RV-Archive.digest.vol-cx

May 26, 1997 - June 01, 1997



      > 
      >     Bob . . .
      >     AeroElectric Connection
      >                    ////
      >                   (o o)
      >     ==========oOOo=(_)=oOOo==========
      >     |                               |
      >     |  Go ahead, make my day . . .  |
      >     |   Show me where I'm wrong.    |
      >     =================================
      >     72770.552(at)compuserve.com
      >     http://www.aeroelectric.com
      
      
________________________________________________________________________________
Date: May 26, 1997
From: Michael McGee <jmpcrftr(at)teleport.com>
Subject: Re: Parachutes
>I'm confused. How do you jump out of a RV? My RV6-A can't release the >canopy because of the lift struts. And if it did release, it would probably >decapitate me anyway. What is the reason for paying good money for something >that is uncomfortable and cannot be used? I guess I missed a point >somewhere. If I'm not mistaken, any aircraft that you intend to do acro with is supposed to have an inflight escape route (like the door releases on the Cessna 150 Aerobat or the little red handle on the instrument panel of the RV-6 that releases the canopy) and the crew is supposed to be wearing parachutes that are rated for the speed of the aircraft. If you don't build this into your airplane (and no one says you have to) you probably won't get a cert for acro when it is given its final blessing. As far as the lift struts go, I'm surprised no one has devised a way for them to let go in the event of a canopy release. The canopy should come off up and away clean. Maybe ding the tail if it's still there. Remember you're getting out because the airplane is too broken to land. Mike McGee jmpcrftr(at)teleport.com ________________________________________________________________________________
From: "Brian Hitchings" <briandh(at)lantic.co.za>
Subject: Re: Artificial Horizons
Date: May 24, 1997
Hi there A few days ago I posted a question about surplus military 28 volt electric A.H's for approx $200 (excl posting and local taxes). Bob N. replied that I should check out whether it is not an AC (as opposed to DC) instrument: as usual he is right. They are AC. I'm investigating appropriate power supplies, and have received a couple of replies from the list in this regard. I have asked the supplier to give me a couple of photo's and details of the A.H's for me to post to this list. I'm due to see a military avionics engineer this coming weekend. Hang in there for a couple of days, and I will post all the info as soon as I have it to hand. Kind regards Brian Hitchings South Africa RV6A : Wings ________________________________________________________________________________
Date: May 26, 1997
From: Thomas Velvick <tvelvick(at)caljet.com>
Subject: Re: Wanted-Pneumatic Squeezer
Greg, I just finished the HS also and am in agreement with you. The pneumatic squeezer with the longeron yoke looks like the way to go. Of course the $650 would almost pay for a set of preassembled wing spars. Just wait until you try to set the 3/16 rivets. You'll need the Popeye forarms. Cheers Tom Velvick tvelvick(at)caljet.com riveting the HS&VS skins >I just finished the rear spar of my HS. Before my forearms look like >Popeye's, does anyone know of a used or decent lower priced air-powered >rivet squeezer and yokes? ($450+ is a bit steep right now.) > >Greg (Is this list great or what?) > >gregbrew(at)gte.net >RV-6A >Building up the skelton on the HS >(Say...this isn't so bad...) > ________________________________________________________________________________
From: dralle(at)matronics.com (Matt Dralle 510-606-1001)
Date: May 26, 1997
Subject: Canopy Woes...
Hi Bill, I have a question for you about the canopy latch. On the front nylon block, it isn't clear exactly how the nylon block is suppose to negotiate the piece of angle that is used to attach the instrument to the top longeron with a bolt. This angle is not shown in the canopy drawings anywhere. Notching the nylon to fit over the top of the angle seemed like a weird idea and I never gave it another thought. I proceeded to make the nylon piece just fit down on top of the top angle, and placed the screws at the top of the roll pin hole and to the right of it. Here's a lame drawing that should be viewed using a fixed width font like Courier: | (Front of inst panl looking toward engine) | | | | | |+---------------------+ || | || | | || -+- <-------+ | || | \ | || | \ | || __ -+- <-+------- Bolts to hold nylon to Inst Panl. || / \ | | || \__/ <------------------------- Roll Pin Hole || | |+---------------------+ |+--------------------------+ || | || +----+ | <------- Angle Alum. || +----+ | |+- - ||- - - - - - - - - - + |+----||-----------------+--+ || +----+ | || +----+ <--+ | <------- Cockpit rail || \ |___________________________Bottom of inst pnl___ | \ | \ | +--------- Bolt and Nut After I finished this installation, I got to thinking that *if* the nylon was suppose to fit over the top of the angle via a notch or some other arrangement, then the bottom screw holding the nylon in place would actually be going through the angle, thus renforncing the attachment of the nylon better. Do I worry too much? Thanks Bill! Matt -- Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94551 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: dralle(at)matronics.com (Matt Dralle 510-606-1001)
Date: May 27, 1997
Subject: Bouncing Email Handling... [Please Read Completely]
Hello everyone, There was about 2.3Mb worth of bounced email to the RV and Zenith email lists today. All of the messages that are sent to the Lists are sent from Matronics with a special header set to the following: "Errors-To: bounces(at)matronics.com". This header instructs most mailers to return mail with 'problems' to the listed email account. 'Problems' generally include things like the user doesn't exist anymore, their mail box is full, the machine isn't accepting email for some reason, or the machine just doesn't exist. To deal with all the mail that get's retured to the 'bounces' account at Matronics, some time ago I wrote a program that goes through the bounced email account looking for key strings like "joe.user(at)internet.com is an unknown user" and prints a report. I periodically run this program on the bounces email account and based on the report data, go through the rv-list and zenith-list address files and, well, clean house. The bounces account is automatically purged each day at midnight and I try to run the report program every week or so just before the current day's bounce email is cleared. The purpose of all this is to keep the Lists running smoothly and more importantly to keep the amount of bounced email to a minimum. The amount of mail to the bounce email account had been running in the 500k-1Mb range each day for about a year or so. The amount would go up and down based on how often I got around to running the report and cleaning up the Lists and to a lesser degree how much traffic there had been on the Lists. Tonight I noticed that there was 2.3MBs of bounced email in just one day! I ran the program and found that there were about 15 email addresses that had gone bad for one reason or another. To minimize the impact to the List members, I had generally limited the flagging of bad addresses to obvious problems like "no such user", but had *not* flagged things like "connection refused" and "host unknown" since many times these types of problems go away in a few days. With the high growth of the RV List in the last year or so, and the incredable amount of bounced mail each day, I have decided to increase the 'sensitivity', if you will, of the report generator. The reason I tell everyone these boring details is so that if your List mail stops arriving for some reason, and I havn't posted a message indicating that my ISP is causing problems again, that you will check your email account and the status of your subscription to the List. Both the RV-List and the Zenith-List FAQ detail how you can check to see if you are currently subscribed to the list. If you find that you have been removed from the List, assume that your email address was causing problems for some reason. Verify that your email is working okay again, and then go ahead and resubscribe. Please *do not* consider yourself "spanked" if you find that you have been removed. It is just a way of keeping the Lists running smoothly and its definately nothing personal. I try to get to the subscribe requests at least once a day, but only run the report program about every week or two. I want to stress that this is really no major change to the List operation, but more a reminder of what goes on behind the scenes and why your List mail might have stopped. Great discussions of late! Keep up the good work, one day it will fly - that's what I keep telling myself... Matt Dralle RV and Zenith List Admin. RV-4 Builder Matronics -- Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94551 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: GRAY Doug <GRAY.Doug@tms-pty.com>
Subject: Hawaii visit
Date: May 27, 1997
I will be visiting Hawaii on business and will have Friday the 30th and Saturday 1st free. 1.Can anyone tell me if there is a WalMart store likely to stock the Magellan GPS in Hawaii? If not are the Sears prices compedative? 2.Any recommendations for an organisation who might do local flying trips at reasonable prices. My colleague and I are pilots and looking for an opportunity to do some sightseeing by air. Please contact me off list. ( gray.doug@tms-pty.com) Doug Gray, Sydney, Australia, the RV6 kit is in transit. ________________________________________________________________________________
From: MAlexan533(at)aol.com
Date: May 27, 1997
Subject: Doug Stenger's phone number?
Doug Stenger in Oregon was recently mentioned as being available to build RV parts. I am looking for his phone number, as I would like him to do an RV-4 wing and fuselage for me. Thanks. MAlexan533 ________________________________________________________________________________
Date: May 27, 1997
From: "David J. Fitzgerald" <theredbaron(at)earthlink.net>
Subject: Re: Wanted-Pneumatic Squeezer
Greg, I was in favor of getting a bucking bar and going at it. It didnt take very long and it was MUCH easier than squeezing. I use the squeezer only when necessary (read that as mandatory - I dont really like the squeezer). A pneumatic squeezer would be great - but it is very costly. Is there a reason for not bucking these with a rivet gun?? -- ----------------------------------- David Fitzgerald RV-8 Serial #80333 theredbaron(at)earthlink.net ----------------------------------- ________________________________________________________________________________
From: RV4Brown(at)aol.com
Date: May 27, 1997
Subject: Re: Junk email: Free Aircraft Tool Catalog
AOL has a filter that allows mail to be forwarded from only the addresses that you list. In addition they have a spam address to dorward all junk mail to. If they determine it should be banned as a nusiance, they block it from everyones AOL address. AOL also has a check off block for requesting that junk mail that has been blocked will not be forwarded to you. All that being said, I still get 10 to 15 pieces of crap a week ________________________________________________________________________________
Subject: Re: Experimental Maintenence
39,41-42,44-47
From: wstucklen1(at)juno.com (Frederic W Stucklen)
Date: May 27, 1997
Listers: So WHERE in the regs does it say a repairmans certificate is needed? We all should know that this is indeed the PRACTICED and FAA SUPPORTED position, but where does is say so in the regs? Also, where does it say that an A&P or IA can sign off work done on an experimental? My understanding is that neither conditions exist in the FAR's, but only in an FAA letter of agreement (or something of the nature). Maybe someone should ask the FAA for an explaination. Fred Stucklen RV-6A N925RV wstucklen1(at)juno.com writes: > >As a student A&P I have just gone through this same question. The builder of >an Experimental aircraft may perform all maintenance and repairs on his/her >aircraft provided he/she holds a repairman license for that aircraft. When I >completed my Kitfox applying for the Experimental Aircraft Repairman >Certificate was part of the paperwork package sent out by the FAA. My FAA >inspector was very helpful in providing direction to get this necessary piece >of paper. An A&P can also perform work on your Experimental, but why --- You >built it so you can fix it, I hope. However, if you purchase an Experimental >used (as in already built) you may not perform anything other than the >preventive main. listed in Part 43. You must get an A&P, I.A. to perform the >Annual Condition Inspection and other repairs etc. One option available when >purchasing a second hand homebuilt would be for you to get the >builder to do this work for you (free by the way) . He can legally do this >for you as long as he does not surrender his Repairman Cert. for that >aircraft. Hope this helps . Kitfox N390SH, RV-4 no. 2280. > ________________________________________________________________________________
Date: May 27, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: Elevator skin thickness question...
m > >I recently visited an RV-4 owner who had a suggestion about the elevator skin >thickness. Apparently, the 0.016" skin is known to form cracks at the >trailing edge about 2/3 of the way out. His suggestion was to use 0.020" >skins for the elevator instead. > You will probably get a number of answers on this, but just in case I'll toss in too. I have talked to one fellow who did this to a RV-4 and had no problems after 400 + hrs. Most that I know of are putting RTV under the tips of the interior angles as they rivet the surfaces together. I have seen or heard of any cracking problems with this method. Have A Stupendous Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
Date: May 27, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: "N" Number
> > So, just call your Freindly Aviation Ass'n and request a number. >It's easier than you think. > > Carroll Bird, Buffalo Gap, TX That's better then the lottery...going to try it to day! I need a transponder, so I'll hold out for $1500. :^) Have A Stupendous Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
Subject: Oil
From: lm4(at)juno.com (Larry Mac Donald)
Date: May 27, 1997
A number of years ago I sold a secondary oil filtering device. The only thing this filter would leave behind was the dark color of the oil made by ashless detergents. When I would use non-detergent oils, the oil would always be dirt free and golden in color. During those years one of the " car manufacturers " claims were that " oil breaks down " . The filter manufacturer countered that " oil doesn't break down ". Now it appears that I am hearing some expertise on the list, so maybe I can finally get a good answer. Can someone out there tell me, Does oil break down? And if it does, What does that mean? Larry Mac Donald lm4(at)juno.com ________________________________________________________________________________
Date: May 27, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: "N" solved
I took used the suggestion that were so kindly posted and low and behold, the FAA person said there was no reason I didn't get my 1st reguest as all my number were available. No one knew there knew why I was assigned a number, but I will be getting it as soon as they redue the paper work..... Thanks to all! Have A Stupendous Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
From: teetime(at)konza.flinthills.com
Date: May 27, 1997
Subject: Yikes!
It's that time of year and the local wildlife are alive and well. Recently, I found a 1 1/2 foot snake skin in my shop but didn't think much of it. A couple of days later I found a 5 foot snake skin right by my radio! That got my attention. In Kansas here we get some pretty big Copperhead snakes. My recent situation is that the snakes are out of hibernation and the wasps and spiders are starting to build their nests. I have two wings done and the empennage. Guess where they want to build their nests? That's right! Inside the newly constructed pieces. It prompted me to tape up all of the openings so there are no unauthorized passengers in the future. My advice to any builders that are like me and live in areas with a lot of wildlife; be careful when you move pieces around that cover up attractive areas for them to live. I spend 10 to 20 hours a week in my shop so they are definately not afraid of me being there. Does this deter me in any way? NO WAY! I want my RV4! (I am retired Army, so this might account for my absense for common sense in these areas) Good Luck! Tim Sweemer RV4 started fuselage ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: May 27, 1997
Subject: Re: Doug Stenger's phone number?
<< Doug Stenger in Oregon was recently mentioned as being available to build RV parts. I am looking for his phone number, as I would like him to do an RV-4 wing and fuselage for me. Thanks. MAlexan533 >> Check the Yeller Pages at http://www.sound.net/~hartmann/yelrpage.htm -GV ________________________________________________________________________________
Date: May 27, 1997
From: johntate(at)essex1.com (John Tate)
Subject: Re: Wanted-Pneumatic Squeezer
David J. Fitzgerald wrote: > > > Greg, > > I was in favor of getting a bucking bar and going at it. It didnt take > very long and it was MUCH easier than squeezing. I use the squeezer > only when necessary (read that as mandatory - I dont really like the > squeezer). A pneumatic squeezer would be great - but it is very costly. > Is there a reason for not bucking these with a rivet gun?? > -- > ----------------------------------- > David Fitzgerald > RV-8 Serial #80333 > theredbaron(at)earthlink.net > ----------------------------------- Dave. I also did my spar with a rivet gun. A local 6 builder said that was the best way. ________________________________________________________________________________
Date: May 27, 1997
From: "Robert L. Nuckolls, III" <RNuckolls(at)compuserve.com>
Subject: Antenna Coax
/Two questions occur to me. = /I have heard that length of coax is critical = /to performance but when I mention this to techs they scoff = /and brush me off with the comment that this is old data /and no longer applies?! = > Actually, it NEVER applied . . . at least not for any = > good reason. . //Beg to differ.. it doesn't make a difference only if the = //source and termination are the same impedance as the cable, = //i.e., a flat line. If there are voltage standing waves = //(VSWR) on the line, then the length of the cable matters. But matters to what and why? There's no way that a 1/4 spike sticking out of the top of an airplane is going to present a 50-ohm, non-reactive load to a piece of coax over the full range of communications frequencies. In fact, it will never present such an idealized load at ANY frequency in that range. So . . . how would you proposed the coax length be "adjusted"? //If the line is not flat, the impedance or more correctly the = //reactance varies from point to point along the cable. Assuming = //the transmitter, coax, and the antenna and its installation = //all show an impedance of the same value, the length of the = //cable is not critical, it will only cause an attenuation with = //distance; however if the impedances are not matched all bets are = //off and the length of the line will make a VERY BIG difference. Everything you say is true from an idealized, textbook analysis of an antenna/feed-line system. However, in the real world of working with airplanes and their radios, the words "critical" and "difference" need definitions. When we advise people that something has significance, we should be prepared to follow up with a practical means for achieving the optimal result. In fact, as the power handling capabilities of RF amplifier transistors for trasmitters grew, their ability to tolerate some conditions of mis-match between antenna and coax was lagging behind. For a brief period in the development of these radios, there was a flurry of activity to tailor coax feedline lengths to minimize stresses on the comm transmitters that tended to blow their brains out under some antenna loading conditions. Thankfully, those days are long gone and I'm aware of no manufacturer= of a VHF comm transmitter that recommends feed line length optomizati= on for use of their product. To do so would announce to the world that = they've not done their homework in selection of parts or in the desig= n of their product. Regards, Bob . . . = AeroElectric Connection //// (o o) =3D=3D=3D=3D=3D=3D=3D=3D=3D=3DoOOo=3D(_)=3DoOOo=3D=3D=3D=3D=3D=3D=3D=3D= =3D=3D | | | Go ahead, make my day . . . | | Show me where I'm wrong. | =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 72770.552(at)compuserve.com http://www.aeroelectric.com= ________________________________________________________________________________
Date: May 27, 1997
From: "Robert L. Nuckolls, III" <RNuckolls(at)compuserve.com>
Subject: Fuses/Breakers in flight?
Kitfox List /I am using fuse blocks, so it can be turned off by = /pulling the correct fuse in the Vital power panel. Arrrgghhhh! you're going to fiddle with fuses in flight!!!!! . . . . I gotta go get a asprin! >True,not necessary but I don't think it will give you or = >anyone else a headache.With 3000 plus hours I have changed a = >few fuses and reset as many circuit breakers.Sometimes you = >just can't wait until you get the bird on the ground. Agreed . . . in most certified airplanes, the electrical system is so cumbersome and ill-designed that the pilot has no choice but to deal with inflight electrical systems issues. We're talking about amateur built airplanes now. We can eliminate all of the little deamons that have plagued the carved-in-stone-certified ships for about 40 years. I'll suggest that the optimally configured flight system will NEVER present a situation to a pilot requiring any sort of fiddling with breakers and fuses in flight. Our system confguration recommendations have evolved over ten years of one-on-one communications with hundreds of builders. Rather than seek out holy-grail of design philosophy with a goal of certification, we've constantly tweaked, evaluated, and analysed the failure modes to the extent that inflight fiddling is eliminated . . . as far as we know right now . . . if some new problem shows up; wonder of wonders, we'll FIX it! At Cessna, Beech, Piper and Mooney, a committee of 20 will debate the issue for weeks and trade off perceived value, governmental edicts and market forces before deciding to assign another committee to study the problem some more. I know it sounds ridiculous but belive me, that's the way it works in aviation's jurassic parks. I've attended several such meetings myself in the past two weeks. It's sure refreshing to come home and be able to slay the dragons as they hatch out instead of waiting for them to grow up before joining the battle. Regards, Bob . . . = AeroElectric Connection //// (o o) =3D=3D=3D=3D=3D=3D=3D=3D=3D=3DoOOo=3D(_)=3DoOOo=3D=3D=3D=3D=3D=3D=3D=3D= =3D=3D | | | Go ahead, make my day . . . | | Show me where I'm wrong. | =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 72770.552(at)compuserve.com http://www.aeroelectric.com= ________________________________________________________________________________
Date: May 27, 1997
From: Charlie Kuss <charliekuss(at)sprintmail.com>
Subject: Source of airtool part numbers and parts
I recently was given several air tools by Lynn Woofter of prop extention fame. I've managed to get them all working but they need some TLC. I've emailed Chicago Pneumatic requesting exploded views of the tools with part numbers so that I could order the needed parts from my local distributer. 5 days and no reply yet. Does anyone on the list know where I could get the above info for the following tools. Chicago Pneumatic Rivet squeezer Model 214 Serial # H274560 " " Right angle air drill Model unknown Cleco 1/4" air drill Model 11 DP 27 Serial # 23216 I would also appreciate any info on where I might buy these parts by mail. Charlie Kuss ________________________________________________________________________________
From: "Doug Rozendaal" <DougR(at)netins.net>
Subject: Re: Oil
Date: May 26, 1997
charset="iso-8859-1" ---- From: Larry Mac Donald <juno.com!lm4(at)matronics.com> Date: Tuesday, May 27, 1997 9:57 AM Subject: RV-List: Oil . Can someone out there >tell me, Does oil break down? Like everything else the answer is yes and no so, so the answer is yes, the "but" part is not in 25 or 50 hours that we use it in an airplane. > And if it does, What does that mean? > >Larry Mac Donald lm4(at)juno.com What we mean by breakdown is chemical change in the composition of the oil, most notably, oxidation. This occurs when an oxygen atom attaches to the oil molecule. In oil we want saturated molecules unlike in our food. Saturated means that a higher % of the available bonding sites are filled with hydrogen. Synthetics are VERY highly saturated and therefore, and for other reasons are more resisitant to oxidation. However oxidation is not the problem in aircraft oil because it is built in very heavy basestock (15w-50 excepted) and so it is thermally stable at the temps we see in healthy aircraft engines for far longer than 50 hours which is the normal drain interval. Shell uses PAO's (see previous post) for the light componet in 15w-50 so it too is very thermally stable. Our 50 hour drain interval is a function of combustion by-products in the crankcase, some are particulate (filtered out) and some are chemical (not currently additive stabilized). Until we use bettter additive chemistry ( it is available), there is little or no benefit to the increased thermal stability of synthetics (15w-50 excepted). imho looking for an rv-4 Tailwinds, Doug Rozendaal dougr(at)netins.net http://www.petroblend.com/dougr ________________________________________________________________________________
Date: May 27, 1997
From: Terry Mortimore <terry.mortimore(at)sympatico.ca>
Subject: Help from California RV'ers
Hi guys, this is a real shot in the dark but I thought I'd try. I have e-mailed with a fellow who purchased a military surplus "Fuel/Air Heat exchanger" made by Air Research that measures 10" x 7" x 6" deep. I'm thinking that this unit would make a good radiator for my project. Unfortunately he has been unable to supply the address or phone number for the surplus store (long story). All I know is that it is in California. Is there anybody in California that would know of a surplus store that would carry such a unit. If not, could I get a phone number of any surplus store that I could start a calling search with. Thanks for any help, terry Terry Mortimore 2.7L Subaru RV-6A 38 Cartier St. Sault Ste Marie terry.mortimore(at)sympatico.ca Ontario Canada P6B-3K2 ________________________________________________________________________________
Date: May 27, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Jon Johansen
Les, You can reach Jon at *sportair(at)attmail.com (Jon Johanson)* Bill >Would any person on the list be able to help me with Jon's Johanson's email >adress? Thanks in advance. > >lmrowles(at)netspace.net.au >Les Rowles >Po Box 1895 >Traralgon >Australia 3844 > > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
Date: May 27, 1997
From: Terry Mortimore <terry.mortimore(at)sympatico.ca>
Subject: Help from California RV'ers
Hi guys, this is a real shot in the dark but I thought I'd try. I have e-mailed with a fellow who purchased a military surplus "Fuel/Air Heat exchanger" made by Air Research that measures 10" x 7" x 6" deep. I'm thinking that this unit would make a good radiator for my project. Unfortunately he has been unable to supply the address or phone number for the surplus store (long story), all I know is that it is in California. Is there anybody in California that would know of a surplus store that would carry such a unit. If not, could I get a phone number of any surplus store that I could start a calling search with. Thanks for any help, terry Terry Mortimore 2.7L Subaru RV-6A 38 Cartier St. Sault Ste Marie terry.mortimore(at)sympatico.ca Ontario Canada P6B-3K2 ________________________________________________________________________________
Date: May 27, 1997
From: John Ammeter <ammeterj(at)seanet.com>
Subject: Re: Yikes! CHATTER
In some ways I hesitate to mention this but we don't got these problems on the Wet Side (as we Washingtonians fondly refer to the western side of the Cascade Mountains). Granted, I may see an occasional small spider making a web in my shop or have to chase a wasp. Snakes?? I haven't seen one in Seattle for at least 20 years. We do have them in the country but, even there, they are respectable snakes and don't invade the people domain. Now, I have a cousin living just west of San Antonio, TX. I visited her about two months ago and plan to drive down there in about two weeks. They have SNAKES and FIRE ANTS. I was baptized by a fire ant on my last trip there. I hope to avoid that this time. As far as snakes go, if I was to find ANY snake skin in my shop you can count on the fact that I would not be going in there until I was certain that no snake, alive or dead, was any in the vicinity. You note that you are retired Army; maybe that is a criteria for being able to live in these areas. My cousin is retiring from the Air Force on June 13, rank of bird Colonel. Not bad for a woman with only 22 years service; I tell her it is because she follows my advice, NOT!! John > > It's that time of year and the local wildlife are alive and well. >Recently, I found a 1 1/2 foot snake skin in my shop but didn't think much >of it. A couple of days later I found a 5 foot snake skin right by my >radio! That got my attention. In Kansas here we get some pretty big >Copperhead snakes. > My recent situation is that the snakes are out of hibernation and >the wasps and spiders are starting to build their nests. > I have two wings done and the empennage. Guess where they want to >build their nests? That's right! Inside the newly constructed pieces. > It prompted me to tape up all of the openings so there are no >unauthorized passengers in the future. > My advice to any builders that are like me and live in areas with a >lot of wildlife; be careful when you move pieces around that cover up >attractive areas for them to live. I spend 10 to 20 hours a week in my shop >so they are definately not afraid of me being there. > Does this deter me in any way? NO WAY! I want my RV4! (I am >retired Army, so this might account for my absense for common sense in these >areas) > >Good Luck! > >Tim Sweemer > >RV4 started fuselage > > > John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA 206-525-5445 RV-6 N16JA First flight August 1990 ________________________________________________________________________________
Date: May 27, 1997
From: Robert Acker <r.acker(at)ix.netcom.com>
Subject: Re: Parachutes
>...and the crew is supposed to be wearing >parachutes that are rated for the speed of the aircraft. The archives toss this around at length, but I thought I would check for myself this morning. Crew does not require a parachute: Sec. 91.307 Parachutes and parachuting. (c) Unless each occupant of the aircraft is wearing an approved parachute, no pilot of a civil aircraft carrying any person (other than a crewmember) may execute any intentional maneuver that exceeds-- (1) A bank of 60 degrees relative to the horizon; or (2) A nose-up or nose-down attitude of 30 degrees relative to the horizon. I could find no exit speed ratings in Parts 91 or 105. A jumper friend I asked is not aware of such a rating (there are max *deployment* speed & weight parameters for a particular chute). I believe at exit the horizontal velocity component diminishes almost instantaneously. Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
Date: May 27, 1997
From: Terrance Jantzi <tjantzi(at)netrover.com>
Subject: O2 flow rate
Listers, I now have an airplane that climbs at a tremendous rate. I want to fly really high. I have an aviators oxygen bottle that is set up for masks. I want to use disposable cannulas from a medical gas supply company. Does anyone have any info on required flow rates for such a setup. I suspect that the flow rate could be set lower with the cannulas, thus extending bottle time. These cannulas are really neat. AT .80CDN you can give your passengers a sealed and sterilized unit. They are about as comfortable as anything could be while its stuck up your nose. This way I get to use my headset mike and avoid the discomfort of a rubber mask. Terry Jantzi C-GZRV flying ________________________________________________________________________________
From: sheinlein(at)VNET.IBM.COM
Date: May 27, 1997
Subject:Tip on delaying the decision between 6 and 6A... For some reason, I seem to be having a much harder time than most in trying to decide whether to build the 6 or the 6A. I really want to build the 6, but I'm hesitating because I don't want to compromise "safety" for "looks". (Sorry, that is a very simplified view of my own personal problem here, PLEASE don't take this as flamebait!) :) I have NEVER flown a taildragger, but I like the looks of them and their rough-field handling abilities (forget that 2 knot speed difference!).. But, I don't want to make the decision without some taildragger time. So, I am joining a flying club that has a 1946 Aeronca Champ (can someone please comment on the handling differences between this and an RV-6? AS THEY RELATE TO LEARNING TO T/O or LAND?!). I hope to use what I learn from flying the Champ to help me decide which RV to build. (Again, please don't think I'm implying that the Champ and RV handle the same! I just want to know if I feel comfortable handling the Champ, would I feel at least as comfortable handling the RV-6?) Anyway, after talking to Bill at Van's, it appears that I can delay my 6 vs 6A decision a little bit longer, as follows. Any tips you can offer me would be much appreciated, as I'd like to order the fuselage by the end of this week! The construction differences between the 6 & 6A appear to be: 1. the 6 has an extra steel fixture in the back for the tailwheel 2. the 6 has an extra bulkhead near the tail 3. the 6A has larger gussets for mounting the main gear 4. the 6A has a different engine mount (for the nosewheel) After talking with Bill, I think the thing to do is to build a "combo" plane until we hit #4, which is part of the finishing kit and at least a 1/2 a year away. I can do #1, #2, and #3 above... and in effect delay the decision until I hit item #4, which is at the very end of this year. The only drawback would be an extra 1 1/2 pounds in the tail where the extra weldment for the tailwheel is located. Not a big deal, since I will be installing a metal prop (not wood) anyway, which will help balance out the extra weight in the tail. Any comments/suggestions on my "plan" would be much appreciated. Except for something like "You should'a built a -4 and then you wouldn't have to make that decision!" :) Thanks in advance... Stephen Heinlein sheinlein(at)vnet.ibm.com (Almost done with second wing...) ________________________________________________________________________________
Date: May 27, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: Elevator skin thickness question...
SORRY didn't proof the message. >I have talked to one fellow who did this (.020 controls) to a RV-4 and had no problems after 400 + hrs. Most that I know of are putting RTV under the tips of the >interior angles as they rivet the surfaces together. I have NOT seen or heard >of any cracking problems with this method. > Have A Stupendous Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: May 27, 1997
Subject: Re: Experimental Maintenence
Fred, No where in the Regs does it say a repairmans certificate is needed. Your repairmans certificate is only good for signing off your condition inspection. If you do not have a repairmans certificate for that aircraft you must find an IA or A&P to do your annual condition inspection sign off. Can you work on your own airplane? Yes you just cant sign off the condition inspection unless your holding one of the above certificates. AC 20-27D par 9 The builder of this aircraft, if certificated as a repairman, FAA certified mechanic holding an Airframe and Powerplant rating and or appropriately rated repair stations may perform condition inspections in accordance with FAR Part 43 appendix D. Repairman certificate privleges and limitations are found in FAR 65.104 its all there Fred . Ryan ________________________________________________________________________________
From: NSGE82A(at)prodigy.com (MR NORMAN W RAINEY)
Date: May 27, 1997
Subject: Doug Stenger's phone number?
Doug Stenger's number in Banks, OR. is (503)324-6993. ________________________________________________________________________________
From: rust47rg(at)one.net
Date: May 27, 1997
Subject: Re: Elevator skin thickness question...
> >m >> >>I recently visited an RV-4 owner who had a suggestion about the elevator skin >>thickness. Apparently, the 0.016" skin is known to form cracks at the >>trailing edge about 2/3 of the way out. His suggestion was to use 0.020" >>skins for the elevator instead. >> >You will probably get a number of answers on this, but just in case I'll >toss in too. > >I have talked to one fellow who did this to a RV-4 and had no problems after >400 + hrs. Most that I know of are putting RTV under the tips of the >interior angles as they rivet the surfaces together. I have seen or heard >of any cracking problems with this method. > I have experienced cracks in both the rudder and elevators. Mine appeared at the first rivet at the front of the stiffeners at around 200 hours TT. I had used RTV at the trailing edge and had none there. From what I've been able to find it appears the cracking problem is more common in the high horsepower constant speed RV's. The prop pulse seems to beat the tails up quicker and usually they show up on the rudder first. I have a 180 C/S. I rebuilt my rudder with .020" skin but I don't have enough time on it to tell anything yet. If I were to build another RV it would have .020 control surfaces on the tail. Regards: Rusty Gossard N47RG RV-4 Flying since 8-94 ________________________________________________________________________________
Date: May 27, 1997
From: Tim Bronson <70773.2700(at)CompuServe.COM>
Subject: "N" solved
Denny Harjehausen wrote: "...the FAA person said there was no reason I didn't get my 1st request... I will be getting it as soon as they redo the paper work....." Denny: Could you tell us all what number you called and who you spoke to? Thanks. Tim Bronson - Pittsburgh, PA ________________________________________________________________________________
Subject: Re: Bulkhead/Horizontal Stab angle pieces
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: May 27, 1997
>There are two angle pieces that are attached to the rear bulkheads >where >they will eventually be bolted to the horizontal stab. Question, are >the angles put in place while the skeleton is being done or after the >lower skins are on and the fuselage is upright? > Don, I don't have my manual handy, so I am responding from memory. I assume you are talking about the forward HS attach point. I recommend waiting until you get the fuselage upright to drill these angles. That way you can better see how all the parts are supposed to fit together. However, while you are jigging the skeleton, make SURE you measure the distance between the forward face of the HS rear spar and the forward (I think) face of the HS forward spar on YOUR horizontal stab. Then jig the appropriate fuselage bulkheads to match YOUR horizontal stab, regardless of the plans dimensions. I found that mine differed from the plans dimensions by about 1/8". Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 on the gear ________________________________________________________________________________
Subject: Re: Wanted-Pneumatic Squeezer
<338AB631.41C6(at)earthlink.net>
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: May 27, 1997
David, For what it's worth, I find that I set 1/8" rivets much more cleanly with a gun and bucking bar than by any other method. For 3/32" rivets I prefer a hand squeezer. For the 3/16" rivets on the wing spar I obtained excellent results with a press arbor from Harbor Freight and a 3-lb short-handled sledge hammer (considerably cheaper than a pneumatic squeezer!) Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 on the gear writes: > > >Greg, > >I was in favor of getting a bucking bar and going at it. It didnt >take >very long and it was MUCH easier than squeezing. I use the squeezer >only when necessary (read that as mandatory - I dont really like the >squeezer). A pneumatic squeezer would be great - but it is very >costly. >Is there a reason for not bucking these with a rivet gun?? >-- > ----------------------------------- > David Fitzgerald > RV-8 Serial #80333 > theredbaron(at)earthlink.net > ----------------------------------- > ________________________________________________________________________________
Date: May 27, 1997
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Doug Stenger's phone number?
>From the rv yeller pages <http://www.sound.net/~hartmann/yelrpage.htm>: DOUG STENGER 503-324-6993 RV SUBASSY BUILDER Suggestion: download this very useful list, print it out, tack it to your wall, keep it in your computer so you can do searches on it... a great resource! Randall Henderson, RV-6 randall(at)edt.com http://www.edt.com/homewing ________________________________________________________________________________
From: Tony Atkinson <aja(at)twizel.ecnz.co.nz>
Date: May 28, 1997
unsubscribe ________________________________________________________________________________
Date: May 27, 1997
From: Bill Frazell <Bill.Frazell(at)OAG.STATE.TX.US>
Subject: V-stab tolerances -Reply
Oh how nice it is to see my name being dragged through the mud and not being able to defend myself. Kevin, I bought the tail kit from a fellow here who builds harmon rockets (who's name I won't mention for fear of you dragging his name through the mud also) with the Items that need gigging already riveted, but still needing detail work(i.e. vertical stablizer). I worked on the elevators and rudder. I finished the Tail Kit and had just ordered the wing kit as you will recall. SO PLEASE GET YOUR FACTS STRAIGHT BEFORE YOU TRASH THE WRONG SOMEONE. THANKS! By the way, the RV-6 project you saw when you came down to Texas has now flown, first flight on March 2, 1997 - N1150S. >>> kevin lane 05/25/97 07:30pm >>> After a momentous day of moving two RV's to TTD hanger Brian had to comment on how my V stab looked crooked. "Optical illusion", I said as I proudly proved with a tape measure that the diagonals were exact. Exact at the rear top, exact at the bottom front, BUT, what about the top leading edge? 5/8" warp towards the passenger. I bought the kit from Bill Frazell who built the VS. The skins look real nice. Apparently his jig wasn't. So, my question is, how much is bad? I will fly it as to start out, is but wondered what others thought about solutions: build a new one?, drill out rivets and enlarge holes and twist it into place?, always roll left?, sue Frazell? (he's an attorney, so that's real unlikely). What kind of tolerances are flying now? It was quite "enlightening" to see my plane in the sunlight after two years of fluorescents. I am in greater awe of that flawless RV4 at Vans fly-in that was simply polished. Those reflections have one hell of a memory, "oh yea, this is where the bucking bar slipped a bit, this is where the bulkhead didn't fit by 1/32", this is where the wife tried bucking, this is where Dad bucked the wrong rivet, .........." kevin "the painters will fix it" 6A, wings on tomorrow! ________________________________________________________________________________
Date: May 27, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: Vapor Lock
There was a recent thread on the list about Jet Hot Coatings for exhaust systems. I know of a number of local hot rodders who have used this to reduce underhood temps on their cars. Presumably this would help reduce undercowl temps on an aircraft as well. The various exhaust wraps/header tapes on the market do reduce temps but tend to promote corrosion on mild steel exhaust systems. I have heard of brand new headers corroding away to nothing in less than 6 months using these wraps. Dont know what they would do to stainless. Mike Wills RV-4 (wings) willsm(at)manta.nosc.mil >>I had considered taping the exhaust with asbestos (as they also do in >>race cars) but decided against it on advice from others. > > Good idea: don't do it. I seems like it may overheat the exhaust pipes > ________________________________________________________________________________
Date: May 27, 1997
From: "Gregory S. Brewsaugh" <gregbrew(at)gte.net>
Subject: Re: Wanted-Pneumatic Squeezer
RodWoodard wrote: > > > Hello Popeye: > > I bought my used pneumatic squeezer...etc > Thanks Rod, I'll give them a call. Greg ________________________________________________________________________________
Date: May 27, 1997
From: Dr John Cocker <jcocker(at)medhumor.com>
Subject: Re: Aircraft oils
You make a good case for all the extra goodies put in modern oils. My question remains --- so why don't our engines last longer ? John ________________________________________________________________________________
Date: May 27, 1997
From: Paul Rosales <prosales(at)qnet.com>
Subject: [Fwd: WANTED RV6a project]
This is a multi-part message in MIME format. --------------12C22839510 >From Paul.Cress(at)worldnet.att.net --------------12C22839510 From: Paul.Cress(at)worldnet.att.net (Paul Cress) Subject: WANTED RV6a project Date: Mon, 26 May 1997 20:38:16 GMT NNTP-Posting-Host: 207.147.203.125 I an interested in purchasing a half built or more RV6a please contact me if you have, or know of someone, who is selling one I would prefer dealing with someone located in the south west --------------12C22839510-- ________________________________________________________________________________
Date: May 27, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Parachutes, Canopy jettison
No one has mentioned that the strut system for the -6's was developed like the hinge system on the RV-4. The pop-rivets are designed to shear off if the canopy is jettisoned, much like a couple of RV-4 pilots have discovered when their canopy swung open in flight. I do not believe any RV-6 canopies have been jettisoned to date. Van's is not looking for volunteers. We are also not looking for people to modify the attachments of their lift struts. If installed per the instructions, the struts will detach if the canopy is released. Bill > >>I'm confused. How do you jump out of a RV? My RV6-A can't release the >>canopy because of the lift struts. And if it did release, it would probably >>decapitate me anyway. What is the reason for paying good money for something >>that is uncomfortable and cannot be used? I guess I missed a point >>somewhere. > >If I'm not mistaken, any aircraft that you intend to do acro with is >supposed to have an inflight escape route (like the door releases on the >Cessna 150 Aerobat or the little red handle on the instrument panel of the >RV-6 that releases the canopy) and the crew is supposed to be wearing >parachutes that are rated for the speed of the aircraft. If you don't >build this into your airplane (and no one says you have to) you probably >won't get a cert for acro when it is given its final blessing. As far as >the lift struts go, I'm surprised no one has devised a way for them to let >go in the event of a canopy release. The canopy should come off up and away >clean. Maybe ding the tail if it's still there. Remember you're getting >out because the airplane is too broken to land. >Mike McGee >jmpcrftr(at)teleport.com > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
From: "mcomeaux" <mcomeaux(at)cmc.net>
Subject: Under construction
Date: May 27, 1997
Is there currently any RV6 or 8's under construction in the Bend, Oregon area? If so could someone get in touch with me at (541)593-2364 evenings or (541)593-2554 Day time. Thanks-----Mike Comeaux RV6A Emmpenage ________________________________________________________________________________
Date: May 27, 1997
From: "James K. Hurd" <hurd(at)riolink.com>
Subject: Yikes
Easy solution to all critter problems except dirt-daubers: get a hangar cat(s). Additional benefit: no birds in hangar. Put dry food and water on a work bench and make sure they have access to rafters to discourage the birds. Keep food dish full so they won't go out at night where the coyotes can get 'em. You might get a few dusty footprints on your plane but you won't find a scorpion under your air drill! Jim New Mexico RV6A wings in the jig/cats on the job ________________________________________________________________________________
Date: May 27, 1997
From: Al Mojzisik <prober(at)iwaynet.net>
Subject: Source of airtool part numbers and parts
>Does anyone on the list know where I could get the above info for the >following tools. >Chicago Pneumatic Rivet squeezer Model 214 Serial # H274560 > " " Right angle air drill Model unknown >Cleco 1/4" air drill Model 11 DP 27 Serial # 23216 >I would also appreciate any info on where I might buy these parts by >mail. >Charlie Kuss Charlie, Here's what I do...... Find the city for the manufacturer usually stamped on the tool and look up the area code and call information (XXX) 555-1212 and get the phone number for the company. Sometimes if you have access to a Thomas Register you can look it up yourself. Call the Mfgr. and tell them you need a local supplier. Then have the local supplier either FAX you the exploded views or have the Mfgr. send you hard capies. I have yet to be refused. Oh yea, one time they told me that I couldn't get the repair manuals for my copier so I told them that I was going to send them a request for the manuals via certified letter and then go to work on the machine after they refused me the manuals in writing. I told them should I get hurt working on it I might see them in court. They allowed me to purchase the manuals after I sent them a signed release that they faxed me. I just don't believe that people should keep information from someone who wants to do the work themselves if it is available to others. I paid for the information just like a service center would. Anyway........................ ARO-----Bryan, Oh Dotco-------Hicksville, Oh Chicago Pneu.----------Utica, N.Y. US Industrial Tool---------Plymouth, Mi. Sioux--------Sioux City, Iowa. Rockwell---------Pittsburg, Pa. Aircraft Tools Inc. L.A. Cal. APT -------- Gardena, Cal. Jiffy--------- Don't know United Air Tool ------ Don't know Cleco---- Don't know Try: Nu-Matic Tool Repair & Parts Co. U.S. Industrial Tool & Supply Co. 15101 Cleat St. Plymouth, Mi. 48170-6098 (313) 455-3388 The only thing easier to rebuild than compressors are air tools. E-Mail me off list if you have any more questions. Al Col. Oh. prober(at)iwaynet.net ________________________________________________________________________________
Date: May 27, 1997
From: Gil Alexander <gila(at)flash.net>
Subject: Re: O2 flow rate
The western states glider guiders know all about this stuff ...:^) To be legal in the US, the disposable cannulas require the same flow rates as a mask, and are only certified to 18,000 ft (probably OK for RV use ..:^) The only way to go is to use a "nasal re-breather cannula" -- this will use about 1/5 the expen$ive O2 that a mask will use. It sort of looks like a hot dog on top of your upper lip ..:^) As a rough comparison, the 18,000 ft. oxygen flow rate for the re-breather cannula is about the same as the 11,000 ft. rate for a mask/straight cannula. To set the right flow rate, Nelson makes a dual scale flow meter/flow adjuster that goes with their regulator. The regulator fits on the tank, and drops the pressure down to about 40 psi, and the flow adjuster is a simple needle valve in the base of the flow meter (which is of the "floating ball in a tube" type). All you do is adjust the flow to set the ball alongside the altitude mark on the flow meter scale. On the low pressure side of the regulator, flexible 3/16 Tygon tubing is all that is needed. No rebuild interval needed on the regulator (unlike the ex-military stuff). If you use this system, you could mix and match Oxysaver cannulas and regular cannulas with the dual scale flow meters. Buy a Oxysaver for you and the SO, and give occasional passengers the disposable cannulas. The oxygen you save (costing at least $20 for a 22 cu. ft. tank) will soon pay for the more expensive Oxysaver cannulas. Parts: Nelson A-4 flow meter about $47 need one per occupant Nelson 300-1 regulator about $159 need only one Oxymiser cannula about $25 need one per occupant Regular cannulas 2 for $7 One source for all of the above is Wings and Wheels, a glider supplier in NY state. The owner is Tim Mara 716-664-6895 ... hope this helps ... ... Gil (used this system for years in my sailplane) Alexander RV6A, #20701 ... on hold > >Listers, > >I now have an airplane that climbs at a tremendous rate. I want to fly >really high. I have an aviators oxygen bottle that is set up for masks. >I want to use disposable cannulas from a medical gas supply company. > >Does anyone have any info on required flow rates for such a setup. I >suspect that the flow rate could be set lower with the cannulas, thus >extending bottle time. > >These cannulas are really neat. AT .80CDN you can give your passengers a >sealed and sterilized unit. They are about as comfortable as anything >could be while its stuck up your nose. This way I get to use my headset >mike and avoid the discomfort of a rubber mask. > >Terry Jantzi >C-GZRV flying > > ------------------------------------ RV6A, #20701 "REPLY" sends to entire RV-list mailto:gila(at)flash.net to reply privately ________________________________________________________________________________
Date: May 28, 1997
From: Gil Alexander <gila(at)flash.net>
Subject: Re: Parachutes
> >>...and the crew is supposed to be wearing >>parachutes that are rated for the speed of the aircraft. > >The archives toss this around at length, but I thought I would check for >myself this morning. > >Crew does not require a parachute: > > Sec. 91.307 Parachutes and parachuting. > (c) Unless each occupant of the aircraft is wearing an approved parachute, > no pilot of a civil aircraft carrying any person (other than a crewmember) > may execute any intentional maneuver that exceeds-- > (1) A bank of 60 degrees relative to the horizon; or > (2) A nose-up or nose-down attitude of 30 degrees relative to the horizon. > >I could find no exit speed ratings in Parts 91 or 105. A jumper friend I >asked is not aware of such a rating (there are max *deployment* speed & >weight parameters for a particular chute). I believe at exit the horizontal >velocity component diminishes almost instantaneously. > >Rob Acker / r.acker(at)ix.netcom.com / RV-6Q Rob, ... try looking in the TSO C23b documents that define the categories that the parachutes are certified to (that what makes it "approved" to meet the above FAR). .... Gil (it's always in the documents :^) Alexander > > ------------------------------------ RV6A, #20701 "REPLY" sends to entire RV-list mailto:gila(at)flash.net to reply privately ________________________________________________________________________________
From: bennett(at)healey.com.au
Date: May 28, 1997
Subject: Re: Yikes
> > Easy solution to all critter problems except dirt-daubers: get a hangar > cat(s). Negative, Jim. My cats mark their territory on the car's mag wheels and that stuff's potent. It would reduce my fuselage to a little pile pile of white powder between weekend sessions. Besides, cats would be useless at flushing out the 500000 ants that I found nesting in the fluoro light fittings last weekend. I used a surface spray and ants rained down for about two hours. I vacuumed them out of the fus, but I'd be interested if anyone knows the effect of formic acid on aluminium. Peter Bennett Sydney Australia RV6 building sliding canopy ________________________________________________________________________________
Date: May 28, 1997
From: Fran Malczynski <"Fran Malczynski"@IBM.net>
Subject: Re: RV6 vs 6A decision
Steve you wrote: "I seem to be having a much harder time than most in trying to decide whether to build the 6 or the 6A." I know what your going through because I'm still going through it. I was firmly convinced that I wanted to buld a 6. The reason is that that they look so damn sexy sitting on the ground. Pretty shallow, huh? I then followed your plan. I hooked up with a tail wheel instructor type and me, him and his Champ went flying so I could get the tailwheel sign off in in my log. We are still doing this, however a lack of an operating carburator has kept the plane on the ground for the past several months. I also asked for a tail dragger video for Christmas and my daughter and son-in-law came through and got me two of them....I thought it was a good plan and still do....except I made the mistake of going to SNF and dragging my wife over to Van's tent so we could look at more RV's. And there I saw N2NR, an RV6A painted in Navy colors that I absolutely fell in love with. Being ex Navy, the blue, grays and yellows along with the military bearing of the aircraft really appealed to me. So here I sit sending notes and signing them with RV6(A), with the "A" in parens because I still don't know what I'm going to do. But, it's fun trying to decide.....Good luck. Fran Malczynski RV6(A) - Working on wings ________________________________________________________________________________
Date: May 28, 1997
From: Boris <smbr(at)digital.net>
Subject: Re: Yikes
Another solution: Mix a can of fresh cayene pepper with a minimum of light food oil in a blender. Let it sit a day or two. Paint it on cross beams over the plane, etc. This was recomended to me by a farm supply freind (for poulrty barns) and it really works. It deters birds and also mice size/type critters. Great for those of us who are typically somewhat environmentally challenged. Good luck. ________________________________________________________________________________
Subject: Re: Experimental Maintenence
From: wstucklen1(at)juno.com (Frederic W Stucklen)
Date: May 28, 1997
writes: > >Fred, > No where in the Regs does it say a repairmans certificate is needed. Your >repairmans certificate is only good for signing off your condition >inspection. I agree.... >If you do not have a repairmans certificate for that aircraft you >must find an IA or A&P to do your annual condition inspection sign off. It's my understanding that there are no FAR's the specifically state this, but that the FAA does ALLOW it. Does anybody have any suportive info in this area? > Can you work on your own airplane? Yes you just cant sign off the condition >inspection unless your holding one of the above certificates. AC 20-27D par 9 When you state "airplane", I assume you mean experimental class. Does this mean that an owner of an experimental class aircraft, that does not hold a repairmans certificate, can remove the wingtips or landing gear, the tail surfaces, etc, and will not require an IA or A&P to sign off the work? This is certainly not the case with a certified aircraft. > The builder of this aircraft, if certificated as a repairman, FAA certified >mechanic holding an Airframe and Powerplant rating and or appropriately rated >repair stations may perform condition inspections in accordance with FAR Part >43 appendix D. I agree... >Repairman certificate privleges and limitations are found in FAR >65.104 its all there Fred . I agree.... Fred Stucklen RV-6A N925RV wstucklen1(at)juno.com ________________________________________________________________________________
From: "Dave and/or Diane Irwin" <dirwin(at)ibm.net>
Subject: Re: Tip on delaying the decision between 6 and 6A...
Date: May 28, 1997
Steve - I went through the same process about two years ago between the -6 and the -6A. I have about 700 hours on Grumman Yankees which are much like an under-powered RV-6A but I had no taildragger time and liked the looks of the RV-6 better than the -6A. In order to help me decide I took a couple of hours of dual in a Luscombe. They are considered to be a difficult taildragger as they seem to need to be landed in a three-point attitude at minimum airspeed and they will wander off the runway quite easily on rollout if you are not quick on the rudder pedals. The Luscombe, like the RV-6, has side-by-side seating, a control stick and a centre throttle. These advantages would seem to make it a good conversion aircraft. I would suggest that you get a checkout on a Champ first (which I did after the Luscombe...) and then move to a Luscombe. I reckon that if you can fly/land the Luscombe then the RV-6/6A decision will be easier for you!. BTW - I could land the Luscombe OK after the dual but we decided to build the -6A... Dave Irwin RV-6A #22607/C-GCRV (prov) dirwin(at)ibm.net . ---------- > From: VNET.IBM.COM!sheinlein(at)matronics.com > To: rv-list(at)matronics.com > Subject: > Date: May 27, 1997 1:54 PM > > > Subject:Tip on delaying the decision between 6 and 6A... > > For some reason, I seem to be having a much harder time than most in > trying to decide whether to build the 6 or the 6A. I really want to > build the 6, but I'm hesitating because I don't want to compromise > "safety" for "looks". (Sorry, that is a very simplified view of my > own personal problem here, PLEASE don't take this as flamebait!) > :) > > Stephen Heinlein > sheinlein(at)vnet.ibm.com (Almost done with second wing...) > > ________________________________________________________________________________
From: "Jeffrey Davis" <jdavis1(at)ford.com>
Date: May 28, 1997
Subject: Tip on delaying the decision between 6 and 6A...
--- Forwarded mail from rv-list(at)matronics.com From: sheinlein(at)VNET.IBM.COM Date: Tue, 27 May 97 13:54:07 EDT I have spent time in many different conventional gear aircraft ranging from Champs to Beech 18s. The Champ is a great plane to learn the fundamentals. The Champs I have flown are very easy to land. In a couple hours you should start to feel comfortable. Don't forget to start on the grass and move to the pavement as your confidence and experience builds. Grass is the place to learn.. After you master the Champ I would recommend getting some time in something like a Luscombe 8 or a Stinson 108. Both of these airplanes will provide you with a new challenge. The Luscombe is a little quicker on final and has narrow, tall gear (and a bad reputation). The Stinson also is a bit more difficult to land smoothly and adds the complexity of flaps. I am building a 6 and have a few hours in the conventional gear version. They are very easy to handle on the ground. If you can handle a Champ/Super Cub or Luscombe, you will do fine in the RV. My wife is a pilot (C152) and wanted a trike but after a few hours in a Super Cub and now in a Luscombe, she can't understand why she was so scared of conventional gear. Good luck with your conventional gear training - Utilization should be one of the main drivers behind selection of the gear configuration. If you think you will fly the trike more, build it. If cross wind landings and "Fly until it is tied down" are more your style, go for the conventional gear. >I have NEVER flown a taildragger, but I like the looks of them and their >rough-field handling abilities (forget that 2 knot speed difference!).. >But, I don't want to make the decision without some taildragger time. >So, I am joining a flying club that has a 1946 Aeronca Champ (can someone >please comment on the handling differences between this and an RV-6? >AS THEY RELATE TO LEARNING TO T/O or LAND?!). I hope to use >what I learn from flying the Champ to help me decide which RV to build. >(Again, please don't think I'm implying that the Champ and RV handle >.the same! I just want to know if I feel comfortable handling the Champ, >would I feel at least as comfortable handling the RV-6?) >Stephen Heinlein >sheinlein(at)vnet.ibm.com (Almost done with second wing...) ---End of forwarded mail from rv-list(at)matronics.com -- Jeffrey S. Davis Senior Research Engineer Advance Vehicle Technology Ford Motor Company Phone (313)845-5224 Fax (313)845-4781 ________________________________________________________________________________
Date: May 28, 1997
From: Scott Gesele <scottg(at)icsnet.com>
Subject: Re:
Stephen, One thing to consider is that the "traditional" way to build an RV-6A is to align the main gear and drill the main gear mounts while the fuse is inverted in the jig. IMHO, you should make up your mind prior to ordering the fuse and not build a "combo" fuse that will have you hauling around needless structure (weight) for the life of the aircraft. My $.02 Scott Gesele M506RV (finally painting) ________________________________________________________________________________
From: cecilth(at)juno.com
Subject: Re: Parachutes
Date: May 28, 1997
Of the several reasons I decided on a slider, I forgot this one. Thanks writes: > >I'm confused. How do you jump out of a RV? My RV6-A can't release >the >canopy because of the lift struts. And if it did release, it would >probably >decapitate me anyway. What is the reason for paying good money for >something >that is uncomfortable and cannot be used? I guess I missed a point >somewhere. >I don't want to start anything controversial but as I said before "I'm >confused". >Gene cafgef(at)aol.com >Starting to make canopy dust today. Fear & Trepidation > > > ________________________________________________________________________________
Date: May 28, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: "N" solved
> > > > Denny Harjehausen wrote: > >"...the FAA person said there was no reason I didn't get my 1st request... >I will be getting it as soon as they redo the paper work....." > > >Denny: > >Could you tell us all what number you called and who you spoke to? Thanks. > >Tim Bronson - Pittsburgh, PA > > Hi, I believe the lady that answered the phone was said her name was Norma.... If you are already in the computor have your serial number handy. She called over to the department that assigned my number and spoke to "Paula". The first lady just relayed the message from that department. She was very helpful. I had re-checked my numbers with www.landings.com as someone suggested and verified with "Norma" (?). The Number at FAA OK is 405-954-3116. Have A Great Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
Date: May 28, 1997
From: Robert Acker <r.acker(at)ix.netcom.com>
Subject: Re: Yikes
>Easy solution to all critter problems except dirt-daubers: get a hangar >cat(s). Additional benefit: no birds in hangar. Cat urine makes big ugly white spots on aluminum (speaking from experience) . Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
Date: May 28, 1997
From: Bill Frazell <Bill.Frazell(at)OAG.STATE.TX.US>
Subject: Kevin Lane V-stab.
Kevin - you need to look up the definition of Libel before you post any further E-Mails. Also, you need to remind yourself that I simply finished the Tail Kit, but did not do anything requiring a jig. I bought the Tail Kit from a local fellow here named Weldon Tadlock as being 60% complete. I bought it as is where is with no warranty, just like you did. If the situtation warrants, couldn't you reskin the part? Would you blame me for stuff wrong with the Wing Kit even though it was in the box when you bought it? Weldon used the rocket builder's jigs after hours, and perhaps Weldon did not set them up correctly. Neither the rocket builder, who's work is impeccable and much admired, nor myself built the piece you complain of. I hate the take up the list's bandwith with items such as this, but under the circumstances I felt this response both necessary and appropriate. ________________________________________________________________________________
Date: May 28, 1997
From: Robert Acker <r.acker(at)ix.netcom.com>
Subject: Re: Help from California RV'ers
>Is there anybody in California that would know of a surplus store that >would carry such a unit. If not, could I get a phone number of any >surplus store that I could start a calling search with. Terry, Try National Aircraft Parts at 562-426-8309 for a possible lead. Also try BJ Nash (rv-list archives), he resells surplus stuff. Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
Subject: Re:
From: ebundy(at)juno.com (Ed Bundy)
Date: May 28, 1997
>For some reason, I seem to be having a much harder time than most in >trying to decide whether to build the 6 or the 6A. I really want to >build the 6, but I'm hesitating because I don't want to compromise >"safety" for "looks". Another factor is insurance. As a low time TD pilot, Avemco quoted me $200-$250/yr more for insurance over the nose-dragger. > Not a big deal, since I will be >installing a metal prop (not wood) anyway, which will help balance out >the extra weight in the tail. 1.5 pounds that far aft MIGHT be a concern, even with a metal prop. Probably not so much with a CS. At the very least, it will clip some of your baggage capacity due to CG concerns. I would *definitely* make the decision before putting that much unnecessary weight in the extreme aft location of the tailcone. Ed Bundy RV6A - first flight 11/20/96 ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
From: "Doug Rozendaal" <DougR(at)netins.net>
Subject: Re: Aircraft oils
Date: May 27, 1997
charset="us-ascii" ---- From: Dr John Cocker <medhumor.com!jcocker(at)matronics.com> Date: Wednesday, May 28, 1997 2:53 AM Subject: Re: RV-List: Aircraft oils You make a good case for all the extra goodies put in modern oils. My question remains --- so why don't our engines last longer ? John The answer is that our automotive engines do last longer, much longer more than twice as long as they did 20 years ago and the "goodies" that you describe have played a large role in that. Our airplane engines don't last any longer because the oil is exactly the same (excepting Multi-vis) as it was in WWII for mineral oil and in 1962 for ashless dispersant. But just like magnetos, carbs and everything else in our airplanes except electronics, we seem to be unwilling to accept change. The price we pay for that is 2000 hour TBO. ________________________________________________________________________________
Date: May 28, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: RV6 vs 6A decision
> >Steve you wrote: > "I seem to be having a much harder time than most in > trying to decide whether to build the 6 or the 6A." > I struggled with this one too even though I have a lot tail dragger time. I felt that when it comes time to sell the -A would have a bigger market, it would be a safer trip down the runway and it doesn't really........ So I ordered the -A. Sometime later I purchased a used engine only to discover just in time that it would not fit a -A because of the nose gear would conflict with the carb. So after some phone calls Van's people agreed to exchange with me (it didn't make anyone in the office very happy because they didn't have neat package to do this)...it cost me some bucks...but I'm much happier now that necessity won the battle for the type I really wanted in the first place. I don't have to feel guilty now about not being practical. If your worried about landing it, don't be. When I learned to fly there wasn't any thing else. Everyone was a taildragger so we didn't have all the scare stories you hear now. these stories do nothing but make the beginner nervous (and thereby more apt to screw up) and make the guy who is tail dragger feel he has more hair on his chest. Have A Great Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: May 28, 1997
Subject: Re: No Subject
Stephen, Your are making a fine choice, some tail wheel time is a great idea! The champ will differ from the RV6 quite a bit, if you master the handling of the champ the 6 will be a piece of cake. The champ will react to inputs slower on the ground then the 6 will. Excellent choice for tail wheel training. If your used to only nose wheel aircraft it will feel strange at first give it 5 to 10 hrs and you will begin to feel very comfortable. Once you get the hang of it you wont feel unsafe and wont want that wheel meant for the rear end hanging off your front end. Good luck, have fun Ryan B ________________________________________________________________________________
From: Mlfred(at)aol.com
Date: May 28, 1997
Subject: Re: RV6 vs 6A decision
<< And there I saw N2NR, an RV6A painted in Navy colors that I absolutely fell in love with. Being ex Navy, the blue, grays and yellows along with the military bearing of the aircraft really appealed to me. >> I too saw that bird, and it is as you said. It would look just as good with a t/w, don't you think? Then, you could put a tailhook on it (for display only). Think of the questions you'd get! I remember reading that the most common accident that kills 172's is a groundloop! Now, very few of those have tailwheels, but they do have a high CG. Go figure. Check six! Mark ________________________________________________________________________________
From: "Noel Drew" <noeldrew(at)iafrica.com>
Date: May 28, 1997
Subject: Re: Antennas
Just a note to confuse the comments on the critical nature of coax cables. I recently had my usually well behaved radio criticised by the tower as being low on transmission strength and a check to a friend with a nearby receiver confirmed this. I transmit through a standard antenna located on top behind the cabin and receive through Van's tape antenna inside the windshield. (Narco Escort II). My first diagnosis was a faulty joint on the transmitting antenna and while performing the usual gymnastics under the panel, the local avionics man stuck his head in and enquired after my health. He then volunteered his help and kindly produced all the necessary test gear for a proper analysis. He found the output from the set healthy and nothing wrong with the antenna system. Switching transmission to the tape antenna produced a reasonable output signal despite the poor rating this antenna received from his test quipment. Reception on this tape antenna was however quite acceptable. The problem with the main antenna persisted and he suggested a bench test for the radio. No fault was found and in desperation I consulted a friend who had worked on military radios for many years. His suggestion was to make up a short length of coax and insert it in the line to the antenna. Strength 5! Next step? Leave it there. His explanation was that radios sometimes behave this way. I cannot totally rule out a fault with a connector which was disturbed by my experiments but his advice was deliberate and it came from experience. Kind regards, Noel Drew South Africa RV6 ZU-APF noeldrew(at)iafrica.com ________________________________________________________________________________
Date: May 28, 1997
From: "Larry D. Hoatson" <lhoatson(at)e2.empirenet.com>
Subject: Kit Shipping Charges
Would any of the Southern California builders be willing to provide some information, thoughts, and personal experieces regarding shipping charges for an RV-6 kit from the factory. We're trying to determine what the $$ difference would be by ordering the entire kit, and then having to store everything, versus receiving each kit about the time we're ready to begin work on it. Thanks in advance Larry -- Larry D. Hoatson Yucaipa, CA Redlands (L12) Airport lhoatson(at)empirenet.com KC6WYF via packet at: KC6WYF(at)W6JBT.SOCAL.CA.USA.NOAM Restoring 1950 Cessna 170A N9948A... Looking forward to RV-6 ________________________________________________________________________________
From: Tedd McHenry <tedd(at)idacom.hp.com>
Subject: RV Builders in Vancouver Area?
Date: May 28, 1997
I've just moved to the Vancouver (BC) area--specifically Cloverdale, near the Langely airport. I've seen one or two RVs flying around, and I've heard there are builders in the area. If you're a builder, or know of any, I'd love to hear from you. Email me directly, to avoid cluttering up the list. Tedd McHenry tedd(at)idacom.hp.com [RV-6 plans; still no workshop!] ________________________________________________________________________________
From: MAlexan533(at)aol.com
Date: May 28, 1997
Subject: RV-4 Kit
Looking for a half or more completed RV-4 kit. Must be good workmanship and good price. Must be located in the west. E-mail direct to: MAlexan533, or fax 503-838-3834. ________________________________________________________________________________
From: John Walsh <jwalsh(at)ftp.com>
Date: May 28, 1997
>>Reply to your message of 5/28/97 3:20 AM >> :) >> >>I have NEVER flown a taildragger, but I like the looks of them and their >>rough-field handling abilities (forget that 2 knot speed difference!).. >> >>But, I don't want to make the decision without some taildragger time. Stephen, I made the decision to go tailwheel with NO tailwheel time for the simple r= eason that I wanted to enhance my skills( and of course poke fun at my nose= wheel buddies). I like landing an airplane. I like it to be a litt= le bit challenging. The tailwheel option provides more opportunity to bui= ld those skills. =20 Now, as far as a Champ vs. an RV... HA HA HA HA HA HA !!!!!!!! That was = a good one. I always appreciate someone with a subtle sense of humor. = I'm flying a Citabria now and it is an absolute TANK compared to an RV. Heavy controls, long throw to get a response, an= d lousy feedback. =20 Nonetheless, it is forgiving, flies slow and is easy to land. It is a who= le barrel of fun compared to a Cherokee. Taildraggers are scarce in my n= eck of the woods and you can't be too fussy. I have also=20 heard that the Luscombe is a bit ill-tempered but they are not exactly read= ily available to try out. =20 So, I hope to rack up 50-100 hours in the Citabria and Cub and I hope that = will be enough when the big day comes.. =20 Good luck in your choice. I'm sure you'll enjoy either one immensely. John RV4 (working on wings)=09 ________________________________________________________________________________
Date: May 28, 1997
From: John Top <jjtop(at)cts.com>
Subject: Re: Aircraft oils
> But just like magnetos, carbs and everything else in our airplanes except electronics, we seem to be unwilling to accept change. The price we pay for that is 2000 hour TBO. Doug the real culprit is the Freindly Aviation Agency who has made so durn complicated and expensive to change anything on a certified (Jurasic) engine that Lycomming and Continental are stuck with cloning dinasours. John Top Phone: (619) 549-3556 ________________________________________________________________________________
From: Tedd McHenry <tedd(at)idacom.hp.com>
Subject: Re: RV-6 Aerobatics
Date: May 28, 1997
I have a related question. All my aerobatic experience is in jets--I've never done anything but straight-and-level and spins in a piston airplane, and damned little of that! As many have already stated, you can do any positive G manoeuvre in an RV (if you don't exceed the various limits). But what about manoeuvres that are sort of in the grey area, such as a vertical roll? What's a vertical roll going to do to your oil pressure and fuel pick-up? How about a hesitation roll at zero G--can you sustain that for long without running out of oil pressure or starving the engine of fuel? Tedd McHenry [RV-6 plans only] ________________________________________________________________________________
Date: May 28, 1997
From: "Vincent S. Himsl" <himsl(at)mail.wsu.edu>
Subject: RV8 #2 Changes?
Hello, Just received latest RVator and read the changes of RV8 #2 over the prototype. Mention was made of a new improved vertical stabilizer and rudder. Question to the list/Van's is..... Do our empennage kits have the newer version? If not, could someone who knows the difference between ours and the new elaborate a little more on the difference in performance. Any options for those who have not begun the improved pieces? Retrofits? This request is to the RV-list rather than Van's directly as I believe it to be a question of general interest. Vince Himsl Moscow, ID RV80296 Tail ________________________________________________________________________________
From: BigCfly001(at)aol.com
Date: May 28, 1997
Subject: Re: Wanted-Pneumatic Squeezer
Tom, could you e-mail me the details on your "harbor freight" press setup,I like the cost alternative to the squeezers.thanks chris marion RV-6 HS cincy,OH ________________________________________________________________________________
Date: May 28, 1997
From: KOZINSKI GARY <kozinski(at)symbol.com>
Subject: Re: Kit Shipping Charges
Larry, Buy the kits as you go and don't worry about the $$ differences. Doing it this way will give you the latest modifications in the kit when it arrives. Buying it outright you will have to make upgrades and/or changes as they happen. True, most of the bugs have been worked out but over time things change and get easier and better so its to your advantage to buy as you go. Considering how much you will spend overall, I would worry about a few dollars of shipping charges. If you budget is that tight then you should reconsider what you are doing. Gary - 10+ years building my 6 and still going! s/n 20038 ________________________________________________________________________________
Date: May 28, 1997
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Kit Shipping Charges
[snip!] > charges for an RV-6 kit from the factory. We're trying to determine > what the $$ difference would be by ordering the entire kit, and then > having to store everything, versus receiving each kit about the time > we're ready to begin work on it. Larry: Unless you are one of these FAST builders (or are getting a fast-build kit) -- get it one sub-kit at a time. The $$ you might save in shipping will almost certainly be offset by the fact that you will miss out on any future improvements. Van's is improving the kits all the time -- I would guess that kits shipped today involve 200-300 hours less build time for not much increase in cost than when I bough my kit. Randall Henderson, RV-6 randall(at)edt.com http://www.edt.com/homewing ________________________________________________________________________________
From: "Joe Rex" <jfr(at)ix.netcom.com>
Subject: Custom Builders
Date: May 28, 1997
Listers, For the last few months, I have been looking at my unstarted -4 fuselage kit sitting in the garage, feeling guiltier by the day. I am considering having someone build the fuselage. I would appreciate any input from someone on the list who has gone this route. I have talked to several of these outfits.. There is considerable difference in what they charge. Naturally all of them tout their abilities and quality. I am anxious to here what others think of their work. Joe Rex Looking at fuselage box ________________________________________________________________________________
From: "Daniel H. Morris III" <Morristec(at)icdc.com>
Subject: Re: Antennas
Date: May 27, 1997
All of Bob Nuckolls messages from the list that I get do not contain text. Is anyone else having this problem? Dan Morris ---------- > From: rv-list(at)matronics.com > To: Morristec > Subject: RV-List: Antennas > Date: Monday, May 26, 1997 4:43 PM > > > Received: from netcomsv.netcom.com [163.179.3.9] by bbs.icdc.com with smtp > 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: Mon, 26 May 1997 17:27:13 -0400 > From: "Robert L. Nuckolls, III" <compuserve.com!RNuckolls(at)matronics.com> > Subject: RV-List: Antennas > To: rv-list > Cc: europa , Glastar-List , > Kitfox List > Message-Id: <199705261727_MC2-1751-B3E4(at)compuserve.com> > Sender: owner-rv-list(at)matronics.com > Precedence: bulk > Reply-To: rv-list(at)matronics.com ________________________________________________________________________________
Date: May 28, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: Kevin Lane V-stab.
I sure hope we arent going to hear from Weldon or "the rocket builder" or their attorneys with a further definition of libel. You have made your point. Could you now stop please? Thanks, Mike Wills RV-4 (wings) willsm(at)manta.nosc.mil > I >bought the Tail Kit from a local fellow here named Weldon Tadlock as being 60% complete. I >bought it as is where is with no warranty, just like you did. If the situtation warrants, couldn't you >reskin the part? Would you blame me for stuff wrong with the Wing Kit even though it was in the >box when you bought it? Weldon used the rocket builder's jigs after hours, and perhaps Weldon >did not set them up correctly. ________________________________________________________________________________
From: jpl(at)showpg.mn.org (Joe Larson)
Subject: Re: Kit Shipping Charges
Date: May 28, 1997
Shipping charges are not terribly significant. I think the wing kit cost $119 to Minnesota, or something along those lines. If I had ordered the entire kit up front, I would NOT have gotten the significant changes Van has been making to the completeness of the kit. I recommend waiting -- it costs you a little bit, but the improvements are darn well worth it. -Joe > Would any of the Southern California builders be willing to provide some > information, thoughts, and personal experieces regarding shipping > charges for an RV-6 kit from the factory. We're trying to determine > what the $$ difference would be by ordering the entire kit, and then > having to store everything, versus receiving each kit about the time > we're ready to begin work on it. -- Joe Larson jpl(at)showpg.mn.org 612-551-1072 14190 47th Ave N. http://www.wavefront.com/~showpg Plymouth, Mn 55446 Future RV-6A pilot. ________________________________________________________________________________
From: "Joe Rex" <jfr(at)ix.netcom.com>
Subject: Custom Builders
Date: May 28, 1997
Listers, First off, this is the second time I've sent this message. The first one seems to have disappeared. My apologies if they both show up on the list. Quick question. Has anyone on the list had experience with any of the custom RV builders? I am interested in your comments about the person you dealt with. I'm considering it for my -4 fuselage. Joe Rex ________________________________________________________________________________
Date: May 28, 1997
From: Darwin Esh <103126.3212(at)CompuServe.COM>
Subject: Unsubscribe
Please Unsubscribe Darwin Esh 103126.3212 Sat May 31 will be my last day with CompuServe. So please UNSUBSCRIBE me ________________________________________________________________________________
Subject: Re: RV-6 or RV-6A?
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: May 28, 1997
writes: > >Subject:Tip on delaying the decision between 6 and 6A... > >For some reason, I seem to be having a much harder time than most in >trying to decide whether to build the 6 or the 6A. >So, I am joining a flying club that has a 1946 Aeronca Champ (can >someone >please comment on the handling differences between this and an RV-6? >AS THEY RELATE TO LEARNING TO T/O or LAND?!). I hope to use >what I learn from flying the Champ to help me decide which RV to >build. > Stephen, I heartily recommednd you build the RV-6. Taildragger experience will discipline your flying. The Champ will more than adequately prepare you for the RV-6. I have quite a bit of time in both the 7ECA Citabria and the RV-3,4,6. I find the RVs easier to land than the Citabria. Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 preparing to mount wings ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@iceland-c.it.earthlink.net>
Date: May 28, 1997
Subject: RST audio panel and marker beacon receiver
I need to start my panel pretty soon, so I'm planning it and getting ready to order the radios ($$$). I'm considering an RST 564 audio panel and an RST marker beacon receiver. I've corresponded with folks who have built these units, but I don't think I've spoken to anybody who has flown with them. I have a vague recollection of somebody who was unhappy with an RST marker beacon receiver, but I can't remember who it was. Anybody on the list have any experience to share? Thanks, Tim Lewis Canopy nearly finished --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
Date: May 28, 1997
From: John <john(at)catlover.com>
Subject: Re: Kit Shipping Charges
Larry: Don't forget to unpack so the paper doesn't stay in contact with the aluminum. -- Best Regards, John Bright, Newport News, VA, USA, john(at)catlover.com ________________________________________________________________________________
Date: May 28, 1997
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Yikes (CHATTER)
Jeez -- snakes, fire ants, scorpions.... and I was worried about that little puddle of water that always leaks in under the shop wall when it rains.... I guess I should count my blessings! Randall (sure glad to be an Oregonian) Henderson, RV-6 randall(at)edt.com http://www.edt.com/homewing PS. My kitty would NEVER pee on my airplane! (Then again, he'd probably never go after a copperhead either....) ________________________________________________________________________________
Date: May 28, 1997
From: Bob Bolander-RFLB50 <Bob_Bolander-RFLB50(at)email.sps.mot.com>
Subject: RE>Re- RV-List- Yikes! CHAT
RE>Re: RV-List: Yikes! CHATTER 5/28/97 I live in Austin, Tx. 2 days ago, killed a 3" scorpion in my garage, left on motorcycle to get ice cream and ran over a 5' rattler on loop 360. Just comes with the territory. BB -------------------------------------- Date: 5/28/97 2:08 AM From: rv-list(at)matronics.com@AZBCSM1 In some ways I hesitate to mention this but we don't got these problems on the Wet Side (as we Washingtonians fondly refer to the western side of the Cascade Mountains). Granted, I may see an occasional small spider making a web in my shop or have to chase a wasp. Snakes?? I haven't seen one in Seattle for at least 20 years. We do have them in the country but, even there, they are respectable snakes and don't invade the people domain. Now, I have a cousin living just west of San Antonio, TX. I visited her about two months ago and plan to drive down there in about two weeks. They have SNAKES and FIRE ANTS. I was baptized by a fire ant on my last trip there. I hope to avoid that this time. As far as snakes go, if I was to find ANY snake skin in my shop you can count on the fact that I would not be going in there until I was certain that no snake, alive or dead, was any in the vicinity. You note that you are retired Army; maybe that is a criteria for being able to live in these areas. My cousin is retiring from the Air Force on June 13, rank of bird Colonel. Not bad for a woman with only 22 years service; I tell her it is because she follows my advice, NOT!! John > > It's that time of year and the local wildlife are alive and well. >Recently, I found a 1 1/2 foot snake skin in my shop but didn't think much >of it. A couple of days later I found a 5 foot snake skin right by my >radio! That got my attention. In Kansas here we get some pretty big >Copperhead snakes. > My recent situation is that the snakes are out of hibernation and >the wasps and spiders are starting to build their nests. > I have two wings done and the empennage. Guess where they want to >build their nests? That's right! Inside the newly constructed pieces. > It prompted me to tape up all of the openings so there are no >unauthorized passengers in the future. > My advice to any builders that are like me and live in areas with a >lot of wildlife; be careful when you move pieces around that cover up >attractive areas for them to live. I spend 10 to 20 hours a week in my shop >so they are definately not afraid of me being there. > Does this deter me in any way? NO WAY! I want my RV4! (I am >retired Army, so this might account for my absense for common sense in these >areas) > >Good Luck! > >Tim Sweemer > >RV4 started fuselage > > > John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA 206-525-5445 RV-6 N16JA First flight August 1990 ________________________________________________________________________________
Date: May 28, 1997
From: Bob Reiff <Reiff(at)execpc.com>
Subject: Quickbuild primer
I am posting this for Mr. Jerry Thorpe, a local builder who is working on a RV-6 quickbuild kit and does not use PC's. He would appreciate replies from anyone who may have had a problem similar to the following, and if so what they did about it. Jerry was rinsing off primed aluminum sheets with water and the primer started peeling off in hand-sized pieces. He contacted Van's and got a letter back saying it was either a bad batch of paint, or the folks who produce the QB kits applied it wrong. He was told not to worry about it as primer is not necessary ("Piper and Cessna don't do it"), but if he wanted to he (Jerry) could re-prime it. He contacted the manufacturer, Sherwin-Williams, and was told one characteristic of the P60G2 Vinyl primer Van's is using is a tendency to lift itself if it is applied too thick. The dry film thickness should be 0.2 to 0.4 mils, compared to 1 mil for DuPont Variprime. He has measured the film thickness of the lifted pieces. Jerry is concerned about the quality of the prime job in the inaccessable areas like inside the wing, that if it peels off there he can't do anything about it, and he won't have the extra corrosion protection he paid for. If anyone has had a similar experience, Jerry would appreciate you contacting him at 414-593-5470, or E-mail me and I will pass on to him (E-mail me directly as I am not on the list). Thanks. Bob Reiff RV-4 #2646 ________________________________________________________________________________
From: dralle(at)matronics.com (Matt Dralle 510-606-1001)
Date: May 28, 1997
Subject: Message Problems...
Hi Bob, More than a few people have been complaining that messages you post to the List don't have any data in them. I'm not sure what do or say about it since the messages I get from you through the List have data, and the archive file also contains the data. The only thing I can think of is that somehow your messages contain some special characters or control character that is terminating the message before it is completely resent. Have you changed email programs or ISPs in the last few weeks that might be a place to start troubleshooting? I have subscribed a non-Matronics email account of mine to the List and will monitor it for your messages and see if it happens to me too. Could you send a couple of test messages to me and separately to the List so that I can compare the headers and data? Thanks, Matt Dralle RV-List Admin. -- Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94551 510-606-1001 Voice | 510-606-6281 FAX | dralle(at)matronics.com Email http://www.matronics.com/ W.W.W. | Featuring Products For Aircraft ________________________________________________________________________________
Date: May 29, 1997
From: "Stan Mehrhoff" <99789978(at)msn.com>
Subject: Dirt dobbers
I have a 66 X 90 hanger with the big end open. Have always had lots of dirt dobbers. I always fought them with soapy water in a backpack sprayer. Last fall I bought 4 of the things you plug into an outlet to keep rodents away. Guess what? So far this year no dirt dobbers. I am still keeping my fingers crossed. Stan Mehrhoff ________________________________________________________________________________
Date: May 28, 1997
From: Al Mojzisik <prober(at)iwaynet.net>
Subject: Re: Antennas
>All of Bob Nuckolls messages from the list that I get do not contain text. >Is anyone else having this problem? > >Dan Morris Dan, (And Matt) I get two messages from Bob N. and the second one is always identical to the first with the "=" followed by a number. Several listers do this double message thing. I don't know if it's me or them or the list but it started after Matt had that long down time over a week ago. Al ________________________________________________________________________________
Date: May 28, 1997
From: "Ray Murphy, Jr." <murphy(at)mail.coos.or.us>
Subject: Re:
Yes, I know that quandry that you're in concerning the 6-6A choice. My wife would prefer the 6A and we both like the looks of the 6. We decided on the 6A since my wife is terrified of a taildrager. When I took my test flight I asked Ken about the differences. I told him that one of my dreams was to be able to fly to some of the back contry strips and fish in Idaho. He told me that he'd had his 6A into many of those same strips with no problem and that the 6A had an advantage in landing and stopping over the 6. Good Luck on your decision. Ray and Nancy Murphy murphy(at)mail.coos.or.us RV6A empenage ________________________________________________________________________________
Date: May 28, 1997
From: Michael McGee <jmpcrftr(at)teleport.com>
Subject: Re: Parachutes
> Sec. 91.307 Parachutes and parachuting. > (c) Unless each occupant of the aircraft is wearing an approved parachute, Key word: "approved" FAR Part 21 (TSO C23c), NAS-804 and AS 8015-A Note that "approved" includes having it inspected and repacked within the last 120 days by a licensed parachute rigger rated for that particular type of parachute. Parachute Types: Back, Seat, Chest, and Lap. The last two are not practical for a pilot and the Seat is rare enough that if you actually found one you would have a tough time finding a rigger that could service it. > no pilot of a civil aircraft carrying any person (other than a crewmember) > may execute any intentional maneuver that exceeds-- > (1) A bank of 60 degrees relative to the horizon; or > (2) A nose-up or nose-down attitude of 30 degrees relative to the horizon. > >I could find no exit speed ratings in Parts 91 or 105. Ok, out comes the Parachute Manual :) The official document is Aerospace Standard 8015A-Minimum Performance Standards for Parachute Assemblies and Components, Personnel. .. 1.2 Weight/Speed Ranges 1.2.1 Category A: 90kg (198 lb) @ 130 knots 1.2.2 Category B: 115kg (254 lb) @ 160 knots 1.2.3 Category C: 115kg (254 lb) @ 175 knots --snip-- >weight parameters for a particular chute). I believe at exit the horizontal >velocity component diminishes almost instantaneously. > >Rob Acker / r.acker(at)ix.netcom.com / RV-6Q > > How fast does a "broken" airplane, that has a redline of say 220mph, go? Now realistically, if you get out of the plane at say 150 knots you will slow to about 100 knots in about 3 to 4 seconds --that's about a thousand feet-- and it isn't likely that you are going horizontal when you try to get out. If you can get the airplane to go into level flight you will probably stay with it. This is just a practical thing. If you are going to go to the trouble of wearing and maybe depending on a parachute you might want to know what it is rated for. Personally I've walked away from over 1500 half-an-airplane-ride (skydive) landings. Realistically it is only easy to get out of an airplane that is flying straight and level as recently demonstrated by 5 parachutists in a C-205 who were surprised by a flat spin from 3500 feet. They probably had almost 30 seconds to get out (no I didn't see the video footage). No disrespect here, my sympathies go out to their families. If I looked back and, say, saw the tail or just the elevator missing at say 2000 feet I know I'm behind schedule (getting out). Easy or not, if I'm going to go up and fly in a manner that I might possibly screw something up so as not to be able to get it back and no matter how remote the chance of me actually being able to get out is I still think it is nice to have a "Plan B". And some of them do make comfortable seat backs. This is only meant to offer some practical information about parachutes and getting out of an airplane. I'm a former parachute center operator/instructor, licensed parachute rigger and parachutist (customer now). If anyone finds fault with any of the info I have presented (aside from jumping out of perfectly good airplanes) please feel free to correct it. (Sorry about rambling on but today was my day to jump and, well, that good ol' northwet sunshine had the ceiling too low.. and raindrops are pointed on top). I think I just heard the beer light come on. Mike McGee jmpcrftr(at)teleport.com N6358G A ship in port is safe but that is not what ships are for.. ..the ship has sailed. ________________________________________________________________________________
Subject: Re: Aircraft oils
From: triedel(at)juno.com (Ted W Riedel)
Date: May 28, 1997
unsubscribe ________________________________________________________________________________
From: Bumflyer(at)aol.com
Date: May 29, 1997
Subject: Re:6 VS 6A
I have really tried to throttle myself and confined my opinions to a private reply; however the question of center of gravity has puzzled me for years. Which is more tail heavy? The 6 or the 6A? No one seemed to know and the samples in the handbook didn't show the all important engine and prop differences. This is something we all wanted to know as a consideration for our choice. I know this could spark a great debate with 20 or thirty opinions well substantiated with arguments about heavy tail wheels and heavy nose wheels. Or how about the effect of more aft main gear on the 6A. Unfortunately I know the answer. I you are making the choice based on Center of Gravity (or baggage capacity), forget it. They are both the same. A fellow builder and I used the same engine and prop but his was a tail dragger and mine was a 6A. Mine has a slider and is ten pounds heavier. Our center of gravity was within a few hundredths of an inch, which is beyond our ability to measure. We used the same scales. Now I know the next question is which is faster and how much? I assume his is but will let you know in about a month. Right now Mine has no fairings or pants and his is in the paint shop. ________________________________________________________________________________
From: JamesCone(at)aol.com
Date: May 29, 1997
Subject: Re: No Subject
I have over 1200 hours in tail draggers and learned to fly in them so I feel qualified to comment on the RV-6 vs the RV-6A. I have flown both the 6 and the 6A and the both fly the same in the air. I can feel no difference in handling. Both are outstanding!!! On the ground is another matter. To taxi a 6, you have to stretch to see over the nose or do "S" turns. If you have the tip up canopy, it is even more difficult to taxi if the canopy is tilted up to let a bit of air in. In the 6A, visibility is excellent. The 6A is much easier to taxi. On takeoff, the 6 requires quick reactions to keep things going right down the runway and when the tail comes off the ground even quicker reaction is required to keep things straight. It is possible to crash on takeoff in a 6 if you are not ahead of the plane. In fact, a 6 did just that on its first flight a Spirit of St. Louis airport. On the 6A a bit of right rudder is all that is required to keep things going right and takeoff is a breeze. I can't imagine how you could loose control on takeoff in a 6A. Landing is much more difficult in a 6. If you are not right on speed and have just the right attitude, you will bounce. This bounce can quickly become a series of bounces if you are not careful. Directional control in a 6 is also much more difficult. you literally have to fly the plane down to walking speed. The 6A is a peice of cake to land. When you touch down, the natural tendency is for the nose to fall and the plane does not bounce. Once the nose gear is on the ground the rest is a total no brainer. The plane wants to track down the runway like an arrow. Why subject yourself to grief to gain a couple of miles per hour and some possible improved looks. The tail dragger croud will tell you that "Real pilots fly tail draggers." Well, I'm here to tell you that Real pilots also fly nose draggers and have a lot more fun because they don't have to worry every time they land that they may bend their toys and they can taxi with ease to and from the runway. I would bet that the average RV pilot flying a 6 can't land any shorter than the average pilot flying a 6A. I can land and stop my 6A in less than 600 feet consistently. When Mike Seager was at my house for four days and gave 24 check out rides in the factory 6, I watched every one of the flights. I saw a lot of good pilots have a lot of trouble both on takeoff and landing in the 6. I have never seen a pilot have trouble with a 6A. Decide now and you won't end up with a heavy tail. Other considerations include resale value and insurance costs. Both favor the 6A. I am standing by in my Air Force issue Nomex fireproof flying suit for the flames about to come my way from the 6 guys, so fire away. You'll never convince me that a 6 is worth the trouble. Jim Cone, RV-6A flying great. jamescone(at)aol.com ________________________________________________________________________________
Date: May 28, 1997
From: Jerry Forrest <gforrest(at)nwc.net>
Subject: Re: Message Problems...
Bob I receive all your messages;however, all of your messages stop downloading of the remainder of the messages. I get a message saying that there are characters that are not recognized and ask if I want to delete or retry. Your messages look fine until after your name in the cartoon area. I see several strings of =30=30=30=30. This might be the area that is causing problems. Jerry Forrest > > > >Hi Bob, > >More than a few people have been complaining that messages you post to >the List don't have any data in them. I'm not sure what do or say about it >since the messages I get from you through the List have data, and the >archive file also contains the data. > ________________________________________________________________________________
Date: May 29, 1997
From: Mark & Candy LaBoyteaux <tailspin(at)ix.netcom.com>
Subject: IO-320B1A Problems.
Well, I have a few questions for those of you who are familiar with Lycomings. I have an IO-320B1A to put on my -6a, and I have already replaced the sump in order to mount the injector unit on the bottom. My Barry mounts arrived from Van's today, and I discovered that there are four special spacers that are used on the mounting of -B1A and -C1A engines that I am missing. The first place I called to try to track down a set of these was Bobby's Plane Parts in Texas, with no luck. My next call was to Van's. I recieved much sympathy and they wished me luck in my search. The part number that I need is LW-74465, does anyone know where I might be able to locate a set of these? Another thing that I discovered is that the engine mount bolts that I bought from Van's are going to be too short once I locate the missing spacers that this engine requires. Do any of you builders that are using a -B1A engine happen to know what length of AN bolts you wound up using? One more thing, I also bought a new Woodward prop governor from Van's. So I decided to go ahead and bolt it on. The studs on the governor pad are too short. There's just about one thread sticking out. Rats! Now I'm really bummed out! Has anyone else had this problem with the Woodward governor? It looks like all I need to do is install some longer studs, but where is the best place to buy this type of hardware? Aircraft Spruce and Specialty and others list AN hardware, but I haven't seen anybody list the coarse thread hardware that is used on Lycoming engines. By the way, why is it that all other aircraft hardware uses fine threads, but Lycoming engines all use coarse thread hardware? Looks like it's not gonna get bolted on by this weekend. Mark LaBoyteaux tailspin(at)ix.netcom.com RV-6a N106RV ________________________________________________________________________________
From: kevin lane <n3773(at)worldnet.att.net>
Subject: RPM limiters
Date: May 29, 1997
I received a Jeg's car racing parts catalog today and noticed they sell rpm limit modules. Does something similar exist for aircraft? I was thinking about the 2650 rpm limitation on the Sensenich prop. and how easy it will be to overrev in loops or 8's. Apparently it randomly grounds out the coil rather than simply shutting the engine down to keep the engine within limits. kevin ________________________________________________________________________________
Date: May 28, 1997
From: "Jerry H. Prado" <jerryprado(at)wa.net>
Subject: Re: Quickbuild primer
Bob Reiff wrote: > > > I am posting this for Mr. Jerry Thorpe, a local builder who is working on > a RV-6 quickbuild kit and does not use PC's. He would appreciate replies > from anyone who may have had a problem similar to the following, and if > so what they did about it. > > Jerry was rinsing off primed aluminum sheets with water and the primer > started peeling off in hand-sized pieces. > > He contacted Van's and got a letter back saying it was either a bad batch > of paint, or the folks who produce the QB kits applied it wrong. He was > told not to worry about it as primer is not necessary ("Piper and Cessna > don't do it"), but if he wanted to he (Jerry) could re-prime it. > > He contacted the manufacturer, Sherwin-Williams, and was told one > characteristic of the P60G2 Vinyl primer Van's is using is a tendency to > lift itself if it is applied too thick. The dry film thickness should be > 0.2 to 0.4 mils, compared to 1 mil for DuPont Variprime. He has measured > the film thickness of the lifted pieces. > > Jerry is concerned about the quality of the prime job in the inaccessable > areas like inside the wing, that if it peels off there he can't do > anything about it, and he won't have the extra corrosion protection he > paid for. > > If anyone has had a similar experience, Jerry would appreciate you > contacting him at 414-593-5470, or E-mail me and I will pass on to him > (E-mail me directly as I am not on the list). > > Thanks. > > Bob Reiff > RV-4 #2646 Two weeks ago, I spoke with Van's who informed me that the primer used on the quick builds was a clone of the Sherwin-Williams product. I just completed applying primer to a large number of parts using the Sherwin-Williams eg2-980 product - 1:1 mix with the 981 reducer. I applied it at approx 45 degrees and was very impressed with the adhesion. As the day warmed up, I was no longer able to visually see it migrate and etch so I stopped. Tonight, I ran some tests on scraps that I had sprayed. After bending, sanding and applying various solvents, only MEK or the reducer itself had any effect. I had the opportunity to talk to the regional rep who insisted that 'moisture sensitivity" was an issue with this product and he insisted that it should be 'sealed'. While putting my parts up, a drop of sweat fell on a spar web. The water was quickly absorbed and discolored the product. In summary, I am very happy with the etching and adhesive qualities of the product, however, don't expect moisture to bead up like it will with an epoxy product. Any feedback on applying a 'shop coat' of something on top of it on spar components ? Is build up an issue? Jerry Prado rv6A, wing ________________________________________________________________________________
From: ve7fp(at)jetstream.net (Ken Hoshowski)
Subject: Re: RV Builders Vancouver Area
Date: May 28, 1997
---------- > From: Ken Hoshowski <ve7fp(at)jetstream.net> > To: tedd(at)idacom.hp.com > Subject: RV Builders Vancouver Area > Date: Wednesday, May 28, 1997 9:36 PM > > Ted, > Send me your mailing address and I will send you a complimentary copy of > the Western Canada Rvator along with a membership list. This will give you > the names of many lower mainland builders. If you enjoy the newsletter. > We would welcome you to our group. Membership dues are $10.00 Ccn or $7.50 > U.S. for our quarterly newsletter. > > Regards > > Ken Hoshowski, Editor RV6 C-FKEH 160 HP C/S > Western Canada Rvator First Flight Sept 8 1994 > > Note : Our local Salmon Arm Flying Club Air Affair is coming up on June > 14/15. Free spaghetti dinner to flyins on Sat. Sunday pancake breakfast > starts at 8 A.M. Fly bys, Aerial demo's, giant flea market, etc. Good > motels available or Billets available for visiting RVers. Our good friend > John Ammeter from Seattle didn't know what a billet was. We Canadians talk > funny??? Eh, John.! We call it a chesterfield, you call it a couch, > anyway a billet is free accomodation and we welcome our American friends > to our fly in. The last time John flew up we had to put him in the dungeon > (bedroom under the garage) and the house still reverberated from his > snoring. Les Williams, I am sure will confirm this. Van's have been > invited but as yet have not confirmed attendance. They have been up a > number of times along with some of that great bunch from the Portland area. > I understand that Mike Seager will be up to give training rides to those > who want them. We expect about a dozen RV's in attendance. Last year we > had 10 RV's out of 85 flyins. Hope you might consider some of our local > hospitality. All Rver's on the list are invited. > > P.S. Matt, This is a great list and you are to be commended for the effort > you put in. We started building in 1989 (serial # 20332) and can honestly > say we have met and continue to meet and enjoy the friendships we have > made. With few exceptions the RV bunch are a great bunch of people. In > addition to building and flying a great airplane we appreciate the > comaraderie and friendship of all the RV builders we have met in both the > U.S. and Canada. > ________________________________________________________________________________
Date: May 29, 1997
From: L & M Rowles <lmrowles(at)netspace.net.au>
Subject: Re: Dirt dobbers
At 03:03 AM 29/05/97 UT, you wrote: > >I have a 66 X 90 hanger with the big end open. Have always had lots of dirt >dobbers. Stan what are dirt dobbers? Les Rowles Po Box 1895 Traralgon Australia 3844 ________________________________________________________________________________
Date: May 29, 1997
From: Rick Bottiglieri <rb(at)ozramp.net.au>
Subject: (no subject)
unsubscribe ________________________________________________________________________________
Date: May 29, 1997
From: L & M Rowles <lmrowles(at)netspace.net.au>
Subject: Fuel pressure
Hi All, Has anybody experienced fluctuating fuel pressure in the cruise? The engine is a 0-360. The bloke is convinced it not vapor lock. Les Rowles. Les Rowles Po Box 1895 Traralgon Australia 3844 ________________________________________________________________________________
Subject: Re: Dirt dobbers
From: bshaw5(at)juno.com (William H Shaw)
Date: May 29, 1997
Les - Dirt dobbers or mud daubers, as we call them in my area (upstate NY) are wasps that love to build their nests in any small hole or tube, e.g., pitot tubes or fuel tank drains. I've had these things happen on my Cessna 120 and are a royal pain. Hope this answers your question. Bill Shaw bshaw(at)juno.com ________________________________________________________________________________
Date: May 29, 1997
From: Phil Arter <philip.arter(at)mci2000.com>
Subject: Re: RV8 #2 Changes?
Vincent S. Himsl wrote: > > > Hello, > > Just received latest RVator and read the changes of RV8 #2 over the > prototype. Mention was made of a new improved vertical stabilizer and > rudder. Question to the list/Van's is..... Do our empennage kits have the > newer version? If not, could someone who knows the difference between ours > and the new elaborate a little more on the difference in performance. > > Any options for those who have not begun the improved pieces? Retrofits? > > This request is to the RV-list rather than Van's directly as I believe it to > be a question of general interest. > > Vince Himsl > Moscow, ID > RV80296 Tail Vince, hi I believe all the RV-8 kits have the larger VS and counter-balanced rudder. The prototype was unique. -- Phil Arter, RV-8 #80005 philip.arter(at)mci2000.com http://acd.ucar.edu/~arter/RV8.html (303)459-0435 home ________________________________________________________________________________
From: "Jeffrey Davis" <jdavis1(at)ford.com>
Date: May 29, 1997
rv-list(at)matronics.com
Subject: (Fwd) Tip on delaying the decision between 6 and 6A...
--- Forwarded mail from ("Jeffrey Davis") From: "Jeffrey Davis" <jdavis1(at)av5036.pd8.ford.com> Date: Wed, 28 May 1997 08:46:42 -0400 Subject: Tip on delaying the decision between 6 and 6A... I have spent time in many different conventional gear aircraft ranging from Champs to Beech 18s. The Champ is a great plane to learn the fundamentals. The Champs I have flown are very easy to land. In a couple hours you should start to feel comfortable. Don't forget to start on the grass and move to the pavement as your confidence and experience builds. Grass is the place to learn.. After you master the Champ I would recommend getting some time in something like a Luscombe 8 or a Stinson 108. Both of these airplanes will provide you with a new challenge. The Luscombe is a little quicker on final and has narrow, tall gear (and a bad reputation). The Stinson also is a bit more difficult to land smoothly and adds the complexity of flaps. I am building a 6 and have a few hours in the conventional gear version. They are very easy to handle on the ground. If you can handle a Champ/Super Cub or Luscombe, you will do fine in the RV. My wife is a pilot (C152) and wanted a trike but after a few hours in a Super Cub and now in a Luscombe, she can't understand why she was so scared of conventional gear. Good luck with your conventional gear training - Utilization should be one of the main drivers behind selection of the gear configuration. If you think you will fly the trike more, build it. If cross wind landings and "Fly until it is tied down" are more your style, go for the conventional gear. >I have NEVER flown a taildragger, but I like the looks of them and their >rough-field handling abilities (forget that 2 knot speed difference!).. >But, I don't want to make the decision without some taildragger time. >So, I am joining a flying club that has a 1946 Aeronca Champ (can someone >please comment on the handling differences between this and an RV-6? >AS THEY RELATE TO LEARNING TO T/O or LAND?!). I hope to use >what I learn from flying the Champ to help me decide which RV to build. >(Again, please don't think I'm implying that the Champ and RV handle >.the same! I just want to know if I feel comfortable handling the Champ, >would I feel at least as comfortable handling the RV-6?) >Stephen Heinlein >sheinlein(at)vnet.ibm.com (Almost done with second wing...) ---End of forwarded mail from rv-list(at)matronics.com -- Jeffrey S. Davis Senior Research Engineer Advance Vehicle Technology Ford Motor Company Phone (313)845-5224 Fax (313)845-4781 ---End of forwarded mail from ("Jeffrey Davis") -- Jeffrey S. Davis Senior Research Engineer Advance Vehicle Technology Ford Motor Company Phone (313)845-5224 Fax (313)845-4781 ________________________________________________________________________________
Date: May 29, 1997
From: Brian & Sharon Eckstein <eckstein@net-link.net>
Subject: Re: Dirt dobbers
Stan Mehrhoff wrote: > > > I have a 66 X 90 hanger with the big end open. Have always had lots of dirt > dobbers. I always fought them with soapy water in a backpack sprayer. Last > fall I bought 4 of the things you plug into an outlet to keep rodents away. > Guess what? So far this year no dirt dobbers. I am still keeping my fingers > crossed. > > Stan MehrhoffI was very surprised to rid my infested out-building of mice with one of these devices. Before installing it, I would see and hear mice every time I went out there. It's been a year now since I've seen one. Since the RV is being built in there, it's very important to keep those corroders out! You can bet they'll be in the hangar too. Brian Eckstein 6A-Wings ________________________________________________________________________________
From: sheinlein(at)VNET.IBM.COM
Date: May 29, 1997
Subject:Effects of "swivel" nosewheel on 6A vs 6 decision Thanks to everyone so far for their replies concerning my recent post on my dilemma as to whether to build a 6a or a 6. This list is fantastic and all the info I have been getting is GREAT! Thanks to everyone for their help, please keep the stuff coming! Also, everyone avoided the flamebait... awesome! I have gotten nothing but flame-free, super-helpful comments, suggestions, and opinions. I haven't decided yet what I'm going to do, but I do have another question which might influence my decision somewhat. And that is: "What is the story on that swivel nosewheel?" I have only a Cessna background and so am only familiar with a steerable nosewheel. I understand how a steerable nosewheel aircraft would be less susceptible to ground-looping. But, I can't understand how a swivel nosewheel plane could be any better in this case than a tailwheel! As far as I can see, there's nothing that keeps the plane tracking straight, since the nosewheel doesn't provide any "sideways" resistance? As always, any help here is much appreciated! Stephen Heinlein sheinlein(at)vnet.ibm.com (still pondering 6 vs 6a decision) ________________________________________________________________________________
From: CYoung9519(at)aol.com
Date: May 29, 1997
Subject: Re: RV-6 or RV-6A?
Stephen, I have several hundred hours in various tail dragger types, from ultralights to factory built and homebuilt. I took transition training in the RV6 a year ago and bought a 6A in January of this year. I'm very happy with my decision to go with the 6A. It really is easier to land, taxi and do anything on the ground. In the air, there seems to be very little difference including speed. Good luck. Chuck ________________________________________________________________________________
Date: May 29, 1997
From: Patrick Kelley <patk(at)mail.ic.net>
Subject: Re: Dirt dobbers
L & M Rowles wrote: > > Stan what are dirt dobbers? Les, they are a kind of wasp that builds it's nest of dirt and spit. If they can, they will build in an existing hole or tube and stop up the ends with their 'mud', but they will also happily attach a dirt tube to a flat surface if it is in a protected area (say, between stored sheets of aluminum). Each tube is filled with an egg and a paralysed spider. These are solitary wasps, not like the paper wasps, and not as agressive. However, their nests are a pain to remove. Sorry for the natural history lesson, but there is a way to reduce the population. Fill an old pickle jar about half full of gatorade and leave it out in the area you want to protect. The stuff in gatorade is poison to the wasps. This won't completely stop them, but every bit helps. PatK - RV-6A - Wing structure complete, top skins going on. ________________________________________________________________________________
Date: May 29, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re:6 VS 6A
> (Snip) >I know this could spark a great debate with 20 or thirty opinions well >substantiated with arguments about heavy tail wheels and heavy nose wheels. > Or how about the effect of more aft main gear on the 6A. ________________________________________________________________________________
Date: May 29, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: Custom Builders
(snip), > >For the last few months, I have been looking at my unstarted -4 fuselage >kit sitting in the garage, feeling guiltier by the day. I am considering >having someone build the fuselage. >Joe Rex >Looking at fuselage box > As I see it, it would not be any different then buying the Quick build kit. I don't know where you are located. Art Chard of Van's (now retired was doing it) here in Oregon along with the fellow mention a few postings ago (Dave, I believe). Both of these fellows are good builders. Many many others out there. Have A Great Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
From: Cafgef(at)aol.com
Date: May 29, 1997
Subject: Re: Junk email: Free Aircraft Tool Catalog
I'm missing all that junk mail. Are you sure that the junk comes from being on the matronics list? Gene -- Still trying to work up the nerve to cut on the canopy cafgef(at)aol.com ________________________________________________________________________________
Date: May 29, 1997
From: "Robert L. Nuckolls, III" <RNuckolls(at)compuserve.com>
Subject: Test Message for Matt . . .
Matt, Here's a lengthy test message . . . direct and copy through the list server . . . I'll let you know what I see too = =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D Re: Copy of: switch ratings /It is important to check the DC rating on the switch. = /You will note that many of the RS Switches only have = /AC ratings. = There are about 100 ways for manufacturer's to "rate" thier switches. I know of at least 20 different specifications in the military documents alone. The way switches are used in airplanes (less than 500 operations per year) the mechanical ratings of about ANY switch will give good service in an airplane. Generally speaking, a switch that is suited for = 10 amps at 125 volts AC will perform well at 10 ams and 14 volts DC. The most important aspect of switch selection for d.c. operation is how "snappy" it is. I'll quote an excerpt from the AeroElectric Connection's opening for the chapter on switches . . . . ----- Switches, relays and contactors are a family of basic = devices used to control flow of current in an electrical = system. The generic switch has been around from the = very beginning of electrification. Houses were convert ed from gas or oil to electrical illumination by literally = fastening lamp fixtures to ceilings, switches to walls and = connecting the whole mess together with wires that = were stapled to the surface. Even in these rudimentary = beginnings, switches were constructed to accomplish = connection or disconnection of electrical circuits with a = snap. As one rotated the handle of an early light = switch, a feeling of winding up a spring was unmistaka ble. At some point, tension was sufficient to push = internal parts past a detent and the switch would = complete its operation with a "click"; a sudden release = of tension could be felt in the fingers. = The need for snap action was well understood, espe cially in the early days of domestic power distribution. = Most houses were first supplied with direct current = (d.c.) in contrast with present day systems which supply = alternating current (a.c.). In the section on over voltage = protection I described special design efforts required = to control the fire between spreading relay contacts = which are attempting to bring a failed alternator/regu lator system under control. When d.c. was routed to = our ancestors homes, the problem of controlling high = voltage had to be addressed. In this instance, the high = d.c. voltage was not developed by a collapsing magnetic = field. The voltage was already high; 100 volts or so as = delivered to the back of the house! = A simpler device known as a knife switch was universal = in industrial applications. It operates in a manner which = is suggested by its name: a blade of conductive material = was moved by an insulated handle so that it was forced = between two spring loaded leaves of conductive materi al thus making a connection. Breaking connection was = accomplished by simply pulling the blade from between = the leaves. = = My earliest recollection of knife switches is from old = black and white movies. The good Doctor Frankenstein, = standing over his patient, is yelling instructions to Igor = who manipulates many switches and knobs on the = laboratory apparatus. Operation of these switches is = always accompanied with flashes of fire and puffs of = smoke. The effects were undoubtedly enhanced for the = benefit of the movie viewers, but then fire and smoke = was not totally out of character for this type of switch. = Indeed, hesitant or sloppy operation of a knife switch in = a high voltage circuit would produce long, hot blue = sparks accompanied by subsequent damage to the switch. = Purveyors of early electrification products and services = knew that consumers would not be favorably impressed = with little fires and puffs of smoke at their fingertips. = Snap action switches were developed in a successful = attempt to keep "lights" off of walls and up on ceilings = where they belonged! Control of high voltage d.c. using = snap action switches required no instruction or special = action on the part of the switch operator. A child could = easily accomplish a making or breaking of connection. = Thus children began to "make" more connections than = they "broke" and the seeds of eternally illuminated = children's bedrooms were planted. They thrive to this = day! -------------------------- 14 volt d.c. circuits DO NOT fall into the "too hard" pile for controlling arcing at contacts. The battery contactor should have a diode or MOV across its coil to corral inductive kickback, the starter contactor too. Landing lights are the only devices with a potentially high inrush and this is generally limited to about 5X due to wire losses; a 50 amp inrush isn't going to kill a switch with a few operations. I like to call people's attention to the switches used on thousands of Cessna 150's. I'll guarantee you those little plastic rockers cost under $1 when they were originally installed. The vast majority of them are still in service after 30 years. The C-150 I fly the most has all original switches and the airplane has over 3000 hours on it. /They almost certainly have gold contacts on the switches = /and probably would only support low current DC unless = /specifically stated that they can support higher currents. = Gold is used only on very LOW current switches and it is easily burned away if the switch's current ratings are exceeded even for an instant. You won't find any ordinary switches that use gold contacts. /Putting high current DC through these switches could = /possibly result in arc over and welded contacts. I've never seen a welded contact in a hand operated switch. Contactors do it regularly and that's mostly due to contact wear and metal transfer after many operations. Even the very best Cuttler-Hammer "aircraft quality" contactors weld shut and or burn up . . got one on my desk right now that came out of a KingAir air conditioning system. Sucker is pure toast! Except for an occasional sticking starter contactor (you need a starter energized light on panel !!!) stuck contacts in single engine airplanes are VERY rare. /Automobile switches would work fine but do check the = /rating of the switch first. Except for landing light and pitot heat, most airplane power control circuits are quite light . . . Even if you OVERLOAD a switch to 200% of its "rating" you may reduce it's laboratory life from 50,000 cycles down to 5,000 cycles . . . how long is it going to take you to "wear out" that switch in your airplane? Pick switches with substantial mechanical "feel" and good construction. Wiring terminals should be secure in the housing and not "wiggle" when pushed on. And yes, get a switch good for 7-10 amps and it will work fine about anywhere in your airplane. /RS do have some miniature toggles with high current = /DC contacts - my catalogue is in the office and I = /am a home wid a code so I can't dig out the numbers. The miniature toggles are generally limited to 5 amps and they have pretty close contact spacing when open. I do not recommend these devices for power control in airplanes. They're fine for audio and instrumentation switching or power control under an amp or so. /Are automobile switches of suitable quality for = /fitting into our Europa? I have looked high and low for = /suitable DC rated units without much joy. Is there a = /common divider to work out a dc rating for an ac rated switch? = The terms "quality" and "rating" are certainly unquanitified terms and in the context of this discussion, pretty meaningless. We need to learn failure tolerant design . . ASSUME that EVERYTHING you put in is going to fail at some point in time. If you need it for comfortable completion of flight, have a backup system. If NOT don't worry about it. In any case, the only reason for upgrading the QUALITY of a part should be because you're tired of replacing it, not because it damned near got you killed. Then it doesn't matter WHAT kind of switches you use. I hightly recommend the standard toggles that mount in 15/32" round holes. They are universally produced by hundreds of manufacturers, they are available with .25" fast-on tabs for easy installation and replacement. My idea of the ideal switch is one that can be replaced in 5 minutes for $5, sitting in the pilot's seat with only a nut-driver in = hand. /I was just wondering about using themocouples for an = /alternate power supply? A very perceptive question!!! And . . . believe it or not, it's not really to far out of reach . . = at least in principal. /AFAIK they are used on missiles and bomb { as in H, = /as in serious big bangs } fuses. = Actually, the device you're refering to is a "thermal battery" which is still a chemical battery like the ones you use in your flashlight. In this case, the electrolyte doesn't work until it's heated to a molten state at about 700 degrees F or hotter. We did a design review to consider a thermal battery in our latest upgrade to the AQM-37D, high altitude, Mach 4 target. These batteries are attractive for weapons systems because of their ability to deliver a lot of watts for a short period of time (generally limited to 10-20 minutes). They store very well (shelf life on the order of 10-50 years) and come to life in about 100-300 milliseconds after the thermite is touched off inside by an electrical squib from outside. We decided not to use it this time due to some changes in our lauch protocols that would have risked reduced reliability in other areas of the target's performance. But back to your original premise . . . Thermocouples are capable of delivering useful amounts of energy. One of the most common examples are the early electric gas valves for furnaces that took advantage of a remote thermostat. A thermocouple on the pilot light was connected in series with a thermostat in the house and a coil in the gas valve. The output voltage of these thermocouples was only 150-200 MILLIVOLTS so the valve coil was a special design. The CURRENT available was considerable so there was a useful amount of energy but a common mistake of installers or repair-persons unfamiliar with the technology was to = wire with ordinary 22AWG thermostat wire and throw away = too many millivolts in the conductors. I discovered this in my first exposure to such a system in a house I was = renting about 25 years ago. The house had been remodeled = in the summer; the thermostat moved and rewired. In the fall, End of test . . . . ________________________________________________________________________________
From: RV6ator(at)aol.com
Date: May 29, 1997
Subject: Re: No Subject
Hey Jim, GO FLY A KITE!!! Bill Mahoney Sherman, CT RV-6 N747W ________________________________________________________________________________
Date: May 29, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: Kit Shipping Charges
Ditto from me! $102 to ship my wing kit to San Diego. If I had ordered my wing when I ordered the empennage I would not have gotten the prepunched wing skins. It was worth waiting for. Mike Wills RV-4 (wings) willsm(at)manta.nosc.mil I recommend waiting -- >it costs you a little bit, but the improvements are darn well worth it. ________________________________________________________________________________
Date: May 29, 1997
From: RodWoodard <rodwoodard(at)mcione.com>
Subject: Re: Swivel nosewheel
Hello Stephen: I've got 90% of my time in a Piper Cherokee. Last August, Fred Stucklen was out here in Colorado visiting. He let me fly left seat in his 6A. (Fred's a brave man.) I can tell you that it the swivel nosewheel was absolutely no problem for me. I had no problem taxiing the length of our 8800' runway. Landing and the subsequent roll-out felt every bit as secure and stable as my Cherokee. The only problem I encountered in flying Fred's airplane is that RV's are so incredibly aerodynamic. I'm used to reducing power from cruise about 1/2 mile from the airport. I've got no problem losing the 20 mph or so down to a reasonable downwind speed. I tried that with Fred's -6A.... reduced the power all the way back to 1900rpm... the RV only slowed to about 130 mph. I didn't want to just pull the plug on the power and shock cool Fred's engine so I made gradual power reductions as I continued on downwind. Needless to say, I was still carrying far too much speed on final and we went around and tried it again. I'm pretty confident though that I could feel very comfortable transitioning from my Cherokee to the -6A after a couple of hours with an experienced RV-driver. Best regards, Rod Woodard Loveland, Colorado RV-8, #80033 > And that is: "What is the story on that swivel nosewheel?" > > I have only a Cessna background and so am only familiar with a steerable > nosewheel. > > I understand how a steerable nosewheel aircraft would be less > susceptible to ground-looping. But, I can't understand how a swivel > nosewheel plane could be any better in this case than a tailwheel! > As far as I can see, there's nothing that keeps the plane tracking > straight, since the nosewheel doesn't provide any "sideways" resistance? > > As always, any help here is much appreciated! > > Stephen Heinlein > sheinlein(at)vnet.ibm.com (still pondering 6 vs 6a decision) ________________________________________________________________________________
Date: May 29, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Tail/Nose (decision chatter)
I would like to say that I agree with Jim Cone for the most part. I have some tail wheel time (3000+) most all back 40 yrs.+ in Cubs, Luscombe, Swift, etc. For about 35 yrs I was in the heavies (25,000+) and didn't fly the light stuff during that period. I got an instructor here last year and took a several hrs of instruction in a 140. I have to admit there was some wobbling for a while and the wheel landings on a windless day I still work hard, (for me wheel landing work better under the condition that they are intented for..windy/x-winds) anyway it was a re-learning experience. Not only keeping the plane straight but flaring down in that hole (747 does that to your perspective). But soon I was think about watching that nose very carefully. I still drawing deep breathes as I sink into the above mentioned hole and so I have to force my self to go lower, but I still land a little high and firmer then is desired. I fly the 140 now mostly because I enjoy it for some unexplainable reason. But my ldgs & TO's are better in the 172 now, which I believe is due to the taildragger training. I can personally testify that even a 747 can give you test in a cross wind, it like to go into the wind just like its smaller brothers. So I'm of the opinion that some tail training would help us all. I intend to budget a minimum of 10 hrs of dual with Mike Seagar if he is available before I fly my -6. I have found over the years I start get the drift around 10 hrs. Now some folks are faster on the up take then me. That is a personal figure I have worked out. And the record shows it has worked so far for me. I stated before that I ended up with a -6 because of my engine (and I kind of wanted one anyway). I had originally choose the -6A. I believe Jim is correct in re-sale, seeing down the taxi way and someother things about the tail dragger, also. There are just a lot scare stories about tail draggers and fear breeds mistakes...but how do you RV-3, RV-4 and RV-6 guys with experience feel? Would you do it again? There must be a good cross section of experience and skill to help the new guys and the guys on the fence. I hope this type of exchange does not upset the majority of net guys. I do feel this type information is part of the whole process and might help some new builders. What do You think? Have A Great Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
Date: May 29, 1997
From: "Grant E. Young" <gyoung(at)crl.nmsu.edu>
Subject: Re: Quickbuild primer
If that isn't a Van's answer, I don't know what is. grant- (a less than anonymous RV-6 builder who thinks Van's has a great airframe but lousy customer/technical support) ________________________________________________________________________________
From: "Austin Tinckler" <tinckler(at)axionet.com>
Subject: Lawsuits
Date: May 29, 1997
Oh Boy ! Libel..Defamation..Lawsuit...Good name sullied...Ad infinitum. Ad nauseum. Are these RV terms ? Is it any wonder that people don't invite other people up for a ride too often anymore ? Let's enjoy the list for good RV comment.. Austin Rv-6, paint soon ? ________________________________________________________________________________
Date: May 29, 1997
From: "David J. Fitzgerald" <theredbaron(at)earthlink.net>
Subject: Re:
-> RV-List message posted by: "David J. Fitzgerald" Hello, An easy way to understand nosewheel stability is to look at a Big Wheel or kid's tricycle. A big wheel is a castoring type device also. If you roll it backwards it will tend to swap ends due to the placement of the center of gravity with respect to the wheels and center of rotation. This is deemed negative stability. If you roll the big wheel like a tricycle gear airplane it tends to straighten out even if you roll it with the wheel slightly turned. (this is positive stability). Therefore, a tricycle gear aircraft will still have a positive stability whether it is a steerable or swivel type! The Grumman Tiger has a full castoring nosewheel and needs to be steered with the brakes and not rudder inputs. This makes for a much less complex system. On the plus side there is no limit to the nosewheel angle like there is on a Cessna - this allows for very tight turns. On the negative side it is slightly more difficult to control tracking with brake inputs, but nothing major. ----------------------------------- David Fitzgerald RV-8 Serial #80333 theredbaron(at)earthlink.net ----------------------------------- ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: May 29, 1997
Subject: Re: RPM limiters
-> RV-List message posted by: RV4131rb(at)aol.com Kevin, I would consider using your self as the RPM limiter. You never know when a situation may arrise when you need that extra RPM. Ryan ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: May 29, 1997
Subject: Re: No Subject
-> RV-List message posted by: RV4131rb(at)aol.com OVER REACTING JUST A BIT ARENT WE JIM? Ryan ________________________________________________________________________________
From: dralle(at)matronics.com (Matt Dralle 510-606-1001)
Date: May 29, 1997
Subject: Re: Test Message for Matt . . .
-> RV-List message posted by: dralle(at)matronics.com (Matt Dralle 510-606-1001) Hi Bob, Well, I did find something interesting with your message. On my non-matronics email account, the "==> RV-List message..." line had been corrupted and a the "==>" replaced with some binary (non-ascii) character! The reason the characters were converted appears to be related to the MIME headers in your message - specifically the "quoted printable". On my non-matronics mailer, the following headers were added when the message was received: Content-Transfer-Encoding: 8bit X-MIME-Autoconverted: from quoted-printable to 8bit by roxanne.llnl.gov id IAA17 904 Basically the conversion as described in these two headers will convert a sort of 'ascii encoded' binary data. It also appears that the encoding uses the "=" character as the signal that the following two characters actually represent some binary character. The sequence "=3D" that many people see in your messages is actually how the "=" character is escaped so that "=" can be printed. So here's my theory: Each RV-List message starts with the sequence "==> RV-List...". Note the un-escaped "=" as far as MIME is concerned. It appears that "==>" when translated is some binary character. It would also appear that some people's mail programs are ending the message download when they encounter the character. I have changed the "posted by" banner from "==>" to the less controversial sequence "-->". I could be completely full of fuel lube on what's going on here, but hey, its a theory! Bob Nuckolls - Please post another message to the List for testing. Those of you having no-data problems - Please let me know via direct email to "dralle(at)matronics.com" if Bob's first message entitled "RV-List: Test Message for Matt . . ." contained any data, and more importantly, if his second test (yet to be sent, and beginning with the new "--> RV-List Message posted..." banner contained readable text. Thanks for the help everyone. Like I said, I'm not sure if this is it or not but is seems like a good possibility. Matt Dralle RV-List Admin. >-------------- > >Matt, > >Here's a lengthy test message . . . direct and copy >through the list server . . . I'll let you know what >I see too = > >=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D -- Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94551 510-606-1001 Voice | 510-606-6281 FAX | dralle(at)matronics.com Email http://www.matronics.com/ W.W.W. | Featuring Products For Aircraft ________________________________________________________________________________
Date: May 29, 1997
From: Robert Acker <r.acker(at)ix.netcom.com>
Subject: Re:
-> RV-List message posted by: Robert Acker >I have only a Cessna background and so am only familiar with a steerable >nosewheel. I tried to stay out of the nose vs. tailwheel debate since the archives are *packed* with the issue. I remember it was a very difficult decision for me too though. I am nosewheel trained, and have a whopping 1.5 hours of tailwheel time so weigh my opinions accordingly. The 6A is easier when on the ground in all respects, you "drive" it around. The 6 must be "flown" until tiedown, like all taildraggers. In the air, no difference. Unlike some have witnessed, I have seen many 3's, 4's and 6's taking off and landing and none bounced around madly or looked like they were out of control in any way. I know of one instance where two people each thought the other was taxiing the 6 they were in. It just rolled straight with no input until an object up ahead finally caused some pedal pushing. Discussions with many 4/6 pilots convinced me its not that big a beast, and generally much easier than any other taildragger they've flown. My mission is lots of localized fun flying, with the occasional x/c. If my mission was lots of x/c, I think I would consider the 6A (flight fatigue, local unfamiliarity, etc). In the end, I changed my 6A order to what I really wanted to build and fly. Just wait till you get to the engine/prop and VFR/IFR panel decisions, those are worser (spelling police - spelling error intentional)!!! Good luck, Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
Date: May 29, 1997
From: Robert Acker <r.acker(at)ix.netcom.com>
Subject: Re: Antennas
-> RV-List message posted by: Robert Acker >Several listers do this >double message thing. I don't know if it's me or them or the list but it >started after Matt had that long down time over a week ago. Al It's not on purpose. Ever since the list got back up and running, if I hit "reply" to a message it puts rv-list(at)matronics.com twice in the "To:" field. I have to remember to remove one of them, or the list gets hit with a double message. Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
Subject: Re: -6 vs -6A
From: bstobbe(at)juno.com (Bruce D Stobbe)
Date: May 29, 1997
\-\-\> RV-List message posted by: bstobbe(at)juno.com (Bruce D Stobbe) Steve wrote: snip >As far as I can see, there's nothing that keeps the plane tracking >straight, since the nosewheel doesn't provide any "sideways" >resistance? > I'm not a high time taildragger pilot, but I think that the main reason a trike is less prone to ground looping has more to do with the fact that the CG is forward of the main gear rather than aft of the main gear - and the heavy end wants to be in front. As I understand it, that's also why it is important to make your directional control inputs as soon as you detect movement of the nose, rather than wait until the heavier tail builds up some momentum which can develop into a ground loop rather quickly (on some aircraft). FWIW, I also struggled with this decision and ended up with the taildragger. My reasoning: looks better (IMO), ever-so-slightly faster (I hope), and, I wanted to add a new challenge and skill to my flying abilities (I hope the new skill doesn't end up having anything to do with salvaging a ground-looped a/c :>)). As an aside, and not that I'd recommend it, the FARs do not require a signoff or any other special rating to fly an experimental taildragger aircraft. If you're crazy enough you can legally hop right in and go for it. What's the logic behind that? Bruce Stobbe RV-6; N508RV (res) fuselage becoming lonely - I gotta get back at it. ________________________________________________________________________________
Date: May 29, 1997
From: randall(at)edt.com (Randall Henderson)
Subject: Re: (no subject)
-> RV-List message posted by: randall(at)edt.com (Randall Henderson) please send unsubscribe messages to the correct address, rv-list-request(at)matronics.com. 600 people have to hit the delete key whenever someone sends an "unsubscribe" to the rv-list. ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: May 29, 1997
Subject: Re: Experimental Maintenence
-> RV-List message posted by: RV4131rb(at)aol.com Fred, This is becoming a very interesting subject. Just being a pilot provides you with the authority to perform preventive maintenance, or does it? Prevntetive maintenance is part of Part 43 we are excluded from part 43 with the exception of 43D (used for condition inspections). I have gone through pages and pages of FAR's over the last couple of weeks trying to determine legaly what we can or cannot do. The truth is there is nothing I can find that says we can or we cannot work on our own aircraft. They have put the responsobility in our laps and given us no guidelines to follow. Part 91.163 (a) The owner or operator of an aircraft is primarily responsible for maintaining that aircraft in an airworthy condition, including compliance with Part 39 of this chapter. (b) No person may perform maintenance, preventive maintenance, or alterations on an aircraft other than as prescribed in this subpart and other applicable regulations , including Part 43. Here we are again part 43, we are excluded does this also mean we cannot do preventive maintenance on experimentals? preventive maintenance all falls under part 43. You are also correct on inspections 91.169 subpart (c) excludes us again from 100hr inspections and annual inspections and I see nothing about condition inspections. I know Ive read most of the information I use as my guideline from the advisory circulars. I dont believe the advisory circulars are legaly binding, however they offer us a good source of information to work from. I personally maintain my airplane as if it were a (spam can) for my own safety as well as whoever I might be taking along. would anyone else like to take a crack at this? Its not so easy! Ryan ________________________________________________________________________________
Date: May 29, 1997
From: Don McNamara <mcnamara(at)sbt.infi.net>
Subject: Re:
--> RV-List message posted by: Don McNamara > I understand how a steerable nosewheel aircraft would be less > susceptible to ground-looping. But, I can't understand how a swivel > nosewheel plane could be any better in this case than a tailwheel! > As far as I can see, there's nothing that keeps the plane tracking > straight, since the nosewheel doesn't provide any "sideways" resistance? Stephen-- I currently drive a Grumman Yankee, which is a lot like a -6A in many respects. Of course, it's also a lot different in most of the important characteristics (speed). Anyhow, it also has a free-castoring nosewheel, and I've never had any trouble tracking on a runway. You use differential braking to maintain direction while taxiing and during initial powerup for takeoff (which, in the Grumman, is less than exhilirating.) After that, the rudder becomes effective, and it flies like anything else. Plus, it turns on a dime, so spinning around at the gas pumps is a blast. Building the -8, and expecting there to be an -8A before I have to make that decision, I'll face the same dilemma. I'll probably stick with conventional gear so I can become one of those fabled "real pilots." Don't worry about the nosewheel. If you can groundloop a plane with a training wheel, you've got bigger problems to deal with. Hope that helps. --Don McNamara 80113 ________________________________________________________________________________
From: Chris D Cencula <ccencula(at)ford.com>
Subject: Re: Unsubsribe
Date: May 29, 1997
--> RV-List message posted by: Chris D Cencula UNSUBSCRIBE CCENCULA(at)MAILHOST.ELD.FORD.COM UNSUBSCRIBE CCENCULA(at)MAILHOST.FORD.COM UNSUBSCRIBE CCENCULA(at)ETCH08.ELD.FORD.COM ________________________________________________________________________________
Date: May 29, 1997
From: johntate(at)essex1.com (John Tate)
Subject: Re: 6 or 6A
--> RV-List message posted by: johntate(at)essex1.com (John Tate) VNET.IBM.COM!sheinlein(at)matronics.com wrote: > > > Subject:Effects of "swivel" nosewheel on 6A vs 6 decision > > Thanks to everyone so far for their replies concerning my recent post > on my dilemma as to whether to build a 6a or a 6. This list is > fantastic and all the info I have been getting is GREAT! Thanks to > everyone for their help, please keep the stuff coming! Also, everyone > avoided the flamebait... awesome! I have gotten nothing but flame-free, > super-helpful comments, suggestions, and opinions. I haven't decided > yet what I'm going to do, but I do have another question which might > influence my decision somewhat. > > And that is: "What is the story on that swivel nosewheel?" > > I have only a Cessna background and so am only familiar with a steerable > nosewheel. > > I understand how a steerable nosewheel aircraft would be less > susceptible to ground-looping. But, I can't understand how a swivel > nosewheel plane could be any better in this case than a tailwheel! > As far as I can see, there's nothing that keeps the plane tracking > straight, since the nosewheel doesn't provide any "sideways" resistance? > > As always, any help here is much appreciated! > > Stephen Heinlein > sheinlein(at)vnet.ibm.com (still pondering 6 vs 6a decision) Stephen The key here is the position of the main gear to the center of gravity of the aircraft. A nose weel aircraft will track straighter by having its mains behind the center of gravity. Picture a cart as apposed to a weelbarow. ________________________________________________________________________________
Date: May 29, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: Re: Quickbuild primer
--> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) Hi all, One of you complained about Van's support: > (a less than anonymous RV-6 builder who thinks Van's has a great > airframe but lousy customer/technical support) My experience with Van's technical support is that they do an excellent job. Okay, I confess, I've had a lot of experience with computer support -- as both receiver and giver of it. A friend once dealt with a nasty customer by hanging up on him in a clever way. While customer was ranting, the engineer shouted "Hello, hello" into the phone as if he was unable to hear anything and then hung up. I have more trouble reaching people in other companies when I want to buy something than I do from Van's when I want free support. In about a dozen calls, I've gotten one busy signal. The phone is almost always answered by some human who actually knows something, in fact, they've known all I needed. I've yet to ride in one but I believe all the reports on how great the RV flies but I can say that the documentation needs a lot of work. Many points of the design need work to make the aircraft easier to build. But customer support? I wonder what you want? Hal Kempthorne RV-6AQ -- Installing the canopy frame halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
From: SCHRICK_Mark/usa_carrollton_tx(at)usx011.stm.com
Importance: High
Date: May 29, 1997
Subject: For SALE: 76' Decathlon 8KCAB
rv-list-request(at)matronics.com, rv-list(at)matronics.com --> RV-List message posted by: SCHRICK_Mark/usa_carrollton_tx(at)usx011.stm.com --openmail-part-00dac823-00000001 1976 Decathlon 8KCAB 1350TTAF Lycoming 0-320 (150 Hp) Strong Engine 484 SMOH Compression HIGH (77,78,76,77) FULL inverted system Constant Speed Prop Apollo 760 COMM King KT-76A Transponder G-meter EGT/CHT (2) 5-point harnesses Gap Seals Spades Wheel pants Fresh Cover 1989 2 parachutes available Annual: April 97 extensive ($2000) New seat AD, cables,ect... Logs available by fax or mail Red/ White/ Blue stars and stripes scheme from factory Book value: $47,000 plus ; $39,500 Low book Asking: $41,500 Mark Schrick 1397 Boysea Drive San Jose, Ca 95118 (408) 266-1599 Phone/Fax --openmail-part-00dac823-00000001 FROM: SCHRICK_Mark/usa_carrollton_ca@usx011 djason(at)ix.netcom.com, rv-list-request(at)matronics.com, rv-list(at)matronics.com, rv-list-request(at)matronics.com, cmadden(at)wwi.net, rstear(at)mipos2.intel.com --openmail-part-00dac823-00000001-- ________________________________________________________________________________
From: BARNES_ERIC(at)Tandem.COM
Date: May 29, 1997
Subject: Re: Kit Shipping Charges - Financial Perspective
--> RV-List message posted by: BARNES_ERIC(at)Tandem.COM I'm doing the sub-kit route at this point. Here's why: 4) I think shipping/crating costs are somewhat cummulative. 3) Shipping costs are not too much for tail & wing kits. 2) LATEST UPDATES on sub-kit. 1) If I put the money I'm not spending in the bank (4%), or don't borrow it (12%): 4% 12% ------ ------- a) $3700 wing kit - wait 6 months = $ 70 $ 210 b) $3000 emp. kit - wait 12 months = $ 120 $ 360 c) $3500 finish kit - wait 18 months = $ 210 $ 630 ------ ------- TOTAL SAVED NOT purchasing entire kit $ 400 $ 1200 Now, some of that gets eaten up with price increases, but not that much. And you can time your purchases before prices go up. Plus there are the insurance/storage costs and headaches (any cats in the storage place?) when buying all at once. I think it definitely shows that WAITING DOESN'T COST ANYTHING, and may save you money. So, given #2, why buy all at once? EB #80131 - Rudder (HS and VS done, FINALLY!) ________________________________________________________________________________
Date: May 29, 1997
From: Scott Gesele <scottg(at)icsnet.com>
Subject: Re: RPM limiters
--> RV-List message posted by: Scott Gesele > >I received a Jeg's car racing parts catalog today and noticed they sell rpm >limit modules. Does something similar exist for aircraft? I was thinking >about the 2650 rpm limitation on the Sensenich prop. and how easy it will be >to overrev in loops or 8's. Apparently it randomly grounds out the coil >rather than simply shutting the engine down to keep the engine within >limits. kevin > > > Kevin, I'd be hesitant to install an RPM limiter that grounds the mags on a dual magneto system. Does this thing have a failure mode that would permanently ground both mags? On a race care it's no big deal, you loose the race and coast to a stop. In an aircraft over water you get wet. I consider the throttle the best, and most fail safe, RPM limiter available. Just my $.02 Scott Gesele N506RV (Learning to paint) ________________________________________________________________________________
Date: May 29, 1997
From: "John B. Abell" <jbabell(at)ix.netcom.com>
Subject: Pitot-Static Tube Alternatives
--> RV-List message posted by: "John B. Abell" I'm about ready to install a pitot-static tube and other components in my wing. I intend to use my RV-6A primarily for cross country flying including IFR. I've been considering two alternative heated pitot-static tubes: (a) the AN5814, which is mounted under the wing and is one of the pitot tubes for which Warren Gretz sells an installation kit that looks like a good deal, and (b) the AN5816-1 Kollsman type. The Kollsman tube is about 9.5 inches long and is intended to fasten to what I think would be a 1 inch O.D. tube with four screws. There's a picture of both types in the ACS catalog. The Kollsman is mounted so that it projects straight forward of the wing leading edge. It seems to me that the Kollsman tube has the better probability of sampling undistrubed air than the under-wing type. I would greatly value the comments and opinions of RV-List members on these two alternatives. Observed and validated airspeed data would be especially helpful. Thanks. Jack Abell RV-6A N333JA (Reserved) ________________________________________________________________________________
Date: May 24, 1997
From: "Jerry E. Walker" <efford(at)bellatlantic.net>
Subject: Re: How to prime lots of pieces at once?
--> RV-List message posted by: "Jerry E. Walker" > > << Stamping the numbers into the aluminum is a possibility, but presents > dangers of its own. Another alternative would be to make a part > number map of the pieces as they lay on the painting stand and > re-write the numbers on top of the primer with a Sharpie pen after the > paint dries. > > Has anyone else painted large numbers of parts at once? How did you > remember which part was which? Any advice is welcome! Thanks in > advance. >> > > After cleaning, just use a sharpie to write the number on. It will show > through the primer > I bought a Black & Decker vibrascriber to mark parts. Works great just like the parts to the wings that Van does.. Jerry Walker ________________________________________________________________________________
Date: May 29, 1997
From: mheaps(at)direct.ca (mike heaps)
Subject: Re: RV8 #2 Changes?
--> RV-List message posted by: mheaps(at)direct.ca (mike heaps) > >Hello, > >Just received latest RVator and read the changes of RV8 #2 over the >prototype. Mention was made of a new improved vertical stabilizer and >rudder. Question to the list/Van's is..... Do our empennage kits have the >newer version? If not, could someone who knows the difference between ours >and the new elaborate a little more on the difference in performance. > >Any options for those who have not begun the improved pieces? Retrofits? > >This request is to the RV-list rather than Van's directly as I believe it to >be a question of general interest. > >Vince Himsl >Moscow, ID >RV80296 Tail > Hi Vince I belive that the prototype is only a prototype, and changes mention in the RVator are reflected in all pre delivery kits. Mike Heaps Chilliwack British Columbia RV80280 wings ________________________________________________________________________________
Date: May 29, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re:
--> RV-List message posted by: Denny Harjehausen t. > >And that is: "What is the story on that swivel nosewheel?" > >I have only a Cessna background and so am only familiar with a steerable >nosewheel. > >I understand how a steerable nosewheel aircraft would be less >susceptible to ground-looping. But, I can't understand how a swivel >nosewheel plane could be any better in this case than a tailwheel! >As far as I can see, there's nothing that keeps the plane tracking >straight, since the nosewheel doesn't provide any "sideways" resistance? > Tracking is slightly better even with a free castering nose wheel, as mentioned earlier because of the main wheels and CG relationship. I saw a Grumman take for the weeds and cave the the nose gear under and slide to a halt on the prop. It is equiped like the -6A. The instructor on the aircraft said they had a weak brake on the down wind side and couldn't hold it with rudder. A Steerable in that case probably would have save the day. Have A Great Day! Denny Harjehausen, retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
Date: May 29, 1997
From: mauser(at)claris.com (Richard Chandler)
Subject: Re: Pitot-Static Tube Alternatives
--> RV-List message posted by: mauser(at)claris.com (Richard Chandler) >--> RV-List message posted by: "John B. Abell" > The Kollsman is mounted so that it projects straight forward of the > wing leading edge. It seems to me that the Kollsman tube has the > better probability of sampling undistrubed air than the under-wing type. I think the Kollsman tube also has a better chance of sampling someone's thigh on an airshow field. It may also disturb airflow over the top of the wing. On the other hand, it might be cool if you put a couple of them on each side and paint them to look like machine guns.... :-) -- Richard Chandler RV-6: Garage bought and being finished, saving for tools and tail kit. ________________________________________________________________________________
Date: May 29, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: Quickbuild primer
--> RV-List message posted by: Mike Wills Hal, Your assembling a quickbuild and asking for it to be easier? I would ask you the same question, what do you want? I have yet to find anything that could not be figured out by a careful study of the plans, but I would agree that Vans leaves it up to the builder to figure out the most suitable technique to assemble some parts. Personally I enjoy the challenge. As far as support, we have phone and online support as well as this list. There are also 1500+ flying aircraft worldwide that can be studied for tips and inspiration. It cant get much better than this can it? Mike Wills RV-4 (wings) willsm(at)manta.nosc.mil >--> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) Many points of the >design need work to make the aircraft easier to build. But customer support? I >wonder what you want? > > >Hal Kempthorne RV-6AQ -- Installing the canopy frame >halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC > > > > > ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@denmark-c.it.earthlink.net>
Date: May 29, 1997
Subject: Re: Pitot-Static Tube Alternatives
--> RV-List message posted by: "Tim Lewis" <timrv6a@denmark-c.it.earthlink.net> > I've been considering two alternative heated > pitot-static tubes: (a) the AN5814, which is mounted under the wing and > is one of the pitot tubes for which Warren Gretz sells an installation > kit that looks like a good deal, and (b) the AN5816-1 Kollsman type. >... The Kollsman is mounted so > that it projects straight forward of the wing leading edge. I opted for the AN5814 with Warren's mounting hardware. I've not yet flown my RV-6A, but I can tell you I was quite impressed with Warren's work and his customer service. His product was first rate, and installed easily. FWIW, I suspect the design sticking out of the front of the wing might be more likely to be damaged by people accidentally walking in to it. Tim --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
Date: May 29, 1997
From: "Jerry H. Prado" <jerryprado(at)wa.net>
Subject: Re: Quickbuild primer
--> RV-List message posted by: "Jerry H. Prado" Grant E. Young wrote: > > > If that isn't a Van's answer, I don't know what is. > > grant- > (a less than anonymous RV-6 builder who thinks Van's has a great > airframe but lousy customer/technical support) Grant, I respect your position. However, I never meant to convey such an oppinion as mine. I have had very good support from Van's. My situation was less than ideal, having bought a built tail from someone on the east coast who mis-stated the quality of the work and a wing kit circa 1992. Between Van's and the EAA advisor, I've been able to start building. Jerry Prado #22418 - RV6A ________________________________________________________________________________
Subject: Fwd: Tools for sale
Date: May 29, 1997
From: HARRY PAINE <HPair(at)thegrid.net>
--> RV-List message posted by: HARRY PAINE -- [ From: HARRY PAINE * EMC.Ver #2.5.02 ] -- ------ TOOL LIST FOR SALE Harry Paine 477 printz rd Arroyo Grande Cal 93420 805-481-2524 90% angle drills 1/4 28 thread rebuilt---------------------- ----------- 225.00* 45% angle drills 1/4 28 thread rebuilt -------------------- ----------- 225.00* * D Flush Rivet set with rubber guard extra wide 1 1/4 " wide much nicer than Averys. This is the best I've even seen while they last $10.00 # 8 nut plate jig .............................................. ..........12.00 15 mil thick 3M Alum sound damping tape (used on 767) 9" wide not available anywhere else other than 3M Sold by linear foot minimum 10' order 1.00/ln. ft. All Items tools guaranteed 30 days or your money back. Items sold and shipped UPS COD Cash or certified check. ** Limited Availability sold on a first come first serve basis. Email Harry Paine @ Hpair(at)thegrid.net call 805-481-2524 & leave message ------- FORWARD, End of original message ------- ________________________________________________________________________________
Date: May 29, 1997
From: David Price <dwprice(at)webspan.net>
Subject: Re: Quickbuild primer
--> RV-List message posted by: David Price Hal Kempthorne wrote: > > --> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) > > Hi all, > > One of you complained about Van's support: > > > (a less than anonymous RV-6 builder who thinks Van's has a great > > airframe but lousy customer/technical support) > > My experience with Van's technical support is that they do an excellent job. > Okay, I confess, I've had a lot of experience with computer support -- as both > receiver and giver of it. A friend once dealt with a nasty customer by hanging > up on him in a clever way. While customer was ranting, the engineer shouted > "Hello, hello" into the phone as if he was unable to hear anything and then hung > up. > > I have more trouble reaching people in other companies when I want to buy > something than I do from Van's when I want free support. In about a dozen > calls, I've gotten one busy signal. The phone is almost always answered by some > human who actually knows something, in fact, they've known all I needed. > > I've yet to ride in one but I believe all the reports on how great the RV flies > but I can say that the documentation needs a lot of work. Many points of the > design need work to make the aircraft easier to build. But customer support? I > wonder what you want? > > Hal Kempthorne RV-6AQ -- Installing the canopy frame > halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC Hal may I suggest you read the original post,My brother is expecting a QB to be delivered any day now and I hope he dos'nt see the same thing. Dave Price ________________________________________________________________________________
Subject: Sensenich props, et al...
From: ebundy(at)juno.com (Ed Bundy)
Date: May 29, 1997
--> RV-List message posted by: ebundy(at)juno.com (Ed Bundy) >I received a Jeg's car racing parts catalog today and noticed they >sell rpm limit modules. Does something similar exist for aircraft? I was >thinking about the 2650 rpm limitation on the Sensenich prop. and how easy it >will be to overrev in loops or 8's. Apparently it randomly grounds out the I've noticed a lot of concern lately on the Sensenich prop in regards to overspeeding. Folks, it just isn't a problem with reasonable throttle management. I loop and roll my 6A regularly with a Sensenich/0-320 combo. In a loop, as you come over the top and start back down, you smoothly retard the throttle. That's it. I've never used a CS equipped aircraft for aerobatics, but I would imagine that even then you need to retard the throttle on the way down to keep the airspeed down. For the record, the limit is 2600, and I've only exceeded it twice by about 20-30 rpm for a couple of seconds. Neither time was due to acro, but just descending at too high an airspeed. It is possible to overspeed at high power settings during descent, but I don't do that very often anyway. I have an E.I. tach, which can be calibrated for any max RPM. The red LED at the top of the arc flashes when you hit 2600 and is very noticeable. I think the Sensenich prop is VERY efficient, and has more than enough going for it to compensate for the rpm limitation. A lot of people think the limitation causes a lot of problems, but everyone I know that uses it loves it. The limitation is really a non-issue. P.S. If anyone cares, the picture in the new RVator of Ed O'Grady is actually me. Ed (O'Grady) Bundy RV6A - first flight 11/20/96 ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
Date: May 29, 1997
From: Al Mojzisik <prober(at)iwaynet.net>
Subject: Re: Sensenich props, et al...
--> RV-List message posted by: Al Mojzisik >--> RV-List message posted by: ebundy(at)juno.com (Ed Bundy) >I've noticed a lot of concern lately on the Sensenich prop in regards to >overspeeding. tle on the way down to keep the airspeed down. >For the record, the limit is 2600, and I've only exceeded it twice by >about 20-30 rpm for a couple of seconds. Neither time was due to acro, >but just descending at too high an airspeed. It is possible to overspeed >at high power settings during descent, but I don't do that very often Ed, Isn't the concern for overspeeding in a "power applied" condition and not a "windmilling" situation? I thought the power pulses are what set up the prop harmonic that may lead to destruction. (Shuddering all over at the thought) Al ________________________________________________________________________________
Date: May 29, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: Antennas
--> RV-List message posted by: John Darby <johnd@our-town.com> >>All of Bob Nuckolls messages from the list that I get do not contain text. >>Is anyone else having this problem? >I get two messages from Bob N. and the second one is always identical to >the first with the "=" followed by a number. Several listers do this >double message thing. I don't know if it's me or them or the list but it >started after Matt had that long down time over a week ago. Al If it helps to find the problem-- I get the same as Al has stated. It will also stop my coping from the server and ask me if I want it converted or ignored. I must then select one or the other before it will continue. I am using Eudora Pro and I think there is something called mimi or so that I have on 'yes'. Seems like some time ago someone mentioned that may make a difference? John Darby RV6 N61764 flying Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: May 29, 1997
From: Kenneth Turner Demmons <demon(at)netside.com>
Subject: unsubscribe
--> RV-List message posted by: Kenneth Turner Demmons unsubscribe ________________________________________________________________________________
From: "Daniel H. Morris III" <Morristec(at)icdc.com>
Subject: Re: Pitot-Static Tube Alternatives
Date: May 29, 1997
--> RV-List message posted by: "Daniel H. Morris III" A pitot sense head or static source must be extended a minimum of about 1/3 cord in front of the leading edge to get to undisturbed air. Dan Morris Morristec(at)icdc.com ---------- > From: rv-list(at)matronics.com > To: Morristec > Subject: Re: RV-List: Pitot-Static Tube Alternatives > Date: Thursday, May 29, 1997 5:38 PM > > > Received: from netcomsv.netcom.com [163.179.3.6] by bbs.icdc.com with smtp > 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 > X-Mailer: InterCon TCP/Connect II 2.3.1 > Message-Id: <9705291624.AA16552(at)marble.claris.com> > Date: Thu, 29 May 1997 16:24:16 -0800 > From: claris.com!mauser(at)matronics.com (Richard Chandler) > To: rv-list(at)matronics.com > Subject: Re: RV-List: Pitot-Static Tube Alternatives > Sender: owner-rv-list(at)matronics.com > Precedence: bulk > Reply-To: rv-list(at)matronics.com > > --> RV-List message posted by: mauser(at)claris.com (Richard Chandler) > > >--> RV-List message posted by: "John B. Abell" > > The Kollsman is mounted so that it projects straight forward of the > > wing leading edge. It seems to me that the Kollsman tube has the > > better probability of sampling undistrubed air than the under-wing type. > > I think the Kollsman tube also has a better chance of sampling someone's thigh > on an airshow field. It may also disturb airflow over the top of the wing. > > On the other hand, it might be cool if you put a couple of them on each side > and paint them to look like machine guns.... :-) > > > -- > Richard Chandler > RV-6: Garage bought and being finished, saving for tools and tail kit. ________________________________________________________________________________
From: Gusndale(at)aol.com
Date: May 29, 1997
Subject: Re: Aeroflash Strobe Kits
--> RV-List message posted by: Gusndale(at)aol.com Hi Everyone! I've been lurking on the list for a few months now and really appreciating the wealth of expertise and experience here. I'm getting close to finishing my wings (RV6A) now and have a question I hope you can help me with. I want to put nav/strobe/position lights on the wingtips with separate power supplies at each wingtip. I know I can get a Whelen kit from Van's or a lot of other sources for about $700. Here's the Question: Aeroflash has a "double flash" Nav/strobe/position kit available through Frederick Custom Airframe; Austin,Texas for about $400. This sounds like a deal, but I don't know anything about the Aeroflash kit or Frederick Custom Airframe except what was on a one page flyer I picked up at a builder's group meeting. Does anyone have enough experience with Aeroflash kits (reliability,completeness of kit, etc.) to offer an opinion whether the Aeroflash unit is good or if I should just spend the money and go with Whelen? Also does anyone have experience with Frederick Custom Airframe? Thanks in advance to all who respond. Dale Wotring Vancouver, WA RV6A finishing up the wings ________________________________________________________________________________
Date: May 29, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: RV8 #2 Changes?
--> RV-List message posted by: Bill Benedict Vince and RV-List, The RV-8 #1 first flew in July '95. Obviously, we put time on it prior to arriving at Oshkosh '95, but the flight there and back, plus subsequent testing confirmed that some changes were necessary for that *RV feel*. One of the noticeable items was a small amount of yaw when encountering turbulence. Van spent the fall of '95 evaluating this annoyance and changes that could be made to regain the RV feel. This change was as described in the RVator. By Sun 'N Fun '96, we had a handle on it and introduced the tail kits. Although the #1 -8 is still sporting the original tail, it did have a different unpainted stab and rudder on it for a while, but not wanting to waste an almost good component and paint job, we are still flying the original. With all the demo flights that we have done in the aircraft during the last year, not one person has commented about the yaw. So, where does that leave us? Chances are most people would probably not even "pick up the problem" if you were building the original tail, but all of the tail kits in the field are just like the yellow #2. Now all 375 RV-8 builders can sleep peacefully tonight;) The changes to the fuselage are just creature comforts, like more elbow room in the back seat. The baggage door was moved to the opposite side and I do not know what prompted that move, possibly because the area was expanded vertically down the side of the fuselage by the entrance to the baggage area, and the engine controls and fuel lines needed the left side of the fuselage for traveling to the firewall. I believe Van also lowered the top of the fuselage slightly to improve visability over the nose. Bill > >Hello, > >Just received latest RVator and read the changes of RV8 #2 over the >prototype. Mention was made of a new improved vertical stabilizer and >rudder. Question to the list/Van's is..... Do our empennage kits have the >newer version? If not, could someone who knows the difference between ours >and the new elaborate a little more on the difference in performance. > >Any options for those who have not begun the improved pieces? Retrofits? > >This request is to the RV-list rather than Van's directly as I believe it to >be a question of general interest. > >Vince Himsl >Moscow, ID >RV80296 Tail Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@norway-c.it.earthlink.net>
Date: May 29, 1997
Subject: Accomodating Instrument Placement
--> RV-List message posted by: "Tim Lewis" <timrv6a@norway-c.it.earthlink.net> In the RV-6A slider configuration there are 3 ribs that support the glareshield and to which the instrument panel attaches. The three pieces are 2 ea F-6107 and 1 ea F6108. Wouldn't you know it, these pieces interfere with my ideal location of my flight instruments. These pieces are 1.5 - 2" high at the instrument panel, but they get longer (more vertical extent) forward of the instrument panel, so they sit right where the back end of some of my instruments and radios should go. (view this with a non-proportional font to see picture clearly) ------------------------------------| | | | F-6107 / | | / | | / |<--instrument panel | / | | / | | / I'm considering modfying F-6107 by cutting off some of the angled portion and reinforcing it with some angle. The result would be: ------------------------------------| | F-6107 _______________________| | | | | | | | | |<--instrument panel | | | | / | | / It seems to me that F-6107 thus modified would still be strong enough to support the instrument panel and glare shield, especially in view of the notched angle piece that's riveted to the entire underside of the glareshield right behind the instrument panel. Any comments on my idea? Also, does anybody know how big of a hole is required for the post lights Van's sells? Thanks, Tim --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
Date: May 29, 1997
From: "Robert L. Nuckolls, III" <RNuckolls(at)compuserve.com>
Subject: Test Message for Matt . . .
--> RV-List message posted by: "Robert L. Nuckolls, III" Matt, It seemed to all come though intact this time . . . = Bob . . . ________________________________________________________________________________
Date: May 29, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Nose wheel not ground looping.
--> RV-List message posted by: Bill Benedict Ground looping is primarily caused by the relationship of the center of mass of the aircraft with respect to the axle placement. Trigear aircraft have the center of mass forward of the main axles, so this mass pulls the gear along. The conventional gear has the center of mass aft of the gear, so the mass is pushing the main gear. All is fine until this mass gets out from behind the gear, then it swings around and wants to pull the mass with it. If you want to see a simple example, next time your wife goes grocery shopping, volunteer to go along and push the cart. This will earn you points!, as long as she does not know that you are experimenting. When the cart is about half full, go around a corner at normal cart speed and notice how easy it is to straighten out once you have made a 90 degree turn. The mass of the cart is pulling the main non-steerable wheels. Then turn the cart around and push it around the corner at the same speed with the castering wheels in the back, like a tail dragger. Now the mass is pushing the main wheels and you will experience a different steering sensation as you go around the corner. Yes Martha, even a grocery cart can ground loop. Make sure your wife is out of sight when performing the experiment. Bill, the backward grocery cart driver, but supporter of the training wheel up front, not because of the landings, but the great visability when taxiing on the ground. Actually, landing a tail dragger gives a pilot a greater sense of accomplishment than landing a trike. > >Subject:Effects of "swivel" nosewheel on 6A vs 6 decision > >Thanks to everyone so far for their replies concerning my recent post >on my dilemma as to whether to build a 6a or a 6. This list is >fantastic and all the info I have been getting is GREAT! Thanks to >everyone for their help, please keep the stuff coming! Also, everyone >avoided the flamebait... awesome! I have gotten nothing but flame-free, >super-helpful comments, suggestions, and opinions. I haven't decided >yet what I'm going to do, but I do have another question which might >influence my decision somewhat. > >And that is: "What is the story on that swivel nosewheel?" > >I have only a Cessna background and so am only familiar with a steerable >nosewheel. > >I understand how a steerable nosewheel aircraft would be less >susceptible to ground-looping. But, I can't understand how a swivel >nosewheel plane could be any better in this case than a tailwheel! >As far as I can see, there's nothing that keeps the plane tracking >straight, since the nosewheel doesn't provide any "sideways" resistance? > >As always, any help here is much appreciated! > >Stephen Heinlein >sheinlein(at)vnet.ibm.com (still pondering 6 vs 6a decision) > > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
Date: May 30, 1997
From: "Robert L. Nuckolls, III" <RNuckolls(at)compuserve.com>
Subject: RPM limiters
--> RV-List message posted by: "Robert L. Nuckolls, III" /I received a Jeg's car racing parts catalog today = /and noticed they sell rpm limit modules. Does = /something similar exist for aircraft? = How about a constant speed prop? /I was thinking about the 2650 rpm limitation on the = /Sensenich prop. and how easy it will be to overrev = /in loops or 8's. Apparently it randomly grounds out = /the coil rather than simply shutting the engine down = /to keep the engine within limits. kevin Such a device may well limit rpms but remember that you have to shut off TWO systems. Also, when sparks stop happening, uncombusted fuel/air piles up in exhaust systems with predictable results when the sparks come back on! Very hard on exhaust systems . . . Bob . . . ________________________________________________________________________________
Date: May 29, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Sensenich props, et al...
--> RV-List message posted by: Bill Benedict >>I've noticed a lot of concern lately on the Sensenich prop in regards to >>overspeeding. tle on the way down to keep the airspeed down. > >>For the record, the limit is 2600, and I've only exceeded it twice by >>about 20-30 rpm for a couple of seconds. Neither time was due to acro, >>but just descending at too high an airspeed. It is possible to overspeed >>at high power settings during descent, but I don't do that very often > >Ed, >Isn't the concern for overspeeding in a "power applied" condition and not a >"windmilling" situation? I thought the power pulses are what set up the >prop harmonic that may lead to destruction. (Shuddering all over at the >thought) > >Al > Ed and Al and others, If we could get Martin Sutter to comment, He has some interesting info on the 180hp Sensenich prop (it is not available so don't ask. They are still working on it). Sens has been using his plane for most of the tests. On one version of the prop, they determined that the prop developed a serious harmonic that would terminate the props existence (and maybe the planes) in just a few minutes if left in this mode. This mode was when the plane was pushing the prop during a low power-setting descent. Sensenich has a web page and they openly discuss the tests they have performed. It is quite interesting. You can get there through the Yeller pages (sp) or Van's homepage (I think) or try www.sensenich.com (it works, I just tried it). Bill Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
From: "Robert Greener" <rgreener(at)micron.net>
Subject: EGT probes
Date: May 29, 1997
--> RV-List message posted by: "Robert Greener" Hi everyone, I have an RMI engine analyser / 0-320 Lycoming engine with the High Country exhaust system as supplied by Vans. Question: Where do I drill the hole on the exhaust system for the EGT probes? Any help would be greatly appreciated. Many thanks. Rob Greener, RV-6A, N418RL (Reserved), WILL fly in June 1997. rgreener(at)micron.net ________________________________________________________________________________
Date: May 29, 1997
From: John Top <jjtop(at)cts.com>
Subject: Re: Antennas
--> RV-List message posted by: John Top >--> RV-List message posted by: John Darby <johnd@our-town.com> >If it helps to find the problem-- I get the same as Al has stated. It will >also stop my coping from the server and ask me if I want it converted or >ignored. I must then select one or the other before it will continue. I am >using Eudora Pro and I think there is something called mimi or so that I >have on 'yes'. Seems like some time ago someone mentioned that may make a >difference? John: I also use Eudora Pro and get the same alert on Bob's and several other lister's messages. If you select the delete option you only get one message, the one without all the "=" codong. doesn't solve the total problem but helps some. John Top Phone: (619) 549-3556 ________________________________________________________________________________
Date: May 30, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: Quickbuild primer
--> RV-List message posted by: "les williams" I don't have any experience with the QB primer lifting, but I do have a question as to what "primed aluminum sheets" he had a problem with. As far as I know there are no parts primed that have not already been made a part of an assembly, and I wonder what one would be doing washing it down with water to start with. If he was preparing to recoat it, I think a cleaner like "acryli-clean" or similar should have been used. But I agree that it shouldn't come off, regardless, and that the only solution is to re-prime or leave it as is. I have found one area on my QB where the primer wiped away as if it wasn't mixed or applied properly and had not etched into the metal. I will be re-priming that area anyway and applying a top coat, so I won't worry about it. Les Williams/RV-6AQB/N24LW (res)/started finish kit 5/23/97 ---------- From: owner-rv-list(at)matronics.com on behalf of Bob Reiff Sent: Wednesday, May 28, 1997 7:12 PM Subject: RV-List: Quickbuild primer I am posting this for Mr. Jerry Thorpe, a local builder who is working on a RV-6 quickbuild kit and does not use PC's. He would appreciate replies from anyone who may have had a problem similar to the following, and if so what they did about it. Jerry was rinsing off primed aluminum sheets with water and the primer started peeling off in hand-sized pieces. He contacted Van's and got a letter back saying it was either a bad batch of paint, or the folks who produce the QB kits applied it wrong. He was told not to worry about it as primer is not necessary ("Piper and Cessna don't do it"), but if he wanted to he (Jerry) could re-prime it. He contacted the manufacturer, Sherwin-Williams, and was told one characteristic of the P60G2 Vinyl primer Van's is using is a tendency to lift itself if it is applied too thick. The dry film thickness should be 0.2 to 0.4 mils, compared to 1 mil for DuPont Variprime. He has measured the film thickness of the lifted pieces. Jerry is concerned about the quality of the prime job in the inaccessable areas like inside the wing, that if it peels off there he can't do anything about it, and he won't have the extra corrosion protection he paid for. If anyone has had a similar experience, Jerry would appreciate you contacting him at 414-593-5470, or E-mail me and I will pass on to him (E-mail me directly as I am not on the list). Thanks. Bob Reiff RV-4 #2646 ________________________________________________________________________________
From: KennyCobb(at)aol.com
Date: May 30, 1997
Subject: Re: Bakersfield Fly-In & Bar-B-Que
--> RV-List message posted by: KennyCobb(at)aol.com Bakersfield, Ca EAA Chapter 71 BBQ & Fly-In will be June 7th. The Bar-B-Que dinner will be served around 3:30 pm. Our featured speakers for the fly-in will be Jon Sharp, owner/pilot of "Nemesis" and his crew chief Steve Ericson. Jon will trailer his world record holding Formula One racer for display. There may even be a few RV's there. Last year I think we had 33 RVs in attendance. The Fly-In will be at Bakersfield Muni airport ( L-45 ) . Ken Crabtree kennycobb(at)aol.com ________________________________________________________________________________
Date: May 29, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: RV-6 vs RV-6A
--> RV-List message posted by: Jerry Springer Well I started to write a long response to Jim Cones view of -6 vs -6A but after going back and re reading his post I realized he must be writeing tongue in cheek because the -6 is just as easy to land and takeoff as the -6A. Most people tend to over control the rudder inputs at first on a -6 but as soon as you get the feel of it there is no more rudder input required than there is -6A to keep going straight down the runway. I don't care if you are flying a nose dragger or tail dragger you should not stop flying the airplane until the engine is stopped. I learned to fly in a tail dragger and soloed in 6 hrs and having instructed for the last 20 years specilizing in tail draggers have taught several Cessna types to fly their RV's in ten hours or less. The -6 is a pussycat so if you want a -6 do not let the fear of not being able to handle it stop you from building one, and yes the -6 is sexier thank you very much.:-) Now having said all that, build what you really want and well feel comfortable with knowing your own piloting skills. Nose wheel airplanes crash just as easy on landings and takeoffs as tail draggers so just be carefull. I have landed my RV-6 in 24 knot 90 degree crosswind, it was not comfortable but I feel it was just as safe as it would be in a trigear airplane. Happy building and flying Jerry -- Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR jsflyrv(at)ix.netcom.com ________________________________________________________________________________
Date: May 30, 1997
From: Elon <elon.o(at)worldnet.att.net>
Subject: Re: RPM limiters
--> RV-List message posted by: Elon kevin lane wrote: > I received a Jeg's car racing parts catalog today and noticed they sell rpm > limit modules. Does something similar exist for aircraft? (snip) ----------------------------------- Kevin: Most of the rev limiters I know work in conjunction with the same brand electronic ignition system i.e., MSD, Acell, Mallory and they don't work with aircraft mags. However, I'm sure the electronic ignition folks could find a way to adapt it. But why? It will limit the RPM but it can't stop overspeed. By that I mean if you are decelerating in a race car and accidently downshift to a lower gear you will overspeed the engine. In your airplane, if you don't pull back enough on the throttle you will still overspeed. Esentially, you will be windmilling the engine and the prop will be driving the engine to overspeed. With or without the rev limiter you will still have to pay careful attention to the throttle setting. Limiters work if NO EXTERNAL FORCE is applied to the engine. If you are decelerating in a car or windmilling in a plane both forces are driving the engine toward overspeed and the limiter cannot cancel the effect. Nice idea, but you just can't beat that constant $peed prop! Elon ps. Now a "compression release" or a "jake" brake may be another story :-). ________________________________________________________________________________
Date: May 30, 1997
From: "Robert G. Miller, Jr." <rgmiller(at)sprintmail.com>
Subject: Re: FAA finds several design omissions
--> RV-List message posted by: "Robert G. Miller, Jr." aol.com!Bumflyer(at)matronics.com wrote: > > > Second, I just had my RV-6A inspected by the real FAA. It was three weeks > ago and his name was David Soucie, from the Maintenance division of the > Denver FSDO. It was a two and a half hour ordeal where he checked everything > I could imagine. I hope my inspector is as good as yours was. A few months back I mentioned in a post on a totally different topic that a friend of mine (an airline capt. with 9000 hours and a professional air show pilot) was killed because the Russian manufacturer of his brand new fancy aerobatic plane neglected to install a one cent cottar pin in the nut that held the elevator push rod to the bell crank. It is rather sobering to think that something so small and inexpensive could cause such tragic results. Robert Miller ________________________________________________________________________________
Date: May 30, 1997
From: KOZINSKI GARY <kozinski(at)symbol.com>
Subject: Re: EGT probes
--> RV-List message posted by: KOZINSKI GARY Bob, drill a hole about 6 inches down on the #3 output. This is what I was told to do by a Lycoming rep. on my 172 with an 0-320. Gary K 20038 ________________________________________________________________________________
From: John Walsh <jwalsh(at)ftp.com>
Subject: RV-6 vs RV-6A
Date: May 30, 1997
--> RV-List message posted by: John Walsh >>Reply to your message of 5/30/97 4:16 AM >>--> RV-List message posted by: Jerry Springer >> >>Well I started to write a long response to Jim Cones view of -6 vs -6A =09 FWIW, AOPA has an article on their web page about taildraggers and takeoff= /landing accidents. They found that the overall number of accidents is only slightly higher for= taildraggers. They suggested that most of this may be due to the fact th= at most taildraggers are MUCH older than their nosegear counterparts and su= bject to more mechanical problems. If you want to read it, you're on you= r own.=20 I don't recall exactly where it is. =20 John =09 ________________________________________________________________________________
Subject: Re: Experimental Maintenence
49-51,53,55,57,59-62,64-65,67,69-70,72,74-75,77,79-80,82,84,86,88-92
From: wstucklen1(at)juno.com (Frederic W Stucklen)
Date: May 30, 1997
--> RV-List message posted by: wstucklen1(at)juno.com (Frederic W Stucklen) Ryan, I agree with your findings as I've also searched the FAR's for the same answers. I finally resorted to getting advice from several FAA FSDO personal. I say several, because, as we all know, each and every one of them has their own interpretations of the FAR's. Getting the opinion of several, spread out over the country, has lead me to believe that if we, as repairman certificated individuals for our own planes, approach maintainable issues the same way as an A&E or IA does on a certified aircraft, the FAA will be satisfied. This also includes the record keeping process and the use of certified parts where ever possible. Using this approach, and having a good working relationship with the local FAA personnel, seems to be working for me. I personally won't let this limit me from utilizing the "experimental" nature of our aircraft. This degree of freedom from the FAR's certainly opens up the realm of improvement over the 1930's level technologies to which certified aircraft are limited. But if we are to retain that freedom, we must ALL work towards the zero accident level goal of the FAA. This means that everything from basic workmanship standards, to innovative implementations of new technologies, to the standard and necessary implementations of basic systems, must be approached from the standpoint of the best life and overall reliability that is possible. With "experimental" aircraft being built predominately by persons whom are still learning the processes involved, it's also important that the experimental community work together to educate those involved. This list, the EAA, and others certainly work in those directions. At it's present rate of growth, "experimental" aircraft could soon become the predominate type flying. With that growth will come greater scrutiny and more regulation. Our future success may lay in the fact that we are able to regulate ourselves. writes: >-> RV-List message posted by: RV4131rb(at)aol.com > >Fred, > This is becoming a very interesting subject. Just being a pilot provides you >with the authority to perform preventive maintenance, or does it? Prevntetive >maintenance is part of Part 43 we are excluded from part 43 with the >exception of 43D (used for condition inspections). > I have gone through pages and pages of FAR's over the last couple of weeks >trying to determine legaly what we can or cannot do. The truth is there is >nothing I can find that says we can or we cannot work on our own aircraft. > They have put the responsobility in our laps and given us no guidelines to >follow. >Part 91.163 >(a) The owner or operator of an aircraft is primarily responsible for >maintaining that aircraft in an airworthy condition, including compliance >with Part 39 of this chapter. >(b) No person may perform maintenance, preventive maintenance, or alterations >on an aircraft other than as prescribed in this subpart and other applicable >regulations , including Part 43. > Here we are again part 43, we are excluded does this also mean we cannot do >preventive maintenance on experimentals? preventive maintenance all falls >under part 43. > You are also correct on inspections 91.169 subpart (c) excludes us again >from 100hr inspections and annual inspections and I see nothing aboutcondition inspections. > I know Ive read most of the information I use as my guideline from the >advisory circulars. I dont believe the advisory circulars are legaly binding, >however they offer us a good source of information to work from. I personally >maintain my airplane as if it were a (spam can) for my own safety as well as >whoever I might be taking along. would anyone else like to take a crack at >this? Its not so easy! > Ryan > > ________________________________________________________________________________
From: Bumflyer(at)aol.com
Date: May 30, 1997
Subject: Re: Pitot-Static Tube Alternatives
--> RV-List message posted by: Bumflyer(at)aol.com Van has done a bit of writing on the subject which I can't recall where or when but I remember the bottom line which is he has put his in the right place for accuracy. Forward of the airplane is best BUT it must be a lot further than the example you cite. IE more like two or three feet. ________________________________________________________________________________
From: Cafgef(at)aol.com
Date: May 30, 1997
Subject: Re:6 VS 6A
--> RV-List message posted by: Cafgef(at)aol.com << I you are making the choice based on Center of Gravity (or baggage capacity), forget it. They are both the same. >> No one has mentioned this so far so here's my .02 The thrill of the tail dragger has to do with the location of the CG in relationship to the brakes. The CG has to be situated between the three wheels so that the airplane will sit in a stable position. RV-6A has CG in front of brakes (main wheels). That is leading the brakes. RV-6 has CG following the brakes. When you put on the brakes, the CG wants to be if front of the drag. If you have a tail tragger, then there is a turning moment because the CG wants to get into the place it really wants to be. That is in front. Stomp the brakes hard in a tail dragger and the tail will sure want to get in front if there is any unbalance at all. Gene Cafgef(at)aol.com with a 6A so I can get the thrill of flying and not so much thrill in landing. ________________________________________________________________________________
Date: May 30, 1997
From: jnl96(at)hcnews.com (Jim & Linda Hyde)
--> RV-List message posted by: jnl96(at)hcnews.com (Jim & Linda Hyde) subscribe ________________________________________________________________________________
From: Bumflyer(at)aol.com
Date: May 30, 1997
Subject: Re: Kit Shipping Charges - Financial Perspective
--> RV-List message posted by: Bumflyer(at)aol.com Having been a Van's customer for over five years, I realize the list newcomers are indeed discovering why there are so many of us enthusiastic customers, even with the myriad of gripes about customer support etc. First and I think foremost, is the sub kit approach. It is a great way to go. It is cheaper for 95% of us who are going to take a few years to complete. This approach always instilled a confidence in my mind that Van intended to be around for a long time, supporting his customers, and not after the quick buck. His advertising budget is also miniscule, and he obviously isn't paying those folks who answer the phones the big bucks to give Public Relations answers. No they are builders who can answer your questions on building. He hasn't had slick instructions and plans because they cost a lot of dough and might encourage folks to build without studying them which Van would find distasteful. These things are all related. We get weird answers on the phone sometimes but we get about three times the value in the kits and we get incredible customer support where it counts- The very best airplane on the market, at a low cost which is totally supported with spare parts and follow on engineering. These are my own opinions and definitely biased. I welcome any debate. I don't work for Van's or anyone else. ________________________________________________________________________________
Subject: Elevator skins
Date: May 30, 1997
From: Paul and Janet Lein <37xjglj(at)cmuvm.csv.cmich.edu>
--> RV-List message posted by: Paul and Janet Lein <37xjglj(at)cmuvm.csv.cmich.edu> While installing my elevator control stops, I got to thinking about the thread that runs occasionally about oil canning and cracking in elevators with .016 skins. The elevators on my particular airplane were built by a previous owner, but a look inside the elevator skin with a flashlight shows there's no RTV, etc. (This kit has had more homes than little orphan annie.) I did an archive search and could not get any conclusive answers about the advisability of injecting RTV or some other sealant foam into the existing elevators. Do any of you RV-listers have any advice? Paul Lein RV 6A - IO-360 and AD prop on order ________________________________________________________________________________
Date: May 30, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Transponder/encoder re-certification
--> RV-List message posted by: Bob Skinner Sorry to bother the whole list with this question. Can any Colo. RVers recommend an avionics shop where I can get my transponder/encoder re-certified? I live in Lexington, Nebraska (south central) so eastern Colo or Wyoming or western South Dakota would be fine. I could go to Lincoln or Omaha, NE but they charge "biz jet" rates and I think they prefer not to deal with us little guys. Mine was certified June 21, 1995. Does the certification expire on the 21st or the end of June? Please respond off-list. Thanks, Bob Skinner RV-6 BSkinner(at)navix.net ________________________________________________________________________________
Subject: Nosewheel/Tailwheel
From: ron.taborek(at)flight642.com (RON TABOREK)
Date: May 30, 1997
--> RV-List message posted by: ron.taborek(at)flight642.com (RON TABOREK) I've enjoyed the nosewheel/tailwheel discussion since I got my licence on Champs, flew nosewheel aircraft ever since, and am about to get some supercub time as a prelude to flying my RV-4. My appreciation is that while the tailwheel requires more skill those skills are well within the capabilities of pilots. One of the best descriptions of exactly what those skills are, I believe, is contained in an article in Sport Aviation of April 1992, page 35, entitled " Taming The Taildragger Pilot." I recommend it highly. Essentially it describes why and how to use the rudder to control an unstable system which has a tendency to overswing. it recommends catching any deviation as early as possible and using brief rudder taps to stop, reverse and restore any deviation. The author, Davisson, describes it much better than I do! For me he took away the mystery of tailwheel aircraft being difficult and replaced it with a good description of what you do to control something like this. ron.taborek @flight642.com RV-4 Installing O-320 Toronto ________________________________________________________________________________
Date: May 30, 1997
From: "Robert L. Nuckolls, III" <RNuckolls(at)compuserve.com>
Subject: Transponder/encoder re-certification
--> RV-List message posted by: "Robert L. Nuckolls, III" Bob, Why don't you bring it down to Wichita? We've got about a half dozen shops in the area that can handle it. = Bob. . . ________________________________________________________________________________
Date: May 30, 1997
From: Richard Bibb <rbibb(at)fore.com>
Subject: Re: Aeroflash Strobe Kits
--> RV-List message posted by: Richard Bibb I have the Aeroflash units installed on my -4 and they appear to work fine. THe reason I say appear is that I have not flown yet so I can't speak to reliability in an operational environment. RB >--> RV-List message posted by: Gusndale(at)aol.com > >Hi Everyone! > I've been lurking on the list for a few months now and really >appreciating the wealth of expertise and experience here. I'm getting close >to finishing my wings (RV6A) now and have a question I hope you can help me >with. > I want to put nav/strobe/position lights on the wingtips with separate >power supplies at each wingtip. I know I can get a Whelen kit from Van's or >a lot of other sources for about $700. Here's the Question: Aeroflash has a >"double flash" Nav/strobe/position kit available through Frederick Custom >Airframe; Austin,Texas for about $400. This sounds like a deal, but I don't >know anything about the Aeroflash kit or Frederick Custom Airframe except >what was on a one page flyer I picked up at a builder's group meeting. Does >anyone have enough experience with Aeroflash kits (reliability,completeness >of kit, etc.) to offer an opinion whether the Aeroflash unit is good or if I >should just spend the money and go with Whelen? Also does anyone have >experience with Frederick Custom Airframe? > Thanks in advance to all who respond. > > >Dale Wotring >Vancouver, WA >RV6A finishing up the wings > > Richard E. Bibb Direct: 301-571-2507 Vice President, Federal Operations Main: 301-564-4404 Fore Systems Federal, Inc. FAX: 301-564-4408 6905 Rockledge Drive, #800 Pager: 800-719-1246 Bethesda, MD 20817 www.fore.com ________________________________________________________________________________
From: dralle(at)matronics.com (Matt Dralle 510-606-1001)
Date: May 30, 1997
Subject: Re: Transponder/encoder re-certification
--> RV-List message posted by: dralle(at)matronics.com (Matt Dralle 510-606-1001) >-------------- >--> RV-List message posted by: "Robert L. Nuckolls, III" > >Bob, > >Why don't you bring it down to Wichita? We've got about >a half dozen shops in the area that can handle it. = > > >Bob. . . >-------------- Did those of you having problems receiving messages from Bob Nuckolls without any data receive the above message alright? It came across fine to my non-matronics account. Please reply directly to me at "dralle(at)matronics.com" and not to the List. Thanks! Matt Dralle RV-List Admin. -- Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94551 510-606-1001 Voice | 510-606-6281 FAX | dralle(at)matronics.com Email http://www.matronics.com/ W.W.W. | Featuring Products For Aircraft ________________________________________________________________________________
Date: May 30, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: Re: Accomodating Instrument Placement by cutting F-6107
--> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) Hi, Depth of a beam gives it it's strength. If I remember right - check up on me and no lawsuits! The strength of a beam is: W * D * D * D where W is width and D is depth. Width times depth cubed! You propose to reduce depth dramatically. Maybe you could make and fit another part - call it F-6107a. Fit it to be as big as F-6107 but move it to one side, between instruments. Or, make a F-6107 from 4130 which is maybe 3 times as stiff as the original and make it thicker. I've wondered if it wouldn't be a good idea to run a "post" from the aft end of F-6107, down the panel and then down behind the console to the floor. The panel is pretty sturdy stuff but considering that 40 pounds of panel and avionics becomes 360 pounds at 9G... I'd hate to have it fall out in my lap during a maximum G manuver. Hal Kempthorne RV-6AQ -- Installing canopy frame halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
Date: May 30, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: Re:Elevator skins
--> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) Apparently to prevent possible future oil-canning, Paul asked : > I did an archive search and could not get any conclusive > answers about the advisability of injecting RTV or some other sealant > foam into the existing elevators. Do any of you RV-listers have any > advice? > There is the old mechanic's maxim, "If it ain't broke, don't fix it." Hal Kempthorne RV-6AQ -- Installing canopy frame halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: May 30, 1997
Subject: Re: Transponder/encoder re-certification
--> RV-List message posted by: RV4131rb(at)aol.com Bob, There is a shop at Downtown Fort Collins airport that does excellent work . This job will run you around 50 bucks. Unfortunatly I cant remember the buisnesses name. There is another good shop at Centenial airport named Mastcom this is run by a father daughter teem and they do nice work at a very fair price. Mastcom 7395 S Peoria Englewood Co. 303-799-6289 ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: May 30, 1997
Subject: Re: Experimental Maintenence
--> RV-List message posted by: RV4131rb(at)aol.com Fred, My hats off to you!!! And I agree with you 100% Ryan ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: Re: Elevator skins
Date: May 30, 1997
--> RV-List message posted by: "Dennis Persyk" ---------- > From: Paul and Janet Lein <cmuvm.csv.cmich.edu!37xjglj(at)matronics.com> > To: rv-list(at)matronics.com > Subject: RV-List: Elevator skins > Date: Thursday, May 29, 1997 11:53 PM > > --> RV-List message posted by: Paul and Janet Lein <37xjglj(at)cmuvm.csv.cmich.edu> > > While installing my elevator control stops, I got to thinking about the > thread that runs occasionally about oil canning and cracking in elevators > with .016 skins. The elevators on my particular airplane were built by a > previous owner, but a look inside the elevator skin with a flashlight > shows there's no RTV, etc. (This kit has had more homes than little > orphan annie.) I did an archive search and could not get any conclusive > answers about the advisability of injecting RTV or some other sealant > foam into the existing elevators. Do any of you RV-listers have any > advice? > Paul Lein > RV 6A - IO-360 and AD prop on order Paul, The RTVs which have sufficient durometer value ("hardness") to do any good are generally pretty viscous. You would need a low-viscosity RTV that was "runny" enough to flow into the trailing edge cavity. I work with several RTVs and gels in my profession, so I have access to quite a few, but none currently are of the type you need. The RTV should also be a "neutral cure" variety that cures without releasing acetic acid, another limiting requirement. If you try and inject the RTV in from the ends you will only secure the end-most few inches. I wouldn't worry about it. There are lots of RVs flying with 0.016 elevators, no RTV and no cracks. Dennis 6A fuselage in jig ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: May 30, 1997
Subject: Re: Accomodating Instrument Placement
--> RV-List message posted by: RV6junkie(at)aol.com << It seems to me that F-6107 thus modified would still be strong enough to support the instrument panel and glare shield, especially in view of the notched angle piece that's riveted to the entire underside of the glareshield right behind the instrument panel. Any comments on my idea?>> I did the same thing as you have described. Make the notch as small as necessary but leave enough clearance for vibration (3/4" or so). <> Standard Instrument-screw holes. Gary Corde RV-6 N211GC - NJ ________________________________________________________________________________
From: kevin lane <n3773(at)worldnet.att.net>
Subject: two RV6A's, one T hanger
Date: May 30, 1997
--> RV-List message posted by: kevin lane we are currently figuring out how to best store two RV6A's in a 40' x 40' T hanger. A dolly which allows the planes to be rolled in sideways so the props are facing one another seems most pratical. This way the engines are readily accessible, not tucked up against the wall. Has anyone designed a dolly that works? I was thinking it would need only two wheels, like the lumber carts at Bld Sqr., and the wings could be used to steer it in. Maybe a lever could lower the bed to ground level to ease loading the plane. Our other idea was a ramp and raised platform with overlapping wings. This would require a 18" high platform and winch to pull the plane up, which conjures images of winching a wing thru a door or something equally disasterous. A solution is worth $210/mo.( One folding wing, that's all I need, the ultimate for that Navy paint scheme). kevin ________________________________________________________________________________
From: "David Moore" <dmoore8(at)tuelectric.com>
Subject: Re:Elevator skins
Date: May 30, 1997
--> RV-List message posted by: "David Moore" > --> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) > > Apparently to prevent possible future oil-canning, Paul asked : > > > I did an archive search and could not get any conclusive > > answers about the advisability of injecting RTV or some other sealant > > foam into the existing elevators. Do any of you RV-listers have any > > advice? > > I would advise against it for three reasons: - additional weight - would have to mass balance (more lead or switch to uranium) - unless environmentally sealed, it could trap moisture against the skin, and that means corrosion. ________________________________________________________________________________
From: Mlfred(at)aol.com
Date: May 30, 1997
Subject: Re: Aeroflash Strobe Kits/Frederick Custom Airframe
--> RV-List message posted by: Mlfred(at)aol.com << I want to put nav/strobe/position lights on the wingtips with separate power supplies at each wingtip. I know I can get a Whelen kit from Van's or a lot of other sources for about $700. Here's the Question: Aeroflash has a "double flash" Nav/strobe/position kit available through Frederick Custom Airframe; Austin,Texas for about $400. This sounds like a deal, but I don't know anything about the Aeroflash kit or Frederick Custom Airframe except what was on a one page flyer I picked up at a builder's group meeting. Does anyone have enough experience with Aeroflash kits (reliability,completeness of kit, etc.) to offer an opinion whether the Aeroflash unit is good or if I should just spend the money and go with Whelen? Also does anyone have experience with Frederick Custom Airframe? Thanks in advance to all who respond. >> Well, I know the guy who runs the place. I usually see him in the mirror. I also know his wife.;-) She's VERY supportive. (Boy, that should get me some points!) The price is correct ($415 plus shipping), with a manufacturers 2 yr from date of purchase warranty. I have arranged with the manufacturer to put longer (18") leads on the strobe bulbs, so we can mount the power supplies no the front of the main spar, behind the Duckworks landing light cutouts (for serviceability). I'm sure those on the list who've purchased from me will attest to the arrival of the parts. I ask folks to send a check AFTER arrival of the units. I haven't been stiffed yet! Single flash is a bit cheaper, and I can also get the single unit (adapted wingtip unit) for the v stab for $155 (single flash) plus shipping. Let me know if I can help! Who posted the flyer? I need to thank this person. Check six! Mark Frederick mlfred(at)aol.com ________________________________________________________________________________
Date: May 30, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: paint scheme
--> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) Does anyone else have a military camouflage paint scheme on their rv? I am seriously considering one for a rv-4, but can't find any info on patterns and paint type. If anyone has info like this please e-mail me or give me a number where I can call you. Thanks, alot. MCL ________________________________________________________________________________
Date: May 30, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: insurance
--> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) I just got a quote from an insurance company (Falcon Ins. Comp. of Arizona) 20,000.00 hull coverage. $1019.00 per year. 500.00 earned since test hours not flown off yet. 100.00 deduct not in motion. 1,000,000.00 liability. Covered from first flight. My experience: commercial, single eng. land. no instrument rating. total time 1240 hrs. 300 of that in taildraggers. How does this coverage sound to others who have insurance? Is this a good price, or can it be beat by much? Tell me what you think. thanks. ________________________________________________________________________________
Date: May 30, 1997
From: Charlie Kuss <charliekuss(at)sprintmail.com>
Subject: [Fwd: Tools, tools and more tools]
--> RV-List message posted by: Charlie Kuss Date: Fri, 30 May 1997 13:26:35 -0400 From: Charlie Kuss <charliekuss(at)sprintmail.com> Subject: Tools, tools and more tools Hi everybody, Yah, it's me, the new kid again. I want to thank everyone who responded to my last question. I may give Sid a call if my local Cleco and CP distributers can't get the job done.(or done at an exorbitant price). FYI You can find your local Chicago Pneumatic distributer at: http://www.chicagopneumatic.com/itdl.html Cleco was a little tougher to find. I did some searching on Alta Vista's search engine and discovered they are now Industrial Energy Products Division of INTOOL Inc. http://www.i-trade.com/catalog/tpusa/00000090/airetool.htm I sent an email to them airetool(at)airetool.com and Larry Van Deusen larryvan(at)erinet.com answered the next day with the info on my local distributer. Both local distributers faxed me the parts list info within the hour. The parts are now ordered and I didn't even have to drive down to Miami 30 miles away. :-) Hell, I knew if I wasted enough time on my computer it would eventually save me a few seconds. Does anyone have any experience with Wick's spring back dimple dies? By the ad copy, I suspect they are the same as Avery's. Any experiences and/or opinions out there? Charlie Kuss Drooling and trying to separate the pages of all these tool catalogs. ________________________________________________________________________________
Date: May 30, 1997
From: Mark Ruddock <markr(at)iwl.net>
Subject: Re:Elevator skins
--> RV-List message posted by: Mark Ruddock Hal Kempthorne wrote: > > --> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) > > Apparently to prevent possible future oil-canning, Paul asked : > > > I did an archive search and could not get any conclusive > > answers about the advisability of injecting RTV or some other sealant > > foam into the existing elevators. Do any of you RV-listers have any > > advice? > > > There is the old mechanic's maxim, "If it ain't broke, don't fix it." > > Hal Kempthorne RV-6AQ -- Installing canopy frame > halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC I am very new to RVs but I felt it important to say that if you do decide to do anything to the control surfaces, make sure to aerodynamically balance them again. Regards, Mark Ruddock ________________________________________________________________________________
Date: May 30, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Re: Transponder/encoder re-certification
--> RV-List message posted by: Bob Skinner >--> RV-List message posted by: RV4131rb(at)aol.com > >Bob, > There is a shop at Downtown Fort Collins airport that does excellent work . >This job will run you around 50 bucks. Unfortunatly I cant remember the >buisnesses name. > There is another good shop at Centenial airport named Mastcom this is run by >a father daughter teem and they do nice work at a very fair price. >Mastcom >7395 S Peoria >Englewood Co. >303-799-6289 Thanks for the info. Bob ________________________________________________________________________________
From: "Union Hydraulics" <unionhyd(at)s140.aone.net.au>
Subject: unscribe
Date: May 31, 1997
--> RV-List message posted by: "Union Hydraulics" unscribe unionhyd(at)s140.aone.net.au ________________________________________________________________________________
Subject: Re: Wanted-Pneumatic Squeezer
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: May 30, 1997
--> RV-List message posted by: tcraig-stearman(at)juno.com (John T. Craig-Stearman) writes: > >Tom, > could you e-mail me the details on your "harbor freight" press >setup,I >like the cost alternative to the squeezers.thanks > >chris marion >RV-6 HS >cincy,OH > Chris, Harbor Freight sells an inexpensive (aoubt $20, I think) press arbor. It has a very heavy steel base, stout yoke, 1" square ram, and a handle to manually control the ram. I drilled a .401" hole in the steel base to accept standard cupped rivet sets. I set the spars with the 3/16" rivets shop-head-down, and braced the rest of the spar with wood blocks to keep it level. I drove the rivets by pounding the ram against the shop heads with a 3-lb short-handled sledge hammer, while applying constant pressure to the handle on the press arbor. I found that this method requires two guys: one to wield the hammer, and one to stabilize the rest of the spar. The rivets turned out beautifully. Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 preparing to mount wings ________________________________________________________________________________
Subject: Re: -6 vs -6A
<19970529.132734.18190.0.BStobbe(at)juno.com>
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: May 30, 1997
--> RV-List message posted by: tcraig-stearman(at)juno.com (John T. Craig-Stearman) >\-\-\> RV-List message posted by: bstobbe(at)juno.com (Bruce D Stobbe) > >Steve wrote: > >snip > >>As far as I can see, there's nothing that keeps the plane tracking >>straight, since the nosewheel doesn't provide any "sideways" >>resistance? I have seen some less than rigorous answers to this question and just can't resist responding :-). To answer the question, consider the layout of a taildragger and a trike relative to the center of gravity on each airplane. On the taildragger, the CG is behind the main wheels, while on the trike the CG is forward of the main wheels. Draw a diagram of the footprint of each airplane (at pavement level), showing the three wheels and the center of gravity. Now apply a side load to the main wheels of each airplane (as, for instance, when landing in a crab). For the taildragger, the resistance of the main wheels to scrubbing sideways applies a destabilizing force. That is, the side load on the main wheels will tend to increase the crab angle, increasing the side load still more. For the trike, the opposite is true. The resistance of the main wheels to scrubbing sideways applies a stabilizing force. That is, the side load on the main wheels will tend to decrease the crab angle, decreasing the side load. Now consider a second effect. Landing with any vertical velocity in the taildragger will tend to increase the airplane's angle of attack, usually just as the pilot applies aft elevator to correct his sink rate. The combined effect increases the tendency to bounce. Landing with a small vertical velocity in the trike will tend to decrease the airplane's angle of attack, which will decrease the tendency to bounce. These effects require the pilot to pay greater attention to detail when flying a taildragger, producing a better pilot. This discussion illuminates my greatest complaint about my six years teaching Air Force student pilots to fly the T-37. The Tweet is a trike, and hell-for-stout. The student could flare the thing twenty feet in the air and slam it into the runway in a thirty-degree crab. The ol' Tweet would absorb the impact without complaint and straighten itself out without any correction from the hyperventilating student, who then likely thought he made a decent landing! A taildragger would not tolerate such abuse, and would therefore teach the students to recognize crab angles and descent rates. Van has done a wonderful job addressing the usual complaints about a trike airplane (heavier, slower, less maneuverable than a comparable taildragger). Even so, I much prefer a taildragger for pure pleasure and for disciplining lazy pilot habits. And let us face the ugly truth: a taildragger is ALWAYS prettier than its nosewheel counterpart! (C-140 vs C-150, C-180 vs C-182, T-6 vs T-28, DC-3 vs DC-(6?), RV-6 vs RV-6A) Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 preparing to mount wings ________________________________________________________________________________
Date: May 30, 1997
From: mauser(at)claris.com (Richard Chandler)
Subject: Re: Transponder/encoder re-certification
--> RV-List message posted by: mauser(at)claris.com (Richard Chandler) > Did those of you having problems receiving messages from Bob > Nuckolls without any data receive the above message alright? It > came across fine to my non-matronics account. Please reply directly to > me at "dralle(at)matronics.com" and not to the List. Thanks! Since you made the change to --> in the from line, I have not had a single MIME-encoded message that I needed to open in literal mode. The change seems to have worked. -- Richard Chandler RV-6: Garage bought and being finished, saving for tools and tail kit. ________________________________________________________________________________
Date: May 30, 1997
From: mauser(at)claris.com (Richard Chandler)
Subject: Re: unscribe
--> RV-List message posted by: mauser(at)claris.com (Richard Chandler) > --> RV-List message posted by: "Union Hydraulics" --> RV-s140.aone.net.au> > > unscribe unionhyd(at)s140.aone.net.au Dang! These Aussies have a different word for everything! :-) -- Richard Chandler RV-6: Garage bought and being finished, saving for tools and tail kit. ________________________________________________________________________________
From: "ROY HARRILL" <KHarrill(at)worldnet.att.net>
Subject: Re: Pitot-Static Tube Alternatives
Date: May 30, 1997
--> RV-List message posted by: "ROY HARRILL" John, I have just gone through that decision process and identified at least two other alternatives: using a Piper pitot and using a Cessna pitot. Using a Cessna and the Gretz mount puts the pitot within the range specified on the plans; the Piper approach places the pitot opening aft and closer to the skin than the specs in the plans. Reports by builders who have used the Piper say it is accurate. Van's says they haven't tried it. After purchasing and fitting a Cessna pitot, I have decided to use a Piper because of the location on my tiedown rings. Hopes this helps! Ken Harrill RV - 6 wings PS I now have an extra pitot and mount (Cessna) available at a very attractive price to anyone who may be interested. ---------- > From: John B. Abell <ix.netcom.com!jbabell(at)matronics.com> > To: rv-list(at)matronics.com > Subject: RV-List: Pitot-Static Tube Alternatives > Date: Thursday, May 29, 1997 11:07 AM > > --> RV-List message posted by: "John B. Abell" > > I'm about ready to install a pitot-static tube and other components in > my wing. I intend to use my RV-6A primarily for cross country flying > including IFR. I've been considering two alternative heated > pitot-static tubes: (a) the AN5814, which is mounted under the wing and > is one of the pitot tubes for which Warren Gretz sells an installation > kit that looks like a good deal, and (b) the AN5816-1 Kollsman type. > The Kollsman tube is about 9.5 inches long and is intended to fasten to > what I think would be a 1 inch O.D. tube with four screws. There's a > picture of both types in the ACS catalog. The Kollsman is mounted so > that it projects straight forward of the wing leading edge. It seems to > me that the Kollsman tube has the better probability of sampling > undistrubed air than the under-wing type. > > I would greatly value the comments and opinions of RV-List members on > these two alternatives. Observed and validated airspeed data would be > especially helpful. > > Thanks. > > Jack Abell > RV-6A N333JA (Reserved) ________________________________________________________________________________
Date: May 30, 1997
From: Mike Flaherty <yogieb(at)pipeline.com>
Subject: Re: Elevator skins
--> RV-List message posted by: Mike Flaherty >--> RV-List message posted by: "Dennis Persyk" > > > >---------- >> From: Paul and Janet Lein <cmuvm.csv.cmich.edu!37xjglj(at)matronics.com> >> To: rv-list(at)matronics.com >> Subject: RV-List: Elevator skins >> Date: Thursday, May 29, 1997 11:53 PM >> >> --> RV-List message posted by: Paul and Janet Lein ><37xjglj(at)cmuvm.csv.cmich.edu> >> >> While installing my elevator control stops, I got to thinking about the >> thread that runs occasionally about oil canning and cracking in elevators > >> with .016 skins. The elevators on my particular airplane were built by a >> previous owner, but a look inside the elevator skin with a flashlight >> shows there's no RTV, etc. (This kit has had more homes than little >> orphan annie.) I did an archive search and could not get any conclusive >> answers about the advisability of injecting RTV or some other sealant >> foam into the existing elevators. Do any of you RV-listers have any >> advice? >> Paul Lein >> RV 6A - IO-360 and AD prop on order > >Paul, >The RTVs which have sufficient durometer value ("hardness") to do any good >are generally pretty viscous. You would need a low-viscosity RTV that was >"runny" enough to flow into the trailing edge cavity. I work with several >RTVs and gels in my profession, so I have access to quite a few, but none >currently are of the type you need. The RTV should also be a "neutral >cure" variety that cures without releasing acetic acid, another limiting >requirement. >If you try and inject the RTV in from the ends you will only secure the >end-most few inches. >I wouldn't worry about it. There are lots of RVs flying with 0.016 >elevators, no RTV and no cracks. >Dennis 6A fuselage in jig Paul, I hesitate to use any foam inside any control. Some early Cessna 206's had a foam material in the elevator trim tab. After some years, water would soak into the foam and cause corrosion. Cessna produced a new tab that had stiffeners riveted to the skin. > > ________________________________________________________________________________
Date: May 30, 1997
From: John Ammeter <ammeterj(at)seanet.com>
Subject: Re: two RV6A's, one T hanger
--> RV-List message posted by: John Ammeter I've got a 42' wide by 32' deep T hangar and, using a CAD program, decided that I couldn't fit two RV's in it. I'm assuming that you've got 20' from the front to the first wall and then 20' into the bottom of the T. Since the RV is over 20 feet long you'll have to overlap the noses. That will mean that one RV is closer to the door than the other. The Horizontal Stab is about 10 feet long so the centerline of the fuselage will be about 5 feet from the wall; this gives 15 feet left for the wing. Sounds good until you remember the other RV will be a fuselage width closer to the door. Forget the above. I just went into my CAD program and tried it out using RV-6's drawn to scale. It'll work but you will have very little extra room. Maybe it's worth the $210/month to you, especially if you don't fly much. I think you would have to use a dolly as you mentioned, however. John >--> RV-List message posted by: kevin lane > >we are currently figuring out how to best store two RV6A's in a 40' x 40' T >hanger. A dolly which allows the planes to be rolled in sideways so the >props are facing one another seems most pratical. This way the engines are >readily accessible, not tucked up against the wall. Has anyone designed a >dolly that works? I was thinking it would need only two wheels, like the >lumber carts at Bld Sqr., and the wings could be used to steer it in. Maybe >a lever could lower the bed to ground level to ease loading the plane. Our >other idea was a ramp and raised platform with overlapping wings. This >would require a 18" high platform and winch to pull the plane up, which >conjures images of winching a wing thru a door or something equally >disasterous. A solution is worth $210/mo.( One folding wing, that's all I >need, the ultimate for that Navy paint scheme). kevin > > > John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA 206-525-5445 RV-6 N16JA First flight August 1990 ________________________________________________________________________________
Date: May 30, 1997
From: John Ammeter <ammeterj(at)seanet.com>
Subject: Re: insurance
--> RV-List message posted by: John Ammeter Just a couple of thoughts. Would you sell me your RV for $20,000? That's what you're offering to the insurance company. It sounds high to me but then I don't have hull coverage. I think my liability only cost around $400/year and I'm a 260 hour SEL pilot with about 190 hours in TD's. I'd check with AVEMCO and definately get more hull coverage if I had to have that coverage. John >--> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) > >I just got a quote from an insurance company (Falcon Ins. Comp. of >Arizona) 20,000.00 hull coverage. $1019.00 per year. 500.00 earned >since test hours not flown off yet. 100.00 deduct not in motion. >1,000,000.00 liability. Covered from first flight. My experience: >commercial, single eng. land. no instrument rating. total time 1240 >hrs. 300 of that in taildraggers. How does this coverage sound to >others who have insurance? Is this a good price, or can it be beat by >much? Tell me what you think. thanks. > > John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA 206-525-5445 RV-6 N16JA First flight August 1990 ________________________________________________________________________________
Date: May 30, 1997
From: Al Mojzisik <prober(at)iwaynet.net>
Subject: Re: paint scheme
--> RV-List message posted by: Al Mojzisik >--> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) > >Does anyone else have a military camouflage paint scheme on their rv? I >am seriously considering one for a rv-4, but can't find any info on >patterns and paint type. If anyone has info like this please e-mail me >or give me a number where I can call you. Thanks, alot. MCL > Michael, I have a gallon of Mil-Spec Olive Drab paint. Let me know if you need it. Al ________________________________________________________________________________
Date: May 30, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: Elevator skins
--> RV-List message posted by: John Darby <johnd@our-town.com> Paul; Sometime back, The RVator had some info regarding this. Seems to me it was more prevalent in those that had the 360s in them. There was discussion about not 'stopping up' the drain ability of the elev etc. and then there was some discussion about using a tube on some of the RTV applicators to get the stuff back to where you wanted it. You may want to check back issues of the RVator on this, around 93 or so. > about the>thread that runs occasionally about oil canning and cracking in elevators >with .016 skins. could not get any conclusive >answers about the advisability of injecting RTV or some other sealant >foam into the existing elevators. Do any of you RV-listers have any >advice? >Paul Lein >RV 6A - IO-360 and AD prop on order > John Darby RV6 N61764 flying Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: May 30, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: Sensenich props, et al...
--> RV-List message posted by: John Darby <johnd@our-town.com> Al; If you read what Sens. put out, they don't differentiate between what kinds of over speed it is, just a 'never exceed' rpm. You may well be correct in your understanding of it, but at no time have I seen any such supported by Sens. And yet, they make no such caveat for the acrobatic limit as well on their paper work, but as you may have seen on their homepage, they immediately adjacent mention that you would probably exceed the rpm in a dive. This gives rise to my belief that their assumption that the pilots inability (?) to control the rpm is the reason they limit the acro. approval of the prop. >Isn't the concern for overspeeding in a "power applied" condition and not a >"windmilling" situation? I thought the power pulses are what set up the >prop harmonic that may lead to destruction. (Shuddering all over at the >thought) > >Al > John Darby RV6 N61764 flying Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: May 30, 1997
From: "Louis E. Smith Jr." <lsmith(at)coastalnet.com>
Subject: Re: Aeroflash Strobe Kits/Frederick Custom Airframe
--> RV-List message posted by: "Louis E. Smith Jr." >--> RV-List message posted by: Mlfred(at)aol.com > > ><< I want to put nav/strobe/position lights on the wingtips with separate > power supplies at each wingtip. I know I can get a Whelen kit from Van's or > a lot of other sources for about $700. Here's the Question: Aeroflash has >a > "double flash" Nav/strobe/position kit available through Frederick Custom > Airframe; Austin,Texas for about $400. This sounds like a deal, but I don't > know anything about the Aeroflash kit or Frederick Custom Airframe except > what was on a one page flyer I picked up at a builder's group meeting. Does > anyone have enough experience with Aeroflash kits (reliability,completeness > of kit, etc.) to offer an opinion whether the Aeroflash unit is good or if I > should just spend the money and go with Whelen? Also does anyone have > experience with Frederick Custom Airframe? > Thanks in advance to all who respond. >> > I purchased the Aeroflash kit for my RV-8 from Frederick Custom Airframe. The units are very similar to the Whelen ones. I would say that the average person probably could not tell the installed units apart. The kits are complete. Don't hesitate to do business with Mark Frederick. I met him at Oshkosh 96 and have since been out to Ausin, TX on a business trip and stopped by for a visit at Frederick Custom Airframe. Mark is a great guy to do business with. Regards, Louis Smith lsmith(at)coastalnet.com Rocky Mount, NC RV-8 #80126 N801RV reserved RV-4 #2844 N102LS sold ________________________________________________________________________________
Date: May 30, 1997
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: [Fwd: Tools, tools and more tools]
--> RV-List message posted by: "r.acker" >Does anyone have any experience with Wick's spring back dimple dies? By >the ad copy, I suspect they are the same as Avery's. Any experiences >and/or opinions out there? I've bought lots of stuff from Avery's and its all good. However, when I broke my 3/32" dimple dies (my fault...very tight corner on thick skins) I replaced them with a pair from Cleaveland. The Cleaveland dies are definitely worth the extra money...polished to a mirror finish and I do get better dimples. Also, their edge rolling tool is much better. If anyone wants an Avery one let me know. Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
Date: May 30, 1997
From: Don Mack <donmack(at)flash.net>
Subject: Updated web site
--> RV-List message posted by: Don Mack I have added emp. & wing pictures to my web page. Thanks to Matt D. for letting me "borrow" one of Matronics pics. Don Mack donmack(at)flash.net http://www.flash.net/~donmack/ ________________________________________________________________________________
Subject: Re: Sensenich props, et al...
From: ebundy(at)juno.com (Ed Bundy)
Date: May 30, 1997
--> RV-List message posted by: ebundy(at)juno.com (Ed Bundy) >Ed, >Isn't the concern for overspeeding in a "power applied" condition and >not a windmilling" situation? I thought the power pulses are what set up >the prop harmonic that may lead to destruction. (Shuddering all over at Al, I don't know where the nodes actually come in, and I don't really want to find out. :-) Although, you can't really get there in a windmilling situation. To hit 2600 you have to have a LOT of power in, and be in a pretty good descent. I can't get that RPM in level flight with full power at 3000'. Ed Bundy RV6A - first flight 11/20/96 ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
From: RV6Russ(at)aol.com
Date: May 30, 1997
Subject: Re: Vapor Lock
--> RV-List message posted by: RV6Russ(at)aol.com I installed a vapor return line using the .030 orifice. Tee off next to the carburetor and run the return line back to at least upstream of the elec boost pump.(would be better to go all the way back to a tank - but its a big plumbing job). I also have a fuel flow meter and so I installed a shut-off valve down behind my heels so I can shut it off when I don't need or want it open. This system is widely used and works well. Good luck - RV6Russ ________________________________________________________________________________
Date: May 31, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: Re:Elevator skins
--> RV-List message posted by: "les williams" I don't have the dates of the RVators that this subject was discussed, but it was. I believe that it was suggested to insert some non-corrosive RTV (like Permatex Ultra Blue) at the trailing edge at the end of each stiffener pair, if this becomes a problem. Access would be by drilling a small hole. Not all planes have experienced this. My first RV-6A had two small cracks start at the trailing edge of the rudder. I was running an 0-320 with wood prop. After I sold it, a metal prop was installed, and I understand that the skin has now cracked at the last rivet on every rudder stiffener. I don't know if this is from an unbalanced prop or from the added vibration transmission of a metal prop, or? Bottom line is, I don't think I would worry about it now, but would keep a real close eye out for any crack developing and then take measures to stop and prevent any more. Les Williams/RV-6AQB/N24LW (res)/finish kit ---------- From: owner-rv-list(at)matronics.com on behalf of David Moore Sent: Friday, May 30, 1997 1:05 PM Subject: Re: RV-List: Re:Elevator skins --> RV-List message posted by: "David Moore" > --> RV-List message posted by: halk(at)sybase.com (Hal Kempthorne) > > Apparently to prevent possible future oil-canning, Paul asked : > > > I did an archive search and could not get any conclusive > > answers about the advisability of injecting RTV or some other sealant > > foam into the existing elevators. Do any of you RV-listers have any > > advice? > > I would advise against it for three reasons: - additional weight - would have to mass balance (more lead or switch to uranium) - unless environmentally sealed, it could trap moisture against the skin, and that means corrosion. ________________________________________________________________________________
Date: May 30, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Re: insurance
--> RV-List message posted by: Bob Skinner >--> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) > >I just got a quote from an insurance company (Falcon Ins. Comp. of >Arizona) 20,000.00 hull coverage. $1019.00 per year. 500.00 earned >since test hours not flown off yet. 100.00 deduct not in motion. >1,000,000.00 liability. Covered from first flight. My experience: >commercial, single eng. land. no instrument rating. total time 1240 >hrs. 300 of that in taildraggers. How does this coverage sound to >others who have insurance? Is this a good price, or can it be beat by >much? Tell me what you think. thanks. Michael, I have my RV-6 insured with AUA, 800-727-3823. The premium is $880.00. Hull value is $35,000 and I have $500 deductable all risk basis, all risks basis not in flight and 100 deductable all risks not in motion. Single limit bodily injury and property damage including passengers of: $100,000 each passenger; $1,000,000 each occurrence. Pilot data: 49 years young, SEL, 1,102 tt, 287 in RV-6, 944 tailwheel, 127 hrs last 12 months. Bob Skinner RV-6 BSkinner(at)navix.net ________________________________________________________________________________
Date: May 31, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: Re: -6 vs -6A
--> RV-List message posted by: "les williams" Putting aside all the reasons why taildraggers and nosewheel aircraft do this or that and getting back to the original question, I will tell you what I did. After ordering a 6A, most of my "macho" taildragger friends chided me into changing my order to a 6 and that's what I first received. But the closer I got to putting that extra bulkhead in, the more I struggled with that choice. Finally, I sat down and listed all the positive and negative points that I felt about each. After counting each and weighing them out in my mind, I "consciously" ended up with what my "unconscious" knew was right for me all along. I left out that extra bulkhead so that changing back would be most difficult. I finished building and then thoroughly enjoyed flying my -6A for 350 hrs and never regretted choosing that gear design. And, as you will see in my signature line, I'm doing it again. It' a tough decision for a lot of people, but whichever you chose, in the end, it will be the right one for you! Good luck. Les Williams/RV-6AQB/N24LW (res)/finish kit ---------- From: owner-rv-list(at)matronics.com on behalf of John T. Craig-Stearman Sent: Friday, May 30, 1997 3:15 PM Subject: RV-List: Re: -6 vs -6A --> RV-List message posted by: tcraig-stearman(at)juno.com (John T. Craig-Stearman) >\-\-\> RV-List message posted by: bstobbe(at)juno.com (Bruce D Stobbe) > >Steve wrote: > >snip > >>As far as I can see, there's nothing that keeps the plane tracking >>straight, since the nosewheel doesn't provide any "sideways" >>resistance? I have seen some less than rigorous answers to this question and just can't resist responding :-). To answer the question, consider the layout of a taildragger and a trike relative to the center of gravity on each airplane. On the taildragger, the CG is behind the main wheels, while on the trike the CG is forward of the main wheels. Draw a diagram of the footprint of each airplane (at pavement level), showing the three wheels and the center of gravity. Now apply a side load to the main wheels of each airplane (as, for instance, when landing in a crab). For the taildragger, the resistance of the main wheels to scrubbing sideways applies a destabilizing force. That is, the side load on the main wheels will tend to increase the crab angle, increasing the side load still more. For the trike, the opposite is true. The resistance of the main wheels to scrubbing sideways applies a stabilizing force. That is, the side load on the main wheels will tend to decrease the crab angle, decreasing the side load. Now consider a second effect. Landing with any vertical velocity in the taildragger will tend to increase the airplane's angle of attack, usually just as the pilot applies aft elevator to correct his sink rate. The combined effect increases the tendency to bounce. Landing with a small vertical velocity in the trike will tend to decrease the airplane's angle of attack, which will decrease the tendency to bounce. These effects require the pilot to pay greater attention to detail when flying a taildragger, producing a better pilot. This discussion illuminates my greatest complaint about my six years teaching Air Force student pilots to fly the T-37. The Tweet is a trike, and hell-for-stout. The student could flare the thing twenty feet in the air and slam it into the runway in a thirty-degree crab. The ol' Tweet would absorb the impact without complaint and straighten itself out without any correction from the hyperventilating student, who then likely thought he made a decent landing! A taildragger would not tolerate such abuse, and would therefore teach the students to recognize crab angles and descent rates. Van has done a wonderful job addressing the usual complaints about a trike airplane (heavier, slower, less maneuverable than a comparable taildragger). Even so, I much prefer a taildragger for pure pleasure and for disciplining lazy pilot habits. And let us face the ugly truth: a taildragger is ALWAYS prettier than its nosewheel counterpart! (C-140 vs C-150, C-180 vs C-182, T-6 vs T-28, DC-3 vs DC-(6?), RV-6 vs RV-6A) Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 preparing to mount wings ________________________________________________________________________________
Date: May 30, 1997
From: "Jerry H. Prado" <jerryprado(at)wa.net>
Subject: Re: paint scheme
--> RV-List message posted by: "Jerry H. Prado" Michael C. Lott wrote: > > --> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) > > Does anyone else have a military camouflage paint scheme on their rv? I > am seriously considering one for a rv-4, but can't find any info on > patterns and paint type. If anyone has info like this please e-mail me > or give me a number where I can call you. Thanks, alot. MCL Just visit your local serious hobby shop specializing in radio control planes. They will have all the infor and detail you need. Jerry Prado ________________________________________________________________________________
Date: May 30, 1997
From: "Larry D. Hoatson" <lhoatson(at)e2.empirenet.com>
Subject: Re: insurance
--> RV-List message posted by: "Larry D. Hoatson" Michael C. Lott wrote: > > --> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) > > I just got a quote from an insurance company (Falcon Ins. Comp. of > Arizona) 20,000.00 hull coverage. $1019.00 per year. 500.00 earned > since test hours not flown off yet. 100.00 deduct not in motion. > 1,000,000.00 liability. Covered from first flight. My experience: > commercial, single eng. land. no instrument rating. total time 1240 > hrs. 300 of that in taildraggers. How does this coverage sound to > others who have insurance? Is this a good price, or can it be beat by > much? Tell me what you think. thanks. Have you checked Avemco, with their EAA discount? I was VERY SURPRISED at how competetive they were on the Cessna 170A - I had zero taildragger time, and there was no surcharge for a spouse student pilot with zero hours period. Couldn't find any of the discount or 'free agents' that could touch the rates. They do a funny thing with the hours, and count the taildragger time double, which would make you a 1,540 hour pilot for insurance purposes - it worked for us! Love to know what else you come up with... Larry -- Larry D. Hoatson Yucaipa, CA Redlands (L12) Airport lhoatson(at)empirenet.com KC6WYF via packet at: KC6WYF(at)W6JBT.SOCAL.CA.USA.NOAM Restoring 1950 Cessna 170A N9948A... Looking forward to RV-6 ________________________________________________________________________________
Date: May 30, 1997
From: "Larry D. Hoatson" <lhoatson(at)e2.empirenet.com>
Subject: Rivet sets
--> RV-List message posted by: "Larry D. Hoatson" Hello, I've been putting together a list of tools, primarily based on the section in the preview plans from Van's for the RV-6/6A. There is a recommendation of a swiveling head flush rivet set. Does anyone use these, are there specific applications where they're necessary? Any feedback will be appreciated. We've just about made it through the total restoration of the Cessna, and never even knew they existed, let alone wish I had one. Also, what about single and/or double offset universal sets? Preferance, or are there places one cannot reach with one style or the other? Thanks in advance Larry -- Larry D. Hoatson Yucaipa, CA Redlands (L12) Airport lhoatson(at)empirenet.com KC6WYF via packet at: KC6WYF(at)W6JBT.SOCAL.CA.USA.NOAM Restoring 1950 Cessna 170A N9948A... Looking forward to RV-6 ________________________________________________________________________________
Date: May 30, 1997
From: "Larry D. Hoatson" <lhoatson(at)e2.empirenet.com>
Subject: Kit Shipping Charges
--> RV-List message posted by: "Larry D. Hoatson" Thanks to all those who responded! I appreciate the collective wisdom, and as usual, there were other factors involved that I didn't know to consider until I asked! One kit at a time seems most reasonable, I didn't realize the kits were upgraded as time goes by. Thanks again, Larry -- Larry D. Hoatson Yucaipa, CA Redlands (L12) Airport lhoatson(at)empirenet.com KC6WYF via packet at: KC6WYF(at)W6JBT.SOCAL.CA.USA.NOAM Restoring 1950 Cessna 170A N9948A... Looking forward to RV-6 ________________________________________________________________________________
From: bennett(at)healey.com.au
Date: May 31, 1997
Subject: Re: Elevator skins
--> RV-List message posted by: bennett(at)healey.com.au > --> RV-List message posted by: Paul and Janet Lein <37xjglj(at)cmuvm.csv.cmich.edu> I did an archive search and could not get any conclusive > answers about the advisability of injecting RTV or some other sealant > foam into the existing elevators. Do any of you RV-listers have any > advice? > Paul Lein > RV 6A - IO-360 and AD prop on order I understand it is standard now to put a plug of RTV at the aft end of each stiffener during construction. I built mine before Van made this change. I will find a way to do the same, although I have yet to figure how. I have seen a cracked elevator and it's not a pretty sight. There has been quite some discussion on the list about neutral vs normal cure RTV, and there were test results reported that indicated no problems with the acetic acid cure on aluminum. Peter Bennett Sydney Australia RV6 building sliding canopy ________________________________________________________________________________
From: bennett(at)healey.com.au
Date: May 31, 1997
Subject: Re: [Fwd: Tools, tools and more tools]
--> RV-List message posted by: bennett(at)healey.com.au The Cleaveland dies are > definitely worth the extra money...polished to a mirror finish and I do get > better dimples. > > Also, their edge rolling tool is much better. If anyone wants an Avery one > let me know. > > Rob Acker / r.acker(at)ix.netcom.com / RV-6Q > I found my edge rolling tool (two rollers on a tube) less use than pockets in underpants. The Avery one is better but it is a hair trigger touch difference between getting a turn down and getting a sharp crease along the edge. You can get a more aggressive roll without a sharp crease by radiussing the roller edges. Let your Scotchbrite wheel spin the roller as it grinds the radius. Peter Bennett Sydney Australia RV6 building sliding canopy ________________________________________________________________________________
Date: May 31, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: Rivet sets
--> RV-List message posted by: Denny Harjehausen (Snipped) >There is a recommendation of a swiveling head flush rivet set. Does >anyone use these, are there specific applications where they're >necessary? If you or who ever has a good sense of straight you won't need it. I like it cause some people that help don't always get the gun straight and put smilies in the thin skin (not me of course) so I always use it. >Also, what about single and/or double offset universal sets? I've used the single offset a couple of times, then I wished I would have had the double offset. But then I really needed it. So then....(?) >Larry D. Hoatson Yucaipa, CA Redlands (L12) Airport > >lhoatson(at)empirenet.com > >KC6WYF via packet at: KC6WYF(at)W6JBT.SOCAL.CA.USA.NOAM > >Restoring 1950 Cessna 170A N9948A... Looking forward to RV-6 > > > > Have A Great Day! Denny retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
From: JRoss10612(at)aol.com
Date: May 31, 1997
Subject: Re: Rivet sets
--> RV-List message posted by: JRoss10612(at)aol.com Larry, I purchased the swivel flush set before beginning construction. I pulled it out during my first riveting session with another experienced metalworker, he was surprised at the ease of use the tool. Excellent results were obtained with this set, myself driving the rivets, my friend bucking. He had completed his aircraft without a swivel flush set and was impressed with the results. In my opinion, the straight set is more difficult to use, although I'm sure that with care excellent results can be obtained. The swivel set makes the angle that the gun is held to the curved skins less critical, although it is still important to drive rivets with the gun held 90 degress to the rivet shank. Sure, you can do it with a regular straight set... but try holding things perfectly straight with the rivet gun at 1 AM after a hundred rivets or so. Much the same was experienced with the double offset. It is easier to control the set during driving as the double offset removes the eccentric loading from the rivet head. Simply put, the set is less likely to slip off the rivet head during driving. There are places on an RV (because of clearance) where you will require the use of the double offset, so consider it necessary. You may get away without one for a while, but you will eventually find just the place where you will wish you had it. In general, you will find more and more tools along the way that make things easier and can help you obtain better results more quickly. Such is the case with the pneumatic squeezer, pneumatic cleco tool, the many flush sets of different lengths and diameters, dimple die sets and a bunch or bucking bars. In building both wings, I found that the pneumatic cleco tool was invaluable in reducing/eleiminating RMI (repetitive motion injury), however I held off buying one for the longest time. By the way, I'm sure you've heard it before, but Avery and Cleveland are both first class tool sellers, deal with either one and you will not be sorry. Anyway, just my opinion. Hope that spelling cop on the list isn't lurking... Best of luck, Jon Ross RV-80094 - getting ready to complete fuel tanks, fuselage should be shipped in a week or so ________________________________________________________________________________
Date: May 31, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: -6 vs -6A
--> RV-List message posted by: "les williams" One more comment on this question. I've talked to several -6 builder/pilots who have said that they wish they had built a -6A, but I haven't talked to one single -6A builder/pilot that wishes they had built a 6. Les Williams/RV-6AQB/N24LW (res)/finish kit ________________________________________________________________________________
From: MikeT(at)aol.com
Date: May 31, 1997
Subject: Diagrams for Vision Instrumentation
--> RV-List message posted by: MikeT(at)aol.com A local Puget Sound builder is installing the full up Vision engine instrumentation system. I borrowed the install manual and made a set of wiring diagrams for him ( and maybe me). I have posted these to John Hovan's home page. They are titled 77-03/1 thru /6. Feel free to use them as needed. Mike Talley - just finishing drilling the lh tank - RV-6 ________________________________________________________________________________
From: Cafgef(at)aol.com
Date: May 31, 1997
Subject: Re: Sensenich props, et al...
--> RV-List message posted by: Cafgef(at)aol.com Does anyone know the failure mode of a sensenich prop? Just how does it fail and where? How does one go about preflighting the prop so that one can find the incipient failure before it progresses to the point of failure? I get nervous about all this talk of props failing, especially when I have one such prop on order. Gene Francis: cafgef(at)aol.com ________________________________________________________________________________
From: "craig" <craig(at)future.atlcom.net>
Subject: unsubscribe
Date: May 18, 1997
--> RV-List message posted by: "craig" unsubscribe ________________________________________________________________________________
From: "craig" <craig(at)future.atlcom.net>
Subject: RV-4 Kit For Sale
Date: May 18, 1997
--> RV-List message posted by: "craig" FOR SALE Empennage Kit (Vertical Skin Drilled up) (Horzional Skeleton assembled) , Wing Kit (Bannard Fast build kit in crate) (Phlogiston spar in Crate) and COMPLETE plans. I have approx. 8000.00 invested. Located in the Atlanta area. Make offer. Could deliver. craig(at)future.atlcom.net ________________________________________________________________________________
From: OrndorffG(at)aol.com
Date: May 31, 1997
Subject: Re: insurance
--> RV-List message posted by: OrndorffG(at)aol.com That sounds too high becki and I pay $1600 a year for both of us on our RV6A with $60,000 full coverage....George Orndorff ________________________________________________________________________________
Date: May 31, 1997
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: Rivet sets
--> RV-List message posted by: "r.acker" >>There is a recommendation of a swiveling head flush rivet set. Does >>anyone use these, are there specific applications where they're >>necessary? > > If you or who ever has a good sense of straight you won't need it. > I like it cause some people that help don't always get the gun straight > and put smilies in the thin skin (not me of course) so I always use it. The swivel rivet set is very useful in situations were you don't have a bucker to help you. I riveted most of my wing solo (I did get help for the last 2/3 of the top skin...it went oh so much faster that way!). I ran into situations where it was impossible to view the gun/surface relationship...with the swivel set I could put it somewhere near what I felt to be straight while my head and bucking bar were inside the wing. Pull the trigger, good rivet, no smileys. I normally don't recommend ATS, but they sell the same tool for cheaper as I found out walking from the Avery booth to theirs at sun'n'fun :( Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
From: JHeadric(at)aol.com
Date: May 31, 1997
Subject: Re: paint scheme
--> RV-List message posted by: JHeadric(at)aol.com Contact me and I will mail you some pix of my "P-51" RV5 paint scheme. Looked good! Jheadric ________________________________________________________________________________
Date: May 31, 1997
From: David Fitzgerald <theredbaron(at)earthlink.net>
Subject: Re: insurance
--> RV-List message posted by: David Fitzgerald Hello, I tried the Forrest agency and they quoted $1600/year with the $45,000 hull coverage - the rest was the same. I only have 180 hours tho' - 70 of which is in taildraggers. Let me know if you find other good quotes - I just started the kit so it will be a while before I decide. Talk Soon, Dave ----------------------------------------------------------------- RV-8 Builder Serial #80333 ----------------------------------------------------------------- ________________________________________________________________________________
Date: May 31, 1997
From: Michael McGee <jmpcrftr(at)teleport.com>
Subject: Re: Sensenich props, et al...
--> RV-List message posted by: Michael McGee >--> RV-List message posted by: Cafgef(at)aol.com > >Does anyone know the failure mode of a sensenich prop? Just how does it fail >and where? How does one go about preflighting the prop so that one can find >the incipient failure before it progresses to the point of failure? I get >nervous about all this talk of props failing, especially when I have one such >prop on order. >Gene Francis: cafgef(at)aol.com > Failures of props like we are talking about here are not a product of a pre flight condition--i.e., a crack or imperfection in the prop somewhere. Try this prop test demo: Find a yard stick (36" ruler) or just a thin piece of wood or metal that is 3 to 6 feet long. Hold it in the middle (just like your crankshaft holds onto your prop. Now twist your forearm/wrist/hand back and forth to swing the "propeller", slowly at first then gradually faster. As you twist back and forth--faster, faster, faster--you begin to see the stick in your hand (your prop) flex in the shape of as S. Even though it is spinning, this is what your prop looks like under a strobe light any time the engine is running. With a yard stick or a thin piece of wood you can twist it back and forth fast enough that the tips will stand still. This is what your prop is doing at those critical rpm's where the placard says AVOID CONTINUOUS OPERATION AT... Now with your test prop in your hand, twist it at that critical frequency (rpm) you just found and give it full throttle (twist harder at the same rate). You probably just broke your stick. That is what can happen if you run CONTINUOUSLY at those placarded rpm's. So, it is not a problem that existed pre-flight. This is a dynamic thing that is a product of a piston engine. It is not necessarily a design flaw any more than the red line on your airspeed indicator. It is one of those little compromises that come under the heading of design goals or mission profiles. One more thing, note that if you try two different length sticks you will get two different resonant frequencies. This is why you are not supposed to shorten your prop blades beyond the limits established by the manufacturer. They've already tried them shorter in a test cell and had a prop come apart. If you have a prop that you want to shorten the blades on look up the limits first. Mike McGee jmpcrftr(at)teleport.com ________________________________________________________________________________
Date: May 31, 1997
From: Tim Bronson <70773.2700(at)CompuServe.COM>
Subject: Engine acquisition
--> RV-List message posted by: Tim Bronson <70773.2700(at)CompuServe.COM> Hi Folks: Another new guy question: Since conventional wisdom has it that inactivity is not good for an engine, how do you who know feel about the idea of buying a freshly overhauled (or new) engine for a project that won't be completed for a few years? What is involved in storing an engine long term? What needs to be done to "un-store" it when the airplane is ready for it? Would this all be worth the trouble or would it be better to just buy the engine when it's needed (at the new, higher price)? Thanks. Tim Bronson, planning in Pittsburgh ________________________________________________________________________________
Date: May 31, 1997
From: Tim Bronson <70773.2700(at)CompuServe.COM>
Subject: 3rd Wheel
--> RV-List message posted by: Tim Bronson <70773.2700(at)CompuServe.COM> Hi Folks: The nose vs. tail dragger discussion has made for some interesting reading. I offer the following observations: If you are not real comfortable with your situation, the joy of flight will be greatly diminished. Many of us have completed flights successfully that certainly could not be described as "fun." If getting the taildragger back on the ground is something you worry about, this pleasure flying deal may not be so enjoyable. A few hours of dual instruction should help with the decision. The question you need to answer is not whether or not you CAN handle a taildragger, but rather, do you ENJOY flying a taildragger? Don't think you have to have "the right stuff" to check out in taildraggers. Remember, a few years back every student pilot started in a t/d. If a non-pilot can learn to fly one, someone who already has flight experience can certainly do it. I logged all of two hours of t/d time in my first ten years of flying, then I checked out in a J-3 in about an hour and a half. I am not Sky King either, I just went out with a good instructor on a nice day. I logged about ten hours in the J-3, then took another ten years "off" before returning to the tailwheel. Now my pleasure flying is exclusively taildragger, since that's what I have access to. I prefer it, but certainly would never turn my nose up at a tri-gear airplane. Once you've satisfied yourself that you are competent and confident in a tailwheel airplane, it becomes a matter of personal preference. You decide whether the additional challenge of the tailwheel is stimulating or aggravating. One other possible consideration is the question of redundancy. There are two ways to steer a -6A on the ground: rudder (with sufficient airflow) and differential brakes. The -6 offers both of those, plus tail wheel steering, which will allow you to taxi even if you lose one or both brakes (which has been known to happen). By the time I start my RV, I'll probably have a choice between the -8 and the -8A. No question in my mind; I'll stick with the straight 8. But the way I see it, either way you end up with an airplane that's custom made for you. You can't go too far wrong. Tim Bronson Pittsburgh, PA Future RV8 ________________________________________________________________________________
Date: May 31, 1997
From: Frank Smidler <smidler(at)dcwi.com>
Subject: Re: Accomodating Instrument Placement
--> RV-List message posted by: Frank Smidler Tim Lewis wrote: > In the RV-6A slider configuration there are 3 ribs that support the > glareshield and to which the instrument panel attaches. The three > pieces are 2 ea F-6107 and 1 ea F6108. > > Wouldn't you know it, these pieces interfere with my ideal location > of my flight instruments. These pieces are 1.5 - 2" high at the > instrument panel, but they get longer (more vertical extent) forward > of the instrument panel, so they sit right where the back end of > some of my instruments and radios should go. > I'm considering modfying F-6107 by cutting off some of the angled > portion and reinforcing it with some angle. > It seems to me that F-6107 thus modified would still be strong enough > to support the instrument panel and glare shield, especially in view > of the notched angle piece that's riveted to the entire > underside of the glareshield right behind the instrument panel. Any > comments on my idea? > I did just this very thing on the left rib so that I could center the 6 gauge flight cluster on the pilots position (9.75" offset from center of panel) and position them high enough so that I could put switches below. I don't see any structual problem with doing this if you reinforce the edge by riveting on an angle. Frank Smidler RV-6, working on instrument panel and canopy. ________________________________________________________________________________
From: hpair(at)thegrid.net
Date: May 31, 1997
Subject: RV4 or RV6 wing tips for sale
--> RV-List message posted by: hpair(at)thegrid.net I have a brand new set of wing tips for sale with nut plates already installed, so ya can take them off for maintenance. Ready to drill the holes in the wings. 1st $250.oo takes em . Harry Paine 805-481-2524 hpair(at)thegrid.net ________________________________________________________________________________
From: rvbildr(at)juno.com
Subject: V Stab Strobe fit
Date: May 31, 1997
--> RV-List message posted by: rvbildr(at)juno.com How does one install the Whelen strobe tube, p/n # A625, inside the vertical stab fairing on the RV-6? The base of the strobe tube is too wide to fit inside the fiberglas tip, unless it is installed diagonally. I've seen several fitted in the faired, (parallel to the longitudinal axis) orientation, but haven't had the opportunity to ask the builder how it was done. Any clues? Thanks. You can fax me a drawing of same to 770-412-6655. Mal rvbildr(at)juno.com ________________________________________________________________________________
Subject: Re: paint scheme
From: lm4(at)juno.com (Larry Mac Donald)
Date: May 31, 1997
--> RV-List message posted by: lm4(at)juno.com (Larry Mac Donald) RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) (Michael C. Lott) writes: Does anyone else have a military camouflage paint scheme on their rv? If anyone has info like this please e-mail me or give me a number where I can call you. Thanks, alot. MCL Michael, The paint you are looking for is made by PPG and comes in sand,black, (which turns purple within six months), forest green and sage green. Sorry, I don't have the numbers anymore, but then again, maybe you don't want them. You can buy this stuff at Rochester Lead Works, 100 Anderson Ave., Rochester, N.Y.,14607--(716)-244-3800). I know that these people have a book that tells what the numbers are. BUT, If you consider that this is a Mil. Spec. paint and that the military has been using it in an effort to hide the heat signature of their equipment, then you might consider finding out what the numbers are and then find a commercial flat paint that matches. You might want to take a look at a tank or hummer before you go the mil. spec. route. HTH larry Mac Donald lm4(at)juno.com ________________________________________________________________________________
Date: May 29, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: Re: IO-320B1A Problems.
--> RV-List message posted by: Dave Barnhart Mark: >I have an IO-320B1... I too have an IO320-B1A. Fortunately, Mine came with the spacers (The engine was still hanging from the Twin Comanche mount). If you can wait until this weekend, I'll go out to my hangar and measure the bolts for you. As for locating the spacers, I would just start calling the parts houses list in Trade-A-Plane under "Lycoming Parts". (Just out of curiosity, how much is a set of spacers new from Lycoming?) Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
Date: May 31, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: IO320-B1A Mount Bolt Lengths
--> RV-List message posted by: Dave Barnhart I applogize for sending this to the entire list. Someone posted a query about the lengths of the mount bolt needed for an IO320-B1A, but unfortunately, I have deleted that message and so I don't know who to reply directly to. All four bolts in mine were AN7-50A Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
Date: May 29, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: Re:
--> RV-List message posted by: Dave Barnhart >The 6A is easier when on the ground in all respects, you "drive" it around. >The 6 must be "flown" until tiedown, like all taildraggers. That sentence sure caused me to chuckle. I've been flying nothing but taildraggers (Champ and a C120) for the past 18 months. Last weekend I went for a BFR, and on a whim did the BFR in an Archer. There I was, out of habit, taxiing around at very slow speeds and holding full up elevator, and essentially 'flying' it all the way to the tiedown. Several times the CFI commented "This isn't a taildragger". I chuckled at how much less skill and attentivness it took to taxi the archer. Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
From: JHeadric(at)aol.com
Date: May 31, 1997
Subject: Re: Engine acquisition
--> RV-List message posted by: JHeadric(at)aol.com When the engine is assembled, it is usually put together with a heavy preservative type lubricant and unless the engine is run, will not have any contaminants inside, such as carbon, moisture, etc. ________________________________________________________________________________
Subject: Re: Sources for Alumiprep and Alodine
From: schmidtjm(at)juno.com (James M Schmidt)
Date: May 31, 1997
--> RV-List message posted by: schmidtjm(at)juno.com (James M Schmidt) Most automotive paint stores will carry those products. ________________________________________________________________________________
From: REEVES322(at)aol.com
Date: May 31, 1997
Subject: Re: Rivet sets
--> RV-List message posted by: REEVES322(at)aol.com I have use swivel head rivet sets for some time now and Love them,,them comform to the skin with out having to be so careful as to being perpendictular..keeps the smily faces to a minimun. I bought mine from Avery Tools and have nothing but the highest reguard for their tools..Good people to do business with. The offset sets come in handy once in a while but I cant remember exactly where. Good Luck! ________________________________________________________________________________
Date: May 31, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Re: V Stab Strobe fit
--> RV-List message posted by: Bob Skinner >How does one install the Whelen strobe tube, p/n # A625, inside the >vertical stab fairing on the RV-6? The base of the strobe tube is too >wide to fit inside the fiberglas tip, unless it is installed diagonally. >I've seen several fitted in the faired, (parallel to the longitudinal >axis) orientation, but haven't had the opportunity to ask the builder >how it was done. Any clues? Thanks. >You can fax me a drawing of same to 770-412-6655. >Mal >rvbildr(at)juno.com Mal, All I have to look at is a picture but it appears that this unit would be too large. The strobe that I used in the V.S. location is a A650 wing tip strobe, which is smaller. I discarded the metal housing that holds the glass to the base of the strobe. I cut a hole in the tip fairing and gradually enlarged it so that the lens fit with the lip of the glass bearing on the fiberglass. Where the material was thin, I potted in a mill fiber/resin mix to make a more solid installation. To hold the lens in place, I made a right angle bracket out of .032 with one leg pressing on the base of the strobe, forcing the assembley tight into the tip. The other leg fit against the rear spar of the V.S. and was attached with one nut plate mounted on the inside of the tip rib/V.S. spar juncture. I'll bet if you trade for a A650, you'll be able to make it work. Bob Skinner RV-6 BSkinner(at)navix.net ________________________________________________________________________________
From: RV6AIR(at)aol.com
Date: May 31, 1997
Subject: RV6 C.G.
--> RV-List message posted by: RV6AIR(at)aol.com Just finishing up an RV6, 180, C/S, S/C. A few things remain to be installed and I was wondering if someone has completed a similar airplane and could tell me what empty weight and C.G. to expect. Thanks, Bob Lovering RV6 22021 N7LA ________________________________________________________________________________
Date: May 31, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: Engine acquisition
--> RV-List message posted by: Denny Harjehausen >--> RV-List message posted by: Tim Bronson <70773.2700(at)CompuServe.COM> > >Hi Folks: > >Another new guy question: Since conventional wisdom has it that inactivity is >not good for an engine, how do you who know feel about the idea of buying a >freshly overhauled (or new) engine for a project that won't be completed for a >few years? What is involved in storing an engine long term? What needs to be >done to "un-store" it when the airplane is ready for it? Would this all be >worth the trouble or would it be better to just buy the engine when it's needed >(at the new, higher price)? > Mr. Hatch, who is widely respected in the engine department told a friend and I to fill our engines up to top of the filler pipe with oil and turn it over once a month, top to bottom..bottom to top and as I recall, to change the oil after few months, that should gurantee that the cam and crank are protected.....Price is something else, I keep saying they can't get any higher, but they seem to....but who knows for sure when that will change. There is all this talk of a new engine being developed by Cont. and others at half the price of the current Lycs & Cont....It could happen...I bought a used engine and am having it rebuilt and fancied up inside a little. Hoping for some better than stock results. The projected cost is about 70% of a new one. Have A Great Day! Denny retflygtiger(at)proaxis.com RV-6/ Fuselage Lebanon, OR ________________________________________________________________________________
Subject: Re: two RV6A's, one T hanger
From: ebundy(at)juno.com (Ed Bundy)
Date: May 31, 1997
--> RV-List message posted by: ebundy(at)juno.com (Ed Bundy) >we are currently figuring out how to best store two RV6A's in a 40' x >40' T hanger. A dolly which allows the planes to be rolled in sideways so >the props are facing one another seems most pratical. This way the You might be able to "nest" them if you have 20' from the doors to the walls of the indentations. With one facing in and the other facing out they should fit. A 6A is just a hair under 20' long. You will have to roll out the out-facing one to get the in-facing one out, but I think this will be a lot less hassle than using a dolly and going sideways. I have a 6A and an ultralight nested in this fashion and it works well. Before putting them away, give a guess at which one will be utilized next and nest accordingly. Ed Bundy RV6A - first flight 11/20/96 ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
Date: May 31, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: KLX135A info
--> RV-List message posted by: Dave Barnhart Now that I've finished installing a King KLX-135A in my RV-6, I thought I'd pass along a couple of interesting bits of information about it that may help someone in the future who is trying to make a purchase decision: 1. The KLX-135A will accept Mode C altitude information from your encoder. (This altitiude info is used by the KNLX-135A for SUA alerts.) When wiring up the outputs from your encoder, simply parallel the KLX-135a and your transponder. Of course, the encoder output PRESSURE altitude, which brings us to fact #2: 2. The KLX-135A does not have an RS232 serial air data input. If it did, my RMI microEncoder could send it the altimieter setting. I do not know if other GPS/COM products have such a serial air-data input, but it's worth checking out. Entering the current altimeter setting into the KLX-135A is also a bit of a pain. You must use the right-hand pair of knobs to get to SETUP page 8, hit the CRSR button, and then use the same knobs to enter the current altimeter setting. Entering the current altimeter setting in this manner involves so much heads-down time that I suspect I'll end up turning the SUA Alert feature off. As an aside, for the first time today, I was sitting in the airplane, with the KLX135A Comm, PS2000 intercomm, AND the CD player going, listening to it all through the headset. Pretty Cool. Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
Date: May 31, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: Master & Starter relay on battery box
--> RV-List message posted by: Dave Barnhart I need some input from those of you who have mounted your master and battery relays on the battery box. It appears that this would make it difficult to remove the battery box and gain access to the battery without disconnecting cables from the relays. How did you do it? Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
From: grihen(at)juno.com
Date: May 31, 1997
Subject: RV6 Wing Mounting
--> RV-List message posted by: grihen(at)juno.com Well Guys and Gals, I guess I have taken leave of my senses after working on my RV6 for a year and a half. I am in the process of bolting on my wings but I cannot find anything in the plans that show what nuts and washers go on the bolts that hold the wings on the 604 bulkhead. Drawing 15 comes the closest by telling what size reamer to use on the holes. What am I missing here? I am sure that I have overlooked something. John Henley (grihen(at)juno.com) Standing By ________________________________________________________________________________
Date: May 31, 1997
From: Glenn & Judi <flyers@anet-chi.com>
Subject: MP gauge on fixed pitch prop
--> RV-List message posted by: Glenn & Judi <flyers@anet-chi.com> Hi, I have recently heard of a normally aspirated, fixed pitch RV that was equipped with a manifold pressure gauge. Until now, a MP gauge is something I have only seen on aircraft equipped with a constant speed or variable pitch prop. Has anyone else seen this who might be able to explain how it is used on a normally aspirated fixed pitch engine? Thanks in advance, Glenn Gordon ________________________________________________________________________________
From: JamesCone(at)aol.com
Date: May 31, 1997
Subject: Re: RV-6 vs RV-6A
--> RV-List message posted by: JamesCone(at)aol.com My tongue was not in my cheek when I wrote about the 6 vs the 6A. The 6A is easier to takeoff and land by a long shot. Insurance and resale values are facts. The 6A is cheaper to insure and gets more at resale time. The 6 is a great plane and can be mastered but the 6A is easier. Jim Cone jamescone(at)aol.com ________________________________________________________________________________
From: JamesCone(at)aol.com
Date: May 31, 1997
Subject: Rvator
--> RV-List message posted by: JamesCone(at)aol.com I was pleased to see my plane and instrument panel in the Rvator as well as the picture of me after my first flight with the RV grin. I was also pleased that my first flight was noted. However, there was an error in the comment about how much they liked my newsletter. It is not the Mid-America RVator. It is Van's Air Force, Tri-State Wing Newsletter, incorporating the Midwest RVator. It really isn't a local newsletter, and is dedicated to helping you build your RV better and easier while avoiding the mistakes that others have made who are ahead of you in construction. Many people, including Tony Bengelis, have told me that it is one of the best newsletters around. If you are interested, subscriptions are $5.00 per year, which just covers my costs. It is published quarterly. Subscribers get all issues for the years that they subscribe to. I have the back issues for 1995 and 1996 which cover the building of an RV from the beginning. They are also available for $5.00 per year. I offer a money back guarantee and have never had any takers. Send me an E-mail if you want to subscribe and I will send you the first two issues of 1997 and they can cross your check in the snail mail. I wish that some of the subscirbers who have written me about my newsletter would have send a copy of their praise to the RV list. I work very hard to produce a newsletter that is helpful and entertaining. Thanks for the opportunity to toot my own horn. Jim Cone, Editor Van's Air Force, Tri-State Wing Newsletter 422 Savannah Ridge Drive St. Charles, MO 63303 jamescone(at)aol.com ________________________________________________________________________________
Date: May 31, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: King KLX-135A & Navaid Devices
--> RV-List message posted by: Dave Barnhart I called the folks at Navaid devices yesterday, and they told me that some customers are reporting problems interfacing their autopilot to the King KLX-135A, but they also had no more data that that. In looking at the specs of both units, I fail to see the reason why. The KLX-135A has the standard pair of 0-150mv outputs designed to drive a CDI needle, and according to the man I talked to at Navaid Devices, that's exactly what the autopilot wants. Has anyone else on the list had any experience connecting a King KLX-135A to a Navaid Devices autopilot? Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
Date: May 31, 1997
From: George McNutt <GMcNutt(at)compuserve.com>
Subject: INSURANCE QUESTIONS
--> RV-List message posted by: George McNutt Here is my 2 cents about insurance. Insurance rates vary from company to company because of the different fin= e print restrictions which limit company exposure to loss. To get an accura= te analsys of rates you must compare apples to apples. This can only be done= by asking for quotes on identical coverage from each company. In my case = I ask for a million dollar combined single limit policy with no restriction= on family members, and that is the coverage I carry on my C-182. You will find that most companys quotes will be very close for identical coverage and many will be lower than Avemco. Most pilots feel they need a million or more liability, hundred thousand passenger hazard per seat plus hull coverage. Why "combined single limit" - here is how my agent explained it to me. If we prang into a school yard full of kids the million liability coverag= e will not be enough, however the insurance risk is low because statisticll= y most prangs only take out a few trees or part of a wheat field. = One hundred thousand per seat passenger hazard is inadequate if the accident is serious, the combined single limit would divide the million between third party liability and your buddy in the right seat. Beware th= e policy that limits coverage of family members to $25,000 (see fine print = in policy). Statistics show that the majority of serious accidents involve a= smoking hole in a wheat field with a family member in the right seat, thi= s means a low payout for the insurance company. Farmer $500, wifes estate $25,000 + hull. Combined single limit would pay farmer $500, wifes estate balance of the million, plus the hull. (Wifes estate hopefully willed to kids) = Combined single limit coverage is about $200 more than standard policy because the insurance companys exposure is higher. As for numbers, I pay $1125 Canadian ($875 U.S.) for one million combined single limit policy including $55,000 hull. Hull rates decreased this year. (ATR, active airline pilot =3D lowest rate) = The above is my understanding and may not be gospel, however it may set y= ou to thinking of questions to ask your insurance agent. George McNutt, - H.S. = ________________________________________________________________________________
Date: Jun 01, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Re: MP gauge on fixed pitch prop
--> RV-List message posted by: Bob Skinner > I have recently heard of a normally aspirated, fixed pitch RV that was >equipped with a manifold pressure gauge. > Until now, a MP gauge is something I have only seen on aircraft equipped >with a constant speed or variable pitch prop. > Has anyone else seen this who might be able to explain how it is used on >a normally aspirated fixed pitch engine? >Glenn Gordon Glenn, I have a M.P. gauge in my 150 hp RV-6. According to an article in the RVator, you can determine 75% power by adding the first two digets of the rpm to the m.p. If the figures add up to 48, it equalls 75% power. I took the figures from the article and interpolated (?) and came up with the "inbetween numbers" of: 40 48.0% 42 55.0% 43 58.0% 44 62.0% 45 65.0% 46 68.0% 47 72.0% 48 75.0% 49 78.0% 50 82.0% 51 85.0% 52 88.0% Hopefully, this is correct as I've been flying my RV using these figures. Manifold pressure can also be used to help determine the health of the engine. By the way, I do have the Lycoming manual that has the power charts for the 150 hp. However, the print quality is poor and very small and even a magnifying glass is no help to my bi-focalled eyes. Does anyone on the list have this info and would you be willing to make a copy for me? At the very least, would someone be willing to use the above figures and compare them to "the book". I was just reading AOPA and in one of the articles, they indicated that a IO-360 in a Mooney would be at 75% power at 4,000 feet when operated at 23"/2,700 rpms, 24"/2,600 rpms or 26"/2,400 rpms. These figures add up to 50 so, which one is correct? Have I been operating under 75% power all this time? Bob Skinner RV-6 BSkinner(at)navix.net ________________________________________________________________________________
From: LesDrag(at)aol.com
Date: Jun 01, 1997
Subject: Re: MP gauge on fixed pitch prop
--> RV-List message posted by: LesDrag(at)aol.com << Hi, I have recently heard of a normally aspirated, fixed pitch RV that was equipped with a manifold pressure gauge. Until now, a MP gauge is something I have only seen on aircraft equipped with a constant speed or variable pitch prop. Has anyone else seen this who might be able to explain how it is used on a normally aspirated fixed pitch engine? Thanks in advance, Glenn Gordon >> Hi All, Brad Overholser (Pelican Aviation), Kent Rockwell (Rocky) and I have flown our RV-3's with a MP gauge, fixed pitch props, and a Lyc. O-320, Lyc. IO-320, and Lyc. O-290, respectively. The one significant advantage of having the MP gauge is that it allows you to set the power before the transition from climb to cruise is complete. Knowing the difference in MP between the three RV's allowed us to state a power setting during the transition to cruise, or for any power changes. BTW, I heard that certification is going to be required for formation flight. Anyone one know any particulars?? In order to determine the horsepower from the engine, an accurate MP and tach are required. Spam cans with fixed pitch props have "known" MP's for given RPM and altitudes, for there charts. So they don't need a MP gauge. Jim Ayers LOM M332A Ivoprop RV-3 N47RV Maroon Marauder LesDrag(at)aol.com ________________________________________________________________________________
Date: Jun 01, 1997
From: "Robert G. Miller, Jr." <rgmiller(at)sprintmail.com>
Subject: Re: insurance
--> RV-List message posted by: "Robert G. Miller, Jr." Michael C. Lott wrote: > > --> RV-List message posted by: lottmc(at)datastar.net (Michael C. Lott) > > I just got a quote from an insurance company (Falcon Ins. Comp. of > Arizona) 20,000.00 hull coverage. $1019.00 per year. 500.00 earned > since test hours not flown off yet. 100.00 deduct not in motion. > 1,000,000.00 liability. Covered from first flight. My experience: > commercial, single eng. land. no instrument rating. total time 1240 > hrs. 300 of that in taildraggers. How does this coverage sound to > others who have insurance? Is this a good price, or can it be beat by > much? Tell me what you think. thanks. Mike: I don't know about price, but your hull coverage is too low. Do you realize that if your a/c suffers $20,000 or more in damage, the company is going to write the check for $20,000 and TAKE YOR PLANE FOR SALVAGE. Robert Miller ________________________________________________________________________________
Date: May 31, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: Re: RV-6 vs RV-6A
--> RV-List message posted by: Jerry Springer aol.com!JamesCone(at)matronics.com wrote: > > --> RV-List message posted by: JamesCone(at)aol.com > > My tongue was not in my cheek when I wrote about the 6 vs the 6A. The 6A is > easier to takeoff and land by a long shot. Insurance and resale values are > facts. The 6A is cheaper to insure and gets more at resale time. The 6 is a > great plane and can be mastered but the 6A is easier. > > Jim Cone > jamescone(at)aol.com Well Jim I don't want to get into a pissing match with you on the list because I appreciate the good information you post to the list. When you say that the -6A is is easier by a long shot you are just plain wrong, it may be easier for you to land and take off a tri-gear but that does not mean that that is so for the rest of us. The -6 is one of the easiest taildraggers there is to land and take off. Your long post on how much safer the -6A is made it sound like the -6 was dangerous and I just don't want anyone that is building a -6 to get the idea that it is unsafe because that is just not so. By the way how are going to steer your 6A on landing or takeoff if you should lose a brake? the -6 does not need brakes to takeoff or land. I am baseing my feelings on 21 years of instructing and almost 900 hrs of RV time. I realize I may not be as experienced as you but the -6 is as safe and easy as the -6A, You've got me on the visability on the ground but even that is not a problem because visibility is still great. and yes I will land just as short as you do and on rougher fields without fear of damageing the nose gear. Sorry that I did not get to meet you when you were out here at Van's Bill Benedict told me that you came all the way out here to see the picture of your airplane on Van's customer desk.:-) Fly safe Jerry -- Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR jsflyrv(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 01, 1997
From: Frank van der Hulst <frankv(at)pec.co.nz>
Subject: Re: V Stab Strobe fit
z> --> RV-List message posted by: Frank van der Hulst >How does one install the Whelen strobe tube, p/n # A625, inside the >vertical stab fairing on the RV-6? The base of the strobe tube is too >wide to fit inside the fiberglas tip, unless it is installed diagonally. >I've seen several fitted in the faired, (parallel to the longitudinal >axis) orientation, but haven't had the opportunity to ask the builder >how it was done. A thought... an RV-4 builder suggested I be careful where I fitted the flashing red beacon on the VS of my RV-6. If you fit it too near the front, it'll flash into the cockpit. I'd imagine a strobe flashing into the cockpit would be even more distracting! Frank. ________________________________________________________________________________
From: CYoung9519(at)aol.com
Date: Jun 01, 1997
Subject: Re: INSURANCE QUESTIONS
--> RV-List message posted by: CYoung9519(at)aol.com George: Thanks for the information on aviation insurance. Would you be willing to tell us the name of your company? Thanks in advance for your anticipated cooperation. Chuck ________________________________________________________________________________
From: Bumflyer(at)aol.com
Date: Jun 01, 1997
Subject: Re: Rvator
--> RV-List message posted by: Bumflyer(at)aol.com Jim I don't want the list to think no body loves you. I have published a newsletter for the last three years, called the Rocky Mountain RVator. (Don't send money we aren't looking for circulation records). In the process of doing this job I established exchange agreements with all known RV newsletter publishers and hence have read most out there. Jim's is the best . It is also the cheapest, most dependable, best reproduced and has a sense of humor. Send him your 5. If you're smart you will go for the last two years while they are available. Must reading for slider builders. On the matter of 6 vs. 6A. They are both great airplanes well within the capabilities of average aviators. To the listers, who tend to decide by surveys and analysis.... Listen to the guy who said he had known some 6 owners who wished they had built a 6A and no 6A builders who wished they had built a 6. For you listers who are hassling with a decision, first define what is fun for yourself. You can no more define which is best for some one else than you can define what is fun for someone else. For example for me hiking swimming and parachuting are emergency procedures and not fun. Skydiving and tail dragging are not my idea of fun. But a whole lot of people out there think differently. My idea of fun is flying a powered responsive airplane in the air. Taxiing to the hangar is no more fun for me than putting air in the tires. My favorite comment so far was the fellow who said he wouldn't 'turn up his nose' at a nose dragger. How about the rest of you lighten up?? I don't work for Jim Cone or anyone else. D Walsh ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@denmark-c.it.earthlink.net>
Date: Jun 01, 1997
Subject: Re: Rvator
--> RV-List message posted by: "Tim Lewis" <timrv6a@denmark-c.it.earthlink.net> > I wish that some of > the subscirbers who have written me about my newsletter would have send a > copy of their praise to the RV list. > > Jim Cone, Editor > Van's Air Force, Tri-State Wing Newsletter > 422 Savannah Ridge Drive > St. Charles, MO 63303 > jamescone(at)aol.com OK, here goes: I subscribed to Jim's newsletter in 1996. The $5 subscription was THE BEST $5 I've spent on my RV-6 project. Jim's article on canopy construction saved me countless hours. As I and others have noted in the RV-list over the years, Van's instructions on the canopy aren't so good. Jim's instructions are great, and they WORK. I sent Jim another $10 to buy the 1995 back issues and to subscribe for 1997. Absolutely worth every penny. Thanks Jim. Tim --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
Date: Jun 01, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: MP gauge on fixed pitch prop
--> RV-List message posted by: John Darby <johnd@our-town.com> >Has anyone else seen this who might be able to explain how it is used on >a normally aspirated fixed pitch engine? Glenn; It's not very technical on my part, I use the man. press. gauge to fill up that hole over there in my panel. Since it is there, I use it to set power on let downs (keep m/p at or above 15 in.) and to mach it together with the rpm for approximate power output of the engine. Other than that, it's just cool. I had one given to me, thought it would look better in the panel than on the shelf. Just thankful they didn't give me an anvil!!! Can't think of a better reason at the time. If you look close and do some interpolation on the Lyc. operators manual, you can figure out the combination of mp and first two digits of rpm as 48 is 75% of engine power. And I thank Bob Skinner for admitting that he too is having trouble with that chart, I thought for a while there that I was getting old. John Darby RV6 N61764 flying Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: Jun 01, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: RV6 Wing Mounting
--> RV-List message posted by: John Darby <johnd@our-town.com> >I cannot find anything in the plans that show what nuts and >washers go on the bolts that hold the wings on the 604 bulkhead. Drawing >15 comes the closest by telling what size reamer to use on the holes. >What am I missing here? I am sure that I have overlooked something. >John Henley; I would suggest putting 3/8 nuts and washers on the 3/8 bolts and 1/4 nuts and washers on the 1/4 bolts. :<) Having gotten that out of my system...... I did have trouble with the length of the bolts on mine. I had to use the max. number of washers on some of them. The problem seemed to be that the spar laminates are a little splayed apart in there and by time you get a bolt hammered in, the thread showing looks as if it will take X number of washers and then the bolt to leave the magical two threads showing. But as you torque it down, the spar laminates compress and next thing you know you are trying to tighten the nut up against the shoulder of the bolt. Good way to get proper torque but it doesn't tighten the spar to the frame! Add to this that some bolts need to be longer due to passing through some of the additional flanges in front of the bulkhead, well, that lead to a lot of ins and outs!!! Mine were so different that when I took the bolts out to disassemble to move to the airport, I wrote next to the hole what length and how many washers each took, because the first assemble took so many trial and errors to get it right. But they are so accessible(this is tongue in cheek for those who don't have a sense of humor), you don't HAVE to do that!!! After the exercise of all of this, some one told me to take a wire with a 90 degree bend in the end that sticks out very short, run it in the hole, hook the 90 degree bend on the back side, use your finger to mark the front side, hold your finger mark, take the wire out and match it to a bolt length that would work, and then put that bolt in. Damned simple, it shows that I'm smart because I don't think simple!! (hows that for ego?) John Darby RV6 N61764 flying Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: Jun 01, 1997
From: Rick Osgood <Rick(at)ccc.henn.tec.mn.us>
Subject: Chevy Vortec project Belted Air Power
--> RV-List message posted by: Rick Osgood Has anyone heard any new info on the Belted Air project?? Is it available, final cost, new performance figures, etc.... Thanks to all RV6A - wings (finally warm in Minnesota :) -- Rick Osgood Rick(at)ccc.henn.tec.mn.us ________________________________________________________________________________
Date: Jun 01, 1997
From: "Robert L. Nuckolls, III" <RNuckolls(at)compuserve.com>
Subject: Exp-Bus . . .
rv-list --> RV-List message posted by: "Robert L. Nuckolls, III" /The same board is used for the 40 and 60 Amp versions - = /The board is capable of 60 Amps but the master relay, on /the board, is only rated at 40 Amps. When 60 Amps is desired, = /you solder three pads together on the board, or buy it already = /done and add a remote master solenoid. Typical wiring diagrams = /are provided. Master relays should always be mounted within inches of the battery to minimize the amount of un-protected, always hot wire between the battery and the master relay. VERY IMPORTANT . . . the battery master should also control starter current . . . starter contactors can stick shut and give you no auxiliary means for shutting off the flow of power to the starter. /Any load over 9 Amps will require a regular circuit breaker, or = /heaven forbid, a fuse. So your pitot heat will need it's own = /breaker and switch. Why is it desirable to put part of your circuit protection on an expensive, fabricated assembly that is NOT flexible in terms of future additions that still makes you cover things like pitot heat and landing lights as a separate bus and protection system? What's the problem with a fuse? If the job is done right, the probability of a fuse opening is very close to zero . . . when it does, there's something broke . . . and there's no value in fiddling with it it flight. /If you don't use switch 2 for the alternator field, it's = /available for any 5 amp load. What are the alternatives? Are you considering an alternator with a built-in regulator? Granted, they're attractive for simplicity of installation but cannot be fitted with over voltage protection. One of my readers smoked several expensive gizmos in his airplane on the way to Sun-n-Fun due to failure of a built-in regulator. He planned to modify the system per my recommendations after Sun-n-Fun but it didn't last that long. . . /The remote switch capability is neat in that it allows you to group = /switches as you desire, not as they require. As long as you're going to dismount the switches, what's the advantage to be gained with a $250 product that costs more than two to three times as much as some very practical alternatives? /I install a lot of specialty items in buildings /and since they have started using ptc's our service problems have = /plummeted. I'm just tickled with their performance, besides, I = /no longer have to worry about the location of the nearest radio = /shack for replacement fuses when "I" blow one. Buildings and airplanes have nothing in common with respect to electrical systems design considerations. Airplane branch feeds from the bus DO NOT nuisance trip . . . at least they shouldn't if they're designed right. The fact that self-reseting breakers are a boon to anyone's lifestyle is a testament to poor design. In over 1,000 hours of flying, I've never had a breaker open in flight on airplanes ranging from C-120 to A-36. If a breaker ever DOES open, I'm NOT going to mess with it in flight (except for the 60 amp alternator breaker on Pipers and Cessnas . . . that one is DESIGNED to nuisance trip). Of the 150,000 airplanes in the GA fleet and assuming an average of 15 breakers per airplane, there are over 2 million breakers flying of which the vast majority will never be called upon to do their job. Why? because reliabilty is supposed to be designed in. Hate to be pedantic about this but there are serious deficiencies with the EXP-Bus design in addition to failure to meet their advertising hype. I've caught some flack about posting the 4-page critical design review on this product to the list . . . yet people among = you recommend this product and at the same time, didn't = read what I wrote about it . . . one fellow told me he automatically deletes any piece over a few thousand bytes; a "don't bother me with facts, my mind is already made up" syndrome. If someone believes in this product, then at least do me the honor of debating my evaluation, especially if you're going to recommend it to the less enlightened in such glowing terms. List-servers are for the disemination of good information and = a forum for weeding out the bad . . .I won't post the design = review again but if anyone cares to read it for information = -or- the purpose of engaging in useful debate, I'll respond = to e-mail requests for copies. = Regards, Bob . . . = AeroElectric Connection //// (o o) =3D=3D=3D=3D=3D=3D=3D=3D=3D=3DoOOo=3D(_)=3DoOOo=3D=3D=3D=3D=3D=3D=3D=3D= =3D=3D | | | Go ahead, make my day . . . | | Show me where I'm wrong. | =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D 72770.552(at)compuserve.com http://www.aeroelectric.com = ________________________________________________________________________________
Date: Jun 01, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: rvator
--> RV-List message posted by: "les williams" Hey Jim, Ya got a great newsletter. Those you don't get it are missing out. Listers: subscribe. Thanks, Les Williams/RV-6AQB/N24LW (res)/finish kit ________________________________________________________________________________
From: OrndorffG(at)aol.com
Date: Jun 01, 1997
Subject: Re: INSURANCE QUESTIONS
--> RV-List message posted by: OrndorffG(at)aol.com Chuck, we us AUA 1-800-727-3823 and ask for Mac McGee tell him you had talked with me he's a good guy and like to insure RV's....George ________________________________________________________________________________
From: MAlexan533(at)aol.com
Date: Jun 01, 1997
Subject: RV-8 Tilt Canopy?
--> RV-List message posted by: MAlexan533(at)aol.com I own an RV-4 and am contemplating building an RV-8, mostly because I need a project! My question is, is the RV-8 available with the standard RV-4 type tilting canopy? I sat in the RV-8 at Sun n Fun, and I love everything about the plane except the big roll bar going across my field of vision. This bugs the heck out of me, as I'm used to having unrestricted visibility in the RV-4, and I feel it is very important for safety reasons. Also it is simpler to build, and lighter to go with the tilt canopy. Another question; Has anyone finished their RV-8 tail kit yet? If so, how long did it take you? If you built an RV-4 before, what time-savings would you estimate is attained due to pre-punched parts? Thanks! ________________________________________________________________________________
Date: Jun 01, 1997
From: Charlie Kuss <charliekuss(at)sprintmail.com>
Subject: 95-96 back issues of newsletter
--> RV-List message posted by: Charlie Kuss Jim, I like the 2 issues of your newsletter so much that I want you to send me the 1995 & 1996 back issues before they are all gone!! You'll find my check for $10 in your mail this week. Charlie Kuss 3000 S. Ocean Blvd. #103 Boca Raton, Fl. 33432 ________________________________________________________________________________
Date: Jun 01, 1997
From: George McNutt <GMcNutt(at)compuserve.com>
Subject: INSURANCE QUESTION
--> RV-List message posted by: George McNutt Thanks for the information on aviation insurance. Would you be willing t= o tell us the name of your company? Thanks in advance for your anticipated= cooperation. Chuck My insurance is through a local aviation insurance broker in Vancouver B.C., Willis Corroon Aerospace, and is placed with CAIG (Canadian Aviatio= n Insurance Group) of Toronto Canada. CAIG places the insurance risk with several member companies and my designated company is St. Paul Fire & Marine Insurance Co. Prior to 1994 I used Avemco, however when I requested removal of their limits of liability on family members the rates increased to the point th= at they were uncompetative. = George McNutt - H.S = ________________________________________________________________________________
From: "Dave Bergh" <dbergh(at)cyberhighway.net>
Subject: Re: Rvator
Date: Jun 01, 1997
--> RV-List message posted by: "Dave Bergh" ---------- > > --> RV-List message posted by: JamesCone(at)aol.com > > I was pleased to see my plane and instrument panel in the Rvator as well as > the picture of me after my first flight with the RV grin. I was also pleased > that my first flight was noted. However, there was an error in the comment > about how much they liked my newsletter. It is not the Mid-America RVator. > It is Van's Air Force, Tri-State Wing Newsletter, incorporating the Midwest > RVator. It really isn't a local newsletter, and is dedicated to helping you > build your RV better and easier while avoiding the mistakes that others have > made who are ahead of you in construction. Many people, including Tony > Bengelis, have told me that it is one of the best newsletters around. If you > are interested, subscriptions are $5.00 per year, which just covers my costs. > It is published quarterly. Subscribers get all issues for the years that > they subscribe to. I have the back issues for 1995 and 1996 which cover the > building of an RV from the beginning. They are also available for $5.00 per > year. I offer a money back guarantee and have never had any takers. Send me > an E-mail if you want to subscribe and I will send you the first two issues > of 1997 and they can cross your check in the snail mail. I wish that some of > the subscirbers who have written me about my newsletter would have send a > copy of their praise to the RV list. I work very hard to produce a > newsletter that is helpful and entertaining. Thanks for the opportunity to > toot my own horn. > > Jim Cone, Editor > Van's Air Force, Tri-State Wing Newsletter > 422 Savannah Ridge Drive > St. Charles, MO 63303 > jamescone(at)aol.com > Dear Jim, I would like a subscription to your newsletter and would also be interested in the 2 years of back issues you talked about. Let me know how much and to whom to make the check to and I will put it in the mail. Thanks, Dave Bergh. RV6 -working on rudder Dave Bergh RT 1 Box 814 Mountain Home, ID 83647 (208)587-8203 ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@iceland-c.it.earthlink.net>
Date: Jun 01, 1997
Subject: Pondering the essential bus concept
--> RV-List message posted by: "Tim Lewis" <timrv6a@iceland-c.it.earthlink.net> On 28 Feb 97 Bob Nuckolls posted an article entitled "Aircraft Electrical Systems: a Philosophy for Reliability" to the RV-list. A circuit diagram of this system is shown in the Aero Electric connection. The basic idea is that the builder puts his/her "essential" electrical equipment on one bus, and the "non-essential" electrical equipment on the non-essential bus. The essential bus is fed from the non-essential bus via a diode. If the non-essential bus goes off line (battery contactor fails, or pilot shuts it down to conserve power in the event of alternator failure) then the pilot flies with the essential bus. The essential bus can get power from the battery directly (avoiding the failed battery contactor) via an alternate feed path which is switched on when needed. (I hope I've summarized this concept accurately). The feature of this system I really like is it rescues the pilot from the single point of failure represented by the battery contactor. In attempting to adopt this design, however, I'm finding that nearly my entire electrical system ends up on the "essential" side of the essential/non-essential sheet. I'm considering using a single bus, but providing an alternate feed path (switched and fused, of course) to the bus that avoids the battery contactor. In the event of battery contactor failure I would switch on the alternate feed path. In the event of alternator failure (as annunciated by my electronic engine monitor which also monitors bus voltage) I'd simply shut off all non-essential loads (as dictated by my needs at the time) and land as soon as practical. Any comments on this idea? Thanks, Tim Lewis --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@iceland-c.it.earthlink.net>
Date: Jun 01, 1997
Subject: Re: Exp-Bus . . .
--> RV-List message posted by: "Tim Lewis" <timrv6a@iceland-c.it.earthlink.net> I don't question Bob's assessment of the experimental bus, but I do have an experience to share here. > If the job is done right, the probability of a fuse opening > is very close to zero . . . when it does, there's something > broke . . . and there's no value in fiddling with it it flight. ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ That's ALMOST always true. I once had an intermittent short in my panel wiring ground out my panel lights while I was IMC at night shortly after departure from San Diego (in a Grumman Yankee). The momentary grounding blew the fuse. I flew the airplane thru the overcast using a flashlight in my teeth to see the panel (that's why I always keep the flashlight on a string hanging from my neck... easy to find). After I was thru the overcast I replaced the fuse, and found that the panel lights worked OK for the approach back into Los Angeles. It was a lot easier with working panel lights than with just a flashlight. The next day I found the abraded wiring and made sure it was properly insulated. Given that experience I'll likely opt to keep my fuses/breakers within reach. In general, however, if a fuse blows it'll probably blow again if replaced, 'cause it blew for a reason. Tim --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
Date: Jun 02, 1997
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Re: Accomodating Instrument Placement
--> RV-List message posted by: Leo Davies Tim, I suspect that you are not the first person to notice this. I am at the stage of contemplating the area behind the panel and wondering what it is save to remove. Several of the IFR 6As that I have seen have swiss cheese like arrangements of both these ribs and the bulkhead immediately forward of the panel. I have not seen much comment on this from any source and would be delighted to hear from the completed builders how they coped with these restraints........Jim, you still putting out the newsletter now you're flying? Leo Davies leo(at)icn.su.oz >--> RV-List message posted by: "Tim Lewis" <timrv6a@norway-c.it.earthlink.net> > >In the RV-6A slider configuration there are 3 ribs that support the >glareshield and to which the instrument panel attaches. The three >pieces are 2 ea F-6107 and 1 ea F6108. > >Wouldn't you know it, these pieces interfere with my ideal location >of my flight instruments. These pieces are 1.5 - 2" high at the >instrument panel, but they get longer (more vertical extent) forward >of the instrument panel, so they sit right where the back end of >some of my instruments and radios should go. > ________________________________________________________________________________
Date: Jun 01, 1997
From: Tom Martin <fairlea(at)execulink.com>
Subject: fuel injection
--> RV-List message posted by: Tom Martin I am close to purchasing a used engine for my new project and the bendix fuel control needs to be rebuilt. Does anyone have any opinions on getting the bendix rebuilt vs. buying a new airflow performance unit? It would seem that the cost is about the same. Would I be able to use the same flow divider and injectors? Thanks in advance Tom Martin RV-4 ________________________________________________________________________________
Date: Jun 02, 1997
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Re: MP gauge on fixed pitch prop
--> RV-List message posted by: Leo Davies Glenn, Lovely article by Bill Benedict in the last RVator will answer your question in a way that will make you buy one. Leo >--> RV-List message posted by: Glenn & Judi <flyers@anet-chi.com> > >Hi, > >I have recently heard of a normally aspirated, fixed pitch RV that was >equipped with a manifold pressure gauge. > >Until now, a MP gauge is something I have only seen on aircraft equipped >with a constant speed or variable pitch prop. > >Has anyone else seen this who might be able to explain how it is used on >a normally aspirated fixed pitch engine? > >Thanks in advance, >Glenn Gordon > > ________________________________________________________________________________
Date: Jun 01, 1997
From: chester razer <crazer(at)egyptian.net>
Subject: RMI Micro Monitor
--> RV-List message posted by: chester razer Just finished wiring up Micro Monitor, Initially monitor showed only zero's. Trouble shot system and isolated wiring to Manifold Pressure Transducer Finally got system to display and calibrate by eliminating signal ground conductor on Manifold pressure transducer. Wiring diagram definitely shows using this third conductor. . Currenly only have 5.12 volt supply conductor and signal conductor hooked up. Anybody else have this problem -- Chet Razer crazer(at)egyptian.net ________________________________________________________________________________
From: Lothar Klingmuller <lothark(at)worldnet.att.net>
Subject: Re: Rvator
Date: Jun 01, 1997
--> RV-List message posted by: Lothar Klingmuller >--> RV-List message posted by: JamesCone(at)aol.com >I was pleased to see my plane and instrument panel in the Rvator SNIP Having seen Jim's plane in the building stage, I am pleased he now wears the RV smile and has joined the lucky flying force! Jim, what about a CLEAR photo ( one where EVERY instrument can be deciphered) of your instrument panel in your next edition of VAN'S AIR FORCE, TRI-STATE WING? > It is Van's Air Force, Tri-State Wing Newsletter, incorporating the Midwest >RVator. It really isn't a local newsletter, and is dedicated to helping you >build your RV better and easier while avoiding the mistakes that others have >made who are ahead of you in construction. Many people, including Tony >Bengelis, have told me that it is one of the best newsletters around. If you >are interested, subscriptions are $5.00 per year, which just covers my costs. > >Jim Cone, Editor >Van's Air Force, Tri-State Wing Newsletter >jamescone(at)aol.com All RV-List: If you don't subscribe to Jim's newsletter, you are missing out! Jim has the knack of good, clear writing And writes about mistakes made so hopefully we will learn from these. All of my issues are marked up for future reference. Lothar* Klingmuller | lothark(at)worldnet.att.net | Denver (303) 922-2329 h & FAX ||6A: continueing w/ fuse'ge when garage is build || *(pron'd: "low-TARR") ________________________________________________________________________________
From: Mitch Faatz <mfaatz(at)sagenttech.com>
Subject: RV-6 vs RV-6A
Date: Jun 01, 1997
--> RV-List message posted by: Mitch Faatz >>--> RV-List message posted by: Jerry Springer >> >Well Jim I don't want to get into a pissing match with you on the list.. ><..followed by a pissing match, of course> >>you say that the -6A is is easier by a long shot you are just plain >>wrong, it may be easier for you to land and take off a tri-gear but that >>does not mean that that is so for the rest of us. The -6 is one of the >>easiest taildraggers there is to land and take off. Please separate these two issues. 1) Tricycle gear aircraft were invented because, and remain to be, a little bit more foregiving on the landing because of the CG. Visiblity during taxi is just a nice side benefit. I think everyone should take some hours in a taildragger to really drive home all the forces in motion during a landing. Then choose the configuration which meets your mission. 2) You are a man among pilots, and should paint HUGE testicles on your verticle stabilizer to show everyone. Just kidding Jerry, but you need to relax a little. Do you sneer at F-16's because they aren't tail draggers? I have to laugh when I hear people say things like "everybody just *knows* that taildraggers look sexier!". Yeah, and if you're wife isn't a brunette, you shouldn't take her out in public! ____________________ Mitch Faatz, San Jose CA RV-6AQME, finishing flaps and fuel tanks, ruffling people's feathers. ________________________________________________________________________________
Date: Jun 01, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: RE: RV-6 vs RV-6A Humour
--> RV-List message posted by: Dave Barnhart Real pilots not only *fly* taildraggers, they do carrier landings in them ;-) Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
Date: Jun 01, 1997
From: David Fitzgerald <theredbaron(at)earthlink.net>
Subject: RV-6 vs RV-6A
--> RV-List message posted by: David Fitzgerald You guys really should grow up. >--> RV-List message posted by: Mitch Faatz > >>>--> RV-List message posted by: Jerry Springer >>> >>Well Jim I don't want to get into a pissing match with you on the list.. > >><..followed by a pissing match, of course> > >>>you say that the -6A is is easier by a long shot you are just plain >>>wrong, it may be easier for you to land and take off a tri-gear but that >>>does not mean that that is so for the rest of us. The -6 is one of the >>>easiest taildraggers there is to land and take off. > >Please separate these two issues. > >1) Tricycle gear aircraft were invented because, and remain to be, >a little bit more foregiving on the landing because of the CG. >Visiblity >during taxi is just a nice side benefit. I think everyone should take >some >hours in a taildragger to really drive home all the forces in motion >during >a landing. Then choose the configuration which meets your mission. > >2) You are a man among pilots, and should paint HUGE testicles on >your verticle stabilizer to show everyone. Just kidding Jerry, but you >need to relax a little. Do you sneer at F-16's because they aren't tail >draggers? > >I have to laugh when I hear people say things like "everybody just >*knows* that taildraggers look sexier!". Yeah, and if you're wife isn't >a brunette, you shouldn't take her out in public! > >____________________ >Mitch Faatz, San Jose CA >RV-6AQME, finishing flaps and fuel tanks, ruffling people's feathers. > > > Talk Soon, Dave ----------------------------------------------------------------- RV-8 Builder Serial #80333 ----------------------------------------------------------------- ________________________________________________________________________________
Date: Jun 01, 1997
From: Dave Barnhart <barnhart(at)A.crl.com>
Subject: Re: fuel injection
--> RV-List message posted by: Dave Barnhart Tom: >I am close to purchasing a used engine for my new project and the bendix >fuel control needs to be rebuilt. Does anyone have any opinions on getting >the bendix rebuilt vs. buying a new airflow performance unit? It would seem >that the cost is about the same. Would I be able to use the same flow >divider and injectors? Thanks in advance The airflow performance folks quoted me $250-$400 to overhaul my Benix servo. I can't imagine that you can actually buy a new airflow performance unit for that. Best Regards, Dave Barnhart rv-6 sn 23744 N601DB installing electrical and avionics ________________________________________________________________________________
Date: Jun 01, 1997
From: "Louis E. Smith Jr." <lsmith(at)coastalnet.com>
Subject: Re: fuel injection
--> RV-List message posted by: "Louis E. Smith Jr." >--> RV-List message posted by: Tom Martin > >I am close to purchasing a used engine for my new project and the bendix >fuel control needs to be rebuilt. Does anyone have any opinions on getting >the bendix rebuilt vs. buying a new airflow performance unit? It would seem >that the cost is about the same. Would I be able to use the same flow >divider and injectors? Thanks in advance > >Tom Martin >RV-4 > > Tom, Don at Airflow Performance overhauled my bendix fuel control for $250.00. He also overhauled my flow divider for $60.00. This work was done in January of 97. Regards, Louis Smith lsmith(at)coastalnet.com Rocky Mount, NC RV-8 #80126 N801RV reserved RV-4 #2844 N102LS sold ________________________________________________________________________________
From: RV4Brown(at)aol.com
Date: Jun 01, 1997
Subject: Nutplate Question
--> RV-List message posted by: RV4Brown(at)aol.com I am looking for alternatives in attaching k1000-08 nutplates to thin material i.e. less than .032 where machine countersinking the base material is impractical. Assuming you have to dimple the base material this poses the question as to what to do with the dimple protruding out the backside ? This situation is encountered numerous times in the floor and baggage area on the RV4. Does anyone manufacture a nutplate with countersunk attachment holes with the same spacing as a normal K1000 nutplate? If so, what is the part number and where on the big blue marble might one look to find. Other alternatives I have considered: Adding a thick doubler plate under the nutplate. The doubler would be machine countersunk to accept the dimple from above. This works but adds mass and is time consuming. Attempting to use brute force and dimple the steel ends of the nutplate. This is hard on the dies and the results are not of the quality I would like. Any other alternatives? What did the oldbies do? Tom Brown RV4 fuselage in jig, fitting floors ________________________________________________________________________________
Date: Jun 01, 1997
Subject: Re: Rvator
From: ab6a(at)juno.com (ALLAN E POMEROY)
--> RV-List message posted by: ab6a(at)juno.com (ALLAN E POMEROY) writes: >--> RV-List message posted by: JamesCone(at)aol.com snip> I wish that >some of >the subscribers who have written me about my newsletter would have >send a >copy of their praise to the RV list. I work very hard to produce a >newsletter that is helpful and entertaining. Thanks for the >opportunity to >toot my own horn. > >Jim Cone, Editor >Van's Air Force, Tri-State Wing Newsletter >422 Savannah Ridge Drive >St. Charles, MO 63303 >jamescone(at)aol.com > Jim Cone produces a fine newsletter with lots of good information for us RV builders. At $5 for a year, it is a hard value to beat. Jim is also VERY prompt in his replies to customers. A lot of businesses could take lessons from him on how to keep customers happy. Just read his newsletter and gain more information about the aircraft we are building to help make it a bit easier. Allan Pomeroy CNY AB6A(at)juno.com HS, beginning skinning ________________________________________________________________________________
Subject: Re: Engine acquisition
From: ebundy(at)juno.com (Ed Bundy)
Date: Jun 01, 1997
--> RV-List message posted by: ebundy(at)juno.com (Ed Bundy) >Another new guy question: Since conventional wisdom has it that >inactivity is not good for an engine, how do you who know feel about the idea of >buying a freshly overhauled (or new) engine for a project that won't be >completed for a few years? What is involved in storing an engine long term? What >needs to be done to "un-store" it when the airplane is ready for it? Would this >all be worth the trouble or would it be better to just buy the engine when >it's needed (at the new, higher price)? I know people do this, but I would avoid it at all costs. There is excellent material on this subject in Tony Bingelis' book "Firewall Forward". I would strongly recommend you buy this (and ALL of his other) book(s). He generally frowns on the practice, and states also "A well used aircraft engine will survive storage or inactivity better than a newly majored engine... newly honed cylinder walls can show signs of rust in JUST A FEW DAYS (emphasis mine) if precautions aren't taken. If the engine is PROPERLY preserved, it might be okay. However, the Lycoming approved process is lengthy and uses ingredients that are hard to find locally. Even with that, Lycoming only guarantees it for 6 months. There must be a reason... I tend to be very cautious about things relating to the most important and expensive piece of the airplane. Ed Bundy RV6A - first flight 11/20/96 ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
Date: Jun 01, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: RV-8 Tilt Canopy?
--> RV-List message posted by: Bill Benedict >--> RV-List message posted by: MAlexan533(at)aol.com > >I own an RV-4 and am contemplating building an RV-8, mostly because I need a >project! My question is, is the RV-8 available with the standard RV-4 type >tilting canopy? I sat in the RV-8 at Sun n Fun, and I love everything about >the plane except the big roll bar going across my field of vision. This bugs >the heck out of me, as I'm used to having unrestricted visibility in the >RV-4, and I feel it is very important for safety reasons. Also it is simpler >to build, and lighter to go with the tilt canopy. Another question; Has >anyone finished their RV-8 tail kit yet? If so, how long did it take you? If >you built an RV-4 before, what time-savings would you estimate is attained >due to pre-punched parts? Thanks! > MAlexan533, When Van started on the RV-8, he planned on both a sliding and a tip-over canopy. To date, we have only developed the slider. I don't know if we will follow through with the other canopy, but even if we do, I think the roll bar and fixed windscreen will remain. In the event of the loss of a canopy, he wants the windscreen to be there to keep from filling your cheeks with air. So, don't base your decision on a tip-over canopy like the -4, because I don't think it will appear. I haven't built an -8 emp, but I have heard of 2 people working 7 days to complete one (maybe 1.5 people, 8 hours/day, 7 days), another took 68 hours, less fiberglass. It is quite a bit less that the previous kits. Bill Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 01, 1997
Subject: Re: RV-6 vs RV-6A
--> RV-List message posted by: Vanremog(at)aol.com << I have to laugh when I hear people say things like "everybody just *knows* that taildraggers look sexier!". Yeah, and if you're wife isn't a brunette, you shouldn't take her out in public! >> Nicely said, Mitch. Would you like to buy some pictures of your wife? Just kidding. After looking at both the 6 and the 6A at dozens of airshows, I just had to admit that they both looked great, either way. That is, unless they were painted with a mop. Then they both looked like crap. I have far more hours in taildraggers than in trigear but I am building a 6A because I like it. I know I run the risk of my flyboy buddies not thinking me the godly stud I am, but who cares, really? -GV ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 01, 1997
Subject: Re: Accomodating Instrument Placement
--> RV-List message posted by: Vanremog(at)aol.com << I suspect that you are not the first person to notice this. I am at the stage of contemplating the area behind the panel and wondering what it is save to remove. Several of the IFR 6As that I have seen have swiss cheese like arrangements of both these ribs and the bulkhead immediately forward of the panel. I have not seen much comment on this from any source and would be delighted to hear from the completed builders how they coped with these restraints. >> Leo- I used CAD to optimize the position of everything on the panel with the bracing just as the plans show. With clever manipulation and placing the shorter instruments in certain places, you can make a nice balanced appearing panel. I have full gyros and all the goodies except Stormscope. They can fit but you have to define well the "keep out areas". If you wish the .DWG file I can send it to you. -GV ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 01, 1997
Subject: Re: Pondering the essential bus concept
--> RV-List message posted by: Vanremog(at)aol.com << In attempting to adopt this design, however, I'm finding that nearly my entire electrical system ends up on the "essential" side of the essential/non-essential sheet. I'm considering using a single bus, but providing an alternate feed path (switched and fused, of course) to the bus that avoids the battery contactor. In the event of battery contactor failure I would switch on the alternate feed path. In the event of alternator failure (as annunciated by my electronic engine monitor which also monitors bus voltage) I'd simply shut off all non-essential loads (as dictated by my needs at the time) and land as soon as practical. Any comments on this idea? >> Tim- I too liked the theory of separating out the essentials from the non-essentials, however I felt that depending on the circumstances of an incident/accident/failure/whatever the definition of essential might change. For example: 1) At night in crowded complex airspace your strobe/position lights might be essential to making you visible, if only for the few seconds you need to switch them on. How about using landing lights for the last 30 seconds of the approach? Would they be essential or not? 2) If you had to go thru a cloud layer at night to land you might need your wing leveler/autopilot to help you for a minute or so. At that moment is it essential or not? 3) I have the VM1000 telling me the electrical system usage and engine status. Is it essential or not? 4) In icing conditions you might need the heated pitot/static in a pinch. Would you consider it essential or not? 5) A transponder might help ATC find you at night in unfamiliar territory and help steer you to the nearest pea patch. Is it essential to succesful completion of the flight or not? 6) I have a KLX-135A and you can't separate the power to the GPS from the power to the comm, so if the comm is essential to declare an emergency, the GPS goes along for the ride, or they both are non-essential if you know where you are and don't need to talk to anyone. 7) What about your boost pump on a hot day in Gila Bend and you have to go around? Is it essential or not. What about power to the fuel gauges? E or NE? ad nauseum, but you get the idea. I once read a Marketing Engineer for Bell Helmets saying "Show us the accident and we will design an effective helmet for it". He was commenting on the difficulty of making all the necessary tradeoffs in design requirements based on a wide array of possible causal factors without knowing the specific details of a given accident. Make it too thick and the head might be crushed because transmissibility is too high, make it too thin in the wrong area and it might not protect against point pressures and the head might be crushed, make it too heavy weight and the neck might be broken. It occurs to me that we have the same situation here. I consider Bob Nuckoll's non-essential/essential bus split with diode isolation to be a great concept, and I do believe that a two battery system is necessary for redundancy for ships with electronic ignition, however, I am not yet ready to commit to what IS and what IS NOT essential in an aircraft with conventional magneto ignitions, without knowing under what the circumstances a given failure occurs. I can turn off the non-essentials myself within 5 seconds of seeing the low volts light come on and with a 25Ah RG battery I will not have a problem maximizing the use of the remaining energy to the sucessful completion of my flight. I do not need an essential bus. What I have is a managable main bus. The greater the degree of systems integration, the more difficult it becomes to realize the clear divide between "essential" and "non-essential" functions. Further, I like to use a pullable 50A circuit breaker left normally open and tucked away just under the panel to be my Master Bypass in case the Master contactor dies. This will support all loads except starter. I consider what Bob Nuckolls is doing to be a great service to all builders and he has been very supportive and generous with his time, CAD files and expertise. The Aeroelectric Connection is must read material for anyone contemplating building an aircraft. I also know that a little professional disageement is healthy once you have an understanding of the circuits Bob has presented and why they are designed as they are. -Gary VanRemortel ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: Re: Nutplate Question
Date: Jun 01, 1997
--> RV-List message posted by: "Dennis Persyk" Tom, I followed the Frank Justice method of dimpling the nutplates. I found this satisfactory using either my Cleveland or my Avery dies. I also always use the smaller NAS rivets for nutplates so that a couple of twists of the deburring tool gives me the required countersink depth. Dennis 6A fuselage in jig ---------- > From: aol.com!RV4Brown(at)matronics.com > To: RVList(at)matronics.com > Subject: RV-List: Nutplate Question > Date: Sunday, June 01, 1997 8:02 PM > > --> RV-List message posted by: RV4Brown(at)aol.com > > I am looking for alternatives in attaching k1000-08 nutplates to thin > material i.e. less than .032 where machine countersinking the base material > is impractical. Assuming you have to dimple the base material this poses the > question as to what to do with the dimple protruding out the backside ? This > situation is encountered numerous times in the floor and baggage area on the > RV4. > Does anyone manufacture a nutplate with countersunk attachment holes > with the same spacing as a normal K1000 nutplate? If so, what is the part > number and where on the big blue marble might one look to find. > Other alternatives I have considered: Adding a thick doubler plate under > the nutplate. The doubler would be machine countersunk to accept the dimple > from above. This works but adds mass and is time consuming. > Attempting to use brute force and dimple the steel ends of the > nutplate. This is hard on the dies and the results are not of the quality I > would like. > Any other alternatives? What did the oldbies do? > > Tom Brown RV4 > fuselage in jig, fitting floors ________________________________________________________________________________
Date: Jun 01, 1997
From: Ronald Vandervort <rvanderv(at)linknet.kitsap.lib.wa.us>
Subject: Re: Accomodating Instrument Placement
--> RV-List message posted by: Ronald Vandervort Regarding instrument interference behind panel; Lower the major six instruments and put the switches and small stuff at the top. It seems to be working for me on my mockup at least. Ron Vandervort, RV-6Q on instrument panel and canopy ________________________________________________________________________________
Date: Jun 01, 1997
From: Thomas Velvick <tvelvick(at)caljet.com>
Subject: Re: RE: RV-6 vs RV-6A Humour
--> RV-List message posted by: Thomas Velvick >--> RV-List message posted by: Dave Barnhart > >Real pilots not only *fly* taildraggers, they do carrier landings in them ;-) Well, my tail is dragging from all the late hours I am spending in the garage and I do plan to carry her. My question is, if I decide to go with a 6a instead of a 6, will you still let me come over and drool over your N601DB again? Regards, Tom Velvick tvelvick#caljet.com ________________________________________________________________________________
Date: Jun 01, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Re: Nutplate Question
--> RV-List message posted by: Bob Skinner > I am looking for alternatives in attaching k1000-08 nutplates to thin >material i.e. less than .032 where machine countersinking the base material >is impractical. Assuming you have to dimple the base material this poses the >question as to what to do with the dimple protruding out the backside ? This >situation is encountered numerous times in the floor and baggage area on the >RV4. >Tom Brown RV4 Tom, There are two different methods that I've used. One is to dimple the nut plates. This is easily done with either the Avery "C" tool or a pnuematic squezzer. You may have to "relieve" the female die a bit for clearance. The other method is simply to set the nutplate on top of the dimples. This, of course, leaves a little space between the nutplate and the sheet but whether the nutplate sits high or flush, the shear force on the attach rivets is the same, right? I'm bias towards dimpling the nut plate as the nesting of the dimples helps keep the threaded part of the nutplate lined up with the drilled hole. Bob Skinner RV-6 BSkinner(at)navix.net ________________________________________________________________________________
Date: Jun 01, 1997
From: Steve Colwell <colwell(at)innercite.com>
Subject: Re: Engine acquisition
--> RV-List message posted by: Steve Colwell Tim Bronson wrote: > > --> RV-List message posted by: Tim Bronson <70773.2700(at)CompuServe.COM> > > Hi Folks: > > Another new guy question: Since conventional wisdom has it that inactivity is > not good for an engine, how do you who know feel about the idea of buying a > freshly overhauled (or new) engine for a project that won't be completed for a > few years? What is involved in storing an engine long term? What needs to be > done to "un-store" it when the airplane is ready for it? Would this all be > worth the trouble or would it be better to just buy the engine when it's needed > (at the new, higher price)? > > Thanks. > > Tim Bronson, planning in Pittsburgh


May 26, 1997 - June 01, 1997

RV-Archive.digest.vol-cx