mostly for positioning the rear spar; they do not have to bear much weight. But I used the same material anyway because it was cheap enough. I also used it to attach the threaded rod that maintains tip rib alignment. A six foot length was sufficient for my single jig as described. 109" is fine - your main spar will fit comfortably on that distance. The rear spar will not reach, but a piece of flat stock bridges the gap just fine (remember, the rear spar is not supported, just positioned). I made one mistake: I put the spar supports on the face of the posts farthest from each other. The spars fit Ok, but the posts were in the way for drilling the skin to the tip rib, so I had to disassemble the structure and move the supports to the inside faces of the posts. Now I can reach the entire surface of the wing facing the jig. By the way, I also had to remove the crosspost as it interfered with access to the wing surface. I was afraid that this would weaken the lateral stability of my free-standing jig. My solution was to clamp the main spar in place before removing the crosspost. The main spar acts as a replacement crosspost and my jig has not moved at all. For you guys with floor to ceiling posts, this should not even be a problem. Hope all of this helps you. PatK - RV-6A - Left tank under construction (how I HATE pre-punched skins!!) PatK ________________________________________________________________________________
Date: Jun 13, 1996
From: PatK(at)gnn.com (Patrick Kelley)
Subject: Re: -8 arrives!
The empennage kit is small enough to be shipped UPS (pronounced OOPS!), but the remainder of the kits are too large and have to be shipped by common carrier. Also, (don't know if this is the current practice), my empennage arrived in cardboard(!) boxes. Sure could have used the wood crating to make jigs and such. Pertaining to the thread about trimming the stab skins, I advise trimming the root end (if necessary; mine overhangs about 1/8" - I don't think the weight savings is worth the effort to trim it), as trimming later you will find the spars interfering with your work. At the tips, leave it until later. I trimmed the aft portion when I fitted the elevators; trimming by measurement would not have worked because of small variences in the location of the elevator counterweights. I am saving the forward portion until I am ready to do the tips; a rough fitting has already shown me that I may need to vary from the measured line by about 1/16" at one end. (Up until this point, I thought I was being exceptionally precise. Small errors add up.) PatK - RV-6A - Still banging on those wing spars... PatK ________________________________________________________________________________
Date: Jun 13, 1996
From: PatK(at)gnn.com (Patrick Kelley)
Subject: Re: Trim Tab
You wrote: >Another question -- has anyone had any luck with the bend-over-the-tabs >method of constructing the trim tab, or is everyone pretty much agreed >that the best method is to make a couple of little ribs? I bent the tabs over; it worked just fine. IMHO, it's six of one or a half dozen of the other. I think both methods come out looking Ok, though I personally thought it was easier to do the tabs than try to design and fabricate riblets and rivet them in such close quarters. Others think I did it the hard way - it just goes to show you. :-) PatK - RV-6A - LE Skin fitting to the left wing PatK ________________________________________________________________________________
Date: Jun 13, 1996
From: Scott Gesele <scottg(at)villagenet.com>
Subject: Re: Fuel primer solenoid
>A while back someone mentioned an electric fuel primer solenoid. Can someone >give me a contact to obtain one of these? > >Thanks, >Ed Bundy (hooking up engine guts) >ebundy2620(at)aol.com > > Ed, I just ordered mine from Aircraft Spruce. It's in the fuel section. I think it's on the same page as the gascolators, let's not get THAT discussion started again :). Cost was about $35-$40 for the valve. I can't comment on it because it hasn't been received yet. -Scott N506RV engine and prop are hung :) scottg(at)villagenet.com ________________________________________________________________________________
Date: Jun 13, 1996
From: kingm(at)whidbey.net (Monte King)
Subject: Lubbock Builders?
My friend, Mark Myres, who is not on this list will be flying his beautiful new RV-6 to Lubbock to visit family next week. I offerred to see if I could round up anyone from the list interested in looking at his plane and possibly anyone who might have some hanger space to offer at the airport. He'll be arriving at Lubbock June 20 and leaving June 22. E-mail me directly if you're interested. Thanks. Monte King kingm(at)whidbey.net ________________________________________________________________________________
Date: Jun 13, 1996
From: csanchez(at)BayNetworks.com (Cheryl Sanchez)
Subject: Re: RV6 Wing Spars
> >Most of you have probably been here, but for you guys just starting your >wings, this may be worth while. I prepared the 1/8th and 1/4 inch flange >strips according to instructions. Then I primed all those parts with epoxy >primer--per instructions. Then I tried to assemble the parts according to >instructions. When I put the flange strips together and tried to "S-L-I-D-E" >those 3/8, 1/4, and 3/16 inch bolts into the holes to align everything I >discovered that the bolts would not fit. After a lot of reading and >studying, I concluded that the first 18 holes, starting with the first 1/4 >inch bold, are underdrilled and tapped for a "close tollerance fit." When I >primed the spar strips, I got primer in the holes and the primer made the >holes too small for the bolds to fit. To solve the problem I have spent >hours using 400 grit sand paper wrapped around approperatly sized round >objects to get the primer out without enlarging the holes. If I had it to do >other, I would roll up pieces of paper and stick them in the holes before I >started priming. Maybe someone has a better solution--or am I the only one >that had this problem. By the way, I've heard that it is a good idea to >paint the bolts with primer and dirve them in wet when you get ready to >install the wings. Anyone know about that? > BrabstonD (don't know your real name) Try a reamer. It is called for in the RV-3 manual. A reamer will cut a round hole of the correct diameter. The idea is to first drill the hole to be about 1/64" undersize and then ream. I did it on my spars and they came out great. The bolts would slide in like pistons in a cylinder. Cheryl Sanchez csanchez(at)world.std.com ________________________________________________________________________________
Date: Jun 13, 1996
From: joehine(at)mi.net (joehine)
Subject: Re: FW: VS Tip Attach
>'Listers -- due to some unfortunate trimming errors, I have wound up with a VS >skin that is a little short on the top. More precisely, I have wound up with >the skin extending past the tip rib by about 1/4 to 5/16", instead of the >designated 1/2". In thinking about this for a while, I've come up with a couple >of ideas. > Terry, Glue it on with proseal. You have to heat it and expand it a bit so it is a tight fit in the top of the VS. I masked the top of the VS and a line about 1/8 inch up the tip from the line the top of the VS would make and then spread proseal on the fiberglass and pressed it in place. I then took a popsical stick and make a nice neat bead of proseal at the joint, using the excess that squeezed out. Looks good, no rivits, the proseal takes paint ok. I just hope I never have to take it off Hope this helps Joe joehine(at)mi.net Comp. 9, Site 8, RR#4 506-452-1072 Home Fredericton, NB 506-452-3495 Work Canada, E3B 4X5 Nobody on their death bed has ever been heard to say "Geeze,I wish I'd spent more time at work" ________________________________________________________________________________
From: Greg Bordelon <greg(at)brokersys.com>
Subject: Too Fay - ing
Date: Jun 13, 1996
Greg, please enlighten me. What is a 'faying compound'? I learned a lot of things I had not known when building the plane, but this is something that got completely by me. Have I left something out that I should have put in? Are my joints going to swell and become arthritic?:<) John D I had not questioned this issue before, but in my 9 years in the airforce we were always required to use faying compound between riveted joints. What is it? well - we used a yellow chromate type paste. I guess its a bit like gasket cement on cars, but its never supposed to harden. The maintenance manuals I have for military aircraft all require the use of a faying compound. I have not been using it on my RV6, although I am now wondering whether I would be better off using it? Mike Parkinson I've been in aircraft 25 years and have either built, repaired, rebuilt aircraft by all major aircraft companies. All majors require that most joints be fay sealed with a product similiar to pro seal only better and easier to use... it just costs 3 - 4x more. later Harry Paine John as I understand it, a faying compound is sorta like a sealer. When applied to lap joints, plates and stuff it seals out moisture. No moisture in the joint means no electrolyte which equals no corrosion. Hey, Harry Paine help me out here! Please? There are other corrosion proofing products that can be used to displace moisture after assembly i.e. CorrosionX, ACF50. I'm looking on the list for a faying compound to carry around in my tool box. My local supplier said the chromatic paste is no longer available and he did not have a replacement. I could not find anything listed in Wick's or Aircraft Spruce's catalogs. Any Ideas out there? Greg Bordelon Houston Texas greg(at)brokersys.com not worked on RV in a week ________________________________________________________________________________
From: Greg Bordelon <greg(at)brokersys.com>
Subject: FW: VS Tip Attach
Date: Jun 13, 1996
Terry, I think in this case I'd just glue the tip on and glass it in. I'm not a fan of glass stuff to aluminum but I think in this case that would be the ideal fix. Just drill a couple of holes to cleco the thing together while the glue cures.You could also just glue a block of foam to the VS and make a new glassed in tip.....this may be redundant as you already have a tip. OR you could drill our the tip rivets and re-rivet back together with a new strip flange on the inside of rib flange. This new flange would extend past your skin and the fiberglass tip would slip over it. Anyhow, I'm going to put antenna/strobe/lights and stuff in the tips. I really don't think your going to like that strobe in the VS tip. I'd glass it in! Greg Bordelon Houston Texas greg(at)brokersys.com ---------- From: SceptreCal.CCMAIL.CompuServe.COM!Terryg(at)matronics.com[SMTP:SceptreCal.C CMAIL.CompuServe.COM!Terryg(at)matronics.com] Sent: Wednesday, June 12, 1996 6:44 PM Subject: RV-List: FW: VS Tip Attach 'Listers -- due to some unfortunate trimming errors, I have wound up with a VS skin that is a little short on the top. More precisely, I have wound up with the skin extending past the tip rib by about 1/4 to 5/16", instead of the designated 1/2". In thinking about this for a while, I've come up with a couple of ideas. 1) The rivets attaching the VS tip are shown a 1/4" back from the top of the VS. I can still do that with mine, although I'll end up nicking the edge of the flange of the tip rib. Also, I'll have to modify the flange a little on the tip itself. 2) I can attach a nut plate behind each of the two tooling holes in the tip rib, and again, with a few minor changes to the tip itself, screw the tip on with two bolts into these nutplates. I'll have to make sure that they can seal though, so that they don't permit water to enter the VS. Of the two, I'm leaning toward the latter. Looks like I'm going to want to get that tip off, anyway, as there may well be antennae/strobe stuff in there that I want to get at. Any thoughts on the above, or the situation in general, I would most appreciate! Cheers... Terry in Calgary "Skinning VS" ________________________________________________________________________________
Date: Jun 13, 1996
From: pilla(at)emmanuel.espinc.com (Michael Pilla)
Subject: Re: Trim Tab
Saved the file. Thanks for the README help. Mike ________________________________________________________________________________
Date: Jun 13, 1996
From: wigmore(at)lancelot.chs.lane.edu (Jack Wigmore)
Subject: rv6 wing and empenage
Sorry if this is posted for a second tome ..I believe the first one was lost in cyber space. Please spread the word. HELP! SAVE TIME AND MONEY? Buy my completed RV6/6A empenage kit (excellent) and untouched wing kit ( not pre-punched) for $4000 USD / offer. Located in Eugene Oregon. Contact J. Wigmore (541) 935-2639 or wigmore(at)lancelot.chs.lane.edu ________________________________________________________________________________
From: Michael Angiulo <mikeang(at)MICROSOFT.com>
Subject: FW: VS Tip Attach
Date: Jun 13, 1996
Are you saying that all the fiberglass tips can be glued right to the aluminum? Will it be as permanent as riveting? I would love not to have to drill, countersink, reinforce and pop rivet fiberglass. Is this something others have tried/found successful? I'd hate to see one of these tips come loose during flight as it could jam the control surface -Mike ---------- From: mi.net!joehine(at)matronics.com[SMTP:mi.net!joehine(at)matronics.com] Sent: Thursday, June 13, 1996 8:17 AM Subject: Re: RV-List: FW: VS Tip Attach >'Listers -- due to some unfortunate trimming errors, I have wound up with a VS >skin that is a little short on the top. More precisely, I have wound up with >the skin extending past the tip rib by about 1/4 to 5/16", instead of the >designated 1/2". In thinking about this for a while, I've come up with a couple >of ideas. > Terry, Glue it on with proseal. You have to heat it and expand it a bit so it is a tight fit in the top of the VS. I masked the top of the VS and a line about 1/8 inch up the tip from the line the top of the VS would make and then spread proseal on the fiberglass and pressed it in place. I then took a popsical stick and make a nice neat bead of proseal at the joint, using the excess that squeezed out. Looks good, no rivits, the proseal takes paint ok. I just hope I never have to take it off Hope this helps Joe joehine(at)mi.net Comp. 9, Site 8, RR#4 506-452-1072 Home Fredericton, NB 506-452-3495 Work Canada, E3B 4X5 Nobody on their death bed has ever been heard to say "Geeze,I wish I'd spent more time at work" ________________________________________________________________________________
Date: Jun 13, 1996
From: ecole(at)ix.netcom.com (EDWARD COLE)
Subject: Re: A suggestion for the elevators
You wrote: > >I was just fitting my elevators to my HS so that I could weigh the amount of >load I needed in the counterbalance. (I didn't have the *slightest* intention >of setting up the tail feathers on the desk, setting a chair in front facing >away, and making vroom-vroom, rat-a-tat-tat noises! No, not me!) > >I discovered a slight fitting problem that I want to warn people about so >they don't have this problem. As you can figure out, the counterbalance >arms will bind if they are angled into the HS at all. Well, one of mine is >pretty good, but the other one is too tight. Sigh. The only way I can fix >it now is to remove some material, or build it again. (I'm going to remove >the material). > >A method to avoid this problem -- after you've drilled the elevator skin to >the skeleton, but before you have drilled the holes into the tip ribs, clamp >the tip ribs and skin with cleco side clamps, take it all out of the jig, >and fit it to the HS. You'll probably find that the skins are in the way a >little bit, as you haven't formed the leading edge bend yet, but should be >able to find some method of making sure everything matches. > >I was extremely careful to get things square. Obviously not *quite* careful >enough. You only have to be off a degree or so to have a problem. > >Another suggestion -- when you are making your elevator skeleton, don't be >too tight when locating the holes for the rod ends. The tips of the elevators >must extend past the tips of the HS, but everything just has to be close at >the middle. Don't be *too* sloppy, of course, but I've got about a 16th on >the good end, and I think I would be happier with twice that. > >-Joe Joe, The angle can be controlled by the rod end bearing lengths to some degree, but this assumes you have not drilled the contol horns yet. The one rule that I have noted in building the empennage is "DON'T TRIM ANY ALUMINUM UNTIL YOU HAVE TO". A previous post concerning the VS skin overhang being too narrow for the fiberglass cap attach reinforces this rule. Hope you can solve this one without much pain. Ed Cole RV6A #24430 ecole(at)ix.netcom.com ________________________________________________________________________________
From: Mlfred(at)aol.com
Date: Jun 13, 1996
Subject: Re: A suggestion for the elevators
>I discovered a slight fitting problem that I want to warn people about so >they don't have this problem. As you can figure out, the counterbalance >arms will bind if they are angled into the HS at all. Well, one of mine is >pretty good, but the other one is too tight. Sigh. The only way I can fix >it now is to remove some material, or build it again. (I'm going to remove >the material). How about this: There are 4 rivets holding the counterbalance arm at the angle it is. Drill out these rivets, move the arm to where it should be, and re-rivet the assy. You may want to use the NAS1097 rivets where applicable, and simply ream the hole that has the pop rivet in it. I wouldn't re-build the parts when the "fix" is so easy... Check six! Mark ________________________________________________________________________________
Date: Jun 13, 1996
From: ammeterj(at)seanet.com (John Ammeter)
Subject: Re: Fuel primer solenoid
>A while back someone mentioned an electric fuel primer solenoid. Can someone >give me a contact to obtain one of these? > >Thanks, >Ed Bundy (hooking up engine guts) >ebundy2620(at)aol.com > Sure, I hate to plug ACS but they sell the primer solenoid, part number 05-29823 (12 Volt) for $35.50. Page 135 in the '95/'96 catalog. John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA RV-6 N16JA Flying 5 years ________________________________________________________________________________
Date: Jun 13, 1996
From: Stuart Fraley <swfraley(at)alpha.comsource.net>
Subject: Wingtip lighting
After hearing of inconveniences with mounting the tail light, I'm considering returning my rudder bottom for the one without the light hole. However, looking at the whelen wingtip lighting system with the 3 lights on each tip, it doesn't look like you get visible white light directly behind the centerline of the airplane. Has everyone who has applied for night certification using this system gotten it? I'd hate to go to the hassle and expense of installing it and then have the inspecto tell me it wasn't adequate. Stuart Fraley RV-6 Tail, done except weights and tips Wings coming July ________________________________________________________________________________
Date: Jun 13, 1996
From: ammeterj(at)seanet.com (John Ammeter)
Subject: Re: Lubbock Builders?
>My friend, Mark Myres, who is not on this list will be flying his beautiful >new RV-6 to Lubbock to visit family next week. I offerred to see if I could >round up anyone from the list interested in looking at his plane and >possibly anyone who might have some hanger space to offer at the airport. >He'll be arriving at Lubbock June 20 and leaving June 22. E-mail me >directly if you're interested. Thanks. > >Monte King >kingm(at)whidbey.net > > > I want to add a little detail to this posting. Mark has built a beautiful RV-6 and deserves to win Grand Champion at any airshow he attends. He's added an extra fuel (around 8 to 10 gallons) behind the instrument panel, installed custom machined control levers, installed an original design canapy latch system and much more. The workmanship is unquestionably the best I've seen. John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA RV-6 N16JA Flying 5 years ________________________________________________________________________________
Date: Jun 13, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: RV6 Wing Spars
I have read that, plus I read somewhere about something, I think, is LDS #2 or #3. It was available from the FBO here. If I remember correctly, Vans recommended it as well. It is a spray on type that is made for the purpose of lubricating and protecting such. I think one of it's advantages is that it stays flexible rather than becoming brittle. I used it when I put my bolts in for the final time. The first time I put the bolts in, they were extremely hard to drive. In one AF manual, It described the size hammer that it would take to 'fit' a close tolerant bolt in it's hole--pretty big and lots of blows. The second time, it was somewhat easier. John D By the way, I've heard that it is a good idea to >paint the bolts with primer and dirve them in wet when you get ready to >install the wings. Anyone know about that? > > > John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: Too Fay - ing
Date: Jun 13, 1996
I think with epoxy primers, the use of any chromate paste (faying compound) between seams is not required. The only place would be where fluids might leak through, for example the firewall (solvents when you wash the engine) or canopy (water). I used some proseal on the firewall. The silicon based products should be good to calk seams (assuming they are primed as most of these give off aceatic (?sp) acid. Herman > > Greg, please enlighten me. What is a 'faying compound'? I learned a lot > of > things I had not known when building the plane, but this is something that > got completely by me. Have I left something out that I should have put in? > Are my joints going to swell and become arthritic?:<) > John D > > > I had not questioned this issue before, but in my 9 years in the airforce > we were always required to use faying compound between riveted joints. What > is it? well - we used a yellow chromate type paste. I guess its a bit like > gasket cement on cars, but its never supposed to harden. The maintenance > manuals I have for military aircraft all require the use of a faying > compound. I have not been using it on my RV6, although I am now wondering > whether I would be better off using it? > Mike Parkinson > > > I've been in aircraft 25 years and have either built, repaired, rebuilt > aircraft by all major aircraft companies. All majors require that most > joints be fay sealed with a product > similiar to pro seal only better and easier to use... it just costs 3 - 4x > more. > later Harry Paine > > > John as I understand it, a faying compound is sorta like a sealer. When > applied to lap joints, plates and stuff it seals out moisture. No moisture > in the joint means no electrolyte which equals no corrosion. Hey, Harry > Paine help me out here! Please? There are other corrosion proofing products > that can be used to displace moisture after assembly i.e. CorrosionX, > ACF50. I'm looking on the list for a faying compound to carry around in my > tool box. My local supplier said the chromatic paste is no longer available > and he did not have a replacement. I could not find anything listed in > Wick's or Aircraft Spruce's catalogs. Any Ideas out there? > > Greg Bordelon > Houston Texas > greg(at)brokersys.com > not worked on RV in a week > > Herman Dierks, Dept. E54S, AWSD, Austin, Texas mail: dierks(at)austin.ibm.com ________________________________________________________________________________
From: mcarob(at)ozemail.com.au
Date: Jun 14, 1996
Subject: Sender: owner-rv-list
My name is Rob McAnally, a mid career Air Traffic Controller from Melbourne Australia who needed something to do in his spare time. Then I commenced building my RV-6 and spare time is no longer a problem. I have completed the Empennage kit and both my wings are approaching final skinning. There are a group of four builders of RV-6/6A kits in my vicinity who get together on a regular basis to see if we are all making the same mistakes and all recovering from them in satisfactory (and legal) ways. Australia has no Experimental Catagory as yet so we build under normal Civil Aviation regs. One of my group did me a big favour and introduced me to the Internet so now I may just have to retire to get time to keep up. ________________________________________________________________________________
Date: Jun 13, 1996
From: "Elon Ormsby" <Elon.Ormsby(at)quickmail.llnl.gov>
Subject: Pre-Punched
REGARDING Pre-Punched Patrick Kelly, why do you hate pre-punched skins? ________________________________________________________________________________
From: HowardRV(at)aol.com
Date: Jun 13, 1996
Subject: adddress's
My computer crashed and I lost some addresses. I need Frank Justice, Orndorf, Vans, Hal Downes. Excuse the personal request. Howard Kidwell Howardrv(at)aol.com ________________________________________________________________________________
Date: Jun 14, 1996
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Jigs in sydney
There are two (2) RV6/6A jigs available in Sydney for any Australian builders interested. Both beautifully built examples of the type. Call me on (02) 99068975 AH if interested. ________________________________________________________________________________
Date: Jun 13, 1996
From: finnlass(at)ix.netcom.com (Finn Lassen )
Subject: Aircraft Spruce
I just received my order from Spruce West - 8 feet of 3/16" x 1.25" ALU bar. I had put on my order that I wanted 2 peices of 4'. However, they shipped it as 8' adding 2 pounds of unnessesary packaging weight PLUS oversize charges from UPS - total shipping charges $18 on a $19 order! (I'm not sure what good what Spruce East is - they didn't have it in stock so it was shipped from CA to here in FL.) Seems my idea of building an airplane at low cost is going down the drain. Anyway, I guess the moral of the story is to put this kind of order on two lines on the order form (2 identical lines, 4' on each line) -- thought this might be useful to some of you. Finn (on horz stab, and grumpy) finnlass(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 13, 1996
From: finnlass(at)ix.netcom.com (Finn Lassen )
Subject: Spar bolts
Since no-one else mentioned it - Why not put the bolts in the freezer overnight and maybe even take a heater to the spars? Of cause it won't handle an excessive mismatch in diameter, but could make extensive hammering unneccessary. Finn (finished cutting the taper in horz stab spar flanges with hacksaw - better than going to gym for workout!) finnlass(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 13, 1996
From: wbpace(at)adnc.com (Bill Pace)
Subject: Re: A suggestion for the elevators
>I discovered a slight fitting problem that I want to warn people about so >they don't have this problem. As you can figure out, the counterbalance >arms will bind if they are angled into the HS at all. Well, one of mine is >pretty good, but the other one is too tight. Sigh. The only way I can fix >it now is to remove some material, or build it again. (I'm going to remove >the material). I had this same problem with the right elevator. I had already drilled the skeleton to the skin, but had not yet riveted them. Upon a quick and final check, I found that I had too much "toe-in" to be assured of enough clearance between the outer HS rib and the elevator arm. &%^#! I ended up redrilling the angling out the rib and redrilling the skin, with the new rivet holes offset along the rib to provide adequate distance between the new and old holes. It isn't pretty, but it's also not as bad as I expected. It'll just be a few more holes to fill with micro before I paint it. > >A method to avoid this problem -- after you've drilled the elevator skin to >the skeleton, but before you have drilled the holes into the tip ribs, clamp >the tip ribs and skin with cleco side clamps, take it all out of the jig, >and fit it to the HS. You'll probably find that the skins are in the way a >little bit, as you haven't formed the leading edge bend yet, but should be >able to find some method of making sure everything matches. This is just how I found my problem. If I hadn't, it probably would have required a complete rebuild of the elevator. Ouch. Just call me Mr. Bondo! ----- Bill Pace The only expensive tool wbpace(at)adnc.com is a cheap tool. ________________________________________________________________________________
From: "Ernst Totland" <ernto(at)weald.air.saab.se>
Date: Jun 14, 1996
Subject: Re: New member of the list (Volvo convertion)
On Jun 13, 8:46am, John Morrissey wrote: > Subject: Re: RV-List: New member of the list (Chatter - humor) > Oh my God NO!! not a Volvo in the air!!! Having been run over twice by Volvo > drivers (who have a particullarly bad reputation for poor driving here in > Australia1) The thought of a sky full of Volvo drivers fills me with terror!! > :-) > > An RV with a crash crumple zone?? > > Welcome to the list!! > > How much did the installation cost?? how many hours has it run?? what sort > of problems have they encountered with the engine? > > John Morrissey > > > > >I am hoping to build an rv6 in time, in that respect I am wondering if any > >of you have heard anyting about putting a Volvo engine in a rv? > > > >There are these swedish guys who have put the 6cylinder version of a > >960Volvo engine in a Piper Pony, it has been running for some time now > >pulling gliders with a 4 bladed prop and silencer, nice and quiet! > > > >I recently heard that someone has put a Volvo engine in an rv, probably > >the 5 cylinder version of the same engine, but that's all I have heard. > > > >Finn Egil Grimnes > > > >-- End of excerpt from John Morrissey Interesting to hear about the reputation of Volvo drivers abroad. How about Saab drivers? Well, I had the opportunity to take a closer look at the "PiVo" project a couple of weeks ago. It is a modified PA-25 Pawnee with a straight Volvo 960, 6 cylinder, 3 liter engine running on 91/96UL fuel. The idea is to use an off-the-shelf engine and the only physical modification encountered is the addition of a double belt, 3 to 1 reduction drive. The original injection and ignition systems were retained (only one spark plug per cylinder). Acessories like the exhaust system and the huge external muffler are custom made. Some modification to the engine computer software has also been necessary (done by Volvo engine engineers). The propeller, a custom made two blade fix pitch, is designed for a cruise rpm of approx 1700. The aircraft is extremely quiet, hardly any engine noice at all at some distance, just a little whisper from the propeller could be heard. The engine is claimed to be rated to 200 hp at 6000 rpm, but judging from the observed climb performance the thrust is not equivalent to the original installation, as claimed. It is however sufficient for towing a fiberglass two-seat glider. First flight was in June -95 and I they have about 60 hours in the air by now. What I have heard, they have not had any serious problems. The engine has been running hot, mainly due to poor air flow through the radiator and oil coolers, but also due to exhaust system problems. These defects have been corrected. I also suspect they have an inefficient propeller, which to some extent explains the relatively poor climb performance. Regarding installation cost, I do not know how much money is invested. However, it is an off the shelf engine, and the rumour says they got it for free from Volvo. I have also heard of another team working on converting a 5 cylinder Volvo engine for a Cessna 172. Personally, I cannot understand this love for Volvo when there are Saabs!!!! Well, Volvo has a reputation for reliability, but I would not rely on a car engine in my RV6. At least not until it has been proven in thousands of flight hours. Hope this is of some interest. Ernst Totland ernto(at)weald.air.saab.se RV-6 #20898 SE-XOI ________________________________________________________________________________
From: "Graham Taylor" <gmt(at)mail.iinet.net.au>
Date: Jun 14, 1996
Subject: Jon Johanson - details
As Royce Craven has already posted, Jon Johanson will depart Point Cook, Melbourne on 10.00am local time, Friday 21 June, starting his second global trip. His first leg is to Perth, thence to Port Hedland (North up the west coast of Australia), then out over the Indian Ocean to Cocos Islands, Rodrigues Island, Mauritius, then Durban in South Africa. He will spend 2 weeks in South Africe, then off the Ascension Island in the mid Atlantic, on to Brazil, Barbados, Florida (I'll post an exact destination when I have it), and on to Oshkosh. The return to Australia will be in late September, from Vans down to Monterey, to Hilo in Hawaii, Christmas Island, Pago Pago, Norfolk Island, Sydney, Point Cook, and finally back home to Adelaide. He will have a digital camera, laptop, and modem, and will upload to a web page details and pictures of his flight. The site address (It's not quite ready yet) will be www.nasma.com.au/saaa This page will be sponsored by the National Air & Space Museum at Point Cook, and will be supported by SAAA (Sport Aircraft Association of Australia, the Downunder equivalent off EAA) Jon will be staying with me during his spell in Perth, so if you want to say a personal Hi to him, send your message here. Later you will be able to get him via the web page. Graham Taylor gmt(at)iinet.net.au RV-6A - the light is at the end of the tunnel. Graham Taylor gmt(at)iinet.net.au Ph (619) 310 3254 Fax (619) 310 6048 ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 14, 1996
Subject: Re: Wingtip lighting
> Has everyone who has applied for night >certification using this system gotten it? >Stuart Fraley >RV-6 Tail, done except weights and tips >Wings coming July > Stuart: I have seen plenty of RV's with this system. You can see them from a reasonable distance behind. I have a tail srobe in the rudder bottom and while it was more difficult than the wing tip rear light system it wasn't all that bad. IMHO it gives you one more strobe that might just keep somebody from running up your tail. Regards: Rusty Gossard N47RG RV-4 Flying ________________________________________________________________________________
Date: Jun 14, 1996
From: Harry Paine <HPair(at)ix10.ix.netcom.com>
Subject: Re: Aircraft Spruce
>I just received my order from Spruce West - 8 feet of 3/16" x 1.25" ALU >bar. I had put on my order that I wanted 2 peices of 4'. However, >they shipped it as 8' adding 2 pounds of unnessesary packaging weight >PLUS oversize charges from UPS - total shipping charges $18 on a $19 >order! (I'm not sure what good what Spruce East is - they didn't have >it in stock so it was shipped from CA to here in FL.) > >Seems my idea of building an airplane at low cost is going down the >drain. > >Anyway, I guess the moral of the story is to put this kind of order on >two lines on the order form (2 identical lines, 4' on each line) -- >thought this might be useful to some of you. > >Finn (on horz stab, and grumpy) > >finnlass(at)ix.netcom.com > Finn & everyone >just for the record in the last five years I have talked to no one who was happy with aircraft screwup.... they consistly overcharge on their shipping.... they don't know what you are talking about when you're trying to order something..they will ship a partially filled order so you have to pay the overcharged shipping twice....(which I think do with glee) they are back ordered. Now then about them know about your dissatifation by changing vendors, there are plenty others. > > ________________________________________________________________________________
From: rwoodard(at)lawyernet.com
Date: Jun 14, 1996
Subject: Spar bolts
RV>Finn (finished cutting the taper in horz stab spar flanges with RV>hacksaw - better than going to gym for workout!) RV>finnlass(at)ix.netcom.co OUCH!! Buy, beg, borrow or _steal_ a bandsaw!! My little brother's saw worked very nice for my HS flange cutting. :-) Rod Woodard RWoodard(at)lawyernet.com ________________________________________________________________________________
From: WStucklen(at)aol.com
Date: Jun 14, 1996
Subject: Re: User Fees
>I'm curious as to how effective it is to post things about >political issues such as the recent "AOPA Alert" regarding >the Aviation Trust fund and User Fees. If you saw my posting, >and wrote to your senator as a result, could you drop me >a _private_ e-mail please? > >Thanks. > >Randall Henderson >randall(at)edt.com > > > > I sent letters to Senator's Dodd, Kennelly, and Leiberman of Conn.... Fred Stucklen RV-6A N925RV wstucklen(at)aol.com ________________________________________________________________________________
From: ted_boudreaux(at)om.cv.hp.com
Date: Jun 14, 1996
Subject: Re: Spar bolts
Item Subject: RV-List: Spar bolts There is a guy in the local (Eugene, OR) RV builders' group who used to work for Boeing. Apparently they soak the very large spar bolts in liquid nitrogen for several days. The bolts are then inserted into deliberately undersized holes in the spar. When the bolts heat back up to room temp., they expand. He says that the spar and bolts are essentially one part after this process, and that removing the bolt is basically impossible. Makes for a very strong spar, though. Ted Boudreaux ted_boudreaux@hp-pcd.hp.com RV6A #22435 in limbo while I move ______________________________ Reply Separator _________________________________ Subject: RV-List: Spar bolts HP-Corvallis,shargw1 Date: 6/13/96 10:08 PM Since no-one else mentioned it - Why not put the bolts in the freezer overnight and maybe even take a heater to the spars? Of cause it won't handle an excessive mismatch in diameter, but could make extensive hammering unneccessary. Finn (finished cutting the taper in horz stab spar flanges with hacksaw - better than going to gym for workout!) finnlass(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 14, 1996
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Too Fay - ing
[snip!] > I used some proseal on the firewall. > The silicon based products should be good to calk seams (assuming they > are primed as most of these give off aceatic (?sp) acid. > Herman I believe the acetic acid RTV thing has been shown to be a non-issue. The following is an article I wrote for the Van's Air Force Home Wing Newsletter (December 1995 issue), and also posted here at that time. Randall Henderson RV-6 ----- RTV Revisited First some history: A couple of years ago some concern popped up among builders about the fact that normal RTV contains acetic acid which can allegedly be corrosive to aluminum. Since then there has been a lot of discussion about what to use instead, and Van's manual now specifies "Electronic grade" RTV which contains no acetic acid. Last night at our monthly meeting, Bill Benedict (Van's GM) related some interesting new information on this subject. Van's had spoken to someone at one of the RTV manufacturers who said that the Acetic acid based RTV was originally developed for the _purpose_ of making it stick better to aluminum! Apparently the other type would peel off a lot easier, and the acetic acid gave it self-etching properties. Van's then made two samples, one with acetic acid and one without, and gave them to local builder Steve Harris who put them in an environmental chamber where (salt spray and the whole bit) for something like 2 months. After that time neither sample showed any corrosion, but the NON-acetic acid based RTV would peel off relatively easily while the acetic acid based would not. So maybe now we're back to using normal RTV after all! ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 14, 1996
Subject: Re: Aircraft Spruce
>>I just received my order from Spruce West - 8 feet of 3/16" x 1.25" ALU >>bar. I had put on my order that I wanted 2 peices of 4'. However, >>they shipped it as 8' adding 2 pounds of unnessesary packaging weight >>PLUS oversize charges from UPS - total shipping charges $18 on a $19 >>order! (I'm not sure what good what Spruce East is - they didn't have >>it in stock so it was shipped from CA to here in FL.) I must admit when I first heard that Alexander Aero was being bought by Aircraft Spruce my first reaction was "oh, no..." as now there is one more competitor sucked up by Big Business. ACS has been variably OK but it is nice to have choices out in Aircraft Land where things that have AIRCRAFT stamped on them are somewhat overpriced. I don't know any other mailorder business that charges you for freight when something is backordered. Was it MY falt they didn't have it in stock??? If you ship 2000 orders a day and charge each one an extra dollar, adds up, yes it does. "We're only in it for the money." Frank Zappa Michael Kosta RV-4 232SQ Fly By July (or August, September, I don't know) ________________________________________________________________________________
Date: Jun 14, 1996
From: Dan Boudro <dboudro(at)nmia.com>
Subject: Re: Aircraft Spruce
Just for the record; I used AS throughout my second RV-4 project. I called and talked to the man in charge of email orders first and gave him my cc number, Jerry said he would be personally responsible for it and would not enter it electronically in their system. I ordered all items via email, Jerry usually got the order out the same or next day. They did partial ship orders but I was never charged for the backorder shipping. In general I am pleased with AS and will continue to order the products I need from them. Dan Boudro RV-4 N9167Z Albuquerque, NM dboudro(at)nmia.com ________________________________________________________________________________
Date: Jun 14, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Spar bolts
> There is a guy in the local (Eugene, OR) RV builders' group who used > to work for Boeing. Apparently they soak the very large spar bolts in > liquid nitrogen for several days. The bolts are then inserted into > deliberately undersized holes in the spar. When the bolts heat back > up to room temp., they expand. He says that the spar and bolts are > essentially one part after this process, and that removing the bolt is > basically impossible. Makes for a very strong spar, though. > >Ted Boudreaux Too tight of a fit might not be a good idea in case dis-assembly is required. I helped a RV-6A owner remove his wings so the wrecked airplane could be transported home. It was about 20 degrees in an unheated hanger. They had hammered their close tolerance bolts in and they were a nighmare to remove. What is there, 70 some bolts? Standing on your head removing all of these bolts was fun. We worked in shifts. The weldments for the main gear were a real pain to work around. What happened? The pilot took off on a rough (moguls?) grass strip, got launched but didn't have flying speed, tensed up and fed in some rudder and when he hit, hit cockeyed. He bent the nose gear back under the belly. In fact, the nose gear fairing poked a hole in the .040" belly skin. The left gear was bent back and punched a hole in the .032" bottom skin, just ahead of the rear spar. Suprisingly, there was almost no damage to the fiberglass fairings, just paint scuffs. It went down on the left wing and popped the wing tip off. Very little damage. We speculated that had the wing tips been installed with machine screws, much more metal damage would have occured. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 14, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Spar bolts
>Why not put the bolts in the freezer overnight and maybe even take a >heater to the spars? > >Of cause it won't handle an excessive mismatch in diameter, but could >make extensive hammering unneccessary. > >Finn Probably would work. In a perfect world, the bolts should be a better fit. On my first RV, the bolts were very tight. The bolts would hardly fit into one flange strip. I polished the close tolerance holes with Scotch brite on a mandrel to get a good fit (and to take out the primer). The bolts on the second set of spars were a better fit. After priming each spar flange strip, I cleaned the primer out of the close tolerance holes before it dried. (The other 3/16" holes didn't present any problems, even with primer in them.) You should not have to beat on the bolts with a big hammer. I'm sure a lot of spars are drilled with the same reamer, hence the different tolerances from spar to spar (new bit vs. old) Adjustable reamers would work good in this application but adds to the tool cost inventory. BTW, I reamed the rear spar attach and where the fuel tank attaches to the fuselage. Not called for in the plans, but made me feel better. Your idea of heat and cold works on the installation of the AN fittings in the fuel selector valve. Typical pipe thread problem, too tight or not tight enough. I was afraid to put the torque on the aluminum fittings that was required to get the fittings to point straight down. Put the AN fittings in the freezer and heated the valve. Worked well. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 14, 1996
From: rdunn(at)ionet.net (Ronald M. Dunn)
Subject: Shimming
Last night I began to assemble the HS skeleton on my -8. I clecoing the six ribs to the rear spar. Then I clamped the front spar to those ribs. The left end rib was square to the rear spar but the right end rib need a full 1/8 of an inch to be square (when clamped to the front spar). That seems like a lot of shimming to me. HS-810 & HS-814 were challenging but everything seemded to measure correctly when building the front spar. What happened? Any suggestions. Thanks for your help, y'all. Ron Ron Dunn (RV-8 #80078) rdunn(at)ionet.net Broken Arrow, OK ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Jun 14, 1996
Subject: Re: User Fees
Randall, I kept my mail-o-gram from AOPA with the intention of firing off a letter. But the reality is I would not have done it....if it wasn't for your form letter. Thank you for taking the time to post that letter. BTW it was well written. Gary ________________________________________________________________________________
From: DenDulkRV6(at)aol.com
Date: Jun 14, 1996
Subject: Remove
I would like to be removed from the mailing list since it takes to long to go through and read and delete the same questions that are asked over and over again largely from the same person. ________________________________________________________________________________
From: Herman Dierks <dierks(at)austin.ibm.com>
Subject: Re: Aircraft Spruce
Date: Jun 14, 1996
FYI, I have also have had my share of dis-satisfaction with ACS. However, I saw some time back that they had changed their policy and they now pay the shipping charges on any Back Ordered items. That should help a lot, but it can still be a pain to have items on BO. Herman > >I just received my order from Spruce West - 8 feet of 3/16" x 1.25" ALU > >bar. I had put on my order that I wanted 2 peices of 4'. However, > >they shipped it as 8' adding 2 pounds of unnessesary packaging weight > >PLUS oversize charges from UPS - total shipping charges $18 on a $19 > >order! (I'm not sure what good what Spruce East is - they didn't have > >it in stock so it was shipped from CA to here in FL.) > > > >Seems my idea of building an airplane at low cost is going down the > >drain. > > > >Anyway, I guess the moral of the story is to put this kind of order on > >two lines on the order form (2 identical lines, 4' on each line) -- > >thought this might be useful to some of you. > > > >Finn (on horz stab, and grumpy) > > > >finnlass(at)ix.netcom.com > > > > > Finn & everyone > >just for the record in the last five years I have talked to no one who was > happy with aircraft screwup.... they consistly overcharge on their shipping.... > they don't know what you are talking about when you're trying to order > something..they will ship a partially filled order so you have to pay the > overcharged shipping twice....(which I think do with glee) they are back > ordered. > > Now then about them know about your dissatifation by changing vendors, there > are plenty others. > > -------------------------------------------------------- *NOTICE for internet mail*: Any ideas or thoughts expressed here are my own and are independent of my employer. Herman Dierks, Dept. E54S, AWSD, Austin, Texas mail: dierks(at)austin.ibm.com ________________________________________________________________________________
Subject: RV-6Q
Date: Jun 14, 1996
From: Jack Abell <abell(at)rand.org>
What's an RV-6Q? Jack Abell RV-6A N333JA (Reserved) ________________________________________________________________________________
Date: Jun 14, 1996
From: finnlass(at)ix.netcom.com (Finn Lassen )
Subject: Re: Spar bolts
Actually have a cheap one (fixed speed) but I ruined the blade trying to cut 4130 steel. Didn't want to spend another $15 on a blade - anyway, good exercise, and really makes you feel YOU are building the plane (felt I was cheating a bit because bought old kit with wings already skinned)! Finn You wrote: > >RV>Finn (finished cutting the taper in horz stab spar flanges with >RV>hacksaw - better than going to gym for workout!) > >RV>finnlass(at)ix.netcom.co > >OUCH!! Buy, beg, borrow or _steal_ a bandsaw!! My little brother's saw >worked very nice for my HS flange cutting. :-) > >Rod Woodard >RWoodard(at)lawyernet.com > > > ________________________________________________________________________________
From: rwoodard(at)lawyernet.com
Date: Jun 14, 1996
Subject: Remove
RV>I would like to be removed from the mailing list since it takes to long to g RV>through and read and delete the same questions that are asked over and over RV>again largely from the same person You need to send a message to rv-list-request(at)matronics.com with the word unsubscribe as the **ONLY** word in the body of the message. toodles. ________________________________________________________________________________
Date: Jun 14, 1996
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: Remove
>I would like to be removed from the mailing list since it takes to long to go >through and read and delete the same questions that are asked over and over >again largely from the same person. > It appears you missed the messages on unsubscribing from the list . Rob Acker (r.acker(at)ix.netcom.com) Rancho Santa Margarita, CA / RV-6Q / N164RA reserved ________________________________________________________________________________
Date: Jun 14, 1996
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: RV-6Q
> >What's an RV-6Q? > >Jack Abell >RV-6A N333JA (Reserved) > > It's the ordering code for the RV-6 Quickbuild kit. Rob Acker (r.acker(at)ix.netcom.com) Rancho Santa Margarita, CA / RV-6Q / N164RA reserved ________________________________________________________________________________
Date: Jun 14, 1996
From: Harry Paine <HPair(at)ix5.ix.netcom.com>
Subject: duh?
>Harry > >Would you send me your snail-mail address? > >Rgds >Mark > >Its on the last newletter.... 477 Printz Rd Arroyo Grande, Calif 93420 ________________________________________________________________________________
Date: Jun 14, 1996
From: Boris Robinson <smbr(at)inetw.net>
Subject: Re: RV6 Wing Spars
> By the way, I've heard that it is a good idea to >paint the bolts with primer and dirve them in wet when you get ready to >install the wings. Anyone know about that? > > I started with epoxy primer and switched to Sherman William's 980 self etching primer, (with zinc chromate). During assembly I had great difficulty with tight bolts and rivets. The only way to install the bolts and many of the rivets on the spars was to first wet the hole by using the liquid primer with a Q-tip. The bolts and rivets (that fit properly) easily slid into place. I now do this with all of the bolts. It gives me a measure of confidence against future corrosion. ________________________________________________________________________________
From: Blpzk(at)aol.com
Date: Jun 14, 1996
Subject: Re: Spar bolts
Freezing the bolts won't make much of a difference, Finn. There are various techniques for easing interference fits, the idea is to heat the undersized part (oil bath or heat lamps), and/or cool the oversized part ( freezer or a dry ice&acetone bath). It works great for larger parts, say over an inch diameter, but for anything smaller, the change in diameter won't be significant. What works very well is to drive (tap) the bolt in with a rivet gun and flush set while backing up the other side (beside the hole, not covering it!) with a bucking bar. Of course, it's recommended by some sources (required, even) to prime the shank of the bolt and install it wet. On cad-plated bolts, the plating will usually scrape off and gather under the head, so it might be wise to remove this excess before driving the head completely home. When the time comes to remove the bolt, do the reverse, but don't get too wild: if you mushroom the end, things get more difficult. Often when I'm taking something apart, I just drill off the heads of close tolerance bolts and drive through rather than going to the trouble of taking the nut (or whatever) off. As for masochism: I don't even own a hacksaw or a set of "aviation" snips, and my time is worth far, far more than the expense of the tools I use instead. John Kimmel ________________________________________________________________________________
From: Cecil Hatfield / Fourstar Printing <cecil(at)alto1.altonet.com>
Date: Jun 13, 1996
Subject: Wing Jig and Brackets
Ron, I put the spar sholder high for most of the work is from spar down. The leading edge and tanks are made on the bench. I also rigged it so that after the skins are in place with clecos, I could swivel it up to lap level to work on the flaps and aelirons while seated. worked great. I to am building them both at the same time. Mine are end to end. Almost done. Cecil Hatfield RV-6A in Thousand Oaks California ________________________________________________________________________________
From: Cecil Hatfield / Fourstar Printing <cecil(at)alto1.altonet.com>
Date: Jun 13, 1996
Subject: Re: RV-List:----Nice----
FYI Last week I mailed Van's an order for fuel sending units, and added a note saying that if they had gotten around to making inspection plates and reinforcing rings for the tanks, to send me some. Great days, - - - they not only had them, but they have all the rivinut holes punched, sending unit holes punched, fuel pick-up hole punched and the two nose reinforcement pieces made. What a deal. I went back to the catalog to see if I had missed them and still didn't see them so thought I would post this for you guys and gals that are in-to wing construction. I'm sure Van will have these in his next catalog. Cecil Hatfield RV-6A in Thousand Oaks California ________________________________________________________________________________
Date: Jun 14, 1996
From: Tom Redfield <75160.3373(at)CompuServe.COM>
Subject: Electrical conduit cut outs, wing
I am at the point in building a RV-6A where the holes for the electrical conduit must be drilled in the wing ribs. Orndorf's video puts them in the bottom of the wing behind the spar. F. Justice says about 2-1`/4 behind the spar and 1-1/2 below the top skin, which puits them in a lightening hole, by my calculations. What are the popular locations and why are they preferred? Tom Redfield 75160.3373(at)compuserve.com ________________________________________________________________________________
Date: Jun 14, 1996
From: ammeterj(at)seanet.com (John Ammeter)
Subject: Any builders near Banff/Calgary
My wife and I will be vacationing in the east BC/Alberta area this August. She's not too interested in RV's but I may be able to get away from the poolside/tourist areas. Any builders or flyers in that area that would like a visitor please give me an email. I'm an EAA Tech Counselor as well as RV builder/flyer (RV-6). Thanks, John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA RV-6 N16JA Flying 5 years ________________________________________________________________________________
From: JamesCone(at)aol.com
Date: Jun 15, 1996
Subject: Re: Electrical conduit cut outs, wing
Where ever you put them, just be sure to leave room to buck the rivets when you install the skin. I didn't and had a heck of a time getting some of them bucked. Jim Cone jamescone(at)aol.com ________________________________________________________________________________
From: JamesCone(at)aol.com
Date: Jun 15, 1996
Subject: Re: User Fees
I too sent off your letter to my senators and representative. Thanks for making it easy for me. Jim Cone jamescone(at)aol.com ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 15, 1996
Subject: Re: Remove
>I would like to be removed from the mailing list since it takes to long to go >through and read and delete the same questions that are asked over and over >again largely from the same person. > > Well, if you're going to get grouchy about it, maybe you'ld be better just answering your own questions. Have fun out there by yourself...we'll be here enjoying each other without you. :.] ________________________________________________________________________________
From: "Peter Bennett" <bennett(at)healey.com.au>
Date: Jun 15, 1996
Subject: Painting inside
I am starting to put various stuff inside the cabin area. At the moment it it a beautiful vomit colored green, being primed only. When is the best time to paint the inside of the cabin area? Is it best to mask rudder cables, fuel fittings, wiring etc, or pull it out to paint? Or is it best to paint now and patch up the chips later? All suggestions gratefully considered. Peter Bennett RV6 the right way up. ________________________________________________________________________________
From: DerFlieger(at)aol.com
Date: Jun 15, 1996
Subject: Re: Aircraft Spruce
> In general >I am pleased with AS and will continue to order the products I need from >them. > >Dan Boudro Likewise! I haven't ordered a lot from them recently, but in the past I would say I was 95% satisfied with them. I think there are many folks building aircraft who have the wrong impression about how the aviation world REALLY works. I believe its related to the "Sue them" mentality, and would like to see it stop. Jim Stugart ________________________________________________________________________________
Date: Jun 15, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: Spar bolts
For what it's worth: my old AF manual on Aircraft sheet metal maintenance has the following information under Installation of bolts and nuts. Close tolerance bolts are a tight drive fit. "A tight drive fit, for example, is one in which a sharp blow of a 12- or 14-ounce hammer is required to move the bolt." To me, when I was 'hammering ' in the wing bolts, I thought that something must be wrong, too tight. A few nights later when looking up something else, I ran across this information, made me feel a little better regarding the fit. I have not sweated the ones that didn't require a 'sharp' blow or many blows. One thing that has not been mentioned, the possible need for extra washers to make sure that the nut does not bind at the end of the threads before seating on the plate. I had assumed the bolts to be the right length, but not so. I had to use up to 4 washers on some of mine. When I disassembled to move to the airport, I used a marker to put on the spar how many washers I used at each hole, sure made it easier at final assembly. With the close work space, it was frustrating originally to tighten the nut, only to have the bolt still rotateable afterwards, necessitating removal of the nut, install washers, and then try again. Seems that the spar sort of springs apart, and the eyeball says the bolt is the right length, but then the spar compresses, hence the need for the washers. I know that this is pretty basic, but it was frustrating to me that first time on the wing spars. Hope it saves someone out there some additional frustration. I may have screwed up, but I used old fashion axle grease to lub. my spars to slip into the fus. location. It was very tight and I guess the gold treatment on the spar made it rougher, hence the need for the grease. I did the same on the first install. of the bolts. the final install. I used the LDS (not the religion) and sprayed each bolt just before installing. John D John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
Date: Jun 15, 1996
From: Pat McClung <pmc123(at)airmail.net>
Subject: RV-3 Parts
I Still have the two new wing-tips and usable cowl for the RV-3. Have not heard further from anyone--- They will be relegated to "permanent storage" soon ________________________________________________________________________________
Date: Jun 15, 1996
From: dcahoon(at)intellinet.com (David Cahoon)
Subject: Fire extinguisher
In the last Sport Aviation there is an article by Tony B. that shows a picture of his RV-3 with a fire extinguisher system installed. This looks like a good thing that we all probably overlook or leave out. Let's visit this idea. Most race cars have some type system that pipes "halon" gas to vital trouble spots. i seems this could be done with alum. tubing to the carb.,rear case, battery without a great expense. Any thoughts or have you seen such a system. I wrote Tony for details. One thing that started this was my A&P was somewhat upset over the fuel boost pump location on my RV-4. (Under the front console as shown in the plans) Anybody find a different location that works better, both from saftey and mechanics? David Cahoon - Arkansas - Fininshing up canopy dcahoon(at)intellinet.com David Cahoon ( ) Jonesboro, Arkansas ( ) ) ^^ dcahoon(at)intellinet.com ( ) )^^ (____________) ___________ | \______________________(*)_____________________/ 0 Memphis Soaring Society ________________________________________________________________________________
Date: Jun 15, 1996
From: inet(at)intellisys.net (brian whatcott)
Subject: Re: Electrical conduit cut outs, wing
>I am at the point in building a RV-6A where the holes for the electrical conduit must > be drilled in the wing ribs. /// Nobody seems to have mentioned recently that it's a good idea to thread a string through a conduit for the NEXT time a wire needs pulling. There's always a next time. brian ________________________________________________________________________________
Date: Jun 15, 1996
Subject: Re: RV-3 Parts
From: William Curtis Chapin <wmchapin(at)dmci.net>
>I Still have the two new wing-tips and usable cowl for the RV-3. > Have not heard further from anyone--- > > They will be relegated to "permanent storage" soon What are your terms? Maybe I could store them alongside mine... ________________________________________________________________________________
Date: Jun 15, 1996
From: Greg Puckett <71155.2336(at)CompuServe.COM>
Rod Woodard
Subject: Screwed up VS
Well, I knew it was just a matter of time but it looks like I screwed up pretty bad. While dimpling for the VS skin for the forward spar using a C-frame tool, between hammer blows the skin lifted and the next blow put a nice new dimpled hole just next to the real one. I am now wondering should I just join the DIA club and order a new skin or try to salvage this one, here are my concerns that I hope some of you can give me your opinion of: - I believe that filling the hole with microballoons would cover things cosmetically but the two holes are touching each other, that is it's really only one big goofy looking hole. I re-dimpled the real hole and doing that flattened the unwanted holes dimple. With a rivet in the real hole it still looks like it would be ok cosmetically with ballons but I'm worried about the rivet not holding very well with a incomplete hole. - If I do just suck it up and order a new skin, how am I going to make sure I can final drill the holes accuratelly to the skeleton that I have that's already dimpled? Are there option any of you know of that I don't. Perhaps covering both of these holes with ballons and drilling a third close by for a real rivet? Just what I want is another hole, but that's probably the best thing structurally. Greg Puckett RV-8 sn 80081 ________________________________________________________________________________
From: jpl(at)showpg.mn.org (Joe Larson)
Subject: Re: Screwed up VS
Date: Jun 15, 1996
> While dimpling for the VS skin for the forward spar using a C-frame tool, > between hammer blows the skin lifted and the next blow put a nice new dimpled > hole just next to the real one. I am now wondering should I just join the DIA > club and order a new skin or try to salvage this one, here are my concerns that One bad rivet is not going to cause your airplane to fall out of the sky. My suggestion: put it together like you would have normally, and worry about cosmetic repairs later. However, you do want to make sure you get rid of any sharp edges so it doesn't promote cracking. -J -- Joe Larson jpl(at)showpg.mn.org 612-591-1037 Showpage Software, Inc. http://www.wavefront.com/~showpg 6121 St. Croix Ave. N. Golden Valley, Mn 55422 Future RV-6A pilot. ________________________________________________________________________________
Date: Jun 15, 1996
From: John Darby <johnd@our-town.com>
Subject: Re: Screwed up VS
Greg, That's not a big error. To me a big error is something like sawing the spar in half by mistake! Remember the spacing is usually shown as 'nominal', meaning approximately. So you add a new hole on or just over minimum clearance spacing either side (assuming it's not some very critical obstruction area) and there you put your 'construction' rivets. You just have the thing with some extra strength! Yes, the 'mistake' rivet is there, with a little micro to fill, may mess up the beautiful, even spacing, but if you're going for number one at Osh., and have unlimited funds, then start over completely. I wasn't and I didn't, and this is the way I corrected some of my 'little' goofs. And you know what? Now that the whole thing is finished, painted and flown, I have to remember hard and look close to see those that I thought were major problems at the time of construction. Press on and do what suits you best, but what you have described isn't really major, it just hurts your pride that you did it. I know, been there, done that. John D >Are there option any of you know of that I don't. Perhaps covering both of these >holes with ballons and drilling a third close by for a real rivet? Just what I >want is another hole, but that's probably the best thing structurally. > > > Greg Puckett > RV-8 sn 80081 > > > > John Darby RV6 N61764 flying johnd@our-town.com ________________________________________________________________________________
Date: Jun 15, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Screwed up VS
>- I believe that filling the hole with microballoons would cover things >cosmetically but the two holes are touching each other, that is it's really only >one big goofy looking hole. I re-dimpled the real hole and doing that flattened >the unwanted holes dimple. With a rivet in the real hole it still looks like it >would be ok cosmetically with ballons but I'm worried about the rivet not >holding very well with a incomplete hole. >Are there option any of you know of that I don't. Perhaps covering both of these >holes with ballons and drilling a third close by for a real rivet? Just what I >want is another hole, but that's probably the best thing structurally. Greg Puckett RV-8 sn 80081 Greg, I would suggest that you drill new holes on each side of the mis-drilled hole (utilizing the appropriate spacing) and rivet all three holes. If you really want peace of mind, call the factory. Hopefully, you will receive other input from this list so you don't base your actions on just my recommendation. Bob Skinner RV-6 ________________________________________________________________________________
From: av8r(at)hic.net
Date: Jun 15, 1996
Subject: Re: Screwed up VS
Greg Puckett wrote... >Well, I knew it was just a matter of time but it looks like I screwed >up pretty bad. While dimpling for the VS skin for the forward spar >using a C-frame tool, between hammer blows the skin lifted and the >next blow put a nice new dimpled hole just next to the real one. I am >now wondering should I just join the DIA club and order a new skin or >try to salvage this one,....SNIP Greg, If that is the biggest mistake you have on the A/C when finished, expect to pick up a "grand Champion" award.... IMHO go ahead and rivet and fill the extra "bit of hole" with some micro. When it is painted, there will be only you [and of course all of us other 499 listers ;)] who will know..... As for structure, so long as you dont have any cracks or sharp corners there should be no problem. To meet official specs not all rivets need to be perfect... so waht have you got - 1 bad in 100?. - I'll repeat my advice... any time you are feeling bad, go to the ramp and look - really look - closely at some spam-cans. Good luck with the rest Rob Lee N517RL - RV6A flying ________________________________________________________________________________
From: BrabstonD(at)aol.com
Date: Jun 15, 1996
Subject: Re: Spar bolts
reference the band saw. That brings back memories. When I was tapering my spar strips for my wing spars, I tried to buy a band saw. I looked at the typical $139.00 variety you find at Walmarts and Sears. When I found that they didn't sell aluminum cutting blases, I called Black & Decker and asked why. They told me that those saws could not be used to cut aluminum. They were made for wood only. They recommended that I purhcase the heavy metal shop version, $300 and up. I used the hollow ground planer blade and my table saw. I still think the typical inexpensive woodshop band saw would have done the job if I had ordered the blades special made. Has anyone tried that? Doug Brabston ________________________________________________________________________________
From: "Peter Bennett" <bennett(at)healey.com.au>
Date: Jun 16, 1996
Subject: Lycoming electronic ignition
Does anyone have info on the Lycoming electronic ignition? In particular, does it require dual batteries or any other precautions against single point of failure. Have details been published? I don't recall seeing this on the list but if it's had a run I'll use it as an excuse to learn about the archive search. Peter Bennett Sydney Australia RV6 fus out of jig ________________________________________________________________________________
Date: Jun 15, 1996
From: Pat McClung <pmc123(at)airmail.net>
Subject: Re: RV-3 Parts
William Curtis Chapin wrote: > > >I Still have the two new wing-tips and usable cowl for the RV-3. > > Have not heard further from anyone--- > > > > They will be relegated to "permanent storage" soon > > What are your terms? Maybe I could store them alongside mine... First come, first served---One group said they would pick them up but no show, no word. I would prefer someone make use of them rather than end up in someone's junk pile--that is where they came from! ________________________________________________________________________________
Date: Jun 15, 1996
From: inet(at)intellisys.net (brian whatcott)
Subject: Re: Spar bolts
>reference the band saw. > >That brings back memories. When I was tapering my spar strips for my wing >spars, I tried to buy a band saw. I looked at the typical $139.00 variety >you find at Walmarts and Sears. When I found that they didn't sell aluminum >cutting blases, I called Black & Decker and asked why. /// I found a metal-working bandsaw at a garage sale. I had been looking to buy the same model, which sells new for $180 The blades are under $10 each. It cuts up to 4 x 7 inch steel. It goes through 2 in diam hi-tensile alum rod no trouble. Cutting 1/8 inch slices is fun. It is a 'made in China' deal. brian ________________________________________________________________________________
Date: Jun 15, 1996
From: jmpcrftr(at)teleport.com (Michael McGee)
Subject: Thanks Bakersfield (chatter)
I just wanted to express my appreciation for the excellent flyin and feast put on by the Bakersfield EAA Ch 71 last weekend. We got there a little late but the talk by Jack Norris (?) was great. You folks have some tremendous resources down there, and lots of helping hands when a couple of us showed up with some bad-cylinder-karma. ...Ok, so I am a little aggressive on leaning when its 100 degrees, I'm from the northwest where best power always seems to be ok :). After 17 total hrs in a C-150 from Vancouver, WA to Bakersfield and back I had some nice white exhaust stacks. And if that trip in a C-150 isn't incentive to get busy building then nothing is! Special thanks to Bill Lewis for his services on sunday morning and to all those who loaned us tools to get us going and to get us both back home again. We hope to see some of you at the Northwest RV Flyin at Scappoose OR on June 22. And always on the first saturday of every month, the EAA Ch 105 Breakfast at Twin Oaks Airpark south of Hillsboro. Blue skies, Mike & Jackie sn's 23530 & 23596 ________________________________________________________________________________
From: BPattonsoa(at)aol.com
Date: Jun 15, 1996
Subject: Tubing Flares ... HELP
I know this is supposed to be educational, but not this frustrating. I am having the following problems trying to flare the 3003 soft alum. tubing for the brake/fuel lines: 1. The Imperial Eastman flaring tool I am using puts major circumferential ridges on the outside of the tube. 2. It also leaves a little ridge on the outside at the flare parallel to the tube. This is where the split is in the die holder. Problem #1 is not serious, this is. 3. An A&P friend, (a First Class craftsman, "assisting" with a Lancair IVP) says he does not use 3003 for anything, but uses the rigid tubing, I assume he means 5052. 4. I borrowed a "Rolo-Flair" tool from him. It does not leave the ridges on the outside, but does have problem #2. So, what is it opinion of the List? Bruce Patton -6A, with finishing kit, 3 months early. ________________________________________________________________________________
Date: Jun 16, 1996
From: Rion Bourgeois <RION(at)worldnet.att.net>
Subject: Re: Screwed up VS
>Well, I knew it was just a matter of time but it looks like I screwed up pretty >bad. While dimpling for the VS skin for the forward spar using a C-frame tool, >between hammer blows the skin lifted and the next blow put a nice new dimpled >hole just next to the real one. I am now wondering should I just join the DIA >club and order a new skin or try to salvage this one, here are my concerns that >I hope some of you can give me your opinion of: > >- I believe that filling the hole with microballoons would cover things >cosmetically but the two holes are touching each other, that is it's really only >one big goofy looking hole. I re-dimpled the real hole and doing that flattened >the unwanted holes dimple. With a rivet in the real hole it still looks like it >would be ok cosmetically with ballons but I'm worried about the rivet not >holding very well with a incomplete hole. > >- If I do just suck it up and order a new skin, how am I going to make sure I >can final drill the holes accuratelly to the skeleton that I have that's already >dimpled? > >Are there option any of you know of that I don't. Perhaps covering both of these >holes with ballons and drilling a third close by for a real rivet? Just what I >want is another hole, but that's probably the best thing structurally. > > > Greg Puckett > RV-8 sn 80081 > > > > Don't order a new skin yet. You probably don't need to do anything but fill the unwanted hole with the body putty of your choice: how much stress is ever imposed on the skins of the VS? If you want to exercise an abundance of caution, drill another #40 hole as far away as you can on the other side of the inadvertent one without hitting a flute, then countersink it for the smaller headed "oops" rivet, NAS1097AD3-3 or -4. These are available from Van's, and you will want a supply of them for attaching nutplates later. If you are careful in your countersinking, it will probably be invisible after painting. ________________________________________________________________________________
Date: Jun 15, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Tubing Flares ... HELP
>4. I borrowed a "Rolo-Flair" tool from him. It does not leave the ridges on >the outside, but does have problem #2. >Bruce Patton Bruce, I use the "Rolo-Flair". As you say, it does leave raised areas where the dies come together. I just went over to the bench grinder and buffed these bumps out with the Scotchbrite wheel. If you're careful, you can buff these out without touching the surrounding surfaces. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 15, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Lycoming electronic ignition
>Does anyone have info on the Lycoming electronic ignition? In >particular, does it require dual batteries or any other precautions >against single point of failure. Have details been published? > >I don't recall seeing this on the list but if it's had a run I'll use >it as an excuse to learn about the archive search. > >Peter Bennett Peter, The way I understand it, the Laser ignition package consists of regular magnetos with the addition of electronic ignition. If the electronic ignition fails, operation reverts to conventional mag operation. Neat idea. Kind of pricey, though. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 14, 1996
From: chester razer <crazer(at)egyptian.net>
Subject: Fuselage Jig Tip
Just finished riveting some of the aft fuselage side skins and though I'd post this tip for would be fuselage jig builders. When you make the 8"-10" triangular wood gussetts that are shown in the plans and are intended to add stability to the jig be sure they are at least 10" or more, you'll be forever laying tools, drills, clekos etc on them. If you really want to do it right add a small lip on the outby edge to keep clekos from rolling off on to the floor. chet razer: still haven't seen an RV6A in real life. ________________________________________________________________________________
Date: Jun 15, 1996
From: chester razer <crazer(at)egyptian.net>
Subject: Re: Spar bolts
aol.com!BrabstonD(at)matronics.com wrote: > > reference the band saw. > > That brings back memories. When I was tapering my spar strips for my wing > spars, I tried to buy a band saw. I looked at the typical $139.00 variety > you find at Walmarts and Sears. When I found that they didn't sell aluminum > cutting blases, I called Black & Decker and asked why. They told me that > those saws could not be used to cut aluminum. They were made for wood only. > They recommended that I purhcase the heavy metal shop version, $300 and up. > I used the hollow ground planer blade and my table saw. I still think the > typical inexpensive woodshop band saw would have done the job if I had > ordered the blades special made. Has anyone tried that? > > Doug Brabston Yes Doug, I purchased a Black & Decker Band saw from Wal Mart and put a B&D metal blade on it (14 tpi). I used my Radial Arm saw to taper my wing spar flange strips. So far the band saw has been great and I don't know how I ever got along without it. I believe it would work well for tapering the flanges. chet razer: riveting second aft side skin. ________________________________________________________________________________
Date: Jun 12, 1996
From: Fred Hiatt <hiatt001(at)gold.tc.umn.edu>
Subject: Re: Spar bolts
Finn Lassen wrote: > > Actually have a cheap one (fixed speed) but I ruined the blade trying > to cut 4130 steel. Didn't want to spend another $15 on a blade - > anyway, good exercise, and really makes you feel YOU are building the > plane (felt I was cheating a bit because bought old kit with wings > already skinned)! > Finn > > You wrote: > > > >RV>Finn (finished cutting the taper in horz stab spar flanges with > >RV>hacksaw - better than going to gym for workout!) > > > >RV>finnlass(at)ix.netcom.co > > > >OUCH!! Buy, beg, borrow or _steal_ a bandsaw!! My little brother's saw > >worked very nice for my HS flange cutting. :-) > > > >Rod Woodard > >RWoodard(at)lawyernet.com > > > > > >Try a bimetalic blade, more expensive, but it works. Fred Hiatt ________________________________________________________________________________
Date: Jun 12, 1996
From: Fred Hiatt <hiatt001(at)gold.tc.umn.edu>
Subject: Re: Spar bolts
aol.com!BrabstonD(at)matronics.com wrote: > > reference the band saw. > > That brings back memories. When I was tapering my spar strips for my wing > spars, I tried to buy a band saw. I looked at the typical $139.00 variety > you find at Walmarts and Sears. When I found that they didn't sell aluminum > cutting blases, I called Black & Decker and asked why. They told me that > those saws could not be used to cut aluminum. They were made for wood only. > They recommended that I purhcase the heavy metal shop version, $300 and up. > I used the hollow ground planer blade and my table saw. I still think the > typical inexpensive woodshop band saw would have done the job if I had > ordered the blades special made. Has anyone tried that? > > Doug BrabstonDoug, I hacked with a hand hacksaw for about 5 minutes. Then went and bought a 12" Delta bandsaw using a nonferrous metal blade. It cust 1/4" stock easily and I can still use it for wood, haven't broken a blade yet in 9 months. Just don't try to cut steel without an expensive bimetal blade. Fred Hiatt ________________________________________________________________________________
From: Blpzk(at)aol.com
Date: Jun 15, 1996
Subject: Boeing Surplus
Any scavengers (Portland area) want to go to Boeing Surplus with me next week? (any weekday except Monday) I'll brief you on the good deals if you buy me lunch. John Kimmel reply to: blpzk(at)aol.com ________________________________________________________________________________
Date: Jun 15, 1996
From: Tim Lewis <lewis2(at)mailcenter.cmet.af.mil>
Subject: Tools (band saw blade)
I took the advice of several people on this list and returned my direct drive, oil free compressor. The replacement ($290 from Sams) is a 5 hp, 20 gal belt drive, oil bath compressor. Y'all were right... much quieter. Thanks. Problem de jour: I bought a 300-3000 rpm, Black and Decker band saw. Black and Decker's customer service folks tell me that one isn't supposed to use their saws for metal, but after reading the RV list archives on the subject I'm convinced it won't be a problem if I use the proper blade. (Or am I confused?) Black and Decker doesn't make a bi-metal blade for their saws (according to their customer service line), and I've not had any luck finding one that'll fit (the required length is 59 1/4 inches). I've been able to find 56 1/8 inch bi-metal blades no problem, but that doesn't help. Any suggested sources or advice? Thanks, Tim Lewis RV-6A(Q) Waiting for delivery ________________________________________________________________________________
From: OrndorffG(at)aol.com
Date: Jun 15, 1996
Subject: Re: adddress's
Howard, The Orndorff's address is orndorffg(at)aol.com. Please feel free to send us any and all of your questions. George and Becki ________________________________________________________________________________
From: "Michael C. Gamble" <mgamble(at)chiba.netxn.com>
Subject: Thanks Bakersfield (chatter)
Date: Jun 15, 1996
------ =_NextPart_000_01BB5AFA.F32913E0 Hi Gang: I went today to the Portervile, CA fly in and got to see the RV8 up = close and personal! Cool is all I can say. There were several RV-4s, 3s, = and a harmod Rocket. Had fun, where did I put my check book? Mick ---------- From: Michael McGee[SMTP:teleport.com!jmpcrftr(at)matronics.com] Sent: Saturday, June 15, 1996 4:39 PM Subject: RV-List: Thanks Bakersfield (chatter) I just wanted to express my appreciation for the excellent flyin and = feast put on by the Bakersfield EAA Ch 71 last weekend. We got there a little late but the talk by Jack Norris (?) was great. You folks have some tremendous resources down there, and lots of helping hands when a couple = of us showed up with some bad-cylinder-karma. ...Ok, so I am a little aggressive on leaning when its 100 degrees, I'm from the northwest where best power always seems to be ok :). After 17 total hrs in a C-150 from Vancouver, WA to Bakersfield and back I had some nice white exhaust = stacks. And if that trip in a C-150 isn't incentive to get busy building then nothing is! Special thanks to Bill Lewis for his services on sunday morning and to = all those who loaned us tools to get us going and to get us both back home = again.=20 We hope to see some of you at the Northwest RV Flyin at Scappoose OR on = June 22. And always on the first saturday of every month, the EAA Ch 105 Breakfast at Twin Oaks Airpark south of Hillsboro. Blue skies,=20 Mike & Jackie sn's 23530 & 23596 ------ =_NextPart_000_01BB5AFA.F32913E0 eJ8+IjcDAQaQCAAEAAAAAAABAAEAAQeQBgAIAAAA5AQAAAAAAADoAAENgAQAAgAAAAIAAgABBJAG AKQDAAACAAAAFAAAAAMAADAFAAAACwAPDgAAAAACAf8PAQAAAEkAAAAAAAAAgSsfpL6jEBmdbgDd AQ9UAgAAAABydi1saXN0QG1hdHJvbmljcy5jb20AU01UUABydi1saXN0QG1hdHJvbmljcy5jb20A AAAAHgACMAEAAAAFAAAAU01UUAAAAAAeAAMwAQAAABYAAABydi1saXN0QG1hdHJvbmljcy5jb20A AAAeABoAAQAAABQAAABSRVBPUlQuSVBNLk5PVEUuTkRSAEAAMgBg6mIjNVu7AQMABAwAAAAAAwAF DP////8DABUMAAAAEAMA/g8GAAAAHgABEAEAAABEAAAATm8gdHJhbnNwb3J0IHByb3ZpZGVyIHdh cyBhdmFpbGFibGUgZm9yIGRlbGl2ZXJ5IHRvIHRoaXMgcmVjaXBpZW50LgAeAAEwAQAAABgAAAAn cnYtbGlzdEBtYXRyb25pY3MuY29tJwACAQswAQAAABsAAABTTVRQOlJWLUxJU1RATUFUUk9OSUNT LkNPTQAAAwAAOQAAAAACARI6AQAAAEkAAAAAAAAAgSsfpL6jEBmdbgDdAQ9UAgAAAABydi1saXN0 QG1hdHJvbmljcy5jb20AU01UUABydi1saXN0QG1hdHJvbmljcy5jb20AAAAAHgATOgEAAAAYAAAA J3J2LWxpc3RAbWF0cm9uaWNzLmNvbScAAgEUOgEAAAAbAAAAU01UUDpSVi1MSVNUQE1BVFJPTklD Uy5DT00AAAsAQDoBAAAAAgH2DwEAAAAEAAAAAAAABQ4AAAADAAAwBgAAAAsADw4BAAAAAgH/DwEA AABJAAAAAAAAAIErH6S+oxAZnW4A3QEPVAIAAAAAcnYtbGlzdEBtYXRyb25pY3MuY29tAFNNVFAA cnYtbGlzdEBtYXRyb25pY3MuY29tAAAAAB4AAjABAAAABQAAAFNNVFAAAAAAHgADMAEAAAAWAAAA cnYtbGlzdEBtYXRyb25pY3MuY29tAAAAHgAaAAEAAAAIAAAASVBNLk5PVEUDABUMAQAAAAMA/g8G AAAAHgABMAEAAAAYAAAAJ3J2LWxpc3RAbWF0cm9uaWNzLmNvbScAAgELMAEAAAAbAAAAU01UUDpS Vi1MSVNUQE1BVFJPTklDUy5DT00AAAMAADkAAAAAAgEUOgEAAAAQAAAAyK0DlNDGzxG3WjS8/cAE HwsAQDoBAAAAAgH2DwEAAAAEAAAAAAAABuTJAQiABwAYAAAASVBNLk1pY3Jvc29mdCBNYWlsLk5v dGUAMQgBBIABACoAAABSRTogUlYtTGlzdDogVGhhbmtzIEJha2Vyc2ZpZWxkIChjaGF0dGVyKQD9 DQEFgAMADgAAAMwHBgAPABQAKAAkAAYATgEBBgAHABgAAABJUE0uTWljcm9zb2Z0IE1haWwuTm90 ZQAxCAEggAMADgAAAMwHBgAPABQAIQAsAAYATwEBCYABACEAAABDOEFEMDM5NEQwQzZDRjExQjc1 QTM0QkNGREMwMDQxRgBbBwEDkAYARAcAABMAAAALACMAAAAAAAMAJgAAAAAACwApAAAAAAADADYA AAAAAEAAOQBgwDSUNVu7AR4AcAABAAAAKgAAAFJFOiBSVi1MaXN0OiBUaGFua3MgQmFrZXJzZmll bGQgKGNoYXR0ZXIpAAAAAgFxAAEAAAAWAAAAAbtbNQOqlAOtycbQEc+3WjS8/cAEHwAAHgAeDAEA AAAFAAAAU01UUAAAAAAeAB8MAQAAABgAAABtZ2FtYmxlQGNoaWJhLm5ldHhuLmNvbQADAAYQFaYP rgMABxCMBAAAHgAIEAEAAABlAAAASElHQU5HOklXRU5UVE9EQVlUT1RIRVBPUlRFUlZJTEUsQ0FG TFlJTkFOREdPVFRPU0VFVEhFUlY4VVBDTE9TRUFORFBFUlNPTkFMQ09PTElTQUxMSUNBTlNBWVRI RVJFV0VSRQAAAAACAQkQAQAAAJcFAACTBQAAxggAAExaRnUC5LoZ/wAKAQ8CFQKoBesCgwBQAvIJ AgBjaArAc2V0MjcGAAbDAoMyA8UCAHByQnER4nN0ZW0CgzN3AuQHEwKAfQqACM8J2TvxFg8yNTUC gAqBDbELYOBuZzEwMxRQCwoUUQUL8mMAQCBIaSBHxRkBOgqFSSB3CfAFQDJ0BHBheRxBHEBoZSwg UBWxBJB2AxBlLHAgQ0EgGOAckAuAIKEAcGQgZ28cMiARsAcdABziB/BWOCB1cFwgYxWgEbAec3AE kHPrAiAHQCEd0G8G8B5ABCBXB0ADIBvgYwORcxyALnwgVBzwFhAb8SMREbB2RwSQB0AfsS00cx3A M3MkUR6CYSARgQRhB/FjJmsRwCLASGEeoGZ1ym4dwHci82RpHqAb4HRwdQVAbRyQEXAFkGtiIAbg b2s/CoUKhU0OaSWwKIwK9GxpMTiCMALRaS0xNDQN8OcM0CuDC1kxNgqgA2AT0PpjBUAtLacKhyxb DDAtJvpGA2E6Lq4tJgyCKVIRgBJlD7FjRwngW1NNWFRQOhPQHaBwFbEuwQWgbSFqbXAFAAGAvHJA AMA0wAIgKXBzNBL+XS5PL10GYAIwMI8xmwYQbnQIcBxxHcBKJmAdADECNR3AMTk5NiA0aDozOR0Q TTXfL11U7m84HzGbHXAtKuATwDTs4zvvNu51YmotYT4PMZu9JBFMQCFDoCLgAHBrBCB8QmElwBGg K1AysB6gKDcRcQJABJApKa8qszM2zywnGkUtJhvganUTwBvwzwBwE9AeoByxZXgTUAeQUwQgJ6Fh cEwBYwcwdL5pAiAeAAWxHOJL4GMysI8doBwhHhEeVWZlYRPAdwqFJ2JNMWIckRzxRopFwkEd8ENo IDca0Atgn0sSCeAlwB6QIsAgVx0A/x7DIvMlACrgAkAdoAqFC2DfE9AoICdxHOIBkGwoERyQdkoA 0CgQTgWwBRAEICh8PylLMQQgCcE1AFLhWf8IYE1RVcAEIBGAI7AfIANw/1RWNMAT4FKxCGAEIEwR CGH3TgAEIFngdwOgU4MkpBWgsnQEIG9mJRAysHALgP5nJREekAQgJqEeYSAgCGCfC1AdAFwgCoVa AXNoWuB/S4EgAQPwHOBYwyggJiAtnGN5KuAekASQLWslMcphIsAuYVBPax3AIQDJG9FhbVPeYWcJ wQQQ/mlYoU0xHaAAcFySXTNUEGsEIBkwMCbwZQnCJFFJridiIANSHNNuFbFoHAD3SxIi8gqFYmci M9AjQSHh90tAE7AfIm0EIByxaCBQEGkoEDopUuFBAYBooTH+NxxBVaElEBGgHkMd0Ctw7jVlQANS CoVWAHBdoSOx/R3AVx3wHLFGih6CYBAoAb8b4BGAHqBfwzVBIyFoVBB/TcIRgEsCE8BWMTVwCoVB /x6RBpAc0TUAWXEFIGuqBAD8bicFQAuATgACMGOiHLH2ZxHAVRFzHJBVIAMQJwD7XKEc4W4KhWbA HOBckgQA+iEojFMg0EzhAyByoUZC923yAxADIEwH0CHBTWJwgO9pIh1xWpJNMXMmYBxyBGD/BKBc kh6CHLEh8VkWXuAgYf8moBzAFaAAcF8SaYIG8GmD/3UiWgEewHxJf2UG4F+RbyP/XuBf4WMwC3Ei wCiMUxFe4O8g0B72X8NcIXlX8XLCHPH/VnFm9R/AMDBOlDexIlBMoHMhgCBhT1JQEjqSCoUy/jJq UiTSaORNMRziK1ARoL9xMToFXBIjonviAjBoHcBXHOJRhRkwNQqFQldxa7ZmUjJywVQD8AOgT0aQ /QQgQYoACrEoEFpRX5FcIfsa8CIAcwbgA2BxtozGCkE9HyBrCJAkUSj3JcAgJh9WEwiQCoV0AQQg MjM1/jNlQJKwk/E7QCiMR99I7xdJ/AqFFTEAmVAAAwAQEAAAAAADABEQAAAAAEAABzBgiqKeNFu7 AUAACDBgiqKeNFu7AQIBFDoBAAAAEAAAAMitA5TQxs8Rt1o0vP3ABB8eAD0AAQAAAAUAAABSRTog AAAAAHtA ------ =_NextPart_000_01BB5AFA.F32913E0-- ________________________________________________________________________________
From: EBundy2620(at)aol.com
Date: Jun 16, 1996
Subject: Re: Wingtip lighting
<< t gives you one more strobe that might just keep somebody from running up your tail. Regards: Rusty Gossard >> Wait a minute Rusty - isn't that why we're building an RV in the first place? So noboby CAN run up our tail? Personally, I'm getting tired of being passed by birds in a Cessna. -- Ed Bundy ________________________________________________________________________________
From: EBundy2620(at)aol.com
Date: Jun 16, 1996
Subject: Re: Aircraft Spruce
<< happy with aircraft screwup.... they consistly overcharge on their shipping.... they don't know what you are talking about when you're trying to order something..they will ship a partially filled order so you have to pay the overcharged shipping twice....(which I think do with glee) they are back ordered. >> I've had some bad experience with ACS, but they usually solve any problems to my satisfaction. On the plus side they ship FREE if your order is over $500 (not usually a problem for me ) and they don't charge a handling fee, just shipping. For example, Van's charges an additional $4 handling fee for just about anything. Plus, I have NEVER been billed additional shipping charges on a back ordered item. I think it must have been a mistake. For the bewildering array of items they carry, IMHO they do a pretty good job. Ed Bundy ebundy2620(at)aol.com ________________________________________________________________________________
Date: Jun 15, 1996
From: n21pe(at)ix.netcom.com (Peter B. Mortensen)
Subject: Re: Tools (band saw blade)
You wrote: >Problem de jour: I bought a 300-3000 rpm, Black and Decker band saw. >Black and Decker's customer service folks tell me that one isn't supposed >to use their saws for metal, but after reading the RV list archives on the >subject I'm convinced it won't be a problem if I use the proper blade. >(Or am I confused?) Black and Decker doesn't make a bi-metal blade for >their saws (according to their customer service line), and I've not had >any luck finding one that'll fit (the required length is 59 1/4 inches). >I've been able to find 56 1/8 inch bi-metal blades no problem, but that >doesn't help. Any suggested sources or advice? > > >Thanks, > >Tim Lewis >RV-6A(Q) >Waiting for delivery > Tim, I go to my local tool supplier (Arenson) and they can make up any size bandsaw blade I want. I just bring in my old broken one and they make me a custom one to the same length. They have reels and reels of all kinds of different tooth pattern blades. They weld them together custom and it costs no more than buying them elsewhere. ($6 as I recall). For aluminum get a blade that is fairly wide with widely spaced teeth. Get a "skip tooth" if you can. The only difference between a metal cutting and a wood cutting bandsaw is the speed. The metal saw has an extra belt and pulley to slow down the blade speed. If you put a widely spaced tooth blade on a wood bandsaw, it will cut aluminum just fine. Peter B. Mortensen n21pe(at)ix.netcom.com _______________________________________________ ________________________________________________________________________________
Date: Jun 15, 1996
From: ammeterj(at)seanet.com (John Ammeter)
Subject: Re: Tools (band saw blade)
>I took the advice of several people on this list and returned my direct >drive, oil free compressor. The replacement ($290 from Sams) is a 5 hp, >20 gal belt drive, oil bath compressor. Y'all were right... much >quieter. Thanks. > >Problem de jour: I bought a 300-3000 rpm, Black and Decker band saw. >Black and Decker's customer service folks tell me that one isn't supposed >to use their saws for metal, but after reading the RV list archives on the >subject I'm convinced it won't be a problem if I use the proper blade. >(Or am I confused?) Black and Decker doesn't make a bi-metal blade for >their saws (according to their customer service line), and I've not had >any luck finding one that'll fit (the required length is 59 1/4 inches). >I've been able to find 56 1/8 inch bi-metal blades no problem, but that >doesn't help. Any suggested sources or advice? > > >Thanks, > >Tim Lewis >RV-6A(Q) >Waiting for delivery > > > I've had good luck getting blades from a local shop where they build your blade from stock to whatever length you need. They simply weld the blade stock to the length you want. Call around in your area; I'm sure you'll be able to find what you need. If you can't I could probably get my local supplier to send you what you need. John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA RV-6 N16JA Flying 5 years ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 16, 1996
Subject: Re: Frank Zappa vs the RV builders
Mike- Glad to hear that there are other Zappa fans building planes. Still crazy after all these years. Escape from the weight of your Corporate Logo!-FZ Vanremog(at)aol.com N1GV ________________________________________________________________________________
From: Rvbildr(at)aol.com
Date: Jun 16, 1996
Subject: Re: Aircraft Spruce
Speaking of shipping,watch out for Roadway trucking! I ordered a Steve Frey RV-6 fuselage jig. It was missent to Lubbock, Tx instead of Ga., then it got lost in Dallas for a day or two. It finally arrived after 2 weeks in very sad shape. Some of the damage looked as though it had to be intentional. Now I have to hassle with them to send an inspector out and then return the jig. Then the process will start all over again!!!!!!!!!!!!!!!!! Mal rvbildr(at)juno.com waiting............... ________________________________________________________________________________
Date: Jun 16, 1996
From: DM Cooke <dmcooke(at)rand.nidlink.com>
Subject: Re: Spar bolts
Ref. Band Saw. I purchased a 12" band saw from Harbor Freight (1-800-423-2567) for $99. It works great. I buy my blades mail order from: Supercut Bandsaw Co., Inc. N2705 HWY 41 Post Falls, Idaho 83854 1-208-773-3546 I purchased the 62" length, 3/8" width, 14tooth blade. What a cut-up. :-) Dave Cooke dmcooke(at)rand.nidlink.com ________________________________________________________________________________
Date: Jun 16, 1996
From: Bob Skinner <BSkinner(at)ltec.net>
Subject: Re: Tools (band saw blade)
>Problem de jour: I bought a 300-3000 rpm, Black and Decker band saw. >Black and Decker's customer service folks tell me that one isn't supposed >to use their saws for metal, but after reading the RV list archives on the >subject I'm convinced it won't be a problem if I use the proper blade. >(Or am I confused?) Black and Decker doesn't make a bi-metal blade for >their saws (according to their customer service line), and I've not had >any luck finding one that'll fit (the required length is 59 1/4 inches). >I've been able to find 56 1/8 inch bi-metal blades no problem, but that >doesn't help. Any suggested sources or advice? >Tim Lewis Tim, If you can get a blade with 14 TPI and operate the saw at 300 rpms and use some cutting fluid, I'll bet you'll get along OK. I have used a cheap 3-wheel band saw and have found that if I apply a bead of LPS TAP-ALL tapping fluid (ACS, page 234, '95-'96 catalog) down the cut line that the band saw blade will last a very long time. I use this, even on thin material. Bob Skinner RV-6 BSkinner(at)ltec.net ________________________________________________________________________________
Date: Jun 16, 1996
From: Rick Osgood <74774.54(at)CompuServe.COM>
Subject: Wing - order of build
I am looking for input on the following issue. The Frank Justice supplements do not have you skin the leading edge until later in the whole process. He has you do the ribs and aligned everything but then has you do the Ailerons. George Orndorff builds the ribs, skins the leading edge and then the tank. How have others done this and which way worked better for you? Any and all opinions would be appreciated. Thanks RV6 left wing Rick 74774.54(at)compuserve.com ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 16, 1996
Subject: Re: Wingtip lighting
> ><< t gives you one more strobe that might just keep somebody from running up > your tail. > Regards: > Rusty Gossard >> > >Wait a minute Rusty - isn't that why we're building an RV in the first place? > So noboby CAN run up our tail? Personally, I'm getting tired of being >passed by birds in a Cessna. > >-- Ed Bundy Ed: Think about it the next time your cutting through the local MOA when a flight of lawn darts hauls ass by al low level..... and I have only been passed by 1 single engined GA aircraft. A Mirage. But passed him after we landed as he was sitting at the fuel truck.:) Regards: Rusty Gossard N47RG Flying ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 16, 1996
Subject: Re: Tools (band saw blade)
> >>Problem de jour: I bought a 300-3000 rpm, Black and Decker band saw. >>Black and Decker's customer service folks tell me that one isn't supposed >>to use their saws for metal, but after reading the RV list archives on the >>subject I'm convinced it won't be a problem if I use the proper blade. BOY am I glad I didn't know all this before I bought my band saw. I bought a 8 inch POJ (piece of junk) band saw from the local hardware store and used it for 3 years using just the standard metal cutting blade. Worked great. I finally went to Sears and got a 10 inch to have the extra room for cutting and to have a better choice of blades. I have had NO trouble cutting just about anything I needed to cut and the thing cost $85 for the small one and $109 for the larger one. My only objection to the Sears model is that no one sells the blade size except Sears. BUT there is a hardware store near that will weld up whatever size and blade style I need. Have never used their services. Bimetal?? Most of my cutting is Aluminum. Synopsis: the Ordinary Shop Tools usually work just fine and I can spend my hard earned cash on things for the airplane. Michael Kosta RV-4 232SQ Fly By July (or August, September, I don't know. What?) ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 16, 1996
Subject: Re: Fire extinguisher
>In the last Sport Aviation there is an article by Tony B. that shows a >picture of his RV-3 with a fire extinguisher system installed. This looks >like a good thing that we all probably overlook or leave out. Let's visit >this idea. Sport Aviation May 1994 features an article on Dean Hall's RV-4 and he has a Halon system installed for the fire wall forward. It's a neat system and he says it only added 4 pounds. If you look at the photo at the bottom of page 81 of the engine, the tubing that is at the very top of the engine ending in a blue fitting is the engine block outlet. I think there are 2 more in the engine compartment. The GO knob is a large red doorknob-looking thing in the cockpit. The system is the Phoenix system from International Safety Systems, 2227 Idlewood Rd, Suite 4, Tucker GA, 30084; 404-938-2166 if they're still in business. Michael Kosta RV-4 232SQ Fly By July (or..........) ________________________________________________________________________________
Date: Jun 16, 1996
Subject: Re: RV-3 Parts
From: William Curtis Chapin <wmchapin(at)dmci.net>
>First come, first served---One group said they would pick them up but no >show, no word. I would prefer someone make use of them rather than end >up in someone's junk pile--that is where they came from! Where are the parts located? ________________________________________________________________________________
Date: Jun 13, 1996
From: Fred Hiatt <hiatt001(at)gold.tc.umn.edu>
Subject: Re: Tools (band saw blade)
Tim Lewis wrote: > > I took the advice of several people on this list and returned my direct > drive, oil free compressor. The replacement ($290 from Sams) is a 5 hp, > 20 gal belt drive, oil bath compressor. Y'all were right... much > quieter. Thanks. > > Problem de jour: I bought a 300-3000 rpm, Black and Decker band saw. > Black and Decker's customer service folks tell me that one isn't supposed > to use their saws for metal, but after reading the RV list archives on the > subject I'm convinced it won't be a problem if I use the proper blade. > (Or am I confused?) Black and Decker doesn't make a bi-metal blade for > their saws (according to their customer service line), and I've not had > any luck finding one that'll fit (the required length is 59 1/4 inches). > I've been able to find 56 1/8 inch bi-metal blades no problem, but that > doesn't help. Any suggested sources or advice? > > Thanks, > > Tim Lewis > RV-6A(Q) > Waiting for delivery Tim, You can use a 14 tooth blade for alum. You should be able to run it at the normal speed for wood. The only time you need a bimetallic blade (moving slow) is with ferrous metals. Fred Hiatt ________________________________________________________________________________
Date: Jun 17, 1996
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Re: Fire extinguisher
David, This is of great interest. Fire is the nightmare in a forced landing. There was an article in Sports Aviation about a very nice fully optioned RV4 that had a halon system installed in the cabin (late 1994 I think). Halon is now unavailable in Australia due to environmental laws, I would be interested to hear of alternative systems people have used. Leo Davies, RV6A. >In the last Sport Aviation there is an article by Tony B. that shows a >picture of his RV-3 with a fire extinguisher system installed. This looks >like a good thing that we all probably overlook or leave out. Let's visit >this idea. >Most race cars have some type system that pipes "halon" gas to vital trouble >spots. i seems this could be done with alum. tubing to the carb.,rear case, >battery without a great expense. Any thoughts or have you seen such a >system. I wrote Tony for details. > One thing that started this was my A&P was somewhat upset over the >fuel boost pump location on my RV-4. (Under the front console as shown in >the plans) >Anybody find a different location that works better, both from saftey and >mechanics? >David Cahoon - Arkansas - Fininshing up canopy >dcahoon(at)intellinet.com >David Cahoon ( ) >Jonesboro, Arkansas ( ) ) ^^ >dcahoon(at)intellinet.com ( ) )^^ > (____________) ___________ > | > \______________________(*)_____________________/ > 0 > Memphis Soaring Society > > > ________________________________________________________________________________
Date: Jun 17, 1996
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Re: Screwed up VS
>Well, I knew it was just a matter of time but it looks like I screwed up pretty >bad. While dimpling for the VS skin for the forward spar using a C-frame tool, >between hammer blows the skin lifted and the next blow put a nice new dimpled >hole just next to the real one. I am now wondering should I just join the DIA >club and order a new skin or try to salvage this one, here are my concerns that >I hope some of you can give me your opinion of: > >- I believe that filling the hole with microballoons would cover things >cosmetically but the two holes are touching each other, that is it's really only >one big goofy looking hole. I re-dimpled the real hole and doing that flattened >the unwanted holes dimple. With a rivet in the real hole it still looks like it >would be ok cosmetically with ballons but I'm worried about the rivet not >holding very well with a incomplete hole. > >- If I do just suck it up and order a new skin, how am I going to make sure I >can final drill the holes accuratelly to the skeleton that I have that's already >dimpled? > >Are there option any of you know of that I don't. Perhaps covering both of these >holes with ballons and drilling a third close by for a real rivet? Just what I >want is another hole, but that's probably the best thing structurally. > > > Greg Puckett > RV-8 sn 80081 > > > > Greg, Put in an extra rivet between the goof and the next planned rivet (both sides) Then just smooth off your new lightning hole. If you replace every skin you make a blemish in you will enrich Alcoa beyond their wildest dreams. Leo > ________________________________________________________________________________
Date: Jun 16, 1996
From: Hal & Suzanne Smith <smithhm(at)phoenix.net>
Subject: Re: Screwed up VS
> Greg Puckett > RV-8 sn 80081 Greg, I to dimpled the skin next to the actual hole. I called Van's about it and they said "not to worry". When you get ready to prime the piece just fix the hole first. We all seem to goof at times. We just hope it is recoverable. Hal Smith (Riviting the wing spars) ________________________________________________________________________________
Date: Jun 17, 1996
From: John Morrissey <John.Morrissey(at)its.csiro.au>
Subject: Re: Fire extinguisher
Hi Leo, Actually you can get a special dispensation for the use of Halon Fire extinguisher's in Australia. I received a letter from the Lands and Environment department asking if I wanted to register a Halon extinguisher for use in my Jodel D11. I can get you the address if your interested. BTW I will give you a call tonight about that jig. I would like to take you up on your offer. I will probably Beg/Steal/hire a car trailer to pick it up. Regards John Morrissey >David, >This is of great interest. Fire is the nightmare in a forced landing. There >was an article in Sports Aviation about a very nice fully optioned RV4 that >had a halon system installed in the cabin (late 1994 I think). Halon is now >unavailable in Australia due to environmental laws, I would be interested to >hear of alternative systems people have used. > >Leo Davies, >RV6A. >>In the last Sport Aviation there is an article by Tony B. that shows a >>picture of his RV-3 with a fire extinguisher system installed. This looks >>like a good thing that we all probably overlook or leave out. Let's visit >>this idea. >>Most race cars have some type system that pipes "halon" gas to vital trouble >>spots. i seems this could be done with alum. tubing to the carb.,rear case, >>battery without a great expense. Any thoughts or have you seen such a >>system. I wrote Tony for details. >> One thing that started this was my A&P was somewhat upset over the >>fuel boost pump location on my RV-4. (Under the front console as shown in >>the plans) >>Anybody find a different location that works better, both from saftey and >>mechanics? >>David Cahoon - Arkansas - Fininshing up canopy >>dcahoon(at)intellinet.com >>David Cahoon ( ) >>Jonesboro, Arkansas ( ) ) ^^ >>dcahoon(at)intellinet.com ( ) )^^ >> (____________) ___________ >> | >> >\______________________(*)_____________________/ >> 0 >> Memphis Soaring Society >> >> >> > > > ________________________________________________________________________________
From: Cecil Hatfield / Fourstar Printing <cecil(at)alto1.altonet.com>
Date: Jun 16, 1996
Subject: Re: Wingtip lighting
Wait a minute Rusty - isn't that why we're building an RV in the first place? So noboby CAN run up our tail? Personally, I'm getting tired of being passed by birds in a Cessna. The bird in the Cessna, did he have a smile on? Cecil ________________________________________________________________________________
Date: Jun 16, 1996
From: "Thomas N. Martin" <103212.65(at)CompuServe.COM>
Subject: hand helds
Hi all I would like to purchase a hand held com/vor for my RV-4. I have a terra com now and it is almost always Ok but I would like a backup I need advice on which ones are reliable,and cheap or course, and what options should I buy. Thanks in advance, Tom Martin RV-4 the RaVen 130 hours and climbing ________________________________________________________________________________
Date: Jun 16, 1996
From: Michael Harris <mharris(at)mail.microsys.net>
Subject: Another screwed up VS.
Hi all. I am working on the VS - I have assembled the entire skeleton and was getting ready to rivet on the skin (I have pre-drilled pilot holes per the Orndorf video...). Unfortunately, I noticed that I measured the VS 406 angle incorrectly - I measured the 1 1/2" offset from a vertical from a line drawn on the wrong side of the VS406. As consequence, the end rib is not at the correct angle - it's closer to vertical than it should be. Another problem is that I've already pilot drilled the skin which of course conforms to the incorrect angles. I have left it as it is - I have to decide how much to rebuild - or is it feasible to use it as it is? Any advice appreciated... Despondently yours, MIKE HARRIS ________________________________________________________________________________
From: EBundy2620(at)aol.com
Date: Jun 16, 1996
Subject: Re: Spar bolts
<< hat brings back memories. When I was tapering my spar strips for my wing spars, I tried to buy a band saw. I looked at the typical $139.00 variety you find at Walmarts and Sears. When I found that they didn't sell aluminum cutting blases, I called Black & Decker and asked why. They told me that those saws could not be used to cut aluminum. They were made for wood only. They recommended that I purhcase the heavy metal shop version, $300 and up. I used the hollow ground planer blade and my table saw. I still think the typical inexpensive woodshop band saw would have done the job if I had ordered the blades special made. Has anyone tried that? >> Actually, reg'lar old wood cutting blades work fine. Aluminum is a very soft metal and is only slightly tougher to cut. I'm using a cheapie bandsaw and I've gone through about 5 blades at $7 each. Not too bad. Just DON'T use it on steel. It won't cut, and it's time to buy a new blade. Ed Bundy ________________________________________________________________________________
Date: Jun 17, 1996
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: pro-sealed joints
I have read comments on the list to the extent that Pro-seal produces a weaker joint than a plain riveted seam (? because of greater distance between the surfaces). Well it may be so but I would want to see the data. I discovered last weekend that I had installed my firewall recess upside down (ie boxy part at the top). I bit the bullet and removed it. During installation I had put a pro-seal bead underneath the flange to fume proof the joint. I am here to tell you that with all rivets drilled and punched out that joint was still a structural entity. It took me an hour and a half with a chisel and pliers.....lift the seam for a millimetre, bend away flange, lift, bend etc...... to get that damn recess off. I would cheerfully do aerobatics in a plane built with pro-seal and no rivets. I would build bridges with pro-seal. If they'd pro-sealed that O ring in place the Challenger would still be with us......etc Yours, waiting for a new piece of SS for a new recess, Leo Davies 6A, out of the jig, big hole in the firewall. ________________________________________________________________________________
Date: Jun 16, 1996
From: crazer(at)egyptian.net (Abby Razer)
Subject: Re: Wing - order of build
>I am looking for input on the following issue. > >The Frank Justice supplements do not have you skin the leading edge until >later in the whole process. He has you do the ribs and aligned everything >but then has you do the Ailerons. George Orndorff builds the ribs, skins the >leading edge and then the tank. How have others done this and which way >worked better for you? > > >Any and all opinions would be appreciated. > > >Thanks >RV6 left wing >Rick 74774.54(at)compuserve.com I followed Georges video without any problems, in fact I've followed his empennage, wing and now fuselage videos. I also use Frank's written text for more detailed information. Between the two and the construction manuel and this list, combined with brain power you should get the job done. Stick to the basics, you'll have edge distance problems, dimpling and countersinking problems and lots of other problems but remember, always take the big problems and make little ones out of them, then solve the little problems and the big ones will take care of themselves. chet razer: still haven't seen a 6A in real life. Abby Razer e-mail: crazer(at)egyptian.net ________________________________________________________________________________
From: EPTS72A(at)prodigy.com (MR HAROLD J DOWNES)
Date: Jun 16, 1996
Subject: Re: Spar bolts
I have used a Sears $139 bandsaw with metal cutting blades to do all my aluminum cutting. The blades are available from the Sear catalog and seem to work fairly well if you don't force the saw too much on thick stuff. Hal N969HD RV6A ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 17, 1996
Subject: Re: hand helds
IMNSHO get the Bendix-King KX-99 handheld. Discount shops have for around $500. It comes with Ni-Cd battery pack, is rugged, has good key action, has OBS and has NOAA weather channels to boot. TX, RX and VOR are solid and reliable. Make sure you get the adapter cable assy for your headset (in case your panel mount comm goes belly up) and the optional Alkaline Battery Pack. Further, I find that a cable from cigarette lighter to 12V input is handy to have in order to maintain charge during long flights between charging opportunities. I have a fused aux 12V outlet on the plane. N1GV Vanremog(at)aol.com ________________________________________________________________________________ Importance: normal
Subject: exhaust system for RV 4
From: Klaus Roth <rothk(at)oims.med.siemens.de>
Date: Jun 17, 1996
Because I have to add two additional mufflers, I can not use a 4 pipe system for the RV 4. I saw a cross over system in the Aircraft spruce catalog. Does anyone know this system ?? Any advise is greatly appreciated. Klaus Roth Germany RV 4 klaus.roth(at)med.siemens.de ________________________________________________________________________________
From: JDC999(at)aol.com
Date: Jun 17, 1996
Subject: Re: Downloading RV-archive digest
unsuscribe ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 17, 1996
Subject: Re: exhaust system for RV 4
>Because I have to add two additional mufflers, I can not use a 4 pipe > system for the RV 4. > >I saw a cross over system in the Aircraft spruce catalog. > >Does anyone know this system ?? > >Any advise is greatly appreciated. >


June 06, 1996 - June 17, 1996

RV-Archive.digest.vol-bn