RV-Archive.digest.vol-hl

December 03, 1999 - December 07, 1999



      >68"x 78-80" prop for an RV-4 with 150hp.  I see Thomas McIntyre advertise
      >his prop as a good 230mph RV3 cruise prop with only a 71" pitch - he flew
      it
      >so it must work, but how?  Are there big differences in the way prop makers
      >determine pitch?
      >
      >Pat Perry
      >Dallas, PA
      
      Pat:  There are significant differences in the way prop pitches are measured
      and Sensenich props do not compare numerically with others.  I had a 68-78
      Sens wood on my 160hp -4 and it was not enough prop.  With 150hp they are
      probably about right.  As far as the 230mph RV3, ask what rpm the speed was
      achieved at.  At reasonable advance ratios it was probably turning somewhere
      between 3000 and 3300.  If so, one might see 180-190 at 2700 in a -4.  The
      first two sentences in the above are from my experience.  The rest is
      conjecture, but springs from my own observations.  Perhaps there is
      something else happening in the case of the RV-3.  I would suggest you find
      people with props like the ones you are considering and ask for specific
      performance information.
      
      Gordon Comfort
      N363GC
      
      
      
________________________________________________________________________________
Date: Dec 03, 1999
From: Dennis Brown <glide303(at)southwind.net>
Subject: Re: Prop pitch confusion
Yes, there is no agreed, iron-clad way to measure pitch between manufacturers. Some, maybe most, measure from the flat underside of the blade at .7 radius. One of the biggest errors is to assume that less pitch means less speed. You can get more speed out of less pitch. You just run at full throttle and several hundred rpm above red line. This gives you the advantage of more power. The limit is where the engine self destructs or its life is measured in tens of hours. Most of us will not accept normal operation above red line, so we come back on the throttle with a low pitch prop. Speed for a given airplane depends on power. It doesn't care what the pitch values are stamped on the blades. Some props are a percent or two more efficient than others and they may indeed be a "fast" prop. Dennis Brown At 03:16 AM 12/4/99 GMT, you wrote: > >I don't get it, I'm just starting to look for a prop for my plane and I >can't seem to get the picture on how to pick the right pitch. I looked up >the prop spec on Sensenich's wood prop web site and found they recomend a >68"x 78-80" prop for an RV-4 with 150hp. I see Thomas McIntyre advertise >his prop as a good 230mph RV3 cruise prop with only a 71" pitch - he flew it >so it must work, but how? Are there big differences in the way prop makers >determine pitch? > >Pat Perry >Dallas, PA >RV-4 fuse almost done >Engine being rebuilt >I need a prop! > > ________________________________________________________________________________
Date: Dec 03, 1999
From: Hal Kempthorne <kempthorne(at)earthlink.net>
Subject: Re: [Fwd: Flaring Tool]
Do you have your own special definitions for terms like "stress" and "strain"?? hal > > So are there good reasons NOT to use steel fuel lines that I, in my > > inexperience, am simply not aware of? > >I am no expert in aircraft design, but I can think of two good reasons: 1) >airplanes use aluminum fuel lines - be extremely careful in changing >anything from "standard" aircraft design, and 2) as the airframe moves >under stress, strain is imparted to the fuel lines. Steel lines will see 3 >times the stress loads as aluminum when deflected the same amount. Good >enough reasons for me. > >Alex Peterson >Maple Grove, MN 6A > > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Dec 03, 1999
Subject: Re: Prop pitch confusion
In a message dated 12/3/99 7:47:58 PM Pacific Standard Time, pperryrv(at)hotmail.com writes: << I don't get it, I'm just starting to look for a prop for my plane and I can't seem to get the picture on how to pick the right pitch. I looked up the prop spec on Sensenich's wood prop web site and found they recommend a 68"x 78-80" prop for an RV-4 with 150hp. I see Thomas McIntyre advertise his prop as a good 230mph RV3 cruise prop with only a 71" pitch - he flew it so it must work, but how? Are there big differences in the way prop makers determine pitch? >> Yes. Pitch is not necessarily measured at the same station, the amount of blade twist is different, the blade chord and tip configurations vary. Some blades are straight, others curved (scimitar) to obtain certain pitch characteristics at different torsional loadings. About the only similarity between props from different manufacturers that fit on the same engine is bolt circle diameter. -GV ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: [Fwd: Flaring Tool]
Date: Dec 03, 1999
> I fail to see why a steel line would be subjected to more stress than an > aluminum line. See very few aluminum springs. Most automotive fuel lines > are steel. Injector lines for aircraft under high pressure are steel. A > simple loop in a line relieves most any destructive stresses. Where there is > a lot of movement, flexible hoses are placed inline even with aluminum. >Cy Galley - Editor, B-C Contact! If you deflect a steel line the same amount as an aluminum one, the steel one will have three times the stress as the aluminum one. This is because the elastic modulus of steel is three times that of aluminum. I make no claims to whether or not this is significant, just that it is a fact. For example, if some portion of the airframe moves .030" during flight, and there is a line attached to it, the steel line will undergo three times the stress (probably insignificant in either case). If the steel line has three times the fatigue strength than the aluminum, there is equivalence. I suspect that in most aircraft applications, it would not matter from this viewpoint. Alex Peterson ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: [Fwd: Flaring Tool]
Date: Dec 03, 1999
> Do you have your own special definitions for terms like "stress" and "strain"?? > > hal No, just the classic ones. Strain is the physical amount something is deformed. For example, if a 100 inch long wire is stretched 1/2", the strain is 1/2 divided by 100, which equals .005, or .5%. Stress is force divided by area. Strain times elastic modulus equals stress. Each material has its own elastic modulus. The elastic modulus of aluminum is about 10,000,000 psi. Steel is about 30,000,000 psi. These numbers for modulus do not vary significantly with different alloys/strengths of the materials (high strength steel has the same modulus as low strength steel, a surprising fact). What these relationships tell us, is that for the same deflections (strain), steel has three times the stress as aluminum. As the airframe deflects, the steel lines attached to it will undergo three times the stress as an aluminum one will. I'll crawl back into my engineering hole now, and quit stirring the pot :>) Alex Peterson ________________________________________________________________________________
Date: Dec 03, 1999
From: Fred Kunkel <rvator(at)earthlink.net>
Subject: Flaring Tools - The Final Answer
On page 127 of the 5th edition of the Standard Aircraft Handbook (available from Van's & others), it states: "The flaring tool (Fig. 6-8) used for aircraft tubing has male & female dies ground to produce a flare of 35 to 37 degrees. Under no circumstances is it permissible to use an automotive flaring tool that produces a 45-degree flare". The only thing I can't find in Chpt. 6, Aircraft Plumbing, is the question of whether or not it is permissible to mix steel, stainless steel, or aluminum fitting with the different types of fluid lines, but I guess the guidelines for which type of lines to use in particular applications addresses that question. I was wondering, just out of curiosity only, if there is any type of dialectric (sp?) corrosion that occurs as a result of mixing the different materials in the same application. Shouldn't safety of flight be our primary consideration? Blue Skies! ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Dec 04, 1999
Subject: Re: strobe positon question
In a message dated 12/3/99 8:34:34 PM Pacific Standard Time, Bobpaulo(at)aol.com writes: << if i install perturbing wing tip strobe/position lights, a tail strobe/postion light (in lower part of rudder), and a belly strobe, must i have additional strobe on top of fusel. or on vert stab??? >> IMO, start with the Whelen provided guidelines in the ACS catalog. Although it has been pointed out ad nauseum that the FAR 23 requirements do not apply to Experimentals, I agree with Das Fed that they are probably a good foundation for discussion. A protruding strobe on each wing tip is probably sufficient for the desired coverage. A white tail position light is needed unless the wing tip fixture rear lamps converge within a certain distance (1200ft?) of the rear of the a/c. Just try to glean the intent of the rules, use good common sense and check with your local builders to see what Das Feds in your area are buying off. -GV ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Re: New Site: SourceRV.com!
Date: Dec 03, 1999
> I have decided to try it out for one reason alone. Drawing revisions are > available as soon as they are approved by Van's. I must confess that I have > a lot of trouble understanding why anyone building any RV would not take > advantage of every source of information available. There have been enough > complaints about the construction manual that I'm surprised that everyone > isn't jumping on this opportunity to improve the quality of construction > information at what I would consider a very nominal cost. Van's couldn't > provide this level of support at the same cost for many reasons, including > legal considerations. Flame away. > > Steve Johnson > RV-8 #80121 Steve, Flame? Sorry, I completely agree, and have already signed up myself already. $24/yr is a steal for access to this kind of information. Randy Lervold RV-8, #80500, finish kit www.pacifier.com/~randyl Home Wing VAF ________________________________________________________________________________
Date: Dec 03, 1999
From: Michael McGee <jmpcrftr(at)teleport.com>
Subject: Re: RV-List Digest: Vortex Generators: a RV4 pirep
Extra thanks for the write up on VG's. One of the things I had a hard time getting used to was the landing speed on my RV-4. I was used to landing a Cessna with NO flying speed left so I apent 20 hours learning how to not land on the tailwheel with the mains still a foot off the ground. So, my question is: How did the VG's affect your landing speed and attitude? (This may be obvious but it's late, I've had two glasses of wine and my fingers are typing faster than my brain). Thanks again, Mike RV-4 N996RV >___________________________________________________________________________ _____ >From: Mark Todd <motodd(at)pol.net> >Subject: RV-List: Vortex Generators: a RV4 pirep > > >The archives have several inquiries about vortex generators (VG's) but I >couldn't find any responses that gave an actual report on how they >affected their RV. I thought the RV-List might be interested in what >I've learned about the effects of VG's that I temporarily put on my RV4. > ________________________________________________________________________________
From: "Jeremy Benedict" <list(at)infoav.com>
Subject: Re: New Site: SourceRV.com!
Date: Dec 03, 1999
--> RV-List message REALLY posted by: , not the above! I encourage anyone interested in RV aircraft to read this... > Sounds to me like this crew is trying to con-in on a look-alike RV List for a > profit...Jim Brown, NJ, RV- 3 Dear Jim: I am deeply troubled by your public accusation about my intentions and this new venture. I'd like to present a little background on the subject to help inform you and anyone who might share your feelings about SourceRV.com. The web site in question was developed to provide an optional, value-added service to those interested in RV aircraft. My background is quite extensive in RVs and Van's Aircraft. I have been Van's Webmaster for the past 4.5 years, and have done a host of other things for Van's including spending countless hours helping to prepare RVators and Accessories Catalogs, sweating in yellow tents at various fly-ins, etc. Most of the work I have done has not really been "work", but rather my time volunteered to the RV and Van's cause...I don't work for Van's and I never have. I hesitate to think of how much time I've "volunteered"; I often question whether the 1000+ hours of time would have been better spent on things like my career and my life. During the past decade, I've heard from many RV builders and pilots. I've been subscribed to the rv-list since 1994. I've read the 1,500 comments submitted about Van's web site. I've talked to hundreds if not thousands of RV enthusiasts, builders, and pilots throughout the country and the world. I know Van's operation and product fairly well. Through all this interaction, one thing has become very clear. People want more information and resources. Much more. The options for providing what people really wanted were quite limited. It was too much of a resource commitment for Van's, so after five months of consideration last spring, Van's agreed to support in principal (not $$) the ideas I had. I've formed a company, InfoAv, to develop and present these ideas. Stated again, I've developed a service to present information that people told me they wanted. Isn't this somewhat consistent with the ideas of capitalism and the free market economy in this country? I seem to recall the story of a young man in the 1970s who designed and built his own airplane. Soon after others flew his airplane, they desired, they asked, they wanted to have this airplane. In response to their pressure, not because he was trying to make a buck, this young man made his airplane available. Like this young man, Richard VanGrunsven, and his airplane, the RV-3, I have developed SourceRV.com because people have told me they wanted this. It is my full intention to continue in the tradition of Van by producing quality products at very reasonable prices. You claim that I'm trying to "con-in...for a profit." I have to ask, do you work for free? Probably not. Most people I know get paid to work at a job, and have expenses to pay. I'm no different. Only my job now is to produce the services I've mentioned above. Will I make a profit? I hope so...much in the same way that your "profit" probably comes in the form of a paycheck. Now, there will be no Gulfstreams flying around with "SourceRV.com" written on the side. You can do the math. The revenue generated from SourceRV.com won't even be sufficient to solely support a full-time position. It is only through working on several additional projects that I can put bread on the table, and maybe even take in an EAA pancake breakfast here and there. Perhaps it would be wiser to completely drop out, forget about what people want, give up on Van's site, and go back to the computer industry. But that's not what I want and not what others have told me they wanted. I think it would be great to make SourceRV.com free. I've analyzed different potential revenue models. When it comes down to it, the web site has to generate income. I think it has been positioned in the best way possible given the requirements and circumstances. You may have noticed one benefit of my decision already...Van's web site went from a deteriorating condition to new, active, and updated almost daily. Soon to come will be a new Accessories Catalog and on-line ordering with cool things like order tracking. Without the development of InfoAv, Van's web site likely would have been seriously downsized or closed altogether. This past fall, I've mentioned what I am doing to a number of people. So far, everyone has been positive, expressing interest in the idea. Many reactions have been very enthusiastic. People have understood that the resources (aka money) to develop the site _have_ to come from somewhere. If you still feel the same about SourceRV.com, then the best thing to do is simply not subscribe. Trying to influence everyone's opinion is not productive for anyone. I want to make clear that I'm not trying to recoup what I've given in the past. My focus is on the future and trying to produce and provide what people want. Sincerely, Jeremy Benedict jeremy(at)infoav.com InfoAv Corporation ________________________________________________________________________________
From: JHeadric(at)aol.com
Date: Dec 04, 1999
Subject: Re: Prop pitch confusion
Pat- The first number on a prop is the diameter in inches. The second number is how many inches forward the prop (and attached airplane) will move in one revolution thru a semi-solid substance such as butter or some other theoretical stuff. All prop manufacturers SHOULD be using the same identifying numbers but I guess some of them are just more accurate than others. I had a 150hp 'RV4 and used a 69x70" prop and it worked fine. Jim ________________________________________________________________________________
Date: Dec 03, 1999
From: Denton Harjehausen <harje(at)proaxis.com>
Subject: Re: Tailwheel Fairing
> >I meant to say, can anyone tell me where to get an RV tail wheel fairing? >Thanks, Chuck In case you didn't know, if you have a full swivel tail wheel the tail wheel pant won't fit without modification or a smaller wheel. I ran into this, drat! Have a great Day! Denny Harjehausen Lebanon, OR RV-6 ________________________________________________________________________________
From: Gusndale(at)aol.com
Date: Dec 04, 1999
Subject: Re: New Site: SourceRV.com!
Jeremy & listers, Thanks for your thorough and informative response to the list regarding the "con-in .... for a profit" issue. Hopefully this has put the issue to rest. Giving Jim the benefit of the doubt, he apparently didn't notice that you created Van's website and if he isn't from the Portland local area may not have been aware of the amount of volunteering you have contributed both in labor and expertise to the Van's operation. At any rate, for those of you on the list who don't know Jeremy, trust me, Jim is waaay off base in characterizing this as "con-in...for a profit". This is going to be a first rate service to the RV community. It isn't in competition with the RV-list, it's another resource. I signed up yesterday and I figure I'll recoup the $24 cost in a matter of weeks via less 'practice parts' not to mention the convenience and time saved in being able to quickly locate Rvator articles and plans revisions, etc. right when I need them. Rest assured, Jeremy, that Jim speaks only for himself. I, and I expect many others are grateful that you are providing this new service and realize that if the Gulfstream were the goal you wouldn't have chosen the RV community as your target population. Regards, Dale Wotring RV6A (working on engine hookups and panel planning) Vancouver, WA ________________________________________________________________________________
From: Bobpaulo(at)aol.com
Date: Dec 04, 1999
Subject: wig-wags
where could i find wig-wags and info to wire?? bob ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: strobe positon question
Date: Dec 04, 1999
I think you still need a strobe on the top of the plane. Don't the wing tip strobes mount in such a way that they can't be seen from above? Has anyone put a strobe on the top of the fuselage about half way between the canopy and the tail on a RV? I think that one on top of the fuselage and one on the bottom would be easy to mount and service. Steve Soule Huntington, Vermont RV-6A nose wheel fairing -----Original Message----- From: Bobpaulo(at)aol.com [mailto:Bobpaulo(at)aol.com] Sent: Friday, December 03, 1999 11:04 PM To: rv-list(at)matronics.com Subject: RV-List: strobe positon question if i install perturbing wing tip strobe/position lights, a tail strobe/postion light (in lower part of rudder), and a belly strobe, must i have additional strobe on top of fusel. or on vert stab??? thanx, bob ________________________________________________________________________________
Date: Dec 04, 1999
From: "R.James" <vtx(at)ntplx.net>
Subject: Lightening holes? or Not?
Hi all, I'm about to bore out lightening holes in the Flap Brace & Spar. And a thought popped in mind while setting up the fly-cutter.. The plans say "Optional" for lightening holes here? Is there any major drawback with leaving them solid OTHER THAN the few measley ounces of weight reduction? IE: Aerodynamic air-flow (through the holes) impedance? IE: No inner access to rivets, etc (through holes)? Thanks in advance, (fly-cutter on hold) RJ in CT ________________________________________________________________________________
Date: Dec 04, 1999
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: RV Source.com
I meet Jeremy Benedict about 4 years ago. At that time I was very impressed with his intelligence, enthusiasm, and work ethic. He was working at Van's tent at one of the major Fly-Ins. Since that time, I have seen him at many fly-ins and talked to him at almost all of them. With all the people that Jeremy has meet at the different Fly-Ins, he remembered my name this year at Van's Homecoming and I did NOT have a name badge on. Since I live on the other side of the country from Jeremy, I find this impressive. I am in southern California 5 RV flight hours away from the Pacific North Wet. This is not a typo. At the Homecoming, I spoke a little with him about his work with Intel. At that time, he wanted to start out on a new endeavor. I encouraged him that I thought he had what it takes to succeed and wished him luck. I signed up for SourceRV the first day. I have a flying RV-6 that I built and have enjoyed for 470 flying hours in the last 26 months. I do not need to spend more money for info on building RV's. I want to see Jeremy succeed and am willing to help him however I can. I know that his SourceRV is going to be the greatest success on the Internet since Amazon.com. I know he has about a half dozen RV photos that I have scanned for him. I am sure that he will have the largest collection of RV photos on the web. I would love to be remembered as paying the first dollar to Jeremy on the millions he will make in his lifetime. I believe that the info Jeremy will have on the SourceRV will be more accurate than the rest of the Internet. Anyone can say anything and he or she does. An example was a post to the RV-List that I made recently about Carb Ice. I was hoping to start a "thread" and did. There were about one dozen posts. I only asked for info that people had on flying RVs with Lycoming engines. Only 5 responses were from RVs and two came directly to me. The other ones about Cessna and Piper were not what I wanted to know. In any case, 2 out of 5 RVs have seen Carb Ice. 2 out of 5 have NEVER seen any Carb ice. One had seen Carb ice once in about as many hours as my RV has. I am one that has never seen any Carb Ice and am afraid that someday I will. This brief survey is not factual other than telling me that some day, I may have Carb ice in my RV. Over the past 4 years, I have seen Jeremy grow into young adult and only hope that the leaders of our country (and this planet) are just like him in the Twenty-First Century. I wish Jeremy a Merry Christmas and a successful New Year with his new undertaking. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, So. CA, USA ________________________________________________________________________________
Date: Dec 04, 1999
From: Mike Thompson <grobdriver(at)yahoo.com>
Subject: strobe positon question
--- "Stephen J. Soule" wrote: > > I think you still need a strobe on the top of the plane. Don't the > wing tip > strobes mount in such a way that they can't be seen from above? > > Has anyone put a strobe on the top of the fuselage about half way > between > the canopy and the tail on a RV? Careful about strobe placement and unintended results - like blinding the pilot. A strobe behind the canopy could easily reflect off the instruments/panel/windscreen at night and make your life miserable. Even tip-mounted strobes sometimes due to dihedral of the wing and placement on the tip require small fences to shield the flash from view. Mike Thompson Austin, TX -6 N140RV (Reserved) Wings ________________________________________________________________________________
Date: Dec 04, 1999
From: Mike Thompson <grobdriver(at)yahoo.com>
Subject: Re: wig-wags
--- Bobpaulo(at)aol.com wrote: > > where could i find wig-wags and info to wire?? bob I have my Gall's unit handy. What info do you need? Mike Thompson ==== Michael E. Thompson (Grobdriver(at)yahoo.com) Austin, TX, USA RV-6 in progress, N140RV (Reserved) EX-AX1 Sub Hunter, P-3 (B/B-TACMOD/C) Orion Aircrew, PP-G,ASEL, Motorglider Driver and Unlimited Air Race Nut! ________________________________________________________________________________
From: DAVENDANA1(at)aol.com
Date: Dec 04, 1999
Subject: Re: Lightening holes? or Not?
I don't remember where I read this, but one builder kept all the discarded "circles" and weighed them. He saved 8 pounds by cutting the holes when he was finished. Dave Funk They said it takes how long to build one of these????? ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Dec 04, 1999
Subject: Re: wig-wags
In a message dated 12/4/99 3:27:35 AM Pacific Standard Time, Bobpaulo(at)aol.com writes: << where could i find wigwags and info to wire?? >> A wigwag is simply an alternating relay used to pulse the landing lights. Depending on the wattage of your lamps this can be accomplished easily or with additional considerations. For the 55W Halogen bulbs Precise Flight has the Pulselite system that is a self contained flasher system. Some have used School Bus flashers from Gall's. For 100W incandescent bulbs you probably want to incorporate a relay for each lamp to reduce the switching load seen by your panel switch(es). The landing light relays I use are Mouser P/N R51-5D40-12F and are rated at 40A. I have an SSAC P/N KRD3120B adjustable rate alternating relay that is connected thru a switch to the landing light relays. The rate is set so that the filaments aren't allowed to go out between flashes. All the contact info for these sources is in my Yeller Pages. All of this shown in a complete schematic for my RV-6A done in AutoCAD Rel14. I can send you the file if you wish. -GV ________________________________________________________________________________
Date: Dec 04, 1999
From: Bob Skinner <bskinner(at)vcn.com>
Subject: strobe positon question
Steve, I would think there would be good visibility of the wing tip strobes if they are mounted on "blisters" on the wing tip. Van's now sell these in the catalog. We used the 3 position strobes on Charlie's 6A which gives you two tail lights to the rear. On my six, I used nav light only on the wing tips and a single strobe in the vert. stab. tip. The strobe in the vert. stab. tip will reflect off the wings at night. I would think a strobe on the top of the fuselage would be even worse in this regard. Bob Skinner Buffalo, WY (1995 RV6 sold after 4 years & 470 hrs) EAA Tech Counselor # 3726 > >I think you still need a strobe on the top of the plane. Don't the wing tip >strobes mount in such a way that they can't be seen from above? > >Has anyone put a strobe on the top of the fuselage about half way between >the canopy and the tail on a RV? I think that one on top of the fuselage >and one on the bottom would be easy to mount and service. > >Steve Soule >Huntington, Vermont >RV-6A nose wheel fairing ________________________________________________________________________________
Date: Dec 04, 1999
From: RV6BLDR <calverjl(at)flash.net>
Subject: Re: wig-wags
Bobpaulo(at)aol.com wrote: > > > where could i find wig-wags and info to wire?? bob > > _ Bob, Here's a post I sent a few months ago on wig-wags. At this site they have a wire diagram you can download. ****** Was looking at the latest Gall's catalog and noticed there is a new Wig-Wag flasher available. Check it out at:(Give it a minute to completely load. It will be slow at first, but once it gets going, it's really cool!) <http://www.galls.com/service/fs013.asp> For those who have been wondering what the standard Wig-Wag pattern looks like, go to: <http://www.galls.com/service/fs020.asp> Since there was a thread on the Wig-Wags last week, thought you Wig-Wag wannabes would be interested in this. Jerry Calvert Edmond Ok -6 wings ________________________________________________________________________________
Date: Dec 04, 1999
From: RV6BLDR <calverjl(at)flash.net>
Subject: Re: Lightening holes? or Not?
DAVENDANA1(at)aol.com wrote: > > > I don't remember where I read this, but one builder kept all the discarded > "circles" and weighed them. He saved 8 pounds by cutting the holes when he > was finished. > > Dave Funk > They said it takes how long to build one of these????? > He must of had the older kit that didn't have the lightning holes cut in the wing ribs and spars, etc. I don't think the lightning holes that are cut out by the builder in today's kits would weigh that much. Jerry Calvert Edmond Ok -6 wings & fuse ________________________________________________________________________________
From: BumFlyer(at)aol.com
Date: Dec 04, 1999
Subject: Re: cold
In a message dated 12/2/99 18:55:45, jkitz(at)greenapple.com writes: << I was wondering about rerouting the air that has passed through > the oil cooler that is usually mounted to the rear engine baffle bulkhead. > The air is warm and should be clean. It would be easy to attach a > fiberglass manifold to the back of the oil cooler and duct the air to the > needed locations. >> This is something I researched a little, and was discouraged from the idea by Larry Vetterman. I would also add there are some out there who use the oil cooler outlet as a pre heater for the muff heated air. Now that I have flown in the cool for a couple years I can see why this is an exercise in futility. When you need the cabin heat is precisely when the oil cooler is probably near stone cold, like your feet. I have had three hour cross countries where the oil temp never stayed above 150.. This probably means the vernatherm is still open and allowing only a dribble of oil through the cooler. Geo Orndorff recommended taking your pressure air for the muff from a low spot on the aft baffle where you can get a little radiation from the aft cylinder head. This will help a little, and the pot scrubbers may too. Having said that I will add I think for most of us the chill problem is overrated. If you only fly in the sunlight, you will find the RV-6/6A a very comfy plane even in the extreme cold because of the solar heat and the inherent warmth of the firewall area where your unsolarized feet are. i really love flying in the winter on sunny days in Colorado, including the x country mentioned above at 10,000 feet. Spend your time and energy on sealing the drafts, particularly those on the back of your neck, and in your nether regions where the stick boot is. Now for those of you who need to fly at night, or IFR or to fly in the aft of tandem airplanes with the flap actuator hole near you and a flop over canopy skirt behind your neck, I have nothing to offer. These are recreational activities which I have foregone in my advanced years. Just my $0.01 worth. D L Walsh ________________________________________________________________________________
Date: Dec 04, 1999
From: "Keith H. Wooddell" <KHWooddell(at)worldnet.att.net>
Subject: Re: LRI Group Buy
Al, My name is Keith Wooddell and I'm building an RV-8 in Cleveland, OH. I'm very interested in purchasing a LRI. Is it possible to still purchase at the group price of those that did so in November? Thank you for your help. Best Regards, Keith W. Al Mojzisik wrote: > > If you were one of the 5 people in the November LRI group buy, I just sent > out a confirming e-mail directly to you. > > So if you ordered an LRI in this current deal and do not recieve this > confirming e-mail by this evening please contact me off list. Thanks, AL > prober(at)iwaynet.net > -- Keith H. Wooddell, Applications Engineer The S. G. Morris Company 699 Miner Rd. Highland Hts., OH 44143 (440) 243-0462 (440) 243-0462 KHWooddell(at)worldnet.att.net adr: 699 Miner Road;;;Highland Heights;OH;44143;USA title: Applications Engineer tel;work: 440-243-0462 tel;fax: 440-243-0462 ________________________________________________________________________________
From: JHeadric(at)aol.com
Date: Dec 04, 1999
Subject: Re: Carb Ice
Gary- I have iced up with an RV4 a couple of times. Once, when making a long descent without carb heat, it iced up and I lost some rpm, but kept flying okay and with a little carb heat, it cleared up okay. Second time was taxiing with typical Oregon wx and by the time I did my runup, I could tell there was some ice, so I just waited until the carb heat cleared it up. Flying was okay with no icing problems. I have developed the habit of leaving carb heat on from downwind to shutdown and then to startup for the next flight and taxi out. When I do my mag check, I then cycle the carb heat off and on and then turn it off for the takeoff. I never use heat in flight, but I sure would if I felt like I was icing up. Jim RV4, RV6A and RV6A ________________________________________________________________________________
From: RVBryan(at)aol.com
Date: Dec 04, 1999
Subject: RV4 Parts
Listers, I want to thank all of you that were so kind to send any extra RV4 parts or RV4 compatible parts to me. You guys are really great and I appreciate it tremendously. Maybe this project will actually happen. My folks have said that they will foot the bill for the engine if I can maintain my grades in college and if I get this thing built. Seems like alot of incentive there. If there are any other listers out there that have any extra RV4 parts or compatible RV4 parts that are cluttering up your shop and want to help, please let me know. thanks! Bryan ________________________________________________________________________________
From: "Ed Bundy" <ebundy(at)access1.net>
Subject: Re: Lightening holes? or Not?
Date: Dec 05, 1999
There are no "other" drawbacks, but then again, some of us don't consider ANY extra weight "measly". :-) There are lots of places where you can end up ignoring a seemingly insignificant amount of weight, but it's amazing how fast it adds up. I was ruthless in my quest for light weight, and I ended up with a metal-propped 6A that weighs in at 997 lbs without exterior paint. They just fly better that way. Although I do plan on "splurging" for some paint soon. Ed Bundy - Eagle, ID - RV6-A First flight 11/20/96 ebundy@access1.net http://home.cwix.com/~ebundy@cwix.com/ > I'm about to bore out lightening holes in the Flap Brace & Spar. > And a thought popped in mind while setting up the fly-cutter.. > > The plans say "Optional" for lightening holes here? > Is there any major drawback with leaving them solid OTHER THAN > the few measley ounces of weight reduction? ________________________________________________________________________________
Date: Dec 04, 1999
From: Mark Todd <motodd(at)pol.net>
Subject: Re: Re: RV-List Digest: Vortex Generators: a RV4 pirep
Michael McGee wrote: > How did the VG's affect your landing speed and attitude? I know what you mean about the difference in landing an RV vs a Cessna 170 (my first love). I have to fly a RV on if I want a three point landing. I can't say that I see any definite difference in landing behavior with the VG's, other than getting to fly the pattern a few knots slower. It seems that I've made a few of my nicer landings since putting on the VG's (but, of course, I'd rather give myself the credit). Mark ________________________________________________________________________________
Date: Dec 04, 1999
From: Hal Kempthorne <kempthorne(at)earthlink.net>
Subject: Steel & alum tubing - was Flaring Tools
Strain is the deformation of a part caused by stress. (Roughly) I don't remember learning much about fatigue in school - maybe because I was at Mel's Happy Tavern with a bunch of the boys instead of in class! As soon as my Debonair's first annual I found that fatigue is very important in airplanes! As soon as I started building my RV I began to worry about it. I did know that if a part is deformed repeatedly beyond its elastic limit - that is, where it doesn't spring back, it will soon crack and break. I didn't realize that it will eventually break EVEN IF it is NEVER deformed beyond the elastic limit. I found out that the number of cycles of stress the part can endure before cracking varies with the material and with how close each cycle gets to the elastic limit. So, flexing of baffle parts will eventually start cracks. Many stop drills and patches have I put on my Deb's baffles drive this message home. Your RV will eventually break. If you make fuel lines of aluminum and let them flex they will eventually break. If the flexing is less than half the elastic limit, the number of flex cycles will be well over a million before failure. For landing gear legs, for example, failure after a million landings (and bounces) may be acceptable but for your crankshaft, not, since it does thousands of flex cycles per minute. So, the crankshaft is made very stiff so that the flexes are well below the limit but there is still a limit and grinding the crank undersize makes that limit more imminent. I understand that is why Lycoming does not condone grinding below .020 undersize. If you expect fuel lines to flex more than an extremely tiny amount, make them hoses. The issue I have with aluminum lines is that they nick and scratch so easily. This seems especially important where they are near your feet or open to abrasion. Production automobile fuel lines are of steel and I suspect abrasion resistance is the main reason. Lines are not commonly made up in the shop but purchased as spare parts, fully formed and terminated. The mechanic doesn't need to be trained to handle them with kid gloves while installing as she would with aluminum. Maybe I should have done my RV6A with hoses as the tubing shaping is at least 100 time more difficult than with an RV6 due to gear mounts. Hoses are now available without lifetime limitations but I suppose this was true in 1903 too. Modern materials make steel braided hoses pretty attractive tho surely costing and weighing more. Aluminum lines seems to have worked for all the other RVs. Nearly all? What are the details on the fire in flights that we have seen? Hal Kempthorne - SJC RV6a N7HK at SCK Hangar H-13 Debonair N6134V for sale ________________________________________________________________________________
Date: Dec 04, 1999
From: John Lawson <jwlawson(at)hargray.com>
Subject: Opinion on drill press
I'm looking for a decent bench-mounted drill press - Harbor Freight carries a number of them made by Central Machinery. Anyone have any opinions, pro or con, about Central Machinery products? Thanks! Semper Fi John ________________________________________________________________________________
From: GLPalinkas(at)aol.com
Date: Dec 04, 1999
Subject: Re: New Site: SourceRV.com!
Jeremy.... Don't let a few nay-sayers influence what the rest of us want. You are right. We want more information and I was one of the first to put my money where my mouth is as soon as the site accepted subscriptions. Count the subscription totals and then don't worry about a few negative comments. It was nice to hear you give us an over-view of your past efforts and future vision. You are on the right track and we wish you well. (speaking IMHO for the majority) Gary Palinkas Parma, Ohio RV6 QB finishing up control systems (finally) In a message dated 12/4/99 1:11:40 AM, list(at)infoav.com writes: << Dear Jim: I am deeply troubled by your public accusation about my intentions and this new venture. I'd like to present a little background on the subject to help inform you and anyone who might share your feelings about SourceRV.com. The web site in question was developed to provide an optional, value-added service to those interested in RV aircraft. My background is quite extensive in RVs and Van's Aircraft. I have been Van's Webmaster for the past 4.5 years, and have done a host of other things for Van's including spending countless hours helping to prepare RVators and Accessories Catalogs, sweating in yellow tents at various fly-ins, etc. Most of the work I have done has not really been "work", but rather my time volunteered to the RV and Van's cause...I don't work for Van's and I never have. I hesitate to think of how much time I've "volunteered"; I often question whether the 1000+ hours of time would have been better spent on things like my career and my life. During the past decade, I've heard from many RV builders and pilots. I've been subscribed to the rv-list since 1994. I've read the 1,500 comments submitted about Van's web site. I've talked to hundreds if not thousands of RV enthusiasts, builders, and pilots throughout the country and the world. I know Van's operation and product fairly well. Through all this interaction, one thing has become very clear. People want more information and resources. Much more. The options for providing what people really wanted were quite limited. It was too much of a resource commitment for Van's, so after five months of consideration last spring, Van's agreed to support in principal (not $$) the ideas I had. I've formed a company, InfoAv, to develop and present these ideas. Stated again, I've developed a service to present information that people told me they wanted. Isn't this somewhat consistent with the ideas of capitalism and the free market economy in this country? I seem to recall the story of a young man in the 1970s who designed and built his own airplane. Soon after others flew his airplane, they desired, they asked, they wanted to have this airplane. In response to their pressure, not because he was trying to make a buck, this young man made his airplane available. Like this young man, Richard VanGrunsven, and his airplane, the RV-3, I have developed SourceRV.com because people have told me they wanted this. It is my full intention to continue in the tradition of Van by producing quality products at very reasonable prices. You claim that I'm trying to "con-in...for a profit." I have to ask, do you work for free? Probably not. Most people I know get paid to work at a job, and have expenses to pay. I'm no different. Only my job now is to produce the services I've mentioned above. Will I make a profit? I hope so...much in the same way that your "profit" probably comes in the form of a paycheck. Now, there will be no Gulfstreams flying around with "SourceRV.com" written on the side. You can do the math. The revenue generated from SourceRV.com won't even be sufficient to solely support a full-time position. It is only through working on several additional projects that I can put bread on the table, and maybe even take in an EAA pancake breakfast here and there. Perhaps it would be wiser to completely drop out, forget about what people want, give up on Van's site, and go back to the computer industry. But that's not what I want and not what others have told me they wanted. I think it would be great to make SourceRV.com free. I've analyzed different potential revenue models. When it comes down to it, the web site has to generate income. I think it has been positioned in the best way possible given the requirements and circumstances. You may have noticed one benefit of my decision already...Van's web site went from a deteriorating condition to new, active, and updated almost daily. Soon to come will be a new Accessories Catalog and on-line ordering with cool things like order tracking. Without the development of InfoAv, Van's web site likely would have been seriously downsized or closed altogether. This past fall, I've mentioned what I am doing to a number of people. So far, everyone has been positive, expressing interest in the idea. Many reactions have been very enthusiastic. People have understood that the resources (aka money) to develop the site _have_ to come from somewhere. If you still feel the same about SourceRV.com, then the best thing to do is simply not subscribe. Trying to influence everyone's opinion is not productive for anyone. I want to make clear that I'm not trying to recoup what I've given in the past. My focus is on the future and trying to produce and provide what people want. Sincerely, Jeremy Benedict jeremy(at)infoav.com InfoAv Corporation >> ________________________________________________________________________________
From: aquila33(at)webtv.net (dann mann)
Date: Dec 04, 1999
Subject: Re: Opinion on drill press
In my opinion, Some of the Central machinery stuff is usable. If you can spring fo just a few more bucks look at the line of tools now sold by Home Depot under the Ridgid name. The quality is just fantastic. They are still Asian tools but built to a much higher standard. ________________________________________________________________________________
Date: Dec 04, 1999
From: Al Mojzisik <prober(at)iwaynet.net>
Subject: Re: LRI Group Buy
Keith, I believe I can still get you in. I am mailing the check to Jim on Monday but since you live so close to me I can cover you. Please E-mail me off list with your address and phone number and we'll exchange the details. AL PS: I am from the Cleveland area too and still visit up there. > > >Al, > >My name is Keith Wooddell and I'm building an RV-8 in Cleveland, OH. I'm very >interested in purchasing a LRI. Is it possible to still purchase at the group >price of those that did so in November? > >Thank you for your help. > >Best Regards, > >Keith W. > >Al Mojzisik wrote: > >> >> If you were one of the 5 people in the November LRI group buy, I just sent >> out a confirming e-mail directly to you. >> >> So if you ordered an LRI in this current deal and do not recieve this >> confirming e-mail by this evening please contact me off list. Thanks, AL >> prober(at)iwaynet.net >> > > >-- >Keith H. Wooddell, Applications Engineer > >The S. G. Morris Company >699 Miner Rd. >Highland Hts., OH 44143 > >(440) 243-0462 >(440) 243-0462 >KHWooddell(at)worldnet.att.net > > >adr: 699 Miner Road;;;Highland Heights;OH;44143;USA >title: Applications Engineer >tel;work: 440-243-0462 >tel;fax: 440-243-0462 > > ________________________________________________________________________________
From: "Bryan E. Files" <BFiles(at)corecom.net>
Subject: Re: Gel Cell Battery
Date: Dec 04, 1999
Bob, Doesnt the RG batteries ie Panther, have a 3psi pop vent in them that is why we can not put them inside the passenger compartment of an aircraft without a vented battery box. On the other hand the Powersonic does not have this feature since it is suppose to be a gel cell and we can put them in the cabin on a tray and not a vented box. **** Bryan E. Files **** Ever Fly Maintenance Palmer, Alaska A&P, IA, FAA Safety Counselor mailto:BFiles(at)corecom.net ----- Original Message ----- From: Robert L. Nuckolls, III <nuckolls(at)aeroelectric.com> Sent: Friday, December 03, 1999 5:11 PM Subject: RV-List: Re: Gel Cell Battery > > > > >I believe that the Powersonic is a gel cell battery. I am looking through > >my stuff. > > To a large number of people who sell batteries, > ANY battery that is sealed and doesn't slosh is > a "gel" battery. I've found a number of websites > that specifically call the RG batteries a "gel". . . > Fortunately, they're actually recombinant gas > (or starved electrolyte) construction that exhibits > cold weather cranking performance 2-4 times better > than a flooded battery and 3-6 times better than > a gel-cel. > > > Bob . . . > > ________________________________________________________________________________
From: "Zeidman, Richard B" <Richard.Zeidman(at)PHL.Boeing.com>
Subject: Skyforce Skymap II
Date: Dec 04, 1999
Have any listers tried the Skymap II in their RV's. I really like the panel mount feature with the large map, but would like to hear some comments from anyone who has actual experience with it. I am also planning to couple it to a Nav-Aid autopilot. Rich Zeidman Ridley Park, Pa RV6A finish kit working on canopy ________________________________________________________________________________
Date: Dec 04, 1999
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: bottom flap skin
Got the wings mounted on the RV4. Getting ready to set the incidence angle, etc. Went to mount the flap and have interference between the lower fuselage skin and the bottom flap skin on the fuse side. Looks like I will have to cut the bottom fuselage skin flush with the fuselage side to get enough clearance and maybe the flap skin also. Will get the plans out and study some more. Any short cuts or advice will be welcome. Thanks Earl RV4 ________________________________________________________________________________
From: "Terry Watson" <tcwatson(at)seanet.com>
Subject: Re: RV Source.com
Date: Dec 04, 1999
I'm not quite as quick to dismiss Jim's comment as out of line as some of you seem to be. While I don't agree with him, I did have some concerns along those lines. If I didn't know who Jeremy is, and that he is responsible for Van's website, including the recent excellent update, I might have the same suspicions. First, I feel a great loyalty to Matt and those of you whose posts to this list have provided so much insight to the building process, and the rewards and pitfalls of my project. Second, I have mixed feelings about paying another fee to get information that I thought I had already paid for - the drawings, Van's customer support, my Rvator subscription, and my contributions to Matt for providing this list. I also feel just a little bit like I did a couple of month's ago when Moe started an RV-8 list to replace the previous RV-8 shortlist, and then after that when Matt started all the more specific lists, including the RV-8 list. I hate to see the source of information and discussions that are vital to me to get so diffused that I miss something important. But when I went to Jeremy's site to look at what he is doing, the sample downloadable drawings were all for the RV-8, and they were revisions to the drawings that I don't believe I have seen before. Maybe I missed them in the Rvator; maybe they were never disseminated to kit owners. Regardless, it is information that I don't think I can afford to be without. I subscribed. The way I see it, Jeremy is in a unique position where he has the background, experience, and access to Vans so he can provide us with a real service. I guess I would prefer that Vans had put him on the payroll to provide what he is doing as a part of their customer service, but then the price of the kits would probably have had to increase more than what I will be paying Jeremy. Besides, Jeremy is an entrepreneur. He will make it or not, depending on whether he gives us our money's worth. From what I have seen of his work to date, I think he will do just fine. Terry Watson RV-8A wings Seattle ----- Original Message ----- From: Gary A. Sobek <rv6flier(at)yahoo.com> Sent: Saturday, December 04, 1999 6:03 AM Subject: RV-List: RV Source.com > > I meet Jeremy Benedict about 4 years ago. At that > time I was very impressed with his intelligence, > enthusiasm, and work ethic. He was working at Van's > tent at one of the major Fly-Ins. Since that time, I > have seen him at many fly-ins and talked to him at > almost all of them. With all the people that Jeremy > has meet at the different Fly-Ins, he remembered my > name this year at Van's Homecoming and I did NOT have > a name badge on. Since I live on the other side of the > country from Jeremy, I find this impressive. I am in > southern California 5 RV flight hours away from the > Pacific North Wet. This is not a typo. At the > Homecoming, I spoke a little with him about his work > with Intel. At that time, he wanted to start out on a > new endeavor. I encouraged him that I thought he had > what it takes to succeed and wished him luck. > > I signed up for SourceRV the first day. I have a > flying RV-6 that I built and have enjoyed for 470 > flying hours in the last 26 months. I do not need to > spend more money for info on building RV's. I want to > see Jeremy succeed and am willing to help him however > I can. I know that his SourceRV is going to be the > greatest success on the Internet since Amazon.com. I > know he has about a half dozen RV photos that I have > scanned for him. I am sure that he will have the > largest collection of RV photos on the web. I would > love to be remembered as paying the first dollar to > Jeremy on the millions he will make in his lifetime. > > I believe that the info Jeremy will have on the > SourceRV will be more accurate than the rest of the > Internet. Anyone can say anything and he or she does. > An example was a post to the RV-List that I made > recently about Carb Ice. I was hoping to start a > "thread" and did. There were about one dozen posts. > I only asked for info that people had on flying RVs > with Lycoming engines. Only 5 responses were from RVs > and two came directly to me. The other ones about > Cessna and Piper were not what I wanted to know. In > any case, 2 out of 5 RVs have seen Carb Ice. 2 out of > 5 have NEVER seen any Carb ice. One had seen Carb ice > once in about as many hours as my RV has. I am one > that has never seen any Carb Ice and am afraid that > someday I will. This brief survey is not factual > other than telling me that some day, I may have Carb > ice in my RV. > Over the past 4 years, I have seen Jeremy grow into > young adult and only hope that the leaders of our > country (and this planet) are just like him in the > Twenty-First Century. I wish Jeremy a Merry Christmas > and a successful New Year with his new undertaking. > > > ==== > Gary A. Sobek > "My Sanity" RV-6 N157GS O-320 Hartzell, > So. CA, USA > > ________________________________________________________________________________
From: "jim jewell" <jjewell(at)okanagan.net>
Subject: Lightening holes? or Not?
Date: Dec 04, 1999
Hello R James: Having read some comments regarding cracks etc. in the area of the flap brace and spar areas, I chose to put fewer holes in the flap spar and none in the flap brace. The few ounces this choice represented (near C/G ) are not an issue with me. I have however tried to avoid adding any weight to this project. On assembly I did not find any need for access to rivets as a problem I don't foresee any aerodynamic difficulties comming into play, I'm no expert on aerodynamics so I'll stand to be corrected on this. Jim in Kelowna BC. 6-A, fitting stuff inside fuse and preparing to do the big bucks things. -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of R.James Sent: Saturday, December 04, 1999 5:43 AM Subject: RV-List: Lightening holes? or Not? Hi all, I'm about to bore out lightening holes in the Flap Brace & Spar. And a thought popped in mind while setting up the fly-cutter.. The plans say "Optional" for lightening holes here? Is there any major drawback with leaving them solid OTHER THAN the few measley ounces of weight reduction? IE: Aerodynamic air-flow (through the holes) impedance? IE: No inner access to rivets, etc (through holes)? Thanks in advance, (fly-cutter on hold) RJ in CT ________________________________________________________________________________
From: "John" <fasching(at)amigo.net>
Subject: $24 rv site
Date: Dec 04, 1999
I too feel uncomfortable about paying again for what I feel has already been paid for....what is the RVAtor for if not to provide on-going information and corrections to the many drawing errors? Also has anyone paid any attention to the fact that we have only 27 days left in 1999 and there are still 2 more RVAtors due for this year? Maybe Van should consider putting the RVAtor on the web and charging for that ONLY! RV-6A Flying Salida, CO ________________________________________________________________________________
Date: Dec 04, 1999
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Gel Cell Battery
> >Bob, >Doesnt the RG batteries ie Panther, have a 3psi pop vent in them that is why >we can not put them inside the passenger compartment of an aircraft without >a vented battery box. On the other hand the Powersonic does not have this >feature since it is suppose to be a gel cell and we can put them in the >cabin on a tray and not a vented box. No, yet another name for RG and starved electrolyte batteries is VRSLA for vent regulated, sealed lead acid. All of the sealed batteries have some form of over-pressure relief valve whether recombinant gas or the older, now nearly obsolete "gel" cells. The Panther folk may choose 3 psi for their products, last time I discussed it with Skip Koss on Concord's products, I think he said they vent at about 1.5 psi. Hawker/Gates batteries are on that same order. I asked Skip why the batteries don't outgass at altitude and he said it was because they operated at negative pressure inside the case. Concord has been supplying RG batteries to the military for years that are operated in un-pressurized compartments of aircraft with no degredation due to passage of gasses through the vent valve. Any of the RG batteries can be simply strapped down to a tray and operated out in the open. In fact, this is the safest way to use them. Out of perhaps a dozen battery induced explosions I been aware of over the years, only one was internal to a battery. The rest were actually battery BOX explosions where severely abused batteries outgassed into the battery box and the box provided the containment. An RG battery cannot vent liquid. Only gas and then only when severely abused. It's better to let it barf its innards into a large open volume as opposed to containing it in any enclosure. Bob . . . ________________________________________________________________________________
From: "Chris & Kellie Hand" <ckhand(at)earthlink.net>
Subject: Re: Opinion on drill press
Date: Dec 04, 1999
John and others, I posted a similar question last year and got a pretty even split in opinions on Central Machinery (should be able to find that thread in the archives). I bought the 16 speed floor stand Central Machinery model and have been happy with it. No problems, can run it slow enough for the fly cutter (slowest speed is around 195 rpm I believe) and holes are plenty straight and round enough for RV building. Price was good too, around $170 on sale. Just have to use a level to check the clamping surface as the scale showing the angle on mine is not quite accurate. That being said, it sits idle much of the time as I've found that other than using the fly cutter, the hand drills are fine. Don't know what other tools you have already but looking back, I would by a band saw and/or bench top belt/disc sander first (still haven't got either of those, but would use them more often than the drill press if I had them). Chris Hand Seaside, CA RV-6A, wings... ----- Original Message ----- From: John Lawson <jwlawson(at)hargray.com> Sent: Saturday, December 04, 1999 10:57 AM Subject: RV-List: Opinion on drill press > > I'm looking for a decent bench-mounted drill press - Harbor Freight carries a number of them made by Central Machinery. Anyone have any opinions, pro or con, about Central Machinery products? > > Thanks! > > Semper Fi > John > > ________________________________________________________________________________
Date: Dec 04, 1999
From: sarg314(at)azstarnet.com (tom sargent)
Subject: alternate air
I have an Air Flow Performance fuel injection system on my O-360 (just delivered a few days ago). I learned recently that some injected engines have an "alternate air" source for the intake in the event that the filtered air inlet gets clogged with ice. Apparently the alternate air is just taken from under the cowling. You'd have to be flying in some pretty mean weather to get ice in the intake like that. I would think the whole plane would be icing up too. That's the kind of weather I stay hundreds of miles away from. How essential is an alternate air source? Is it as essential as carb heat on a carburated engine? --- Tom Sargent, sarg314(at)azstarnet.com ________________________________________________________________________________
From: TRAASHMAN(at)webtv.net (Joe Waltz)
Date: Dec 04, 1999
Subject: Re: Problem!! with Cap Engraving Please read if you have
sent Caps. Steve, Looks to me that version "B" on your websiste is best since it would be readable while standing in front of the wing. I'm assuming that everyone would want the tab to the rear since this is the streamlined position (i.e. if its up then the air would try to push it down). I wasn't aware that you did the "RV-__" on the tab. I think that this is neat but I don't think I told you that I have an "8". I vote for "B". ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: alternate air
Date: Dec 04, 1999
Also helps when you suck a bird!!! Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: tom sargent <sarg314(at)azstarnet.com> Date: Saturday, December 04, 1999 5:11 PM Subject: RV-List: alternate air > > I have an Air Flow Performance fuel injection system on my O-360 >(just delivered a few days ago). I learned recently that some injected >engines have an "alternate air" source for the intake in the event that the >filtered air inlet gets clogged with ice. Apparently the alternate air is >just taken from under the cowling. > > You'd have to be flying in some pretty mean weather to get ice in >the intake like that. I would think the whole plane would be icing up too. >That's the kind of weather I stay hundreds of miles away from. How >essential is an alternate air source? Is it as essential as carb heat on a >carburated engine? > >--- >Tom Sargent, sarg314(at)azstarnet.com > > ________________________________________________________________________________
From: "Joe Hine" <joehine(at)nbnet.nb.ca>
Subject: Re: bottom flap skin
Date: Dec 04, 1999
Earl If I remember this part of RV4 building correctly, the part of the belly skin that sticks out the side is only as long as the main part of the wing. In the area ajacent to the flap the belly skin is flush with the fus. side. Alot of 4's have some interferance with the flap bottom skin and fus. The problem is usually that the bottom skin is not flush with the bottom of the fus. The simple fix for this (what I did) is bend the portion of the flap bottom skin that is suppost to go under the fus. to a Z arrangement that allowes the flap to rise up above the bottom of the fus. but the skin goes under the bottom. You could also just cut the piece of flap skin off, but that would leave the hole for the flap actuating rod open. There should be lots in the archives about this. I hope I have made myself somewhat clear. Joe Hine RV4 C-FYTQ > >Got the wings mounted on the RV4. Getting ready to set the incidence >angle, etc. Went to mount the flap and have interference between the >lower fuselage skin and the bottom flap skin on the fuse side. Looks >like I will have to cut the bottom fuselage skin flush with the fuselage >side to get enough clearance and maybe the flap skin also. Will get the >plans out and study some more. > >Any short cuts or advice will be welcome. > >Thanks Earl RV4 > > ________________________________________________________________________________
From: "Gar & Jan Pessel" <pessel(at)ptialaska.net>
Subject: rear spar fit on qb6
Date: Dec 04, 1999
I finally reached the point where it was time to mate the wings to the fuselage. We tried sliding the left wing into place and find that the tab off the rear spar will not fit into the slot between the tabs on the fuselage. It is too far back by over 1/8th of an inch. I do not have the faintest idea how to bend those two tabs or if I should be bending on the tab on the wing. Bending anything labeled as part of a spar , even just a rear spar, is not something that sounds like a particularly good idea. Anybody else ever encountered this problem? Gar Pessel, Fairbanks, AK ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: alternate air
Date: Dec 04, 1999
I have injection on mine, and I built the alternate air door, which will simply take air from under the engine. It is pre-filter, which will give me an alternate should some piece of stuff get plugged into the scoop. Pretty unlikely, but then I want to make engine failure pretty unlikely also. I don't think post filter is necessary, as anything small enough to fit through the scoop is also not large enough to cover the whole filter, should it get that far. If one is worried about snow, pull the alternate air before losing intake pressure. Alex Peterson Maple Grove, MN 6A ---------- > From: tom sargent <sarg314(at)azstarnet.com> > To: rv-list(at)matronics.com > Subject: RV-List: alternate air > Date: Saturday, December 04, 1999 5:07 PM > > > I have an Air Flow Performance fuel injection system on my O-360 > (just delivered a few days ago). I learned recently that some injected > engines have an "alternate air" source for the intake in the event that the > filtered air inlet gets clogged with ice. Apparently the alternate air is > just taken from under the cowling. > > You'd have to be flying in some pretty mean weather to get ice in > the intake like that. I would think the whole plane would be icing up too. > That's the kind of weather I stay hundreds of miles away from. How > essential is an alternate air source? Is it as essential as carb heat on a > carburated engine? > > --- > Tom Sargent, sarg314(at)azstarnet.com > ________________________________________________________________________________
Date: Dec 04, 1999
From: Gert <gert(at)execpc.com>
Subject: Re: alternate air
Why can y'all only think of ice, Just read a story of a filter clogged with fresh cut grass...........happy ending thanks to alternate.... Gert Cy Galley wrote: > > > Also helps when you suck a bird!!! > > Cy Galley - Editor, B-C Contact! > (Click here to visit our Club site at http://www.bellanca-championclub.com) > > -----Original Message----- > From: tom sargent <sarg314(at)azstarnet.com> > To: rv-list(at)matronics.com > Date: Saturday, December 04, 1999 5:11 PM > Subject: RV-List: alternate air > > > > > I have an Air Flow Performance fuel injection system on my O-360 > >(just delivered a few days ago). I learned recently that some injected > >engines have an "alternate air" source for the intake in the event that the > >filtered air inlet gets clogged with ice. Apparently the alternate air is > >just taken from under the cowling. > > > > You'd have to be flying in some pretty mean weather to get ice in > >the intake like that. I would think the whole plane would be icing up too. > >That's the kind of weather I stay hundreds of miles away from. How > >essential is an alternate air source? Is it as essential as carb heat on a > >carburated engine? > > > >--- > >Tom Sargent, sarg314(at)azstarnet.com > > > > > -- Pursuant to US Code, Title 47, Chapter 5, Subchapter II, '227, any and all nonsolicited commercial E-mail sent to this address is subject to a download and archival fee in the amount of $500 US. E-mailing denotes acceptance of these terms. ________________________________________________________________________________
From: "jim jewell" <jjewell(at)okanagan.net>
Subject: wig-wags
Date: Dec 04, 1999
Hello Jerry Calvert: Apperently Galls.com/etc. is no longer a valid web site. My attempts to find Galls on the web failed, is it the same for others out there? jim Kelowna BC. -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of RV6BLDR Sent: Saturday, December 04, 1999 8:40 AM Subject: Re: RV-List: wig-wags Bobpaulo(at)aol.com wrote: > > > where could i find wig-wags and info to wire?? bob > > _ Bob, Here's a post I sent a few months ago on wig-wags. At this site they have a wire diagram you can download. ****** Was looking at the latest Gall's catalog and noticed there is a new Wig-Wag flasher available. Check it out at:(Give it a minute to completely load. It will be slow at first, but once it gets going, it's really cool!) <http://www.galls.com/service/fs013.asp> For those who have been wondering what the standard Wig-Wag pattern looks like, go to: <http://www.galls.com/service/fs020.asp> Since there was a thread on the Wig-Wags last week, thought you Wig-Wag wannabes would be interested in this. Jerry Calvert Edmond Ok -6 wings ________________________________________________________________________________
From: "James E. Clark" <jclark(at)conterra.com>
Subject: Re: New Site: SourceRV.com!
Date: Dec 04, 1999
I was about to comment in detail but this is so well put Jeremy. One other observation from my view, the RV-List is a "service" that provides a mechanism for **US** to share with each other. And I am a contributor. SourceRV =appears= to be a "service" that focusses more on "content" that has to be otherwise obtained at **SOMEBODY's** expense. And $24 is a **SMALL** amount for the promised/anticipated content ... much less that what I (and I suspect many others) have contributed to the RV-List. Go for it!!! And best wishes for the sake of us RV builders who do want as much info as possible **AND** you for taking the risk to get it provided. James Being beaten by sliding canopy but a happy RV-List and SourceRV supporter (so far ;-) ) ----- Original Message ----- From: Jeremy Benedict <list(at)infoav.com> Sent: Saturday, December 04, 1999 12:57 AM Subject: Re: RV-List: New Site: SourceRV.com! > > --> RV-List message REALLY posted by: , not the above! > > I encourage anyone interested in RV aircraft to read this... > > > Sounds to me like this crew is trying to con-in on a look-alike RV List > for a > profit...Jim Brown, NJ, RV- 3 > > Dear Jim: > > I am deeply troubled by your public accusation about my intentions and this > new venture. I'd like to present a little background on the subject to help > inform you and anyone who might share your feelings about SourceRV.com. > > The web site in question was developed to provide an optional, value-added > service to those interested in RV aircraft. My background is quite extensive > in RVs and Van's Aircraft. I have been Van's Webmaster for the past 4.5 > years, and have done a host of other things for Van's including spending > countless hours helping to prepare RVators and Accessories Catalogs, > sweating in yellow tents at various fly-ins, etc. Most of the work I have > done has not really been "work", but rather my time volunteered to the RV > and Van's cause...I don't work for Van's and I never have. I hesitate to > think of how much time I've "volunteered"; I often question whether the > 1000+ hours of time would have been better spent on things like my career > and my life. > > During the past decade, I've heard from many RV builders and pilots. I've > been subscribed to the rv-list since 1994. I've read the 1,500 comments > submitted about Van's web site. I've talked to hundreds if not thousands of > RV enthusiasts, builders, and pilots throughout the country and the world. I > know Van's operation and product fairly well. Through all this interaction, > one thing has become very clear. People want more information and resources. > Much more. > > The options for providing what people really wanted were quite limited. It > was too much of a resource commitment for Van's, so after five months of > consideration last spring, Van's agreed to support in principal (not $$) the > ideas I had. I've formed a company, InfoAv, to develop and present these > ideas. > > Stated again, I've developed a service to present information that people > told me they wanted. Isn't this somewhat consistent with the ideas of > capitalism and the free market economy in this country? I seem to recall the > story of a young man in the 1970s who designed and built his own airplane. > Soon after others flew his airplane, they desired, they asked, they wanted > to have this airplane. In response to their pressure, not because he was > trying to make a buck, this young man made his airplane available. Like this > young man, Richard VanGrunsven, and his airplane, the RV-3, I have developed > SourceRV.com because people have told me they wanted this. It is my full > intention to continue in the tradition of Van by producing quality products > at very reasonable prices. > > You claim that I'm trying to "con-in...for a profit." I have to ask, do you > work for free? Probably not. Most people I know get paid to work at a job, > and have expenses to pay. I'm no different. Only my job now is to produce > the services I've mentioned above. Will I make a profit? I hope so...much in > the same way that your "profit" probably comes in the form of a paycheck. > > Now, there will be no Gulfstreams flying around with "SourceRV.com" written > on the side. You can do the math. The revenue generated from SourceRV.com > won't even be sufficient to solely support a full-time position. It is only > through working on several additional projects that I can put bread on the > table, and maybe even take in an EAA pancake breakfast here and there. > Perhaps it would be wiser to completely drop out, forget about what people > want, give up on Van's site, and go back to the computer industry. But > that's not what I want and not what others have told me they wanted. > > I think it would be great to make SourceRV.com free. I've analyzed different > potential revenue models. When it comes down to it, the web site has to > generate income. I think it has been positioned in the best way possible > given the requirements and circumstances. > > You may have noticed one benefit of my decision already...Van's web site > went from a deteriorating condition to new, active, and updated almost > daily. Soon to come will be a new Accessories Catalog and on-line ordering > with cool things like order tracking. Without the development of InfoAv, > Van's web site likely would have been seriously downsized or closed > altogether. > > This past fall, I've mentioned what I am doing to a number of people. So > far, everyone has been positive, expressing interest in the idea. Many > reactions have been very enthusiastic. People have understood that the > resources (aka money) to develop the site _have_ to come from somewhere. > > If you still feel the same about SourceRV.com, then the best thing to do is > simply not subscribe. Trying to influence everyone's opinion is not > productive for anyone. > > I want to make clear that I'm not trying to recoup what I've given in the > past. My focus is on the future and trying to produce and provide what > people want. > > Sincerely, > Jeremy Benedict jeremy(at)infoav.com > InfoAv Corporation > > ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: RV8 N94BD weigh-in
Date: Dec 04, 1999
Listers, I finally found a scale and completed the weight and balance on my RV8 today. With the able assistance of several patient souls with strong backs, the results are as follows: RV8 N94BD Ser.#: 80379 Engine: Lyc O-360A4J Prop: Sensenich 72FM8S9-83 (metal) Battery: On firewall Oil Cooler: on firewall, Positech..soon to be replaced w/Niagara. Spinner: Van's fiberglass Panel: Deluxe VFR w/ gyros and all analog engine gauges Lighting: panel lights, landing light, Whelan 3 in 1 strobes on wingtips (single power pack aft of rear baggage hold). Seats: custom made, high density foam, w/auto interior fabric Belts: Pacific Aero Harness five point front and rear. Total weight, no fuel, 7 quarts oil: 1037 pounds Empty aircraft CG: 76.82" aft of 70" datum forward of wing leading edge. We used a single, balance beam scale calibrated by me standing on it! The scale was moved to each wheel at a time, and this worked out quite well. It does take some strong backs to lift the mains, but with four guys, it was quick work. I'm pleased with the outcome, and hope to stay under 1100 pounds with the gear fairings, wheel pants and paint. Another weigh-in will be required after all this is done, of course. With just me in the front seat with full fuel, the CG is well forward, but within limits. I plan to make a survival kit and will locate it on the aft baggage shelf where it will remain at all times. This should help a little. We ran the engine afterwards to check a few squawks from the last test run, and this machine feels like it wants to leap off the ground right now! Alas, only one more hurdle until it does fly...and "Das Fed" will come for a visit next week to give my airplane a checkup. (Ok now, this won't hurt a bit....now turn your rudder and cough). Brian Denk RV8 N94BD fairings, gadgets, sanding, testing, etc. ________________________________________________________________________________
Date: Dec 04, 1999
From: Larry Olson <lolson(at)doitnow.com>
Subject: Need to sell one of my engines...
Hi Folks, I need to sell one of my engines, or completely redesign a twin. (hummmm a RV12 maybe...) I have: For Sale Lycoming 0320-A1A History: S/N 3475-27 Was in a Piper Apache N1386P Complete logs In service 3-1-56 Majored 6-22-61 1452 hrs TT after apparent gear up landing. Top overhaul 5-16-75 at 2996 TT This overhaul at 3566 hrs TT Conical mount Cases done at Divco Yellow tagged rods, crank, and cylinders from Rick Romans New cam and carb. New Slick mags and harnesses New Prop Governor Fuel Pump Oil cooler Ring gear Most all hardware re-plated All applicable AD's complied with (inc oil pump) Engine is just back from inspection. Not assembled. Overhaul labor is paid for at Aeroparts of Arizona but not started yet. If I kept the engine I didn't want it assembled until I was ready for it. Have not specified HP yet so you could have 150 hp or 160 hp. Pistons are already paid for. Overhaul will be by Bill Castles. A very respected rebuilder at Phoenix, DVT. To be complete you will need a starter, alternator and optional vacuum pump. Price: Assembled and ready to go - $12,500 Not assembled - $11,600 Warranty - If installed in an airplane at DVT, overhauler will fix anything that is not right. He guaranties that it will be right. No real time frame. I've seen several planes with his engines in them with no problems. I'm going to use him on my other engine. Prices are FOB Phoenix, AZ OR engine #2: Lycoming 0320-A2A History: S/N L-38687-27A Was in a Piper TriPacer Conical mount 450hrs SFOH* No Logs No Mags Ring gear Carb Alternator Starter Oil cooler * With no logs it's hard to confirm so I took the engine to Lycon and had them disassemble and evaluate. They confirmed very low time (with no prompting they estimated 400hrs) never been turned crank. It is a wide deck. Cylinders showed some sign of wear but not bad. They said I should have just run it the way it was. It is machined for a fuel pump. Engine is just back from inspection. Not assembled. Price: $5500 Price is FOB Phoenix, AZ If I kept it I would buy 160 hp pistons, bearings, gasket set, fuel pump and mags. I have a rebuilder that will put it back together for $900 + any incidentals. It would be a cheep running low time engine. Let me know... Larry Olson Cave Creek, AZ RV6-Finish kit on order ________________________________________________________________________________
Date: Dec 04, 1999
From: Denton Harjehausen <harje(at)proaxis.com>
Subject: Re: rear spar fit on qb6
> >I finally reached the point where it was time to mate the wings to the >fuselage. We tried sliding the left wing into place and find that the tab >off the rear spar will not fit into the slot between the tabs on the >fuselage. It is too far back by over 1/8th of an inch. I do not have the >faintest idea how to bend those two tabs or if I should be bending on the >tab on the wing. Bending anything labeled as part of a spar , even just a >rear spar, is not something that sounds like a particularly good idea. >Anybody else ever encountered this problem? Gar Pessel, Fairbanks, AK I would call Van's on that. My belief is that it should jsut slip in...no bending. Good luck, denny, RV-6 ________________________________________________________________________________
Date: Dec 05, 1999
From: pagan <pagan(at)cboss.com>
Subject: Electric Tach
Seems like I remember something on the list about electric tach not recording time on the hour meter unless they are running at a certain rpm. Searched the archives but couldn't get a good hit. Anybody know the answer? Bill Pagan N565BW "The original RV-8A builders page on the web" http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html ________________________________________________________________________________
Date: Dec 04, 1999
From: Gary Zilik <zilik(at)bewellnet.com>
Subject: Re: wig-wags
Apperently Galls.com/etc. is no longer a valid web site. Try http://www.galls.com Gary Zilik ________________________________________________________________________________
Date: Dec 04, 1999
From: Glenn & Judi <foxinsocks(at)mediaone.net>
Subject: Re: Electric Tach
pagan wrote: > > Seems like I remember something on the list about electric tach not > recording time on the hour meter unless they are running at a certain rpm. > Searched the archives but couldn't get a good hit. Anybody know the answer? > > Bill Pagan > N565BW > "The original RV-8A builders page on the web" > http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html > Bill, I think the Electronics Intl. Tach operates how you mentioned, but they give you an option of hooking it up to an oil pressure switch as well. -Glenn Gordon ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: RV8 N94BD weigh-in
Date: Dec 04, 1999
I hope that when you weighed your plane there was a block under the other two wheels the same height as the scale so that the plane was always in the same plane. Other wise, you may find that you do not have the right numbers. Of course you did weight it inside out of the wind so those wonderful airfoils didn't change the true weight either. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Brian Denk <akroguy(at)hotmail.com> Date: Saturday, December 04, 1999 8:56 PM Subject: RV-List: RV8 N94BD weigh-in > >Listers, > >I finally found a scale and completed the weight and balance on my RV8 >today. With the able assistance of several patient souls with strong backs, >the results are as follows: > >RV8 N94BD >Ser.#: 80379 >Engine: Lyc O-360A4J >Prop: Sensenich 72FM8S9-83 (metal) >Battery: On firewall >Oil Cooler: on firewall, Positech..soon to be replaced w/Niagara. >Spinner: Van's fiberglass >Panel: Deluxe VFR w/ gyros and all analog engine gauges >Lighting: panel lights, landing light, Whelan 3 in 1 strobes on wingtips >(single power pack aft of rear baggage hold). >Seats: custom made, high density foam, w/auto interior fabric >Belts: Pacific Aero Harness five point front and rear. > > >Total weight, no fuel, 7 quarts oil: 1037 pounds >Empty aircraft CG: 76.82" aft of 70" datum forward of wing leading edge. > >We used a single, balance beam scale calibrated by me standing on it! The >scale was moved to each wheel at a time, and this worked out quite well. It >does take some strong backs to lift the mains, but with four guys, it was >quick work. I'm pleased with the outcome, and hope to stay under 1100 >pounds with the gear fairings, wheel pants and paint. >Another weigh-in will be required after all this is done, of course. > >With just me in the front seat with full fuel, the CG is well forward, but >within limits. I plan to make a survival kit and will locate it on the aft >baggage shelf where it will remain at all times. This should help a little. > >We ran the engine afterwards to check a few squawks from the last test run, >and this machine feels like it wants to leap off the ground right now! >Alas, only one more hurdle until it does fly...and "Das Fed" will come for a >visit next week to give my airplane a checkup. (Ok now, this won't hurt a >bit....now turn your rudder and cough). > >Brian Denk >RV8 N94BD >fairings, gadgets, sanding, testing, etc. > > ________________________________________________________________________________
From: PANELCUT(at)aol.com
Date: Dec 04, 1999
Subject: Drawing of Fuel cap
Group Sorry about the confusion on the picture on my web site, some had mentioned the RV8 on the tab. That's just for me to be sure I keep the different gallons straight it doesn't get engraved. I did all the drawings in one file and that was for me only. I want to thank everyone for their understanding on the confusion and the hold up, but I thought this was an important issue and wanted everbody to be happy with their caps. I plan on starting them monday and hope to start sending them back. Steve Davis The Panel Pilot http://members.aol.com/panelcut ________________________________________________________________________________
From: "Larry Pardue" <n5lp(at)carlsbad.net>
Subject: Re: Electric Tach
Date: Dec 04, 1999
> >Seems like I remember something on the list about electric tach not >recording time on the hour meter unless they are running at a certain rpm. >Searched the archives but couldn't get a good hit. Anybody know the answer? > > This probably works differently on different electric tachs. On the Vision it is true and the RPM is 1500. Makes sense. Larry Pardue Carlsbad, NM RV-6 N441LP ________________________________________________________________________________
From: PANELCUT(at)aol.com
Date: Dec 04, 1999
Subject: Fuel Cap Drawing Everyone who has caps for engraving READ
Group I have posted the drawings of the fuel caps on my page it is http://members .aol.com/panelcut. Please go look at this and vote this is the last chance for you to let me know. I plan on starting them Monday and If I don't hear form you they will be engraved like Pauls. I have heard form a few you do not have to answer again, but there are still alot I have not. The RV8 on the tab DOES NOT GET ENGRAVED that's was for my reference only, when I created the files I did the RV4 and RV6 as well and that was so I keep them straight when I engrave your caps. Again I want to thank everyone for your understanding. Steve Davis The Panel Pilot http://members.aol.com/panelcut ________________________________________________________________________________
From: "Bryan E. Files" <BFiles(at)corecom.net>
Subject: Re: Gel Cell Battery
Date: Dec 04, 1999
Bob, Thank you for the information. **** Bryan E. Files **** Ever Fly Maintenance Palmer, Alaska A&P, IA, FAA Safety Counselor mailto:BFiles(at)corecom.net ----- Original Message ----- From: Robert L. Nuckolls, III <nuckolls(at)aeroelectric.com> Sent: Saturday, December 04, 1999 12:34 PM Subject: Re: RV-List: Re: Gel Cell Battery > > > > >Bob, > >Doesnt the RG batteries ie Panther, have a 3psi pop vent in them that is why > >we can not put them inside the passenger compartment of an aircraft without > >a vented battery box. On the other hand the Powersonic does not have this > >feature since it is suppose to be a gel cell and we can put them in the > >cabin on a tray and not a vented box. > > No, yet another name for RG and starved electrolyte batteries > is VRSLA for vent regulated, sealed lead acid. All of the > sealed batteries have some form of over-pressure relief valve > whether recombinant gas or the older, now nearly obsolete > "gel" cells. The Panther folk may choose 3 psi for their products, > last time I discussed it with Skip Koss on Concord's products, > I think he said they vent at about 1.5 psi. Hawker/Gates > batteries are on that same order. > > I asked Skip why the batteries don't outgass at altitude > and he said it was because they operated at negative pressure > inside the case. Concord has been supplying RG batteries to > the military for years that are operated in un-pressurized > compartments of aircraft with no degredation due to passage > of gasses through the vent valve. > > Any of the RG batteries can be simply strapped down to a > tray and operated out in the open. In fact, this is the > safest way to use them. Out of perhaps a dozen battery > induced explosions I been aware of over the years, only > one was internal to a battery. The rest were actually > battery BOX explosions where severely abused batteries > outgassed into the battery box and the box provided the > containment. An RG battery cannot vent liquid. Only gas > and then only when severely abused. It's better to let it > barf its innards into a large open volume as opposed to > containing it in any enclosure. > > > Bob . . . > > ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: RV8 N94BD weigh-in
Date: Dec 04, 1999
> > >I hope that when you weighed your plane there was a block under the other >two wheels the same height as the scale so that the plane was always in the >same plane. Other wise, you may find that you do not have the right >numbers. >Of course you did weight it inside out of the wind so those wonderful >airfoils didn't change the true weight either. > >Cy Galley - Editor, B-C Contact! Yup, sure did! The scale came with blocks that are exactly the same height as the scale platform. A smart level was used to verify the longerons were level at all times. Brian Denk ________________________________________________________________________________
From: PANELCUT(at)aol.com
Date: Dec 04, 1999
Subject: Re: Problem!! with Cap Engraving Please read if you have
sent Caps. Joe Got you down for B, Sorry about the tab that's just so I don't confuse the different planes and engrave the wrong gallons. It just for reference. Steve ________________________________________________________________________________
Date: Dec 04, 1999
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: RV-6A O-360 FAB
What have others done to increase the clearance between the Filtered Air Box and the training wheel gear leg? :-) I have been told that the GBI video shows cutting the filter to allow more clearance at the carb. Has anyone cut a piece of the FAB fiberglass off and then created a slanted replacement piece of fiberglass to cover it? ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, So. CA, USA ________________________________________________________________________________
Date: Dec 04, 1999
From: pdsmith <pdsmith(at)pacbell.net>
Subject: RV-8 seat floor questions
Hi Listers: Pardon my "dumminess" but do the F829 footwell flanges and flooring go under or on top of the F-830 and F-831 seat floors. I can't tell from DWG 29 or the video. If I want to make the floors removable (I read the archives on this), should I use #8 nutplates or are #6 beefy enough? Thanks, Phil Smith, 80691 ________________________________________________________________________________
Date: Dec 04, 1999
From: Bob Skinner <bskinner(at)vcn.com>
Subject: Re: RV-6A O-360 FAB
Gary, A quick and dirty way is to mark the area where you want clearance, heat the FAB box and press the area down on a flat surface. A more refined fix would be to cut and fill. We didn't have a clearance problem on Charlie's 160 hp with the nose gear but the FAB box was a bit close to the edge of the cowl scoop so this is what we did and it worked OK. I guess we can always make it pretty, now that Charlie has his six about worn out but, at the time, we were in a hurry to get airborne:) Bob Skinner Buffalo, WY (1995 RV6 sold after 4 years & 470 hrs) EAA Tech Counselor # 3726 >What have others done to increase the clearance >between the Filtered Air Box and the training wheel >gear leg? :-) I have been told that the GBI video >shows cutting the filter to allow more clearance at >the carb. > >Has anyone cut a piece of the FAB fiberglass off and >then created a slanted replacement piece of fiberglass >to cover it? > > >==== >Gary A. Sobek >"My Sanity" RV-6 N157GS O-320 Hartzell, >So. CA, USA ________________________________________________________________________________
Date: Dec 05, 1999
From: Michael Hartmann <hartmann(at)sound.net>
Subject: Yeller Pages Update
The latest version of the Yeller Pages is online at www.sound.net/~hartmann/yelrpage.htm I'm sure you find it useful. Be sure and tell Gary thanks. - Mike hartmann(at)sound.net ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)home.com>
Subject: Re: Vacuum System
Date: Dec 04, 1999
>Anyway, at this time, I don't want to install a vacuum pump, gyros, a vacuum >gauge, etc. I do want to install all of the other stuff so the system is more >or less "plug & play" when I get the expensive parts. I assume I'll need a >filter, a regulator, a firewall pass through, and some tubing. Have I >forgotten anything? The regulator can be used as a firewall pass-through. I would think that you wouldn't be able to do much more than the regulator and the filter. There are no hoses between these two components so you wouldn't have any hose yet. It might be difficult to guess where to put the filter and regulator for optimal routing of the hoses without the other stuff. Either way you're still going to have much cutting and fitting of hoses up behind the panel, and possibly cutting holes in the next bulkhead forward for the instruments and/or hoses. Not quite "plug & play".... Randall Henderson, RV-6 N6R (~50 hrs) Portland, OR http://www.edt.com/homewing ________________________________________________________________________________
From: "Ken Hoshowski" <ve7fp(at)jetstream.net>
Subject: Re: Need to sell one of my engines...
Date: Dec 04, 1999
Larry, On your list of options you include a prop governor. I am running a 0 320 B3B out of an Apache and the prop. governor that came with my engine works backwards to the one required if you buy a Hartzell fron Vans. First time I fired up my prop went to course pitch and on shutdown the oil filter was extremely bulged out. I mention this in the event you were not aware of it. I learned the hard way. Seems to me my Governor was a Hamilton Standard but can check make and model next time I am in the Hanger if you like. Ken Hoshowski RV6 C-FKEH Salmon Arm B.C. -----Original Message----- From: Larry Olson <lolson(at)doitnow.com> Date: Saturday, December 04, 1999 7:31 PM Subject: RV-List: Need to sell one of my engines... > >Hi Folks, > >I need to sell one of my engines, or completely redesign a twin. >(hummmm a RV12 maybe...) > >I have: > >For Sale > >Lycoming 0320-A1A > >History: >S/N 3475-27 >Was in a Piper Apache N1386P >Complete logs >In service 3-1-56 >Majored 6-22-61 1452 hrs TT after apparent gear up landing. >Top overhaul 5-16-75 at 2996 TT >This overhaul at 3566 hrs TT >Conical mount >Cases done at Divco >Yellow tagged rods, crank, and cylinders from Rick Romans >New cam and carb. >New Slick mags and harnesses >New Prop Governor >Fuel Pump >Oil cooler >Ring gear >Most all hardware re-plated >All applicable AD's complied with (inc oil pump) > >Engine is just back from inspection. Not assembled. >Overhaul labor is paid for at Aeroparts of Arizona but not started yet. >If I kept the engine I didn't want it assembled until I was ready >for it. Have not specified HP yet so you could have 150 hp or 160 hp. >Pistons are already paid for. Overhaul will be by Bill Castles. A very >respected rebuilder at Phoenix, DVT. > >To be complete you will need a starter, alternator and optional vacuum >pump. > >Price: > >Assembled and ready to go - $12,500 >Not assembled - $11,600 > >Warranty - If installed in an airplane at DVT, overhauler will fix anything >that is not right. He guaranties that it will be right. No real time frame. >I've >seen several planes with his engines in them with no problems. I'm going >to use him on my other engine. > >Prices are FOB Phoenix, AZ > > >OR engine #2: > > >Lycoming 0320-A2A > >History: >S/N L-38687-27A >Was in a Piper TriPacer >Conical mount >450hrs SFOH* >No Logs >No Mags >Ring gear >Carb >Alternator >Starter >Oil cooler > > >* With no logs it's hard to confirm so I took the engine to Lycon and >had them disassemble and evaluate. They confirmed very low time >(with no prompting they estimated 400hrs) never been turned crank. >It is a wide deck. Cylinders showed some sign of wear but not bad. >They said I should have just run it the way it was. It is machined for >a fuel pump. Engine is just back from inspection. Not assembled. > >Price: $5500 > >Price is FOB Phoenix, AZ > >If I kept it I would buy 160 hp pistons, bearings, gasket set, fuel pump >and mags. I have a rebuilder that will put it back together for $900 + any >incidentals. It would be a cheep running low time engine. > > >Let me know... > >Larry Olson >Cave Creek, AZ >RV6-Finish kit on order > > ________________________________________________________________________________
From: pbennett(at)zip.com.au
Date: Dec 04, 1999
Subject: Re: Carb Ice
Other RMI users report the same. The sensor is enclosed in a brass plug which seems to ensure that it measures the carb body temp rather than the mixture temp. It is quite conceivable with this configuration that there could be ice on the butterfly valve with the sensor reading well above freezing. I have the RMI and would like to hear of any practical way of isolating the sensor from the carb body. Peter Bennett RV6 Sydney (not yet flying) > > > Gary, this is an area I have wondered about as well. I too have a temp > probe on the carb, and the temp always rises as the engine warms. Earlier > this week, the ambient temp was 0 degrees Celsius before the plane was > started, and by takeoff, the carb temp had risen to 16 degrees C. I have > never seen the carb temp go down and it almost always runs at an indicated > 19 degrees C which is as high as the RMI uMonitor will display. > > My guess is that the carb stays warm because it is bolted directly to the > oil sump. > > Sam Buchanan (hoping a bird doesn't fly up the carb intake because the > Van's carb heat rig is not a true alternate air system...) > ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: strobe positon question
Date: Dec 05, 1999
I am familiar with the phenomena of strobe light from the top of the fuselage bouncing about in the cockpit. Because the turtle deck slopes aft, I wondered if anyone had successfully mounted a strobe on the top aft skin far enough back so that the light in the cockpit was not a problem. Maybe nobody has ever done it, but I thought that the RV List would be a good place to post the question. I am inclined to put a strobe in the Vertical Stabilizer, but I riveted the tip on about 4-5 years ago, before I thought of it. That's what's got me thinking about easier-to-mount and easier-to-service alternatives. Steve Soule Huntington, Vermont -----Original Message----- A strobe behind the canopy could easily reflect off the instruments/panel/windscreen at night and make your life miserable. ________________________________________________________________________________
Date: Dec 06, 1999
From: pagan <pagan(at)cboss.com>
Subject: Re: RV-8 seat floor questions
Hi Phil, I'm not sure about the numbers but the footwells connect together by a floor piece that runs between them. this whole assy is removable. I put the flanges on the wells over the middle piece. As for making the floors removable, I'd use #8 nutplates. The #6 screws are much weaker. This is really only a problem here because of the screw snapping off and then you're faced with having to get the shank of the screw out of the nutplate. (ask me how I know so much about #6 screws breaking off) If I was to do the whole thing over I don't think I'd use #6 anywhere, but would go with #8 instead. Bill Pagan N565BW "The original RV-8A builders page on the web" http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html > >Hi Listers: > >Pardon my "dumminess" but do the F829 footwell flanges and flooring go under >or on top of the F-830 and F-831 seat floors. I can't tell from DWG 29 or >the video. > >If I want to make the floors removable (I read the archives on this), should >I use #8 nutplates or are #6 beefy enough? > >Thanks, > >Phil Smith, 80691 > > ________________________________________________________________________________
From: DFCPAC(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV3-List Digest: 12/04/99
does anyone use this list, or do they use the regular rv list? i own an rv3 and would like to talk to other owners of rv3's. regards dan carley rv3a-148cw ________________________________________________________________________________
Date: Dec 05, 1999
From: Denny Harjehausen <harje(at)proaxis.com>
Subject: Re: Electric Tach
RMI's works on oil pressure and RPM and maybe adjusted for different cruise RPMs. Have a good day! Denny Harjehausen RV-6 - done except for the bugs! Lebanon, OR ________________________________________________________________________________
Date: Dec 05, 1999
From: "Bob U." <r.r.urban(at)worldnet.att.net>
Subject: Re: RV3-List: Re: RV3-List Digest: 12/04/99
Hi Dan, Glad to see you here. I thought I was all alone until now..... other than Matt's notices showing up occasionally, letting me know the link was up and alive. I've been going to the regular RV list for lack of action here. My RV-3 project is in need of most things firewall forward and last Friday, I went looking for a used prop on the regular RV list. My project needs a 4 inch spool prop extension, starter ring gear/flywheel, Mark Landoll harmonic damper, exhausts, etc. I'm just east of Kansas City, MO and would like to get my project flying by late 2000. With your RV flying, what's going on with you? Bob ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ DFCPAC(at)aol.com wrote: > > --> RV3-List message posted by: DFCPAC(at)aol.com > > does anyone use this list, or do they use the regular rv list? i own an rv3 > and would like to talk to other owners of rv3's. > > regards > dan carley > rv3a-148cw > ________________________________________________________________________________
Date: Dec 05, 1999
From: chester razer <razer(at)midwest.net>
Subject: Re: RV-6A O-360 FAB
Gary, I also had the same clearance problem during construction in my 6A with the FAB. I have flown for 220 hours now and it has not presented a problem. My thinking was that I would let the gear leg wear a hole in the f-glass air box and then repair it with a small fiberglass repair (simple) but it has never happened. I guess my advice would be to "not repair the problem until it occurs" since its not going to be the kind of problem that causes you to abort a flight. This is the kind of problem you look for during the many times you'll have the cowl off during your first 200 hours of flight. chet "Gary A. Sobek" wrote: > > > What have others done to increase the clearance > between the Filtered Air Box and the training wheel > gear leg? :-) I have been told that the GBI video > shows cutting the filter to allow more clearance at > the carb. > ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Dec 05, 1999
Subject: Re: Prop pitch confusion
Every prop manf. has a different way of determining mean pitch station & cord position along the blade. The only item I am able to quantify among the different manf.s is the length. I use word of mouth on the specific vender as to what specific grind on the blade. Grind on the blade is almost meaningless to compair among different manufactures....... pperryrv(at)hotmail.com on 12/03/99 10:16:04 PM Please respond to rv-list(at)matronics.com Subject: RV-List: Prop pitch confusion I don't get it, I'm just starting to look for a prop for my plane and I can't seem to get the picture on how to pick the right pitch. I looked up the prop spec on Sensenich's wood prop web site and found they recomend a 68"x 78-80" prop for an RV-4 with 150hp. I see Thomas McIntyre advertise his prop as a good 230mph RV3 cruise prop with only a 71" pitch - he flew it so it must work, but how? Are there big differences in the way prop makers determine pitch? Pat Perry Dallas, PA RV-4 fuse almost done Engine being rebuilt I need a prop! ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: RV8 N94BD weigh-in
Date: Dec 05, 1999
Good Job! Well done! Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Brian Denk <akroguy(at)hotmail.com> Date: Saturday, December 04, 1999 10:56 PM Subject: Re: RV-List: RV8 N94BD weigh-in > > >> >> >>I hope that when you weighed your plane there was a block under the other >>two wheels the same height as the scale so that the plane was always in the >>same plane. Other wise, you may find that you do not have the right >>numbers. >>Of course you did weight it inside out of the wind so those wonderful >>airfoils didn't change the true weight either. >> >>Cy Galley - Editor, B-C Contact! > >Yup, sure did! The scale came with blocks that are exactly the same height >as the scale platform. A smart level was used to verify the longerons were >level at all times. > >Brian Denk > > ________________________________________________________________________________
From: BumFlyer(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV-6A O-360 FAB
In a message dated 12/4/99 22:09:10, rv6flier(at)yahoo.com writes: What have others done to increase the clearance between the Filtered Air Box and the training wheel gear leg? :-) I have been told that the GBI video shows cutting the filter to allow more clearance at the carb. Has anyone cut a piece of the FAB fiberglass off and then created a slanted replacement piece of fiberglass to cover it? >> Actually my in service experience would suggest that a very small clearance is probably ok. Nonetheless I did create a dimple at the point of closest clearance, by applying a heated steel tube of the approximate diameter of the gear leg to the fiberglass FAB at the same angle as the gear leg. Then I reinforced as required. Still not at all sure it was necessary but it looks cool and didn't take much effort. BTW my recollection of the Orndorff tape was to cut the filter where it was interfering with the bottom of the carb bell-- a different thing altogether. D Walsh ________________________________________________________________________________
From: OrndorffG(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV-6A O-360 FAB
Our video does not show cutting the Filtered Air Box. Yes, this was a problem with the old gear legs that you fiberglassed the wood fairing on. With the new gear and the fiberglass fairing, this should not be a problem George Orndorff ________________________________________________________________________________
Date: Dec 05, 1999
From: Denny Harjehausen <harje(at)proaxis.com>
Subject: More Radio
Radio trouble shooting still. I changed antennas. The reception increased dramtically. The transmission is still garbled. Note as bad, but still not really readable and far from clear. Could this be the radio itself? I would think the transmission would not have improved at all if it was the intercom. But then again what I know about these things? I am looking for a radio expert locaaly here. Hope one of you guys have some more simple ideas I can try. Have a good day! Denny Harjehausen RV-6 - done except for the bugs! Lebanon, OR ________________________________________________________________________________
From: Mkraus01(at)aol.com
Date: Dec 05, 1999
Subject: RV4 Horiz Stab gap question
One quick question, how big of a gap should I leave between the horizontal stabilizer and the outboard portion of the counterbalance rib?? I was worried about this area flexing in flight and binding the elevator if the gap is not sufficient. I could not find this dimension on the plans. (I am referring to the gap between the HS skin and the counterbalance rib skin) Thanks -Mike ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Re: RV-8 seat floor questions
Date: Dec 05, 1999
Phil, in addition to Bill's remarks I would suggest that you think twice before making them removeable for two reasons. There's a LOT of stuff that would need to come out in order to remove the panels, including the entire flap mechanism. And second that's a whole lot of platenuts! Like Bill I put my footwells in from the top. Can't remember now but it seems like the plans call for that... look closely for the dotted line indicating one part is on top of another. Regards, Randy Lervold RV-8, #80500, making fuel lines today so I can remove the wings www.pacifier.com/~randyl Home Wing VAF ________________________________________________________________________________
Date: Dec 05, 1999
From: RV6BLDR <calverjl(at)flash.net>
Subject: Re: wig-wags
jim jewell wrote: > > > Hello Jerry Calvert: > > Apperently Galls.com/etc. is no longer a valid web site. > My attempts to find Galls on the web failed, is it the same for others out > there? > jim Kelowna BC. OOOOPS! Gall's has redone their sit and here are the new url's: The multi-flasher demo: <http://www.galls.com/service/FS013.jsp> The original flasher: <http://www.galls.com/service/FS025.jsp> To view wiring diagrams, scroll down on page listed below and select the product number from the droplist and hit submit: <http://www.galls.com/service/techsupport.jsp> Jerry Calvert Edmond Ok -6 ________________________________________________________________________________
Date: Dec 05, 1999
From: Charles Hampton <mrbrownstone(at)home.com>
Subject: Re: More Radio
Had similar problem with a TKM radio, have your radio benchchecked. Denny Harjehausen wrote: > > > Radio trouble shooting still. I changed antennas. The reception increased > dramtically. The transmission is still garbled. Note as bad, but still > not really readable and far from clear. > > Could this be the radio itself? I would think the transmission would not > have improved at all if it was the intercom. But then again what I know > about these things? > > I am looking for a radio expert locaaly here. Hope one of you guys have > some more simple ideas I can try. > > Have a good day! > Denny Harjehausen > RV-6 - done except for the bugs! > Lebanon, OR > ________________________________________________________________________________
Date: Dec 05, 1999
From: WAYNE BONESTEEL <wayneb(at)oakweb.com>
Subject: Re: bottom flap skin
Earl I had to jog the skin just as Joe Hine indicated to get the flap trailing edge up where it aligned with the aileron and fit the wing form cutout. What I want to inject, when drilling the rear spar hole make sure the wing is not pushed back (swept aft) as I believe I did, because it puts the flap tie rod mount plate too close to the fuselage, mine actually hit and I had to peen the fuselage skin for clearance, looks OK now but what a pain. Wayne EARL FORTNER wrote: > Got the wings mounted on the RV4. Getting ready to set the incidence > angle, etc. Went to mount the flap and have interference between the > lower fuselage skin and the bottom flap skin on the fuse side. Looks > like I will have to cut the bottom fuselage skin flush with the fuselage > side to get enough clearance and maybe the flap skin also. Will get the > plans out and study some more. > > Any short cuts or advice will be welcome. > > Thanks Earl RV4 ________________________________________________________________________________
From: DAVENDANA1(at)aol.com
Date: Dec 05, 1999
Subject: Re: More Radio
I haven't been following this, so it may be a very dumb question. Have you tried another headset (or mike)? Good luck! Dave Funk ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)home.com>
Subject: Re: Carb Ice
Date: Dec 05, 1999
I believe I experienced carb ice yesterday morning in my RV-6. Not certain as my carb temp probe isn't hooked up yet. But on run-up, when I pulled the carb heat, the tach went down about 100 RPM, then slowly came back up about 50 RPM. OAT was 323 degrees with a 0 degree temp/due point spread. Randall Henderson, RV-6 N6R (~50 hrs) Portland, OR http://www.edt.com/homewing ________________________________________________________________________________
Date: Dec 05, 1999
From: Hal Kempthorne <kempthorne(at)earthlink.net>
Subject: Re: RV8 N94BD weigh-in
> >Of course you did weight it inside out of the wind so those wonderful >airfoils didn't change the true weight either. I suppose this makes sense but isn't it true that unless the wind reaches the stall speed, NO lift is generated? hal ________________________________________________________________________________
Date: Dec 05, 1999
From: Brian Huffaker <bifft(at)xmission.com>
Subject: Re: RV8 N94BD weigh-in
>>Of course you did weight it inside out of the wind so those wonderful >>airfoils didn't change the true weight either. >I suppose this makes sense but isn't it true that unless the wind reaches >the stall speed, NO lift is generated? >hal Not true. Any airflow over the wing generates lift, stall speed is where the maximum available lift matches the wieght of the plane. A light breeze would be enough the make the plane weigh incorrectly. Brian Huffaker, DSWL (bifft(at)xmission.com) President and Founder Friends of P-Chan RV-8 80091 Riviting 2nd Wing. 1/5 Starduster II N23UT flying ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: RV8 N94BD weigh-in
Date: Dec 05, 1999
Not true! Anytime air is flowing over an airfoil it is generating lift. It might not be enough to lift the airplane but it is enough to overcome some of the pull of gravity making it appear to weigh less. Stall is when the airflow due to angle of attack becomes turbulent and the lift is greatly reduced. Even then there still will be some lift. If there wasn't your plane would not go into a spin because of the unequal lift between the two wings. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Hal Kempthorne <kempthorne(at)earthlink.net> Date: Sunday, December 05, 1999 12:09 PM Subject: Re: RV-List: RV8 N94BD weigh-in > >> >>Of course you did weight it inside out of the wind so those wonderful >>airfoils didn't change the true weight either. > >I suppose this makes sense but isn't it true that unless the wind reaches >the stall speed, NO lift is generated? > >hal > > ________________________________________________________________________________
From: "Bill Shook" <skydiven(at)bellsouth.net>
Subject: steel braided lines
Date: Dec 05, 1999
Stay away from steel braided hoses unless you intend to change them every year. Why you ask? When that pretty steel braid breaks down a little you have several strands of steel poking in the rubber beneath it. You won't see it coming, likely the broken strands are in the center...but when it bursts - BAD DAY. I've seen this in so many race cars over the last several years (steel brake lines) that most of us are back to running the not so stiff, but much safer rubber lines. Like I said, that is unless you have the budget and time to replace them fairly often as a precautionary measure. Bill ________________________________________________________________________________
From: "Doug Weiler" <dougweil(at)pressenter.com>
Subject: RV-4/RV-8 rear seat throttle
Date: Dec 05, 1999
Fellow Listers: Working on the interior of my RV-4. I plan to install a rear seat throttle assembly of some type (only need a throttle lever). I have made a very nice custom throttle quadrant for the front (ala Lyle Hefel's RV-4 and RV-8). I was wondering if anyone has any specific ideas on the methods to fabricate and connect a rear seat throttle lever to the front one. I know the RV-8 has a factory designed rear seat throttle and perhaps this (or its design) may be adaptable to the -4. Any comments or does anyone have any photos on their website of a RV-8 rear seat throttle arrangement? Doug =========== Doug Weiler Hudson, WI 715-386-1239 dougweil(at)pressenter.com ________________________________________________________________________________
Date: Dec 05, 1999
From: Matt Orr <morr(at)vt.edu>
Subject: Re: RV8 N94BD weigh-in
Nope it's not true! ;-) Here's why: Stall is the minimum velocity which you can make lift equal to the weight of the aircraft. The stall speed is dependent only on the atmospheric conditions (density), weight, and wing area of the aircraft. It is fixed with respect to the angle of attack that the aircraft stalls at. (RV's have a NACA 23012 (I thought), CLmax is ~1.8 @ ~18 degrees for wing alone from "Theory of wing Sections") Lift is generated by the wing at any airspeed dependent on the angle of attack (AOA). It is true that if you are at the zero lift AOA for the configuration you will have zero lift, even with flow over the aircraft. If you are at any velocity and not exactly at the RV-8 zero lift AOA (whatever that is) you will be generating lift, perpendicular to the direction of the wind incident to the wing. Lift=CL*.5*rho*v 2*s CL=lift coefficient rho=density v=velocity s=wing area Stall is when the MAXIMUM CL (lift coefficient) is generated, the drag simply goes up a huge amount. Beyond stall (flow separation from the wing) you can still generate lift but the drag is quite high and the lift coefficient drops off. It can even start to climb back up but the power required is huge as the drag is very high. Probably more info. then you wanted. Matt > > I suppose this makes sense but isn't it true that unless the wind reaches > the stall speed, NO lift is generated? > > hal ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Dec 05, 1999
Subject: Re: More Radio
>Radio trouble shooting still...... Don't know if you've tried it yet but your trouble may be in the antenna cable. Test the resistance between the center wire and the sheilding: there should be no ohm reading. It could still be the cable. Junk it and make a new one. I had a batch of bad cable once and the radio did sort of ok (about 5 miles was it). Replacing the whole cable made it a new radio. Maybe so, maybe no..... Michael ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: steel braided lines
Date: Dec 05, 1999
> > >Stay away from steel braided hoses unless you intend to change them every >year. Why you ask? When that pretty steel braid breaks down a little you >have several strands of steel poking in the rubber beneath it. You won't >see it coming, likely the broken strands are in the center...but when it >bursts - BAD DAY. I've seen this in so many race cars over the last >several >years (steel brake lines) that most of us are back to running the not so >stiff, but much safer rubber lines. Like I said, that is unless you have >the budget and time to replace them fairly often as a precautionary >measure. > >Bill Not only is this an issue, but the braid will saw it's way through anything it rubs on with engine vibration providing the motivation. So, those that do have them, make sure they will not rub on the engine mount, wires, primer lines, control cables, etc. Like anything, they do a fine job as long as they aren't neglected. Brian Denk RV8 N94BD two braided hoses in my engine compartment. ________________________________________________________________________________
Date: Dec 05, 1999
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Re: RV4 Horiz Stab gap question
I have 1/16 on my rv4 but am probably a year away from flying. Mkraus01(at)aol.com wrote: > > > One quick question, how big of a gap should I leave between the horizontal > stabilizer and the outboard portion of the counterbalance rib?? I was > worried about this area flexing in flight and binding the elevator if the gap > is not sufficient. I could not find this dimension on the plans. (I am > referring to the gap between the HS skin and the counterbalance rib skin) > Thanks > -Mike > ________________________________________________________________________________
From: dralle(at)matronics.com (Matt Dralle)
Date: Dec 05, 1999
tailwind-list(at)matronics.com, pietenpol-list(at)matronics.com
Subject: List Support Auction Continues...
Dear Listers, The List Support Auction is still underway with about 5 or 6 days left. I have been receiving a number of nice bids on the items generously donated by Steven and Archie. I've listed the items up for auction again below and have included the current high-bid. If there is an item that you wish to bid on, please send your BID along with the DESCRIPTION OF THE ITEM you are bidding on to the following email address: bids(at)matronics.com Thanks again to Steven and Archie for donating these items to support the List. And thank you to those that have sent in bids so far! Best regards, Matt Dralle Email List Admin. ===================================================================== Steven DiNieri (capsteve(at)wzrd.com) has generously offered to donate a CoolStart RS 700-II to support the Lists this year. This unit retails for $299. I have put a brochure for the product up on the web server and you can have a look at it here: http://www.matronics.com/contribution/rsflyer.jpg NEW: $175 * CoolStart RS 700-II ===================================================================== Archie (archie97(at)earthlink.net) has generously donated a number of interesting items to the Support the List cause this year. Each of them are described below. If you have additional questions, please email Archie directly at: archie97(at)earthlink.net > Upon receipt of the donation amount, items will be shipped. > No reasonable offer refused! > Unreasonable ones considered! NEW: - * Heated Pitot Tube, 24v. "L" shaped. - * Aero Instruments #5814-2 - * Flap Motor w/ adjustable stops. 24v. - * Comm.Aircraft Prods. #D145-00-35-7 USED: $45 * Narco Transponder AT5-A - * Astronautics amplifier servo 53-005-214 mod#P1SA $15 * Narco altitude reporter. to 25k' Model# AR500 - * King KS-505 power supply modulator - * RCA AVQ55 Weather radar antenna MI 591000 ===================================================================== -- Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94551 925-606-1001 Voice | 925-606-6281 FAX | dralle(at)matronics.com Email http://www.matronics.com/ W.W.W. | Featuring Products For Aircraft ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)home.com>
Subject: Re: Carb Ice
Date: Dec 05, 1999
>I believe I experienced carb ice yesterday morning in my RV-6. Not certain >as my carb temp probe isn't hooked up yet. But on run-up, when I pulled the >carb heat, the tach went down about 100 RPM, then slowly came back up about >50 RPM. OAT was 323 degrees with a 0 degree >temp/due point spread. Oops -- that should read 32 degrees... ! Randall ________________________________________________________________________________
Date: Dec 05, 1999
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Re: bottom flap skin
I got the same problem but have not aligned the wing to make sure I dont have any sweep back. Thats my next step. Thanks EArl WAYNE BONESTEEL wrote: > > > Earl I had to jog the skin just as Joe Hine indicated to get the flap > trailing > edge up where it aligned with the aileron and fit the wing form cutout. > > What I want to inject, when drilling the rear spar hole make sure the > wing is not pushed back (swept aft) as I believe I did, because it puts > the flap tie rod mount plate too close to the fuselage, mine actually hit > and I had to peen the fuselage skin for clearance, looks OK now but what > a pain. > > Wayne > > EARL FORTNER wrote: > > > Got the wings mounted on the RV4. Getting ready to set the incidence > > angle, etc. Went to mount the flap and have interference between the > > lower fuselage skin and the bottom flap skin on the fuse side. Looks > > like I will have to cut the bottom fuselage skin flush with the fuselage > > side to get enough clearance and maybe the flap skin also. Will get the > > plans out and study some more. > > > > Any short cuts or advice will be welcome. > > > > Thanks Earl RV4 > ________________________________________________________________________________
From: "Eric M. Strandjord" <emstrand(at)isd.net>
Subject: SourceRV.com == Jeremy Benedict
Date: Dec 05, 1999
:-) ON: Listers, I have been "lurking" on the list for about two months (and sent a contribution). The list is a gold mine of very useful information. However, like any "mine" many tons of ore must be processed to glean mere ounces of pure gold. The RV list is what we in the business call an "un-moderated" list, anything goes. Threads about exploding mice, 767 elevator splits, saving whales, the amount of water in liquid ozygen, and other non-related issues are interesting reading but dont help me finish my project. Dont get me wrong, the first thing I do when I get home from work every night, is check email for the RVlist digest -- it's interesting, fun, and contains good information. If I thew out 99% of it, comments from "electric Bob", Sam, and a few other experts justify "mining" through the rest. :-) Still on: For less than half the sum I contributed to this list, Jeremy is providing MODERATED service, fully supported and sanctioned by the manufacturor. Do the math. Clients of mine invest between 5 and 20 thousnad dollars on hardware, software, and services just to get a basic "commerical duty" web site up and running. I sure that Jeremy has made a simlar investment -- without any guarntees of success. (Nit Picker Alert -- yes, he can share the investment with his other ventures) If 1000 Rv builders sign up at $24 a shot (SourceRV's gross income is at best -- pretty small), he still has to pay off his investment, pay for his connection, gather and post content, and pay taxes! I can only hope that the other portions of his company will be able to subsidize the RV portion. :-) Still on: I had the pleasure of meeting Jeremy at OSH this year. (I had just sent in a big check to Van for a tailkit and 8QB the week before). I had a simple question about the plans. Everyone else in the Van's booth had wilted from the heat and was "hiding" behind the counter avoiding eye contact. :-) Jeremy was the only one that was approachable, outgoing, intellegent, and downright friendly. He told me that the QB had a two page addendum to the preview plans that explained the construction sequence and differences. As we talked about Van's existing web site, I positively commented about its organization and content, but wished it could be more up-to-date. I also told him that if he ever wanted to move to Minnesota, a developement job would be wating for him. :-) :-). (I learned later that he did most (all?) of the work without compensation and felt badly that I had asked for more). From this experience and the helpful comments Jeremy has made to this list, I'm sure he a selfless giving person. (IMHO) I think everyone would agree that VAN's new Site is a vast improvent on an already good thing. I think that SourceRV and the RVlist complement each other very well. User experience and entertainment from one. Plans updates, unbroken links, drawings, and a library of pictures (each worth a thousand words), etc. from the other. Sorry about the long note. My experience with Mr. Benedict was so positive, i had to share it. :-) still on!.. Bye... Eric RV8QB (81057 - 586) (polishing HS609PP's) ________________________________________________________________________________
Date: Dec 05, 1999
From: "dgmurray" <dgmurray(at)telusplanet.net>
Subject: Re: steel braided lines
Subject: Re: RV-List: steel braided lines >>Stay away from steel braided hoses unless you intend to change them every >>year. Why you ask? When that pretty steel braid breaks down a little you >>have several strands of steel poking in the rubber beneath it. You won't >>see it coming, likely the broken strands are in the center...but when it >>bursts - BAD DAY. I've seen this in so many race cars over the last >>several >>years (steel brake lines) that most of us are back to running the not so >>stiff, but much safer rubber lines. Like I said, that is unless you have >>the budget and time to replace them fairly often as a precautionary >>measure. >> >>Bill > > >Not only is this an issue, but the braid will saw it's way through anything >it rubs on with engine vibration providing the motivation. So, those that do >have them, make sure they will not rub on the engine mount, wires, primer >lines, control cables, etc. Like anything, they do a fine job as long as >they aren't neglected. > >Brian Denk >RV8 N94BD >two braided hoses in my engine compartment. So - if steel braided lines are so bad, why is Van's supplying these to us. Is it only because he wants repeat business each year? I doubt it. Van's has been straight up with all the builders I have talked to and I cannot see him sending out a product that could potentially cause failures on an aircraft. I have all my lines made out of the steel braided variety and all are covered with firesleeve. Do you think that the hoses still need replacing every year? Doug Murray RV-6 Just a few more million finishing touches :-)) Southern Alberta ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)shuswap.net>
Subject: Carb heat
Date: Dec 05, 1999
Would like to pass on my experience with carb ice over the years and how I have handled it. Most of my flying has been in the cooler temperature range with a lot of it north of 60 degrees and above the arctic circle were carb ice is a consideration at any time of the year. Have found that any carburated engine weather it be a small horizontally opposed or a twin row radial will develop carb ice given the right conditions. With all certified aircraft that I have flown the carb heat available was always adequate provided carb ice was detected early enough. With a fixed pitch prop in cruise a slow loss of RPM was it. With a constant speed a slow loss of manifold pressure was it. With the constant speed I found you have to be alert or your first warning might be a rough running engine. If carb ice is suspected I always use full heat, if there is much of a build-up this is followed by some roughness as the water passes through. Usually return to cold and apply again as required. If conditions dictate I use full carb heat in the circuit when landing and in the case of a go around back to full cold. Use of carb heat with engines equipped with automatic carburetors is another subject that I won't get into here as this will already be to long. I have never experienced any signs of ice with fuel injection. Don't know if it is possible without a venturi, someone else may wish to comment on this. When I built my RV 6 and installed Vans filtered air box the question was what to do about carb heat and a alternate air source. I will not fly a carburated engine without a source of carb heat. I put a flapper valve in the throat of the air box hinged to the top with a depth of 2 1/2 inches from the hinge pin and a width of 4 inches leaving about a 1/16 inch clearance around the flapper when open and 90 degrees to the top surface of the air box. I used 040 for the flapper and a piece of MS20001-4 extruded hinge. When installed this put this opening very nearly under the two exhaust pipes on the crossover system. I decided to do some testing with this before deciding on a positive source of carb heat. One that I remember in particular was a flight of some 2 1/2 hours over flat country in marginal VFR conditions and temperatures around the freezing mark with occasional light precip. resulting in some leading edge ice. Very little carb ice was detected and was easily handled by opening the flapper and using the heat from inside the cowling and the crossover exhaust. By leaving the heat on all the time there was no carb ice and only a slight change in performance. It seems to me that the RV 6 engine installation (in my case a 0360) with Vans airbox is not prone to carb ice. While this flapper valve seems to do the job I still feel that a positive source of carb heat is the correct way to go. I don't get a significant drop in RPM when it is used. I do believe it serves as an excellent means of getting rid of impact snow when flying in these conditions. In the event of a bird strike I feel two things would happen. If the bird or pieces were small enough to get through the cowl inlet it shoudn't be to serious due to the excellent design of Vans air box with the full circle filter and large area. On the other hand if the bird was large enough plug the entrance in the scoop then the flapper would serve as a alternate source. I have never experienced a bird strike through a propeller in 55 years of flying so don't feel it is a real concern. I converted to fuel injection before installing a positive carb heat source so still use my flapper valve for both heat and alternate air. I use it on the ground in dusty conditions to give the filter a bit if a break. Had to replace the hinge at the 450 hour mark. Again just my experiences and thoughts and hope I didn't bore you. Eustace Bowhay Blind Bay, B.C. RV 6 & 6A in progress ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: steel braided lines
Date: Dec 05, 1999
> >Not only is this an issue, but the braid will saw it's way through >anything > >it rubs on with engine vibration providing the motivation. So, those that >do > >have them, make sure they will not rub on the engine mount, wires, primer > >lines, control cables, etc. Like anything, they do a fine job as long as > >they aren't neglected. > > > >Brian Denk > >RV8 N94BD > >two braided hoses in my engine compartment. > > > So - if steel braided lines are so bad, why is Van's supplying these to >us. >Is it only because he wants repeat business each year? I doubt it. Van's >has >been straight up with all the builders I have talked to and I cannot see >him >sending out a product that could potentially cause failures on an aircraft. >I have all my lines made out of the steel braided variety and all are >covered with firesleeve. Do you think that the hoses still need replacing >every year? > >Doug Murray RV-6 Just a few more million finishing touches :-)) >Southern Alberta > > As for my comment, I still consider them to be outstandingly durable and reliable, which is why I used two of them for my fuel pressure and oil pressure hoses from the engine to the gauge or sender. In your installation, with firesleeve encasing them, the chafing issue is taken care of. All aircraft hoses have a finite lifetime. The most recent information on the subject I have seen says to replace all the hoses at major engine overhaul, or five years, whichever comes first. This applies to rubber hoses with inner stainless braid. Sounds like a good idea to me. Have fun with all the millions of details before you fly! I know exactly what that's like. ;) Brian Denk ________________________________________________________________________________
Date: Dec 05, 1999
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Re: flaps
EARL FORTNER wrote: > > Chuck, I just checked the incidence per SK-51 drawing and the wing needs > to be raised aprox 1/4 inch at rear, however the rear carry through spar > is bottomed out on the lower wing skin. If I go with this which way and > how much do I raise the front of the stab. It cannot be lowered and to > raise the rear of stab would require drilling new mount holes which I do > not want to do. > > I will go back and read your orginal reply and see if I can figure it > out. > > Thanks, Earl > > Chuck Brietigam wrote: > > > > Earl, just as a side note. I would suggest aligning you wings so that > > the wings and flaps align perfectly with the bottom of the fuselage > > (without having to make any "joggle").Yes, the angle of incidence > > between the wing and the fuselage will be different than what Van's > > drawning states, but the fuselage/wing intersection will be cleaner and > > easier to build. Now find your new angle of incidence and transfer any > > increase or decrease in the wing/fuselage angle of incidence back to the > > horizontal stab. That way you have not changed the relative angle > > between the two flying surfaces. The only thing you have altered is the > > angle of attack of the fuselage flying through the air. I doubt that you > > will ever be able see any marked change in the aircraft overall > > performance since I would imagine your overall change to the wing was > > absolutely miniscule to begin with. I know of many flying RV-3,4,and 6's > > to have this change.If this is confusing, please call me at > > 502-254-5079. Chuck Brietigam ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV-6A O-360 FAB
In a message dated 12/4/99 9:41:49 PM Pacific Standard Time, rv6flier(at)yahoo.com writes: << What have others done to increase the clearance between the Filtered Air Box and the training wheel gear leg? :-) I have been told that the GBI video shows cutting the filter to allow more clearance at the carb. >> I marked the area, heated the bedpan airbox with a heat gun and then pushed a piece of tubing into it at the correct angle to form a dimple in this area. It clears by .375". -GV ________________________________________________________________________________
From: "A. W. Triff" <tekrep(at)wans.net>
"Rocket List"
Subject: RV-8 HS Stab Rivet Spacing/Alignment
Date: Dec 05, 1999
HI Listers, I'm having a little problem with my RV-8 HS stabilizer skeleton and am wondering if anyone else has come across the same problem. When laying the skins over the skeleton, the intersection of the HS404 (center tip rib), HS405 (center aft rib), HS602 (HSFWD spar channel) and HS814 (reinforcing angle at FWD spar center), the first rivet FWD of the FWD spar on the tip rib does not have sufficient material in the rib for proper edge distance and actually hits the spar on one side (the "ear" on the HS814 bottom reinforcing angle is a bit longer than the other side but is at the proper dimension per the plans). and is right next to the spar ear on the other side. This is where Van tells you to cut a notch in the rib for the spar channel, but then they put a rivet right in the middle of the notch. I'll either have to file the spar ear way down, or move the rivet out on the HS404 rib, any suggestions? Similarly, the aft center rib (HS405) does not seem to have enough material in the end of the rib flange (but the rib does fit in place) to give proper edge distance for a rivet where the skin says it should be. Since I believe this area is under a fairing, can I put a rivet in a little farther out on the rib? Would this compromise structural integrity (it doesn't seem like much of a compromise). Should I put a rivet in it anyway since there will be a skin hole or can I leave the hole empty? Thanks for any input you may have, Wes Triff tekrep(at)wans.net RV-8 tail/F-1 Rocket Atlanta ________________________________________________________________________________
From: PANELCUT(at)aol.com
Date: Dec 05, 1999
Subject: ENGRAVING FUEL CAPS LAST CHANCE TO VOTE
Group I have gotten a great response to the fuel cap delima, but there are a few who have not responded to the last post. If I do not hear from you they will be engraved just like Paul's. Thanks to everyone who got back to me quickly, this has been a nightmare but your response has eased my mind. Thanks to all Steve Davis The panel pilot ________________________________________________________________________________
From: "christopher huey" <clhuey(at)sprynet.com>
Subject: Re: steel braided lines
Date: Dec 06, 1999
Braided hoses are used extensively throughout the aerospace industry. If you ever look into the wheel well of any commercial jetliner you will see steel braided hoses. They are used for brakes, hydraulics systems, etc...I would have no problem using steel braided hoses on any aircraft system which I thought necessary. And a added note: The last fuel problem I had was with a hard Alum fuel line....small crack at the flare. As said before all components of a airplane need to be inspected on a regular basis... C.H. ---------- > From: dgmurray <dgmurray(at)telusplanet.net> > To: rv-list(at)matronics.com > Subject: Re: RV-List: steel braided lines > Date: Sunday, December 05, 1999 3:24 PM > > > Subject: Re: RV-List: steel braided lines > > > >>Stay away from steel braided hoses unless you intend to change them every > >>year. Why you ask? When that pretty steel braid breaks down a little you > >>have several strands of steel poking in the rubber beneath it. You won't > >>see it coming, likely the broken strands are in the center...but when it > >>bursts - BAD DAY. I've seen this in so many race cars over the last > >>several > >>years (steel brake lines) that most of us are back to running the not so > >>stiff, but much safer rubber lines. Like I said, that is unless you have > >>the budget and time to replace them fairly often as a precautionary > >>measure. > >> > >>Bill > > > > > >Not only is this an issue, but the braid will saw it's way through anything > >it rubs on with engine vibration providing the motivation. So, those that > do > >have them, make sure they will not rub on the engine mount, wires, primer > >lines, control cables, etc. Like anything, they do a fine job as long as > >they aren't neglected. > > > >Brian Denk > >RV8 N94BD > >two braided hoses in my engine compartment. > > > So - if steel braided lines are so bad, why is Van's supplying these to us. > Is it only because he wants repeat business each year? I doubt it. Van's has > been straight up with all the builders I have talked to and I cannot see him > sending out a product that could potentially cause failures on an aircraft. > I have all my lines made out of the steel braided variety and all are > covered with firesleeve. Do you think that the hoses still need replacing > every year? > > Doug Murray RV-6 Just a few more million finishing touches :-)) > Southern Alberta > > > > ________________________________________________________________________________
From: "Bill Shook" <skydiven(at)bellsouth.net>
Subject: to steel or not to steel
Date: Dec 05, 1999
Keep in mind that a race car takes more abuse than the average airplane and the brake lines are flexed more often than the ones under your RV's cowl. The steel braided lines do fail, much quicker than the rubber variety, but how long they will last in an airplane is something you can decide for yourself. I have now seen two VERY expensive Porsche race cars go flying off the track at over 130 mph do to stainless brake lines bursting and the subsequent loss of control. One unfortunate soul got to write off his $150k car due to a $30 brake line. The braid is there to minimize tube expansion under heavy pressure....what it also does is hide the hose from any kind of inspection as well as holding any abrasive dirt in contact with the rubber so that flexing can cause damage. This is one of those subjects where the builder obviously just makes a choice, like whether or not to use pop rivets in the empennage. Just because an obviously talented manufacturer supplies or recommends it does not mean it can not be improved upon, or that other industries have not tested that product far more than Vans has. I'm not claiming to be an authority on this subject, just giving up a point of consideration. Bill >-----Original Message----- >From: owner-rv-list-server(at)matronics.com >[mailto:owner-rv-list-server(at)matronics.com]On Behalf Of dgmurray >Sent: Sunday, December 05, 1999 4:25 PM >To: rv-list(at)matronics.com >Subject: Re: RV-List: steel braided lines > > >Subject: Re: RV-List: steel braided lines > > >>>Stay away from steel braided hoses unless you intend to change them every >>>year. Why you ask? When that pretty steel braid breaks down a >little you >>>have several strands of steel poking in the rubber beneath it. You won't >>>see it coming, likely the broken strands are in the center...but when it >>>bursts - BAD DAY. I've seen this in so many race cars over the last >>>several >>>years (steel brake lines) that most of us are back to running the not so >>>stiff, but much safer rubber lines. Like I said, that is unless you have >>>the budget and time to replace them fairly often as a precautionary >>>measure. >>> >>>Bill >> >> >>Not only is this an issue, but the braid will saw it's way >through anything >>it rubs on with engine vibration providing the motivation. So, those that >do >>have them, make sure they will not rub on the engine mount, wires, primer >>lines, control cables, etc. Like anything, they do a fine job as long as >>they aren't neglected. >> >>Brian Denk >>RV8 N94BD >>two braided hoses in my engine compartment. > > > So - if steel braided lines are so bad, why is Van's supplying >these to us. >Is it only because he wants repeat business each year? I doubt it. >Van's has >been straight up with all the builders I have talked to and I >cannot see him >sending out a product that could potentially cause failures on an aircraft. >I have all my lines made out of the steel braided variety and all are >covered with firesleeve. Do you think that the hoses still need replacing >every year? > >Doug Murray RV-6 Just a few more million finishing touches :-)) >Southern Alberta > > ________________________________________________________________________________
From: DFCPAC(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV3-List: Re: RV3-List Digest: 12/04/99
hi bob,bob, and rob, good to here from all of you. how have you been rob? i guessed the rv3 newsletter was a little hard to tackle. i agree with all of you, we should use the rv3 list. the regular rv list is ok but mostly talk about 6's and eights. i'm located on long island in new york. i did not build my rv3a i purchased it from randy compton in fl. but the way he bought a pitts s1 and is very unhappy with it. he wanted to buy his rv back. i've had it for about 7 months and it's one heck of a machine. i love it. i really flys great. i've just started doing basic aerobatics with it. you gotta see this thing roll. don't even need rudders plant your feet on the floor pitch up a little and bang the stick over. i have an 0-320 lyc. and i can cruise at 165 knots at 2400 rpm at 7 gallons an hour. climb rate is over 2000 fpm. and the thing is like a pussy cat to fly. rob, i took a look at installing the sliding canopy i think to leave well enough alone. anyway i have an antenna right behind the canopy that i would have to move. i'm just gonna leave it like it is. so how's the restoration going? i really like to see this list work out it's always nice to chat with others that have the same plane. take care dan carley rv3a-148cw i'll inform chuck about this list. did you get the new calender yet. chuck's rv3 is the first one listed ________________________________________________________________________________
From: "Rick Jory" <rickjory(at)email.msn.com>
Subject: Ground Adjustable Rudder Pedals - 8A
Date: Dec 05, 1999
Anyone building an 8A with ground adjustable rudder pedals . . . the plans show a left and right "F-802G" (drawing OP-3). These are also shown on Drawing 24. However, on my QB kit these are not there . . . and it looks like these may have a function for the tail dragger version but not the tri. Has anyone run up against this? The aft end of F-8108 (L & R) are bent to provide clearance for both of these--but my 8A QB doesn't have them. This may be a question for Van's. Thanks in advance, Rick Jory, Highlands Ranch, Co RV8A QB . . . fuselage ________________________________________________________________________________
From: LeastDrag(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV3-List: Re: RV3-List Digest: 12/04/99
________________________________________________________________________________
From: LeastDrag(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV3-List: Re: RV3-List Digest: 12/04/99
Hello Dan, I haven't seen too much on this list either. But I keep watching. Jim Ayers N47RV RV-3 SN 50 Maroon Marauder (down for electric system overhaul & annual, fuel system change completed) SN 306 RV-3 (basic structure complete, need to complete rudder & elevator) ________________________________________________________________________________
From: flyhars(at)ibm.net
Subject: Re: steel braided lines
Date: Dec 05, 1999
The use of steel hoses are the best you can buy for airplanes. Not comparing it to a race car, All the large transports I flew used them with almost no failure in the hoses themselves usually the failure was at the flare end. They are used almost always in the engine compartments of jet engines, and they are used for lines on the gear of B-747, and there they really shake, but of course they don't shake like a race car. I would not have any fear of using them, as I did on my last RV, and plan on using them again in my latest project, If I can afford them. They are the best. Of course this is only and old Flight Engineer talking. Harvey Sigmon RV-6AQB - Rudder Stuff. ----- Original Message ----- From: dgmurray <dgmurray(at)telusplanet.net> Sent: Sunday, December 05, 1999 4:24 PM Subject: Re: RV-List: steel braided lines > > Subject: Re: RV-List: steel braided lines > > > >>Stay away from steel braided hoses unless you intend to change them every > >>year. Why you ask? When that pretty steel braid breaks down a little you > >>have several strands of steel poking in the rubber beneath it. You won't > >>see it coming, likely the broken strands are in the center...but when it > >>bursts - BAD DAY. I've seen this in so many race cars over the last > >>several > >>years (steel brake lines) that most of us are back to running the not so > >>stiff, but much safer rubber lines. Like I said, that is unless you have > >>the budget and time to replace them fairly often as a precautionary > >>measure. > >> > >>Bill > > > > > >Not only is this an issue, but the braid will saw it's way through anything > >it rubs on with engine vibration providing the motivation. So, those that > do > >have them, make sure they will not rub on the engine mount, wires, primer > >lines, control cables, etc. Like anything, they do a fine job as long as > >they aren't neglected. > > > >Brian Denk > >RV8 N94BD > >two braided hoses in my engine compartment. > > > So - if steel braided lines are so bad, why is Van's supplying these to us. > Is it only because he wants repeat business each year? I doubt it. Van's has > been straight up with all the builders I have talked to and I cannot see him > sending out a product that could potentially cause failures on an aircraft. > I have all my lines made out of the steel braided variety and all are > covered with firesleeve. Do you think that the hoses still need replacing > every year? > > Doug Murray RV-6 Just a few more million finishing touches :-)) > Southern Alberta > > ________________________________________________________________________________
Date: Dec 05, 1999
From: Denton Harjehausen <harje(at)proaxis.com>
Subject: Re: steel braided lines
Flight test is coming soon for me. Hoses worry me. I was told unofficially by a FAA man that the RV-8 that crashed locally had no oil. He said there was nothing official about where the oil went. I did as many other did locally and made my own oil and fuel lines. I did them with Aeroquip 303 hose and 491 fittings, then firesleeved them. One of the local EAA tech guys instructed me on it. This morning I was doing another engine run with the cowl off. I noticed some specks of oil appearing on the canopy. I shut down and investigated. There was oil scattered around the aft left side of the engine & firewall. It appears to be a hose as the most was around one of the firesleeves ends, but I did not have time to start trouble shooting. That will start tomorrow. I had excercised the prop for the first time. It could be a prop govenor gasket...??? Have you vets assemebled your own hoses using Aeroquip 303 & 491? I am getting second thoughts on my hoses! Have a great Day! Denny Harjehausen Lebanon, OR RV-6 ________________________________________________________________________________
Date: Dec 05, 1999
From: Denton Harjehausen <harje(at)proaxis.com>
Subject: Re: Carb heat
Thanks, Eustace! I have wondered since I returned to carb. power why there wasn't an electrically heated system. There seems to be a lot of off field landings/crashes blamed on carb. ice. If it isn't caught in time as we all know there is no heat to clear the passage. Though it does seem like an electric heated system would be another problem to add to the already complex and costly safety sytems of airplanes. And it seems to be more likely in some aircraft then others. A friend of mine had it happened to him in a Tomahawk a couple years ago here in Oregon. He said it happened very suddenly with no warning. The engine started to lose RPM, he pulled the carb heat and it quit. They were low and had little choice in landing fields. He and his wife did walked away with scatches and bruises, but the plane was junk. I have heard of a couple of others in the last couple years, locally. I don't have the prop time you have, Eustace, but I had it happen one time in my prop time, in a Luscombe, in the '50, low over Long Beach, Calif. It lost a lot of power suddenly, I pulled the Carb heat, it got worst, I was looking for some soft place in the city to land and then it roared back to life. It left me with nightmares for awhile, plus a real interest in the subject. Have a great Day! Denny Harjehausen Lebanon, OR RV-6 ________________________________________________________________________________
Date: Dec 06, 1999
From: pagan <pagan(at)cboss.com>
Subject: Re: Ground Adjustable Rudder Pedals - 8A
Yes Rick, I believe the F-802G is only on the taildragger. I used the ground adjustable pedals and simply placed a spacer at the aft end. Bill Pagan N565BW still waitin on the FAA "The original RV-8A builders page on the web" http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html > >Anyone building an 8A with ground adjustable rudder pedals . . . the plans >show a left and right "F-802G" (drawing OP-3). These are also shown on >Drawing 24. However, on my QB kit these are not there . . . and it looks >like these may have a function for the tail dragger version but not the tri. >Has anyone run up against this? The aft end of F-8108 (L & R) are bent to >provide clearance for both of these--but my 8A QB doesn't have them. This >may be a question for Van's. > >Thanks in advance, >Rick Jory, Highlands Ranch, Co >RV8A QB . . . fuselage > > ________________________________________________________________________________
Date: Dec 05, 1999
Subject: Oil cooler air for cabin heat
From: "William R. Davis Jr" <rvpilot(at)juno.com>
Listers, Have followed with interest the thread about using oil cooler exit air for cabin heat. In spite of what the nay-sayers out there are saying, it will work---up to a point. It depends on what climate you are operating in. I have been using this system in my RV-4 for several years with success. If I lived in Minnesota I wouldn't consider it. Sure, I live in SW Florida but I make a lot of trips to NJ and New England and find that the system is more than adequate unless you are flying under a cloud deck (no solar heating) and the temp. is 20 deg. F. or less. Advantages are: Freedom from worry about CO poisoning "softer" more pleasant heat, not scorching as exhaust heat is Disadvantages are: less heat output More complicated to build, you have to put a butterfly valve on the output side of the oil cooler to force the exit air into the cabin heat box. this disadvantage is at least partially offset by the fact that the butterfly valve can be used to regulate the oil temp. to some degree. If using this system, it would be important to seal up all the air leaks into the cabin as much as possible, this would be important if using a normal system too. It may not be for everybody, but it works for me. It's going in my new RV-8 Regards, Bill RV-4 N66WD RV-8 Cowling Stuff ________________________________________________________________________________
Date: Dec 05, 1999
From: meketa <acgm(at)gvtc.com>
Subject: Re: RV-8 seat floor questions
> Pardon my "dumminess" but do the F829 footwell flanges and flooring go > under or on top of the F-830 and F-831 seat floors. I can't tell from > DWG 29 or the video. If I want to make the floors removable (I read > >the archives on this), should I use #8 nutplates or are #6 beefy >enough? > Thanks, > Phil Smith, 80691 On the plans, the F829 front floor and the foot wells are screwed down and the F830 and 831 rear floors are pop riveted down. This would require that that the footwells would go on top of the rear floor. The plans call for #8 screws to be used. I had initially planned on making the rear floors removable with #6 screws. After installing the nutplates for the front I changed my mind. The nutplates against the outside skin are a pain to dimple and buck the rivets. The rear has even less room to work. This is on the quick build with the outside skins installed. Do the front nutplates before you commit on the rear floor nutplates. There are several nutplates on the front floor that call for K1000-8 double leg nutplates which are in very tight corners. In these areas I installed MS21051-L08 single leg nutplates. Only two came with the kit. I also started using Oops rivets from Avery to hold down the nutplates. This makes countersinking in tight areas much easier. Stripping or breaking the #6 and #8 screws is not a problem if you run a tap thru all floor nutplates before installing them. This cleans out the locking crimp. The screws can then be installed by hand. I will install plastic washers under the screws for paint protection and to act as lock washers. George Meketa RV-8Q fuselage P.S.: tricycles are for babies ________________________________________________________________________________
Date: Dec 05, 1999
From: Jeff Point <jpoint(at)execpc.com>
Subject: Rudder Leading Edge
Just got done rolling the leading edge of the rudder. One side turned out beautifully, the other has a slight crease in the skin at the edge of the spar flange, as cautioned about in the manual. Anybody had any success getting this crease out, if so how? Or, should I not be too concerned about it. This crease is not much, can be felt by hand, but not visible unless you look closely under good light. Jeff Point jpoint(at)execpc.com -6 rudder Milwaukee, WI ________________________________________________________________________________
Date: Dec 05, 1999
From: Don McNamara <mcnamara(at)sbt.infi.net>
Subject: Re: Ground Adjustable Rudder Pedals - 8A
Rick-- I ran into this just the other night. I exchanged my in-flight adjustable rudder assembly for the ground-adjustable version, and began the installation. I noticed that Moe Colontonio's web pics showed the F-8108 overlapping the lower firewall angle and the F-802G. Hmmm...mine didn't have any bends in them. I looked at the plans and saw that the angles are supposed to butt up against the firewall angle, and don't even show the F-802G at all! So, I called Van's and was told to just cut them off to fit between the firewall angle and the F-802G. THEN...I called Van's and talked with Ken Krueger, who designed the system about another question. He finally figured out the problem--THEY HAD MAILED ME THE WRONG KIT! I was installing the kit for the -8A, and I have an -8. He said he'd mail me the right kit parts and plans, and that should solve the problem. So, I guess I got your kit and you got mine! The -8A mounting brackets butt against the lower firewall angle and don't overlap anything. I'd suggest a call to Van's. Talk to Ken Krueger. --Don McNamara N8RV Rick Jory wrote: > Anyone building an 8A with ground adjustable rudder pedals . . . the plans > show a left and right "F-802G" (drawing OP-3). These are also shown on > Drawing 24. However, on my QB kit these are not there . . . and it looks > like these may have a function for the tail dragger version but not the tri. > Has anyone run up against this? The aft end of F-8108 (L & R) are bent to > provide clearance for both of these--but my 8A QB doesn't have them. This > may be a question for Van's. ________________________________________________________________________________
From: "Moe Colontonio" <moejoe3(at)home.com>
Subject: RV-8 HS Stab Rivet Spacing/Alignment
Date: Dec 05, 1999
http://www.tabshred.com/moe/HS.htm This is a common problem. Vans advice to me was to just put a rivet in and don't worry. Other builders have riveted new flanges on, while others just cut the flange away and fill the skin hole with a rivet. Hit the above link for a picture. Moe Colontonio moejoe3(at)home.com www.tabshred.com/moe HI Listers, I'm having a little problem with my RV-8 HS stabilizer skeleton and am wondering if anyone else has come across the same problem. When laying the skins over the skeleton, the intersection of the HS404 (center tip rib), HS405 (center aft rib), HS602 (HSFWD spar channel) and HS814 (reinforcing angle at FWD spar center), the first rivet FWD of the FWD spar on the tip rib does not have sufficient material in the rib for proper edge distance ________________________________________________________________________________
From: flyhars(at)ibm.net
Subject: Re: Rudder Leading Edge
Date: Dec 05, 1999
Jeff: I just went through the rudder last week, the crease you are talking about is nothing to worry about. When it is painted you want even notice it. My question is the rudder bottom fairing on my RV-6A was too long and hit on the front edge at the tie down weldement. It seemed to be about 3/4" too long. It might clear on a RV-6 though, Have you tried yours yet? What I did was to cut about a one half inch off and reglassed the leading edge. Harvey Sigmon RV-6AQB ----- Original Message ----- From: Jeff Point <jpoint(at)execpc.com> Sent: Sunday, December 05, 1999 7:38 PM Subject: RV-List: Rudder Leading Edge > > Just got done rolling the leading edge of the rudder. One side turned > out beautifully, the other has a slight crease in the skin at the edge > of the spar flange, as cautioned about in the manual. Anybody had any > success getting this crease out, if so how? Or, should I not be too > concerned about it. This crease is not much, can be felt by hand, but > not visible unless you look closely under good light. > > Jeff Point > jpoint(at)execpc.com > -6 rudder > Milwaukee, WI > > ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: RV-6A O-360 FAB
Date: Dec 05, 1999
Gary, I have the A/P injection on a 360, and there is about .25" clearance between the steel of the gear leg and the FAB. I did have to cut a notch in the fiberglass fairing, however. Alex Peterson Maple Grove, MN > > What have others done to increase the clearance > between the Filtered Air Box and the training wheel > gear leg? :-) I have been told that the GBI video > shows cutting the filter to allow more clearance at > the carb. > > Has anyone cut a piece of the FAB fiberglass off and > then created a slanted replacement piece of fiberglass > to cover it? > > > ==== > Gary A. Sobek > "My Sanity" RV-6 N157GS O-320 Hartzell, > So. CA, USA ________________________________________________________________________________
From: "Mark Phillips" <mphill(at)fgi.net>
Subject: fiberglass tips
Date: Dec 05, 1999
Does anyone have any secrets on installing the vertical stab tips? ________________________________________________________________________________
From: "The Von Dane's" <vondanes(at)hotmail.com>
Subject: Re: fiberglass tips
Date: Dec 05, 1999
Mark... I just drilled and clecoed the fiberglass tip onto the VS today... I had to sand the tip down as it was too long, then I used cleco side grip clamps to hold it on one end, then drilled and clecoed as I went... I bought some Styrofoam I plan to use to fill the open end, if it epoxies ok... I will post some pictures to my web site tomorrow morning... Bill Von Dane, Colorado RV-8A N912V (res), waiting for wing kit http://vondane.tripod.com ----- Original Message ----- From: "Mark Phillips" <mphill(at)fgi.net> Sent: Sunday, December 05, 1999 6:30 PM Subject: RV-List: fiberglass tips Does anyone have any secrets on installing the vertical stab tips? ________________________________________________________________________________
Date: Dec 05, 1999
From: Mark Schrimmer <mschrimmer(at)earthlink.net>
Subject: Re: Carb Ice
Unless you have an optical sensor carb ice detector I doubt that you would have know if you had minor carb icing. Does anybody else have experience with either an optical carb ice detector like the ARP ice detector or a carburator temperature probe? I've often wondered which one is better. Mark Schrimmer Irvine, CA RV9A tail ________________________________________________________________________________
From: "The Von Dane's" <vondanes(at)hotmail.com>
Subject: Mounting Rudder to VS...
Date: Dec 05, 1999
I have read some post lately about attaching the rudder to the VS... On the plans, it calls for 3/16 x 3/8 rod end bearings in 2 places, but there are 3 platenuts... I have 6ea. 3/16 x 3/8 rod end bearings, and 1 larger one... Can someone help me out here? Is the larger one the wrong size? If not, where does it go? Also, I found that I have to screw the bottom rod end bearing in all the way, and the top on to 7/8" out in order for the counter balance arm to clear the VS. What is the minimum clearance here? Thanks in advance... Bill Von Dane, Colorado RV-8A N912V (res), waiting for wing kit http://vondane.tripod.com ________________________________________________________________________________
From: "The Von Dane's" <vondanes(at)hotmail.com>
Subject: Re: fiberglass tips
Date: Dec 05, 1999
Mark... I just drilled and clecoed the fiberglass tip onto the VS today... I had to sand the tip down as it was too long, then I used cleco side grip clamps to hold it on one end, then drilled and clecoed as I went... I bought some Styrofoam I plan to use to fill the open end, if it epoxies ok... I will post some pictures to my web site tomorrow morning... Bill Von Dane, Colorado RV-8A N912V (res), waiting for wing kit http://vondane.tripod.com ----- Original Message ----- From: "Mark Phillips" <mphill(at)fgi.net> Sent: Sunday, December 05, 1999 6:30 PM Subject: RV-List: fiberglass tips Does anyone have any secrets on installing the vertical stab tips? ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Navaid install etc.
Date: Dec 05, 1999
RV-8ers, Help! I'm at the point of installing all the stuff that goes under the pilot butt... Navaid servo, com & xpndr antennas, wing wiring multiconnectors through the side, etc. The plan for fitting all of this stuff in must clearly be a coordinated one considering how they all fit together. Of course future accessibility must be kept in mind with the front part of the floor removeable, but the rear portions pop-riveted down. So, I have the following questions for all you RV-8 guys ahead of me... 1. Does anyone have any photos of how they mounted the Navaid servo and connected it to the W807? 2. Have you put doublers above your antennas, and if so what size? 3. Where did you penetrate the main spar for the antenna leads (and other electrical stuff)? 4. Is there such a thing as a right angle BNC connector for the two antennas so as to possibly fit below the Navaid servo? Any experience, and especially photos, would be appreciated. Thanks! Randy Lervold RV-8, #80500, just took the wings back off www.pacifier.com/~randyl Home Wing VAF ________________________________________________________________________________
Date: Dec 05, 1999
From: Gert <gert(at)execpc.com>
Subject: Re: Ground Adjustable Rudder Pedals - 8A
To all of you who have experience with both the in-flight and ground adjustable pedals.. Which goes further forward, the ground or the in-flight adjustable pedals ?? I need all the space I can get.... Thanks Gert Pursuant to US Code, Title 47, Chapter 5, Subchapter II, '227, any and all nonsolicited commercial E-mail sent to this address is subject to a download and archival fee in the amount of $500 US. E-mailing denotes acceptance of these terms. ________________________________________________________________________________
Date: Dec 05, 1999
From: Gert <gert(at)execpc.com>
Subject: Re: Mounting Rudder to VS...
Bill If I remember correctly, the big one goes at the bottom of the rudder. Did you pre-install the rudder with the dim's given in the drawing when you rivited the top rib on for the counterweight on the rudder ?? When I rivited the rudder, I temporaraly installed it to get the spacing right on top. even so, it seems that one or more of the rod-ends are not in very far. Wonder if I can buy some with more threads ?? Gert The Von Dane's wrote: > > > I have read some post lately about attaching the rudder to the VS... > On the plans, it calls for 3/16 x 3/8 rod end bearings in 2 places, > but there are 3 platenuts... I have 6ea. 3/16 x 3/8 rod end bearings, > and 1 larger one... Can someone help me out here? Is the larger one > the wrong size? If not, where does it go? > > Also, I found that I have to screw the bottom rod end bearing in all > the way, and the top on to 7/8" out in order for the counter balance > arm to clear the VS. What is the minimum clearance here? > > Thanks in advance... > > Bill Von Dane, Colorado > RV-8A N912V (res), waiting for wing kit > http://vondane.tripod.com > -- Pursuant to US Code, Title 47, Chapter 5, Subchapter II, '227, any and all nonsolicited commercial E-mail sent to this address is subject to a download and archival fee in the amount of $500 US. E-mailing denotes acceptance of these terms. ________________________________________________________________________________
From: "PR" <perryrhoads(at)ctnet.net>
Subject: Re: RV3-List: Re: RV3-List Digest: 12/04/99
Date: Dec 05, 1999
What calendar that has an RV-3? Perry Rhoads RV-3 tail kit Pitts SIS N88PR sold -----Original Message----- From: DFCPAC(at)aol.com <DFCPAC(at)aol.com> Date: Sunday, December 05, 1999 6:15 PM Subject: RV-List: Re: RV3-List: Re: RV3-List Digest: 12/04/99 > >hi bob,bob, and rob, >good to here from all of you. how have you been rob? i guessed the rv3 >newsletter was a little hard to tackle. i agree with all of you, we should >use the rv3 list. the regular rv list is ok but mostly talk about 6's and >eights. i'm located on long island in new york. i did not build my rv3a i >purchased it from randy compton in fl. but the way he bought a pitts s1 and >is very unhappy with it. he wanted to buy his rv back. i've had it for about >7 months and it's one heck of a machine. i love it. i really flys great. i've >just started doing basic aerobatics with it. you gotta see this thing roll. >don't even need rudders plant your feet on the floor pitch up a little and >bang the stick over. i have an 0-320 lyc. and i can cruise at 165 knots at >2400 rpm at 7 gallons an hour. climb rate is over 2000 fpm. and the thing is >like a pussy cat to fly. rob, i took a look at installing the sliding canopy >i think to leave well enough alone. anyway i have an antenna right behind the >canopy that i would have to move. i'm just gonna leave it like it is. so >how's the restoration going? i really like to see this list work out it's >always nice to chat with others that have the same plane. > >take care >dan carley >rv3a-148cw > >i'll inform chuck about this list. did you get the new calender yet. chuck's >rv3 is the first one listed > > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Dec 05, 1999
Subject: Re: RV4 Horiz Stab gap question
In a message dated 12/5/99 8:39:09 AM Pacific Standard Time, Mkraus01(at)aol.com writes: << how big of a gap should I leave between the horizontal stabilizer and the outboard portion of the counterbalance rib?? >> Some may disagree, but I like to use the shank of an AN-3 bolt as the arbiter of sufficient control surface clearances. -GV ________________________________________________________________________________
From: "The Von Dane's" <vondanes(at)hotmail.com>
Subject: Re: Mounting Rudder to VS...
Date: Dec 05, 1999
Unfortunately I screwed up and just slapped the rudder skeleton on, secured the counter weight arm, and went to town... It clears the VS, but is there a minimum clearance? Is there any reason to believe the clearance will change in flight? Bill Von Dane, Colorado RV-8A N912V (res), waiting for wing kit http://vondane.tripod.com ----- Original Message ----- From: "Gert" <gert(at)execpc.com> Sent: Sunday, December 05, 1999 7:36 PM Subject: Re: RV-List: Mounting Rudder to VS... Bill If I remember correctly, the big one goes at the bottom of the rudder. Did you pre-install the rudder with the dim's given in the drawing when you rivited the top rib on for the counterweight on the rudder ?? When I rivited the rudder, I temporaraly installed it to get the spacing right on top. even so, it seems that one or more of the rod-ends are not in very far. Wonder if I can buy some with more threads ?? Gert The Von Dane's wrote: > > > I have read some post lately about attaching the rudder to the VS... > On the plans, it calls for 3/16 x 3/8 rod end bearings in 2 places, > but there are 3 platenuts... I have 6ea. 3/16 x 3/8 rod end bearings, > and 1 larger one... Can someone help me out here? Is the larger one > the wrong size? If not, where does it go? > > Also, I found that I have to screw the bottom rod end bearing in all > the way, and the top on to 7/8" out in order for the counter balance > arm to clear the VS. What is the minimum clearance here? > > Thanks in advance... > > Bill Von Dane, Colorado > RV-8A N912V (res), waiting for wing kit > http://vondane.tripod.com ________________________________________________________________________________
From: "pat_hatch" <pat_hatch(at)email.msn.com>
Subject: Re: Carb Ice
Date: Dec 05, 1999
Randall: Happens to me all the time with the conditions you stated. At idle (low manifold pressure) you're getting a pretty good temp drop in the carb, this with a little moist air, and you get the ice. Engine starts to run real rough some times when taxiing out, it will go away after using carb heat. Regards, Pat Hatch RV-4 N17PH @ INT RV-6 Tanks ----- Original Message ----- From: Randall Henderson <randallh(at)home.com> Sent: Sunday, December 05, 1999 12:55 PM Subject: Re: RV-List: Carb Ice > > I believe I experienced carb ice yesterday morning in my RV-6. Not certain > as my carb temp probe isn't hooked up yet. But on run-up, when I pulled the > carb heat, the tach went down about 100 RPM, then slowly came back up about > 50 RPM. OAT was 323 degrees with a 0 degree > temp/due point spread. > > Randall Henderson, RV-6 N6R (~50 hrs) > Portland, OR > http://www.edt.com/homewing > > ________________________________________________________________________________
Date: Dec 05, 1999
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: RV-8 seat floor questions
meketa wrote: > Stripping or breaking the #6 and #8 screws is not a problem if you > run a tap thru all floor nutplates before installing them. This cleans > out the locking crimp. The screws can then be installed by hand. I will > install plastic washers under the screws for paint protection and to > act as lock washers. Get some BoeLube (a dry lubricate available at Cleaveland Tools among other places) and apply it to the screws the first time you insert them into the platenuts. You will be amazed how easy the screws thread in and you won't compromise the locking ability of the platenuts. Sam Buchanan "The RV Journal" http://home.hiwaay.net/~sbuc/journal ________________________________________________________________________________
Date: Dec 05, 1999
From: jason baker <jjbaker(at)home.com>
Subject: Re: RV4 HS 404 Rib Question
Ed, Just completed the task you are speaking about...used AN rivets and bucked them myself. It was hard, as I have large forearms (call me Ahnold) but now it looks great. Get the Orndorf video...Its done for an RV6, but I have a -4 and it shows the rivet order. If you really want to know now...go get drawing 3a and then procede to read. To summarize, Cleco one side completely (leave out 404, but leave the other side open to allow access to buck. Start at the HS407/408 "T" and put in first rivet, then left one rivet/right one rivet/up one rivet/down one rivet... until all you can do is go left and right. Rivet rear spar from HS403 out, then finish up with 406 and 405. Leave 404 aside right now. For the other side, Cleco Skin to HS 402 and all holes forward of HS402. When I mean forward, I mean towards the leading edge. When we are done, we are going to want to rivet while "peeling" back the trailing edge of the skin, but we want a cleco in EVERY hole of the forward spar and all tip ribs. No Clecos aft of the forward spar. Start at the "T" again, but go up one/left one/right one/up one (This is why you leave out 404, so you can reach in there to buck...and thank god there's only about 7 rivets each side, cause its a bitch at the narrowest portion of the Leading Edge. Note not to put in clecoes aft of the leading edge spar, because you want to lift this enuf to get a bucking bar in there. I'm repeating myself-editors note. Once you get the Forward Spar Clecoed, start on HS 408 (where it meets the forward Spar). Leave a hole unclecoed (this is where your first rivet will be) and insert two to four Clecoes below hole. This will leave you enough "bend room" to lift up the skin and buck. Every time you remove a cleco to expose the next target rivet hole, put it in the next hole down so that you always have at least two clecoes below your hole. You will ultimately end up "running" into the rear spar, at which point you will cleco to the rear spar and really reach in to buck the last two rivets on HS 408. Great Tip: I took one of those nice office chairs which rolls. Adjusted the seat back so I recline and bucked the rivets from a recline under the jig post. It was like laying on a creaper and changing my oil. Very comfortable. Insert HS 404 and rivet it in...stand back and look at your accomplishment. Whew.... Jason Baker RV-4 "Damn I wish they made the Emp predrilled." San Ramon, CA P.S. I actually made about $250 dollars worth of mistakes on my emp, including a figure 8 on my skin and HS 407. Every time I did, I bought new parts. Its hard, but once you finish the HS, you are a veteran shop worker. I have made no errors and am flying along the rest of the kit now. If you are dimpling, you will probably save yourself alot of time if you just concede a countersink for the most leading edge rivet on HS404/407/406 as I just couldn't dimple the skin without opening it too much. Ed Funk wrote: > > To rivet or to pop rivet question ? I'm getting ready to assemble the HS > skeleton, and one question Van leaves up to the builder is when to rivet the > 404 rib to the front spar. If one uses solid rivets early they are then > forced to use pop rivets to fasten the skin to the middle (HS-407) ribs. If > one attaches the 404 rib to the front spar later, access is left for solid > riveting in the 407 area thus substituting solid rivets for pop rivets in > the assembly process. > > My question as a new builder is "how difficult is it to reach into this area > and flush rivet the skin the the 407 rib and then rivet the 404 rib in place > ?" > > My first choice is to use the minimum number of pop rivets; however, if this > means reaching into a blind area and taking an unreasonable risk toward > denting skins, etc. I'll swallow and gladly use pop rivets. > > To pop rivet or not to pop rivet..... that is the question. > > Ed Funk > Corning, NY > RV-4 Tail > ________________________________________________________________________________
Date: Dec 05, 1999
Subject: Re: Ground Adjustable Rudder Pedals - 8A
From: Scott R McDaniels <smcdaniels(at)juno.com>
> To all of you who have experience with both the in-flight and ground > adjustable pedals.. > > Which goes further forward, the ground or the in-flight adjustable > pedals ?? > I need all the space I can get.... > - The limiting factor is at what point the rudder peddle hits the firewall at full deflection with the brake applied. Either one will give the most leg room possible. Scott McDaniels North Plains, OR These opinions and ideas are my own and may not reflect the opinions or ideas of my employer. ________________________________________________________________________________
From: "Dave Bristol" <bj034(at)lafn.org>
Subject: Re: rear spar fit on qb6
Date: Dec 05, 1999
Gar, Don't bend anything! If the wing is not lined up perfectly, the rear spar will not fit. If you slide the front spar in or out a little you'll find that the alignment on the rear spar will change. I've had my wings on and off many times and have found this to be a challenge almost every time. Dave. southern CA, paint and interior. -----Original Message----- From: Gar & Jan Pessel <pessel(at)ptialaska.net> Date: Saturday, December 04, 1999 5:24 PM Subject: RV-List: rear spar fit on qb6 > >I finally reached the point where it was time to mate the wings to the >fuselage. We tried sliding the left wing into place and find that the tab >off the rear spar will not fit into the slot between the tabs on the >fuselage. It is too far back by over 1/8th of an inch. I do not have the >faintest idea how to bend those two tabs or if I should be bending on the >tab on the wing. Bending anything labeled as part of a spar , even just a >rear spar, is not something that sounds like a particularly good idea. >Anybody else ever encountered this problem? Gar Pessel, Fairbanks, AK > > ________________________________________________________________________________
Date: Dec 06, 1999
From: Matt Orr <morr(at)vt.edu>
Subject: HELP! Opinions NEEDED!
Hello, I've been looking at the RV's at several other homebuilts for several years and have finally figured out that I really like the RV-4 as it's a bit lighter then the RV-8 (on paper). Do they really weigh less then the -8 when equipped the same (numbers PLEASE)? The RV-4 seems like a better aerobatic airplane as I couldn't find a single one that broke in flight and I looked through each RV-4 accident since 1983. Is the -8 really that much easier to build then the -4? If I could build an Rv-4 in about the same time as an RV-8 I think the -4 would be the better airplane. I've seen an RV-8 tail kit and it seemed nice and I've also seen a Harmon Rocket that's in the final stages. Are there less bugs or headaches in the RV-8 kit? Which is the better way to go? I've been agonizing over this with a friend whose workshop I'll use and who will most likely be a partner building for the last few months. We've worked together on projects similar but not to quite this scale before or we'll each build our own if the kit seems doable. I want to use the aircraft for sport aerobatics with the occasional cross-country. What's the "better" airplane to fly, to build? If you say I should get a ride in each tell me what airport to meet you at on the east coast (near VA). ;-) Thanks, Matt Orr I've looked through the archives and found ~2700 messages on primer. And ~270 comparing RV-4 to RV-8 and didn't find what I was looking for ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Dec 06, 1999
Subject: HELP! Opinions NEEDED!- Go 4
I know that I will be flamed unending but I too still think the RV4 is the perfect sport aircraft. I liked it when it first came upon the scene and I like it no less now. This is not to take away from the 8 or the 6 but the 4 is in my opinion the perfect sporting aircraft. Definitely lighter, possibly stronger, with on center seating, racy canopy and a superb compromise of sporting agility with cross country capability. Yes, it has some negatives---Bubbas on the Van's Bubba Scale beyond 7+ may find the rather roomy accommodations slightly lacking compared to the 8 but not really much less than the 6 as you do not have to share elbow room and then there is the unending legend of the tail heavy RV4. Yes, it is true that I at 180 lbs probably would not want to shove a 240 pounder into the back seat and go zoomering about but fortunately for me all my friends are almost normal in size and my dear wife barely makes 120 dripping wet dressed. I am also of the opinion and it is just an opinion that aerobatics in any RV should be kept to a solo proposition anyway. Yep, I still like the 4 and not looking to build the RV 12 A. JR, RV4 slowly progressing at less than a snails pace ________________________________________________________________________________
From: "Jerry Carter" <rv8abuild(at)mindspring.com>
Subject: Re: Ground Adjustable Rudder Pedals - 8A
Date: Dec 06, 1999
I somehow ended up with both types of rudder pedals in my 8A QB kit, and I chosed the "in-flight" adjustable pedals simply because it was a much simpler, easier installation. The platenuts are already installed for the quick adjustable ones to be installed - no holes to drill in the floor, no rivets to drill out, no pop rivets to install - just bolt them in. The quick adjustable ones are a little heavier, but if I were trying to decide which to order, I would still go with the "in-flight" adjustable pedals. Jerry Carter 8A fuse, installing top skin > > Anyone building an 8A with ground adjustable rudder pedals . . . the plans > show a left and right "F-802G" (drawing OP-3). These are also shown on > Drawing 24. However, on my QB kit these are not there . . . and it looks > like these may have a function for the tail dragger version but not the tri. > Has anyone run up against this? > > ________________________________________________________________________________
From: "Jerry Carter" <rv8abuild(at)mindspring.com>
Subject: Re: Smart-aleck comment about "tricycles"
Date: Dec 06, 1999
________________________________________________________________________________
From: wvu(at)mail.ameritel.net
Date: Dec 06, 1999
Subject: Re: HELP! Opinions NEEDED!
Matt, I'm at 2W6 in Maryland, about 40nmi or so south of BWI. There are two -4's and two -6's on the field. Call me at 301-757-0286 and I'll try to hook you up with the -4's. I'd be careful if I were you. You might get hooked on both the -4 and the -6 at the same time! I have a -6 but still like the look of the -4's. Those bulges on the sides of the cowl are sexy. I agonized over the same decision and have not regret having a -6. The decision was easy for me. My wife refused to look at the back of my head. How about having one of each? Now that's a sporty though. A. Vu N985VU > >Hello, > > I've been looking at the RV's at several other homebuilts for several >years and have finally figured out that I really like the RV-4 as it's a bit >lighter then the RV-8 (on paper). Do they really weigh less then the -8 >when equipped the same (numbers PLEASE)? > > The RV-4 seems like a better aerobatic airplane as I couldn't find a >single one that broke in flight and I looked through each RV-4 accident >since 1983. > > Is the -8 really that much easier to build then the -4? If I could >build an Rv-4 in about the same time as an RV-8 I think the -4 would be the >better airplane. I've seen an RV-8 tail kit and it seemed nice and I've >also seen a Harmon Rocket that's in the final stages. Are there less bugs >or headaches in the RV-8 kit? > > Which is the better way to go? I've been agonizing over this with a >friend whose workshop I'll use and who will most likely be a partner >building for the last few months. We've worked together on projects similar >but not to quite this scale before or we'll each build our own if the kit >seems doable. > > I want to use the aircraft for sport aerobatics with the occasional >cross-country. > > What's the "better" airplane to fly, to build? > > If you say I should get a ride in each tell me what airport to meet you >at on the east coast (near VA). ;-) > >Thanks, >Matt Orr > >I've looked through the archives and found ~2700 messages on primer. >And ~270 comparing RV-4 to RV-8 and didn't find what I was looking for > > ________________________________________________________________________________
From: "Eric.J.Henson(at)chase.com
(Content Technologies SMTPRS 2.0.15) with SMTP id for" ; Mon, 06 Dec 1999 08:04:02.-0500(at)matronics.com
Date: Dec 06, 1999
Subject: Re: steel braided lines
"Brian Denk" on 12/05/99 02:53:09 PM Please respond to rv-list(at)matronics.com Subject: Re: RV-List: steel braided lines Not intended as a flame, but I've changed out many an old steel braided line out of our Phantoms. These old girls all had over 5000 carrier cycles, if something is going to waste a line, getting aboard the boat is it. The trick is the line is simply imobilized. It cant destroy its self if it cant move. Later I worked for a company that made the fuel lines for the C-17 (steel braided), they had a very long life to them. We also made the inflation lines for the emergency slides in airliners (much like an aeroquip). They changed those every few years and they're only used once. Every type of hose we made was burst tested at least once, in fact we did everything we could to destroy them. There is a world of difference between steel braided and cloth braided lines. I don't know how many times I have read stories about someone dead sticking their newly finished plane into a cornfield because the the $2.00 line he pounded out on his work bench to feed his $20,000 engine failed. I'll get off my soapbox now, be sure I will only install steel braided lines in my bird. Eric Henson Skinning the fuse > > >Stay away from steel braided hoses unless you intend to change them every >year. Why you ask? When that pretty steel braid breaks down a little you >have several strands of steel poking in the rubber beneath it. > >Bill Not only is this an issue, but the braid will saw it's way through anything it rubs on with engine vibration providing the motivation. So, those that do have them, make sure they will not rub on the engine mount, wires, primer lines, control cables, etc. Like anything, they do a fine job as long as they aren't neglected. Brian Denk RV8 N94BD two braided hoses in my engine compartment. ________________________________________________________________________________
From: "Larry Pardue" <n5lp(at)carlsbad.net>
Subject: Re: HELP! Opinions NEEDED!
Date: Dec 06, 1999
> >Hello, > > I've been looking at the RV's at several other homebuilts for several >years and have finally figured out that I really like the RV-4 as it's a bit >lighter then the RV-8 (on paper). Do they really weigh less then the -8 >when equipped the same (numbers PLEASE)? > clip > > Which is the better way to go? I've been agonizing over this with a >friend whose workshop I'll use and who will most likely be a partner >building for the last few months. We've worked together on projects similar >but not to quite this scale before or we'll each build our own if the kit >seems doable. > Matt, You sound frustrated that no one will tell you which airplane is better. This is a good reason wise people will avoid making this kind of statement. There is really no "best" among the RV designs. There is a lot of choice which allows one to decide based on their individual priorities. Unfortunately some people are offended when others don't make the same choice they did. Between the 4 and the 8 there are appearance differences that are subjective (I think the 4 is pretty). The 4 is lighter and tighter. The 8 is larger and more flexible in regard to loading and has more fuel capacity. This combination gives better cross-country capability. The 8 is also going to be easier to build due to advances in kit refinement over the years. You make the choice. Larry Pardue Carlsbad, NM RV-6 N441LP ________________________________________________________________________________
From: "Fesenbek, Gary" <fesenbek(at)marykay.com>
Subject: Pitot-Static Woes
Date: Dec 06, 1999
>You could go this way or you could just get one of those new F1 Rocket >kits. Mine arrives in June and I can't wait to blow the doors off the >first RV-8 I see.;~) >Yeeeee HAAAAAAAAAaaaaaaaaaaaa............ > >scot I know what you mean. I saw a Rocket take off in 100' yesterday from Addison. That was the shortest takeoff I had seen of a Rocket thus far. It was being towed by an RV-6A though.... Gary Fesenbek RV6A Dallas, TX ________________________________________________________________________________
From: "Pat Perry" <pperryrv(at)hotmail.com>
Subject: Re: HELP! Opinions NEEDED!
Date: Dec 06, 1999
Hello Matt, I can't give you any advice on which plane is a better flyer, but I'm building an RV-4 and I'll give you my experiences with the 4 over the past year. I'm building on a lower budget than most (I think) and have done everything I could to keep the cost down. One of the big differences between the 8 and 4 is the cost to build. The 8 costs more to purchase and cost more (typically) to power. I think most 8 builders are going with 180-200hp while most 4's are happy with 150hp. The extra cost for the 8 could be as much as $10K by the time your done. I baught an old RV-4 kit used with no work done to it and purchased a new set of plans from Vans to get all the latest changes to the drawings, this saved me quite a few dollars in the long run but did cost me some extra time. I haven't seen the new 8 kits to see how much is done on them, I can say that my 4 kit was probably a good "bad example" of what you won't get if you buy new. I spent at least 40-60 hours of build time just in cleaning, the older kit had etch from the packing paper on the surface of all the wing skins - it took lots of elbow grease to get it off. As far as the rest of the building goes there really isn't any task I considered to be too difficult. They do a good job at the factory getting everything sheared and bent close enough to work with, the rest of the work becomes routine after you get the hang of it on the tail kit. I don't know if the construction manual is any better for the 8 than the 4 but it leaves alot to be desired, I've opted in many cases to set it aside and just use the drawings since the manual is outright wrong in many cases. The build time is dependant on the builder...completely!. I've seen all types of builders and quickbuild or not if you want to get the plane done you have to work...and work steady. On a project this big if you don't work efficiently you will end up spending much more time than is required to actually build the plane. I have just over 700 hrs in the project so far- I started in January of 1999 and have a steady routine of work that I try to follow. My fuse is out of the jig and I'm getting ready to attach the Engine mount and get the thing on gear, my final goal is to have a flying plane this summer - less than 2 years of build time. I've seen guys work everynight for 6 years and not finish the project - set a goal each time you work and work toward that goal. Don't labor over little things like how much is done on the kit when you start, build the airplane you want to buy and fly, you'll find the time to build it. Pat Perry Dallas, PA RV-4 fuse almost done Engine being rebuilt I need a prop! ________________________________________________________________________________
From: "Rick Jory" <rickjory(at)email.msn.com>
Subject: Re: Ground Adjustable Rudder Pedals - 8A
Date: Dec 06, 1999
This has to be the problem . . . my "8108's" have bends on both ends as if the 8A had an 802G. I'll call Van's. Thanks. -----Original Message----- From: Don McNamara <mcnamara(at)sbt.infi.net> Date: Sunday, December 05, 1999 6:05 PM Subject: Re: RV-List: Ground Adjustable Rudder Pedals - 8A > >Rick-- > >I ran into this just the other night. I exchanged my in-flight adjustable >rudder assembly for the ground-adjustable version, and began the installation. >I noticed that Moe Colontonio's web pics showed the F-8108 overlapping the lower >firewall angle and the F-802G. Hmmm...mine didn't have any bends in them. I >looked at the plans and saw that the angles are supposed to butt up against the >firewall angle, and don't even show the F-802G at all! So, I called Van's and >was told to just cut them off to fit between the firewall angle and the F-802G. > >THEN...I called Van's and talked with Ken Krueger, who designed the system about >another question. He finally figured out the problem--THEY HAD MAILED ME THE >WRONG KIT! I was installing the kit for the -8A, and I have an -8. He said >he'd mail me the right kit parts and plans, and that should solve the problem. > >So, I guess I got your kit and you got mine! The -8A mounting brackets butt >against the lower firewall angle and don't overlap anything. I'd suggest a call >to Van's. Talk to Ken Krueger. > >--Don McNamara > N8RV > >Rick Jory wrote: > >> Anyone building an 8A with ground adjustable rudder pedals . . . the plans >> show a left and right "F-802G" (drawing OP-3). These are also shown on >> Drawing 24. However, on my QB kit these are not there . . . and it looks >> like these may have a function for the tail dragger version but not the tri. >> Has anyone run up against this? The aft end of F-8108 (L & R) are bent to >> provide clearance for both of these--but my 8A QB doesn't have them. This >> may be a question for Van's. > > ________________________________________________________________________________
From: "Charlie Kearns" <kearns(at)gte.net>
Subject: RV-8 For Sale
Date: Dec 06, 1999
I got a few responses over the weekend but my kit is still for sale. I have pictures of the project that I can email or mail to anyone interested. Once again I have the tail and wings 100% complete and the fuselage kit is just started. All parts are primed inside with Dupont Variprime. The tail and wings have been inspected and signed off by George Orndorff. Please respond off list, the price is negotiable!! ________________________________________________________________________________
From: "Fesenbek, Gary" <fesenbek(at)marykay.com>
Subject: RV-6A O-360 FAB
Date: Dec 06, 1999
>> Our video does not show cutting the Filtered Air Box. Yes, this was a >>problem with the old gear legs that you fiberglassed the wood fairing on. >>With the new gear and the fiberglass fairing, this should not be a problem >>George Orndorff I have a 6A with the new nosegear and an O-360 FAB. I did have to notch the FAB in the back to clear the nose gear. I did not have to cut the filter. The filter clears this cutout (barely). The cutout matches the slant of the nosegear and gives about 1/4" clearance to the nosegear. Gary Fesenbek RV6A Dallas, TX ________________________________________________________________________________
From: TRAASHMAN(at)webtv.net (Joe Waltz)
Date: Dec 06, 1999
Subject: Re: RV8 N94BD weigh-in
Any wind will create lift. How much? Depends on AOA and airspeed of course. If you get enough lift, the plane flies. ________________________________________________________________________________
From: TRAASHMAN(at)webtv.net (Joe Waltz)
Date: Dec 06, 1999
Subject: Re: Carb heat
Eustace, Why would you use alt. air on the ground in dusty conditions to give your filter a break? Aren't these the conditions that the filter is installed for? How about giving the engine a break and filtering out the dust? ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Dec 06, 1999
Subject: Re: steel braided lines
In a message dated 12/05/1999, 1:14:05 PM, rv-list(at)matronics.com writes: What? <> ________________________________________________________________________________
From: "Gary Baker" <gtbaker(at)bright.net>
Subject: RV-3A For Sale
Date: Dec 06, 1999
Posting this for a friend who is not on the list. Please contact him directly. Thanks. Gary Baker RV-6 (Working on wings) N4GB (Reserved) Medina, OH For Sale: 1996 RV-3A. O-320, wing mods completed, wing tanks, sliding canopy, Garmin 250 GPS/Com, King KT-76A transponder, mode C, two axis electric trim, strobes, nav lights, fuel mixture indicator, day/night VFR. Red, white, blue paint. A high performance eye-catcher. $32,500. Don @ 817 560 0604. TX. Don H Blessing 11717 Pine Creek Ct Aledo, TX 76008 ________________________________________________________________________________
Date: Dec 06, 1999
From: Will Cretsinger <cretsinger(at)arlington.net>
Subject: Re: Skyforce Skymap II
Rich, I am flying the Skymap II and love it...but wish I had the color version. The Skymap II couples beautifully with the NavAid through the Smart Coupler which can be purchased with the NavAid. We used the panel mount...you still must fab a box to contain the panel mount provision. I'll be happy to answer any questions you may have directly. Will Cretsinger, Arlington, TX -6A flying through 130 hours Zeidman, Richard B wrote: > > > Have any listers tried the Skymap II in their RV's. I really like the panel > mount feature with the large map, but would like to hear some comments from > anyone who has actual experience with it. I am also planning to couple it to > a Nav-Aid autopilot. > > Rich Zeidman > Ridley Park, Pa > RV6A finish kit > working on canopy ________________________________________________________________________________
From: "Gary Baker" <gtbaker(at)bright.net>
Subject: RV-4 Kit for Sale
Date: Dec 06, 1999
I was asked to put this on the list for a friend. Please contact him directly off-list. Thanks. Gary Baker RV-6 (Working on wings) N4GB (Reserved) Medina, OH FOR SALE-EMPENNAGE AND WING KIT FOR AN RV-4 Wing kit is still in the crate as it came from Van's Aircraft Empennage kit is partially completed Vertical and horizontal stabilizers finished Rudder and elevator have not been started The kit includes the following extras: Clecoes and cleco pliers All the jigs to complete the empennage and wings Delivery within 300 miles of Denver, Colorado (outside that area may be negotiated) Dimple and riveting tool Additional tools may be negotiated All completed work has been supervised by an A & P mechanic ASKING $4200 Van's current price for these two kits is $5050 and this does not include shipping, crating, or any tools and jigs. This additional cost would add about $500 to the new kit price. You would also have to spend about 200 hours working to complete the pieces I have already finished. Contact Rick or Kassie at (303) 680-8428 OR E-mail us at: krabkove(at)mstg.net ________________________________________________________________________________
Date: Dec 06, 1999
From: Will Cretsinger <cretsinger(at)arlington.net>
Subject: Air Filter--clean or replace
I am approaching my first annual condition inspection. Should the air filter be replaced or cleaned? Also, what is a good criteria to determine when to replace tires? I rotated my main tires at 134 landings since they were worn on one side...they still look pretty good. Is there a good rule as to when to discard? Will Cretsinger, Arlington, TX -6A flying through 130 hours ________________________________________________________________________________
From: "Rob Reece" <reece(at)rt66.com>
"A20driver" , "Bob Adams" , "Boyd Butler" , "Charles R. Chandler" , "Chuck Brietigam" , "DFCPAC" , "Doug Gray" , "FinnLassen" , "Jim Kemp" , "LarryJenison" , "LeastDrag" , "Norman Hunger" , "PILOT8127" , "Randy Compton" , "Rob Reece" , "RobertHughes" , "RobertMiller" , "RV3FLYER" , "RV3PILOT" , "Steve Lopez" , "William \"Bill\" Saindon" , "WILLMINCEY"
Subject: RV-3A For Sale
Date: Dec 06, 1999
Saw this on the RV-list and thought someone might know someone who would be interested. Kinda spendy at $32K though! -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Gary Baker Sent: Monday, December 06, 1999 7:51 AM Subject: RV-List: RV-3A For Sale Posting this for a friend who is not on the list. Please contact him directly. Thanks. Gary Baker RV-6 (Working on wings) N4GB (Reserved) Medina, OH For Sale: 1996 RV-3A. O-320, wing mods completed, wing tanks, sliding canopy, Garmin 250 GPS/Com, King KT-76A transponder, mode C, two axis electric trim, strobes, nav lights, fuel mixture indicator, day/night VFR. Red, white, blue paint. A high performance eye-catcher. $32,500. Don @ 817 560 0604. TX. Don H Blessing 11717 Pine Creek Ct Aledo, TX 76008 ________________________________________________________________________________
Date: Dec 06, 1999
From: Larry -xlax- Lovisone <netters2(at)ns.net>
Subject: Re: RV8-List Digest: 12/05/99
We used nut plates and 8/32 screws on all our floor panels instead of pop rivets... Larry xlax Lovisone RV8 N248PL kit #24 RV8 weak wing theory http://rvators.com/rv8wing.htm ________________________________________________________________________________
Date: Dec 06, 1999
From: pdsmith <pdsmith(at)pacbell.net>
Subject: Re: RV4 Horiz Stab gap question
I called Van's specifically about this question and their answer was - no less than 1/8" to allow for flexing, flight loads etc. Phil Smith 80691 ________________________________________________________________________________
Date: Dec 06, 1999
From: Garry Legare <versadek(at)earthlink.net>
Subject: Re: Air Filter--clean or replace
Will the filter supplied by Vans is a K&N reusable type. Just clean it and re-oil it following K&Ns instructions. If you have misplaced your servicing instructions for the filter, they are available from Vans or at most auto supply stores. As far as the tires go remount them so the other side wears then replace them, or when side wall checking (cracks) become a concern. Will Cretsinger wrote: > > I am approaching my first annual condition inspection. Should the air > filter be replaced or cleaned? > > Also, what is a good criteria to determine when to replace tires? I > rotated my main tires at 134 landings since they were worn on one > side...they still look pretty good. Is there a good rule as to when to > discard? > > Will Cretsinger, Arlington, TX > -6A flying through 130 hours > ________________________________________________________________________________
Date: Dec 06, 1999
From: Stuart B McCurdy <sturdy(at)att.net>
Subject: Re: RV3-List traffic
Hi Guys, I, like you, check the RV-3 list everyday, but see nothing there until now. Glad to see there is somebody out there. I own the RV-3 which Tony Bingelis built as his ninth project. I bought it from him when he had to have a Pacemaker put in and decided to quit flying. I had helped him fly off Phase I and knew what an excellent airplane it was. You may have seen it at Oshkosh this year leading a formation of 9 experimentals during the Showcase portion of the air activities. It is also on the cover of Van's 2000 calendar at the end of the echelon. We took that picture at Van's Homecoming this year and it is unique in that it is the first and only time all 7 RV models have been pictured in flight together. I founded Formation Flying, Inc (FFI) this year in response to FAA's new requirement that any pilot wishing to fly formation in FAA waivered airspace had to possess a formation card issued by an agency approved by FAA. On 21 Apr 99 FAA approved FFI to do so. FFI is available to evaluate and issue cards if you have a desire to do. Agree, the RV-3 is a wonderful flying machine. Light, nicely balanced, great control response, good speed and fuel economy on 150 hp. I also like the non counter balanced elevator because I can feel the pressure on the stick while doing aerobatics, so it gives another feedback in addition to seat of the pants. I recently put a Sensenich RV series prop, 70x77, on the RV-3 and it made a world of difference. I put on 7/16 bolts and replace the 4' spool with a solid extention at the same time. No vibration and 8 knots more speed. Great machine built by a great master. Glad to see some dialog of this list. Stu McCurdy RV3-List Digest Server wrote: > > From: DFCPAC(at)aol.com > Subject: RV3-List: Re: RV3-List Digest: 12/04/99 > > --> RV3-List message posted by: DFCPAC(at)aol.com > > does anyone use this list, or do they use the regular rv list? i own an rv3 > and would like to talk to other owners of rv3's. > > regards > dan carley > rv3a-148cw > ________________________________________________________________________________
Date: Dec 06, 1999
From: Larry Olson <lolson(at)doitnow.com>
Subject: Re: Air Filter--clean or replace
Will, Is it the K&N Filter from Van's? They were meant to be cleaned and reused. Just tap it on the ground to get out the big stuff. Then spin it like a tire in about an inch of solvent. (K&N makes a special solvent sold at motorcycle shops, I always used gas) Tap filter lightly on the side of your solvent container. You'll be surprised how dirty the solvent gets. Let it dry. Then spray it with K&N filter oil. (sold at same cycle shop) Re-install. Works great. Did it for many years on sand buggies & desert racers. Larry Olson Cave Creek, AZ RV6 - Finish kit on order > >I am approaching my first annual condition inspection. Should the air >filter be replaced or cleaned? > >Also, what is a good criteria to determine when to replace tires? I >rotated my main tires at 134 landings since they were worn on one >side...they still look pretty good. Is there a good rule as to when to >discard? > >Will Cretsinger, Arlington, TX >-6A flying through 130 hours ________________________________________________________________________________
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
Subject: prop extension and tailwheel fairing for sale
Date: Dec 06, 1999
I have a 4" prop extension, 6" diameter, 3/8" bolt holes with matching crush plate. The crush plate is factory grooved to hold the bolt heads while torquing the prop bolts (so you don't have to remove the spinner). I bought them from Van's. There's no damage or anything wrong with them. I used them on my O-320- E3D for about 10 hours before switching to a different prop. Van's sells the extension for $215 and the crush plate for $25, according to my 1998 catalog. I will sell them for $190, which is $50 off. I also have a tailwheel fairing, new, unused. Van's sells for $40. I'll sell it for $30. Or buy everything for $210 and save me an extra trip to UPS. Vince Frazier 3965 Caborn Road Mount Vernon, IN 47620 812-985-7309 evenings University of Southern Indiana 812-464-1839 days ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Dec 06, 1999
Subject: Air Filter--clean or replace
>I am approaching my first annual condition inspection. Should the air >filter be replaced or cleaned? Cleaned. There is a kit available to wash and re-oil the filter. I think it is in Van's catalog and it is also available thorugh a race car speciality shop in your area as they use the same filter system. There is a special soap to wash it with and special oil to treat the element with. Don't use just any old thing. And don't overload the filter with the oil when reapplying it. There was some discussion whether they even need to be cleaned every year or not (see archives). The filter will last a long time if properly taken care of. >What is a good criteria to determine when to replace tires? Tires: Are the cloth belts showing? Time to replace them. Well, not quite, although I know some pilots that use that as their time to replace. If they still look good, keep them on. Some tires get so weather cracked before the tread is worn they need replacing. Usually those are ones that sit around in the sun and aren't used much. Not usually on an RV type airplane. Michael ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Dec 06, 1999
Subject: RV-4 vs RV-8
You will be happy with either one, which ever one you build. They are both one of the best values and best airplanes available. I like the LOOKS of the -4 better. The swept-back gear (long or short) and the cowl are the best looking in the business. I REALLY like the -4 cowl. The cockpit: you can pack more into a -8 panel and there is more room in the front office of the -8, but, having been in both, I like the way I FIT in the -4 better. 'Course, that is what I fly, but I like the fact I have somewhere to put my arms and elbows. Feels a bit more fighter-like. Either will fly like nothing you have ever flown. Why do so many ex-fighter jocks gravitate to the RV series? As close as you can get to military on the civilian market. The -8 holds more fuel and baggage. The strength issue is not an issue. Period. Easier to build? Don't know. Either will eventually get built. The final weight will depend on what you stick in it (and on it); it's hard to rely on someone elses weight. I vote for the -4; that is what I fly. Michael RV-4 N232 Suzie Q Beginning year 3 flying....... ________________________________________________________________________________
From: "Bryan E. Files" <BFiles(at)corecom.net>
Subject: Re: Air Filter--clean or replace
Date: Dec 06, 1999
Will, It depends on what air filter you have. Brackett Air Filter says not to clean. Paper Air Filters should be replaced every 500 hours. They should be blown out every 100 hours. **** Bryan E. Files **** Ever Fly Maintenance Palmer, Alaska A&P, IA, FAA Safety Counselor mailto:BFiles(at)corecom.net ----- Original Message ----- From: Will Cretsinger <cretsinger(at)arlington.net> Sent: Monday, December 06, 1999 6:31 AM Subject: RV-List: Air Filter--clean or replace > > I am approaching my first annual condition inspection. Should the air > filter be replaced or cleaned? > > Also, what is a good criteria to determine when to replace tires? I > rotated my main tires at 134 landings since they were worn on one > side...they still look pretty good. Is there a good rule as to when to > discard? > > Will Cretsinger, Arlington, TX > -6A flying through 130 hours > > ________________________________________________________________________________
From: "Bill Christie" <billc(at)dancris.com>
Subject: Re: [Fwd: Flaring Tool]
Date: Dec 06, 1999
Reading the comments on steel vs. aluminum lines reminded me of when I was in the F-14 program in the early seventies. The hydraulic lines for the 3 systems were titanium using 4000 psi. The first prototype was crashed at Calverton NY on approach when the last hydaraulic ststem was lost. It turned out that they had rigidly mounted the lines to the airframe and the vibration work hardened the lines and they fractured. They (Grumman) then used insulated adel clamps and other such mounts and they worked fine from then on. Sure were light too! An armfull of tubing seemed like it weighed nothing. The point is that I think either will work as long as attention is paid to how it is mounted and isolated from vibration. Bill C. RV-8A; Flaps ----- Original Message ----- From: Cy Galley <cgalley(at)accessus.net> Sent: Friday, December 03, 1999 6:53 PM Subject: Re: RV-List: [Fwd: Flaring Tool] > > I fail to see why a steel line would be subjected to more stress than an > aluminum line. See very few aluminum springs. Most automotive fuel lines > are steel. Injector lines for aircraft under high pressure are steel. A > simple loop in a line relieves most any destructive stresses. Where there is > a lot of movement, flexible hoses are placed inline even with aluminum. > Last but not least there is an AD for the 200 HP Lycoming in a Cessna > Cardinal to replace the aluminum prop governor line with a steel line with > aircraft steel fittings. Why the aluminum line and fittings were breaking. > > The major reason is weight for aircraft, especially in the large -8 fittings > and lines. Aluminum is generally strong enough with no internal rust > problems. But plated steel lines have been in automotive use for years as > fuel lines and brake lines as it is cheaper without the electrolysis > problems of aluminum. Probably the ideal would be titanium except for the > cost. > > Cy Galley - Editor, B-C Contact! > (Click here to visit our Club site at http://www.bellanca-championclub.com) > > > -----Original Message----- > From: Alex Peterson <alexpeterson(at)usjet.net> > To: rv-list(at)matronics.com > Date: Friday, December 03, 1999 6:44 PM > Subject: Re: RV-List: [Fwd: Flaring Tool] > > > > > > > >> So are there good reasons NOT to use steel fuel lines that I, in my > >> inexperience, am simply not aware of? > > > >I am no expert in aircraft design, but I can think of two good reasons: 1) > >airplanes use aluminum fuel lines - be extremely careful in changing > >anything from "standard" aircraft design, and 2) as the airframe moves > >under stress, strain is imparted to the fuel lines. Steel lines will see 3 > >times the stress loads as aluminum when deflected the same amount. Good > >enough reasons for me. > > > >Alex Peterson > >Maple Grove, MN 6A > > > > > > ________________________________________________________________________________
From: "Doug Weiler" <dougweil(at)pressenter.com>
Subject: Re: HELP! Opinions NEEDED!
Date: Dec 06, 1999
I guess I need to get my two cents in also. I am building a -4 (on the gear with engine installed). I have flown both the -4 and -8. They handle very much alike (in fact all RVs handle great). After sitting in both airplanes, obviously the -8 is roomier but if you are less than 6 feet and less than, say, 180 lbs, the -4 is fine (the front seat is more than adequate. The -4 kit will take longer since it has not been refined like the new -8 kits (a local professional RV builder just finished a -8 in 1400 hours... not a Quickbuild). He estimates a -4 around 2000 hours. Just a matter of personal preference. Doug Weiler, pres MN Wing RV-4 engine installation ________________________________________________________________________________
From: MRobert569(at)aol.com
Date: Dec 06, 1999
Subject: Re: strobe positon question
IMHO we might be geting a bit carried away here. With that many strobe lights you may need that second alternator just to drive them. Again, acknowledging that the regs are not mandatory here, a strobe system should be visible 75 degrees above and 75 degrees below the horizontal plane of the aircraft. That is the guidline to use. Whatever your combination or where they are, if they meet the guidlines stated then you will have no problem. Mike Robertson RV-8A Baffles and wires and... "Das Fed" In a message dated Fri, 3 Dec 1999 11:28:49 PM Eastern Standard Time, Bobpaulo(at)aol.com writes: > > if i install perturbing wing tip strobe/position lights, a tail > strobe/postion light (in lower part of rudder), and a belly strobe, must i > have additional strobe on top of fusel. or on vert stab??? thanx, bob > > ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Dec 06, 1999
Subject: Re: HELP! Opinions NEEDED!- Go 4 it
Bert, good points but I do not agree. I like center line seating so that when aerobatics are done you get a better feel and can see out both sides equally. I like flying with company too but will not perform aerobatics with two up beyond rolls as I do not think that any of the Rv's have adequate strength reserves (my opinion) for two-up aerobatics. I seem to fly mostly alone and it is that way it seems with most pilots. I like taking people up and giving rides and flying with my wife--what is the problem with this in a RV4--are you saying it is a single place airplane--I do not understand? I am collecting parts now for a Pitts Special--the real McCoy and it will be a single place and I would not have it any other way. With a Kitfox and a RV4 (soon) to give rides the Pitts will be my Aerobatic machine--sportsman and advanced someday (big talk). Each to their own but sorry-I like the RV4 better than the 6 or the 8 and nothing has changed my mind. The advantages of the 6 over the 4 only come to the fore front when one starts into cross country capability and convenience and as I stated the 4 is a more sporting machine and I like that it is compromised in favor of a sporting nature vs cross country and the opposite is true of the 6. If you like the 6 then build the 6, I like the 4 and that is what I am building and do not regret it--no apoligies--I like the 4. JR ________________________________________________________________________________
From: HAROLD1339(at)aol.com
Date: Dec 06, 1999
Subject: Re: RV-4 For Sale
Rv4 for sale excellent condition contact me of list for complete spec sheet. ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Dec 06, 1999
Subject: Re: HELP! Opinions NEEDED!- Go 4 it
When looking at the 4 & 8, they are both good planes, but you should also look at the Harmom Rocket II and the F-1 Rocket. I liked the 4 and then the 8 came out, but I wanted something alottle faster and the F-1 Rocket was that plane chris Wilcox F-1 Rocket ________________________________________________________________________________
From: WoodardRod(at)aol.com
Date: Dec 06, 1999
Subject: RV-3 For Sale
1982 RV-3 For Sale. 425 TT; 615 SMOH. 160hp O-320-B2C; Sensenich metal prop; King digital comm; King Mode C xponder; Full gyros; Electric elevator trim; Imron paint--VERY nice. No spar mods. I bought N99RV in July as a time-builder. It worked! I've been hired by a regional airline, but for what they're paying me I've got no business owning an airplane! Delivery is possible. Please contact me directly if you're interested. Best regards to all. Rod Woodard Ft. Collins, Colorado WoodardRod(at)aol.com ________________________________________________________________________________
From: "Duberstein, Allen" <allen.duberstein(at)intel.com>
Subject: Experience with IVO Props
Date: Dec 06, 1999
Has anyone had experience using an IVO Prop on an O320 Lycoming. I am looking at the in flight adjustable version. Thanks Allen Duberstein allen.duberstein(at)intel.com Phone: 412-831-7302 Fax: 412-831-5742 ________________________________________________________________________________
From: MRobert569(at)aol.com
Date: Dec 06, 1999
Subject: Re: Electric Tach
Bill, It just so happens that I was reading through my VM-100 installation manual about this just the other day. The RPM digital readout gives engine hours when the engine is not running. AS soon as the engine starts then it automatically changes to engine RPM. The hour meter part does not start calculating hours until the engine RPM reaches 1500 revs. This saves me from buying a hobbs meter. Mike Roertson RV-8A "Das Fed" In a message dated Sat, 4 Dec 1999 10:59:37 PM Eastern Standard Time, pagan writes: > > Seems like I remember something on the list about electric tach not > recording time on the hour meter unless they are running at a certain rpm. > Searched the archives but couldn't get a good hit. Anybody know the answer? > > > Bill Pagan > N565BW > "The original RV-8A builders page on the web" > http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html > > ________________________________________________________________________________
From: SportAV8R(at)aol.com
Date: Dec 06, 1999
Subject: Re: HELP! Opinions NEEDED!
Matt: Soon (hopefully) I could get you some air tme in my 6A if you have interest. I am temporarily grounded due to insurance problems (life, not aircraft). When the papers are in order again, I would be glad to visit Tech... my plane is based at the house, about 30 mi N. of ROA. Meanwhile, I am voluntarily restriced to lower-risk activities to keep the wife happy. Contact me off list if you'd like to work something out. Seems like we may have even had this discussion before?? Bill Boyd ________________________________________________________________________________
Date: Dec 06, 1999
From: "Bob U." <r.r.urban(at)worldnet.att.net>
Subject: Re: RV3-List: Re: RV3-List traffic
> I recently put a Sensenich RV series > prop, 70x77, on the RV-3 and it made a world of difference. I put on > 7/16 bolts and replace the 4' spool with a solid extention at the same > time. No vibration and 8 knots more speed. Great machine built by a > great master. > > Glad to see some dialog of this list. > > Stu McCurdy ++++++++++++++++++++++++++++++++++++++++++++ Hi Stu, The catalog recommended metal prop for the RV-3 is 70X79. The 70X77 is listed/recommended for the RV6. Why did you stray from that recommendation knowing that the prop is limited to MAX of 2600 RPM? Got any knowledge of the Sensenich wood props for the RV-3? Seems Sensenich is recommending the 68X82 for the RV-3 series. Bob ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)shuswap.net>
Subject: Re: Carb Ice
Date: Dec 06, 1999
For a lot of us this is the worst time of the year for carb ice with the temperatures around freezing and high humidity, but still this shouldn't cause any real concerns. With a properly installed carb heat system I have never had a problem controlling it. For me the key to it is knowing what is going on and recognizing the symptoms and staying right on top of it. In Randall's case the other day and as others have already mentioned carb ice under those conditions is almost guaranteed. The engine being stone cold at start up and a long slow warm-up gives it every chance for the ice to build. For what it is worth this has been my procedure in these conditions. Because of the temperatures, humidity etc. I am already on guard and ready for it. Assuming the aircraft is in a unheated hangar or tied down outside with the temperature at the freezing point I preheat the engine for half an hour using a flat in-car warmer laying in the outlet at bottom of the cowling. This should be done in the hangar out of the wind or if outside cover the cowling with a good blanket with the aircraft into wind. Then on start-up keep the RPM down to 1000-1100 initially so you don't red line the oil pressure then gradually work up to 1700 RPM until getting oil temp to a minimum 110-120 using carb heat if any roughness occurs. Then taxi to take -off position or preferably into a run-up bay if available at the end of the runway. For me this is the most important part, run up again to 1700-2000 with full carb heat watching for any rise in RPM or manifold pressure. When these stabilize or you have run a minimum of 15-20 seconds go to full cold and take-off immediately. Again this is just the way I have done it over the years and others may have different ideas. Eustace Bowhay Blind Bay, B.C. > From: pat_hatch <pat_hatch(at)email.msn.com> > To: rv-list(at)matronics.com > Subject: Re: RV-List: Carb Ice > Date: Sunday, December 05, 1999 7:34 PM > > > Randall: > > Happens to me all the time with the conditions you stated. At idle (low > manifold pressure) you're getting a pretty good temp drop in the carb, this > with a little moist air, and you get the ice. Engine starts to run real > rough some times when taxiing out, it will go away after using carb heat. > > Regards, > > Pat Hatch > RV-4 N17PH @ INT > RV-6 Tanks > ----- Original Message ----- > From: Randall Henderson <randallh(at)home.com> > To: > Sent: Sunday, December 05, 1999 12:55 PM > Subject: Re: RV-List: Carb Ice > > > > > > I believe I experienced carb ice yesterday morning in my RV-6. Not certain > > as my carb temp probe isn't hooked up yet. But on run-up, when I pulled > the > > carb heat, the tach went down about 100 RPM, then slowly came back up > about > > 50 RPM. OAT was 323 degrees with a 0 degree > > temp/due point spread. > > > > Randall Henderson, RV-6 N6R (~50 hrs) > > Portland, OR > > http://www.edt.com/homewing > > > > > > > ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)shuswap.net>
Subject: Re: Carb heat
Date: Dec 06, 1999
Hi Joe: I guess I didn't give enough detail on the installation of the flapper valve (alternate air, carb heat or what ever you want to call it ). It is installed in the throat of the carb air box ahead of the filter so that the intake air is filtered regardless of what the position of the flapper valve is. If you have noticed the vortex created by the prop when taxiing in dry grass or dusty conditions, by using the alternate air it keeps a lot of the junk out of the filter and cuts down on the servicing of the filter. I have found that under these conditions it works well just to leave it on until airborne as there is very little difference is take-off performance. The intake air area is much the same using the flapper valve. On the otherhand as the airspeed builds after take-off there is a noticeably improvement in performance at the higher power settings using straight ram air. As I have said before the design of Vans air box is the best I have seen. By using the K&N filter which is reusable it is very economical and I believe because of the large filtered area I get the highest full throttle manifold readings I have seen on a naturally aspirated engine. All the best Eustace Bowhay Blind Bay, B.C. ---------- > From: Joe Waltz <TRAASHMAN(at)webtv.net> > To: rv-list(at)matronics.com > Subject: Re: RV-List: Carb heat > Date: Monday, December 06, 1999 6:15 AM > > > Eustace, > > Why would you use alt. air on the ground in dusty conditions to give > your filter a break? Aren't these the conditions that the filter is > installed for? How about giving the engine a break and filtering out > the dust? > > > ________________________________________________________________________________
Date: Dec 06, 1999
From: "Mike Wills" <willsm(at)spawar.navy.mil>
Subject: Re: HELP! Opinions NEEDED!- Go 4 it
> >Bert, good points but I do not agree. I like center line seating so that when >aerobatics are done you get a better feel and can see out both sides equally. >I like flying with company too but will not perform aerobatics with two up >beyond rolls as I do not think that any of the Rv's have adequate strength >reserves (my opinion) for two-up aerobatics. JR JR, As a fellow -4 builder I definitely agree with all your points. Let me add to it. An often mentioned advantage of the -6 is the side by side seating for communication and to avoid forcing your pax to stare at the back of your head. Ive never understood the communication issue; your both on intercom arent you? I will concede that in cross country flying/navigating where both are looking over a sectional side by side would be more convenient. The rear seat visibility in the -4 is still terrific, better than most spam that Ive been up in. For a guy my size (6'1" and 190#) I prefer the the elbow and shoulder room in the tandem airplanes and would trade that for the "improved" seating arrangement af the -6. In my admittedly limited experience (short flights in -4, -6, and HR2) thats my preference. To each his own I guess. Mike Wills RV-4 starting firewall forward willsm(at)spawar.navy.mil ________________________________________________________________________________
Date: Dec 06, 1999
From: Builders Bookstore <winterland(at)rkymtnhi.com>
Subject: Re: Experience with IVO Props
"Duberstein, Allen" wrote: > > Has anyone had experience using an IVO Prop on an O320 Lycoming. I am > looking at the in flight adjustable version. I've flown them on ultralights, and in that category have found them to be somewhat smooth but very inefficient. The blades are too soft and flexed under load causing a 10-15% speed loss compared to other ultralight props. As far as on a Lycoming, I have no first hand experience but have heard several cases of problems with the blades moving in the hub. The conclusions seemed to be that the IVO is just not built to accept the pulsiness of our big bore Lycs. Andy ________________________________________________________________________________
From: "Rob Reece" <reece(at)rt66.com>
Subject: Experience with IVO Props
Date: Dec 06, 1999
Try Jim Ayers at . He uses this prop on his LOM powered RV-3. Rob Reece RV-3 SN45 > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Duberstein, > Allen > Sent: Monday, December 06, 1999 12:34 PM > To: 'rv-list(at)matronics.com' > Subject: RV-List: Experience with IVO Props > > > > > Has anyone had experience using an IVO Prop on an O320 Lycoming. I am > looking at the in flight adjustable version. > > Thanks > > > Allen Duberstein > allen.duberstein(at)intel.com > Phone: 412-831-7302 > Fax: 412-831-5742 > > ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Dec 06, 1999
Subject: Re: Experience with IVO Props
In a message dated 12/6/1999 2:53:26 PM Central Standard Time, winterland(at)rkymtnhi.com writes: << > Has anyone had experience using an IVO Prop on an O320 Lycoming. I am > looking at the in flight adjustable version. I've flown them on ultralights, and in that category have found them to be somewhat smooth but very inefficient. The blades are too soft and flexed under load causing a 10-15% speed loss compared to other ultralight props. As far as on a Lycoming, I have no first hand experience but have heard several cases of problems with the blades moving in the hub. The conclusions seemed to be that the IVO is just not built to accept the pulsiness of our big bore Lycs. Andy >> I am not sure on this, but i think that problem has been corrected. The new IVO props are suppose to be able to handle up to 500 hp. They have made some changes. I know that a friend who is building a dragonfly is looking at an IVO inflight adjustable prop on his 150 hp subara. You might want to check with IVO though if any changes were made Chris Wilcox F-1 Rocket ________________________________________________________________________________
From: Pilotrv6a(at)aol.com
Date: Dec 06, 1999
Subject: Re: shop cleaning sale
Hi Bob Stopped buy Kokomo Airport the other evening and saw this nice looking airplane setting on the ramp with no wings. Looked it over and it looked GREAT. NICE WORK! Sherman Dedman ________________________________________________________________________________
From: "Japundza, Bob" <bjapundza(at)dowagro.com>
Subject: shop cleaning sale
Date: Dec 06, 1999
Hi Sherman, Good to hear from you, and thanks for the compliments! I had to run back home that day after I dropped it off so it sat on the ramp for about an hour. Denny helped me push it back into the hangar. It's been a long process, too long. Gets old after a while. Right now I'm working on the right wing--it's almost ready for the main skins, but I will set the other wing up in another jig before I start skinning, since I am waiting on my fuel tanks to be built. I finished up the flaps this weekend, and have both ailerons built. Should be February-March before it flies, but I plan on hammering away at it during the week I have off over the holidays. I have a feeling that we'll be flying to a lot of places together! Thanks! Bob Japundza Dow AgroSciences Information Management EnterpriseWise IT Consulting 317-337-5348 -----Original Message----- From: Pilotrv6a(at)aol.com [mailto:Pilotrv6a(at)aol.com] Sent: Monday, December 06, 1999 4:42 PM Subject: Re: RV-List: shop cleaning sale Hi Bob Stopped buy Kokomo Airport the other evening and saw this nice looking airplane setting on the ramp with no wings. Looked it over and it looked GREAT. NICE WORK! Sherman Dedman ________________________________________________________________________________
From: "Japundza, Bob" <bjapundza(at)dowagro.com>
Subject: shop cleaning sale
Date: Dec 06, 1999
Oops, meant to reply direct. > Hi Sherman, > > Good to hear from you, and thanks for the compliments! I had > to run back home that day after I dropped it off so it sat on ________________________________________________________________________________
Subject: Re: Articles on refueling with plastic jugs
From: scott.fink(at)microchip.com
Date: Dec 06, 1999
12/06/99 03:32:23 PM We aren't allowed to fuel in the hangar at all, the plane must be pulled out before fueling (this is MUCH easier if the doors are open!). Scott Fink "Cy Galley" To: Sent by: cc: owner-rv-list-server@mat Subject: Re: RV-List: Articles on refueling with plastic jugs ronics.com 12/03/1999 02:59 PM Please respond to rv-list One more good idea is to have the hangar door open when doing the fueling--- if you have a hangar!! Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: scott.fink(at)microchip.com <scott.fink(at)microchip.com> Date: Friday, December 03, 1999 3:20 PM Subject: Re: RV-List: Articles on refueling with plastic jugs > > >Tim, > >In order to (legally) use auto gas at a city of Phoenix airport we were >required to take a 2 hour course. It boils down to this: > >You must use metal gas cans (never, never plastic per your subject line) > >You must use a metal funnel > >The airplane must be "bonded" to earth (i.e. grounded with a wire) >The funnel is bonded to the plane (with a wire) >The gas can is bonded to the funnel. (again with a wire) > >You can use wires for bonding with metal clips that can be bought at Radio >Shack. > >The whole idea is to provide a path for any electrons stripped off by the >flowing fuel a way to return from where they came and to hold everything at >one electrical potential. If everything is at the same potential (plane, >funnel, gas can and therefore gas) there is no chance for a spark. > >We are also required to have a fire extinguisher nearby during the fueling. > >Hope this helps, >Scott Fink >RV6 - about to close left wing > > > "Tim Lewis" > To: rv-list(at)matronics.com > Sent by: cc: > owner-rv-list-server@mat Subject: RV-List: Articles on refueling with plastic jugs > ronics.com > > > 11/30/1999 05:42 AM > Please respond to > rv-list > > >Listers, > >Over the last couple of years I've read articles (Sport Aviation or >AOPA Pilot, I think) on the hazards of refueling aircraft using 5 gallon >gas cans. The danger is static electricity discharge causing fire. I'm >looking for a safe way (if there is one) of transfering fuel this way. > >If anybody knows the location of good articles on this topic please let >me know. > >Thanks, > >Tim Lewis >****** >Tim Lewis >timrv6a(at)earthlink.net >N47TD RV-6A, FAA Inspection scheduled 30 Nov 99 >Springfield VA >http://home.earthlink.net/~timrv6a >http://home.earthlink.net/~timrv6a/jpi.html - No JPI stuff in my airplane > > ________________________________________________________________________________
Date: Dec 06, 1999
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Re: HELP! Opinions NEEDED!
Matt I have a RV4 under construction since 1994 and hope to finish it next year. Comparing the 4 with the 8 I see the RV8 as being an upgraded RV4 with a little more room for baggage, more horses up front, maybe a little more speed and a little more width. Sometime back Van talked about a modification to the RV4. I beleive they called it a fat 4 but it never happened. I think the RV8 is the result. The RV8 will cost you a few more bucks and has refinements you probably won't see on the RV4. As a matter of fact since the 8 came out you see hardly anything about the RV4 in the RVATOR anymore. I guess you could call it Van's redheaded stepchild. I still prefer the RV4 but if I had it all to do again I would go with the RV6 because of the side by side seating when you have a passenger. OK guys I just donned the nomex so fire away. Earl RV4 trying to get the wing angle worked out before I drill the rear spar attatch. Matt Orr wrote: > > > Hello, > > I've been looking at the RV's at several other homebuilts for several > years and have finally figured out that I really like the RV-4 as it's a bit > lighter then the RV-8 (on paper). Do they really weigh less then the -8 > when equipped the same (numbers PLEASE)? > > The RV-4 seems like a better aerobatic airplane as I couldn't find a > single one that broke in flight and I looked through each RV-4 accident > since 1983. > > Is the -8 really that much easier to build then the -4? If I could > build an Rv-4 in about the same time as an RV-8 I think the -4 would be the > better airplane. I've seen an RV-8 tail kit and it seemed nice and I've > also seen a Harmon Rocket that's in the final stages. Are there less bugs > or headaches in the RV-8 kit? > > Which is the better way to go? I've been agonizing over this with a > friend whose workshop I'll use and who will most likely be a partner > building for the last few months. We've worked together on projects similar > but not to quite this scale before or we'll each build our own if the kit > seems doable. > > I want to use the aircraft for sport aerobatics with the occasional > cross-country. > > What's the "better" airplane to fly, to build? > > If you say I should get a ride in each tell me what airport to meet you > at on the east coast (near VA). ;-) > > Thanks, > Matt Orr > > I've looked through the archives and found ~2700 messages on primer. > And ~270 comparing RV-4 to RV-8 and didn't find what I was looking for > ________________________________________________________________________________
Date: Dec 06, 1999
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: HELP! Opinions NEEDED!
Matt Orr wrote: > > > Hello, > > I've been looking at the RV's at several other homebuilts for several > years and have finally figured out that I really like the RV-4 as it's a bit > lighter then the RV-8 (on paper). Do they really weigh less then the -8 > when equipped the same (numbers PLEASE)? > > The RV-4 seems like a better aerobatic airplane as I couldn't find a > single one that broke in flight and I looked through each RV-4 accident > since 1983. > Can't tell you about the -8. My -4 weighs 930 w/lyc 160hp (carb), no gyros, 1 comm, 1 loran. Interior: paint only with foam/cloth seat cushions. By the way, if you'd like to fly (for less money) instead of building, I'm asking $37k. My wife wants to ride up front. It IS the best flying airplane I'v ever flown. Charlie N4375J Slobovia Outernational (MS71) Jackson MS ________________________________________________________________________________
Date: Dec 07, 1999
From: pagan <pagan(at)cboss.com>
Subject: FAA Inspection Lead Time
Just a heads up to everyone. FAA called today to let me know they'll be out on 12/17 to inspect my plane. I sent in my paperwork on 11/22. I suppose the info that I'd have the inspection within 2 weeks after I sent in my paperwork was wrong. I didn't get that info from the FAA. Everyone should keep in mind that the lead time could be more than you anticipate. It probably would have been a good idea to have inquired about the lead time before. Just thought ya'll would like to know. Bill Pagan N565BW "The original RV-8A builders page on the web" http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html ________________________________________________________________________________
Date: Dec 06, 1999
From: Andy <winterland(at)rkymtnhi.com>
Subject: Re: Experience with IVO Props
> > The conclusions seemed to be > >that the IVO is just not built to accept the pulsiness of our big bore Lycs. > > > Pulsiness????? As I understand, the large and relatively slow moving pistons on Lycoming and Continental engines, especially the Lyc 0-360, are particularly hard on props as their rotational movement is very jerky each time they fire. (thump, thump, thump, thump) This compared to a two stroke ultralight engine with small pistons travelling at over 6000 rpm. These light, fast strokes are much smoother as felt by the prop. This is supposedly why an ultralight's prop bolts are just AN-4s while your RV's Prop bolts are AN-10s. It is also why designing fixed pitched metal props for your Lycoming is so difficult, and why Sensenich took so long to get it right, and why many aircraft with fixed metal props have rpm restrictions. I call this "pulsiness", but I'd be glad to give it another name. Andy (I do stand to be corrected on this whole matter, but it's what I've thought I've learned over the years) ________________________________________________________________________________
Date: Dec 07, 1999
From: pagan <pagan(at)cboss.com>
Subject: Hours
If my electric tach only records time on the meter when it runs at 1500+ how should I record my time on the aircraft as well as in my log. I've always just used the hobbs for my log (flying) time. Should I just record time for the aircraft and logbook by real time? Bill Pagan N565BW "The original RV-8A builders page on the web" http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html ________________________________________________________________________________
From: JNice51355(at)aol.com
Date: Dec 06, 1999
Subject: Re: New Site: SourceRV.com!
In a message dated 12/6/99 1:16:54 PM Pacific Standard Time, SSoule(at)pfclaw.com writes: << How did you Listers sign up for this. All I see at www.rvsource.com <http://www.rvsource.com> is a graphic of softwood trees and the words "coming soon." >> Steve Be sure to let us all know when you see more than softwood trees. do not archive ________________________________________________________________________________
From: MRobert569(at)aol.com
Date: Dec 06, 1999
Subject: Re: Ground Adjustable Rudder Pedals - 8A
Rick, I have an 8A but with the fully adjustable pedals, but have ben also having some of the same problems. The first thing I learned was to look at each drawing and see if it had a "A" drawing right after it to go with the 8A verses just the 8. On the 8A there is just one bulkhead forward of the main wing spar. That whole assembly for the -8 landing gear does not exist. For me that created a bit of a problem with the optional rear pedals as the drawing from Van's had part of the mounting attaching to the 802 tower. As this obviously does not exist in the 8A I was a bit perplexed as where to mount them. Van's answer was to drill a couple of holes in the floor and pop rivet them. The very next thing I learned was to check and recheck the parts carefully. I have received numerous wrong parts. Van's has replaced every one of them at no cost to me so there is no complaint there but it has been very trying to figure out some parts that are only meant for the -8 and won't fit the -8A. Good Luck and good building. Mike Robertson RV-8A QB baffling and wiring and ..... In a message dated Sun, 5 Dec 1999 7:09:06 PM Eastern Standard Time, "Rick Jory" writes: > > Anyone building an 8A with ground adjustable rudder pedals . . . the plans > show a left and right "F-802G" (drawing OP-3). These are also shown on > Drawing 24. However, on my QB kit these are not there . . . and it looks > like these may have a function for the tail dragger version but not the tri. > Has anyone run up against this? The aft end of F-8108 (L & R) are bent to > provide clearance for both of these--but my 8A QB doesn't have them. This > may be a question for Van's. > > Thanks in advance, > Rick Jory, Highlands Ranch, Co > RV8A QB . . . fuselage > > ________________________________________________________________________________
From: RV6ARC(at)aol.com
Date: Dec 06, 1999
Subject: Re: Experience with IVO Props
Hi A friend of mine had a Ivo Prop on his 0-320 and kept breaking the copper strips. It vibrated at about 1200rpm,s and it was the new improved model. It is for sale for $350.00 ...(it was in a Glasair Tri Gear) Also another friend had a 3 blade in flight adjustable in his CA65 0-320 He took it off also, (kept breaking strips) He is selling it for $650.00 If you are interested in amy of these e-mail me off line. Bob Cornacchia RV6 RV6ARC(at)AOL.com ________________________________________________________________________________
From: OrndorffG(at)aol.com
Date: Dec 06, 1999
Subject: Re: Experience with IVO Props
Check the archives for IVO. I got 400 hits. It is worth your time to read these posts. I sure hope this IVO prop will perform as advertised. There have been some very serious problems with older models. Becki Orndorff ________________________________________________________________________________
Date: Dec 06, 1999
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Setting Wing Incidence Angle
Thanks to Chuck and all who responded to the flap issue. I now have the wings square with no sweep. The bottom skin is flush with the fuselage. Per vans instructions for setting incidence on RV4 wing & drawing SK-51 I need a block 3 and 3/64 inches to get the bubble in the center of level. this puts the wing rear spar 1/4 inch lower than what Van call for. I have screwed up too many times already and have had to remove and replace the rear spar carry through. I do not want to do it again and would like to get the incidence angle right the first time. My question is about the angle of horizontal stabilizer due to the 1/4 inch difference of the wing. Per SK-48 Van shows a 1/4 spacer under the level at the rear spar. Would this go to 1/2 inch or decrease to 0 inch? Maybe another aproach would be to raise the rear of fuse till Van's measurement of 2.8 inches was reached and then set the angle of the stab til I get the 1/4 inch called for in SK-48. Sorry about the length but I am paranoid about drilling the rear spar attach. All comments welcome. Earl, RV4 ________________________________________________________________________________
From: MRobert569(at)aol.com
Date: Dec 06, 1999
Subject: Re: Hours
Bill, FWIW the people I know log flight time from the moment the wheels move to the time they stop, then log tach time towards their overhaul time. Mike Robertson RV-8A QB In a message dated Mon, 6 Dec 1999 7:09:13 PM Eastern Standard Time, pagan writes: > > If my electric tach only records time on the meter when it runs at 1500+ > how should I record my time on the aircraft as well as in my log. I've > always just used the hobbs for my log (flying) time. Should I just record > time for the aircraft and logbook by real time? > > > Bill Pagan > N565BW > "The original RV-8A builders page on the web" > http://www.geocities.com/CapeCanaveral/Launchpad/9749/william.html > > ________________________________________________________________________________
Date: Dec 06, 1999
From: Mike Thompson <grobdriver(at)yahoo.com>
Subject: Re: Experience with IVO Props
--- OrndorffG(at)aol.com wrote: > > Check the archives for IVO. I got 400 hits. It is worth your > time to > read these posts. I sure hope this IVO prop will perform as > advertised. > There have been some very serious problems with older models. > > Becki Orndorff Warning: Longish musings follow! I've read the archived posts (every one) and I don't get it. There's a pile of money to be made out there for someone who has the expertise; I don't know why Hartzell doesn't go for the experimental market. I fly (renting) behind a manual (pull the rope!) in-flight adjustable prop. Actually, I have three positions: Climb, Cruise and Feather. This is on a Grob 109B motorglider. The prop blades are metal. The problem with IVO seems to be the composite blades (from what I've read) - why don't they just do metal? Maybe good reason, but maybe just a desire to perfect composite props...? I would dearly love to spend the $1800 on a climb/cruise in-flight adjustable metal prop for my -6 rather than the compromise fixed-pitch metal, hanging that on an O320. Something between fixed and fully constant speed. I think a lot of people would go with that. The setup seems perfect for us. Might could even keep the feather handle (Dick Rutan has soared a LongEZ, why not an RV?). :) Mike Thompson Austin, TX -6 N140RV (Reserved) Wings ________________________________________________________________________________
Date: Dec 06, 1999
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: Re: Experience with IVO Props
Please check the Matronics RV-List Archive and search for IVO. http://www.matronics.com/searching/search.html I got 755 hits. I have not heard anything good about IVO Props on Lycoming engines. IMHO: Under no circumstance would I fly behind an Ivo prop on an RV. (or any Lycoming engine powered airplane with an Ivo Prop) It takes a lot of work and time to build an airplane, I will not risk MY airplane on an Ivo Prop. "There are OLD pilots, and there are BOLD pilots. But there are no old bold pilots." I intend to become an OLD pilot. Fly safely. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, So. CA, USA ________________________________________________________________________________
From: DFCPAC(at)aol.com
Date: Dec 06, 1999
Subject: Re: RV3-List: Re: RV3-List traffic
since the question on propellers came up. i have a hendrickson #220892 h68f76 prop. has anyone used or heard of this wood prop. it seems to be working well for the rv but i have noticed when i get into low rpm settings it seems like i might be getting a small vibration. dan carley rv3a-148cw ________________________________________________________________________________
From: "Stephen Johnson" <spjohnsn(at)ix.netcom.com>
Subject: Rear Fuel Tank Baffle
Date: Dec 06, 1999
Hi Listers, I'm thinking about the process of closing up the tank with the rear baffle. I'm building a RV-8 if it matters. I have checked out Sam Buchanan's excellent site, and his method looks good, but there are some conflicts with accounts from other sources. The manual from Van's says the baffle should be sealed first, and then the skin should be countersunk and riveted after the sealant cures. Some posters on the list have suggested using Saran Wrap over the spars and allowing the tank to final cure on the wing to insure a good fit. This would make it impossible to apply the wood clamps as shown on Sam's web page. I know there can be more than one way to do things, but I thought I'd get opinions before doing anything permanent. Thanks in advance, Steve Johnson RV-8 #80121 ________________________________________________________________________________
Date: Dec 06, 1999
Subject: Re: Air Filter--clean or replace
From: Scott R McDaniels <smcdaniels(at)juno.com>
> Is it the K&N Filter from Van's? They were meant to be cleaned > and reused. Just tap it on the ground to get out the big stuff. > Then spin it like a tire in about an inch of solvent. - Do not use solvent , gasoline or any think other than the K&N filter cleaner to clean your filter. The filter media in the filter that you have is cotton. It can be damaged by other chemicals, high pressure air, etc. Unless you want to take a chance at reducing the filtering capability of the element it would be wise to clean and reoil (not with a spray oil by the way, they are only for the foam filters I believe) it only per the instructions that came in your K&N filter or that is included in the recharge kit. Scott McDaniels North Plains, OR These opinions and ideas are my own and may not reflect the opinions or ideas of my employer. ________________________________________________________________________________
From: "Paul Besing" <rv8er(at)home.com>
Subject: Countersunk Washers
Date: Dec 06, 1999
How does one countersink fiberglass for the #6 Countersink washers? Is there is a different size bit? Paul Besing RV-6A (197AB) Arizona http://members.home.net/rv8er Finish Kit ________________________________________________________________________________
From: "Dan Blake" <danblake(at)worldnet.att.net>
Subject: Re: HELP! Opinions NEEDED!- Go 4
Date: Dec 06, 1999
I got 1.5 hrs. two weekends ago in a guy's Subaru powered -4. He is about 150, and me 225 in the back. Needed a little nose down trim, but otherwise flew beautifully. I'll also agree that to my eyes, the -4 is the best looking RV, but... The -4 is more than a little tight in the back seat for me. My dad is 6'2", and all of my brothers are over 200. I've flown in the back of an -8 and a -4, and -8 is much better for the back seater. Although my wife is small, I want her to be as comfortable as possible. She let me talk her out of a -6, so I need to cut her some slack. Good one her. Showed her pictures of a -6a, then bought the -8 tail kit. She took it well. We will x-country quite a bit, too, so the added useful helps with luggage. No QB in a -4, but I guess that's really not a valid argument for most. RV's - They're all damn wonderful, every one of them. Dan Blake -8 tail Atlanta ----- Original Message ----- From: <JRWillJR(at)aol.com> Sent: Monday, December 06, 1999 1:44 AM Subject: RV-List: HELP! Opinions NEEDED!- Go 4 > > I know that I will be flamed unending but I too still think the RV4 is the > perfect sport aircraft. I liked it when it first came upon the scene and I > like it no less now. This is not to take away from the 8 or the 6 but the 4 > is in my opinion the perfect sporting aircraft. Definitely lighter, possibly > stronger, with on center seating, racy canopy and a superb compromise of > sporting agility with cross country capability. Yes, it has some > negatives---Bubbas on the Van's Bubba Scale beyond 7+ may find the rather > roomy accommodations slightly lacking compared to the 8 but not really much > less than the 6 as you do not have to share elbow room and then there is the > unending legend of the tail heavy RV4. Yes, it is true that I at 180 lbs > probably would not want to shove a 240 pounder into the back seat and go > zoomering about but fortunately for me all my friends are almost normal in > size and my dear wife barely makes 120 dripping wet dressed. I am also of the > opinion and it is just an opinion that aerobatics in any RV should be kept to > a solo proposition anyway. Yep, I still like the 4 and not looking to build > the RV 12 A. JR, RV4 slowly progressing at less than a snails pace > > ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: Setting Wing Incidence Angle
Date: Dec 06, 1999
> > Thanks to Chuck and all who responded to the flap issue. I now have the > wings square with no sweep. The bottom skin is flush with the fuselage. > Per vans instructions for setting incidence on RV4 wing & drawing SK-51 > I need a block 3 and 3/64 inches to get the bubble in the center of > level. this puts the wing rear spar 1/4 inch lower than what Van call > for. I have screwed up too many times already and have had to remove and > replace the rear spar carry through. I do not want to do it again and > would like to get the incidence angle right the first time. > > My question is about the angle of horizontal stabilizer due to the 1/4 > inch difference of the wing. Per SK-48 Van shows a 1/4 spacer under > the level at the rear spar. Would this go to 1/2 inch or decrease to > 0 inch? Earl: There would not be a one to one correlation between the amount you have to adjust the aft wing spar and what you need to adjust the horizontal stab to compensate for it. What you want to keep constant is the relative angles between the wing and horiz. stab.. Divide the .25" by the distance between the main wing spar and aft wing spar, and then multiply it by the fore/aft distance between the spars on the horiz. stab. This should get you the amount to adjust the h. stab. It will be something less than half the .25". This is important - you really should try to find a EAA tech counselor or another RV builder to go through this with, as I'm not sure I understood your problem correctly. Hang in there, there is no hurry to drill those aft spar holes. Alex Peterson Maple Grove, MN 6A ________________________________________________________________________________
From: "Bert F. Murillo" <bertrv(at)intellistar.net>
Subject: Re: Personal experience with Aircraft fire
Date: Dec 06, 1999
Ed: ________________________________________________________________________________
From: "Bert F. Murillo" <bertrv(at)intellistar.net>
Subject: Re: Fw: RV VG's costs
Date: Dec 06, 1999
Ted: what type of material are these tabs....For more than $400 they must be an exotic material? Bert DoNot archive ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)home.com>
Subject: Re: Hours
Date: Dec 06, 1999
>If my electric tach only records time on the meter when it runs at 1500+ >how should I record my time on the aircraft as well as in my log. I've >always just used the hobbs for my log (flying) time. Should I just record >time for the aircraft and logbook by real time? From FAR 1.1 General Definitions: Flight time means: (1) Pilot time that commences when an aircraft moves under its own power for the purpose of flight and ends when the aircraft comes to rest after landing; In practice this means you can log time pretty much any time you want. Hobbs and tach time are most commonly used but some people like to keep track of actual "flight" time. I don't think the FAA really cares unless you overstate your time. Randall Henderson, RV-6 N6R (~50 hrs) Portland, OR http://www.edt.com/homewing ________________________________________________________________________________
From: "Terry Watson" <tcwatson(at)seanet.com>
Subject: Re: Rear Fuel Tank Baffle
Date: Dec 06, 1999
I had just the same question about attaching the rear baffle to my '8 tanks. Earlier this evening I watched George's video on sealing the tanks, and he goes ahead and rivets the baffles to the skin and then puts the wood clamps on too. No mention of letting it cure, then countersinking instead of dimpling the skins. Terry Watson, #80729 ----- Original Message ----- From: Stephen Johnson <spjohnsn(at)ix.netcom.com> > I'm thinking about the process of closing up the tank with the rear baffle. > I'm building a RV-8 if it matters. I have checked out Sam Buchanan's > excellent site, and his method looks good, but there are some conflicts with > accounts from other sources. The manual from Van's says the baffle should > be sealed first, and then the skin should be countersunk and riveted after > the sealant cures. Some posters on the list have suggested using Saran Wrap > over the spars and allowing the tank to final cure on the wing to insure a > good fit. This would make it impossible to apply the wood clamps as shown > on Sam's web page. I know there can be more than one way to do things, but > I thought I'd get opinions before doing anything permanent. > > Thanks in advance, > > Steve Johnson > RV-8 #80121 ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Dec 07, 1999
Subject: Re: Experience with IVO Props
Mike Thompson, I disagree, I have IVO experience, and the problem is not the composite blades but the design of the prop itself and the method of securing the blades--a metal or wooden prop with the same design would suffer the same problem. There is at least one list member--the Maroon Marauder or some such--that has had good success with the IVO. I will not go into my saga as it has already been posted to the archives--but for your info I vote NO on IVO. JR ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)home.com>
Subject: Re: Hours
Date: Dec 06, 1999
>In practice this means you can log time pretty much any time you want. Hobbs >and tach time are most commonly used but some people like to keep track of >actual "flight" time. I don't think the FAA really cares unless you >overstate your time. Oops -- I reread the original post and you were talking about aircraft log too... wouldn't want to UNDERstate in your engine/airframe log either! I can't speak with any authority on that although I don't think logging the "over 1500" time would turn out to be much different than what you get from a mechanical tach (assume it's working right), since those are calibrated for a specific cruise RPM. So time logged from that is only a guestimate anyhow. Randall ________________________________________________________________________________
From: Boalty(at)aol.com
Date: Dec 07, 1999
Subject: fuel fittings
Anybody know off the top if there is such an animal as a female union for fuel lines? I'm trying to close couple the facet pump to an Airflow Performance filter w/o having to make up a short section of alum. tube. Thanks, mates. ________________________________________________________________________________
Date: Dec 07, 1999
From: Chuck Brietigam <brietigam(at)earthlink.net>
Subject: Re: fuel fittings
Boalty(at)aol.com wrote: > > Anybody know off the top if there is such an animal as a female union for > fuel lines? I'm trying to close couple the facet pump to an Airflow > Performance filter w/o having to make up a short section of alum. tube. > Thanks, mates. > You might wish to look in an EARL's catalog. They're a car parts supplier that sells 37 degree fitting to the hot rod set. They have many very clever fittings you don't find elsewhere. Their number is 310-609-1602. Chuck Brietigam, RV-3's forever!!! ________________________________________________________________________________
From: GRGSCHMIDT(at)aol.com
Date: Dec 07, 1999
Subject: Re: fuel fittings
Yes there are special fittings available from Earl's Performance Products at 189 W. Victoria St. Long Beach Ca. 90805 Phone 310 609-1602. Most speed shops carry their products and I found them to be of superior quality when compared to Aeroquip. They will send you a catalog within a few days and you can see what is available. Good luck Greg Schmidt RV6S Wiring and Canopy fairing forming PHX Deer Valley (DVT) ________________________________________________________________________________
From: TRAASHMAN(at)webtv.net (Joe Waltz)
Date: Dec 07, 1999
Subject: Re: Carb heat
Eustace, Thanks for the reply. I was worried that you were using unfiltered air in dusty conditions. ________________________________________________________________________________
From: "Fesenbek, Gary" <fesenbek(at)marykay.com>
Subject: HELP! Opinions NEEDED!
Date: Dec 07, 1999
One important item to check before you purchase any airplane is.... Will I be able to insure it? If that is important to you. In-motion aircraft insurance was very important to me. I don't know what the insurance situtation is with the Rocket but you might want to check that out prior to investing a few years building one. The same goes for any other kit. Gary Fesenbek RV6A Dallas, TX ________________________________________________________________________________
From: "Ollie Washburn" <skybolt-aviator(at)msn.com>
Subject: Flyins
Date: Dec 07, 1999
Looking for alist of flying RVers in Fl. to get together for lunch or flyins. Ollie RV6-A N716R ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: HELP! Opinions NEEDED!- Go 4
Date: Dec 07, 1999
Be very careful with that much weight in the back seat of a -4. I lost two friends on the turn to final stall-spin. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Dan Blake <danblake(at)worldnet.att.net> Date: Monday, December 06, 1999 10:48 PM Subject: Re: RV-List: HELP! Opinions NEEDED!- Go 4 > >I got 1.5 hrs. two weekends ago in a guy's Subaru powered -4. He is about >150, and me 225 in the back. Needed a little nose down trim, but otherwise >flew beautifully. I'll also agree that to my eyes, the -4 is the best >looking RV, but... > >The -4 is more than a little tight in the back seat for me. My dad is 6'2", >and all of my brothers are over 200. I've flown in the back of an -8 and >a -4, and -8 is much better for the back seater. Although my wife is small, >I want her to be as comfortable as possible. She let me talk her out of >a -6, so I need to cut her some slack. Good one her. Showed her pictures >of a -6a, then bought the -8 tail kit. She took it well. We will >quite a bit, too, so the added useful helps with luggage. No QB in a -4, >but I guess that's really not a valid argument for most. > >RV's - They're all damn wonderful, every one of them. > >Dan Blake >-8 tail >Atlanta > >----- Original Message ----- >From: <JRWillJR(at)aol.com> >To: >Sent: Monday, December 06, 1999 1:44 AM >Subject: RV-List: HELP! Opinions NEEDED!- Go 4 > > >> >> I know that I will be flamed unending but I too still think the RV4 is the >> perfect sport aircraft. I liked it when it first came upon the scene and I >> like it no less now. This is not to take away from the 8 or the 6 but the >4 >> is in my opinion the perfect sporting aircraft. Definitely lighter, >possibly >> stronger, with on center seating, racy canopy and a superb compromise of >> sporting agility with cross country capability. Yes, it has some >> negatives---Bubbas on the Van's Bubba Scale beyond 7+ may find the rather >> roomy accommodations slightly lacking compared to the 8 but not really >much >> less than the 6 as you do not have to share elbow room and then there is >the >> unending legend of the tail heavy RV4. Yes, it is true that I at 180 lbs >> probably would not want to shove a 240 pounder into the back seat and go >> zoomering about but fortunately for me all my friends are almost normal in >> size and my dear wife barely makes 120 dripping wet dressed. I am also of >the >> opinion and it is just an opinion that aerobatics in any RV should be kept >to >> a solo proposition anyway. Yep, I still like the 4 and not looking to >build >> the RV 12 A. JR, RV4 slowly progressing at less than a snails pace >> >> > > ________________________________________________________________________________
From: "Rob Reece" <reece(at)rt66.com>
Subject: fuel fittings: Earl's
Date: Dec 07, 1999
I stopped by Earl's while on business in Torrance CA. They can make you any custom flex lines/fittings combination you like and are reasonable in price. We had to go there for some emergency 15' flex lines for an aerospace vavle qualification test I was running and they garunteed them to 1500 psi and had them made in about an hour. Great folk, good product. I noticed that they carry nice aluminum oil coolers in a variety of sizes that already have AN fittings welded on to them. They appear perfect for homebuilt use and only run about $80 or so if I remeber correctly. Blue skies & RV-3's forever! Rob Reece RV-3 SN45 > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Chuck Brietigam > Sent: Tuesday, December 07, 1999 5:19 AM > To: rv-list(at)matronics.com > Subject: Re: RV-List: fuel fittings > > > Boalty(at)aol.com wrote: > > > > > Anybody know off the top if there is such an animal as a female > union for > > fuel lines? I'm trying to close couple the facet pump to an Airflow > > Performance filter w/o having to make up a short section of alum. tube. > > Thanks, mates. > > > > You might wish to look in an EARL's catalog. They're a car parts > supplier that sells 37 degree fitting to the hot rod set. They > have many very > clever fittings you don't find elsewhere. Their number is 310-609-1602. > Chuck Brietigam, RV-3's forever!!! > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: Fw: RV VG's costs
Date: Dec 07, 1999
Part of the cost is the engineering and development. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Bert F. Murillo <bertrv(at)intellistar.net> Date: Monday, December 06, 1999 11:00 PM Subject: Re: RV-List: Fw: RV VG's costs > >Ted: what type of material are these tabs....For more than $400 >they must be an exotic material? > >Bert >DoNot archive > > ________________________________________________________________________________
From: FGoggio(at)aol.com
Date: Dec 07, 1999
Subject: Re: Experience with IVO Props
referance the ivo prop conversation i had a hanger mate that had the ivo magnum prop on a rotax 912, flew it about 10 hours,had problem with the copper strips moving also,checked and found that the bolt holes were elogating in the hub, was getting to much play in the hub,the metal in hub was too soft,ivo stated that nothing was wronge with it,he throw it in the trash can, i have it on my wall right now to look at, refuse to even sell it,dont want a friend of mine to have a problem with it,in all fairnes to the design of the prop,it in it self seem to be a good preforming prop , frank goggio fayetteville nc ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Dec 07, 1999
Subject: Re: fuel fittings
In a message dated 12/7/99 12:12:33 AM Pacific Standard Time, Boalty(at)aol.com writes: << Anybody know off the top if there is such an animal as a female union for fuel lines? I'm trying to close couple the facet pump to an Airflow Performance filter w/o having to make up a short section of alum. tube. >> Earl's P/N 915106 Straight female to female swivel coupling 3/8". -GV ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: fuel fittings: Earl's
Date: Dec 07, 1999
> > >I stopped by Earl's while on business in Torrance CA. They can make you >any >custom flex lines/fittings combination you like and are reasonable in >price. >We had to go there for some emergency 15' flex lines for an aerospace vavle >qualification test I was running and they garunteed them to 1500 psi and >had them made in about an hour. Great folk, good product. > >I noticed that they carry nice aluminum oil coolers in a variety of sizes >that already have AN fittings welded on to them. They appear perfect for >homebuilt use and only run about $80 or so if I remeber correctly. > >Blue skies & RV-3's forever! > >Rob Reece >RV-3 SN45 I have many of Earl's AN fittings in my fuel system and they work just fine. I did find one bulkhead fitting that had one flare that looked pretty bad. Obviously a manufacturing flaw. I took it back to the local seal and fitting supply where I bought it and they exchanged it no questions asked. So, just make sure to visually inspect them before use. Of course, this applies to any fitting from any source. Brian Denk RV8 N94BD Albuquerque, NM Inspection time! ________________________________________________________________________________
From: "Gummos" <tg1965(at)linkline.com>
Subject: Re: HELP! Opinions NEEDED!
Date: Dec 07, 1999
> One important item to check before you purchase any airplane is.... > Will I be able to insure it? If that is important to you. In-motion > aircraft insurance was very important to me. I don't know what the > insurance situtation is with the Rocket but you might want to check that out > prior to investing a few years building one Gary, I was one of the first to complain about getting insurance for my rocket project. I have obtained 50 hours of tailwheel time and now have a quote coming. I will supply details once I know. Then maybe we can compare what the rates are for an RV-4 vs Rocket. Tom Gummo Apple Valley,CA engine, cowl, other 90% to go items, first flight in next millennium ________________________________________________________________________________
Date: Dec 07, 1999
From: Garry Legare <versadek(at)earthlink.net>
Subject: AN fittings/ lines & fuel cap engraving
Paul Bessing posted a note regarding Earls back in July. (message #57377) He also noted that if you call Dick at WM. Engineering 800-886-3275, he would give you jobber price. I have dealt with Dick for about three mouths and what Paul didn't mention was how great this guy is to deal with. Your orders no matter how small are shipped instantly and are what you ordered. A couple of times to save me cod fees he just shipped smaller items and asked me to send a check. Lets see, Great service, Good prices and a Great Guy to deal with, WOW. I think we should implement some kind of rating for suppliers. Say a scale of 1 to 5 "Vs", if we did WM. Engineering would get a solid "5Vs". While I'm on the subject of service, you might remember I posted a note regarding fuel cap engraving and a company called Engraphics. Well my caps are back, and the quality of the work is substandard (letters touching each other, letters are not consistent from cap to cap (I have three). I don't recommend Engraphics. They would get 1V and that is only because they did return them in a reasonable time frame. ________________________________________________________________________________
Date: Dec 07, 1999
From: Louis Willig <larywil(at)home.com>
Subject: RV-4 Weight & Balance
In several recent posts, it was mentioned that the RV-4 is a little touchy in the area of weight and balance, and that we have to be careful about passenger and baggage loading. This is true of most RV-4's. However, when you have a -4 with an 0-360, or more, an IO-360, or more yet, an IO-360 with constant speed prop, gross weight is more important to look at than W & B. Its nearly impossible to get out of W&B in my -4 with it's 0-360. And in keeping strictly with Van's suggestions on Maximum Gross Wt. I have always been restricted by weight, but never balance. I do cheat, sometimes, in the gross weight area if I going out in smooth weather with my copilot. But I never cheat in the W&B...Its almost impossible to leave the envelope. And, of course, I would never dare to load too far to the rear anyway. Interestingly, max rear trim is barely enough to keep me on the glide slope with a lightweight passenger. Next week, I'm going to install one of Mark Landoll's flywheel weight rings to smooth out my low RPM vibrations. Then I'm going to have to pull hard to stay on the glide slope. Yukkk. Louis Louis I. Willig, RV-4 - N8ZZ larywil(at)home.com (610) 668-4964 Philadelphia, PA ________________________________________________________________________________
Date: Dec 07, 1999
From: Chris Browne <cebrowne(at)earthlink.net>
Subject: 3M FIRE BARRIER 2000
Has anyone used this to seal gaps in the firewall? I know from the archives most folks use proseal or high temp RTV, but I saw this in ACS and it design to expand and insulate under direct flame. It is supposed to go on just like regular caulk. Chris Browne -6A Altanta ________________________________________________________________________________
From: "Rick Caldwell" <racaldwell(at)hotmail.com>
Subject: Flap Tape
Date: Dec 07, 1999
I need to order some teflon or UHMW tape for my flaps. What is the width required? Should the tape go on the flaps or under the top wing skin overhang? I'm getting my tape locally and don't have Van's catalog with me. Van's leadtime is too long because the RV is going to the airport Saturday! Rick Caldwell RV-6 one wing left to paint. Melbourne, FL ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: RV-4 Weight & Balance
Date: Dec 07, 1999
Maybe I should elaborate on my friends. Even though one might be in proper W&B, when you approach after CG. Stalls with the ball not centered can be a real event. As snap to spin can quickly happen. I had one when my son and I were air camping is a Skyhawk. Poor handling of the controls at low air speed and the normally benign Skyhawk snapped into a spin. Why, our camping gear was in back. Obviously I had enough altitude for recovery. My friends that overbanked the turn to final did not. In both cases, it was due to NOT using the controls smoothly, and not having the ball centered. Aft CG aggravates the situation. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Louis Willig <larywil(at)home.com> Date: Tuesday, December 07, 1999 10:55 AM Subject: RV-List: RV-4 Weight & Balance > > >In several recent posts, it was mentioned that the RV-4 is a little touchy >in the area of weight and balance, and that we have to be careful about >passenger and baggage loading. This is true of most RV-4's. However, when >you have a -4 with an 0-360, or more, an IO-360, or more yet, an IO-360 >with constant speed prop, gross weight is more important to look at than W >& B. Its nearly impossible to get out of W&B in my -4 with it's 0-360. >And in keeping strictly with Van's suggestions on Maximum Gross Wt. I have >always been restricted by weight, but never balance. I do cheat, sometimes, >in the gross weight area if I going out in smooth weather with my copilot. >But I never cheat in the W&B...Its almost impossible to leave the envelope. >And, of course, I would never dare to load too far to the rear anyway. >Interestingly, max rear trim is barely enough to keep me on the glide slope >with a lightweight passenger. > >Next week, I'm going to install one of Mark Landoll's flywheel weight rings >to smooth out my low RPM vibrations. Then I'm going to have to pull hard to >stay on the glide slope. Yukkk. > >Louis > >Louis I. Willig, RV-4 - N8ZZ >larywil(at)home.com >(610) 668-4964 >Philadelphia, PA > > ________________________________________________________________________________
From: "Rob Reece" <reece(at)rt66.com>
Subject: Flap Tape
Date: Dec 07, 1999
You can get it from Avery Tools by Thursday/Friday. Catalog number 8469, .010" UHMW x 3" x 10', for $12.00 roll. It is usually placed under the wing skin. Rob Reece RV-3 SN45 > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Rick Caldwell > Sent: Tuesday, December 07, 1999 10:10 AM > To: rv-list(at)matronics.com > Subject: RV-List: Flap Tape > > > I need to order some teflon or UHMW tape for my flaps. What is the width > required? Should the tape go on the flaps or under the top wing skin > overhang? > > I'm getting my tape locally and don't have Van's catalog with me. Van's > leadtime is too long because the RV is going to the airport Saturday! > > Rick Caldwell > RV-6 one wing left to paint. > Melbourne, FL > > ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)shuswap.net>
Subject: Re: Carb heat
Date: Dec 07, 1999
---------- > From: Denton Harjehausen <harje(at)proaxis.com> > To: rv-list(at)matronics.com > Subject: Re: RV-List: Carb heat > Date: Sunday, December 05, 1999 3:46 PM > > Hi Denton: See my thoughts below: > Thanks, Eustace! I have wondered since I returned to carb. power why there > wasn't an electrically heated system. There seems to be a lot of off field > landings/crashes blamed on carb. ice. If it isn't caught in time as we all > know there is no heat to clear the passage. Though it does seem like an > electric heated system would be another problem to add to the already > complex and costly safety sytems of airplanes. And it seems to be more > likely in some aircraft then others. > > A friend of mine had it happened to him in a Tomahawk a couple years ago > here in Oregon. He said it happened very suddenly with no warning. The > engine started to lose RPM, he pulled the carb heat and it quit. They were > low and had little choice in landing fields. He and his wife did walked > away with scatches and bruises, but the plane was junk. I have heard of a > couple of others in the last couple years, locally. Denton I think what happened here was the pilot did not recognize the warning signals that the engine would be giving such as the gradual loss off RPM or because off the type of maneuvering he was doing and then it got so advanced when he did apply carb heat he got such a slug of water that it killed the engine. If he had the height he probably could have restarted it. This is another case of the pilot not paying enough attention to his engine. > I don't have the prop time you have, Eustace, but I had it happen one time > in my prop time, in a Luscombe, in the '50, low over Long Beach, Calif. It > lost a lot of power suddenly, I pulled the Carb heat, it got worst, I was > looking for some soft place in the city to land and then it roared back to > life. It left me with nightmares for awhile, plus a real interest in the > subject. This is normal when you have a large build up of carb ice it is just the water going through. If you are not used to it it can be a bit disconcerting but on the other hand it can be music to your ears knowing that your carb heat is working. Regards Eustace > > Have a great Day! > Denny Harjehausen > Lebanon, OR > RV-6 > > > ________________________________________________________________________________
Date: Dec 07, 1999
From: Jeff Hays <jshays(at)interaccess.com>
Subject: Re: 3M FIRE BARRIER 2000
Check out this link, it's the 3M webpage for the Fire Barrier: http://www.3M.com/firestop/html/p_01.html Jeff Hays. On Tue, 7 Dec 1999, Chris Browne wrote: > > Has anyone used this to seal gaps in the firewall? I know from the > archives most folks use proseal or high temp RTV, but I saw this in ACS > and it design to expand and insulate under direct flame. It is supposed > to go on just like regular caulk. > > Chris Browne > -6A > Altanta > > > > > ________________________________________________________________________________
Date: Dec 07, 1999
From: Chris Browne <cebrowne(at)earthlink.net>
Subject: Re: 3M FIRE BARRIER 2000
Yeah, I saw it. After visiting the web page, I just bought some from a 3M fire protection products distributor in Atlanta for for $12.00. Or you can buy it for $21.50 from ACS. Think I'll try it out - has to be as good as proseal or RTV. Chris Browne -6A finish Atlanta Jeff Hays wrote: > > Check out this link, it's the 3M webpage for the Fire Barrier: > > http://www.3M.com/firestop/html/p_01.html > > Jeff Hays. > ________________________________________________________________________________
From: donspawn(at)juno.com
Subject: 6A-canopy frame
Date: Dec 07, 1999
I have my F671 fwd top skin clecoed on to overlap the fuselage skins. Have the C602 canopy fwd skin clecoed to the weldment across the top & into the round tubing. I need to drill the "lower row" of rivets into the f616. Can't see how I will allow the plexi to fit on top of this skin, yet duck inside it on the sides. If I nail the lower row of rivets, I will not be able to "joggle" for the glass later. I saw one project with notches cut but would rather joggle. I need to fit the c603 side skin to the F631 rear frame & to the C602 top skin. Should I work from the rear & line up the 603 to the 625 structure , then to the 602. Will C603 side skin " clecoed on" hold the weight & side force of the plexi while I am marking for trimming? Please Helllllpppp. Don Jordan ~ 6A fuselage ~ Arlington,Tx ~ donspawn(at)juno.com ________________________________________________________________________________
Date: Dec 08, 1999
From: Frank and Dorothy <frankvdh(at)ihug.co.nz>
Subject: Re: Setting Wing Incidence Angle
Alex Peterson wrote: > This is important - you really should try to find a EAA tech > counselor or another RV builder to go through this with, as I'm not sure I > understood your problem correctly. Hang in there, there is no hurry to > drill those aft spar holes. What Alex wrote is right about the angles. However, no-one so far has mentioned the thrustline... if the wing is inclined upward relative to the fuselage a few degrees, and the HS the same amount, then when the wing is in level flight the fuselage will be inclined down by that angle. And that means that (unless you adjust your engine mounts accordingly) the engine will also be pointing downward a few degrees. Even if the mounts are shimmed to angle up by the right amount, the relative positions of thrustline, wing, and HS will be displaced vertically from their designed positions by a small amount. I have no idea what effect this might have on flight characteristics. Earl, I suggest you discuss this whole thing with Van's. Frank. ________________________________________________________________________________
From: "Paul Besing" <rv8er(at)home.com>
Subject: Re: 6A-canopy frame
Date: Dec 07, 1999
If I am reading your post correctly, the plexi does not go inside of the skin on the sides. I put in the lower row of rivets, and had no problem doing the joggle with seaming pliers. You should match the side skin up with the forward canopy skin. Leave the aft side long for now, as you should trim it when everything is in place and things won't move. Yes, clecos will hold it down for cutting and trimming. Also, be absolutely sure that all things are attached and tight when you mark and trim. I mean have the latch mechanism in and latched, the gas struts in, etc, etc...this way there will be no surprises when you put those things in...please, don't ask me how I know this...the new bubble will be here in January. Paul Besing RV-6A (197AB) Arizona http://members.home.net/rv8er Finish Kit -----Original Message----- From: donspawn(at)juno.com <donspawn(at)juno.com> Date: Tuesday, December 07, 1999 1:17 PM Subject: RV-List: 6A-canopy frame > >I have my F671 fwd top skin clecoed on to overlap the fuselage skins. >Have the C602 canopy fwd skin clecoed to the weldment across the top & >into the round tubing. I need to drill the "lower row" of rivets into the >f616. > >Can't see how I will allow the plexi to fit on top of this skin, yet duck >inside it on the sides. If I nail the lower row of rivets, I will not be >able to "joggle" for the glass later. I saw one project with notches cut >but would rather joggle. > >I need to fit the c603 side skin to the F631 rear frame & to the C602 top >skin. >Should I work from the rear & line up the 603 to the 625 structure , then >to the 602. >Will C603 side skin " clecoed on" hold the weight & side force of the >plexi while I am marking for trimming? > >Please Helllllpppp. > >Don Jordan ~ 6A fuselage ~ Arlington,Tx ~ donspawn(at)juno.com > > ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Dec 07, 1999
Subject: Re: Electric Bob-alternator question
I am trying to hook a regulator up that is a external unit #F7078 that is about one inch by two inch by 1/4 inch thick that is embedded in potting compound with a small pot sticking out of the potting compound (voltage adjustment)...... You mount this unit to the rear of your alternator and hook the pigtails up as the instructions detail. I am using your supplied drawing.... z fig 2. Where, in the battery alt switch, there exits a wire to the OV module ( which I purchased) to the CB to the "A" lead to the regulator......I can't seem to find this connection on the Mark Landoll regulator ......no "A" lead is described or apparent on this type of regulator ( as described above). I want to use your drawings so am I better off using the Wells/Ford unit or can I still use the small "can" I described above and hope to find the proper lead ?? The instructions that came with the "can" state:: From the alternator connect the red wire to the alternator studd labeled BAT... connect the yellow wire to the studd labeled STA & connect the green wire to the studd labeled FLD...there is no mention of the control line & I want to install (via your z fig 2 )......I assume the regulator is getting its B+ from the BAT terminal. H E L P ....... ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Dec 07, 1999
Subject: Re: Countersunk Washers/Cutting Fiberglass
I took a tip from the Glassair/Lancair/Plastic Porta-Toilet builders...& use a dremmel bit with a "cone shaped stone"on the end. With a little shopping I found a store that a few cone shapped stones that fit my #6,#8 & #10 C/S washers. The neat thing is it dosen't dull your cutter (if you found one) F/G really chewes-up any metal cutter......the stones put a nice cut in the F/G & sorta burnish the hole thereby sealing out oils & watter & dirt from the substratta matrix of the F/G... rv8er(at)home.com on 12/06/99 11:03:23 PM Please respond to rv-list(at)matronics.com Subject: RV-List: Countersunk Washers How does one countersink fiberglass for the #6 Countersink washers? Is there is a different size bit? Paul Besing RV-6A (197AB) Arizona http://members.home.net/rv8er Finish Kit ________________________________________________________________________________
From: TRAASHMAN(at)webtv.net (Joe Waltz)
Date: Dec 07, 1999
Subject: fuel fittings: Earl's
Like Brian Denk said, "inspect it all before use." I got an AN6 fitting from ACS that had no threads on the pipe fitting side. Of course this was easily detected but it points out the fallability of even aircraft parts. ________________________________________________________________________________
From: donspawn(at)juno.com
Subject: 6A-canopy frame
Date: Dec 07, 1999
>If I am reading your post correctly, the plexi does not go inside of the >skin on the sides. My writing never comes out like I am thinking. I understand the 603 side pieces go outside the glass & the frame inside. > I put in the lower row of rivets, and had no problem doing the joggle with >seaming pliers. That is what I wanted to here. When I get there, I will send the Lear for you. >You should match the side skin up with the forward canopy skin. Leave >the aft side long for now, as you should trim it when everything is in >place and things won't move. Yes, clecos will hold it down for cutting and >trimming. Also, be absolutely sure that all things are attached and tight when >you mark and trim. I mean have the latch mechanism in and latched, the >gas struts in, etc, etc...this way there will be no surprises when you put >those things in...please, don't ask me how I know this...the new bubble will >be here in January. Now that is out of the normal order. I will look into that. I just been going with the instructions. I remmember you got a little upset at that first try. Sorry to hear that. The instrustions I was reading last nite, indicated some drill the glass as a hole & some split it & then drill to the roll bar & back frame. Which way do you recommend? Also what caused your canopy to crack? Don Jordan ~ 6A fuselage ~ Arlington,Tx ~ donspawn(at)juno.com ======================================================== > >Paul Besing >RV-6A (197AB) Arizona >http://members.home.net/rv8er >Finish Kit > >-----Original Message----- >From: donspawn(at)juno.com <donspawn(at)juno.com> >To: rv-list(at)matronics.com >Date: Tuesday, December 07, 1999 1:17 PM >Subject: RV-List: 6A-canopy frame > > >> >>I have my F671 fwd top skin clecoed on to overlap the fuselage skins. >>Have the C602 canopy fwd skin clecoed to the weldment across the top >& >>into the round tubing. I need to drill the "lower row" of rivets into >the >>f616. >> >>Can't see how I will allow the plexi to fit on top of this skin, yet >duck >>inside it on the sides. If I nail the lower row of rivets, I will not >be >>able to "joggle" for the glass later. I saw one project with notches >cut >>but would rather joggle. >> >>I need to fit the c603 side skin to the F631 rear frame & to the C602 >top >>skin. >>Should I work from the rear & line up the 603 to the 625 structure , >then >>to the 602. >>Will C603 side skin " clecoed on" hold the weight & side force of >the >>plexi while I am marking for trimming? >> >>Please Helllllpppp. >> >>Don Jordan ~ 6A fuselage ~ Arlington,Tx ~ donspawn(at)juno.com >> >> > > ________________________________________________________________________________
From: "Bob Newman" <newmanb(at)erols.com>
Date: Dec 07, 1999
Subject: Re: 3M FIRE BARRIER 2000
Firestop rated sealant is also available from drywall supply companies; not Lowes or Home Depot, but commercial drywall supply companies that service the trade. I paid $11.95 for a 10 OZ tube. It seems to go on fine. Bob Newman > archives most folks use proseal or high temp RTV, but I saw this in ACS > and it design to expand and insulate under direct flame. > Altanta > ________________________________________________________________________________
Date: Dec 07, 1999
From: John Kitz <jkitz(at)greenapple.com>
Subject: Re: fuel fittings
> > > > > Anybody know off the top if there is such an animal as a female union for > > fuel lines? I'm trying to close couple the facet pump to an Airflow > > Performance filter w/o having to make up a short section of alum. tube. > > Thanks, mates. > > > > You might wish to look in an EARL's catalog. They're a car parts > supplier that sells 37 degree fitting to the hot rod set. They have many very > clever fittings you don't find elsewhere. Their number is 310-609-1602. > Earls has a web site. I bought fittings and an oil cooler from Earls and it has worked great. http://www.earls3.com/ John Kitz N721JK Ohio ________________________________________________________________________________
From: "Morrissey, John" <John.Morrissey(at)its.csiro.au>
Subject: 3M FIRE BARRIER 2000
Date: Dec 08, 1999
Hi All, What about the statement on the web page that says; 3. Limitations 3M Fire Barrier 2000 and 2003 Silicone Sealants should not be applied to: - Building materials that bleed oils, plasticizers or solvents (e.g., impregnated wood, oil-based caulks, green or partially vulcanized rubber) I would have thought that an engine bay would be "Full" of things that bleed oils!! Just a thought. John Morrissey -----Original Message----- From: Chris Browne [mailto:cebrowne(at)earthlink.net] Sent: Wednesday, 8 December 1999 6:21 Subject: Re: RV-List: 3M FIRE BARRIER 2000 Yeah, I saw it. After visiting the web page, I just bought some from a 3M fire protection products distributor in Atlanta for for $12.00. Or you can buy it for $21.50 from ACS. Think I'll try it out - has to be as good as proseal or RTV. Chris Browne -6A finish Atlanta Jeff Hays wrote: > > Check out this link, it's the 3M webpage for the Fire Barrier: > > http://www.3M.com/firestop/html/p_01.html > > Jeff Hays. > ________________________________________________________________________________
From: RV8DRIVER(at)aol.com
Date: Dec 07, 1999
Subject: Re: Rear Fuel Tank Baffle
>Hi Listers, I'm thinking about the process of closing up the tank with the rear baffle. I'm building a RV-8 if it matters. I have checked out Sam Buchanan's excellent site, and his method looks good, but there are some conflicts with accounts from other sources. The manual from Van's says the baffle should be sealed first, and then the skin should be countersunk and riveted after the sealant cures. Some posters on the list have suggested using Saran Wrap over the spars and allowing the tank to final cure on the wing to insure a good fit. This would make it impossible to apply the wood clamps as shown on Sam's web page. I know there can be more than one way to do things, but I thought I'd get opinions before doing anything permanent. Thanks in advance, Steve Johnson RV-8 #80121< Steve. I'm also building an -8, and have given the tank construction some thought. With regard to the idea of letting the tank final cure on the spar, I don't believe its necessary if you carefully control the tank skins in the leading edge jig. By this I mean that if you make certain that the top edges of the skins are perfectly parallel to each other, you obviouslycannot have a twist in it and it should fit fine. This can be done with an acccurate bubble level. It won't matter if the tank is level in the long dimension, just that both ends read the same on the level. Of course, if you have a twist in the spar, the tank won't fit. (Just kidding, Heaven forbid!) Andy Johnson ________________________________________________________________________________
Date: Dec 07, 1999
From: Chris Browne <cebrowne(at)earthlink.net>
Subject: Re: 3M FIRE BARRIER 2000
Hi John, My guess would be adherence since nothing will stick to an oily surface, including proseal and RTV. I'll check the tube, though. Chris Browne -6A finish Atlanta "Morrissey, John" wrote: > > Hi All, > > What about the statement on the web page that says; > > 3. Limitations > > 3M Fire Barrier 2000 and 2003 Silicone Sealants should not be applied to: > > - Building materials that bleed oils, plasticizers or solvents (e.g., > impregnated wood, oil-based caulks, green or partially > vulcanized rubber) > > I would have thought that an engine bay would be "Full" of things that bleed > oils!! > > Just a thought. > > John Morrissey > ________________________________________________________________________________
From: "Paul Besing" <rv8er(at)home.com>
Subject: Re: 6A-canopy frame
Date: Dec 07, 1999
Your best bet is to scrap the Van's instructions, and go by the Wil Cresinger instructions..they are much more detailed, and more logical. You can download them from: http://www.flash.net/~gila/wing_docs/canopy_notes2.htm FWIW, I cut the two first, then did the drilling...I think it would be tough the other way..but then again, I don't think I am that credible, as I am now going to be on canopy #2! Paul Besing RV-6A (197AB) Arizona http://members.home.net/rv8er Finish Kit > ________________________________________________________________________________
From: "Russell Duffy" <rv8(at)mindspring.com>
Subject: breakaway fuel fittings ?
Date: Dec 07, 1999
Greetings, Since we're on the subject of fuel fittings, has anyone ever seen a breakaway fitting small enough for use on the hoses that run from the fuselage to the fuel tanks? Every gas pump has one of these fittings that are made to break away and seal off the hose if someone happens to drive away with the nozzle in their tank. Of course these are huge, but I wondered if anyone makes one small enough to use for the tank hoses. It seems like that would be really good insurance in the case of an accident that pulls the wingtip back. I guess the other option would be to use flex hose and leave enough slack to cover any reasonable amount of seperation between the wing and fuselage. Just an idle thought . Russell Duffy Navarre, FL RV-8, sn-587, N174KT (trade project for 8 hours of sleep) ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: 3M FIRE BARRIER 2000
Date: Dec 07, 1999
The caulk probably doesn't adhere to oily surfaces. For one that bleeds oil, the fire barrier would fall off or become loose. Since aluminum is NOT porous, I don't think it would be a problem. You could ask if gas and oil would do this to the sealing you were doing to your combine enclosure after you applied it to a clean metal surface!!! Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Morrissey, John <John.Morrissey(at)its.csiro.au> Date: Tuesday, December 07, 1999 4:01 PM Subject: RE: RV-List: 3M FIRE BARRIER 2000 > >Hi All, > >What about the statement on the web page that says; > >3. Limitations > > 3M Fire Barrier 2000 and 2003 Silicone Sealants should not be applied to: > >- Building materials that bleed oils, plasticizers or solvents (e.g., >impregnated wood, oil-based caulks, green or partially >vulcanized rubber) > >I would have thought that an engine bay would be "Full" of things that bleed >oils!! > >Just a thought. > >John Morrissey > >-----Original Message----- >From: Chris Browne [mailto:cebrowne(at)earthlink.net] >Sent: Wednesday, 8 December 1999 6:21 >To: rv-list(at)matronics.com >Subject: Re: RV-List: 3M FIRE BARRIER 2000 > > >Yeah, I saw it. After visiting the web page, I just bought some from a 3M >fire protection products distributor in Atlanta for for $12.00. Or you can >buy it for $21.50 from ACS. Think I'll try it out - has to be as good as >proseal or RTV. > >Chris Browne >-6A finish >Atlanta > >Jeff Hays wrote: > >> >> Check out this link, it's the 3M webpage for the Fire Barrier: >> >> http://www.3M.com/firestop/html/p_01.html >> >> Jeff Hays. >> > > ________________________________________________________________________________
Date: Dec 07, 1999
From: Gert <gert(at)execpc.com>
Subject: Re: Drill press
Bill How's your drill press working out for you ?? Gert The Von Dane's wrote: > > > This is the drill press I bought: > http://www.harborfreight.com/cpi/taf/displayitem.taf?Itemnumber=583 > > Grizzly Tools sells a similar 12 speed drill press: > http://www.grizzlyindustrial.com/fcgi-bin/lookup.fcgi/products/lookup. > cfg?q=item&kw=G7944 > > Bill Von Dane > RV-8A N912V (reserved) Elevators > http://vondane.tripod.com > _ > _ > ----- Original Message ----- > From: Ken Balch <kbalch1(at)mediaone.net> > To: > Sent: Sunday, November 28, 1999 5:41 PM > Subject: Re: RV-List: Drill press > > > Hi Bill, > > It's a full size. I, too, am trying to conserve space and funds, but > decided > that the purchase of a good drill press would be an appropriate use of > both. > Just my two cents... > > Ken > -- Pursuant to US Code, Title 47, Chapter 5, Subchapter II, '227, any and all nonsolicited commercial E-mail sent to this address is subject to a download and archival fee in the amount of $500 US. E-mailing denotes acceptance of these terms. ________________________________________________________________________________
From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com>
Subject: Rear Fuel Tank Baffle
Date: Dec 07, 1999
I did both. I riveted on the rear baffle, put on the wood clamps, and let it sit about 24 hours. I then removed the clamps and screwed it onto the spar and pretty much left it there. -- Scott VanArtsdalen, MCSE Network Administrator Union Safe Deposit Bank 209-946-5116 -----Original Message----- From: RV8DRIVER(at)aol.com [mailto:RV8DRIVER(at)aol.com] Sent: Tuesday, December 07, 1999 2:01 PM To: rv-list(at)matronics.com Subject: Re: RV-List: Rear Fuel Tank Baffle >Hi Listers, I'm thinking about the process of closing up the tank with the rear baffle. I'm building a RV-8 if it matters. I have checked out Sam Buchanan's excellent site, and his method looks good, but there are some conflicts with accounts from other sources. The manual from Van's says the baffle should be sealed first, and then the skin should be countersunk and riveted after the sealant cures. Some posters on the list have suggested using Saran Wrap over the spars and allowing the tank to final cure on the wing to insure a good fit. This would make it impossible to apply the wood clamps as shown on Sam's web page. I know there can be more than one way to do things, but I thought I'd get opinions before doing anything permanent. Thanks in advance, Steve Johnson RV-8 #80121< Steve. I'm also building an -8, and have given the tank construction some thought. With regard to the idea of letting the tank final cure on the spar, I don't believe its necessary if you carefully control the tank skins in the leading edge jig. By this I mean that if you make certain that the top edges of the skins are perfectly parallel to each other, you obviouslycannot have a twist in it and it should fit fine. This can be done with an acccurate bubble level. It won't matter if the tank is level in the long dimension, just that both ends read the same on the level. Of course, if you have a twist in the spar, the tank won't fit. (Just kidding, Heaven forbid!) Andy Johnson ________________________________________________________________________________
From: JDaniel343(at)aol.com
Date: Dec 07, 1999
Subject: Re: fuel fittings: Earl's
What was Earl's web address? ________________________________________________________________________________
From: "Dan Blake" <danblake(at)worldnet.att.net>
Subject: Subaru RV-4 (was HELP! Opinions NEEDED!- Go 4)
Date: Dec 07, 1999
----- Original Message ----- From: Dan Blake <danblake(at)worldnet.att.net> Sent: Tuesday, December 07, 1999 5:46 PM Subject: Re: RV-List: Subaru RV-4 (was HELP! Opinions NEEDED!- Go 4) > Yes, it's Bob Goodwin's (Ex F-15 jock) at Briscoe Gwinnett and a chapter 690 > member. I don't have an email address or pictures, but will ask him if he > minds if I snap a few with the digi the next time I'm out there. > > As far as how it flies, it is pretty much standard RV. My seat-of-the-pants > feel is that the engine is _very_ smooth, and seems powerful. He was > keeping the manifold pressure way down, and still we where blowing by 170 > MPH with my heft on board. I'd like to get the numbers solo, once he gets > it sorted out. The sound is as if there are a couple of more smaller > cylinders, but that may be because it's running at a higher RPM. He has > been developing the turbocharger for it with the help of a guy named turbo > Tom. Tom owns a turbocharger business, building a turbocharged Europa, and > they have been working to get exactly the right size turbo. Bob was > purposely keeping the boost down during this development stage. This is the > second one that he's had installed, and I believe that it's just a hair too > large. I will say that the engine install is very neat and compact, even > with the turbo and liquid cooling hardware. > > I'll snaps some pics, and put them on my web site if Bob doesn't mind. > > Dan Blake > -8 tail > Atlanta > > ----- Original Message ----- > From: Chris Browne <cebrowne(at)earthlink.net> > To: > Sent: Tuesday, December 07, 1999 9:29 AM > Subject: Re: RV-List: HELP! Opinions NEEDED!- Go 4 > > > > Hey Dan, > > > > I think I know the -4 you are talking about. Is it a Briscoe? I've > watched it > > over the last few years and it looked like a real challenge. How does it > fly > > with the Subaru? > > > > Chris Browne > > -6A Atlanta > > > > Dan Blake wrote: > > > > > > > > I got 1.5 hrs. two weekends ago in a guy's Subaru powered -4. He is > about > > > 150, and me 225 in the back. Needed a little nose down trim, but > otherwise > > > flew beautifully. I'll also agree that to my eyes, the -4 is the best > > > > looking RV, but... > > > > > > The -4 is more than a little tight in the back seat for me. My dad is > 6'2", > > > and all of my brothers are over 200. I've flown in the back of an -8 > and > > > a -4, and -8 is much better for the back seater. Although my wife is > small, > > > I want her to be as comfortable as possible. She let me talk her out of > > > a -6, so I need to cut her some slack. Good one her. Showed her > pictures > > > of a -6a, then bought the -8 tail kit. She took it well. We will > x-country > > > quite a bit, too, so the added useful helps with luggage. No QB in > a -4, > > > but I guess that's really not a valid argument for most. > > > > > > RV's - They're all damn wonderful, every one of them. > > > > > > Dan Blake > > > -8 tail > > > Atlanta > > > > > > ----- Original Message ----- > > > From: <JRWillJR(at)aol.com> > > > To: > > > Sent: Monday, December 06, 1999 1:44 AM > > > Subject: RV-List: HELP! Opinions NEEDED!- Go 4 > > > > > > > > > > > I know that I will be flamed unending but I too still think the RV4 is > the > > > > perfect sport aircraft. I liked it when it first came upon the scene > and I > > > > like it no less now. This is not to take away from the 8 or the 6 but > the > > > 4 > > > > is in my opinion the perfect sporting aircraft. Definitely lighter, > > > possibly > > > > stronger, with on center seating, racy canopy and a superb compromise > of > > > > sporting agility with cross country capability. Yes, it has some > > > > negatives---Bubbas on the Van's Bubba Scale beyond 7+ may find the > rather > > > > roomy accommodations slightly lacking compared to the 8 but not really > > > much > > > > less than the 6 as you do not have to share elbow room and then there > is > > > the > > > > unending legend of the tail heavy RV4. Yes, it is true that I at 180 > lbs > > > > probably would not want to shove a 240 pounder into the back seat and > go > > > > zoomering about but fortunately for me all my friends are almost > normal in > > > > size and my dear wife barely makes 120 dripping wet dressed. I am also > of > > > the > > > > opinion and it is just an opinion that aerobatics in any RV should be > kept > > > to > > > > a solo proposition anyway. Yep, I still like the 4 and not looking to > > > build > > > > the RV 12 A. JR, RV4 slowly progressing at less than a snails pace > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Date: Dec 07, 1999
From: "Scott A. Jordan" <SAJ_SLJ(at)compuserve.com>
Subject: Re: Rear Fuel Tank Baffle
Message text written by Stephan: >Some posters on the list have suggested using Saran Wrap over the spars and allowing the tank to final cure on the wing to insure a good fit. This would make it impossible to apply the wood clamps as shown on Sam's web page.< Stephan, If I were to do it again (and who knows, I might some day?) I would let the tanks cure on the wing as others have suggested. When I did my tanks I had too large a pro-seal filet on the baffle / tank skin that had to be pealed off to properly fit the tank on the wing. This made it very difficult and time consuming to put the tanks back on the wing, curing them in this position would eliminate this effort. With the tank tightly secured I don't see where there would be a problem but keep in mind that I have not done this and have no first hand knowledge the lead history of those who have done this If you decide to use the time tested cloths pin method be sure to make only a very small filet, especially inboard where the spar will come up very close to the baffle when the tank is installed. Scott A. Jordan 80331 gear and belly skins ________________________________________________________________________________
From: PANELCUT(at)aol.com
Date: Dec 07, 1999
Subject: Shipping Fuel CAPs
Group I had a real good turn out on the fuel cap offer, alot more than I would have ever guessed. The turn around is a little slower than I hoped because I have to keep them all seperated while I engrave them. I have finished all the RV6 caps and will be starting the RV8's tomorrow I should finish all the rest as well. I did ship a few today, but I will not post any names until tomorrow night. I would like to hear from you when you receive them, and let the list know how they look. I am shipping them all UPS ground so I can have a way to track them if it is required. Again Thank you for your quick response to the UPSIDE DOWN ISSUE, and your business, if I can help anyone with any kind of engraving Just drop me a line. Thanks Steve Davis The Panel Pilot ________________________________________________________________________________
Subject: Re: Rear Fuel Tank Baffle
Date: Dec 07, 1999
From: Carl Froehlich <carlfro(at)erols.com>
Steve, Here is what I did on my 8A tanks (and I'm very happy with the results): - Countersink the skin for the rear baffle. - Apply proseal and rivet (don't wait for the proseal to cure). - Touch up with more proseal along obvious areas. - Cover the wing spar with Saran Wrap and fasten the tank to the wing. - After a day or so (sooner if you have a warm shop), take the tank off (the Saran Wrap come off with the tank). Remove the Saran Wrap, do any clean up if required, cover the spar with new Saran Wrap and reinstall the tank. Repeat as required until the Proseal is fully cured. This last step prevents ending up with the Saran Wrap bonded to the proseal. It won't hurt anything but this is easy to do. If the proseal is allowed to cure without doing the Saran Wrap step you most likely have areas of proseal that interfer with the tank fitting on the wing. These areas will need to be ground away (scotch bright wheel works well). The Saran Wrap trick prior to the proseal curing is a very simple way to make sure your tanks fit exactly right with no additional action required. Carl Froehlich RV-8A (still putting in fuselage nutplates) Vienna, VA >Subject: Re: RV-List: Rear Fuel Tank Baffle >Sent: 12/9/19 8:25 PM >Received: 12/7/99 6:39 PM >From: RV8DRIVER(at)aol.com >Reply-To: RV List, rv-list(at)matronics.com >To: RV List, rv-list(at)matronics.com > > >>Hi Listers, > >I'm thinking about the process of closing up the tank with the rear baffle. >I'm building a RV-8 if it matters. I have checked out Sam Buchanan's >excellent site, and his method looks good, but there are some conflicts with >accounts from other sources. The manual from Van's says the baffle should >be sealed first, and then the skin should be countersunk and riveted after >the sealant cures. Some posters on the list have suggested using Saran Wrap >over the spars and allowing the tank to final cure on the wing to insure a >good fit. This would make it impossible to apply the wood clamps as shown >on Sam's web page. I know there can be more than one way to do things, but >I thought I'd get opinions before doing anything permanent. > >Thanks in advance, > >Steve Johnson >RV-8 #80121< > > >Steve. I'm also building an -8, and have given the tank construction some >thought. With regard to the idea of letting the tank final cure on the spar, >I don't believe its necessary if you carefully control the tank skins in the >leading edge jig. By this I mean that if you make certain that the top edges >of the skins are perfectly parallel to each other, you obviouslycannot >have a >twist in it and it should fit fine. This can be done with an acccurate >bubble >level. It won't matter if the tank is level in the long dimension, just that >both ends read the same on the level. Of course, if you have a twist in the >spar, the tank won't fit. (Just kidding, Heaven forbid!) Andy Johnson > ________________________________________________________________________________
Date: Dec 07, 1999
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Re: Setting Wing Incidence Angle
EARL FORTNER wrote: > > It's all coming togeather now. I thank everyone for their input. I did > not try to run the numbers altho the distance on the stabe was aprox 12 > inches and 26 3/8 inches on the wing. I did raise the rear of the plane > til the bubble center on the wing, then went to the stab and it required > 1/16 inch to get the bubble centered. The angle on longeron as measured > with a Johnson magnetic angle locator is about 1 degree best I can tell. > Think I will let set a day or so and take another look at it. The vert > stab is already attached so don't know how I will handle that yet. But > I assume I will have to realign the hinge bearings. I also signed up > for Source RV last night but have not received a confirmation from them > yet. Will query Vans through them when I can get in if possible. > > Thanks to all, Earl > > Chuck Brietigam wrote: > > > > Earl, you're absolutely correct. The thrust line of the engine will be changed. > > But, I don't believe that this small of a change will be that noticeable--in > > handling or performance. I set my RV-3 up in the manner I described to you. The > > main wing was first locked into position and then the angle of incidence of the > > horizontal stab was established from the main wing. I have an IO-320/constant > > speed up front. I have raced both 180HP/CS RV-4's and RV-6's. They couldn't keep > > up-not even close. I regularly see 230 mph after takeoff. (well above Van's > > stated Vne). > > Again, you're right, the thrust centerline is going to change. To what > > amount--it's hard the say. And like you, I labored very intensely while building > > my airplane to get it as straight as possible. But, I know that my plane is not > > perfect. The smallest change in establishing any one of the corner firewall > > positions will effect the thrustline. I'm not an aeronautical engineer--in fact, > > I'm just a pilot having fun. But, I would think that the drag created when you > > joggle the flaps to met the fuselage is about the same as changing the thrustline > > to accomplish the alignment of the wing/fuselage. Somebody smarter than I will > > have to answer this. It's beyond my understanding/knowledge. But, I can tell you > > of my experience and its success/failure. Talk with Van's. They can either valid > > or disprove my thinking. > > > > PS: I recommend doing the least amount of change to correct any problem. > > Take care, Chuck > > > > EARL FORTNER wrote: > > > > > If this changes the angle at which the fuselage goes through the air > > > what does it do to the thrust line from the engine? > > > > > > Charles Brietigam wrote: > > > > > > > > EARL FORTNER wrote: > > > > > > > > > Thanks to Chuck and all who responded to the flap issue. I now have the > > > > > wings square with no sweep. The bottom skin is flush with the fuselage. > > > > > Per vans instructions for setting incidence on RV4 wing & drawing SK-51 > > > > > I need a block 3 and 3/64 inches to get the bubble in the center of > > > > > level. this puts the wing rear spar 1/4 inch lower than what Van call > > > > > for. I have screwed up too many times already and have had to remove and > > > > > replace the rear spar carry through. I do not want to do it again and > > > > > would like to get the incidence angle right the first time. > > > > > > > > > > My question is about the angle of horizontal stabilizer due to the 1/4 > > > > > inch difference of the wing. Per SK-48 Van shows a 1/4 spacer under > > > > > the level at the rear spar. Would this go to 1/2 inch or decrease to > > > > > 0 inch? Maybe another aproach would be to raise the rear of fuse till > > > > > Van's measurement of 2.8 inches was reached and then set the angle of > > > > > the stab til I get the 1/4 inch called for in SK-48. > > > > > > > > > > Sorry about the length but I am paranoid about drilling the rear spar > > > > > attach. All comments welcome. > > > > > > > > > > Earl, RV4 > > > > > > > > Hey Earl, sounds like you've got this thing nearly whipped. Good work. Now > > > > that you know that the main wing is now down from what Van says is ideal, > > > > all you need to do is to raise the horizontal stab the same angular amount > > > > (Not the measured amount--but angular amount). You stated the main spar was > > > > down 1/4 inch. What is this in degrees??? You can either compute the degree > > > > difference (good old geometry) or measure it. I prefer measuring, if you > > > > hace access to an inclinometer. Once you raise the rear spar to match this > > > > angle, both the main wing and the tail will in the same relative plane as > > > > Van requires. Good luck, Chuck Brietigam ________________________________________________________________________________
From: Kerrjb(at)aol.com
Date: Dec 07, 1999
Subject: Re: Flap Tape
In a message dated 12/7/99 12:50:19 PM Eastern Standard Time, racaldwell(at)hotmail.com writes: << Should the tape go on the flaps or under the top wing skin overhang? >>


December 03, 1999 - December 07, 1999

RV-Archive.digest.vol-hl