RV-Archive.digest.vol-db

June 26, 1997 - July 06, 1997



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Date: Jun 26, 1997
From: "Larry D. Hoatson" <lhoatson(at)e2.empirenet.com>
Subject: Re: Pitot Heat Resistance
> >> The spec sheet for the 12-volt AN5812 I installed this weekend claims 4.5 > >> amps. So, should I size up the wire & breaker for 5 or 10 amps? If you have a Digital Volt/Ohms meter, many of them have a circuit that allows it to act as an ammeter. Mine is good for 10A or less. Hook up the unit to a battery, drawing the current through the meter, and you will know the actual rate for your unit, plus any additional draw at startup. Larry -- Larry D. Hoatson Yucaipa, CA Redlands (L12) Airport lhoatson(at)empirenet.com KC6WYF via packet at: KC6WYF(at)W6JBT.SOCAL.CA.USA.NOAM Restoring 1950 Cessna 170A N9948A... Looking forward to RV-6 ________________________________________________________________________________
Date: Jun 26, 1997
From: Michael Lott <Michael.Lott(at)ssc.nasa.gov>
Subject: Balancing
Are any surfaces more critical than another? thanks ________________________________________________________________________________
Date: Jun 26, 1997
From: Tom Martin <fairlea(at)execulink.com>
Subject: update 2
Well the bad news is in, the camshaft in my RV-4 engine is toast! The engine is being removed from the plane for a complete rebuild, including new valves. Interesting to note that the valve stem ended up falling down throught the fuel controller and was in the air filter air box. Thank you to all who responded. The problem is nothing that money won,t fix,(sigh) If I had to go down I am glad that it was with an engine out and not a bird strike! Tom Martin ________________________________________________________________________________
From: Mlfred(at)aol.com
Date: Jun 26, 1997
Subject: LV light- Bob Nuckolls
Bob: I'm looking at your drawing Z-6, and I can't figure out where the other end of the LV warning light hooks up. Can you bail me (and my customer) out on this one? Check six! Mark ________________________________________________________________________________
Date: Jun 26, 1997
From: spjohnsn(at)ix.netcom.com (Stephen Paul Johnson)
Subject: Snap Bushings
Hi all, I just received my plastic duct for wing wiring from Van's, and wonder if there is a source for snap bushings to protect the duct as it passes through the wing ribs. The OD of the duct is about 0.8" and the largest snap bushings from Van's have an ID of 5/8". Nothing in Wicks or Spruce. Thanks, Steve Johnson RV-8 #80121, left wing ________________________________________________________________________________
From: JDaniel343(at)aol.com
Date: Jun 26, 1997
Subject: Re: ANR - Headsets Inc...
Does any one know if Headsets Inc. adapter will work in the Flightcom Eclipse headset? ________________________________________________________________________________
Date: Jun 26, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: ANR - Headsets Inc...
Doug, So back to the original question, what will this system do to the bass notes from a music source that is sent to the headset? The answer should be that it usually has no effect. Did the owner explain how his system works? Typical active cancellation schemes that I am familiar with rely on taking a sample of the offending signal and inverting its phase to provide a cancelling signal. The desired signal is never considered and never effected unless its frequency matches that of the offending signal. In this case the desired signal may be partially cancelled or it may be enhanced, depending on its phase relationship to the offending and cancelling signals. I should point out that my experience is with rf cancellation, not audio, but principle is the same. So if the Headsets Inc. system doesnt sample the input signal, and strip out the offending signal, what is the source of the cancellation signal that makes the whole thing work? Mike Wills RV-4 (wings) willsm(at)manta.nosc.mil >The Bose does compare the input stream so as to not block it out, The ANR >kit from Headsets Inc. does not, That is what you get for your addition >$850.00. That was from the owner of Headsets Inc. >Tailwinds, >Doug Rozendaal RV-4 N240 >dougr(at)netins.net >http://www.petroblend.com/dougr ________________________________________________________________________________
Date: Jun 26, 1997
From: Phil Arter <philip.arter(at)mci2000.com>
Subject: Re: RV-8 Rudder Skeleton
Scott A. Jordan wrote: > > <71341.3505(at)CompuServe.COM> > > The instructions for building the rudder skeleton says to bolt the > R-405PD > rudder horn in place and slide the R-803 rib in place. The rib does > not have a > slot cut to allow it past the bolt. Simply drilling a hole will be > very close > to the edge so I assume I need to cut a slot. Any suggestions or > limitations I > should know about before I cut this slot? > > Thanks > > Scott A. Jordan > 80331 > N733JJ > Scott, hi I think you must mean the R-404 rib, the R-803 is the one on the top end of the rudder. Anyway, I just cut a slot in mine. Edge distance doesn't apply in this case because the rib flange is sandwiched between the heavy R-405PD and R-606PP. (Oh, and make sure you put that 0.032 spacer in below the rib flange). -- Phil Arter, RV-8 #80005 philip.arter(at)mci2000.com http://acd.ucar.edu/~arter/RV8.html (303)459-0435 home ________________________________________________________________________________
From: "jacquelyn eastburn" <jimnjax(at)worldnet.att.net>
Subject: Re: RV-8 Rudder Skeleton
Date: Jun 26, 1997
Scott. your right. you do need to cut a slot to clear the bolt. a had to ask about this also. ________________________________________________________________________________
Date: Jun 27, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: Brake Wheel Cylinders
Carroll, Both sets of Cleveland brakes and wheels that I've received with my two kits have all had bleeder valves already installed in the side opposite the brake pressure line ports which come with plastic plugs installed. If yours do not have the bleeder valves installed, I would query Van's, if you got them with the kit. Les Williams/RV-6AQ/canopy stuff ---------- From: owner-rv-list(at)matronics.com on behalf of TTC Carroll A. Bird Sent: Thursday, June 26, 1997 6:48 AM Subject: RV-List: Brake Wheel Cylinders This is probably a silly question but my Cleveland wheel cylinders has a little red plug on the bottom side. What do I put in this hole? I think there are fittings which you can use to fill the brake system from the bottom up to the top, which purges the air as it fills. If this is true, where do I get them, and what are they called. Thanks in advance for any info. Carroll, RV-4 on gear. Hanging engine soon. ________________________________________________________________________________
Date: Jun 26, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: Re: balance
What does it mean, "The ailerons are dynamically balanced and need no further balancing." ? ________________________________________________________________________________
Date: Jun 26, 1997
From: Phil Arter <philip.arter(at)mci2000.com>
Subject: Re: aileron balance
BARNES_ERIC(at)tandem.com wrote: > > Jim/Phil, > > Am I correct in that overbalancing is fine as far as safety is > concerned? I thought I read that somewhere... Is there something on > the topic that I can read, in layman's terms? > > EB > Eric, hi Control surfaces are balanced to prevent flutter. When there is a disturbance, the counterbalance mass in front of the hinge line prevents the control surface from defecting on it's own because of its inertia. Otherwise the oscillations can increase in amplitude until something breaks. On the RV-8 the ailerons are overbalanced by a large margin. Even with the electric aileron trim, the left one is still slightly overbalanced. This is not a problem because the ailerons are connected by rigid control tubes, and in a bump the forces cancel each other out (unless it is a very local one affecting only one wing). The elevator is a different situation because if it was overbalanced too much, the pilot would feel it very strongly in the stick. It wouldn't be as dangerous, just very unpleasant - kinda like driving a car with worn out shocks. The elevator needs to be balanced carefully AFTER painting. The rudder on the -8 has a counterbalance also, but it does not totally balance the rudder, it was added along with a larger vertical stabilizer to improve the yaw stability. Anyway, most gusts and thermals act in the vertical direction, also the mass of the feet and legs on the rudder pedals help damp out rudder oscillations. Are you still going to Longmont? -- Phil Arter, RV-8 #80005 philip.arter(at)mci2000.com http://acd.ucar.edu/~arter/RV8.html (303)459-0435 home ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 26, 1997
Subject: Re: Panel tilt and gyros
<< Is the important thing the angle between the panel and the horizon in level flight or is it the difference on the ground (for erection purposes)? >> This is referred to more correctly as the "angle of the dangle"? -GV ________________________________________________________________________________
Date: Jun 27, 1997
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Re: balance
It would be nice to hear an aero engineer comment on this but my memory of a discussion with such was that you don't have to have critical balance. If a control surface is "over-balanced" ie has mass in front of the hinge point this provides protection from flutter. It is better to err on this side of the balance equation and accept the small weight penalty. Open to correction. Leo Davies > >>Both of my elevators are still overbalanced and waiting on the finish >>paint before I put the precision balance on 'em.... > >This was tossed around a while back and I can't get into the archives >(Matt?) to find out what the final word was but as I remember, the ailerons >are dynamically (?) balanced and need no further attention. But, as Mark's >original question asked: what do you do with the ELEVATORS? I have never >seen any description on how the elevators are balanced. Instructions are to >"balance them". It seems hard to get the left to balance accurately with >the trim cable in there. Those who will fly before painting will have to >rebalance their elevators after painting.....but how is it done?? I believe >that is your question, right Mark? > >I hung them on the horizontal and played with the weights until they >were......well......balanced, staying put when moved, neither up nor down. >That left one was the hardest as the resistance of the cable made it more >difficult. I also "over balanced" them forward, waiting until paint to fine >tune them. > >Michael > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
Date: Jun 27, 1997
From: Frank van der Hulst <frankv(at)pec.co.nz>
Subject: Re: Snap Bushings
ix.netcom.com!spjohnsn(at)matronics.com wrote: > Johnson) > > Hi all, > > I just received my plastic duct for wing wiring from Van's, and wonder > > if there is a source for snap bushings to protect the duct as it > passes > through the wing ribs. The OD of the duct is about 0.8" and the > largest snap bushings from Van's have an ID of 5/8". Nothing in Wicks > > or Spruce. Someone suggested to me to get 2 feet of the next size up tubing (in your case, with an I.D. of 0.8"). A half-inch or so of this, attached (but how?) either side of the hole in the rib would support the duct tube. Personally, I don't think this will be necessary. Some RTV to stop the duct moving within the hole in the rib should be enough, I believe. But then, I'm using fairly tough PVC piping. And anyway, what do I know? Frank. ________________________________________________________________________________
From: N45189(at)aol.com
Date: Jun 26, 1997
Subject: tools for sale
Am moving and would like to sell complete set of Avery tools-only used for half of RV tail construction. Perfect for new builder. Please call and leave message @ 413-786-2470. I can fax lists with part numbers and descriptions. Send No E-mail since I won't be on line past Friday 6/27. Thanks ________________________________________________________________________________
Date: Jun 26, 1997
From: Mark LaBoyteaux <tailspin(at)ix.netcom.com>
Subject: Re: Snap Bushings
Stephen Paul Johnson wrote: > > > Hi all, > > I just received my plastic duct for wing wiring from Van's, and wonder > if there is a source for snap bushings to protect the duct as it passes > through the wing ribs. The OD of the duct is about 0.8" and the > largest snap bushings from Van's have an ID of 5/8". Nothing in Wicks > or Spruce. > > Thanks, > > Steve Johnson > RV-8 #80121, left wing > I was just down at the local Ace Hardware store this afternoon, and they had a complete collection of snap bushings. I thought to myself,"Hey, these are just like the ones Van's sent me! and all different sizes!". You might give 'em a try. Mark LaBoyteaux tailspin(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 26, 1997
From: Mark LaBoyteaux <tailspin(at)ix.netcom.com>
Subject: Re: balance
dimensional.com!mikel(at)matronics.com wrote: > > snip > I hung them on the horizontal and played with the weights until they > were......well......balanced, staying put when moved, neither up nor down. > That left one was the hardest as the resistance of the cable made it more > difficult. I also "over balanced" them forward, waiting until paint to fine > tune them. > > Michael Michael, I tried to balance my left elevator with the trim cable installed, but like you, I found that the tension from the cable caused the elevator to want to stay in a neutral position unless I put a lot of weight on the balance arm. So I removed the cable and found that with the weights I bought from Van's installed, the left elevator was just slightly overbalanced. I'm wondering if it will be enough to balance after it's painted. Only time will tell, I figure if it comes up underbalanced I can always mix up an epoxy-lead shot mixture to bring it in. Mark LaBoyteaux tailspin(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 27, 1997
From: Robert Fritz <Qmax1(at)compuserve.com>
Subject: Help near SFO
Hey Rod, I'm an RV-6 builder and I live 15 miles south of SFO and 9 miles from Hayward. I've got a buddy who's built a Starduster Two (fabric and tube)= and is an A&P. I'll ask him if he's interested in your offer. Bob Fritz 415/573-5258 ________________________________________________________________________________
Subject: Re: Snap Bushings
<33B359A3.14E1(at)ix.netcom.com>
From: less_drag(at)juno.com (JAMES E AYERS)
Date: Jun 27, 1997
Hi all, Ace Hardware??? That's were I got the 50 watt 2 inch diameter landing lights. Jim Ayers Less_Drag(at)juno.com writes: >I was just down at the local Ace Hardware store this afternoon, and >they >had a complete collection of snap bushings. I thought to myself,"Hey, >these are just like the ones Van's sent me! and all different sizes!". >You might give 'em a try. > >Mark LaBoyteaux >tailspin(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 26, 1997
From: RodWoodard <rodwoodard(at)mcione.com>
Subject: SFO Help Update-Smith Miniplane
Hello fellow listers: Thanks to all of you who responded to offer suggestions and advice re: my potential purchase of a Smith Miniplane near San Francisco. Thanks especially to Doug Rozendaal who was able to put me in contact with a friend of his who inspected the plane last year. After talking with Doug's friend in Iowa, I found that I'm dealing with a rather dishonest person. Apparently the guy switched a bunch of parts off the plane while Doug's friend was enroute to pick it up, trailer in tow, from Iowa. Not only was the plane not as represented but it was basically stripped down to nothing when Doug's friend arrived. They also found that the upper wing spar was broken. I hear that can be hazardous to one's health.... And I'm not even the surgeon general... Sure is a small world out there. :-) I have a feeling there will be a rather surprised aircraft broker tomorrow morning after I get done telling him what I found out about his little gem. Buyer beware! The search continues... Rod Woodard Loveland, Colorado ________________________________________________________________________________
Date: Jun 27, 1997
From: George McNutt <GMcNutt(at)compuserve.com>
Subject: More on Instrument Panel Tilt and Gyros
Having watched the gyro tilt thread for a few days I looked through my aviation books and could find little on AH gyro tilt. Here is the only paragraph I found in a Aircraft Instrument Systems booklet. (Re: air driven artificial horizon) - "The gyro remains upright with the earths gravity because of the erection mechanism, and in a turn the acceleration force on the pendulum valves gives a false indication of a tilt; so when the airplane rolls out of the turn there will be an indication of pitch--the direction depends on the direction of turn. Most instruments compensate for this by tilting the gyro housing slightly= ". I would assume that on modern instruments this is a internal adjustment o= r mod and if not adjusted for the proper panel angle the AH will have slightly more error when rolling out of a turn. Pitch errors are greatest= during shallow banks and after 180 degrees of a turn. George McNutt 6A Rudder. = ________________________________________________________________________________
From: morristec(at)ICDC.COM
Date: Jun 26, 1997
Subject: update 2
Tom, I don't have your original post but I believe that you mentioned something about a series of runs at 2900 RPM. The typical IO360 has a redline at 2700 RPM (yours). If that was the case consider this. The Helicopter versions of the IO360 are designed to turn up to 3100 RPM. They have special intake and exhaust valves, and they still experience a relatively high failure rate, including CAM failures. Maybe your valves were reused, but I'd bet that 2900 RPM operation may have been a contributing factor. Dan Morris Morristec(at)icdc.com RV>Well the bad news is in, the camshaft in my RV-4 engine is toast! RV>The engine is being removed from the plane for a complete rebuild, including RV>new valves. RV>Interesting to note that the valve stem ended up falling down throught the RV>fuel controller and was in the air filter air box. ________________________________________________________________________________
Date: Jun 27, 1997
From: catbird(at)taylortel.com (TTC Carroll A. Bird)
Subject: Re: Brake Wheel Cylinders
les williams wrote: > > > If yours do not > have the bleeder valves installed, I would query Van's, if you got them with > the kit. > > Les Williams/RV-6AQ/canopy stuff > > Thanks in advance for any info. > > Carroll, RV-4 on gear. Hanging engine soon. > > Thanks to all for the info. There was really not anything wrong. I simply thought that the bleeders was a straight tube fitting . I had the wheel cylinders on upside down . I switched them last night. BTW how do the bleeders work? What sort of a pump or tool do you use to put in the brake fluid. Thanks again. Carroll ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 27, 1997
Subject: Re: Snap Bushings
<< wonder if there is a source for snap bushings to protect the duct as it passes through the wing ribs. The OD of the duct is about 0.8" and the largest snap bushings from Van's have an ID of 5/8". Nothing in Wicks or Spruce. >> These items are maufactured by Heyco and can be had thru most industrial fastener suppliers in your area. I know that Olander in Sunnyvale, CA (check the Yeller Pages for the ph#) carries them in all sizes from 1/8" ID up thru 3" or so. They are dirt cheap. -GV ________________________________________________________________________________
From: "David Moore" <dmoore8(at)tuelectric.com>
Subject: Re: Snap Bushings
Date: Jun 27, 1997
The following question was posed: > I just received my plastic duct for wing wiring from Van's, and wonder > if there is a source for snap bushings to protect the duct as it passes > through the wing ribs. The OD of the duct is about 0.8" and the > largest snap bushings from Van's have an ID of 5/8". Nothing in Wicks > or Spruce. Let's not lose the big picture here. The purpose of the conduit is to protect the wires and provide a little more support than snap bushings alone. You don't need to protect the conduit. ________________________________________________________________________________
Date: Jun 27, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: Re: Panel tilt and gyros
> > > > > >This has been said before but I will say it again as there still > seems > >to be allot of questions on this topic. The ONLY reason you need > >the eight degree tilt is so the little adjustable airplane that moves > up > >and down can be lined up with the horizon line. When you fly in > >level flight and the instrument is tilted this moves your horizon > >indicator line up. > > > I'm getting more and more confused on this topic. Does anyone have an > authoritative source? I had always heard tilt was only needed in > taildraggers. My Pacer has an eight degree tilted artificial horizon > that > works fine. Is the important thing the angle between the panel and > the > horizon in level flight or is it the difference on the ground (for > erection > purposes)? > > Usually there is a real expert on any topic brought up on the list but > I'm > not getting that impression on this one. If someone knows, please > explain. > I don't readily accept unsupported assertions. > > Larry Pardue > Carlsbad, NM > Pacer N8025D > RV-6QME N441LP Fuselage Skins > Well Larry Sorry I'm not a *real* expert and I can understand you not accepting *unsupported assertions* but the attitude indicator can't tell if it is a taildragger or nose gear in the air. The tilt of the panel in the RV-6 in level flight, which in turn tilts the AI, tricks the the gyros into thinking you are in a climb which makes the horizon line read high in level flight, then you have to move the adjustable airplane up to match the horizon bar to indicate level flight. I don't have the 8 degree tilt built into my attitude indicator and have to fly with the little airplane adjusted all of the way to the top, not a problem, just a little inconvenience. BTW I have over 2000 hrs in a Pacer does that make me a *little* bit of a expert at least on Pacers? ---- Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Comm-SEL-MEL-Inst.-CFI jsflyrv(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 27, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Piper pitot
For anyone currently flying with a piper pitot on an RV, did you hook your static system up to the static port on your pitot, or did you use the static port in the side of the fuse as most do, or??? Have you been able to verify accuracy of indicated airspeed? Thanks, Mike Wills RV-4(wings) willsm(at)manta.nosc.mil ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 27, 1997
Subject: Re: LV light- Bob Nuckolls
>I'm looking at your drawing Z-6, and I can't figure out where the other end >of the LV warning light hooks up. Bob: Was there a post on drawings for a low-voltage warning light?? I didn't get it. Please repost if there was one (or send it off-list). Thanks' Michael mikel(at)dimensional.com ________________________________________________________________________________
Date: Jun 27, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Longmont Fly-in
Fellow RVers, It looks like the weather is going to great, so I'm off to the Longmont Fly-in. I hope to meet some "listers", there, and talk RVs. A RV-8 builder offered to put me up for a couple of nights. Thanks, Rod----here come the Nebraska steaks! My RV-6 is white with a yellow "wedge" down the side and a yellow rudder, N369X. Bob Skinner ________________________________________________________________________________
Date: Jun 27, 1997
From: Scott Gesele <scottg(at)icsnet.com>
Subject: Re: Balancing
> >Are any surfaces more critical than another? thanks > > > If I remember correctly from past aero. eng. classes, the elevators are the most critical. Flutter is much more critical in high speed aircraft (ie: high mach). At Embry-Riddle, we were shown a slow motion video of flutter in a wind tunnel. It was an F-16 type tail. The structure oscillated at 10 Hz and had a catastrophic structural failure within three cycle. In other words, the empenage departed the aircraft within 1/3 of a second!!! To err on the side of safety would be to over balance the control surface. That would mean adding lead all the way back in the tail. My elevators are over-balanced now and after paint the additional lead will be drilled out, resulting in a perfectly balanced control surface. Bottom line is we're not building BD-10's. A slight over balance will not hurt anything but the empty weight and CG. I doubt that a slight under balance will really hurt either. Doesn't the RV-3 lack balanced control surfaces and they operate at "typical RV speeds" without encountering flutter. Just my $.02 Scott Gesele N506RV (Just starting to get the hang of this painting thing) ________________________________________________________________________________
Date: Jun 27, 1997
From: spjohnsn(at)ix.netcom.com (Stephen Paul Johnson)
Subject: Re: Snap Bushings
> posted by: "David Moore" > > >Let's not lose the big picture here. The purpose of the conduit is to >protect the wires and provide a little more support than snap bushings >alone. You don't need to protect the conduit. > Thanks for the advice. The more I think about it, the more I think I would like to remove as little metal as possible from the ribs. There isn't much extra there to begin with. If I attach the conduit to the ribs with RTV, there won't be motion between the rib and conduit to cause abrasive wear. Steve Johnson RV-8 #80121 ________________________________________________________________________________
Date: Jun 27, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: RV-6 or 6A Slider specific roll bar brace question???
Hi, I put a lot of work into attaching the stainless steel brace tube with no thought whatever that Van's might have sent one that is too long. Mine will come thru the skin right at the sub panel (the first bulkhead after the firewall) and I am afraid that might interfere with the windshield. Or does the windshield contact skin in front of the sub-panel?? Hal Kempthorne RV-6AQ -- On main gear fitting panel halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
Date: Jun 27, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: Re: Panel tilt and gyros - why not vertical panel?
Hi all, I'm serious here - why not make my panel vertical - zero tilt? I'm fitting it now and last night I tried setting it straight and level and I see no problem. If it is tilted fwd at top, won't I see more sky reflections? Maybe it is so I can keep up the scan & still see the lightning? Hal Kempthorne RV-6AQ -- On main gear halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
Date: Jun 27, 1997
From: n5lp(at)carlsbad.net (Larry Pardue)
Subject: Re: Panel tilt and gyros
> >> > >> > snips >the attitude indicator >can't tell if it is a taildragger or nose gear in the air. The >tilt of the panel in the RV-6 in level flight, which in turn >tilts the AI, tricks the the gyros into thinking you are in a >climb which makes the horizon line read high in level flight, >then you have to move the adjustable airplane up to match the >horizon bar to indicate level flight. I don't have the 8 degree >tilt built into my attitude indicator and have to fly with the >little airplane adjusted all of the way to the top, not a problem, >just a little inconvenience. >BTW I have over 2000 hrs in a Pacer does that make me a *little* >bit of a expert at least on Pacers? >---- Ok, Jerry, I think I'm starting to grasp this. The RV panel is tilted forward with respect to the horizon when in level flight. This means the gyro thinks we are in a "dive" (horizon above the little airplane) so you have to move the little airplane up to make it even with the horizon. I think your statement about the gyro thinking we are in a climb is a misprint. Doesn't matter if taildragger or not. I think having heard that taildragger business years ago is what fouled up my thinking. Our prejudices are hard to ignore sometimes. I'll accept you as an expert, especially on Pacers. The only bad thing about finishing my RV-6 will be having to sell the Pacer. What a nice airplane (as you know, being a Pacer expert). Larry Pardue Carlsbad, NM Pacer N8025D RV-6QME N441LP Fuselage Skins ________________________________________________________________________________
From: "Darrell L. Anderson" <d.l.anderson(at)worldnet.att.net>
Subject: Snap Bushings
Date: Jun 27, 1997
<< wonder if there is a source for snap bushings to protect the duct as it passes through the wing ribs. The OD of the duct is about 0.8" and the largest snap bushings from Van's have an ID of 5/8". Nothing in Wicks or Spruce. >> I think Van's says to just cut all the ribs except the ones on the ends of the duct to the major diameter, and the end ribs to the minor diameter, then snap the ends of the duct into the end holes to anchor them. The convoluted duct takes the place of the snap bushings. There might be some chance of the ribs vibrating and chafing the duct, but a dab of RTV or ProSeal would stop that. I installed mine using a UniBit to cut the holes before the ribs were permanently installed, but they could be cut with the UniBit in an angle drive drill. I used a template to locate the holes in the upper forward corner of the aft ribs where it would clear the aileron pushrod and bellcrank, and not block the aileron access panel. Use a vacuum cleaner to suck a thread through the tube, then pull your wire AND another string through. If you always pull a string with the wire, you will always have a means of pulling another wire through if needed. ...it worked for me. D. Anderson RV-4 (ready to close wings) ________________________________________________________________________________
Date: Jun 27, 1997
From: John Ammeter <ammeterj(at)seanet.com>
Subject: RV Picnic at Arlington Airfair
The Arlington Airfair at Arlington, WA (USA) will be held from July 9 to 13. This airport is the home of the world famous 'Blackjack Squadron'. As most of you know, the Blackjack Squadron is an informal group of local RV flyers that enjoy close formation airwork. They fly RV-4's and RV-6's with a wide range of engines and props. The Puget Sound RVators are again hosting a BBQ picnic on Saturday starting at noon in the RV aircraft parking area. Last year we served over 180 hamburgers and 50 pounds of salmon to well over 150 hungry RV'ers and guests. We also provide much needed shade and lots of lawn chairs along with refreshments to RV'ers during the rest of the Airfair. I have tickets available for our guests at the 'air-arrival' rate. For $10.00 you can purchase a ticket good for all week or, if you're only coming for Saturday, you need only pay $5.00. If you're interested in purchasing these tickets please send me a check (made out to me) at the address below. Include a stamped self-addressed envelope and be certain to indicate what ticket('s) you want. BTW, children 15 and under are free if accompanied by an adult. If you're flying in there is no reason to pre-purchase your tickets; you'll get the same price 'at the gate'. This 'deal' only benefits those who are driving in to the Airfair. Hope to see many of you there. Stop by to talk to me; I'll be the one flipping burgers. John Ammeter ammeterj(at)seanet.com 3233 NE 95th St Seattle WA, 98115 USA 206-525-5445 RV-6 N16JA First flight August 1990 ________________________________________________________________________________
Date: Jun 27, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: Piper pitot
Aa piper pitot on an RV, did you hook your >static system up to the static port on your pitot, or did you use the static >port in the side of the fuse as most do, or??? Have you been able to verify >accuracy of indicated airspeed? >Mike Wills For what it's worth, I had the piper blade on my 6. I used the static port on it. The most accurate readings I could get was within about 2 mph ( using the old AF method of an E6B along with the GPS check), which I thought was pretty close for government work. I mounted it in the same location as Vans called for the original tube. Don't sweat it. John Darby RV6 sold Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: Jun 27, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Re: Panel tilt and gyros - why not vertical panel?
> >Hi all, > >I'm serious here - why not make my panel vertical - zero tilt? > >I'm fitting it now and last night I tried setting it straight and level and I >see no problem. If it is tilted fwd at top, won't I see more sky reflections? >Maybe it is so I can keep up the scan & still see the lightning? Just what I'm wondering, Hal. I won't be fitting for at least a couple weeks (depends on the honey-do list). I was wondering if it had to be aft or lowered a bit forward skin angle. Have a Good Day! Denny RV-6 (R)N641DH Fuselage top side Lebanon, OR ________________________________________________________________________________
Date: Jun 27, 1997
From: Scott Gesele <scottg(at)icsnet.com>
Subject: Paint Guns
Ok, I'm breaking a carnal rule and am wearing a flame retardant shirt, but can someone recommend a good NON HVLP spray gun and a place where it can be purchased from. I understand that Binks makes quality equipment and would like to find a mail order house that carries it or an equivalent. I've been attempting to paint the exterior with various HVLP guns and am getting orange peel and runs. Tonight I touched up a primed area (always have to sand the primer due to orange peel) with a non HVLP gun and the finish was smooth as silk. I've wrestled with the HVLP long enough, it's time to finish this thing. I'll admit it, the HVLP beat me and it's time to go with what I'm comfortable with. The entire inside was primed and the cockpit painted with a conventional gun with very good results. Any help on a locating a gun that will do a good job on the exterior will be appreciated. Thanks in advance. Scott Gesele N506RV (Will I ever finish painting this plane?) ________________________________________________________________________________
From: GHLX34A(at)prodigy.com (MR GEORGE T KILISHEK)
Date: Jun 27, 1997
Subject: RV-8 Wing Kit Bulkhead
Eric Barnes wrote, quite correctly: Shortlisters: An FYI note regarding the instructions for the RV-8 kit-- The instructions call for beginning your wing by assembling the fuselage bulkhead where the wings attach. I dutifully began that process, only to stop short when I couldn't find the specified .040" sheet stock from which to make the shim. A call to Van's solved the problem. I was told that the .040" material is supplied with the fuselage kit. He advised me to "forget what the plans say" and just build my wings! So, when you get your wing kit, forget everything about building the bulkhead first, and start with the rear spar. I hope this saves somebody some frustration. --Don McNamara #80113 On the other hand, I plunged ahead with mine, fabricating the shims from double thicknesses of .020" scrap. Worked fine. After I did that, I found two pieces of .040" stock cut to the correct size in one of the envelopes. Now ready for the shims on the bulkhead of my second RV-8. BFirst bulkhead is done, in the attic and waiting. I'll be able to use it in a year or two. George RV-8 #80006 Left wing fuel tank. ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: Smart Pro Level Instructions
Date: Jun 27, 1997
I have misplaced my instruction book for my Smart Pro Level. I would appreciate if someone would send me a private message with the 8-step sequence for the "super" calibration. I would also appreciate the 800 number of the manufacturer so I can call to get another instruction book. I am trying to measure the gear leg symmetry right/left and am not sure I have the gadget calibrated properly. I don't have this calibration problem with my bubble level! Danged digital devices! Thanks. Dennis drilling gear mounts for 6A using false spar method ________________________________________________________________________________
Subject: Fwd: Tools for sale
Date: Jun 27, 1997
From: HARRY PAINE <HPair(at)thegrid.net>
-- [ From: HARRY PAINE * EMC.Ver #2.5.02 ] -- ------- FORWARD, Original message follows ------- From: HARRY PAINE \ Internet: (hpair(at)thegrid.net) ------ TOOL LIST FOR SALE Harry Paine 477 printz rd Arroyo Grande Cal 93420 805-481-2524 90% angle drills 1/4 28 thread rebuilt--rockwell------- -----------225.00* 45% angle drills 1/4 28 thread rebuilt -rockwell ---- ----------- 225.00* * Flush Rivet set with rubber guard extra wide 1 1/4 " wide much nicer than Averys. This is the best I've even seen while they last $10.00 # 8 nut plate jig .............................................. ..........12.00 15 mil thick 3M Alum sound damping tape (used on 767) 9" wide not available anywhere else other than 3M Sold by linear foot minimum 10' order 1.00/ln. ft. All Items tools guaranteed 30 days or your money back. Items sold and shipped UPS COD Cash or certified check. ** Limited Availability sold on a first come first serve basis. Email Harry Paine @ Hpair(at)thegrid.net call 805-481-2524 & leave message ------- ________________________________________________________________________________
Date: Jun 27, 1997
From: John Ammeter <ammeterj(at)seanet.com>
Subject: Re: Paint Guns
I painted a motorcycle with a Craftsman air spray gun. Turned out fine. I also sprayed the inside of my RV with Imron paint with that same gun; had a few runs but I think that, with practice, I could have mastered the gun and done a good job. FWIW, John > >Ok, I'm breaking a carnal rule and am wearing a flame retardant shirt, but >can someone recommend a good NON HVLP spray gun and a place where it can be >purchased from. I understand that Binks makes quality equipment and would >like to find a mail order house that carries it or an equivalent. > >I've been attempting to paint the exterior with various HVLP guns and am >getting orange peel and runs. Tonight I touched up a primed area (always >have to sand the primer due to orange peel) with a non HVLP gun and the >finish was smooth as silk. I've wrestled with the HVLP long enough, it's >time to finish this thing. I'll admit it, the HVLP beat me and it's time to >go with what I'm comfortable with. The entire inside was primed and the >cockpit painted with a conventional gun with very good results. Any help on >a locating a gun that will do a good job on the exterior will be appreciated. > >Thanks in advance. > >Scott Gesele N506RV (Will I ever finish painting this plane?) > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
From: LesDrag(at)aol.com
Date: Jun 28, 1997
Subject: Re: Balancing
<< (Snip) Doesn't the RV-3 lack balanced control surfaces and they operate at "typical RV speeds" without encountering flutter. Just my $.02 Scott Gesele N506RV >> Hi All, The RV-3 has balanced ailerons, but neither the elevator or rudder are balanced. It also has a 210 mph Vne. Jim Ayers LesDrag(at)aol.com ________________________________________________________________________________
Date: Jun 27, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: Re: Panel tilt and gyros
Larry Pardue wrote: > **snip** > I think your statement about the gyro thinking we > are in a climb is a misprint. > I'll accept you as an expert, especially on Pacers. The only bad > thing about finishing my RV-6 will be having to sell the Pacer. What a nice > airplane (as you know, being a Pacer expert). > > Larry Pardue > Carlsbad, NM > Pacer N8025D > RV-6QME N441LP Fuselage Skins > You are right Larry I should have said in a dive instead of in a climb. I know what you mean about having to selling your Pacer I loved flying that airplane I had a lot of fun with it before selling it to build my RV-6. -- Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR jsflyrv(at)ix.netcom.com ________________________________________________________________________________
From: LesDrag(at)aol.com
Date: Jun 28, 1997
Subject: Re: Brake Wheel Cylinders
<< BTW how do the bleeders work? What sort of a pump or tool do you use to put in the brake fluid. Thanks again. Carroll >> Hi Carroll and all, I use a pump oil can with a piece of hobby shop fuel line. I fill the brake reservoir from the brake cylinder. Of course I planned it this way, I ran a 1/16" vent line out of each reservoir (mounted on the master cylinder on the rudder pedals). When the reservoir is full, it vents onto a strategically placed rag on the hangar floor. I have a pressure vent for the fuel tanks, a static vent for the brake reservoirs, and a static vent for the three-in-one case; all in a 2" long 1" tall CNC machined NACA 64-012 aluminum airfoil on the centerline of the fuselage. Jim Ayers LesDrag(at)aol.com ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 27, 1997
Subject: Re: Longmont Fly-in
>It looks like the weather is going to great, so I'm off to the Longmont >Fly-in. I hope to meet some "listers", there, and talk RVs. The Yellow RV-8 is going to be there. It spent the night at the TriCounty airport (near Denver) and I was able to get some unobstructed photos (hard to do at a fly-in). MAN, is the workmanship on that NICE. When I saw it in the air, I knew it was an RV-something, but couldn't tell what until it was closer. I'll never get used to that straight main gear. Nice airplane. (I secretly like the looks of an RV-4 better, but then, that's what I HAVE.) Hope a lot of RVs are going to be there. Michael ________________________________________________________________________________
Date: Jun 27, 1997
From: mauser(at)claris.com (Richard Chandler)
Subject: Re: Paint Guns
I've always wondered, what is the real difference in conventional and HVLP paint guns. I mean, it's been pretty well described what they do, but what is the practical difference in the way the paint gets from the end of the gun to the surface being painted? Both blow a fine mist of paint at what you're painting, so why is one so much different than the other? -- Richard Chandler RV-6: Garage bought and being finished, saving for tools and tail kit. ________________________________________________________________________________
Date: Jun 28, 1997
From: Ronald Vandervort <rvanderv(at)linknet.kitsap.lib.wa.us>
Subject: Re: Sliding Canopy Frame
I had good luck bending the forward part to match the roll-bar profile. The sides now need bowing out about 1/8th inch each side. I am concerned that even placing each end of the sides in a jig may not keep the forward piece from rolling forward during the bowing process. What experience have you veterens had with the "bow the sides out " bend. I will appreciate any input from ye who have been there and done that. Thank You, Ron Vandervort, RV-6Q rvanderv(at)linknet.kitsap.lib.wa Seattle area ________________________________________________________________________________
Date: Jun 28, 1997
From: Blake Harral <bharral(at)mindspring.com>
Subject: Re: Alternator modifications
<33B0B80A.1D05(at)ix.netcom.com> <19970625.081108.12567.2.wstucklen1(at)juno.com> Frederic W Stucklen wrote: > > > Tim & listers, > > Try modifying a Nippon Alternator. It's a very simple process.... > > Fred Stucklen RV-6A N925RV > wstucklen1(at)juno.com > > I'm doing just that. I bought a rebuilt alternator from an popular chain of auto parts stores. The first unit I bought, I returned because I was not happy with the way the bearings felt. I had the same problem with the exchange unit, so I took it to a local shop specializing in alternator/starter rebuilds. They install new OEM Nippondenso bearings. They also offered to help me with removal of the internal regulator, but wanted to know if the external regulator I was using was a type A or B (their terms). I think this has to do with whether the regulator is in the hot side or the ground side of the field circuit. Can anyone tell me about the adjustable requlator that Van's sells? Is there a schematic supplied with this that would show if it could be termed a type A or type B regulator? I was hoping to find some answers before picking up the alternator early next week. I have taken apart several of the small ND alternators, and have been quite impressed (disclaimer: I'm an EE but with no particular expertise in Motors/Alternators). The one I bought was for Geo Metro/Storm. I get conflicting numbers for its output, but all are in the 55-65 amp range. My cheapie fish scale says it weighs a little less than 8 lbs. It has a 15mm shaft - this is the right size to accept the 4 in dia. aluminum pulley that Aircraft Spruce sells. I haven't yet decided about overvoltage protection - My main reason for wanting to use the external regulator is to allow me to adjust the output voltage to the optimum value for whatever battery type I decide to install. I would be interested in a schematic for simple, cheap OV protection. ________________________________________________________________________________
From: kevin lane <n3773(at)worldnet.att.net>
Subject: Re: Panel tilt and gyros - why not vertical panel?
Date: Jun 28, 1997
> >> >>Hi all, >> >>I'm serious here - why not make my panel vertical - zero tilt? >> >>I'm fitting it now and last night I tried setting it straight and level and I >>see no problem when Brian fitted his gyro he ran into problems because of their depth, the subpanel and the hinge mechanism. He ended up tilting his even more to fix this but wouldn't recommend it. A vertical panel will generate less usable volume behind it since the forward top skin angles downward. kevin 6A-on mains ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@norway-c.it.earthlink.net>
Date: Jun 28, 1997
Subject: Re: RV-6 or 6A Slider specific roll bar brace question?
> Mine will come thru the skin right at the sub panel (the first bulkhead after > the firewall) and I am afraid that might interfere with the windshield. Or does > the windshield contact skin in front of the sub-panel?? Hal, My roll bar goes thru the skin right at the sub panel as well. Canopy fits just fine, misses the roll bar no problem. Tim (canopy done!) --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@norway-c.it.earthlink.net>
Date: Jun 28, 1997
Subject: Re: Paint Guns
> I've been attempting to paint the exterior with various HVLP guns and am > getting orange peel and runs. Tonight I touched up a primed area (always > have to sand the primer due to orange peel) with a non HVLP gun and the > finish was smooth as silk. I've wrestled with the HVLP long enough, it's > time to finish this thing. I'll admit it, the HVLP beat me and it's time to > go with what I'm comfortable with. The entire inside was primed and the > cockpit painted with a conventional gun with very good results. Any help on > a locating a gun that will do a good job on the exterior will be appreciated. I'd be interested in knowing what paint you're using. I got the impression from some of the old archives (1994ish) that System III didn't work well with the HVLP guns that folks were using. I've gotta buy a gun pretty soon, so I'll follow this discussion with interest. Tim --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@norway-c.it.earthlink.net>
Date: Jun 28, 1997
Subject: Re: Sliding Canopy Frame
> I had good luck bending the forward part to match the roll-bar profile. > The sides now need bowing out about 1/8th inch each side. I am concerned > that even placing each end of the sides in a jig may not keep the forward > piece from rolling forward during the bowing process. > > What experience have you veterens had with the "bow the sides out " bend. My bending techniques (ideas borrowed from the list, Scott @ Van's fabrication shop and my grandfather the farmer): To correct "whopper jawed" frame (frame crooked w.r.t. the roll bar) tape the frame to the roll bar, pull the rear with all your might. To correct frame mismatch with fuselage profile place some blocks on the floor, lay the frame on the blocks, and step on the frame between the blocks. Bounce up and down as required to get the desired bow. To raise and lower the back of the frame w.r.t. the front the best bet is to slightly tilt the roll bar. If, like me, you have already riveted the stainless steel support structure in place before you realize this, you can bend the frame a bit with a homemade tube bender made from blocks of wood bolted to a 4' 2"x4". It does a little bit of good. For aft frame width adjustments I just put the frame on the floor and pulled/pushed the aft bow as requried. This tends to change the width of the front bow, so a lot of trial and error is involved. I took the advice of a lister who recommended making the frame a little narrow (still fits in the tracks, but hugs the inside), because the plexi will pull the frame out a tad, resulting in the desired width in the tracks. This reduces friction between the rollers and the track, making the canopy slide easier. Good Luck Tim --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
Date: Jun 28, 1997
From: Bob Moore <bobmoore(at)wwd.net>
Subject: Re: RV Picnic at Arlington Airfair
John Ammeter wrote: > The Arlington Airfair at Arlington, WA (USA) will be held from July 9 to 13. > This airport is the home of the world famous 'Blackjack Squadron'. As most > of you know, the Blackjack Squadron is an informal group of local RV flyers > that enjoy close formation airwork. I didn't know that! I thought that the "Blackjack Squadron" was the US Navy Patrol Squadron Twenty- One in which I served from 1959 to 1962. Probably had quite a few more pilots than the RV group you are reffering to. :-) Bob Moore ________________________________________________________________________________
Date: Jun 28, 1997
From: Finn Lassen <finnlass(at)ix.netcom.com>
Subject: Pitot line - plastic or alu?
Searching through the archive I see some mention of using Tygon for the pitot line. Has anyone experienced adverse effects of using plastic instead of alu? Finn ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: 6A Gear Leg Mounting
Date: Jun 28, 1997
For those of you facing gear mount drilling on a 6A, I offer the following experiences. I was initially apprehensive about the 6A gear mounts because when I tried to measure them it was apparent that they were not exactly left-right mirror symmetrical. Now that I have them clamped for drilling I am really impressed with the fit of these complicated parts! I fashioned a false spar from marine plywood and then faced it with 0.025 skin because it was 0.015 too thin. That left me 0.010 oversize. However since winter the plywood swelled to 0.025 oversize due to humidity. My longitudinal holes along the longeron will therefore be shifted 0.025 forward. I will drill them small (maybe #30 or 3/16) for now and final drill them when the actual wings are inserted. The measurements below were made with a Smart Level Pro and were repeatable to the same value or at most 0.1 degree difference on successive measurements. Thus leg angles would measure 45.5 degrees on 4 out of 5 attempts and 45.6 on the non-agreeing measurement. The "leg angle" is the angle measured with the level resting unsupported along the leg. It is a measure of symmetry. I tried to get the legs perfectly level but finally gave up and accepted the 0.2 degree tilt. This will cause one wheel to be about 1/4 inch lower than the other over a 86 inch tread width. The legs didn't seem to go where I thought they would when I made adjustments, and after about five attempts I concluded that 0.2 degrees was as level as I could get things without some very complicated shimming. Measurement on my clamped gear mount geometry per SK-63. Parameter Measured Value Spec Levelness 0.2 degree right side low Level Right leg angle 45.5 degrees N/A Left leg angle 44.7 degrees Spacer-gage right 25/32 inch 23/32 - 24/32 Spacer-gage left 25/32 inch 23/32 - 24/32 Toe-in right 3/32 inch 2/32 Toe-in left 3/32 2/32 Alignment angle right 8.3 degrees 7-8 degrees Alignment angle left 7.3 degrees 7-8 degrees Shims were required: 0.032 against right spar; 0.063 on left forward pad. Dennis 6A fuselage in jig ________________________________________________________________________________
Subject: Re: RV6 VFR or IFR
<19970626.093234.12567.1.wstucklen1(at)juno.com>
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: Jun 28, 1997
On Thu, 26 Jun 1997 Frederic W Stucklen writes: >Glenn, > > You should check the archive for past discussions on this topic. In >short, the RV-6 is NOT a Bonanza or C-182 stability-wise. You >definitely >have to "fly" the plane all the time. Glenn, The RV series are fine IFR airplanes. They handle wonderfully both in and out of the clouds. The airplane, of course, neither knows nor cares whether it is in IMC. I find Mr. Stucklen's comment a bit puzzling. Of course one must fly the airplane all the time. What else do you intend to do in the cockpit? >Most people find that a wing >leveler is a "must have" in an RV-6 for IFR operation. I disagree on the matter of a wing leveler. It adds unnecessary weight and complexity to a light and simple airplane. I have quite a bit of IFR time in the T-37 as a former Air Force instructor pilot. I also have cloud time in the T-38, C-182, C-172, C-150, and Citabria. I find that the civilian airplanes are actually less demanding on instruments, because they fly at slower speeds. Every deviation takes so much longer to develop that corrections are easier. My total flying time on any form of autopilot is precisely zero. It is simply unnecessary. There are many tasks that I don't mind automating in the cockpit. Engine management, cowl flap operation, nav waypoint sequencing, radio tuning by GPS database, are all acceptable areas for automation. There is one task, however, that I will not delegate to a machine under any circumstances, and particularly not under extreme circumstances: flying the airplane. That is my job. An autopilot has two glaring flaws in my opinion. First, it is stupid. It can never think as well as the pilot can when handling unexpected problems. Read about the ATR commuter crashes as an illustration. Second, it does not care about preserving the pilot's soft, fleshly body. The autopilot will quite willingly smack you into the terrain. Whatever task you feel requires the aid of an autopilot is almost certainly LESS important than flying the airplane. Fumbling with charts and flipping approach plate pages can be minimized by pre-flight preparation. If you find yourself so task-saturated that you cannot adequately fly the airplane, it is time to re-prioritize your tasks. FLYING the AIRPLANE must always come first. Tell ATC to stand by, if necessary. One final note: In the T-37, the instructor pilot sits on the right side, but must fly by reference to the instruments on the left side. After a couple thousand hours doing that, my RV-4 instrument layout looks WONDERFUL. Blue skies, Tom Craig-Stearman tcraig-stearman(at)juno.com ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 28, 1997
Subject: Re: Longmont Fly-in
>>It looks like the weather is going to great, so I'm off to the Longmont >>Fly-in. I hope to meet some "listers", there, and talk RVs. >The Yellow RV-8 is going to be there. Nice airplane. >Hope a lot of RVs are going to be there. Weather was GREAT (hot) and a bunch of local and non-local RV's showed. Lozza folks around the RV-8 and Tom was yacking a'plenty and selling hats, T-shirts, and maybe a few RV-8's. Strickland and Barnards airplanes were there from out of town (and others I probably missed). Nice work, guys. It will take me some time to get used to round intakes on an RV cowling but very nice installation. David had the top cowel off to show off the cooling plenum (is that what it's called?). And wing tips that go UP!! Ryan's airplane looks better every time I see it. Good fly-in. Next year: better. And MAN were there a lot of folks at Ryan's feed. (Thanks again, Ryan.) Michael ________________________________________________________________________________
From: REEVES322(at)aol.com
Date: Jun 28, 1997
Subject: Re: Brake Wheel Cylinders
I use a simple oil squirt can. and some plastic tubing to fit the end of the squirt nozzel and the bleeder value.. ________________________________________________________________________________
From: rust47rg(at)one.net
Date: Jun 28, 1997
Subject: Re: RV6 VFR or IFR
Craig-Stearman) > >On Thu, 26 Jun 1997 Frederic W Stucklen writes: >>Glenn, >> >> You should check the archive for past discussions on this topic. In >>short, the RV-6 is NOT a Bonanza or C-182 stability-wise. You >>definitely >>have to "fly" the plane all the time. > >Glenn, >The RV series are fine IFR airplanes. They handle wonderfully both in >and out of the clouds. The airplane, of course, neither knows nor cares >whether it is in IMC. I find Mr. Stucklen's comment a bit puzzling. Of >course one must fly the airplane all the time. What else do you intend >to do in the cockpit? > >>Most people find that a wing >>leveler is a "must have" in an RV-6 for IFR operation. > >I disagree on the matter of a wing leveler. It adds unnecessary weight >and complexity to a light and simple airplane. > >I have quite a bit of IFR time in the T-37 as a former Air Force >instructor pilot. I also have cloud time in the T-38, C-182, C-172, >C-150, and Citabria. I find that the civilian airplanes are actually >less demanding on instruments, because they fly at slower speeds. Every >deviation takes so much longer to develop that corrections are easier. >My total flying time on any form of autopilot is precisely zero. It is >simply unnecessary. There are many tasks that I don't mind automating in >the cockpit. Engine management, cowl flap operation, nav waypoint >sequencing, radio tuning by GPS database, are all acceptable areas for >automation. There is one task, however, that I will not delegate to a >machine under any circumstances, and particularly not under extreme >circumstances: flying the airplane. That is my job. An autopilot has >two glaring flaws in my opinion. First, it is stupid. It can never >think as well as the pilot can when handling unexpected problems. Read >about the ATR commuter crashes as an illustration. Second, it does not >care about preserving the pilot's soft, fleshly body. The autopilot will >quite willingly smack you into the terrain. Whatever task you feel >requires the aid of an autopilot is almost certainly LESS important than >flying the airplane. Fumbling with charts and flipping approach plate >pages can be minimized by pre-flight preparation. If you find yourself >so task-saturated that you cannot adequately fly the airplane, it is time >to re-prioritize your tasks. FLYING the AIRPLANE must always come first. > Tell ATC to stand by, if necessary. > >One final note: In the T-37, the instructor pilot sits on the right >side, but must fly by reference to the instruments on the left side. >After a couple thousand hours doing that, my RV-4 instrument layout looks >WONDERFUL. >Blue skies, >Tom Craig-Stearman >tcraig-stearman(at)juno.com > Mr: Craig-Stearman I couldn't agree less with your feelings re. autopilots. The A/P is a tool to make your job easier, installed properly, used properly,(Don't fly in heavy ice in an ATR with the A/P on) it is a way to make your single pilot IFR experience easier. I can, and do, fly my 4 just fine on the guages. However when the unexpected wind shift occurs on an approach and I have to switch plates or whatever while being vectored around, it's nice to be able to flip the A/P switch while I do it. Thats the point. The RV IS sensitive and I like it that way, but having to interrupt your scan to do other things does happen and it's nice to have the A/P. PERIOD. I don't really care how much T-37,T-38,C-182,C-172,C-150 time you have, how much single pilot RV time do you have in actual? I have found Mr Strucklen's posts to be valid observations from someone that has a fair amount of RV IFR time and I tend to agree with him. I consider the A/P in my RV-4 a nice tool worth it's weight. I fly IFR in numerous aircraft from my 4 and light twins to "smokers" and find your distaste for A/P use narrowminded at the least. You will find coupled approachs required procedure in certain circumstances in the airlines. Did you ever fly a CAT 3 approach? Kind of hard to do without the box. Now obviously we're not going to fly coupled low approachs, but there are times the A/P comes in handy in my RV. IMHO it's a wise choice in an IFR RV. If you want to do it without one , go for it.....but don't hammer those of us that choose to use the available technology. Regards: Rusty Gossard N47RG RV-4 Flying since 8-94 and sometimes IMC with the A/P on...... ________________________________________________________________________________
Date: Jun 28, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: balancing
Why are the rv-3 surfaces not balanced, but the rv-4's have to be? Also, I am getting a lot of matronics type trash at the end of every message. Is any one else? ________________________________________________________________________________
Date: Jun 28, 1997
From: Al Mojzisik <prober(at)iwaynet.net>
Subject: Re: balancing
>Also, I am getting a lot of matronics type trash at the end of every >message. Is any one else? Michael, With all do respect, if it weren't for Matronics there wouldn't be an RV list! I think we can refer to our hosts company as something other than "Trash". I am sure Matt put that there because so many listers were obviously not reading the FAQ sheet and didn't know how to unsubscribe and thought he would plug his website at the some time. I see nothing wrong with that. Al ________________________________________________________________________________
Date: Jun 28, 1997
From: "Gregory S. Brewsaugh" <gregbrew(at)gte.net>
Subject: Oops HS-610
Hello all, While drilling the #40 pilot holes along the centerline of my HS-610, I somehow managed to drill one of the 6 5/8" holes at 6" instead. At this position, the rivet will interfere with the HS-404 and HS-405. (Using a '426' rivet would only solve half the problem.) An empty hole at this location would be 3/8" from the future 404/405 hole at 5 5/8", and 3/8" from the proper 6 3/8" hole. As I've "finished" fabricating the HS-610 (by hand), I'd really rather not do it again. Would an "extra" hole at this location compromise the HS-610? How many of you would fabricate another HS-610? Help!! TIA. Greg Brewsaugh Learning a lot with the empennage. (Finished the HS rear and VS spars.) ________________________________________________________________________________
Date: Jun 28, 1997
From: "Ray Murphy, Jr." <murphy(at)mail.coos.or.us>
Subject: Re: balancing
> > >>Also, I am getting a lot of matronics type trash at the end of every >>message. Is any one else? > > >Michael, >With all do respect, if it weren't for Matronics there wouldn't be an RV >list! I think we can refer to our hosts company as something other than >"Trash". >I am sure Matt put that there because so many listers were obviously not >reading the FAQ sheet and didn't know how to unsubscribe and thought he >would plug his website at the some time. I see nothing wrong with that. Al > > >I wholeheartedly agree with Al!! I'm not sure who posted the original message but it was probably one of those that use the list without sending Matt any money for its operation. > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > Ray and Nancy Murphy murphy(at)mail.coos.or.us RV6A empenage ________________________________________________________________________________
Date: Jun 28, 1997
From: William Costello <bcos(at)ix.netcom.com>
Subject: Matronics trash ?????
Hi Folks, An individual stated that he is getting some Matronics 'trash' at the end of his messages now. That 'trash' is a brief message from the organization that supports this list (all 800 plus of us) free of charge except for donations some of us choose to give. The primary reason for the message is that a number of people who get on and off the list never bother to read the instructions and request Matt Dralle to personally remove them from the list when all it takes is a very simple email. I, for one, am happy to see the brief bit of 'trash' at the end since it makes Matt's job a little less tedious. Let's quit biting the hand that feeds us, please, and continue to use this list as the fantastic RV builder's info source that it is. Best regards, Bill Costello If you want to flame me, please do so directly. bcos(at)ix.netcom.com -- Bill Costello | bcos(at)ix.netcom.com | Building RV-6 | Reserv N97WC Want an extra hour and a half of energy per day with Super Blue Green products? Email for info or call 800-325-7544 Chicago ________________________________________________________________________________
Date: Jun 28, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: Pitot line - plastic or alu?
Has anyone experienced adverse effects of using plastic >instead of alu? > Finn; I had no problem with the plastic. It was installed in Feb 94 and still working when I recently sold it. No sweat. John Darby RV6 sold Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: Jun 28, 1997
From: Robert Fritz <Qmax1(at)compuserve.com>
Subject: Matronics trash ?????
RIGHT ON! and a pox on the poltroons who cast flames upon thy head. Bob Fritz ________________________________________________________________________________
Date: Jun 28, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Wanted to buy: RV-4
There is an RV-4 at Twin Oaks Airpark (near Portland OR) that is for sale. It had a new O-360 installed just before the owner ground looped it and lost confidence in his conventional gear skills. The plane is wanting a new owner. I believe all repairs were made. This plane was owned by a retired doctor (non-builder) and was repaired by an A&P. For more details, call Bob Stark (the A&P) @503-628-2817. > >Looking to buy an RV-4. Would like an 0-360 powered RV but will consider >any. Day/Night VFR between $35,000 - $45,000. JMJN01(at)AOL.Com > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
Date: Jun 28, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: balance
Don't check them. Just use it the way it is. Van does not expect them to be any more balanced than the pipe offers. We get special spec pipe to achieve the correct balance ;-) Bill > >And on the same subject ... > >I know that my RV-6 ailerons have a heavy water pipe in the nose to >balance them. I don't know how to make sure that the pipe alone is >heavy enough or too heavy. Does anyone in RV land have any advise on >how to check the aileron balance? > >Steve >Huntington, Vermont > > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
Date: Jun 28, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Wire Runs
How much do the tips move relative to the fuselage? The tips deflect about 6" at 9g before the spar fails. But let me tell you, you would not believe how deformed the skins are before you reach that point. Yet, when you unload the spar prior to failure, the wrinkles all come out. Aluminum is strange stuff. Bill > >us.oracle.com!SSPRUELL(at)matronics.com wrote: > >> I found some very thin-wall PVC at Home Depot which I am using. It is >> 7/8" >> OD and ~3/4" ID, but weighs less than 1/2" SCH 40. I used a Unibit to >> >> drill a 7/8" hole about 1.5" down from the top main rib flange and >> about >> 2.5" back from the spar. > >I'm doing the same, except I'll put my PVC pipe in front of the main >spar. I'll make up a couple of little brackets to hold it between the >spar and tank. This was recommended to me by Bill Benedict. It >apparently helps solve some wire routing issues in the cockpit. > >> I'm using a dab of RTV at each rib to secure the pipe. > >Are you worried about the pipe chafing on the rib, particularly since >the wing is likely to move a little relative to the pipe? Maybe some >little gussets (someone suggested PVC of a slightly larger diameter) or >is this overkill? I'm thinking of aerobatics, and maybe the difference >between the fuselage hanging off the wings in flight and the wings >hanging off the fuselage on the ground. How much do the tips move up and >down? > >Frank. > > > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
Date: Jun 28, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: cabin air
> >I think that it would be enlightening to place the extra altimeter's port >outside the back of the canopy. If you look at a sampling of T-18's, the most >common fresh air port is: (pause for effect) the trailing edge of the canopy. >It is NOT an exit point. >I'll bet the canopy trailing edge is at a relatively high pressure. >Bill, has Van's measured this? > >Charlie (england(at)vicksburg.com) Not that I am aware of. However, Van has commented that it is a high pressure area where the air going over and around the canopy recombines. Bill Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
Date: Jun 28, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: balance
Do the instructions instruct you to balance the ailerons? I don't think so! The ailerons were not meant to be balanced other than the balance provided by the pipe. Van's words were he was trying to achieve about a 70% balance. Don't ask how to measure this, just build them, paint them and fly them. It ain't broke so lets not try to fix it. Bill > >The trailing edge is level with the nose on both of my unpainted >ailerons. Should I add lead to the water pipe? > >Steve >Huntington, Vermont > > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
From: MarkVN(at)aol.com
Date: Jun 28, 1997
Subject: Re: IO540
Iam looking for an I0540, either C4B5 or D4B5 ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 28, 1997
Subject: Re: Paint Guns
<< Ok, I'm breaking a carnal rule and am wearing a flame retardant shirt >> Yeah, there's alot of that going on in San Francisco too. Sounds kinky and a little unnatural but at least you have something on while you're doing it. -GV ________________________________________________________________________________
Date: Jun 28, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: aileron balance & gap seal (not)
I asked Van about the balance on the ailerons. He did not seem to get hot about people wanting to balance their aileron, but indicated there was not much to be gained. The one thing he did caution on, was not to use weight to balance a heavy wing. Evidently, a local RV-3 buyer/flyer was performing some maintenance on his RV-3 and found lead in the counter-balance pipe. I don't remember the exact amount, but it was around 10 lbs. It appears the plane had a heavy wing when built and the builder elected to add weight to the leading edge of the light wings aileron, thus forcing the light aileron to force the wing down. This could easily have led to flutter of the aileron if the RV wing was not as stiff as it is. I think our advice would be to not static balance the ailerons, just build to the plans. If you add weight, you are changing the acceleration of the roll rate. The one most noticeable thing about the -8 (in my opinion) is the roll accelerates a noticeable amount faster than the -4 or -6. The only thing I can attribute this to is the spar in the -8 is lighter than the others (but it is still a 9g spar and has been demonstrated in static load tests), thus there is less mass to accelerate. Once the roll is established, it rolls at the same rate because the ailerons and their placement from the centerline will primarily determine the roll rate. I also asked about the aileron and gap seals. His comment about this was the aileron is a slotted aileron design. Gap seals are used on ailerons that hinge like the flaps. The slotted aileron design is depending on air flowing from the high pressure side (bottom) of the wing up through the slot and down the top of the aileron to maintain flow attachment on aileron deflection. This gives the aileron more effect at high displacement angles (ie; it does not stall as easily). A good example of detached airflow is to put tufts on the flap and go fly. With the flaps down, as you decelerate into a stall the tufts will dance all over the flap, and even turn around and head forward. If this was the aileron, you would not have much control under these conditions. Once again, we would recommend that you build the ailerons and all the control surfaces as called out in the plans. One person questioned why the elevators on the -3 were not balanced. I did not pose this question but will in the future. Does anyone know if the P-51 has counter-balanced elevators? To date, there has not been a failure that can be attributed to flutter on any of the RV's. So, if it ain't broke, don't fix it! Bill Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
From: kevin lane <n3773(at)worldnet.att.net>
Subject: Re: 6A Gear Leg Mounting
Date: Jun 29, 1997
> >For those of you facing gear mount drilling on a 6A, I offer the following >experiences......... Brian and I both have our 6A's on main gear now. We drilled our sockets to the wing spar/splicer plate back before the fuses were built. I just propped up the wings, trailing edge up, level in the basement, clamped the sockets with legs in place and carefully measured the required distances. I pilot drilled the holes initially using some brass tubing model RR'rs build with and enlarged them later to avoid damaging the existing spar holes. The "hole" thing only took an hour once it was set up. I can't imagine drilling them on the plane as suggested. It took several evenings just to put all the bolts in. I drilled the side fuse bolts after the wings were bolted on. It's always scary to install a major part that was built a year ago(when the project was even foggier!) but the sockets fit, dead on. I will also suggest you think long before riveting the floor pan ahead of the spar in. I waited as long as possible. The productivity between sitting on the floor vs. laying on your side/stomach/back inside the cockpit and working must be 10:1. I've also discovered that by leaving the tanks off the wings you can easily reach into the cockpit to retrieve tools etc... Just wanted to let people know there are many ways to approach the problem. I like how someone even built the push tubes and control stick mechanism with just the wings together. I can't think that far ahead. Next time, right? kevin 6A - running out of bolts, finally ________________________________________________________________________________
Subject: Re: balancing
From: less_drag(at)juno.com (JAMES E AYERS)
Date: Jun 29, 1997
Hi All, This is just my opinion, The RV-4 empennage is very much bigger than the RV-3 empennage. The RV-3 C.G. range is from 18 to 27 percent, while the RV-4 C.G. range is from 15 to 30 percent. The larger H.S. and elevator allow the greater forward C.G. range on the RV-4. But the bigger (heavier) control surface makes it more critical for flutter problems. Therefore, the RV-4 elevator is balanced. Jim Ayers Less_Drag(at)juno.com (Michael C. Lott) writes: > >Why are the rv-3 surfaces not balanced, but the rv-4's have to be? >Also, I am getting a lot of matronics type trash at the end of every >message. Is any one else? ________________________________________________________________________________
Date: Jun 29, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: Balancing and matronics trash
Okay, all you guys that are so quick to flame somebody for asking an innocent question, you deserve a pat on the head and a doggy bone for being so loyal to your master. Now, stop barking and go to sleep. I didn't know what that was that was showing up on my mail all of a sudden. It looked like a bunch of symbols with a couple of intelligible lines mixed in. That kind of stuff I call trash. I know recently other people have had times where a lot of "extra" stuff came along with their mail, and it was fixed after someone said something about it. I simply though it might be one of those occasions, so I asked about it. EXUSE me for calling it trash. I DIDN'T mean anything personal by it. That's a common term for something like that, or at least, what I though it was. I have a lot of respect for what Matt does with this list and the things I learn from most of the people on it. Don't spoil it for me. If you had spent as much thought answering my question about balance, well, never mind. I apologize to the regular people on this list for having to read this. It will never happen again. ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: Jun 29, 1997
Subject: Rocky Mountain Regional Fly In
The Longmont flyin had a heck of a turn out today. Many RV's in attendance flying in from California to Texas and I might of even heard someone tell me they came from Tennessee. The new RV-8 was in attendance with Tom Green at the helm. Rummor had it that Bill B brought it up friday but we soon found out thats what it was a rummor. We had the second annual barbque again this year and fed well over 100 people, a good time was had by all. No one left hungry. Vans should be proud to have a dedicated employee such as Tom. We did every thing we could to pry him away from his post long enough to get some lunch and he woulnt budge. (people were sent to relieve him and he still wouldnt budge.) His lunch was finally delivered to him and I think he was happy. To all who missed out we hope to see you next year. Ryan B P.S. Kept checking six Mark you were never in sight. ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: Jun 29, 1997
Subject: Les Rowles
Les, Please give me your Email address. I have a package for you and need to know what you want me to do with it. Ryan ________________________________________________________________________________
Date: Jun 29, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: Re: Matronics trash
Michael C. Lott wrote: > > > Why are the rv-3 surfaces not balanced, but the rv-4's have to be? > Also, I am getting a lot of matronics type trash at the end of every > message. Is any one else? > Michael Matt at Matronics has probably done more single handily to help builders by providing this list than any other means available. I for one feel that Matt has every right to add anything he wants at the end of each message that goes through Matronics. He provides this list free for all RV builders and wannabe builders I hope he makes a bundle of money by advertising his products here. BTW I will plug one of his products he provides and that is the FuelScan I use it and it is a very fine instrument, after using it I wouldn't leave home without it. On another subject someone said they would not use a autopilot in a RV, here again is another tool that makes flying easier especially if you are in unfamiliar territory and are reading maps. RVer's You do use your map don't and don't depend entirely on a Loran or GPS. :-) Jerry -- Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR jsflyrv(at)ix.netcom.com ________________________________________________________________________________
Date: Jun 29, 1997
From: "W. Tom Glover" <tglovebox(at)bc.sympatico.ca>
Subject: Re: ANR - Headsets Inc...
aol.com!JDaniel343(at)matronics.com wrote: > > > Does any one know if Headsets Inc. adapter will work in the Flightcom Eclipse > headset? > >According to my Headsets Inc. documentation, the ANR adapters DO NOT fit the Flightcom Eclipse. Sorry to be bearer of bad news. Tom Glover ________________________________________________________________________________
Date: Jun 29, 1997
From: "W. Tom Glover" <tglovebox(at)bc.sympatico.ca>
Subject: Re: ANR - Headsets Inc...
Mike Wills wrote: > > > > So if the Headsets Inc. system doesnt sample the input signal, and strip > out the offending signal, what is the source of the cancellation signal that > makes the whole thing work? > > Mike Wills > RV-4 (wings) > willsm(at)manta.nosc.mil > > > >The Bose does compare the input stream so as to not block it out, The ANR > >kit from Headsets Inc. does not, That is what you get for your addition > >$850.00. That was from the owner of Headsets Inc. > > >Tailwinds, > >Doug Rozendaal RV-4 N240 > >dougr(at)netins.net > >http://www.petroblend.com/dougr > >Mike, the Headsets Inc ANR adapters have electret microphones in the earcup that pick up the offending low-frequency racket. The signal is amplified, phase-shifted and output to the second miniature speaker in the earcup. The circuitry is proprietary (I asked), but is very simple. There's just not a lot of parts on the board! 73 Tom Glover ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: balance
Date: Jun 29, 1997
Hi Bill, Thanks for answering my question about balancing the ailerons. Steve Soule Huntington, Vermont -----Original Message----- From: Bill Benedict [SMTP:europa.com!billb(at)matronics.com] Sent: Saturday, June 28, 1997 10:56 PM To: rv-list(at)matronics.com Subject: RE: RV-List: balance Do the instructions instruct you to balance the ailerons? I don't think so! The ailerons were not meant to be balanced other than the balance provided by the pipe. Van's words were he was trying to achieve about a 70% balance. Don't ask how to measure this, just build them, paint them and fly them. It ain't broke so lets not try to fix it. Bill ________________________________________________________________________________
Date: Jun 29, 1997
From: Rick and Barbara Osgood <randbosgood(at)SprintMail.com>
Subject: Gall Strobe light Power Supply
Has anyone used any of the Gall Strobe light Power Supplies to run there strobes?? I am interested in this option but would like to hear from others who may have done the same. Thanks in advance. -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com ________________________________________________________________________________
From: "Austin Tinckler" <tinckler(at)axionet.com>
Subject: Wood props
Date: Jun 29, 1997
Just curious as to what make of wood prop people have used; cost thereof and satisfaction level of prop. Diameter and pitch and engine used would be very interesting. Any response from listers would be very appreciated.. Thanks, Austin RV-6..paint soon. ________________________________________________________________________________
Date: Jun 29, 1997
From: Glenn & Judi <flyers@anet-chi.com>
Subject: RV6 F-644
Hi, I am ready to cut out the two F-644's as per DWG 30. Vans has provided one 14" piece of channel for these parts. 14" would allow for two 7" pieces to be cut, however the plans call for a bend at the end of each F-644, so the 14" piece is too short. Should the overall lenth of the F-644 be shortened? Or how should this be handled? Thanks in advance, Glenn Gordon ________________________________________________________________________________
Date: Jun 29, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: Gall Strobe light Power Supply
Never heard of them. Where did you see info on them? Les Williams/RV-6AQ #60027 ---------- From: owner-rv-list(at)matronics.com on behalf of Rick and Barbara Osgood Sent: Sunday, June 29, 1997 7:31 AM Subject: RV-List: Gall Strobe light Power Supply Has anyone used any of the Gall Strobe light Power Supplies to run there strobes?? I am interested in this option but would like to hear from others who may have done the same. Thanks in advance. -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jun 29, 1997
Subject: Re: Airflow Injection system/etc.
While at the Longmont Fly-in (quite the show) a fellow RVer who is banging together an RV-4 said he had some promlems fitting the Airflow Injection system under the RV-4 coweling. Apparently the orientation of one of the fittings interfered with the "cheek" and he had to add a 4 inch fuel line after turning the fitting around to get it to fit under the coweling without adding a blister on the cowel. He said it probably wouldn't have been a problem on the -6 or -8. Any of you -4 folks running the Airflow system? This builder is not on the list (then HOW has he gotten his airplane together?) ;>` I'll pass on any hints. By the way, Ted Strickland expressed his jealousy for the Colorado builders support and, as good as the support around here is, THE LIST is an instant, multi-source/opinion, guide to builders that NO other resourse could come close to matching. There are questions/answers I have found here that I didn't even know were questions yet until someone brought them up!! Thanks, guys/gals!! Michael ________________________________________________________________________________
Date: Jun 29, 1997
From: "les williams" <lesliebwilliams(at)msn.com>
Subject: RV6 F-644
Glenn, I asked about this not long ago and Tom, at Van's, stated that his plane and others didn't have the flange and the concensus there was to eliminate the depiction of the flange from the drawing. Afterwards, I mentioned that it is shown in several other drawings and pictures but haven't gotten any other response. I just sent another note mentioning this along with some other things. Will post when/if I get a definitive answer. ---------- From: owner-rv-list(at)matronics.com on behalf of Glenn & Judi Sent: Sunday, June 29, 1997 10:09 AM Subject: RV-List: RV6 F-644 Hi, I am ready to cut out the two F-644's as per DWG 30. Vans has provided one 14" piece of channel for these parts. 14" would allow for two 7" pieces to be cut, however the plans call for a bend at the end of each F-644, so the 14" piece is too short. Should the overall lenth of the F-644 be shortened? Or how should this be handled? Thanks in advance, Glenn Gordon ________________________________________________________________________________
Date: Jun 29, 1997
From: Steve Colwell <colwell(at)innercite.com>
Subject: Re: Brake Wheel Cylinders
aol.com!REEVES322(at)matronics.com wrote: > > > I use a simple oil squirt can. and some plastic tubing to fit the end of the > squirt nozzel and the bleeder value.. > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ The hot combination for brake bleeding is a pressure pot (Pump Sprayer $10 to $15 at Garden Shops) with a reducer and clear plastic hose to attach to the bleeder valve at the wheel cylinder. Just be sure to pull the brake pedals back all the way so the master cyl. valves are open. Hook up an overflow at the reservoir and its a one man operation. This is the only way to force enough volume of fluid to push the air bubbles trapped in the high spots. Steve Colwell RV6 flyer-Lancair 360 builder ________________________________________________________________________________
From: "Tim Lewis" <timrv6a@germany-c.it.earthlink.net>
Date: Jun 29, 1997
Subject: Moving a partially complete RV-6A
In a few months I'm probably going to have to move from San Antonio TX to Washington D.C. (Pentagon assignment). I'm building a quickbuild, and wondering about the best, safest way to move it. I've already completed about everything except the instrument panel and engine/cowling. I've already installed the left and right steps, so I can't just lay the fuselage flat on the floor like it was when Van shipped it to me. By the time I'm ready to move, I'll likely have the engine mounted and the gear attached. Can the aircraft tolerate a long trip in a U-Haul on the gear, or should I remove the engine and gear, and build a support structure that supports the fuselage along it's entire length? Thanks for your experience. Tim --------------------- Tim Lewis RV-6AQ #60023 San Antonio TX timrv6a(at)earthlink.net or timrv6a(at)iname.com ----------------------- ________________________________________________________________________________
Date: Jun 30, 1997
From: Frank van der Hulst <frankv(at)pec.co.nz>
Subject: Re: Gall Strobe light Power Supply
SprintMail.com!randbosgood(at)matronics.com wrote: > Has anyone used any of the Gall Strobe light Power Supplies to run > there > strobes?? I am interested in this option but would like to hear from > others who may have done the same. I haven't heard of them. I'm looking into strobes (%-|) at the moment, trying to decide what to buy. I'd appreciate it if you could tell us a little about how these Gall Strobes vary from Whelan and the rest? Frank. ________________________________________________________________________________
Date: Jun 30, 1997
From: Frank van der Hulst <frankv(at)pec.co.nz>
Subject: Empire Development Avionics
Hi All, Has anyone dealt with Empire? They have a Web page at http://users.aol.com/chanik/ed/kk.htm -- amongst other things they advertise a pair of capacitance fuel senders for US$120. I've tried emailing to the address given on the page (chanik(at)aol.com) 3 times so far, with nil response. Frank. ________________________________________________________________________________
Date: Jun 30, 1997
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Re: RV-6 or 6A Slider specific roll bar brace
question??? Hal, The location of the front (knife blade portion) of the roll bar brace is called out on the plans. You then trim the top (tube portion) as required to achieve a 90 degree angle between the roll bar and the canopy decks/top longeron. I cannot quite visualise what you have done but if the attach point of the brace is too far forward you just need to extend the slot rearward as necessary. You may be left with a skin blemish that needs some microballoons later. It it really upsets you there is always the "new forward top skin option". Leo Davies Spending money like water (this last bit is expensive isn't it?) leo(at)icn.su.oz.au > >Hi, > >I put a lot of work into attaching the stainless steel brace tube with no >thought whatever that Van's might have sent one that is too long. > >Mine will come thru the skin right at the sub panel (the first bulkhead after >the firewall) and I am afraid that might interfere with the windshield. Or does >the windshield contact skin in front of the sub-panel?? > > >Hal Kempthorne RV-6AQ -- On main gear fitting panel >halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
Date: Jun 30, 1997
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Re: Paint Guns
> >Ok, I'm breaking a carnal rule..... Scott, I can't resist. I hope you are breaking a cardinal rule, breaking carnal rules will get you nasty infectious diseases. Leo ________________________________________________________________________________
Date: Jun 30, 1997
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: balance
> >Don't check them. Just use it the way it is. Van does not expect them to >be any more balanced than the pipe offers. We get special spec pipe to >achieve the correct balance ;-) Bill > Ummm Bill, I hope that is a grin at the end of that message. The Australian dummy cut his water pipe too short (measure twice cut once...yeahh I know Dad). He then went down to Luigi Brothers Plumbing and Tax Avoidance and bought bog standard water pipe of the same diameter. Tell me youre not using some oddball pipe, rebuilding ailerons at this stage would be reaaally depressing. Leo Leo Davies leo(at)icn.su.oz.au ________________________________________________________________________________
Date: Jun 29, 1997
From: Rick and Barbara Osgood <randbosgood(at)SprintMail.com>
Subject: Re: Gall Strobe light Power Supply
les williams wrote: > > > Never heard of them. Where did you see info on them? > > Les Williams/RV-6AQ #60027 Another person on the list mentioned them as an alternative source to Wheelen. They are one of the major sources for law enforecment vehicles. The unit mentioned cost $44.95, flashes 3 times per minute and can handle 6 heads. -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com ________________________________________________________________________________
Date: Jun 30, 1997
From: Frank van der Hulst <frankv(at)pec.co.nz>
Subject: Re: Paint Guns
Scott Gesele >Ok, I'm breaking a carnal rule..... > I can't resist. Me either. I *did* try. > I hope you are breaking a cardinal rule, breaking carnal rules will > get you > nasty infectious diseases. C'mon guys. Let's talk RVs. Carnal rules relating to RVs are: 1. Don't join the Mile-High Club in an RV-4. 2. Don't even think about joining it in an RV-3. 3. If you're interested in carnal stuff, allow more than 5 years to build an RV. Frank (aiming to have his RV built in less than 5 years :-) ________________________________________________________________________________
Date: Jun 29, 1997
From: "Scott A. Jordan" <SAJ_SLJ(at)compuserve.com>
Subject: Oops HS-610
>>While drilling the #40 pilot holes along the centerline of my HS-610, I= somehow managed to drill one of the 6 5/8" holes at 6" instead. At this position, the rivet will interfere with the HS-404 and HS-405. (Using a '426' rivet would only solve half the problem.) An empty hole at this location would be 3/8" from the future 404/405 hole at 5 5/8", and 3/8" from the proper 6 3/8" hole. As I've "finished" fabricating the HS-610 (by hand), I'd really rather not do it again. Would an "extra" hole at this location compromise the HS-610? How many of you would fabricate another HS-610? << Greg, I made a "couple" similar type errors on my -8 HS front spar, including a= n error on the HS-810. My answer was "it is to early in the project to say= 'good enough'". I made a new 810, although the 810 is probably less work= than your 610 since the "ears" are already cut. One of the nice things about RV's is that parts are cheap! I keep telling myself that the FAA allows home building as an educational experience. If we learn by our mistakes I am on track for the most educational "five years" of my life! Don't take this as a "holier than thou" attitude! I have learned to say "that's acceptable". I was drilling out a lot of rivets until an IA frie= nd came to inspect my HS and VS spars. He told me my rivets were as good as= Challenger and Gulfstreem rivets when I thought they were only marginal i= f they were not picture perfect. Of course, I still hold myself to as high= a standard as practical, especially on visable structures. When I had an "extra" hole my IA said it wouldn't hurt anything if I had proper clearances for the other rivets. When I asked if I should fill th= e hole with a rivet, he said no, to consider it a lightning hole. = I think on many "errors" you must ask yourself what standard you want to accept. I want an airplane whose structure is not up for question. I wa= nt as nice an airplane as I can reasonably build (I'm obviously a first time= r) and don't expect to wil major awards at Oshkosh. As a first time builder= I think I could build a very good AND an excellent airplane in the same amount of time and money it would take to produce an award winner since I= would have to do everything at least twice! Right now I want a solid airplane, maybe the next one I'll try for an awa= rd winner! Scott ________________________________________________________________________________
Date: Jun 30, 1997
From: Kam Yuk CHENG <kamy(at)cyllene.uwa.edu.au>
Subject: crack in the W606A Spar Web
Hi everyone, We are building a RV-6A in the Mechanical Eng. Dept. of the University of Western Australia. This is a final year project where a group of students construct the airframe and conduct aerodynamic and structural design analysis on the airframe. Being a student project, it starts and stops because they have their course work. when a group gets good at what they are doing, the students, being in their last year, would get a job, typically with a mining or oil & gas engineering companies in Western Australia. So new group would start from scratch and get familiar with the construction techniques before they work on RV-6A. So we are progressing fairly slowly. We have completed the tail section. At the moment, a group of 4 stduents are working on the main spar section of the wing and they made a first boo ! While drilling out an unsatisfactory rivet on the W606A spar web, they made a 1/16 inch crack on the shot head side of the web. The riviet is the first one from the bulk head end ( first spreader bar). As far as I can see, the purpose of this rivet is to secure the spar web to the spreader bar. The spreader bar should be taking up all the stress and not the spar web. I am requestiong some suggestions the best way to remedy this situation. We cannot put a larger counter sunk rivet because we cannot access the spreader bar since the rest of the main spar has been rivetted. Is it quite o.k. to clean up the crack (after cleaning up the crack, the hole would be a bit too big for the rivet) and put a small piece of thin plate on the shot head side to prevent the rivet pulling through the hole. Any suggestion would be well appreciated. Very best regards Kamy Cheng Mech. Eng. Dept. University of Western Australia ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jun 29, 1997
Subject: Re: Sliding Canopy Skirt Cap (Crass Commercialism)
For those of you who have sent in your $10 to me for your very own genuine hydraulic press formed (under 2 tons, count 'em, two) RV-6/6A sliding canopy skirt cap (accept no substitutes), they are in the mail as of 06/28/97. I have an initial run of fifty, so the rest of you, don't be shy. Operators are standing by. Don't embarass yourself, your friends and/or your family by topping off the slider with some cobby looking piece of caca. Cough up 2 fins (U.S., includes domestic shipping) and get the best. This is the last shameless solicitation I will post. -Gary VanRemortel vanremog(at)aol.com ________________________________________________________________________________
Date: Jun 27, 1997
Subject: Re: failure update
From: ebundy(at)juno.com (Ed Bundy)
>The intake valve failed in the #4 jug. The valve fell into the >cylinder and bashed the top of the piston and destroyed the head > >At this stage I am looking for advise. >I am going to remove all jugs to inspect/repair/replace as necessary >The sump and induction system will be taken apart and cleaned. There >are some valve pieces unaccounted for. They may have gone out the exhaust >to determine the cause of the failure. Can the remaining valves be >tested for serviceability? Wow. Thanks for sharing this info. If I remember correctly, this was a recent O/H, yes? Do you have any idea how old the cylinder assemblies are? An intake valve failure is extremely rare, and it makes me wonder how old they might be. Intake valves aren't normally replaced during an overhaul. If it were me, I don't think I'd sleep very well at night if I didn't replace all of the cylinder assemblies with new. Ed Bundy RV6A - first flight 11/20/96 ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
Date: Jun 30, 1997
From: Frank van der Hulst <frankv(at)pec.co.nz>
Subject: Re: Oops HS-610
compuserve.com!SAJ_SLJ(at)matronics.com wrote: > I made a "couple" similar type errors on my -8 HS front spar, > including an > error on the HS-810. My answer was "it is to early in the project to > say > 'good enough'". I made a new 810, although the 810 is probably less > work > than your 610 since the "ears" are already cut. I made a new 610. The old one became pratice ear-cutting parts! > Don't take this as a "holier than thou" attitude! I have learned to > say > "that's acceptable". I was drilling out a lot of rivets until an IA > friend > came to inspect my HS and VS spars. He told me my rivets were as good > as > Challenger and Gulfstreem rivets when I thought they were only > marginal if > they were not picture perfect. Of course, I still hold myself to as > high a > standard as practical, especially on visable structures. Agreed. The other thing to consider is that 'fixing' something will *inevitably* mean that something else gets damaged a little. For example, drilling out a rivet will open out the rivet hole a little. In which case, you've got to look at it and say "Is the likely damage going to be worse than the existing fault?" If it is, then don't 'fix' it! Also, try to figure out what you did wrong first time before you fix it. No point in drilling out a bad rivet, damaging the hole a little removing it, then driving it again badly. I find a lot of my mistakes happen after 9:30pm, and a fair amount of those happen after 10pm when trying to fix the first mistake. I've learnt to STOP WORK when I start making mistakes. Frank. ________________________________________________________________________________
Date: Jun 29, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: Re: Moving a partially complete RV-6A
Just curious Tim, are you building this rv for the C.I.A.? You don't have to answer that if it's a secret. ________________________________________________________________________________
From: GHLX34A(at)prodigy.com (MR GEORGE T KILISHEK)
Date: Jun 29, 1997
Subject: RE: Oops HS-610
Greg: Re: whether to accept the HS-610 with an extra 3/8" hole, my two cents worth is: "Don't." One of a the bits of wisdom about building an aluminum container to which you'll someday entrust the life of someone you care about is: "Good enough probably isn't." I remade this particular part once, and many builders I know have done the same. Consider it part of the educational process and/or think of it as getting twice as much fun for your money. George RV-8 #80006 wings. "... Would an "extra" hole at this location compromise the HS-610? How many of you would fabricate another HS-610? Help!! TIA. Greg Brewsaugh Learning a lot with the empennage. (Finished the HS rear and VS spars.)" ________________________________________________________________________________
Date: Jun 29, 1997
From: "Bryon T. Maynard" <bmaynard(at)communique.net>
Subject: Re: Moving a partially complete RV-6A
Tim Lewis wrote: > > > In a few months I'm probably going to have to move from San Antonio > TX to Washington D.C. (Pentagon assignment). I'm building a > quickbuild, and wondering about the best, safest way to move it. > I've already completed about everything except the instrument panel > and engine/cowling. > > I've already installed the left and right steps, so I can't just lay > the fuselage flat on the floor like it was when Van shipped it to me. > > By the time I'm ready to move, I'll likely have the engine mounted > and the gear attached. Can the aircraft tolerate a long trip in a > U-Haul on the gear, or should I remove the engine and gear, and build > a support structure that supports the fuselage along it's entire > length? > > Thanks for your experience. > > Tim > --------------------- > Tim Lewis > RV-6AQ #60023 > San Antonio TX > timrv6a(at)earthlink.net or > timrv6a(at)iname.com > ----------------------- > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ I just moved from Florida to Louisiana with my RV-6A. The trip in the U-Haul was uneventful. Just make sure nothing is vibrating in it or against it. Bryon ________________________________________________________________________________
Date: Jun 29, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Re: Wood props
>Just curious as to what make of wood prop people have used; cost thereof >and satisfaction level of prop. Diameter and pitch and engine used would be >very interesting. >Austin Austin, Several prop makers that I've heard good things about: Warnke (slow to deliver, sometimes), Performance Props, Aymar-Demuth (sp?), Prince and I used a Props Inc, that I liked pretty good (although I've since switched to a Sensenich, fixed pitch.) Prices range from around $500-900. I think most RVers use around a 68" diameter. Prop pitch is hard to pin down as different prop makers measure pitch at different locations. You should be able to tell a prop maker what kind of plane you have, what the horsepower engine and what you want out of the prop and he should be able to come pretty close. Performance Props ship their props without the leading edge strip and final finish for a preleminary test in case re-work needs to be done. When the prop is performing to suit the pilot, you send it back and they finsih the prop. A friend recently went through this and was very satisfied with Performance props. I sent my Props Inc. back for "re-pitch" several times and was not charged for the re-work and was satisfied with the work that Jeff did. Warnke makes a good prop but doesn't seem to get re-work done in a timely manner. Bob Skinner RV-6 BSkinner(at)navix.net ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: Jun 29, 1997
Subject: Re: Airflow Injection system/etc.
Mike, The builder you were referring to is Stewart Bergner. He's a good freind and quite a craftsman. The problem he was having was installing the purge valve the way it was recomended. He remedied the situation by remote mounting it somewhere else. He isnt on the list but he has a good connection ;). Ryan ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: Jun 30, 1997
Subject: Re: Moving a partially complete RV-6A
Tim, I have now made 3 trips from Idaho to colorado in a Ryder truck transporting 3 different airplanes. The trucks were 24' horizontal stab must be removed, wings tied to the wood rails on the sides, and fueselage sits in the middle. Pieces of 2x4 can be nailed or screwed to the wood flooring around the landing gear to keep the fueselage from moving. Ailerons, Flaps, Rudder,& Elevators can be wraped in protective material and placed in boxes or a left over crate and placed under the fueselage. In 3 trips we have had no damage. The job would be much easier with the engine off of the airplane and their would be plenty of room left over in the truck for it. Good Luck Ryan ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Jun 30, 1997
Subject: Re: RV List Cheap HVLP
Have one of the little Camp. Haus. units and am happy with it when I used it to paint my KFOX. Works great with the thin Polyfiber materials and dope but suspect it would not shoot heavier bodied paints with the desired results. They (C.H.) make a pro model for a little more money. Has a higer working pressure and flow rating. Have seen them at Home Depot. Maybe take a look see. JRW. ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Jun 30, 1997
Subject: Re: Dirt dobbers ? Help!
I saw a posting here about a device that would keep the little devils out of my hanger. Was it some type of electronic device? Where do you get them and are there any other suggestions on stopping the pests. Feel free to e-mail me at JRWillJR. Thanks. RV-4 2280. ________________________________________________________________________________
From: bennett(at)zip.com.au
Date: Jun 30, 1997
Subject: Improved Trim Control Handle
I've never been happy with the look or feel of the aileron mechanical trim control handle (6/6A). A far better solution (IMHO) is to substitute the chintzy steel handle with a C656 sliding canopy latch handle. It provides more side area to apply pressure against the friction, it's milled to size and fits perfectly, and it looks far less, well, agricultural. Peter Bennett Sydney Australia RV6 building sliding canopy ________________________________________________________________________________
From: "mcomeaux" <mcomeaux(at)cmc.net>
Subject: Re: Moving a partially complete RV-6A
Date: Jun 30, 1997
Spend alot of time preparing to support the craft. A few years ago Budwieser had a Model 4 Kitfox built and designed to manage floats they were transporting it to lakeland Florida and when "their" truck arrived the craft was pretty badly damaged. The bouncing ride in the truck which is very rigid is something it normally would not experience. ---------- > From: Bryon T. Maynard <communique.net!bmaynard(at)matronics.com> > To: rv-list(at)matronics.com > Subject: Re: RV-List: Moving a partially complete RV-6A > Date: Sunday, June 29, 1997 8:42 PM > > > Tim Lewis wrote: > > <timrv6a@germany-c.it.earthlink.net> > > > > In a few months I'm probably going to have to move from San Antonio > > TX to Washington D.C. (Pentagon assignment). I'm building a > > quickbuild, and wondering about the best, safest way to move it. > > I've already completed about everything except the instrument panel > > and engine/cowling. > > > > I've already installed the left and right steps, so I can't just lay > > the fuselage flat on the floor like it was when Van shipped it to me. > > > > By the time I'm ready to move, I'll likely have the engine mounted > > and the gear attached. Can the aircraft tolerate a long trip in a > > U-Haul on the gear, or should I remove the engine and gear, and build > > a support structure that supports the fuselage along it's entire > > length? > > > > Thanks for your experience. > > > > Tim > > --------------------- > > Tim Lewis > > RV-6AQ #60023 > > San Antonio TX > > timrv6a(at)earthlink.net or > > timrv6a(at)iname.com > > ----------------------- > > > > +-- --+ > > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > > | --- | > > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > > +-- --+ > I just moved from Florida to Louisiana with my RV-6A. The trip in the > U-Haul was uneventful. Just make sure nothing is vibrating in it or > against it. > > Bryon > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ ________________________________________________________________________________
Subject: Re: 6A Gear Leg Mounting
From: wstucklen1(at)juno.com (Frederic W Stucklen)
Date: Jun 30, 1997
Kevin, What a great idea! Definately going to do that on the next one. And the "next one" has been started! I picked up a tail & wing kit (Phlogistin spar) from a guy who couldn't finish it. This one is going to be a Chevy powered VFR -6a...... Fred Stucklen RV-6A N925RV wstucklen1(at)juno.com writes: > > >> >>For those of you facing gear mount drilling on a 6A, I offer the >following >>experiences......... > >Brian and I both have our 6A's on main gear now. We drilled our >sockets to the wing spar/splicer plate back before the fuses were built. I just >propped up the wings, trailing edge up, level in the basement, clamped the >sockets with legs in place and carefully measured the required distances. I >pilot drilled the holes initially using some brass tubing model RR'rs build >with and enlarged them later to avoid damaging the existing spar holes. The >"hole" thing only took an hour once it was set up. I can't imagine drilling >them on the plane as suggested. It took several evenings just to put all >the bolts in. I drilled the side fuse bolts after the wings were bolted on. ________________________________________________________________________________
Subject: Re: RV6 VFR or IFR
<19970628.134233.8207.0.tcraig-stearman(at)juno.com> 43-50,52-56,58-60,62-87,89-92,94-104
From: wstucklen1(at)juno.com (Frederic W Stucklen)
Date: Jun 30, 1997
John, From the standpoint of flying many, many hours of IFR in aircraft that are more demanding than most certified small aircraft, you are probably one of the few who has an IFR competency level far in excess of the majority of people flying IFR. But for those individuals that are doing only 15-20 Hrs per 6 months, in less sensitive aircraft, the proficiency levels just aren't at your level of flying. Most civilian trained individuals never see the disciplinary level, or the level of flying experiences that you and your students enjoyed. Most civilian pilots are not thousands of hours in a T-38 for a living. These individuals certainly can use the lower work load levels a minimal autopilot has to offer. And yes, I agree autopilots are stupid and can kill if the pilot uses them for a cure-all to proficiency. That was not my premiss for suggesting that the most people flying the RV series find a wing level necessary. The pilot is ultimately responsible for the flying of the aircraft, not the autopilot. And he/she must FLY the AIRPLANE first. That means attitude and positional awareness at all times, regardless of what/who is maintaining the that attitude and position. Anybody flying IFR had better be proficient enough to handle any situation that they're dealt. This is by no means an excuse for not obtaining higher proficiency, or the number one task of flying the aircraft. I used my RV-6A to get my IFR ticket, and flew it without an autopilot for over a year in hard IFR. I now have over 200 Hrs of IFR in under three years. (900 Hrs TT on the -6A in under fours years). The RV-6 requires the pilot's proficiency to be above that needed to safely fly other certified small aircraft. While ground planning is essential to safe IFR, ammended clearances are a reality. Flying alone and fumbling with charts IFR conditions does happen. proficiency levels must be maintained to handle these conditions with or without the aid of other equipment. But that doesn't preclude the use of equipment that makes flying a bit less stressful. If we can't put our trust on a wing leveler for short durations while doing other cockpit tasks, then I dare say that we shouldn't be putting our trust in any other mechanical part of the aircraft as well (the engine?). While the autopilot is stupid, when coupled to the human brain, it can be useful. Fred Stucklen RV-6A N925RV wstucklen1(at)juno.com (John T. Craig-Stearman) writes: >Glenn, The RV series are fine IFR airplanes. They handle wonderfully >both in and out of the clouds. The airplane, of course, neither knows >nor cares whether it is in IMC. I find Mr. Stucklen's comment a bit >puzzling. Of course one must fly the airplane all the time. What else do you >intend to do in the cockpit? >>Most people find that a wing leveler is a "must have" in an RV-6 for IFR operation. >I disagree on the matter of a wing leveler. It adds unnecessary weight >and complexity to a light and simple airplane. I have quite a bit of >IFR time in the T-37 as a former Air Force instructor pilot. I also >have cloud time in the T-38, C-182, C-172, C-150, and Citabria. I >find that the civilian airplanes are actually less demanding on >instruments, because they fly at slower speeds. Every deviation takes >so much longer to develop that corrections are easier. My total >flying time on any form of autopilot is precisely zero. It is simply >unnecessary. There are many tasks that I don't mind automating in the >cockpit. Engine management, cowl flap operation, nav waypoint >sequencing, radio tuning by GPS database, are all acceptable areas for >automation. There is one task, however, that I will not delegate to a >machine under any circumstances, and particularly not under extreme >circumstances: flying the airplane. That is my job. An autopilot has >two glaring flaws in my opinion. First, it is stupid. It can never >think as well as the pilot can when handling unexpected problems. >Read about the ATR commuter crashes as an illustration. Second, it >does not care about preserving the pilot's soft, fleshly body. The >autopilot will quite willingly smack you into the terrain. Whatever >task you feel requires the aid of an autopilot is almost certainly >LESS important than flying the airplane. Fumbling with charts and >flipping approach plate pages can be minimized by pre-flight >preparation. If you find yourself so task-saturated that you cannot >adequately fly the airplane, it is time >to re-prioritize your tasks. FLYING the AIRPLANE must always come first. > Tell ATC to stand by, if necessary. One final note: In the T-37, >the instructor pilot sits on the right side, but must fly by reference >to the instruments on the left side. >After a couple thousand hours doing that, my RV-4 instrument layout looks >WONDERFUL. >Blue skies, >Tom Craig-Stearman tcraig-stearman(at)juno.com +-- > --+ | Visit the >Matronics & RV-List Web Sites at http://www.matronics.com! | | > --- | > | To [un]subscribe from the RV-List, email >"rv-list-request(at)matronics.com" | | & put the word "[un]subscribe" >in the *body*. No other text or subject. | +-- > --+ ________________________________________________________________________________
From: "David Moore" <dmoore8(at)tuelectric.com>
Subject: Re: Panel tilt and gyros - why not vertical panel?
Date: Jun 30, 1997
Hal Kempthorne wrote" > > I'm serious here - why not make my panel vertical - zero tilt? > > I'm fitting it now and last night I tried setting it straight and level and I > see no problem. If it is tilted fwd at top, won't I see more sky reflections? > Maybe it is so I can keep up the scan & still see the lightning? I worked on my canopy frame this weekend and the fit between it and the instrument panel is critical. It would also change the alignment between the canopy forward skin and the fuselage forward skin. Could be done, but you need to consider all of the ramifications of a change like this. Probably more trouble than it is worth. ________________________________________________________________________________
Date: Jun 30, 1997
From: "Steven Spruell" <SSPRUELL(at)us.oracle.com>
Subject: Re: Gall Strobe light Power Supply
--=_ORCL_22553445_0_11919706301209210 I hope you meant "3 times per second"... ****************************************************************************** * Steven Spruell Oracle Corporation * * Manager, Information Systems Phone: (713) 658-7748 Two Allen Center * * Houston Development Center Fax: (713) 654-0676 1200 Smith Suite 2700 * * sspruell(at)us.oracle.com Houston, TX 77002 * ****************************************************************************** --=_ORCL_22553445_0_11919706301209210 Date: 29 Jun 97 19:18:18 From:"Rick and Barbara Osgood " Subject:Re: RV-List: Gall Strobe light Power Supply les williams wrote: > > > Never heard of them. Where did you see info on them? > > Les Williams/RV-6AQ #60027 Another person on the list mentioned them as an alternative source to Wheelen. They are one of the major sources for law enforecment vehicles. The unit mentioned cost $44.95, flashes 3 times per minute and can handle 6 heads. -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com --=_ORCL_22553445_0_11919706301209210-- ________________________________________________________________________________
Date: Jun 30, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: aileron balance & gap seal (not)
Bill, I was looking up close at Chuck Hall's P-51 at Ramona a couple of weeks ago. All the control surfaces are counter-balanced. Miike Wills RV-4 (wings) willsm(at)manta.nosc.mil Does anyone know if the P-51 >has counter-balanced elevators? >Bill >RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV >flying hours. >These opinions are mine and do not necessarily represent the opinions or >position of my employer. ________________________________________________________________________________
Date: Jun 30, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: ANR - Headsets Inc...
Tom, Thanks for the response. So with the microphone installed in the earcup, any low frequency present would be considered "offending racket" and would be attacked by the ANR circuitry. This would include any low frequency portion of music (although some may consider this to be "offending racket" also). In our canceller applications we attempt to sample the offending signal at its source rather than its destination so that the canceller descriminates between desired and undesired signals. Some experimentation with placement of that microphone around the cockpit of the airplane (instead of in the headset earcup) may provide the desired results. It seems to me that the use of a seperate speaker to provide the cancellation is redundant. I would think a better place to house the ANR circuitry and pipe the cancellation signal into the audio stream would be at the intercomm box rather than at the headset. Why put any more weight on the pilots head than is necessary. I wonder if any of the intercomm manufacturers have considered this? Mike Wills RV-4(wings) willsm(at)manta.nosc.mil > >Mike Wills wrote: >> >> So if the Headsets Inc. system doesnt sample the input signal, and strip >> out the offending signal, what is the source of the cancellation signal that >> makes the whole thing work? >> >> Mike Wills >> RV-4 (wings) >> willsm(at)manta.nosc.mil >> >> >> >The Bose does compare the input stream so as to not block it out, The ANR >> >kit from Headsets Inc. does not, That is what you get for your addition >> >$850.00. That was from the owner of Headsets Inc. >> >> >Tailwinds, >> >Doug Rozendaal RV-4 N240 >> >dougr(at)netins.net >> >http://www.petroblend.com/dougr >> >>Mike, the Headsets Inc ANR adapters have electret microphones in the earcup that pick up the offending low-frequency racket. The signal is >amplified, phase-shifted and output to the second miniature speaker in >the earcup. The circuitry is proprietary (I asked), but is very simple. >There's just not a lot of parts on the board! >73 >Tom Glover ________________________________________________________________________________
From: "David Moore" <dmoore8(at)tuelectric.com>
Subject: Re: RV6 F-644
Date: Jun 30, 1997
Glen & Judi wrote: > > I am ready to cut out the two F-644's as per DWG 30. > > Vans has provided one 14" piece of channel for these parts. > > 14" would allow for two 7" pieces to be cut, however the plans call for > a bend at the end of each F-644, so the 14" piece is too short. > > Should the overall lenth of the F-644 be shortened? Or how should this > be handled? Ironically enough, I came across the same problem last night. Looking at it from a structural and load bearing standpoint, it appears that there should be some attachment to the sub-panel. I decided to use a small angle segment (3/4 x 3/4 x .063) to attach the F-644 to the sub-panel. On the firewall (forward) end, I trimmed off a chunk as the plans show. RV-6 Finishing kit, t = 5years, 4 months ________________________________________________________________________________
Date: Jun 30, 1997
From: Mike Wills <willsm(at)manta.nosc.mil>
Subject: Re: Pitot line - plastic or alu?
Hi Finn, I was plumbing my pitot over this last weekend and had the same question. I broke out my Sportplane Builder by Tony B. to read his recommendation. Aluminum, nylon, and polyethylene were all mentioned as reasonable choices. I then broke out my ACS catalog and found nylon, polyethylene, and tygon all looking like possible candidates. It occurred to me that the poly tubing looks like the same stuff sold by hardware stores, Home Depot, etc.. to hook up water supply to a refrigerator ice maker, so thats what I used. I assume that if it can take the 60 psi of water pressure I have in my house it should work for pitot. Total investment for 25 feet of tubing and fittings about $5.00. If anyone has tried this and had a problem please let me know. Mike Wills RV-4 (wings) willsm(at)manta.nosc.mil > >Searching through the archive I see some mention of using Tygon for the >pitot line. Has anyone experienced adverse effects of using plastic >instead of alu? > >Finn ________________________________________________________________________________
Date: Jun 30, 1997
From: Ernesto Sanchez <40106(at)utech.net>
Subject: Re: Gall Strobe light Power Supply
Steven Spruell wrote: > > I hope you meant "3 times per second"... > > ****************************************************************************** > > * Steven Spruell Oracle Corporation * > * Manager, Information Systems Phone: (713) 658-7748 Two Allen Center * > * Houston Development Center Fax: (713) 654-0676 1200 Smith Suite 2700 * > * sspruell(at)us.oracle.com Houston, TX 77002 * > ****************************************************************************** > > > > --------------------------------------------------------------- > > Subject: Re: RV-List: Gall Strobe light Power Supply > Date: 29 Jun 97 19:18:18 > From: "Rick and Barbara Osgood <SprintMail.com!randbosgood(at)matronics.com>" > Reply-To: rv-list(at)matronics.com > To: rv-list(at)matronics.com > References: > > > les williams wrote: > > > > > > Never heard of them. Where did you see info on them? > > > Another person on the list mentioned them as an alternative source to > Wheelen. They are one of the major sources for law enforecment vehicles. > The unit mentioned cost $44.95, flashes 3 times per minute and can > handle 6 heads. Gall's is a Law Enforcement and Fireman's equipment suppier. In their catalogs they have all types of lighting available (some of it is Whelen's stuff). Cheaper than airplane stuff but works good. Anyone can order from them. I posted the phone number awhile a go. Search the list for it. I can't find it right now. Free catalogs. Good stuff. Ernesto Sanchez es12043(at)utech.net RV-6 soon. ________________________________________________________________________________
Date: Jun 30, 1997
From: Rick and Barbara Osgood <randbosgood(at)SprintMail.com>
Subject: Re: Gall Strobe light Power Supply
Steven Spruell wrote: > > I hope you meant "3 times per second"... > > ****************************************************************************** > > * Steven Spruell Oracle Corporation * > * Manager, Information Systems Phone: (713) 658-7748 Two Allen Center * > * Houston Development Center Fax: (713) 654-0676 1200 Smith Suite 2700 * > * sspruell(at)us.oracle.com Houston, TX 77002 * > ****************************************************************************** > > > > --------------------------------------------------------------- > > Subject: Re: RV-List: Gall Strobe light Power Supply > Date: 29 Jun 97 19:18:18 > From: "Rick and Barbara Osgood <SprintMail.com!randbosgood(at)matronics.com>" <owner-rv-list(at)matronics.com> > Reply-To: rv-list(at)matronics.com > To: rv-list(at)matronics.com > References: > > > les williams wrote: > > > > > > Never heard of them. Where did you see info on them? > > > > Les Williams/RV-6AQ #60027 > > Another person on the list mentioned them as an alternative source to > Wheelen. They are one of the major sources for law enforecment vehicles. > The unit mentioned cost $44.95, flashes 3 times per minute and can > handle 6 heads. > > -- > Rick and Barbara Osgood > > RandBOsgood(at)sprintmail.com > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ Opps... you are correct, it is 3 times per second. -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com ________________________________________________________________________________
Date: Jun 30, 1997
From: randall(at)edt.com (Randall Henderson)
Subject: Re: RV-6 or 6A Slider specific roll bar brace
> >I put a lot of work into attaching the stainless steel brace tube with no > >thought whatever that Van's might have sent one that is too long. > > > >Mine will come thru the skin right at the sub panel (the first bulkhead after > >the firewall) and I am afraid that might interfere with the windshield. Or > does > >the windshield contact skin in front of the sub-panel?? > > > The location of the front (knife blade portion) of the roll bar brace is > called out on the plans. You then trim the top (tube portion) as required to Try as I might, I never could find this dimension. Where is it? I went looking for it after I made the same mistake that Hal made. The forward edge of my windscreen actually came out a little further back than most, so I did have to move the bar. I fabricated a new F-6109 doubler plate and reinforcing angle. I have yet to patch the slot in the skin, but that shouldn't be a big deal. Randall Henderson, RV-6 randall(at)edt.com http://www.edt.com/homewing ________________________________________________________________________________
Date: Jun 30, 1997
From: randall(at)edt.com (Randall Henderson)
Subject: Re: Oops HS-610
ll, > > While drilling the #40 pilot holes along the centerline of my HS-610, I > somehow managed to drill one of the 6 5/8" holes at 6" instead. [snip!] > Would an "extra" hole at > this location compromise the HS-610? How many of you would fabricate > another HS-610? Help!! TIA. I see someone else responded that "good enough probably isn't". I think I would probably disagree in this case. 3/8" is acceptable edge distance, although it may or may not be less than the minimum distance between rivets. (The military's minimums for this are published in MIL-R-47196A "Rivets, Buck-Type, Preparation and Installation of" -- see the rv-list FAQ for more on that.) If it meets edge distance and minimum spacing requirements, I really don't see why it would be a problem. If it doesn't meet spacing minimums but does meet edge distance, I would think you could leave it un-filled. Just my opinion. I think it would certainly be worth a call to Van's, in any case. Randall Henderson, RV-6 randall(at)edt.com http://www.edt.com/homewing ________________________________________________________________________________
From: JDaniel343(at)aol.com
Date: Jun 30, 1997
Subject: Re: Wood props
I received the following from the Thorp T-18 Newsletter by Rich Snelson: Gary Green to Rich Snelson: Your N.L. also mentioned that another cutdown M74D prop had failed. What are the details on this? I can hardly believe anyone would continue to fly a T-18 (or an RV-4/RV-6, for that matter) with one of those ticking time bombs bolted to the engine. A guy here in Texas has built several of these props for RV's and has experienced about a 20% inflight failure rate, so far. None of them have accumulated more than about 500 hrs before blowing up. If one buys a T-18 or an RV without subscribing to the current newsletter and reviewing the old newsletters, he operates in ignorance. He can avoid a lot of pain and expense by learning from the experiences of others. Gary Green 9111 Bellechase Granbury, Tx 76049 ________________________________________________________________________________
From: Shelby1138(at)aol.com
Date: Jun 30, 1997
Subject: Re: 6A Gear Leg Mounting
Could you go through your explanation in a little more detail. I am having difficulty visualizing what you did. E-mail me directly if you don't anyone else would benefit. Thanks in advance Shelby in Nashville. RV6A ________________________________________________________________________________
Date: Jun 28, 1997
From: Dave Barnhart <barnhart(at)a.crl.com>
Subject: Re: Paint Guns
mauser(at)claris.com (Richard Chandler) asked: > >I've always wondered, what is the real difference in conventional and HVLP >paint guns. I mean, it's been pretty well described what they do, but >what is >the practical difference in the way the paint gets from the end of the gun to >the surface being painted? Both blow a fine mist of paint at what you're >painting, so why is one so much different than the other? I'm not an expert, but due to the lower pressure, the HVLP gun atomizes the paint into larger droplets. This results in less misc paint being blown around, and less overspray. If you are using a Croix-style HVLP gun with a turbine, the turbine heats the air. Thus, if you are shhoting a paint (like Imron) that uses different reducers for different temperature ranges, you probably need to go to the next hotter (slower) reducer. Best Regards, Dave Barnhart rv-6 sn 23744 N601DB assebling engine ________________________________________________________________________________
Date: Jun 29, 1997
From: Dave Barnhart <barnhart(at)a.crl.com>
Subject: Why?
Here's a question I've been wondering about. Why do we use different relays for Master and Starter? Why not use another master relay as the starter relay? Best Regards, Dave Barnhart rv-6 sn 23744 N601DB engine being assembled by Lycon ________________________________________________________________________________
Date: Jun 30, 1997
From: John Ammeter <ammeterj(at)seanet.com>
Subject: RV Picnic at Arlington Airfair/Correction
>Date: Fri, 27 Jun 1997 17:30:39 >To: RV-List >From: John Ammeter <ammeterj(at)seanet.com> >Subject: RV Picnic at Arlington Airfair > >The Arlington Airfair at Arlington, WA (USA) will be held from July 9 to 13. This airport is the home of the world famous 'Blackjack Squadron'. As most of you know, the Blackjack Squadron is an informal group of local RV flyers that enjoy close formation airwork. They fly RV-4's and RV-6's with a wide range of engines and props. > >The Puget Sound RVators are again hosting a BBQ picnic on Saturday starting at noon in the RV aircraft parking area. Last year we served over 180 hamburgers and 50 pounds of salmon to well over 150 hungry RV'ers and guests. We also provide much needed shade and lots of lawn chairs along with refreshments to RV'ers during the rest of the Airfair. > The tickets mentioned below are for admission to the airfair ONLY. BBQ entrance is by donation; amount is up to your conscience (and how hungry you are). Sorry for the confusion. John. >I have tickets available for our guests at the 'air-arrival' rate. For $10.00 you can purchase a ticket good for all week or, if you're only coming for Saturday, you need only pay $5.00. If you're interested in purchasing these tickets please send me a check (made out to me) at the address below. Include a stamped self-addressed envelope and be certain to indicate what ticket('s) you want. BTW, children 15 and under are free if accompanied by an adult. > >If you're flying in there is no reason to pre-purchase your tickets; you'll get the same price 'at the gate'. This 'deal' only benefits those who are driving in to the Airfair. > >Hope to see many of you there. Stop by to talk to me; I'll be the one flipping burgers. > > ________________________________________________________________________________
Date: Jul 01, 1997
From: Leo Davies <leo(at)icn.su.OZ.AU>
Subject: Eastern Avionics International
Dear Listers, I have been looking at avionics packages. Being based some distance from the U.S. but liking the competitive Avionics market in your grand country I plan to use a U.S. distributor. I note that a company called Avionics East advertise a "Kwikmount" system where they provide the wiring harnesses for an avionics package. This looks like a good thing to a non electronics technician. Does anyone have any experience with Eastern Avionics and their Kwikmount system or any other group providing such? I don't want a complete panel build up just a bit of a leg up. If you have nice things to say post them to the list, anything negative send to me privately. Thanks, Leo Davies leo(at)icn.su.oz.au ________________________________________________________________________________
Date: Jun 30, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: Intake valves
I was just on the phone asking about whether to replace my intake valves on the major I'm having done to my O-320. Tom's engine problem brought this about, naturally. I was told that Lycoming does not require it for a major if dimensions and magnaflux checks out OK. The shop that is doing my major is highly recommended. Van's uses them also. They told me they have never had a problem with intake valves on a major. So they agreed with Lycoming. Tom, was your engine majored recently and do you know if they magnaflux them? Have a Good Day! Denny RV-6 (R)N641DH Fuselage top side Lebanon, OR ________________________________________________________________________________
Date: Jun 30, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: Re: Gall Strobe light Power Supply
Actually, neither flashing rate would be acceptable would it? Looks to me as if it is at least 40 flashes per minute (fewer than one per second) and not more than 100 flashes per minute (fewer than two per second). In case of overlaps, max is 180 per minute so 3 times per second would be on the upper edge. Hal Kempthorne RV-6AQ -- On main gear halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC > > I hope you meant "3 times per second"... > > ****************************************************************************** > > * Steven Spruell Oracle Corporation * > * Manager, Information Systems Phone: (713) 658-7748 Two Allen Center * > * Houston Development Center Fax: (713) 654-0676 1200 Smith Suite 2700 * > * sspruell(at)us.oracle.com Houston, TX 77002 * > ****************************************************************************** > > > > ________________________________________________________________________________
From: "Doug Rozendaal" <dougr(at)netins.net>
Subject: Re: Why?
Date: May 25, 1997
It has to do with contiuios vs intermittent duty cycle. The master relay is optimized for long duty cycles. The starter relay contacts are designed to accept the high starting loads of a starter. It would work but it would fail sooner if you used a master relay as a starter. Never use a starter relay as a master relay because the coil will overheat and fail very soon. Tailwinds, RV-4 N240 Doug Rozendaal dougr(at)netins.net www.petroblend.com/dougr ---------- > From: Dave Barnhart <a.crl.com!barnhart(at)matronics.com> > To: rv-list(at)matronics.com > Subject: RV-List: Why? > Date: Sunday, June 29, 1997 9:04 AM > > > Here's a question I've been wondering about. Why do we use different > relays for Master and Starter? Why not use another master relay as the > starter relay? > > Best Regards, > Dave Barnhart > rv-6 sn 23744 N601DB > engine being assembled by Lycon > > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ ________________________________________________________________________________
Date: Jun 30, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: Re: Eastern Avionics International
Hi Leo and others, Chief Aircraft in Grants Pass OR, is a good outfit: Chief AC 1301 Brookside Blvd, Grants Pass 97526 800.447.3408 chief(at)magick.net Have them send you a catalog - color yet! Hal Kempthorne RV-6AQ -- On main gear halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
From: RICKRV6(at)aol.com
Date: Jun 30, 1997
Subject: RV6 For Sale
Listers, Well it's time to start seriously getting some work done on this RV8. Unfortunately, that means giving up my RV6. Therefore, for sale is one 1992 RV6 N523JC, sn:20404, 440 hours TT Airframe, O-320-E2G, 222 hours TT since factory remanufacture with a Warnke 72x70 prop. Panel includes full gyros, Terra digital nav/com, Narco transponder, IIMorrow 612 BCV loran, Sigtronics stereo intercom. The list of features goes on. If you look at your RV calander for this month, July, you will see this airplane. The asking price is $55k. I will be flying throughout the Western US next week and will be (weather permitting) at Arlington for a day or so if your interested in a closer look. I also plan to have the airplane at Oshkosh Tuesday through Sunday. For more information you can call me, Rick McBride at (630) 851-3136 or my partner, Jim Longley at (815) 684-4076. This has been an exceptionally fun airplane and I wouldn't sell it but I'm itching to build again and there has to be a bill payer. Rick McBride RV6 N523JC RV8 80027 ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: 6A Gear Mount - False Spar Method
Date: Jun 30, 1997
Several builders have asked for more detail on the false spar method of 6A gear mount drilling. It saves time and, most importantly, saves space, because it does not require wing insertion. The procedure below is based on a method described to me by 6A builder Scott Johnson. Scott used it successfully and he reported that his mounts fit the wing spar perfectly when he installed the wings during final assembly. 1. Measure spar thickness. 2. Get suitable wood of identical thickness; a planer will be required. I glued together two pieces of marine plywood and planed them. If the wood is not of identical thickness as the spar, the holes in the longeron will be displaced by an amount equal to the difference between the false spar and the real spar. This can be compensated by drilling the holes in the longeron undersized, and drilling to final size when the wing is finally inserted. Drilling larger holes when the two mating holes are slightly offset can create elongated holes, so try to get the thicknesses equal. 3. Saw wood to same outline as spar from root to about 6 inches beyond fuselage sides. 4. Obtain long center drills from Avery: 3/16 and 1/4; a standard-length 3/8 center drill is useful as well for the largest spar holes; else use a transfer punch. Center drills have only a special "starting point" and the rest is a smooth shaft. 5. Rout slots in wood false spars to clear rivets in spar. 6. Clamp false spar to real spar and drill in alignment with center drills; just start hole; transfer punches can be used to transfer hole centers if center drills are not available, but the center drill method is more accurate. 7. Finish drill in drill press to ensure perpendicularity. 8. Use the false spar with splice plates to hold the F604 rigidly while drilling cabin seat ribs; the F604 can easily be deflected from straightness by the force of unequal length ribs. 9. After installing the platenuts in the F604, rout grooves so the false spar can be slipped over them for gear mount drilling. 10. False spars can now be used to drill the landing gear mounts and later serve as outriggers to which legs can be clamped when the fuselage is removed from the jig. 11. Drill landing gear mounts with a 12-inch long modified #12 drill from Avery. Grind down the flutes 1 1/8 inch beyond the tip so the F604 will not be contacted by the full drill diameter. The false spar serves as a sacrificial drill guide. The holes in the F604 are not enlarged because the drill diameter has been reduced in this region of contact. The measurements below were made with a Smart Level Pro and were repeatable to the same value or at most 0.1 degree difference on successive measurements. Thus leg angles would measure 45.5 degrees on 4 out of 5 attempts and 45.6 on the non-agreeing measurement. The "leg angle" is the angle measured with the level resting unsupported along the leg. It is a measure of symmetry. I tried to get the legs perfectly level but finally accepted the 0.2 degree tilt. This will cause one wheel to be about 1/4 inch lower than the other over a 86 inch tread width. The legs didn't seem to go where I thought they would when I made adjustments. The mounts can be either displaced vertically or rotated to effect levelness. I found that rotating introduced other alignment problems and the vertical displacement range was rather limited. After about five attempts I concluded that 0.2 degrees was as level as I could get without some complicated shimming. Measurement on my clamped gear mount geometry per SK-63. Parameter Measured Value Spec Levelness 0.2 degree right side low Level Right leg angle 45.5 degrees N/A Left leg angle 44.7 degrees N/A Spacer-gage right 25/32 inch 23/32 - 24/32 Spacer-gage left 25/32 inch 23/32 - 24/32 Toe-in right 3/32 inch 2/32 Toe-in left 3/32 2/32 Alignment angle right 8.3 degrees 7-8 degrees Alignment angle left 7.3 degrees 7-8 degrees Shims were required: 0.032 against right spar; 0.125 on left forward pad. Dennis Persyk ________________________________________________________________________________
Date: Jun 30, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: Re: Why?
Hi Dave, This is not a good answer to your question but, I was told the master is a continuous duty relay and the starter relay is not. The starter relay can handle much more of a load than the master. If this is wrong, someone straighten me out on this. See ya. ________________________________________________________________________________
From: "mcomeaux" <mcomeaux(at)cmc.net>
Subject: Paperwork--sale of plane
Date: Jun 30, 1997
Does anyone know of any paper work I can down load from computer for sale contract or release of respon- sibility of a experimental aircraft. I have a buyer want- ing to purchase. If someone could e-mail me at mcomeaux(at)cmc.net I would appreciate it. Thanks. Mike Comeaux ________________________________________________________________________________
Subject: Re: Why?
From: less_drag(at)juno.com (JAMES E AYERS)
Date: Jul 01, 1997
writes: > (Snip) >Never use a starter relay as a master relay because the coil will overheat and fail very soon. > >Tailwinds, RV-4 N240 >Doug Rozendaal >dougr(at)netins.net >www.petroblend.com/dougr > Hi All, Doug has a very good comment here. I know of one case where a starter relay was used for a master relay. It took just about one hour of continuous operation for the relay insides to melt down. It shorted the battery cable to ground and started the insulation on the cable burning. This was at the end of the first flight of an RV-3. Fortunately, the pilot was taxiing back to the hangar when it happened. It was still very exciting for him. This RV-3 had the battery in front of the main spar, right under the 25 gallon fuselage fuel tank. The pilot beat the flames out with a shop rag that he had in the cockpit, and jumped out of the cockpit (springing the sliding canopy in the process). The Master Relays I checked had a 12 ohm coil, so they will draw 1 amp from a 12 volt battery. The Starter Relays I checked had a 3, or 4, ohm coil, so they will draw 4, or 3, amps from a 12 volt battery. Jim Ayers Less_Drag(at)juno.com ________________________________________________________________________________
Date: Jul 01, 1997
From: "L. Coats" <lcoats(at)wave.co.nz>
Subject: Re: ANR - Headsets Inc...
>aol.com!JDaniel343(at)matronics.com wrote: >> Does any one know if Headsets Inc. adapter will work in the Flightcom Eclipse >> headset? >>According to my Headsets Inc. documentation, the ANR adapters DO NOT fit the Flightcom Eclipse. Sorry to be bearer of bad news. >Tom Glover Ok, another question, can you use the ANR in the Flightcom Blackhawk headsets or Flightcom Nighthawks. Is there a list that could be put on the list for further reference for the other head set types? L.Coats RV6 193hr ________________________________________________________________________________
Subject: Re: 6A Gear Mount - False Spar Method
From: wstucklen1(at)juno.com (Frederic W Stucklen)
Date: Jul 01, 1997
Dennis, While I didn't use your method, I did find that a piece of 3/16" steel brake line makes a good drill guide for drilling out the landing gear mounting assemblies. Instead of relying on drill to center in the wood, I drilled the false spar out to #12, then slid the steel tubing through the spar assembly. the outside diameter of the steel tubing is exactly the size of the #12 holes in the F604 part. I used a long #30 drill inside the steel tubing to drill pilot holes in the landing gear assemblies. These were then later drilled to the proper size on the drill press. Fred Stucklen RV-6A N925RV wstucklen1(at)juno.com writes: >11.Drill landing gear mounts with a 12-inch long modified #12 drill from >Avery. Grind down the flutes 1 1/8 inch beyond the tip so the F604 will >not be contacted by the full drill diameter. The false spar serves as a >sacrificial drill guide. The holes in the F604 are not enlarged because >the drill diameter has been reduced in this region of contact. >Dennis Persyk > ________________________________________________________________________________
From: justjas(at)mn.frontiercomm.net
Date: Jul 01, 1997
Subject: Oops HS-610
I have had a similar problem recently and called Van's. I was told that the thicker aluminum angle material is not subject to the 2 diameter limit of the thinner aluminum. They would use a 1 diameter test. In my case I had drilled off center (late at night when most of the errors occur). I agree with Randall H, give Van's a call. Jay Jenkins, RV-8, s/n 80017 justjas(at)mn.frontiercomm.net ________________________________________________________________________________
Date: Jul 01, 1997
From: Sharlene Shipley or Bruce Knoll <snsbfk(at)mail.sage.net>
Subject: Re: Paperwork--sale of plane
You need a lawyer - I am not one. I would contact the EAA and also Van's for their direct advice. Please let the "list" know what the final word is! Bruce Planning to start RV6a after Osh. > >Does anyone know of any paper work I can down load >from computer for sale contract or release of respon- >sibility of a experimental aircraft. I have a buyer want- >ing to purchase. If someone could e-mail me at >mcomeaux(at)cmc.net I would appreciate it. Thanks. > > >Mike Comeaux > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
Date: Jul 01, 1997
From: Sharlene Shipley or Bruce Knoll <snsbfk(at)mail.sage.net>
Subject: Re: Paperwork--sale of plane
I am not a lawyer, but you need one. I have heqard this discussed in the distant past and one idea was to unregister the aircraft and sell it as a kit or parts. Again, you need a lawyer. Please enlighten the list when you find out. I know of one fatal accident in Jackson MI about 5 - 6 years ago that was caused by the wing of an RV 4 folding up. The fellow had purchased the planew within the preceeding year. If interested, contact me on my e-mail & I will try to find out any legal details from the locca > >Does anyone know of any paper work I can down load >from computer for sale contract or release of respon- >sibility of a experimental aircraft. I have a buyer want- >ing to purchase. If someone could e-mail me at >mcomeaux(at)cmc.net I would appreciate it. Thanks. > > >Mike Comeaux > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
Date: Jul 01, 1997
Subject: Re: Paperwork--sale of plane
From: jepilot(at)juno.com (J E REHLER)
An airplane is, of course, considered personal property ( not real property) and therefor is subject to the Uniform Commercial Code adopted in most, if not all, states. To disclaim any implied warranty of fitness or suitability or merchantability you should state in the bill of sale or other transfer document that the plane is sold and transferred AS IS and WITH ALL FAULTS. Acceptance of the bill of sale by the buyer is the buyer's agreement to this UCC disclaimer. The FAA requires the use of its "form" bill of sale which is very short and simple but does not provide space for the AS IS disclaimer. I have simply written AS IS and WITH ALL FAULTS in the available space on this form. Also you can use for your purposes a second bill of sale (not delivered to the FAA, just exchanged between seller and buyer) which states the terms of the sale and transfer more completely. In this second document you might state all relevant facts e.g. the plane is experimental, home built, the buyer has had full opportunity to inspect it and has done so to the buyer's satisfaction, the buyer accepts the plane based only on the basis of his/her inspection and not in reliance upon any representation, statement or warranty made by the seller, the buyer confirms that the seller had not made any representation or warranty regarding the condition of the plane ( if this is a true statement, if not state exactly and narrowly what representations are made by the seller and be prepared to stand behind them), and the buyer accepts the plane AS IS and WITH ALL FAULTS. Both the seller and buyer should sign this bill of sale (make duplicate copies so both can have final copies). Also this wording typically does not give any protection to a seller who is lying . If a seller has knowledge of any defect or adverse condition (particularly if hidden from sight), then the seller should fully disclose it to the buyer and have the buyer confirm the disclosure. The AS IS etc. disclaimers do not protect sellers who have knowledge and hide the potential problem. You might try to negotiate a release of claims from the buyer. Typically a release is binding only on the signing (releasing) party and not binding on the spouse, kids, estate, etc. Each state has slightly different laws regarding these matters. The discussion above is only general in nature and if you are really concerned you should consult with an experienced attorney in your state. Using any type of universal form carries with it the risk that a particular state requirement will not be covered adequately. Everyone professes to hate attorneys but we all don't sue people and some of us really to try to assist clients in handling their business affairs hopefully in a manner than eliminates or reduces the risks that have always existed in any society (some people will lie, cheat and take advantage, but only a few). The problem is you must assume the worse to adequately protect yourself. If everyone was honest , open and trustworthy, attorneys, judges, juries, mediators, arbitrators, etc would be out of work which would be great for society, but this is not going to happen. Hope this short course is helpful to you in the sale of your plane. J. E. Rehler RV6A Flying ________________________________________________________________________________
Date: Jul 01, 1997
From: Gene Gottschalk <geneg(at)rattler.gsfc.nasa.gov>
Subject: Re: 6A Gear Mount - False Spar Method
RV List, I corresponded with Dennis off-line, but this may be of interest to the remainder of the group, so I am attaching my comments and reposting. -Gene Gottschalk N700RV, skinning fuselage. Dennis, Thanks for the reply! This is pretty close to what I was thinking. Below are a few additional thoughts. I noticed that when I assembled my wings that the Phlogistin pre-drilled holes were less than perfect. The rivet lines were not straight, wing ribs did not align properly at the specified position, and as near as I could tell, the holes were not perpendicular to the spar face either. The reason I felt the holes were not straight is that when placing the 3/16 rivets into the spar assembly I noticed the heads would show a little gap under one side prior to setting. Since the wing spar pieces were drilled in assemble this did not present a problem assembling the spars. The biggest concern I had was the possible variances in hole location if I drill the substitute wooden spar perpendicular on the drill press and the holes through the spar are not perfectly perpendicular through the thickness of all the spar stiffeners and doubler plate. A little trick I used while drilling the motor mount to the firewall was to use telescoping pieces of brass tubing purchased at the local hobby shop. I was concerned about enlarging or elongating the motor mount weldmount holes drilling through them with a 3/8 inch drill bit. I telescoped the hole size down to 1/8 inch using about 7 or 8 pieces of tubing, and then used progressively larger drill bits to ream out the hole through the original 1/8 inch pilot hole. This results in minimal wear to the weld mount as only the last 1/32 inch of reaming actually touches the inside of the welded tube. It also finds the center accurately. The same thing could be done with the gear leg brackets. I thought about drilling only a couple of holes just to locate the mounts accurately, saving the remainder for final assembly, in case I need to make a slight adjustment. Your concern here is access to the weldmounts after the floor is riveted? -Gene > >Several builders have asked for more detail on the false spar method of 6A >gear mount drilling. It saves time and, most importantly, saves space, >because it does not require wing insertion. The procedure below is based on >a method described to me by 6A builder Scott Johnson. Scott used it >successfully and he reported that his mounts fit the wing spar perfectly >when he installed the wings during final assembly. > > >1. Measure spar thickness. >2. Get suitable wood of identical thickness; a planer will be required. I >glued together two pieces of marine plywood and planed them. If the wood is >not of identical thickness as the spar, the holes in the longeron will be >displaced by an amount equal to the difference between the false spar and >the real spar. This can be compensated by drilling the holes in the >longeron undersized, and drilling to final size when the wing is finally >inserted. Drilling larger holes when the two mating holes are slightly >offset can create elongated holes, so try to get the thicknesses equal. >3. Saw wood to same outline as spar from root to about 6 inches beyond >fuselage sides. >4. Obtain long center drills from Avery: 3/16 and 1/4; a standard-length >3/8 center drill is useful as well for the largest spar holes; else use a >transfer punch. Center drills have only a special "starting point" and the >rest is a smooth shaft. >5. Rout slots in wood false spars to clear rivets in spar. >6. Clamp false spar to real spar and drill in alignment with center drills; >just start hole; transfer punches can be used to transfer hole centers if >center drills are not available, but the center drill method is more >accurate. >7. Finish drill in drill press to ensure perpendicularity. >8. Use the false spar with splice plates to hold the F604 rigidly while >drilling cabin seat ribs; the F604 can easily be deflected from >straightness by the force of unequal length ribs. >9. After installing the platenuts in the F604, rout grooves so the false >spar can be slipped over them for gear mount drilling. >10. False spars can now be used to drill the landing gear mounts and later >serve as outriggers to which legs can be clamped when the fuselage is >removed from the jig. >11. Drill landing gear mounts with a 12-inch long modified #12 drill from >Avery. Grind down the flutes 1 1/8 inch beyond the tip so the F604 will >not be contacted by the full drill diameter. The false spar serves as a >sacrificial drill guide. The holes in the F604 are not enlarged because >the drill diameter has been reduced in this region of contact. > >The measurements below were made with a Smart Level Pro and were repeatable >to the same value or at most 0.1 degree difference on successive >measurements. Thus leg angles would measure 45.5 degrees on 4 out of 5 >attempts and 45.6 on the non-agreeing measurement. The "leg angle" is the >angle measured with the level resting unsupported along the leg. It is a >measure of symmetry. >I tried to get the legs perfectly level but finally accepted the 0.2 degree >tilt. This will cause one wheel to be about 1/4 inch lower than the other >over a 86 inch tread width. The legs didn't seem to go where I thought >they would when I made adjustments. The mounts can be either displaced >vertically or rotated to effect levelness. I found that rotating >introduced other alignment problems and the vertical displacement range was >rather limited. After about five attempts I concluded that 0.2 degrees was >as level as I could get without some complicated shimming. > >Measurement on my clamped gear mount geometry per SK-63. > >Parameter Measured Value Spec >Levelness 0.2 degree right side low Level >Right leg angle 45.5 degrees N/A >Left leg angle 44.7 degrees N/A >Spacer-gage right 25/32 inch 23/32 - 24/32 >Spacer-gage left 25/32 inch 23/32 - 24/32 >Toe-in right 3/32 inch 2/32 >Toe-in left 3/32 2/32 >Alignment angle right 8.3 degrees 7-8 degrees >Alignment angle left 7.3 degrees 7-8 degrees > >Shims were required: 0.032 against right spar; 0.125 on left forward pad. > >Dennis Persyk > > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
From: mikel(at)dimensional.com
Date: Jul 01, 1997
Subject: Re: Paint Guns
>>I've always wondered, what is the real difference in conventional and HVLP >>paint guns. >I'm not an expert, but due to the lower pressure, the HVLP gun atomizes the >paint into larger droplets. This results in less misc paint being blown >around, and less overspray. >If you are using a Croix-style HVLP gun with a turbine, the turbine heats >the air. Thus, if you are shhoting a paint (like Imron) that uses >different reducers for different temperature ranges, you probably need to >go to the next hotter (slower) reducer. The Croix factory recommends thinning and reducing to a slower-drying mix. Orange peel is an indication of: under reduction, improper thinning solvent, improper flow from the gun, improper air pressure or surface-drying too fast (take your pick). Sometimes it helps to visit your paint dealer and ask if they have any returned stock (similar to what you will be using) they will sell for less than usual. Take that out and shoot a quart or two at some scrap auto fenders or other metal and get the settings for the gun down. HVLP guns have different settings than used for a standard gun and it takes Experimentation to get it right. They are great once you figure them out but it is frustrating in the meantime. I wouldn't practice on something I was planning on anyone seeing. Have fun.......... Michael ________________________________________________________________________________
Date: Jul 01, 1997
From: randall(at)edt.com (Randall Henderson)
Subject: rv-list pin, hat, t-shirt, whatever
A while ago there was discussion of an rv-list hat, t-shirt, pin, patch, or whatever that people could use to identify themselves at fly-ins and such. At that time I volunteered to work something up. I recently got a query about how that's going so I figured I'd better fess up -- I have kind of put it on the back burner for now. I may yet get to it but I guess it isn't going to happen by Oshkosh like I had hoped. In the mean time if anyone else wants to do it instead that's fine with me. Feel free to contact me privately and I'll give you what I've come up with so far. Otherwise I may yet get to it but not for a while. Randall Henderson, RV-6 randall(at)edt.com http://www.edt.com/homewing ________________________________________________________________________________
Date: Jul 01, 1997
From: Rick and Barbara Osgood <randbosgood(at)SprintMail.com>
Subject: Gall's and Wheelen power supply
I have a little more info on one of the power supplies available from Gall's. There are different models of higher wattage or for more heads but that is the main difference. I have also requested a wiring diagram and if possible I will post that as well. Here ya go. Gall's Inc. 2680 Palumbo Dr. Lexington, KY 40555-4308 1-800-477-7766 Wheelen Power Supply Model# U-GR083 Price New $99.99 Price reman. $74.99 5 year warranty on new units 90 days on reman units. Input Voltage - 12.0 - 28VDC Input Current - 5.5 amps Flash Rate - 120 per minute Size - 2 1/8 x 5 1/4 x 6" Weight - approx. 1 -2 lbs Supports up to 6 individual strobe heads @ 45 Watts each. -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com ________________________________________________________________________________
From: justjas(at)mn.frontiercomm.net
Date: Jul 01, 1997
Subject: Paperwork--sale of plane
Mr. Rehler said it correctly - "The problem is you must assume the worse to adequately protect yourself. If everyone was honest , open and trustworthy, attorneys, judges, juries, mediators, arbitrators, etc would be out of work which would be great for society, but this is not going to happen." You have to start this analysis with the understanding that you absolutely can not stop someone from filing a complaint naming you as a defendant. If an accident or incident occurs and you are sued, the court system within the U.S. will be inclined to compensate the widow and children of the dear departed (not so well informed) operator / buyer of the aircraft. Depending on the circumstances, the court may go to extremes to find liability. Liability means dollars ($) and the only way to avoid the hit is to have dollars ($$) available. The best way to have dollars available is to have insurance (but I'm getting ahead of myself). Mr. Rehler gave everyone the short course on UCC warranty disclaimers (and you should, additionally, disclaim all express and implied warranties in any sale document) and a small bit on releases. In addition to disclaiming warranties and obtaining a release, there are a couple of other things you should have your attorney put in the sale document (because the more defenses you have available, the better your chances are of avoiding liability ($$$)). Here are the additional things I would have my attorney put in any sale document (signed by the buyer): (1) an acknowledgment from the buyer that buyer understands the aircraft is a homebuilt aircraft, built by someone that is not a professional in aircraft construction [delete if inappropriate], certified by the FAA in the experimental category and that buyer accepts any and all risks associated with such status; (2) an acknowledgement from buyer that the aircraft has been thoroughly inspected by a competent, knowledgable person! and found to be acceptable in all respects; (3) an indemnification from buyer indemnifying seller for everything that has occurred since the creation of time; and (4) [THIS IS THE DOLLAR ($) PART] a requirement that buyer obtain insurance naming seller as an additional insured under the policy and insuring the indemnifcation set forth in the sale document. The sale document with all these provisions will be several pages long and will appear very imposing to your ordinary "run of the mill" buyer, but this is the best way to both sell your aircraft and attempt to avoid liability for the unthinkable. Make sure you use an attorney that understands these issues and have a buyer that understands you don't want any problems after the sale is complete (and that is the reason for all this "stuff"). Jay Jenkins, RV-8 s/n 80017 (Emp) justjas(at)mn.frontiercomm.net ________________________________________________________________________________
Date: Jul 01, 1997
From: "Byron B. Ward" <bbward(at)tardis.svsu.edu>
Subject: Fly-in (not RV related)
I would like to welcome everyone to our EAA Chapter 597 Dawn Patrol on Sunday July 13. It is at Chesaning, MI (50G) airport. Great food, clown and face painting for kids, door prizes, etc. Also there will be a parade later. No fuel on the field however. Any questions please email me. Sorry for straying off topic Byron Ward bbward(at)tardis.svsu.edu ________________________________________________________________________________
Date: Jul 01, 1997
From: Jeremy William Benedict <jbenedic(at)uofport.edu>
Subject: Van's New Web Site
Don't just read it EXPERIENCE IT www.vansaircraft.com July 1, 1997 ________________________________________________________________________________
From: Alex Peterson <alex.peterson(at)deltec.com>
Subject: 6A Gear Mount - False Spar Method
Date: Jul 01, 1997
Regarding drilling the 6A gear mounts without having the wings in the fuselage: I also noted the problem of the holes thru the spar being out of perpendicularity. As was already pointed out, this causes alignment problems when the spar dummies are match drilled to the spars. One can minimize this problem if the spar dummies are made with an aluminum or steel plate (.040 or so) as the forward-most laminate. Clamp just this plate against the forward side of the actual wing spar, and then match drill it to the spar. Once drilled, clamp or fasten it to the remaining spar dummy wooden laminates (I used 5/8" maple plywood from a die cutting shop) and drill (aft-ward, with a drill press) thru this plate. The holes in the aft side of the spar dummy may be slightly mis-aligned with the holes in F604, but the aft end of the holes in the dummy spars can be opened up without causing any problems. The goal here is that the hole locations in the forward side of the dummies match the holes in the forward side of the actual spars. Also, once the gear mounts were aligned, I located and drilled only 2 holes in each mount thru the dummy spars. These two holes will be used to locate the mounts on the actual spars (not in fuse.) for drilling the remainder of the holes. Another tip for those building 6A's in the wing or pre-spar stage: Several holes (I recall about 4 in each spar, check the dwgs) need to be enlarged to 1/4" for the gear mounts. Align the spar parts with the appropriate F604 bulkhead parts and drill/ream as an assembly. I believe this is much easier than doing so in the fuselage. Alex Peterson -6A seat bottoms. ________________________________________________________________________________
Date: Jul 01, 1997
From: dougm(at)mailhost.physio-control.com (Doug Medema)
Subject: Re: Van's New Web Site
Jeremy: I've looked at most of it and it is a BIG improvement. Thanks for putting the complete optional parts catalog on line! Check it out folks! Doug Medema, RV-6A, skinning fuselage. > From uofport.edu!jbenedic(at)matronics.com Tue Jul 1 16:18:21 1997 > Date: Tue, 1 Jul 1997 12:29:43 -0700 (PDT) > From: Jeremy William Benedict <uofport.edu!jbenedic(at)matronics.com> > To: rv-list(at)matronics.com > Subject: RV-List: Van's New Web Site > Mime-Version: 1.0 > > > > Don't just read it > > EXPERIENCE IT > > www.vansaircraft.com > > July 1, 1997 > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ ________________________________________________________________________________
Date: Jul 01, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: Re: Paperwork
Sharlene Shipley or Bruce Knoll wrote: > > > **snip** > I know of one fatal accident in Jackson MI about 5 - 6 years > ago > that was caused by the wing of an RV 4 folding up. The fellow had > purchased > the planew within the preceeding year. If interested, contact me on my > e-mail & I will try to find out any legal details from the locca > Are you sure that it was a RV-4? I have not heard of a -4 or -6 looseing a wing. -- Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR jsflyrv(at)ix.netcom.com ________________________________________________________________________________
From: PhilipR920(at)aol.com
Date: Jul 01, 1997
Subject: Re: Gall Strobe light Power Supply
I can't find anything in the archives related to Gall. Please furnish phone number. Phil Rogerson 6AQ 60057 ________________________________________________________________________________
Date: Jun 30, 1997
From: Dave Barnhart <barnhart(at)a.crl.com>
Subject: Re: Why?
I asked: > Here's a question I've been wondering about. Why do we use different > relays for Master and Starter? Why not use another master relay as the > starter relay? "Doug Rozendaal" replied: >It has to do with contiuios vs intermittent duty cycle. The master relay >is optimized for long duty cycles. The starter relay contacts are designed >to accept the high starting loads of a starter. It would work but it would >fail sooner if you used a master relay as a starter. But during starting, the current flow is thru the Master relay, then thru the starter relay to the starter. So during starting, the master relay is handling the same starting load as the starter relay. So I still don't understand. Best Regards, Dave Barnhart ________________________________________________________________________________
From: "mcomeaux" <mcomeaux(at)cmc.net>
Subject: Thanks for info
Date: Jul 01, 1997
I want to thank everyone for the info and I will be discussing this with a attorney that I have located here close by that has performed this type of sale before. I also recieved a lot of info from the eaa. Regards-------Mike Comeaux RV6QB real soon ________________________________________________________________________________
Date: Jul 01, 1997
From: "Scott A. Jordan" <SAJ_SLJ(at)compuserve.com>
Subject: Static Wicks
I plan on equiping my RV-8 for IFR travel. In looking at other RV's, I don't think I have ever seen static wicks on any. For those of you who f= ly IFR, do you have static wicks installed? How have you decided where and h= ow many to install? If not, is static a problem with your com radios? I'm getting ready to close up my rudder and thought it might be good to p= ut the wicks on at that time. = Thanks for your help Scott RV-8 80331 N733JJ ________________________________________________________________________________
Date: Jul 01, 1997
From: Sharlene Shipley or Bruce Knoll <snsbfk(at)mail.sage.net>
Subject: Re: Paperwork
Jerry, At the time I was told that the wing on the RV4 folded back and hit the pilot in the head and he was instantly killed begfore the plane hit the ground. I lived in Jackson MI at the time and was vaguely acquainted with the fellow in question. He had purchased the plane to learn acrobatics and was returning from his practice area at the time of the mishap. I will try to contact the EAA boys up there and double check my memory. Bruce. > >Sharlene Shipley or Bruce Knoll wrote: >> >> >> > **snip** >> > I know of one fatal accident in Jackson MI about 5 - 6 years >> ago >> that was caused by the wing of an RV 4 folding up. The fellow had >> purchased >> the planew within the preceeding year. If interested, contact me on my >> e-mail & I will try to find out any legal details from the locca >> >Are you sure that it was a RV-4? I have not heard of a -4 or -6 >looseing a wing. >-- >Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR >jsflyrv(at)ix.netcom.com > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
Date: Jul 01, 1997
From: Rick and Barbara Osgood <randbosgood(at)SprintMail.com>
Subject: Re: Gall Strobe light Power Supply
aol.com!PhilipR920(at)matronics.com wrote: > > > I can't find anything in the archives related to Gall. > > Please furnish phone number. > > Phil Rogerson > 6AQ 60057 > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ I posted the entire address this am. Here it is again: Gall's Inc. 2680 Palumbo Dr. Lexington, KY 40555-4308 1-800-477-7766 -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com ________________________________________________________________________________
Date: Jul 01, 1997
From: Ronald Vandervort <rvanderv(at)linknet.kitsap.lib.wa.us>
Subject: Re: Oil Pressure Switch
All the usual sources for oil pressure switches seem to have only the normally open switch. Where can one find a normally closed switch? I think a normally closed oil pressure switch hooked up to a buzzer would do well as a " master switch on" warning setup. Ron Vandervort, RV-6Q, working on instrument panel mockup. Seattle area ________________________________________________________________________________
Date: Jul 02, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: Re: Paperwork (off subject)
Sharlene Shipley or Bruce Knoll wrote: > > > Jerry, > At the time I was told that the wing on the RV4 folded back and hit > the > pilot in the head and he was instantly killed begfore the plane hit > the > ground. I lived in Jackson MI at the time and was vaguely acquainted > with > the fellow in question. He had purchased the plane to learn acrobatics > and > was returning from his practice area at the time of the mishap. I will > try > to contact the EAA boys up there and double check my memory. > > Bruce. > Hi Bruce I did a little checking myself in the NTSB reports in LANDINGS and found the RV in question Aug. 6, 1992, at Jackson, MI it was a RV-3. Living here as close as I do to Van's I usually hear about any problems with RV's plus they are always very conscientious about getting the word out about problems as they get the facts. I have only heard of one RV-4 breakup and that was a horizontal stab. and as far as *I know* it is still in the preliminary stage of investigation. Fly safe Jerry Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR jsflyrv(at)ix.netcom.com ________________________________________________________________________________
Date: Jul 02, 1997
From: "W. Tom Glover" <tglovebox(at)bc.sympatico.ca>
Subject: Re: ANR - Headsets Inc...
L. Coats wrote: > > > > Ok, another question, can you use the ANR in the Flightcom Blackhawk > headsets or Flightcom Nighthawks. Is there a list that could be put on the > list for further reference for the other head set types? > > L.Coats RV6 193hr > >Answer: I don't know. I am not familiar with either of those models. The information I have is old stuff now, but I'll give you what I have. This is taken directly from the installation instructions as I have them. "some headsets have an obstruction inside one earcup. DC 13.4 has obstruction (nylon nut) in left earcup, requiring shallower left earpiece. FlightCom model 5DX has p.c. board in left earcup, requiring shallower left earpiece. Eclipse model does not fit. Softcom C-60 has large volume control in right earcup which must be removed. Also has PTT switch in right earcup, must be disconnected. Hush-a-Com has printed circuit in left earcup, must be removed. This p.c. board has no components on it and acts as junction board and it may be removed." I have not used the "shallower earpiece" In my own experience, they fit and work well in older Clarks, and are particularly well suited to the FlightCom 4DX. That's what I used for a "demonstrator" which the demonstratee decided to keep. I have installed them in my own Telex EBM-1400, and suspect that they will fit easily in the DBM-1000 model. Two recommendations: 1. Gel ear seals are recommended. I prefer the liquid ones; they seal well. 2. Large ear seals (a la Oregon Aero) can disrupt the operation of the ANR adapters. They prefer the smallest possible volume of air next to the ear. In my own opinion, I feel that it requires some electronic expertise to install these adapters. Small soldering irons, small cutters and seizers (haemostats?) are necessary to do the job. It's finnicky trying to install these things on the ends of short, tiny wires half-way inside the earcup. It's real easy to melt the unexpected. The trick, if you are electronically challenged, is to find a buddy who is into doing this stuff to do it for you. It takes me about an hour to do these things. Although I'm sure that others can do it quicker, I take my time and try to avoid misteaks (especially when the headset owner is watching). I'd like to compare some of the other high-end headsets with the Headsets Inc. adapters in flight. Getting suppliers to give out headsets just for tests, however, is unlikely. I will be at Arlington on Saturday, if anyone would like to try out my Telex 1400's. I don't know how we could get together, but I suppose we could meet at the RV Barbecue area at a certain time. It's a good possibility that Paige Brittain from Headsets, Inc. will be at Arlington, also. That's where I first met him a few years ago. For current information on their adapters and what they fit, I recommend calling Headsets, Inc. at: (806) 358-6336, Fax (806) 358-6449 Are they worth it? Yes, I reiterate, they are a good value. The difference between switch off and switch on is surprising, and they don't break the bank. Disclaimer: I don't work for Headsets, Inc., although I do accept hard currency in exchange for supplying and installing these ANR adapters for my friends and acquaintences. I'm not getting rich... Honest! I'm trying to build an RV-6! Apologies for being long-winded, Esteemed Keepers of the list. 73, Tom Glover ________________________________________________________________________________
Date: Jul 02, 1997
From: Blake Harral <bharral(at)mindspring.com>
Subject: Re: Why?
Dave Barnhart wrote: > > > Here's a question I've been wondering about. Why do we use different > relays for Master and Starter? Why not use another master relay as the > starter relay? > > Best Regards, > Dave Barnhart > rv-6 sn 23744 N601DB > engine being assembled by Lycon > Dave, I will probably regret posting this from home without first going to the hanger and inspecting Master and Starter Relays as supplied by Van's. I think the Master relay has both the relay contactor and the one side of the coil connected directly to the terminal labled 'BAT'. This allows activation of the master by simply grounding the control terminal. This is convenient, because without the Master relay on, where you gonna get 12V to energize the coil of a more conventional relay? I think the starter relay is more convential - i.e. apply 12V to the control terminal to close the contactors. Blake (corrections welcome - my relays are bolted on but not wired up yet) ________________________________________________________________________________
From: pbennett(at)zip.com.au
Date: Jul 02, 1997
Subject: Re: Why?
> But during starting, the current flow is thru the Master relay, then thru > the starter relay to the starter. So during starting, the master relay is > handling the same starting load as the starter relay. > > So I still don't understand. > > Best Regards, > Dave Barnhart The master relay and the starter contactor both CARRY the starter current, but the starter contactor has to BREAK it. To avoid destructive arcing as the contacts break the heavy current, the contactor has to open rapidly. Thus it has a heavy spring. Thus it needs a heavy coil current to pull it in. Thus it has a lower resistance coil than the master relay. In comparison, the master relay is called on to break only relatively light loads. To corroborate this, look at AC switch ratings. Much smaller contacts are used. They are adequate to CARRY the current. However when they BREAK the current, the arc extinguishes in less than 8.3 millisecs (60Hz) as the current drops to zero and reverses. No arc, no damage. Hope this sheds some light. Peter Bennett Sydney Australia RV6 building sliding canopy ________________________________________________________________________________
Date: Jul 02, 1997
From: Fran Malczynski <"Fran Malczynski"@ibm.net>
Subject: Re: Gall Strobe light Power Supply
aol.com!PhilipR920(at)matronics.com wrote: > > > I can't find anything in the archives related to Gall. > > Please furnish phone number. > > Phil Rogerson > 6AQ 60057 > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | I found Gall's in the archives using an apostrophe "s" in the search. Their number is 800-477-7766. Hope this helps. Fran Malczynski Olcott, NY RV6(A) Wings ________________________________________________________________________________
Date: Jul 02, 1997
From: RodWoodard <rodwoodard(at)mcione.com>
Subject: Security Warning?!?
Hello Listers: I just tried to browse the new www.vansaircraft.com website and received the following message: ============================ National Security Agency The network you are trying to download information from has received enough traffic as to pose a potential security risk to the country. Apparantly, the file you requested is in great demand. Please try again tomorrow. We are sorry for any inconvenience this may have caused. National Security Agency United States of America ============================= Is this for real? I've _never_ received any message like this before. If it is for real then I guess it's just a testament to the popularity of this list and Van's airplanes. It's pretty spooky though... I'm not sure I like the government in the business of controlling how many "hits" a web site can have. Big brother's watching! Rod Woodard Loveland, Colorado RV-8, #80033 ________________________________________________________________________________
From: "Doug Rozendaal" <dougr(at)netins.net>
Subject: Re: Why?
Date: May 27, 1997
The contacts on the master relay are made at that time. a switch of any kind can carry many multiples of the current it can "make" or start. To say it another way, there will be a big spark in the starter relay when you energize it but no spark in the master relay at all at that time because it is already "made". When you turn the master on there is very little current at all. Hope this helps... Tailwinds, RV-4 N240 Doug Rozendaal dougr(at)netins.net www.petroblend.com/dougr ---------- > From: Dave Barnhart <a.crl.com!barnhart(at)matronics.com> > To: rv-list(at)matronics.com > Subject: Re: RV-List: Why? > Date: Monday, June 30, 1997 3:35 PM > > > I asked: > > > Here's a question I've been wondering about. Why do we use different > > relays for Master and Starter? Why not use another master relay as the > > starter relay? > > "Doug Rozendaal" replied: > > >It has to do with contiuios vs intermittent duty cycle. The master relay > >is optimized for long duty cycles. The starter relay contacts are designed > >to accept the high starting loads of a starter. It would work but it would > >fail sooner if you used a master relay as a starter. > > But during starting, the current flow is thru the Master relay, then thru > the starter relay to the starter. So during starting, the master relay is > handling the same starting load as the starter relay. > > So I still don't understand. > > Best Regards, > Dave Barnhart > > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ ________________________________________________________________________________
Date: Jul 02, 1997
From: Gene Gottschalk <geneg(at)rattler.gsfc.nasa.gov>
Subject: Re: Van's New Web Site
Seems like someone has hacked the web site. I just tried to access the site and received the following msg: "500 Server Error The hard transfer limit for this user has been reached" Earlier when I tried to access it I received something about NSA and a security risk. What gives? -Gene Medema) > >Jeremy: > >I've looked at most of it and it is a BIG improvement. Thanks for >putting the complete optional parts catalog on line! > >Check it out folks! > >Doug Medema, RV-6A, skinning fuselage. > > >> From uofport.edu!jbenedic(at)matronics.com Tue Jul 1 16:18:21 1997 >> Date: Tue, 1 Jul 1997 12:29:43 -0700 (PDT) >> From: Jeremy William Benedict <uofport.edu!jbenedic(at)matronics.com> >> To: rv-list(at)matronics.com >> Subject: RV-List: Van's New Web Site >> Mime-Version: 1.0 >> >> >> >> Don't just read it >> >> EXPERIENCE IT >> >> www.vansaircraft.com >> >> July 1, 1997 >> >> >> >> >> +-- --+ >> | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | >> | --- | >> | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | >> | & put the word "[un]subscribe" in the *body*. No other text or subject. | >> +-- --+ > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
Date: Jul 02, 1997
From: Charlie Kuss <charliekuss(at)sprintmail.com>
Subject: Re: Oil Pressure Switch
Ronald Vandervort wrote: All the usual sources for oil pressure switches seem to have only the normally open switch. Where can one find a normally closed switch? I think a normally closed oil pressure switch hooked up to a buzzer would do well as a " master switch on" warning setup. Ron Vandervort, RV-6Q, working on instrument panel mockup. Seattle area Ron, Most automotive oil pressure switches are normally open. Quality is a big issue with using automotive oil pressure switches in your RV. The majority of auto oil pressure switches are comprised of a steel base and a composite (usually Bakelite) top piece. The two parts are crimped together with a gasket or o-ring to seal between them. It is not uncommon for this seal to fail on older/high mileage cars. This causes a serious (pressure fed) oil leak. The failures are often due to chafing of the gasket/o-ring because of different rates of thermal expansion of the dissimilar materials used in the two halves. The increased heat & vibration found in aircraft engine bays will only excerbate the problem. Look for an all steel oil pressure sending unit, preferably one used in a "police special", as these cars used higher quality components. I seem to remember Chrysler using all steel units in the 1970's. I would also check Mercedes Benz and BMW. Good luck, Charlie Kuss RV-8 H.S. ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jul 02, 1997
Subject: Re: Oil Pressure Switch
<< All the usual sources for oil pressure switches seem to have only the normally open switch. Where can one find a normally closed switch? I think a normally closed oil pressure switch hooked up to a buzzer would do well as a " master switch on" warning setup. >> Get one of the Datcon switches from Chief Aircraft. It is a SPDT type switch. See the Yeller Pages for ph#. -GV ________________________________________________________________________________
Date: Jul 02, 1997
From: "Scott M. Kuebler" <keebs(at)buffnet.net>
Subject: Clarence, NY fly-in (not RV related)
Hello fellow listers, My airport is having their annual fly-in on Saturday, July 12th. There will be food & drinks, EAA chapter 656 is also located at there. This is not an RV fly-in, but we do have two RV-6's being built at the airport. So the more RV's that show up the better it will be, I hope to be skinning my HS by then (starting the skeleton this weekend). For everybody interested I have included some airport information below, anybody needing driving directions can send me a personal E-mail. Hope to see some RV's there. Scott RV-6 (19 hrs. done - 1981 hrs. to go) _____________________________________________________________________ D51 - CLARENCE AERODROME AIRPORT BUFFALO, NY AIRPORT INFORMATION CURRENT AS OF 01/30/97 LOCATION Lat/Long: 43-04-00.208N / 078-40-59.109W (43.0667244/78.6830858) Elevation: 582 ft. / 177 m (estimated) Variation: 10W (1985) >From city: 5 miles NE of BUFFALO, NY County: ERIE AIRPORT OPERATIONS Sectional chart: DETROIT Control tower: no ARTCC: CLEVELAND CENTER FSS: BUFFALO FLIGHT SERVICE STATION [1-800-WX-BRIEF] Attendance: UNATNDD Segmented circle: no Airspace analysis: NO OBJECTION Lights: RDO-CTL ACTVT LIRL RY 10/28 - 122.7. Beacon: none Landing fee: no Airline operations: not certified under FAR Part 139 Int'l operations: not permitted AIRPORT COMMUNICATIONS UNICOM: 122.7 Radio aids to navigate to the Airport VOR radial/distance VOR name Freq Var BUFr357/8.4 BUFFALO VOR/DME 116.40 08W AIRPORT SERVICES Fuel available: 80 Airframe service: MAJOR Powerplant service: MAJOR RUNWAY INFORMATION Runway 10/28 Dimensions: 2000 x 75 ft. / 610 x 23 m Surface: turf, in unknown condition Runway edge lights: low intensity RUNWAY 10 RUNWAY 28 Traffic pattern: left left Displaced threshold: no no Touchdown point: no no OBSTRUCTIONS: PLINE TREES Marked: 1 Height: 10 ft. 35 ft. Slope to clear: 1:1 Distance from threshold:200 ft. 0 Additional obstruction remarks: PLINE 900' FM THR. ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: Jul 02, 1997
Subject: Moving RV6A
Tim, Sorry to return to the whole list but the direct mail was returned. The answer is yes leaving in the false spar will work fine. The airplane will ride fine on the gear. The 6A will just fit width wise in the Ryder 24' truck. You dont need the full length of the 24' truck but you do need the width. Wings will tie to the rails on the sides with straps and padding. For some reason even a direct reply to you is returned to me. Good luck. Ryan ________________________________________________________________________________
Subject: Re: Moving a partially complete RV-6A
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: Jul 02, 1997
>In a few months I'm probably going to have to move from San Antonio >TX to Washington D.C. (Pentagon assignment). I'm building a >quickbuild, and wondering about the best, safest way to move it. Tim, I recently moved my RV-4 project from Del Rio, TX to Oklahoma City. All the components were finished, but the airplane was not yet on the gear and had no engine. I strapped the fuselage down firmly on a cradle along one side of the largest Ryder truck (24', I think). I used ratcheting strap clamps and eyebolts screwed into the floor to hold the fuselage down. I rested both wings on a rolling dolly, leading edge down, tied to the side rails of the truck on the other side Flaps and ailerons were mounted and clamped immobile. The horizontal tail fit neatly in between on its own vertical cradle, screwed into the wooden floor. The vertical tail fit behind the fuselage, also in its own cradle, screwed to the floor. The crate from the finishing kit fit nicely in the space behind the wings. I screwed it to the floor and put fiberglass parts and other odds and ends inside it. The large wing crate fit behind the fuselage, screwed to the floor, and held tools and other heavy things I did not want bouncing around. I still had plenty of room left over for the air compressor and a few household items. The move was uneventful, no damage at all. That truck really bounced around on roads that I never thought bumpy in a car. Make sure that nothing can bounce into your airplane. In retrospect, I probably went overboard strapping everything down, but better that than the alternative! With your 6A, especially on the gear, I expect space will be more limited. I don't see a problem with setting it on the gear, as long as the fuselage cannot move around or bounce. My condolences on the Pentagon assignment. :-) Good luck, Tom Craig-Stearman tcraig-stearman(at)juno.com P.S. In reading my last post about the autopilot, it sounded more strident than I intended. I don't mean to cast aspersion on anyone who wants to install a wing leveler. One nice thing about a homebuilt is that we can put anything on the airplane that our hearts desire! The topic just hit one of my hot buttons. My apologies to Mr. Stucklen and all. ________________________________________________________________________________
From: cecilth(at)juno.com
Subject: Re: Oshkosh Table - Van's Banquet
<19970609.094312.15495.3.cecilth(at)juno.com>
Date: Jul 01, 1997
Oshkosh is only a few weeks away now, The following list is where we are at at this time. If you don't see your name, and thought you were on it, I didn't get the message, so send it again. Cecil Hatfield Tim Sweemer Donna Sweemer Jon Scholl Friend of Jon Scholl Jim Ayers Jim Cone Bev Cone Peter Hanna Les Rowles Les Rowles' Mate Joe Rex Zelda Gifford Bruce Knoll Ted French Jack French Louis Willig Marty Ssiler Barbara Sailer Ed Loveday Richard Reynolds The Banquet this year is Sunday evening starting at 6:30. Ticket cost $20.00 Order your tickets from Vans before July 28. There will only be about 300 tickets available so first come first served. In the past, those that order close to deadline can be picked up at Vans booth. Again this summer, I plan to reserve a table for all us listers that go to Van's Banquet, so we can get to know each other better. We ended up having several no shows, and I felt embarrassed when the place is sold out and here I'm holding some vacant spots. So this year I will strive to do better, by keeping the above sentence posted each time I show the list to date, about once each week. Thisyear we have about 300 more listers than last year, so I'm guessing we will have about 30 or so at our table. So we don't clutter the list, send your name and the number in your party to me at cecilth(at)juno.com Before July 29th (when I leave for mecca), keep me posted if I need to remove your name. Cecil Hatfield Plans No. 23581 working on the fuselage ________________________________________________________________________________
Date: Jul 02, 1997
From: Gene Gottschalk <geneg(at)rattler.gsfc.nasa.gov>
Subject: Re: Security Warning?!?
Your kidding, right? I think the site must have been hacked. First, NSA is not in the business of regulating the internet, second, it's hard for me to believe that Van's would generate more traffic than any number of other sites, take NASA for example! -Gene Gottschalk > >Hello Listers: > >I just tried to browse the new www.vansaircraft.com website and received >the following message: > >============================ >National Security Agency > >The network you are trying to download information from has received enough >traffic as to pose a potential security risk to the country. Apparantly, >the file you requested is in great demand. > >Please try again tomorrow. We are sorry for any inconvenience this may have >caused. > >National Security Agency >United States of America >============================= > >Is this for real? I've _never_ received any message like this before. If it >is for real then I guess it's just a testament to the popularity of this >list and Van's airplanes. It's pretty spooky though... I'm not sure I like >the government in the business of controlling how many "hits" a web site >can have. Big brother's watching! > >Rod Woodard >Loveland, Colorado >RV-8, #80033 > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
From: Keith Warfield <KeithW(at)ncgwpc.syntellect.com>
Subject: Why?
Date: Jul 02, 1997
Dave, The contact side of both the starter and master relay is the same (master may have different current rating).The "difference" is on the coil side of the relay (the part your master or starter switch is attached to with small gauge wire). The impedance of the coil determines how much current it draws. Current generates among other things, heat, and it has to go somewhere. The master relay coil is higher impedance, and therefore draws less current, and produces less heat, and lasts longer than a starter relay, which draws much more current, generates more heat, but physically has no better way to dissipate it than the master relay (same physical size and shape), which if used continuously, will shorten it's life. Keith Warfield RV-6A Emp./:( > ---------- > From: Dave Barnhart[SMTP:a.crl.com!barnhart(at)matronics.com] > Reply To: rv-list(at)matronics.com > Sent: Monday, June 30, 1997 1:35 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Why? > > > I asked: > > > Here's a question I've been wondering about. Why do we use > different > > relays for Master and Starter? Why not use another master relay as > the > > starter relay? > > "Doug Rozendaal" replied: > > >It has to do with contiuios vs intermittent duty cycle. The master > relay > >is optimized for long duty cycles. The starter relay contacts are > designed > >to accept the high starting loads of a starter. It would work but it > would > >fail sooner if you used a master relay as a starter. > > But during starting, the current flow is thru the Master relay, then > thru > the starter relay to the starter. So during starting, the master > relay is > handling the same starting load as the starter relay. > > So I still don't understand. > > Best Regards, > Dave Barnhart > > > > > > +-- > --+ > | Visit the Matronics & RV-List Web Sites at > http://www.matronics.com! | > | --- > | > | To [un]subscribe from the RV-List, email > "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or > subject. | > +-- > --+ > ________________________________________________________________________________
Date: Jul 02, 1997
From: Robert Acker <r.acker(at)ix.netcom.com>
Subject: Re: Security Warning?!?
>I just tried to browse the new www.vansaircraft.com website and received >the following message: > >============================ >National Security Agency... >Is this for real? I just got it too. Its got to be a hoax, did you notice the spelling errors? Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
From: vans(at)europa.com
Date: Jul 02, 1997
Subject: Oshkosh 97 Schedule
The following are the activities planned for Oshkosh. If you plan to attend, this will help you schedule your activities. We would especially like as many people to attend the gathering on Saturday evening as possible. OSHKOSH We continue to receive notes from RV pilots who plan to attend (too many to list) and our goal of 250 airplanes looks achievable -- there may even be more. We are planning a wild party in the RV aircraft parking area for Saturday evening about 7 p.m. There will be an open bar, live hard rock music, exotic dancers....yeah, sure. How about a "reception" with light refreshments, etc. We certainly hope that RVers can stay for this gathering - it may be the only real chance for factory personnel to meet customer/friends and see the airplanes. We need volunteers to man the hospitality tent in the RV parking area. Boy, do we need them, particularly in the morning hours Wednesday through Saturday. We have had some very attractive 25th Anniversary stickers made to present to those who fly in (suitable for vertical stabilizers, etc.) and we'd like to "register" arrivals by name and aircraft registration. This is your chance to meet a bunch of interesting people and get a first look at some fine airplanes. If you can volunteer a couple of hours, please contact Ken Scott at Van's. As a reminder, camping is not permitted in the RV showplane parking area, just as it wasn't in our parking area during previous years. We may be able to work out some camping arrangements, including setting up in Showplane Camping, a few hundred yards to the south. Details will be at the hospitality tent in the RV area. Camping fees and registration requirements will be the same as for any other airplane camping. The banquet will be at the Pioneer Inn Sunday, Aug. 3. Because of the limited seating and the high demand, we recommend you order your tickets early. Cut off date for orders from Van's is July 28. If there are any tickets left, they will be available first come first served at Van's Oshkosh booth. Forums are: RV-3/4/8; Saturday, Aug. 2 11:30 am-12:45 p.m. Tent 3. RV-6/6A Thursday, July 31, 10-11:15 am Tent 3. An added Oshkosh note: Please do not bring your technical or building questions to us in the booth. We are just not adequately equipped to give you good service in this area. Bill/Ken Bill Benedict G.M. ________________________________________________________________________________
From: Bob Japundza <Bjapundza@IIS-INTELLECT.COM>
Subject: Security Warning?!?
Date: Jul 02, 1997
charset="iso-8859-1" I'm sure the webserver Jeremy is using has a feature in it that will display a customizable message when the connection limit has been reached...and a dark sense of humor. Thanks, Bob Japundza Integrated Information Services, LLC bjapundza@iis-intellect.com -----Original Message----- From: RodWoodard [SMTP:mcione.com!rodwoodard(at)matronics.com] Sent: Wednesday, July 02, 1997 8:02 AM To: rv-list(at)matronics.com Subject: RV-List: Security Warning?!? Hello Listers: I just tried to browse the new www.vansaircraft.com website and received the following message: ============================ National Security Agency The network you are trying to download information from has received enough traffic as to pose a potential security risk to the country. Apparantly, the file you requested is in great demand. Please try again tomorrow. We are sorry for any inconvenience this may have caused. National Security Agency United States of America ============================= Is this for real? I've _never_ received any message like this before. If it is for real then I guess it's just a testament to the popularity of this list and Van's airplanes. It's pretty spooky though... I'm not sure I like the government in the business of controlling how many "hits" a web site can have. Big brother's watching! Rod Woodard Loveland, Colorado RV-8, #80033 +-- --+ | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | | --- | | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | | & put the word "[un]subscribe" in the *body*. No other text or subject. | +-- --+ ________________________________________________________________________________
Date: Jul 02, 1997
From: Tim Bronson <70773.2700(at)CompuServe.COM>
Subject: Home page
Hi Folks, I was the 561st hit since July 1st! Tim Bronson Pittsburgh ________________________________________________________________________________
Date: Jul 02, 1997
From: Don McNamara <mcnamara(at)sbt.infi.net>
Subject: Re: Security Warning?!?
RodWoodard wrote: > > > Hello Listers: > > I just tried to browse the new www.vansaircraft.com website and received > the following message: > > ============================ > National Security Agency > > The network you are trying to download information from has received enough > traffic as to pose a potential security risk to the country. Apparantly, > the file you requested is in great demand. > > Please try again tomorrow. We are sorry for any inconvenience this may have > caused. > > National Security Agency > United States of America > ============================= > > Is this for real? I've _never_ received any message like this before. If it > is for real then I guess it's just a testament to the popularity of this > list and Van's airplanes. It's pretty spooky though... I'm not sure I like > the government in the business of controlling how many "hits" a web site > can have. Big brother's watching! > > Rod Woodard > Loveland, Colorado > RV-8, #80033 > Rod-- Relax...Van's only displays that message to lawyers. ;) --Don McNamara ________________________________________________________________________________
Date: Jul 02, 1997
Date-Warning: Date header was inserted by InfoAve.Net
From: GIBBONSR.FTC-I.NET(at)InfoAve.Net (RB Gibbons)
Subject: Re: Security Warning?!?
I'm quite sure that this is an attempt at humor by Jeremy Benedict. > >Hello Listers: > >I just tried to browse the new www.vansaircraft.com website and received >the following message: > >============================ >National Security Agency > >The network you are trying to download information from has received enough >traffic as to pose a potential security risk to the country. Apparantly, >the file you requested is in great demand. > >Please try again tomorrow. We are sorry for any inconvenience this may have >caused. > >National Security Agency >United States of America >============================= > >Is this for real? I've _never_ received any message like this before. If it >is for real then I guess it's just a testament to the popularity of this >list and Van's airplanes. It's pretty spooky though... I'm not sure I like >the government in the business of controlling how many "hits" a web site >can have. Big brother's watching! > >Rod Woodard >Loveland, Colorado >RV-8, #80033 > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > ________________________________________________________________________________
Date: Jul 02, 1997
From: Jerry Springer <jsflyrv(at)ix.netcom.com>
Subject: Re: Security Warning?!?
RodWoodard wrote: > > > Hello Listers: > > I just tried to browse the new www.vansaircraft.com website and > received > the following message: > > ============================ > National Security Agency > > The network you are trying to download information from has received > enough > traffic as to pose a potential security risk to the country. > Apparantly, > the file you requested is in great demand. > > Please try again tomorrow. We are sorry for any inconvenience this may > have > caused. > > National Security Agency > United States of America > ============================= > > Is this for real? I've _never_ received any message like this before. > If it > is for real then I guess it's just a testament to the popularity of > this > list and Van's airplanes. It's pretty spooky though... I'm not sure I > like > the government in the business of controlling how many "hits" a web > site > can have. Big brother's watching! > > Rod Woodard > Loveland, Colorado > RV-8, #80033 > Try clicking on this, works for me. <http://www.vansaircraft.com> -- Jerry Springer RV-6 N906GS First flight July 14, 1989 :-) Hillsboro, OR jsflyrv(at)ix.netcom.com ________________________________________________________________________________
Date: Jul 03, 1997
From: Frank van der Hulst <frankv(at)pec.co.nz>
Subject: Re: Security Warning?!?
> >I just tried to browse the new www.vansaircraft.com website and > received > >the following message: > > > >============================ > >National Security Agency [snip]I helped with the beta-test on Sunday and had no problems accessing the site. But after reading Rod's message I just had to try again, and got the NSA message too. One thing I noticed is that this message is on the page http://www.vansaircraft.com/limits.html. My guess is that Van's ISP limits the amount of traffic allowed, and that the rush to see the new site and/or the added graphics has popped the relief valve. Benedict Jr's sense of humour is also not entirely blameless, I think. :-) NB: I've Cc'ed this to Jeremy so hopefully soon he'll tell us all what's going on. Frank. ________________________________________________________________________________
Date: Jul 02, 1997
From: Alan Carroll <carroll(at)geology.wisc.edu>
Subject: Re: Security Warning?!?
I got the same message - very bizarre. > >============================ >National Security Agency > >The network you are trying to download information from has received enough >traffic as to pose a potential security risk to the country. Apparantly, >the file you requested is in great demand. > >Please try again tomorrow. We are sorry for any inconvenience this may have >caused. > >National Security Agency >United States of America >============================= > >Is this for real? I've _never_ received any message like this before. If it >is for real then I guess it's just a testament to the popularity of this >list and Van's airplanes. It's pretty spooky though... I'm not sure I like >the government in the business of controlling how many "hits" a web site >can have. Big brother's watching! > Alan Carroll RV-8 #80177 (Empenage) ________________________________________________________________________________
Date: Jul 02, 1997
Subject: Re: Oil Pressure Switch
From: ebundy(at)juno.com (Ed Bundy)
>All the usual sources for oil pressure switches seem to have only the >normally open switch. Where can one find a normally closed switch? >I think a normally closed oil pressure switch hooked up to a buzzer >would do well as a " master switch on" warning setup. I couldn't find an oil pressure switch with two sets of contacts (NO & NC) as discussed previously on the list. However, I recently stumbled onto something by accident. I've been operating out of a short crushed gravel strip, and I've been using a rough field takeoff to get the prop above the gravel as soon as possible during takeoff (6A). Using one notch of flaps helps tremendously, but it's also very easy to get involved in the takeoff and forget to raise them in a timely manner. So I installed a microswitch at the manual flap handle wired to a red light in the panel. The light is off only when the flaps are fully retracted. This works great for the flaps, but as a side benefit, it also works as a master warning light. After landing, I always leave the flaps down to facilitate exit and subsequent re-entry. (and to keep some bozo from ignoring the "no step" decal and putting a size 11 hole in the flap) Thus, the light stays illuminated until I turn off the master switch. Sometimes things just seem to work out right... Ed Bundy RV6A - first flight 11/20/96 (100+ hours now!) ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
Date: Jul 02, 1997
From: Patrick Kelley <patk(at)mail.ic.net>
Subject: Re: Security Warning?!?
Robert Acker wrote: > > > >I just tried to browse the new www.vansaircraft.com website and received > >the following message: > > > >============================ > >National Security Agency... > >Is this for real? > > I just got it too. Its got to be a hoax, did you notice the spelling errors? > > Rob Acker / r.acker(at)ix.netcom.com / RV-6Q > At 3:24 pm Eastern, I accessed the Vans site via a LAN/T1 connection. Other than being slow (our provider, I think) there was no problem. Are you SURE you have the URL spelled right? PatK - RV-6A ________________________________________________________________________________
Date: Jul 02, 1997
From: Richard Bibb <rbibb(at)fore.com>
Subject: Carb manual needed
I need an overhaul manual for my Marvel carb on my O-320E2D. I have an overhaul kit but need the specs for float adjustment, etc. Anybody have the data? Is it on the Web someplace? ________________________________________________________________________________
Date: Jul 02, 1997
From: halk(at)sybase.com (Hal Kempthorne)
Subject: Re: Sliding Canopy Skirt Cap (Crass Commercialism)
Gary, I haven't a clue as to what this is so I want one. I can build an airplane but I will probably have $10 worth of struggle out of this. The description makes it sould like something for the Air Force for $10,000! I assume they are warranteed and come with complete instructions. You say they are formed for hydraulic? Do they come with fluid? How do I pay? I do want one just to see what it is. (Seriously!) Hal Kempthorne RV-6AQ -- Asking the usual customer dingy questions. halk(at)sybase.com Santa Clara, CA. Debonair N6134V @ SJC ________________________________________________________________________________
From: BigCfly001(at)aol.com
Date: Jul 02, 1997
Subject: R-410
My R-410 has a "cut here line" drawn on it.The manual says to "make a cardboard mock-up"Is this necassary?Is the line drawn on the R-410 accurate enough? Thanks in advance Chris Marion RV-6 finishing rudder cincy oh ________________________________________________________________________________
From: "Darrell L. Anderson" <d.l.anderson(at)worldnet.att.net>
Subject: ANR - off subject
Date: Jul 02, 1997
I take my time and try to avoid misteaks Thanks, you made my day! ;} ________________________________________________________________________________
From: colquitt(at)ns1.onramp.tuscaloosa.al.us
Date: Jul 02, 1997
Subject: Re: Paperwork
Several people have addressed a fatal crash: > **snip** > > > I know of one fatal accident in Jackson MI about 5 - 6 years > > ago > > that was caused by the wing of an RV 4 folding up. The fellow had > > purchased > > the planew within the preceeding year. > Are you sure that it was a RV-4? I have not heard of a -4 or -6 > looseing a wing. I once spoke to the son of a man who was killed in an RV-3 crash which I thought occurred under very similar circumstances - location, recent purchase, wing fold during aerobatics. I had written the fellow while looking for a good RV-3 and the son called me. That was an RV-3. It may or may not be the same incident. Joe Colquitt RV-3A - flying ________________________________________________________________________________
From: RVator(at)aol.com
Date: Jul 02, 1997
Subject: Re: Security Warning?!?
Rod; I think its some plastic builders idea of a joke. RVator ________________________________________________________________________________
Date: Jul 02, 1997
From: Thomas Velvick <rver(at)caljet.com>
Subject: Re: Oil Pressure Switch
Ed, Do you ever fly into some of the back mountain strips in Idaho? If so, how does your RV6A perform taking off and landing in that type of environment? Regards Tom Velvick rver(at)caljet.com >Ed Bundy RV6A - first flight 11/20/96 (100+ hours now!) >ebundy(at)juno.com - Eagle, ID > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > ________________________________________________________________________________
Date: Jul 02, 1997
From: Thomas Velvick <rver(at)caljet.com>
Subject: Re: R-410
I didn't make a cardboard mock-up and my 410 fitted ok; although a cardboard mock-up would probably help. If you have watched the new Orindorf empannage video, he shows attaching the R410 to the wrong side of the R405 so don't make that mistake. I read in the archives that the plans were wrong when he made the tape. Also, be sure you attach the K1000 plate nut to the R-405 "before" you put R404,R405,R606 together. > >My R-410 has a "cut here line" drawn on it.The manual says to "make a >cardboard mock-up"Is this necassary?Is the line drawn on the R-410 accurate >enough? >Thanks in advance > >Chris Marion >RV-6 finishing rudder >cincy oh > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > ________________________________________________________________________________
From: "Daniel H. Morris III" <Morristec(at)icdc.com>
Subject: Re: Oil Pressure Switch
Date: Jul 02, 1997
---------- Ron, Hobbs makes a suitable switch. The easiest way to get it is at a NAPA auto parts store. Ask for NAPA part number 7011578. The Hobbs p/n is 76062 the switch is normally closed and operates at 15 psi. It adjustable to operate between 4 to 20 PSI. I think that the switch cost about $10 or less. I use this switch for low oil pressure warning. If you need other specs I have them Email direct. Dan Morris Morristec(at)icdc.com > All the usual sources for oil pressure switches seem to have only the > normally open switch. Where can one find a normally closed switch? > > I think a normally closed oil pressure switch hooked up to a buzzer would > do well as a " master switch on" warning setup. > > Ron Vandervort, RV-6Q, working on instrument panel mockup. > Seattle area > > > > > > > > > > > > > > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com! | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ ________________________________________________________________________________
Date: Jul 02, 1997
From: wmills(at)southwind.net (William H. Mills)
Subject: EAA Chapter 88 Fly-In
Sorry for the late notice, but in case you're not aware of it and don't have any other big plans this weekend, EAA Chapter 88 is having their annual fly-in this weekend, July 4-6, at El Dorado, Kansas' Captain Jack Thomas Airport (EQA). El Dorado is about 30 miles east-northeast of Wichita, and the airport is about a mile or so south of town, just east of the main north-south highway into El Dorado from the south. Usually have quite a variety of aircraft there (and usually a bunch of RVs!!)...Friday night is a pot-luck for Chapter members and guests; Saturday night is a banquet in town. Usually a pretty good turnout of people and aircraft. Hope to see you there!! Bill Mills Wichita ________________________________________________________________________________
Date: Jul 02, 1997
From: "r.acker" <r.acker(at)ix.netcom.com>
Subject: Re: Security Warning?!?
>> I just got it too. Its got to be a hoax, did you notice the spelling errors? >> Rob Acker / r.acker(at)ix.netcom.com / RV-6Q >> >At 3:24 pm Eastern, I accessed the Vans site via a LAN/T1 connection. >Other than being slow (our provider, I think) there was no problem. Are >you SURE you have the URL spelled right? >PatK - RV-6A Yes Pat, quite sure. Spelling is one of my stroungist points. Besides, it was from my bookmarked URL list...only then did I try manually entering the URL. I'm wondering if only those using a common ISP, or maybe even POP (never can tell if someone hacked the RAS), got this message and were SOL for a bit? Rob Acker / r.acker(at)ix.netcom.com / RV-6Q ________________________________________________________________________________
From: Btinn(at)aol.com
Date: Jul 03, 1997
Subject: subscription
Suscribe ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jul 03, 1997
Subject: Re: Sliding Canopy Skirt Cap (Crass Commercialism)
<< I haven't a clue as to what this is so I want one. I can build an airplane but I will probably have $10 worth of struggle out of this. The description makes it sould like something for the Air Force for $10,000! I assume they are warranteed and come with complete instructions. You say they are formed for hydraulic? Do they come with fluid? How do I pay? I do want one just to see what it is. (Seriously!) >> Hal- What makes you think I want to sell you something you don't yet know whether or not you'll need? What kind of capitalist pig do you take me for? This is the joining piece for the top rear slider canopy skirt on the 6 and 6A. Send me $10 and you can have one too. No instructions are required as you will know intuitively how to install it when you get to that point. -GV ________________________________________________________________________________
From: cecilth(at)juno.com
Subject: Mars on 4th of July
Date: Jul 02, 1997
Brian and Lynne Cooper have a Quickbuild kit. This list has people from all walks of life and all over the world. Thought I would share we the list what one of our members is up to this week. Cecil Hatfield writes: > >Cecil, >Feel free to post this or pass it on - as long as the disclaimer >is at the bottom. Thanks very much for your interest! >--Lynne > >_______________________ Forward Header _______________________ > >Subject: Earth "Invades" Mars on 4th of July >Author: Lynne P Cooper >Date: 6/30/97 1:12 PM > >On July 4th, 1997 Earth Invades Mars! > >June 27, 1997 > >Dear Family, Friends, & Schoolmates, > >On July 4th, history will be made when the Mars Pathfinder >spacecraft lands on the surface of Mars and deploys the >first ever mobile robot on another planet. This incredibly >exciting event is all the more exciting to us because Brian >will be the first person ever to "drive" a vehicle on >another planet. We're both thrilled to be part of these >events (actually, Brian is part of them -- I'm just along >for the ride!) and want very much to share our excitement >with you! > >An incredible sequence of events leads up to the landing on >the surface of Mars. Pathfinder is currently on an >intercept course to Mars at a speed of ~15,000 mph. > >On July 4th at (Pacific Daylight Time): >9:32 AM the Pathfinder Lander lander separates from the > cruise stage. This is the capsule that has been > protecting the Lander from the environment of > Space during it's 7-month journey from Earth to > Mars. > >10:02 AM Pathfinder enters the upper atmosphere of Mars at > 16,6000 mph. Communications with the spacecraft > will be limited to listening to a very simple > signal from the spacecraft that will "sound" > differently to the folks on earth receiving it as > the spacecraft drastically reduces speed. > >During the next 4.5 minutes > - The spacecraft rapidly slows down in the > atmosphere using a heat shield to protect the > spacecraft from very high temperatures (remember > the old animations of the red hot temperatures > that the Apollo capsule encountered when > returning to Earth?) > - The Parachute deploys. It's a very large > parachute because the atmosphere on Mars is much > less than on Earth. > - The Heat shield separates, and the Lander (which > looks like a closed up flower bud) descends on a > bridle so that it is separated from the other > parts of the capsule. > - The Air Bags inflate. These air bags look a lot > like an inflated cluster of grapes (though they > aren't purple - just plain old off-white). They > completely enclose the spacecraft. At this > point, the whole thing looks like a really large > parachute supporting an empty shell which has a > long cord hanging out the bottom with a big > cluster of inflated air bags. If any Martians > are watching, they are bound to be amused! > - Rockets fire to decrease the speed of the > ensemble. The bridle cable is cut and the > cluster of airbags drops to the surface of Mars. > - It then bounces (maybe as high as a ten story > building), rolls, and eventually comes to rest > on the surface of Mars at approximately 10:07am. > >by 12:33PM The airbags deflate and are pulled up next to > the Lander petals. Then the petals open - like a > flower - exposing the Lander equipment and the > Sojourner Rover to Mars for the first time. > >2:00 PM The sun rises on Mars and the solar panels that > are on the inside of the petals begin collecting > energy to power the spacecraft (there are also > batteries) and the spacecraft is able to > communicate with Earth > >2:09 PM We receive the first pictures of the surface of > Mars and the actual landing site from Pathfinder. > >At this point, it's time for Brian and his co-workers to go >to work. The Sojourner Rover is "parked" on one of the >petals. The first big decision to make is whether/how to >deploy the ramps that enable the Rover to drive off of the >Lander. After they deploy the ramps, that's when "Robonaut" >Brian Cooper will drive the rover off of the lander and onto >the surface of Mars....and the rest is history! > >For Brian, this moment has been 12 years in the making -- >ever since he's come to the Jet Propulsion Laboratory (JPL), >he's been working on technology to enable this to happen. >It's almost impossible to explain how much this means to >him. During the 3-1/2 years, he's been working specifically >on Pathfinder and adapting work done for much bigger robotic >vehicles (and even an Army Humvee) to work with the Rover. >In less than a week, he'll have the opportunity to see the >results of his (and everyone else on the project's) efforts. > >The excitement for this day has really been building since >the launch of the spacecraft from Cape Canaveral in >December. The national and international media have been on >Lab talking to the Pathfinder folks -- and Brian has been >one of the busiest. He's been interviewed by CNN, the BBC, >CBS, Good Morning America, Discovery Channel, Nickelodean >News, MacNeil/Lehrer Report, KCET/PBS Huell Howser (already >aired in Los Angeles), Japan NHK, Newspapers from Orlando, >Germany, Orange County, and Washington State, USA Today, >Newsweek, US News & World Report, and others. (He's a >star!). > >He has also been involved with special school >projects with Cedarwood Elementary in Washington State (who >issued him the first official Martian Driver's License, just >recently signed by Vice President Al Gore), and Tampa Palms >Elementary School, Florida (who had him drive their rover >over the internet & sent him a whole package of Go Brian! >artwork which is displayed outside his office). Silicon >Graphics, the maker of the high-speed computers used to >drive the Rover, made a news brief (featuring Walter >Cronkite & "Robonaut" Brian Cooper!) that will be shown on >United Airlines flights during July. > >I sincerely hope that you can join in the excitement. For >more information, JPL has set up a great website that has >lots of information and pictures. The first photos will be >available through the web site really quickly and there will >be camera images which will include the Rover Control area >on the web. (http://www.jpl.nasa.gov/mars/). Also, I'm >planning to send out email bulletins sharing some of our >personal experiences. If you are interested - please send >me your email address (and any news you have!) to >lynne.p.cooper(at)jpl.nasa.gov. > >This is an experience of a lifetime for us and we really >want to share it with the people we care about. If you know >anything about Brian & me - it's that we really care about >space exploration, education, and, er....high tech toys! > >We look forward to hearing from you! > >--Lynne & Brian Cooper > >p.s. This is the "Cooper-centric" view of Pathfinder -There >are lots of people who are responsible for the success of >the mission and Brian is part of a much larger operations and >development team. (But since I'm the one writing this -- it's >given from my personal viewpoint! --L) > >--------------------- >Copyright 1997 Lynne P. Cooper (portions of the timeline >adapted from the Mars Pathfinder website) >The views expressed within are the personal views of the >author and do not reflect the views of NASA, JPL, or >Caltech. > ________________________________________________________________________________
Subject: Re: R-410
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: Jul 02, 1997
writes: > >My R-410 has a "cut here line" drawn on it.The manual says to "make a >cardboard mock-up"Is this necassary?Is the line drawn on the R-410 >accurate >enough? Chris, I recommend making the cardboard pattern first. The R-410 is a complex part that is difficult to envision from the plans (it was difficult for me, anyway.) If you bend up a cardboard model you can see how all the parts fit together. I don't remember whether I had to adjust the pattern, but I don't think I did. Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 on the gear, mounting brakes and wheel pants ________________________________________________________________________________
Date: Jul 03, 1997
From: Brian Eckstein <eckstein@net-link.net>
Subject: Re: Sliding Canopy Skirt Cap (Crass Commercialism)
aol.com!Vanremog(at)matronics.com wrote: > > I'm over a year away from needing that piece. Do you plan on making future production runs? Thanks Brian Eckstein 6A Wings ________________________________________________________________________________
Date: Jul 03, 1997
From: Brian Eckstein <eckstein@net-link.net>
Subject: Re: R-410
aol.com!BigCfly001(at)matronics.com wrote: > > > My R-410 has a "cut here line" drawn on it.The manual says to "make a > cardboard mock-up"Is this necassary?Is the line drawn on the R-410 accurate > enough? > Thanks in advance > > Chris Marion > RV-6 finishing rudder > cincy oh > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ It worked fine for me Brian Eckstein 6A ________________________________________________________________________________
Date: Jul 03, 1997
From: Sharlene Shipley or Bruce Knoll <snsbfk(at)mail.sage.net>
Subject: Re: Paperwork
To The List: I stand corrected. It was an RV3 at Jackson Mi. Jerry, who raised the first question, researched it, and found it was an RV3. Bruce knoll Hoping to start an RV6A after Oshkosh > >Several people have addressed a fatal crash: >> **snip** >> > >> I know of one fatal accident in Jackson MI about 5 - 6 years >> > ago >> > that was caused by the wing of an RV 4 folding up. The fellow had >> > purchased >> > the planew within the preceeding year. > >> Are you sure that it was a RV-4? I have not heard of a -4 or -6 >> looseing a wing. > >I once spoke to the son of a man who was killed in an RV-3 crash >which I thought occurred under very similar circumstances - location, >recent purchase, wing fold during aerobatics. I had written the >fellow while looking for a good RV-3 and the son called me. That was >an RV-3. It may or may not be the same incident. > >Joe Colquitt >RV-3A - flying > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > ________________________________________________________________________________
Date: Jul 03, 1997
From: "Scott A. Jordan" <SAJ_SLJ(at)compuserve.com>
Subject: Bending Brake
I am about to make a brake to bend my -8 rudder trailing edge. Looks lik= e a brake of just over 4' will work. Will this be sufficient for the futur= e (flaps, ailerons or other bends)? Thanks Scott 80331 N733JJ ________________________________________________________________________________
Date: Jul 03, 1997
From: Alan Carroll <carroll(at)geology.wisc.edu>
Subject: fuel gauge senders
This topic was discussed a couple of years ago, but I'm looking for an update on peoples experiences using capacitance-type fuel senders vs. the normal mechanical/resistance type. The advangtages of the capacitance type seem to be that they are simple (no moving parts), and poentially could provide more accurate readings over the whole tank volume? The resistance type, on the other hand, are much cheaper and more straightforward to install and calibrate? I view fuel gauges as primarily "leak detectors", so I'm not overly concerned with absolute accuracy. Fuel remaining is of course best calculated by conservative time estimates, supported by fuel flow readings if available. However, I do wonder if the mechanical arm of the resistance sender might fail and become an annoying maintainance problem - is there any history of this, or have they been generally reliable? Thanks in advance, Alan Carroll RV-8 #80177 (Empenage) ________________________________________________________________________________
Date: Jul 03, 1997
From: Don Mack <donmack(at)flash.net>
Subject: Re: Security Warning?!?
This is a multi-part message in MIME format. --------------7EA64FAAC0FBE7AC98DFD416 > > I just got it too. Its got to be a hoax, did you notice the > spelling errors? > > If there are spelling errors, it must be from the government Don Mack RV-6A Just crossed the 1000 hour mark, only 1000 more to go....... donmack(at)flash.net http://www.flash.net/~donmack --------------7EA64FAAC0FBE7AC98DFD416 begin: vcard fn: Don Mack n: Mack;Don email;internet: donmack(at)flash.net note: http://www.flash.net/~donmack end: vcard --------------7EA64FAAC0FBE7AC98DFD416-- ________________________________________________________________________________
Date: Jul 03, 1997
From: Chris Ruble <cruble(at)cisco.com>
Subject: Re: Security Warning?!?
Come on guys, this is a joke. Chris > > > >> I just got it too. Its got to be a hoax, did you notice the spelling errors? > >> Rob Acker / r.acker(at)ix.netcom.com / RV-6Q > >> > >At 3:24 pm Eastern, I accessed the Vans site via a LAN/T1 connection. > >Other than being slow (our provider, I think) there was no problem. Are > >you SURE you have the URL spelled right? > >PatK - RV-6A > > Yes Pat, quite sure. Spelling is one of my stroungist points. Besides, it > was from my bookmarked URL list...only then did I try manually entering the URL. > > I'm wondering if only those using a common ISP, or maybe even POP (never can > tell if someone hacked the RAS), got this message and were SOL for a bit? > > Rob Acker / r.acker(at)ix.netcom.com / RV-6Q > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > ________________________________________________________________________________
Date: Jul 03, 1997
From: Phil Arter <philip.arter(at)mci2000.com>
Subject: Re: Bending Brake
Scott A. Jordan wrote: > > > > I am about to make a brake to bend my -8 rudder trailing edge. Looks > like > a brake of just over 4' will work. Will this be sufficient for the > future > (flaps, ailerons or other bends)? > > Thanks > > Scott 80331 > N733JJ > Scott, hi I don't think that is long enough, the RV-8 ailerons are 54". The flaps are 61", but if I remember correctly they are pre-bent and don't require any further bending. -- Phil Arter, RV-8 #80005 philip.arter(at)mci2000.com http://acd.ucar.edu/~arter/RV8.html (303)459-0435 home ________________________________________________________________________________
Date: Jul 03, 1997
From: RodWoodard <rodwoodard(at)mcione.com>
Subject: Re: fuel gauge senders
> if available. However, I do wonder if the mechanical arm of the resistance > sender might fail and become an annoying maintainance problem - is there > any history of this, or have they been generally reliable? > > Thanks in advance, > > > > Alan Carroll > RV-8 #80177 (Empenage) Hi Alan: I have no experience with the type of float fuel senders that Van's sells, but my experience with the float-type senders on my Cherokee was poor. I eventually had to replace the float and the little arm the float attaches to in both the left and right tanks of the Cherokee. Of course, the plane _was_ 28 years old. The logs never showed any previous replacement, but I could imagine somebody replacing them without logging it too. I'm going to follow this thread closely because I'll need to make this decision soon (hopefully) on my -8. Best regards, Rod Woodard Loveland, Colorado RV-8, #80033 ________________________________________________________________________________
Date: Jul 03, 1997
Subject: Re: Static Wicks
From: wstucklen1(at)juno.com (Frederic w Stucklen)
Scott, After flying about 200 Hrs of IFR in my -6A, I've encountered static on only 3-4 occations. Once was because of the procimity of a rather large cell I could see, the other times just in very unstable air. I've been thinking about putting them on just to see if it will eliminate the problem enough to allow communications....... Fred Stucklen Rv-6A N925RV wstucklen1(at)juno.com writes: > > >I plan on equiping my RV-8 for IFR travel. In looking at other RV's, I >don't think I have ever seen static wicks on any. For those of you who fly >IFR, do you have static wicks installed? How have you decided where and how >many to install? If not, is static a problem with your com radios? > >I'm getting ready to close up my rudder and thought it might be good to put >the wicks on at that time. > > >Thanks for your help > >Scott >RV-8 >80331 >N733JJ > > > > +-- > --+ > | Visit the Matronics & RV-List Web Sites at >http://www.matronics.com! | > | --- > | > | To [un]subscribe from the RV-List, email >"rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or >subject. | > +-- > --+ > ________________________________________________________________________________
From: cecilth(at)juno.com
Subject: Re: Mars on 4th of July
Date: Jul 03, 1997
Brian and Lynne Cooper have a Quickbuild kit. This list has people from all walks of life and all over the world. Thought I would share we the list what one of our members is up to this week. Cecil Hatfield writes: > >Cecil, >Feel free to post this or pass it on - as long as the disclaimer >is at the bottom. Thanks very much for your interest! >--Lynne > >_______________________ Forward Header _______________________ > >Subject: Earth "Invades" Mars on 4th of July >Author: Lynne P Cooper >Date: 6/30/97 1:12 PM > >On July 4th, 1997 Earth Invades Mars! > >June 27, 1997 > >Dear Family, Friends, & Schoolmates, > >On July 4th, history will be made when the Mars Pathfinder >spacecraft lands on the surface of Mars and deploys the >first ever mobile robot on another planet. This incredibly >exciting event is all the more exciting to us because Brian >will be the first person ever to "drive" a vehicle on >another planet. We're both thrilled to be part of these >events (actually, Brian is part of them -- I'm just along >for the ride!) and want very much to share our excitement >with you! > >An incredible sequence of events leads up to the landing on >the surface of Mars. Pathfinder is currently on an >intercept course to Mars at a speed of ~15,000 mph. > >On July 4th at (Pacific Daylight Time): >9:32 AM the Pathfinder Lander lander separates from the > cruise stage. This is the capsule that has been > protecting the Lander from the environment of > Space during it's 7-month journey from Earth to > Mars. > >10:02 AM Pathfinder enters the upper atmosphere of Mars at > 16,6000 mph. Communications with the spacecraft > will be limited to listening to a very simple > signal from the spacecraft that will "sound" > differently to the folks on earth receiving it as > the spacecraft drastically reduces speed. > >During the next 4.5 minutes > - The spacecraft rapidly slows down in the > atmosphere using a heat shield to protect the > spacecraft from very high temperatures (remember > the old animations of the red hot temperatures > that the Apollo capsule encountered when > returning to Earth?) > - The Parachute deploys. It's a very large > parachute because the atmosphere on Mars is much > less than on Earth. > - The Heat shield separates, and the Lander (which > looks like a closed up flower bud) descends on a > bridle so that it is separated from the other > parts of the capsule. > - The Air Bags inflate. These air bags look a lot > like an inflated cluster of grapes (though they > aren't purple - just plain old off-white). They > completely enclose the spacecraft. At this > point, the whole thing looks like a really large > parachute supporting an empty shell which has a > long cord hanging out the bottom with a big > cluster of inflated air bags. If any Martians > are watching, they are bound to be amused! > - Rockets fire to decrease the speed of the > ensemble. The bridle cable is cut and the > cluster of airbags drops to the surface of Mars. > - It then bounces (maybe as high as a ten story > building), rolls, and eventually comes to rest > on the surface of Mars at approximately 10:07am. > >by 12:33PM The airbags deflate and are pulled up next to > the Lander petals. Then the petals open - like a > flower - exposing the Lander equipment and the > Sojourner Rover to Mars for the first time. > >2:00 PM The sun rises on Mars and the solar panels that > are on the inside of the petals begin collecting > energy to power the spacecraft (there are also > batteries) and the spacecraft is able to > communicate with Earth > >2:09 PM We receive the first pictures of the surface of > Mars and the actual landing site from Pathfinder. > >At this point, it's time for Brian and his co-workers to go >to work. The Sojourner Rover is "parked" on one of the >petals. The first big decision to make is whether/how to >deploy the ramps that enable the Rover to drive off of the >Lander. After they deploy the ramps, that's when "Robonaut" >Brian Cooper will drive the rover off of the lander and onto >the surface of Mars....and the rest is history! > >For Brian, this moment has been 12 years in the making -- >ever since he's come to the Jet Propulsion Laboratory (JPL), >he's been working on technology to enable this to happen. >It's almost impossible to explain how much this means to >him. During the 3-1/2 years, he's been working specifically >on Pathfinder and adapting work done for much bigger robotic >vehicles (and even an Army Humvee) to work with the Rover. >In less than a week, he'll have the opportunity to see the >results of his (and everyone else on the project's) efforts. > >The excitement for this day has really been building since >the launch of the spacecraft from Cape Canaveral in >December. The national and international media have been on >Lab talking to the Pathfinder folks -- and Brian has been >one of the busiest. He's been interviewed by CNN, the BBC, >CBS, Good Morning America, Discovery Channel, Nickelodean >News, MacNeil/Lehrer Report, KCET/PBS Huell Howser (already >aired in Los Angeles), Japan NHK, Newspapers from Orlando, >Germany, Orange County, and Washington State, USA Today, >Newsweek, US News & World Report, and others. (He's a >star!). > >He has also been involved with special school >projects with Cedarwood Elementary in Washington State (who >issued him the first official Martian Driver's License, just >recently signed by Vice President Al Gore), and Tampa Palms >Elementary School, Florida (who had him drive their rover >over the internet & sent him a whole package of Go Brian! >artwork which is displayed outside his office). Silicon >Graphics, the maker of the high-speed computers used to >drive the Rover, made a news brief (featuring Walter >Cronkite & "Robonaut" Brian Cooper!) that will be shown on >United Airlines flights during July. > >I sincerely hope that you can join in the excitement. For >more information, JPL has set up a great website that has >lots of information and pictures. The first photos will be >available through the web site really quickly and there will >be camera images which will include the Rover Control area >on the web. (http://www.jpl.nasa.gov/mars/). Also, I'm >planning to send out email bulletins sharing some of our >personal experiences. If you are interested - please send >me your email address (and any news you have!) to >lynne.p.cooper(at)jpl.nasa.gov. > >This is an experience of a lifetime for us and we really >want to share it with the people we care about. If you know >anything about Brian & me - it's that we really care about >space exploration, education, and, er....high tech toys! > >We look forward to hearing from you! > >--Lynne & Brian Cooper > >p.s. This is the "Cooper-centric" view of Pathfinder -There >are lots of people who are responsible for the success of >the mission and Brian is part of a much larger operations and >development team. (But since I'm the one writing this -- it's >given from my personal viewpoint! --L) > >--------------------- >Copyright 1997 Lynne P. Cooper (portions of the timeline >adapted from the Mars Pathfinder website) >The views expressed within are the personal views of the >author and do not reflect the views of NASA, JPL, or >Caltech. ________________________________________________________________________________
Date: Jul 03, 1997
From: mheaps(at)direct.ca (mike heaps)
Subject: Re: Security Warning?!?
Hello all, my plane is coming along great I have now started on my wings about 3 or 4 weeks ago and soon I will be working on my body I enjoyed all the wonderful tips you have gave me.I hope to continue this relationship I couldn't have done it without you.. Mike Heaps ________________________________________________________________________________
From: BigCfly001(at)aol.com
Date: Jul 03, 1997
Subject: Re: R-410
Tom, did you cut the mock-up per plans 7pp?I'm having a heck of a time figuring out what this should look like. thanks again chris marion RV-6 finishing rudder cincy oh ________________________________________________________________________________
From: teetime(at)konza.flinthills.com
Date: Jul 03, 1997
Subject: Tail Spring rod
Can anyone tell me how to get a drill bit through the tail spring rod? You know, that 1/4 in hole where it joins to the tail spring mount at the rear bulkhead for an RV4? I have ruined two bits, one being a cobalt high speed bit. Thanks in advance. Tim Sweemer RV4 skinning the fuselage ________________________________________________________________________________
From: "mcomeaux" <mcomeaux(at)cmc.net>
Subject: 6A quick build
Date: Jul 03, 1997
Does anyone have knowledge of a kit looking for new home that builder no longer wants to complete. ________________________________________________________________________________
From: N595CM(at)aol.com
Date: Jul 03, 1997
Subject: Re: Oil Pressure Switch
Ed, I connected a 12 volt N.O./N.C. automotive relay to my N.O. oil pressure switch to get what I wanted and that left one less oil line to run. Chris May RV-4 N595CM ________________________________________________________________________________
Date: Jul 03, 1997
From: Frank Smidler <smidler(at)dcwi.com>
Subject: Vans in Indy?
I heard that Van is going to be addressing the Indianapolis Aero Club on July 8th at Eagle Creek Airport. Maybe Bill Benedict can confirm this and give us a little more details. Frank Smidler ________________________________________________________________________________
Date: Jul 02, 1997
From: Dave Barnhart <barnhart(at)a.crl.com>
Subject: Re: Security Warning?!?
>============================ >National Security Agency > >The network you are trying to download information from has received enough >traffic as to pose a potential security risk to the country. Apparantly, >the file you requested is in great demand. > >Please try again tomorrow. We are sorry for any inconvenience this may have >caused. Having been in the crypto business and somewhat familiar with the NSA, I can assure you that this is bogus Best Regards, Dave Barnhart rv-6 sn 23744 N601DB ________________________________________________________________________________
Date: Jul 03, 1997
From: "Gregory S. Brewsaugh" <gregbrew(at)gte.net>
Subject: Re: Oops: HS-610
All, Thanks for the advice. Results were heavily in favor of re-doing. I re-did. Thanks again. Greg Brewsaugh RV-6A HS Skeleton (Lookin' like something!) ________________________________________________________________________________
Date: Jul 03, 1997
Subject: Re: Oil Pressure Switch
<19970702.103011.8910.0.ebundy(at)juno.com>
From: jepilot(at)juno.com (J E REHLER)
To Ed Bundy - -How about a description of your rough field take off and landing techniques. Do you have wheel pants? If so, how do they handle the unlevel surface. I would appreciate hearing of your experience using partial flaps on take off. Thanks. J. E. Rehler RV6A flying 75hours ________________________________________________________________________________
Date: Jul 03, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: Re: Tail Spring rod
Hi. I used a regular high speed steel bit on my tail spring. Worked very well with no problems. ________________________________________________________________________________
Date: Jul 03, 1997
From: lottmc(at)datastar.net (Michael C. Lott)
Subject: oil temp sender
I was going to hook up my oil temp sender (regular production type 2 in 1 gauge, oil temp and pressure) but the "bulb" would not seat in the housing. It would push straight through the hole as if it were too small for the hole. The nut fit properly. Is there supposed to be another fitting or piece in the housing that I am missing? This is an 0320-e2d, and I am trying to install it in the oil screen housing. Thanks for any advice. ________________________________________________________________________________
Subject: Wire routing thru main spar
Date: Jul 04, 1997
From: "Derrick L. Aubuchon" <n184da(at)cctrap.com>
I'm in the seemingly never-ending phase of wiring my RV-4 and I have a question, or perhaps more of a "survey." Where have most of you 4 builders routed the wire bundles through the main spar?? My original plan was just inboard of the fuselage skin, near an existing tooling-hole. My concern however is the size of the holes required,, which in my case, are fairly large because of my use of QD's. I am thinking I will require one hole on each side, one of which would have to be 1" dia, the other 1 1/4". Of course I am referring to the spar web and not interfering with any stiffeners, straps, etc. I have seen many different configurations including a few incorporating the setup I have already described, but the thought of removing ANY material from the main spar is rather scary to me :/ Thanks in advance,,, Derrick L. Aubuchon n184da(at)cctrap.com ________________________________________________________________________________
Date: Jul 04, 1997
From: catbird(at)taylortel.com (TTC Carroll A. Bird)
Subject: Re: Tail Spring rod
konza.flinthills.com!teetime(at)matronics.com wrote: > > > Can anyone tell me how to get a drill bit through the tail spring rod? You > know, that 1/4 in hole where it joins to the tail spring mount at the rear > bulkhead for an RV4? > I have ruined two bits, one being a cobalt high speed bit. > Thanks in advance. > > Tim Sweemer > > RV4 skinning the fuselage > Tim: I drilled mine on a drillpress. I first drilled a #30 hole, then followed it with a 1/4" bit. They were the bits that I bought from Avery Tool. You have to keep then lubricated. I used Marvel Mystery Oil. The secret to drilling these holes is to keep the bit cutting. If you ever let it spin in the hole, it will burn up very fast. Carroll, Hung engine 7-1-97. RV-4 ________________________________________________________________________________
Date: Jul 04, 1997
From: Craig Hiers <CRAIG-RV-4.@worldnet.att.net>
Subject: Re: Tail Spring rod
konza.flinthills.com!teetime(at)matronics.com wrote: > > > Can anyone tell me how to get a drill bit through the tail spring rod? You > know, that 1/4 in hole where it joins to the tail spring mount at the rear > bulkhead for an RV4? > I have ruined two bits, one being a cobalt high speed bit. > Thanks in advance. > > Tim Sweemer > Tim I drilled mine in steps, starting with a #40 then a #30, 3/16 and the final 1/4. I also used the the vice that mounts to the drill press table to hold it real steady. Use plenty of cutting oil, and turn the bit very slow. Craig Hiers RV-4 N143CH ________________________________________________________________________________
Date: Jul 04, 1997
From: Bob Skinner <BSkinner(at)navix.net>
Subject: Re: Tail Spring rod
>Can anyone tell me how to get a drill bit through the tail spring rod? You >know, that 1/4 in hole where it joins to the tail spring mount at the rear >bulkhead for an RV4? >I have ruined two bits, one being a cobalt high speed bit. >Tim Sweemer Tim, The trick is to turn the bit very slowly and apply a lot of pressure. 50 to 100 rpms would be great. If your weldment is not installed and you can jig the unit up in a slow turning drill press, this would be ideal. Cutting fluid will help but not if you're turning the bit at the speed of light. Our most recent drilling adventure was the gear legs on the Glastar. We drilled them with regular, high speed bits, nothing fancy and used a cordless drill ( a pretty hefty cordless drill.) It still takes time and is a lot of work but if you turn the bit slowly, you'll get the job done. You may want to pilot drill with something smaller than the 1/4" as you will get a better bolt fit. I think a #30 bit is a little small and may tend to wander. I think we used a #19 but can't remember for sure. Also, I drilled undersize and reamed to .2470 as a 1/4" bolt isn't really 1/4". By the way, you want to follow the same procedure when drilling stainless---a slow cutting speed. I don't use cutting fluid on stainless. I usually punch through with a #40 or 30 bit and then go to final size. Also, a handy way to deburr stainless is to chuck your debur tool in a slow turning drill (I use a Makita cordless). For the firewall flanges, I put the deburring bit in a right angle drill and chuck it up in the Makita. This method is much faster and does a better job than trying to use the dog leg crank and doing the job by hand. Bob Skinner RV-6 BSkinner(at)navix.net ________________________________________________________________________________
Date: Jul 04, 1997
From: Todd <tmrv6(at)pop.erols.com>
Subject: Re: Tail Spring rod
Tim, Low RPM, lots of pressure and lots of oil. -- Todd tmrv6(at)erols.com RV-6 N92TM Flying > > > Can anyone tell me how to get a drill bit through the tail spring rod? > > Tim Sweemer > > RV4 skinning the fuselage > --- ________________________________________________________________________________
Date: Jul 04, 1997
From: Finn Lassen <finnlass(at)ix.netcom.com>
Subject: Re: 6A quick build
Check *Kitplanes*: RV-6: 360-794-6036, 76525.1227(at)Compuserve.com mcomeaux wrote: > > > Does anyone have knowledge of a kit looking for new home that builder no > longer wants to complete. ________________________________________________________________________________
Date: Jul 04, 1997
From: Finn Lassen <finnlass(at)ix.netcom.com>
Subject: Re: Wire routing thru main spar
It would seem that one big hole in the center of the fuselage (half in each spar web) would cause the least structual weakening. Derrick L. Aubuchon wrote: > Where have most of you 4 builders routed the wire bundles through the > main spar? ________________________________________________________________________________
Date: Jul 04, 1997
From: Finn Lassen <finnlass(at)ix.netcom.com>
Subject: Re: Tail Spring rod
Tim, First use a small bit (e.g. 3/32" or smaller, then a bit larger, maybe 1/8" then 3/16" and finally 1/4". Note that the bit gets bigger you need to use lower RPMs. When enlarging a hole, use even lower RPMs. > Can anyone tell me how to get a drill bit through the tail spring rod? You ________________________________________________________________________________
Date: Jul 04, 1997
From: Finn Lassen <finnlass(at)ix.netcom.com>
Subject: Re: Tail Spring rod
Tim, If you have hardened the metal by spinning the bit too fast (or overheating by not using "lubrication"), I've found that a couple of taps with a center-punch will break through the hardened layer at the bottom of the hole being drilled and let you continue drilling. TTC Carroll A. Bird wrote: > You have to keep then lubricated. I used Marvel Mystery Oil. The > secret to drilling these holes is to keep the bit cutting. If you ever > let it spin in the hole, it will burn up very fast. ________________________________________________________________________________
Date: Jul 04, 1997
From: "Scott A. Jordan" <SAJ_SLJ(at)compuserve.com>
Subject: Re: Oops: HS-610
>>Greg Brewsaugh >>RV-6A HS Skeleton (Lookin' like something!) Greg, The more it looks like an airplane, the more fun it becomes! That first completed part is a real upper. :-) Scott A. Jordan 80331 N733JJ Rudder almost complete ________________________________________________________________________________
Date: Jul 04, 1997
From: William Costello <bcos(at)ix.netcom.com>
Subject: Re: Bending Brake
Scott A. Jordan wrote: > > > I am about to make a brake to bend my -8 rudder trailing edge. Looks like > a brake of just over 4' will work. Will this be sufficient for the future > (flaps, ailerons or other bends)? > > Thanks > > Scott 80331 > N733JJ I used cedar 2 X 4 X 6ft, with 4 good hinges. Faced the metal contacting surfaces with 2 layers of duct tape placed and smoothed very carefully. Worked fine for me. Haven't done the flaps and ailerons yet, but I didn't want to be cut short. Come to think of it, I bought the lumber from a yard that had a planer and had the faces planed very smooth and accurately. Didn't want to put any waves in that weren't there already. Didn't cost me very much. My 2 cents worth for your consideration. Bill Costello Bill Costello | bcos(at)ix.netcom.com | Building RV-6 | Reserv N97WC Want an extra hour and a half of energy per day with Super Blue Green products? Email for info or call 800-325-7544 Chicago ________________________________________________________________________________
Date: Jul 04, 1997
From: Edward Cole <emcole(at)concentric.net>
Subject: Instruments
I'm beginning to think about purchasing flight instruments for my RV6A and would like to hear all opinions from the list as to what brands are preferred. In addition to what Van's carries in his accessory catalog, what does everyone like? I'll be installing a vacuum system so all the gyro's don't have to be electric. Please comment on the "basic 6." Respond directly to me unless you think the rest of the list will find the info usefull. Thanks. Ed Cole RV6A emcole(at)concentric.net ________________________________________________________________________________
Date: Jul 04, 1997
From: "Larry Bowen" <lcbowen(at)msn.com>
Subject: 6A quick build
BR Smith may still have an RV-4 kit he has to part with. He's near Chattanooga, TN. Contact at brsmith(at)voyageronline.net Larry lcbowen(at)msn.com Dreaming of building an RV-8 -----Original Message----- From: owner-rv-list(at)matronics.com On Behalf Of mcomeaux Sent: Thursday, July 03, 1997 9:54 PM Subject: RV-List: 6A quick build Does anyone have knowledge of a kit looking for new home that builder no longer wants to complete. ________________________________________________________________________________
From: AtkRWC(at)aol.com
Date: Jul 04, 1997
Subject: Re: Van's New Web Site
I was on Van's Web Site last night and all seemed inorder. Who knows what is up??? Could be the Aliens messing with us again! ;-) Happy 4th to all! Richard Clayton Brownsville, Tx ________________________________________________________________________________
From: JDaniel343(at)aol.com
Date: Jul 04, 1997
Subject: Pnuematic Rivet Squeezer
Hi, I recently purchased a used pnuematic rivet squeezer from Bill Wiliams Tool Company. I have heard over the rv-list that his equipment is usually good. The squeezer I purchased will not set even the smallest rivets that come with the RV-6 empanage kit. I called Bill Wiliams Tool Company and they said to send it back and they would credit me. I have a 5hp compressor and am using 125 psi. Ive taken the squeezer apart and cleaned,oiled, ect to see if anything was broken. Everything appears to be ok, but just won't develope enough pressure to set rivets. Is there something I am missing? It does to leak a small amount of air where the pin activates the plunger during operation. Any help would be appreciated. I know I can send it back but they don't have a replacement they can send me at this time. Thanks jdaniel343(at)aol.com Member of Minnesota Wing of Vans ________________________________________________________________________________
From: "Austin Tinckler" <tinckler(at)axionet.com>
Subject: Re: Tail Spring rod
Date: Jul 04, 1997
---------- > From: konza.flinthills.com!teetime(at)matronics.com > To: rv-list(at)matronics.com > Subject: RV-List: Tail Spring rod > Date: Thursday, July 03, 1997 6:43 PM > > > Can anyone tell me how to get a drill bit through the tail spring rod? You may have work-hardened the drill hole surface, but I would try again using a cobalt bit and some Boelube or bee's wax or some good lube, drill slowly using progressively larger bit diameters. ________________________________________________________________________________
Subject: Re: Wire routing thru main spar
Date: Jul 04, 1997
From: "Derrick L. Aubuchon" <n184da(at)cctrap.com>
On an RV4, that won't work as that's where the control torque tube passes through. But I do agree that closer to the center results in less weakening,, however as you move towards the center in the 4, other structural members like floor ribs, complicate such a routing. Finn Lassen responded: >It would seem that one big hole in the center of the fuselage (half in >each spar web) would cause the least structual weakening. Derrick L. Aubuchon n184da(at)cctrap.com ________________________________________________________________________________
From: RV4131rb(at)aol.com
Date: Jul 04, 1997
Subject: Re: Tail Spring rod
Tim, High pressure, slow speed and lots of lubrication while drilling. If done properly the bit will cut through like butter. (ok not butter but quite easily). Ryan ________________________________________________________________________________
Date: Jul 04, 1997
From: Don Mack <donmack(at)flash.net>
Subject: Triming of F604 for control sticks
I am working on the fuse skeleton for RV-6a. I know that I have to trim away part of the top F604 bulkhead flange to allow for the control stick movement. Is that better to do now when I can easily make the cuts or wait until I can determine the amount of stick movement required? Don Mack donmack(at)flash.net http://www.flash.net/~donmack/ ________________________________________________________________________________
Date: Jul 04, 1997
From: Rick and Barbara Osgood <randbosgood(at)SprintMail.com>
Subject: Scanned image for RV6
Hello all.... I scanned the RV6 image from Van's manual and thought others may want a copy as well. You can use this for getting basic ideas for painting. This file is in a .jpg format and I am using Paint Shop Pro to play with the colors. If you want a copy of this file send me your e-mail address off list. Happy 4th!! -- Rick and Barbara Osgood RandBOsgood(at)sprintmail.com ________________________________________________________________________________
Date: Jul 04, 1997
From: Edward Cole <emcole(at)concentric.net>
Subject: Re: Pnuematic Rivet Squeezer
aol.com!JDaniel343(at)matronics.com wrote: > > > Hi, > I recently purchased a used pnuematic rivet squeezer from Bill Wiliams Tool > Company. > I have heard over the rv-list that his equipment is usually good. > The squeezer I purchased will not set even the smallest rivets that come with > the RV-6 empanage kit. > I called Bill Wiliams Tool Company and they said to send it back and they > would credit me. > I have a 5hp compressor and am using 125 psi. Ive taken the squeezer apart > and cleaned,oiled, > ect to see if anything was broken. Everything appears to be ok, but just > won't develope enough pressure to set rivets. > Is there something I am missing? It does to leak a small amount of air where > the pin activates the plunger during operation. > Any help would be appreciated. I know I can send it back but they don't have > a replacement they can send me at this time. > Thanks > jdaniel343(at)aol.com > Member of Minnesota Wing of Vans > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ JD, I don't know how you are using you squeezer, but the power is at the end of the stroke. Make sure you use a small rivit set on the stationary part of the yoke to allow the piston it's fullest extension. I found mine has a problem squeezing real long rivits (-7's) but for the most part works great. I was given this advice by Jerry ? at Action Air Parts where I bought it. Good luck! If you do return it, you may want to contact Action Air Parts as I and a couple of friends have had good luck with them. Ed Cole RV6A (2nd wing 1/2 way done!) emcole(at)concentric.net ________________________________________________________________________________
Date: Jul 04, 1997
From: Glenn & Judi <flyers@anet-chi.com>
Subject: rv-6 elec trim & inst panel
Hi, I just ordered a manual trim wheel for my RV-6 from a company called Aerofab. They also make vibration isolated panel for the RV aircraft. Here is some info about their products. They have their own web site you can check out as well. -Glenn Gordon RV-6, tail going on. ********************************************************************** Aerofab 10950 256th st. Chisago City, Mn. 55013 Dear RV builders, Aerofab is a company devoted to providing quailty products and services to aircraft builders/owners, specilizing in RV's. We have designed an alternate trim control for the rv aircraft that allows for easier operation that indicates trim tab settings. The trim control box we designed shows you were your trim tab is set to for take-off position and in flight. This control will also work on other experimental aircraft as well. Our company has also designed instrument panels both for ifr and vfr operation. These panels are designed for easy replacement of instruments when need be with out removing the instrument panel itself or hard to reach places. These panels also come with and without subpanels. Vibration isolators are incorporated in the panels that have subplanels to protect instruments from vibration which extends out less then 1/8". We believe that the panel is a very important part of the completion of your aircraft on only for appearance but also for safety. For more detailed information on our company and products, visit our web site at http://members.aol.com/aerofab or E-mail us at aerofab@aol.com or fax at 612-257-8642. ________________________________________________________________________________
From: joehine(at)nbnet.nb.ca (joehine)
Subject: Re: Wire routing thru main spar
Date: Jul 04, 1997
> >Derrick L. Aubuchon wrote: >> Where have most of you 4 builders routed the wire bundles through the >> main spar? > > I didn't route any through the spar, I send them down the right side from a switch and breaker panel I also made on the side of the cockpit by my right knee. the wire bundle is covered up with the panels that you make with George and Beckys interior panel kit. Wires that need to go under the floor and out to the wings go down to the floor and under it from the triangular area under the roll bar which is also covered by a panel. Joe C-FYTQ RV4 - at the airport, all assembled, engine runs, final inspection tuesday the eighth, becoming apprihensive about first flight. joehine(at)nbnet.nb.ca 13 James St. 506-452-1072 Home Douglas, NB 506-452-3495 Work Canada, E3A 7Z2 ________________________________________________________________________________
From: Mlfred(at)aol.com
Date: Jul 04, 1997
Subject: Re: Wire routing thru main spar
<< Where have most of you 4 builders routed the wire bundles through the main spar?? My original plan was just inboard of the fuselage skin, near an existing tooling-hole. My concern however is the size of the holes >> We run our wires thru the same hole used by the torque tube (including a #4 battery cable). Be sure to make allowances for anti-chafe, as the edges here could be unfriendly to your wiring! Secondly: Van makes allowances for a heat tube (2"dia) thru the spar, so don't worry about cutting a hole- just be sure to de-burr & smooth the thing! Use liberal amounts of anti-chafe here, also. All wires run thru this hole will have to be disconnected if a wing is pulled for any reason, BTW. Check six! Mark ________________________________________________________________________________
From: BrooksRV6(at)webtv.net (Chris Brooks)
Date: Jul 04, 1997
Subject: Re: Pnuematic Rivet Squeezer
Are you using the correct length rivet sets? The squeezer developes most of it's force at the end of it's travel. If you use sets that are to thick, the squeezer will appear powerless. You use different sets and shims to adjust for different length rivets. Chris Brooks BrooksRV6(at)webtv.net Fuselage in jig ________________________________________________________________________________
From: JHeadric(at)aol.com
Date: Jul 04, 1997
Subject: Re: oil temp sender
There is an adapter that fits in the housing, then the temp bulb screws into that. Good luck, Jim H. ________________________________________________________________________________
Date: Jul 03, 1997
From: Thomas Velvick <rver(at)caljet.com>
Subject: Re: R-410
Hi Chris, I sure did, at least I think so. If you look at the plans on 7PP and look at the R-410 drawing at the bottom of the page. The two cut-out wings will be bent 90 degrees up towards you. (my piece came prebent, I just had to cutout the outline). The large tab on the left side is bent up towards you 44 degrees or just about half way vertical. The smaller tab on the right is bent down away from you 32 degrees. I watched the empannage video, so it was easy to see how it should look. I think a cardboard cutout(or even a quick paper cutout) would be a great idea so you can see how it should turn out. Do you have the rest of your rudder skeleton done? Regards Tom Velvick rver(at)caljet.com RV-6A elevator > >Tom, did you cut the mock-up per plans 7pp?I'm having a heck of a time >figuring out what this should look like. >thanks again >chris marion >RV-6 finishing rudder >cincy oh > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > ________________________________________________________________________________
Date: Jul 04, 1997
From: cliffd(at)mailhost.accesscom.net (Cliff Dominey)
Subject: Chevy V6 R6A kits
Greetings Listers - My apologies if I missed a thread, but I do believe the June issue of Kitplanes has come and gone, and no one here had a comment on the V6 engine kit for the 6A that was discussed in that issue. As a mere 8AQB wannabe, this is not quite my cup of tea, but getting real close. Is anybody out there looking at this? Sounds really interesting. BTW - my compliments also to Tom Martin for the fairy tale dead stick. Maybe this is a chance to make a plug for sailplane training. When things up front get really quiet, and all you hear is the sound of that wind rushing by, at least it wouldn't be for the first time. Cliff Dominey cliffd(at)mailhost.accesscom.net garage workshop (and house) acquired, collecting tools, waiting for Van ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jul 04, 1997
Subject: Re: Instruments
<< I'm beginning to think about purchasing flight instruments for my RV6A and would like to hear all opinions from the list as to what brands are preferred. In addition to what Van's carries in his accessory catalog, what does everyone like? I'll be installing a vacuum system so all the gyro's don't have to be electric. Please comment on the "basic 6." Respond directly to me unless you think the rest of the list will find the info useful >> Ed- Go with Sigmatek or RC Allen for the gyros (not IFR) based on gyro tech info. Put a Navaid A/P in for the T/C. If you want the capabilities and don't mind that it's electrically powered go with the Rkymtn uEncoder or just get the Altimeter, VSI (3000ft+/-) and ASI from Van's. If you do aerobatics get an Accel from Van's. -GV ________________________________________________________________________________
From: colquitt(at)ns1.onramp.tuscaloosa.al.us
Date: Jul 04, 1997
Subject: Operating Pnuematic Rivet Squeezers
Someone wrote asking for info on why their pneumatic squeezer won't operate. I speak from experience. A year of on-again-and-off-again operations until I found someone who gave me the answer! My works great - NOW! > I recently purchased a used pnuematic rivet squeezer * * * I can see this one coming! ;-) It sounds oooh so familiar. > The squeezer I purchased will not set even the smallest rivets* * * As the man on the phone told me, I bet I know what your problem is . . . ;-) Mine would, then wouldn't. > I have a 5hp compressor and am using 125 psi.*** That's plenty. In fact, too much. 90 psi is plenty. > Everything appears to be ok, And it probably is. > but just won't develope enough pressure to set rivets. Is there something I am missing? It's not the pressure. In *all likelihood* it's the way it's been set up. > It does to leak a small amount of air where the pin activates the plunger during operation. Most of the ones I've seen do. Now, are you ready to try this?: A pneumatic squeezer doesn't need *strength* (read that - mucho air pressure) to squeeze. It needs ROOM. It seems that most of us who haven't been around these jewels simply don't know how they operate. The last 3/16" or so of the travel does the squeezing. It 's a leverage thing. Until the squeezer gets to that point, it's really weak. Strong enough for finger mashing, but not a whole lot more. I suggest that you try this: Look at the two rivet squeezer sets you put in your jaws (one on each side of the jaw). Easily squeeze the trigger. Let the squeezer close. Do the sets touch? Or do they even almost touch? If so, remove them. Put in only long enough rivet squeezer sets that *when the squeezer is activated and the plunger is fully closed* close to the length desired of the rivet after it is squeezed. I really don't know how to describe this better, but think of this: When the squeezer is fully closed, there still should be a gap between the two rivet squeezer sets. The gap should equal the desired length of the rivet after it is squeezed. The gap should be *no more* or *no less* that the desired length of the rivet *after* squeezing. If the plunger closes on the rivet *before* the last 3/16" or so of travel, it will just "bump" the rivet and stop. Even a 3/16" (#3) rivet will stop the squeezer. Yet if the plunger only makes contact with the rivet in its last little bit of travel - instant butter. The rivet is squeezed. I changed my sets and instant remedy!!!!! Works great. xxxxxxxxxxxxxx xxxxxxxxxxxxxxx xxxxx xxxxxx xxxxxx xxxxxx xxxxxx xxxxxx xxxxxxxx xxxxxxx xxxxxxxx xxxxxxxxx xxxxxxxx xxxxxxxxx xxxxxxxxxxxxxxxx xxxxxxxxxxxxxxxxxxxxxx TOO LONG JUST RIGHT Joe Colquitt Flying RV-3A (GlaStar on gear) ________________________________________________________________________________
Date: Jul 04, 1997
From: George McNutt <GMcNutt(at)compuserve.com>
Subject: RUDDER HORN
Does anyone have any suggestions for riveting the R-410 to the R-605PP rudder horn. The brace forms a little boxed in area and none of my buckin= g bars or 3" squeezer will fit in to set the center two rivets. Will go to the junkyard tomorrow to find some steel for a smaller bucking= bar, but in the meantime thought someone may have a good idea. Thanks George McNutt - 6A Rudder Langley B.C. = ________________________________________________________________________________
From: DLeihy(at)aol.com
Date: Jul 04, 1997
Subject: RV6A FUSELAGE JIG FOR SALE
Good wood jig, used twice. Available in Northern California (Paradise, California) $200. Call Doug Leihy (916) 876 1234, or Email dleihy(at)aol.com. ________________________________________________________________________________
Date: Jul 04, 1997
From: Thomas Velvick <rver(at)caljet.com>
Subject: Re: RUDDER HORN
Sounds like a good place for 2 pop rivets. Regards Tom Velvick rver(at)caljet.com RV-6A - elevator > >Does anyone have any suggestions for riveting the R-410 to the R-605PP >rudder horn. The brace forms a little boxed in area and none of my bucking >bars or 3" squeezer will fit in to set the center two rivets. > >Will go to the junkyard tomorrow to find some steel for a smaller bucking >bar, but in the meantime thought someone may have a good idea. > >Thanks >George McNutt - 6A Rudder >Langley B.C. > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > ________________________________________________________________________________
Date: Jul 04, 1997
From: Thomas Velvick <rver(at)caljet.com>
Subject: Re: RUDDER HORN
>Does anyone have any suggestions for riveting the R-410 to the R-605PP >rudder horn. The brace forms a little boxed in area and none of my bucking >bars or 3" squeezer will fit in to set the center two rivets. > >Will go to the junkyard tomorrow to find some steel for a smaller bucking >bar, but in the meantime thought someone may have a good idea. George, I just looked at my R-410 assembly again. If you have cut the 2 1/8 inch lightening hole in it, you could probably set the rivets with the Avery longeron yoke for the Avery hand squeezer. Dave Barnhart was good enough to set an couple of rivets for me using his longeron yoke on the rudder horn when I had the same problem. Dave recommended getting the longeron yoke as there are a lot of areas with similar access problems coming up as well. ________________________________________________________________________________
Date: Jul 05, 1997
Subject: Re: Chevy V6 R6A kits
From: wstucklen1(at)juno.com (Frederic w Stucklen)
Cliff, I'm currently building a second -6a that I plan on powering with the Chevy engine... Fred Stucklen RV-6A N925RV wstucklen1(at)juno.com mailhost.accesscom.net!cliffd(at)matronics.com (Cliff Dominey) writes: >Dominey) > >Greetings Listers - > My apologies if I missed a thread, but I do believe the June issue >of >Kitplanes has come and gone, and no one here had a comment on the V6 >engine >kit for the 6A that was discussed in that issue. As a mere 8AQB >wannabe, >this is not quite my cup of tea, but getting real close. Is anybody >out >there looking at this? Sounds really interesting. > BTW - my compliments also to Tom Martin for the fairy tale dead >stick. >Maybe this is a chance to make a plug for sailplane training. When >things >up front get really quiet, and all you hear is the sound of that wind >rushing by, at least it wouldn't be for the first time. >Cliff Dominey >cliffd(at)mailhost.accesscom.net >garage workshop (and house) acquired, collecting tools, waiting for >Van > > > > > > +-- > --+ > | Visit the Matronics & RV-List Web Sites at >http://www.matronics.com | > | --- > | > | To [un]subscribe from the RV-List, email >"rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or >subject. | > +-- > --+ > ________________________________________________________________________________
Date: Jul 05, 1997
From: catbird(at)taylortel.com (TTC Carroll A. Bird)
Subject: Re: RUDDER HORN
George McNutt wrote: > > > Does anyone have any suggestions for riveting the R-410 to the R-605PP > rudder horn. The brace forms a little boxed in area and none of my bucking > bars or 3" squeezer will fit in to set the center two rivets. > > Will go to the junkyard tomorrow to find some steel for a smaller bucking > bar, but in the meantime thought someone may have a good idea. > > Thanks > George McNutt - 6A Rudder > Langley B.C. > > I had a machinist friend who made me a bucking bar out of 1 1/4" keystock. It laid in that opening just right to buck those rivets. Carroll Bird Buffalo Gap TX ________________________________________________________________________________
Subject: Re: R-410
From: tcraig-stearman(at)juno.com (John T. Craig-Stearman)
Date: Jul 05, 1997
writes: > >Tom, did you cut the mock-up per plans 7pp?I'm having a heck of a time >figuring out what this should look like. >thanks again >chris marion Chris, Yes, I made the R-410 mockup exactly to the dimensions shown in the plans. I don't have my plans in front of me, so I can't be any more detailed than that. I just found that a three-dimensional model that I could actually fit to my rudder made the fit much clearer. I am going out to my hangar today. I'll look at the rudder plans. If I remember any more useful info, I will e-mail you off-list. Regards, Tom Craig-Stearman tcraig-stearman(at)juno.com RV-4 fitting the gear leg fairings ________________________________________________________________________________
From: Shelby1138(at)aol.com
Date: Jul 05, 1997
Subject: Re: Moving RV6A
While out at Van's builder's clinic, we all went over to Art Chard's to see a project he was contracted to work on. He had just received his wings, which had been transported from Colorado. During the ride out they bounced on whatever they were riding on and the leading edge was flat over a six inch area. It was a sickening feel ing to run your hand down a smooth leading edge and all of a sudden a flat place. For what it's worth. Shelby in Nashville. RV6A ________________________________________________________________________________
Date: Jul 05, 1997
From: Alan Carroll <carroll(at)geology.wisc.edu>
Subject: Re: RUDDER HORN
I just did this last month, and also struggled with it. The standard method seems to be to bend the R-410 up so that you can under it with a thin bucking bar. Better have strong fingers! One of the Van's crew said you could also attach these parts with pop rivets, but if you do so recommended adding a rivet between each hole (ie 7 total). I went this route - looks a bit funny, but is plenty strong. I aslo ran into a "gottcha" with the R-410. Due to the way this part is pre-bent, you end up having to pull the "90 degree" sides over to the where they attach to the rib flanges and skin. Why Van's doesn't pre-bend this piece so that it will fit the rib I can't imagine. I built my "first" R-410 to plan specs, only to find that after I pulled the sides into place there wasn't adequate edge distance on the holes. I was more successful on the second R-410, by relying less on the plan dimensions and more on the "file and fit" method. > >Does anyone have any suggestions for riveting the R-410 to the R-605PP >rudder horn. The brace forms a little boxed in area and none of my bucking >bars or 3" squeezer will fit in to set the center two rivets. > Alan Carroll RV-8 #80177 (Wings) ________________________________________________________________________________
From: BigCfly001(at)aol.com
Date: Jul 05, 1997
Subject: Re: Pnuematic Rivet Squeezer
JD, I agree with ED,Call Action Air Parts,talk to Jerry Williams @ [313]364-5885.He's great to deal with.I bought a pneumatic sqeezer from him last week. chris marion RV-6 finishing rudder cincy oh ________________________________________________________________________________
From: BigCfly001(at)aol.com
Date: Jul 05, 1997
Subject: Re: R-410
Tom, My rudder skelaton is done,I've got the videos,just didnt think to watch them.last night i layed it out on paper.I'm planning on cutting tonight. thanks for the description that helped alot.I'll let you know how it turns out. chris marion ________________________________________________________________________________
Date: Jul 05, 1997
From: "Grant E. Young" <gyoung(at)crl.nmsu.edu>
Subject: Re: 7/16 in HS spar?
Just wondering how people have handled the elevator trim cable hole in the HS spar. I am currently running the cable to the trim tab, and I drilled a 7/16th inch hole as per the plans. However, this hole is not large enough to put the correct grommet in, and enlarging the hole means zapping some of the HS rear spar reinforcers, and it may be difficult to enlargen because of those stiffeners. Should I leave the hole as is, and bag the grommet, or enlargen the hole and use a grommet. Thanks in advance... Grant in NM ps. To the person at Caballo building the 6 who has been trying to get ahold of me, e-mail me your phone number and I'll give you a call. Gyoung(at)crl.nmsu.edu ________________________________________________________________________________
Date: Jul 05, 1997
From: Charlie Kuss <charliekuss(at)sprintmail.com>
Subject: Surface finishing
Hi all, I admit it, I hate drudge work! There has to be an easier way to finish the edges of all these lovely parts Van's has sent me. After using the 3M Scotch Brite wheel, the surfaces still have fine marks on them. Hand sanding in 90+ degree heat sucks!!!!! Does anyone have a way/ways to automate this process (use power tools)? I was thinking of getting some 3M Scotch Brite "fine" grade (blue color) Rol-lok pads for my die grinder or maybe one of those fine abrasive flapper wheels I see in the machinists catalogs. Any experiences or comments are appreciated. I've got a new router and table I'd love to use to make all the radii on the thicker stock pieces. Does anyone know where I can buy a corner rounding router bit with less than a 1/4" radius? I was hoping to find something closer to 1/32-1/16". Thanks in advance. Charlie Kuss RV-8 empenage ________________________________________________________________________________
Date: Jul 05, 1997
From: Charlie Kuss <charliekuss(at)sprintmail.com>
Subject: Alodine powder
Hi, Does anyone know where I could purchase Alodine in powder form? The Aerospace firm I worked for in Buffalo, N.Y. (15 years ago) used to buy it in 30 gallon drums. I want to make a 10 (or more)gallon tank of it to dip parts in. Buying it in liquid form is expensive because you pay to ship mostly water. Charlie Kuss RV-8 empennage ________________________________________________________________________________
Date: Jul 04, 1997
Subject: Re: Rough field takeoff
From: ebundy(at)juno.com (Ed Bundy)
> To Ed Bundy - -How about a description of your rough field take off and >landing techniques. Do you have wheel pants? If so, how do they >handle the unlevel surface. I would appreciate hearing of your experience >using partial flaps on take off. Thanks. J. E. Rehler RV6A flying I do have wheel pants, and have no problems with them, but the surface is pretty level. The surface is crushed and rolled gravel, with most of the pieces being about the size of Grape Nuts (the cereal). While this is a durable, easy-on-the-tires, rain resistant surface, it is murder on the prop. So the ritual is: 1) get the nose up as soon as possible, 2) get the airplane off the surface and climbing as soon as possible. I start with full aft stick, and one notch of flaps (approx 12deg) and get the airplane rolling with as little power as possible, then gradually pick up speed before smoothly adding full power. (to keep high RPM/low groundspeed from sucking gravel through the prop) As soon as the nose comes up, hold it at takeoff attitude until the aircraft climbs into ground effect, lower the nose slightly, gradual climb while accelerating to Vx, raise the flaps, accelerate to Vy or cruise climb when clear of the airport. This seems to work well, any other ideas appreciated. Anyone have any ideas on how to "toughen-up" the leading edges of a metal prop? Ed Bundy RV6A - first flight 11/20/96 ebundy(at)juno.com - Eagle, ID ________________________________________________________________________________
From: BrooksRV6(at)webtv.net (Chris Brooks)
Date: Jul 05, 1997
Subject: Re-Surface finishing
Charlie, I too found the surface finish using the recommended 7A medium wheel too coarse for my taste. Avery sells a EXL 9S Fine Grade that leaves a much nicer finish. Most of my deburring is done with a 2" fine Roloc disk in a 90 degree die grinder. Practice on some scrap first, until you get used to keeping the wheel turning away from the aluminum it could grab and damage it. I still hand sand .016 but if you hit it real quick with 240 grit before going to 400 it will speed it up. Incidentally, for deburring holes I've switched to a single flute deburring bit it dosen't chatter and leave radial lines around the hole like my three flute bit did. Chris Brooks BrooksRV6(at)webtv.net ________________________________________________________________________________
From: cecilth(at)juno.com
Subject: Re: Surface finishing
Date: Jul 05, 1997
Hi Charlie, I use a metal dremal tool bit for the corners. Also The 6 inch 3M scotch bright wheel that goes on your grinder if you have one, has been indispensable for me. Cecil Hatfield writes: > > >Hi all, >I admit it, I hate drudge work! There has to be an easier way to >finish >the edges of all these lovely parts Van's has sent me. After using the >3M Scotch Brite wheel, the surfaces still have fine marks on them. >Hand >sanding in 90+ degree heat sucks!!!!! >Does anyone have a way/ways to automate this process (use power >tools)? >I was thinking of getting some 3M Scotch Brite "fine" grade (blue >color) >Rol-lok pads for my die grinder or maybe one of those fine abrasive >flapper wheels I see in the machinists catalogs. Any experiences or >comments are appreciated. >I've got a new router and table I'd love to use to make all the radii >on >the thicker stock pieces. Does anyone know where I can buy a corner >rounding router bit with less than a 1/4" radius? I was hoping to find >something closer to 1/32-1/16". Thanks in advance. >Charlie Kuss >RV-8 empenage > > > > +-- > --+ > | Visit the Matronics & RV-List Web Sites at >http://www.matronics.com | > | --- > | > | To [un]subscribe from the RV-List, email >"rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or >subject. | > +-- > --+ > ________________________________________________________________________________
From: cecilth(at)juno.com
Subject: Re: RV-F608 and F628
Date: Jul 05, 1997
I have just finished the skeleton of my 6A and have a couple of things that might help others. While fresh in my mind I will pass them on. Years ago (about 30) I learned to distrust strings as straight edges. So I didn't use them to see if the bottom skin would lay straight over the bulkheads. I jigged five very straight 1x4's from F606 to F612. I found the F608 could not be shifted around so it would lay next to the bottom skin no matter what I tried. It had a good eighth of an inch gap. After much thought I split the bulkhead from longhorn to longhorn about one inch from the flange. I then fashioned a splice plate from .032 material for it after moving the flange into proper position. My bottom skin is now going to fit very, very well. Where the F628 touches the bottom skin. The aft corner stuck up about one eighth inch to high so I had to re-bend it some. Now it will fit the bottom skin good. By the way I redid the 2x4 of the jig here so I could fit F628 now instead of after it comes out of the jig like the Orndorff tapes show. I also fit the baggage compartment backs to make F606 not be so wobbly, early on in construction. If you do this you have to use a .032 shim to simulate the floor here. Just like a computer, there are several ways to 'skin the cat'. Does that statement age me or what. Cecil Hatfield 6A ________________________________________________________________________________
Date: Jul 05, 1997
From: wmills(at)southwind.net (William H. Mills)
Subject: EAA Chapter 88 Flyin @ El Dorado, Kansas
Just a quick summary of the fly-in this weekend for you fellow Listers: Pretty good turnout, all kinds of aircraft from antiques and classics (Tiger Moths, Champs, etc.) to relatively modern-vintage Wichita iron (1984 A36 Bonanza, courtesy of the Beechcraft Employees Flying Club, for example...gotta plug the club!!) to international GA (a DH Chipmunk and a Yak 50), along with about two dozen homebuilts...of which about two-thirds were RVs! In fact, if the RVs hadn't shown up, there would have been only one row of experimentals. The RVs were the only multiple examples of any of the various designs that showed up. There were about a dozen RV-6s (mostly tip-ups with a couple of sliders thrown in); one -6A, 4 -4s, and one -3 (I didn't count too closely; I was too busy taking pictures, gawking, and asking questions). Large delegation from Texas (as usual); one from Enid, Oklahoma, and one from Longmount, Colorado. It was good to meet these guys, but I didn't recognize any Listers there. A couple of the -6 guys are already working on -8s. Lots of really good MOTIVATION supplied today!! Hope to see quite a few of you guys at OSH! Bill Mills Wichita, Kansas STILL RV-8 Dreaming, BEFC A-36 Flying ________________________________________________________________________________
From: RVHI(at)aol.com
Date: Jul 05, 1997
Subject: Re: Surface finishing
<< Does anyone have a way/ways to automate this process (use power tools)? I was thinking of getting some 3M Scotch Brite "fine" grade (blue color) Rol-lok pads for my die grinder or maybe one of those fine abrasive flapper wheels I see in the machinists catalogs. Any experiences or comments are appreciated. >> The 3M 2" fine (blue) polishing discs used with a die grinder, are the best tool I've found for finishing edges. These are the round flat discs that twist 1/4 turn into the plastic disc holder (ROLOC). Just plan on buying a lot of these. Larry Adamson RV6A wings (with 0360 rusting in box) ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jul 05, 1997
Subject: Re: Sliding Canopy Skirt Cap (Crasser Commercialism)
Okay, some of you out there in RV-Land haven't been paying attention. The first Production run of the "way cool, what a joy to behold" RV-6/6A Sliding Canopy Skirt Caps as profusely articulated in my prior posting, is going fast. The Frank Lloyd Wright School of Design has nominated this item for their "1997 Elegance in Design" award. What simplicity, what curves! Although we are knee deep in checks, we need more so we can roll around naked in them. America, what a country! Don't be left out and end up having to hog one out of old bar stock with a dull swizzle stick. What are you waiting for? Get your order in. If you're building a 6/6A slider, YOU NEED THIS PART! If not ours, whose? If not now, when? C'mon, cough up the $10 (which, incidentally, includes US shipping in its own handy laminated organic shipping container). Thousands, if not dozens, of satisfied customers around the globe can attest to the superior quality and low drag characteristics of this hot new item. Go ahead, dare to set yourself off from the unwashed unhorsed multitudes. Seem slimmer, taller, sexier and more intelligent than you really are. Okay? Are you ready to give it up now? I am. Send $10 to Gary VanRemortel 1963 Badgerwood Ln, Milpitas, CA 95035 Thanks for supporting my early retirement, -GV ________________________________________________________________________________
From: JDaniel343(at)aol.com
Date: Jul 05, 1997
Subject: Re: Thanks - Pnuematic Rivet Squeezer
I wish to thank everyone ho answered my questions about a pnuematic squeezer. Sure enough I set it up as everyone suggested a waht do you know rivets are being ser properly. Thanks again. PS: Isn't the internet and e-mail great. Wouldn't have known what to do a few years ago. ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jul 06, 1997
Subject: Re: Alodine powder
<< Does anyone know where I could purchase Alodine in powder form? >> I think Amchem in Ambler, PA sells Alodine 1200 powder. Iridite 14-2 by Allied Research Products in Baltimore, MD is the same thing. Or find a plater in your area that does chem film per MIL-C-5541, Class 3 and you may be able to get some from him. For each gallon of solution desired McDonnell-Douglas process spec 13204 says to mix 2-3 ounces of powder to a gallon of distilled or deionized water and add 1/8 fluid oz of Activol #1357 wetting agent from Haas-Miller Corp, Philadelphia, PA (not absolutely necessary). Add one pound/gallon of Cab-O-Sil thixotroping agent to the above solution for non-dipping applications, like sponging on exterior a/c surfaces. If you are going to use the solution over a long period of time, free oxygen will be depleted so you may need to add a fish aerating stone to the bottom of the tank and blow some air into it for best results. Further, warming the solution to 90 degrees F and agitation improves the chemical film development vs time. -GV ________________________________________________________________________________
From: kevin lane <n3773(at)worldnet.att.net>
Subject: degrees of flap
Date: Jul 06, 1997
What actually is "degree of flap"? I recently started setting mine up and couldn't find what angle was actually supposed to be measured. Since the flaps hinge from the bottom skin the pivot point of the flap cord and the fixed wing cord move aft as the flap lowers, different from the elevators. Is 40 degrees an angle formed between the bottom skins? Is it close enough? But, it seems that the travel down of the flap is already determined by the geometry of the weldment and the travel of the electric flap motor. The length of the linkage determines where the flaps stop in the up position(zero degrees). Am I missing something? kevin 6A -engine permanent this week! (Randall, don't read this, I know how it upsets you--brand new engine huh? wish I was a programmer instead of a carpenter, wait, hey, I used to be, I forgot-money or time, take your pick!) ________________________________________________________________________________
Date: Jul 06, 1997
From: George McNutt <GMcNutt(at)compuserve.com>
Subject: RUDDER HORN
Thanks to those who replied to my question about setting the AN470AD4-6 rivets joining the R-410 brace to the rudder horn inside the boxed in are= a that is formed by these two parts. = I chose not to use pop rivets due to the structural nature of the join. For those who have not done this yet here is a brief description. Went to the local scrap metal dealer and bought some assorted pieces of stainless steel. Found a piece 5/8 X 1-1/8 high and about 10" long, polished the 5/8 face on the belt sander and it worked well as a bucking bar. = Clamped the rudder spar to workbench in horizontal position with area to = be riveted hanging over end of workbench, poked bucking bar up through botto= m of boxed in area and riveted the four rivets working from top to bottom. Also picked up a piece of 3/16 X 2 X 10" stainless in anticipation of bucking rivets at the outer ends of the R-403 & R-404 ribs. = George McNutt 6A Rudder. = ________________________________________________________________________________
Date: Jul 05, 1997
From: "Larry D. Hoatson" <lhoatson(at)e2.empirenet.com>
Subject: Re: Alodine powder
> Hi, > Does anyone know where I could purchase Alodine in powder form? I may be able to come up with a source - I'll check on MondayLarry > -- Larry D. Hoatson Yucaipa, CA Redlands (L12) Airport lhoatson(at)empirenet.com KC6WYF via packet at: KC6WYF(at)W6JBT.SOCAL.CA.USA.NOAM Restoring 1950 Cessna 170A N9948A... Looking forward to RV-6 "Either Raise Your Skill Level... or Lower Your Standards" ________________________________________________________________________________
From: "jacquelyn eastburn" <jimnjax(at)worldnet.att.net>
Subject: chevrolet power
Date: Jul 06, 1997
after reading about the conversion, it sounds like a real choice over conventional aircraft engines. the option possibilities could be endless ie. tuned port injection, after market heads, choice of cam combinations, high voltage ignition systems, tuned exhaust and variable computer chips. oh yeah, a short block at your local chevy dealer for about 800 dollars or 1000 blue printed , if you want. according to the letter from them, the -6A should be ready about now with the -6 and -8 this year. jimnjax(at)worldnet.att.net Hillsboro Oregon RV - 8 Ser. No. 80079 ________________________________________________________________________________
Date: Jul 06, 1997
From: John Darby <johnd@our-town.com>
Subject: Re: degrees of flap
>What actually is "degree of flap"? I recently started setting mine up and >couldn't find what angle was actually supposed to be measured. Since the >flaps hinge from the bottom skin the pivot point of the flap cord and the >fixed wing cord move aft as the flap lowers, different from the elevators. >Is 40 degrees an angle formed between the bottom skins? Is it close enough? >But, it seems that the travel down of the flap is already determined by the >geometry of the weldment and the travel of the electric flap motor. The >length of the linkage determines where the flaps stop in the up >position(zero degrees). Am I missing something? Kevin; Here is a shadetree mechanics version. I think it is accurate enough unless you are designing the breech block for a 16 inch naval gun. A degree is a degree, measured form one angle to another. I used an inclinometer, but it can be done with the old standby Weems plotter. Set the flaps full up, rest the inclinometer on top of the flaps, read what angle the pendulum is on the inclinometer, move the flaps down until the pendulum shows they have changed the angle by ten degrees (or what ever you want), mark the outer left leading edge of the flaps where it comes out from under the trailing edge of the wing skin. This will be your visual reference for that number of degrees of flaps. Do this for however many positions of the flap settings you want. The same can be done with the Weems plotter modified with a string and weight and placed under the flap bottom. I did it. It worked fine for me, but I don't worry about setting my flaps 1/2 to 1 degree off. I placed a slanting tape on the flaps. The slant is full inboard when the flaps are up, and full out board when they are full down. On the slant, I put horizontal bars on it, one at each 10 degrees of flap movement. If I wanted 10 degrees of flaps, I moved it until the first horizon. bar came out from under the wing skin and stopped. That gave me 10 degrees of flaps. No complicated expensive flaps indictor gauge etc. Just the ole Mark I Mod I eyeball. By the way, my inclinometer had a magnet on the bottom of it, I did modify it by replacing the iron magnet with an aluminum magnet. You do have an aluminum magnet don't you? :-) John Darby RV6 sold Stephenville TX johnd@our-town.com ________________________________________________________________________________
Date: Jul 06, 1997
From: Denny Harjehausen <retflygtiger(at)proaxis.com>
Subject: RV & EAA in Corvallis (Chatter)
Bill Benedict, Mike Seager and Jeremy Benedict (our net security agent) flew down to our (new) Chapter #1183 meeting at the invitation of one of out organizers and RV-6A builder, Steve Kamura. We have our meetings the first Staurdau of each month. They arrived early enough to give some rides in the new RV-8 and the RV-6 and get some Mexican food. I think they converted a few to RV types by the look on their faces when they came down. Bill gave us a slide show on the history of Van's and gave us a run down on what was and is being sold. Mike gave us a run down on the training he does for Van's. It is a absolute for me. I'm building a -6, but that RV-8 sure is inviting. Maybe next time. Anyway I thought share that with you listeners and publicly thank Bill and Mike for taking their holiday time and attending our meeting here in Corvallis, OR. If any of you are coming though and would like to contact our group or need a helping hand just E-mail me or phone 259-4500 and ask for Denny. Have a Great Day! Denny, RV-6 (R)N641DH Fuselage-top side Lebanon, OR ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: Re: Surface finishing
Date: Jul 06, 1997
Charlie, There are lots of power tools and accessories that make tedious hand filing and deburring easier! J&L, 1-800-521-9520, sells Corner Rounding End Mills with radii from 1/32 on up. They vary in price from $20.35 for the 1/32 to $22.00 for the 3/16, whose part number is HCR-40600K. These are really meant for milling machines and you may get some chatter from a router due to higher speed and less rigid mounting. I used a hand held belt sander on the horizontal stab spar pieces that need a radius to clear the bend radius in the mating sheet. A 2" Roloc disc is great for taking down a long sheet to a line where you have 3/16 or less to remove. I use an 80 grit aluminum oxide Roloc for fast cutting and 120 for slower, fine cutting. Use a 90 degree die grinder to get a good hand position and practice cutting on the down side of the disk. You may have to turn the piece over to do this. Draw a line with a very fine Sharpie pen and support the long piece with about 1/4 of edge overhang. The Sharpie pen leaves about a 1/32 wide line and with practice you can split it with the 120 grit wheel. Finish with the blue Scotchbrite wheel with wheel perpendicular, and 45 degrees to the edge. Turn piece over to do the bottom edge. This will give you perfectly straight lines with polished radii edges. Don't take down a line with the blue wheel because the fuzzies will polish off the line and you won't have a guide. J&L also sell sanding cartridges that fit straight die grinders. I have mandrels and cartridges from 1/4 to 7/8 diameter and I use them to carve out curved surfaces, holes, etc. Run the die grinder at low PSI (just above stalling) so centripetal force doesn't whip the abrasive roll off. Dennis 6A fuselage in jig ---------- > From: Charlie Kuss <sprintmail.com!charliekuss(at)matronics.com> > To: rv-list(at)matronics.com > Subject: RV-List: Surface finishing > Date: Saturday, July 05, 1997 6:26 PM > > > Hi all, > Does anyone have a way/ways to automate this process (use power tools)? > I was thinking of getting some 3M Scotch Brite "fine" grade (blue color) > Rol-lok pads for my die grinder or maybe one of those fine abrasive > flapper wheels I see in the machinists catalogs. Any experiences or > comments are appreciated. > I've got a new router and table I'd love to use to make all the radii on > the thicker stock pieces. Does anyone know where I can buy a corner > rounding router bit with less than a 1/4" radius? I was hoping to find > something closer to 1/32-1/16". Thanks in advance. > Charlie Kuss > RV-8 empenage > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: Re: degrees of flap
Date: Jul 06, 1997
Procedure with Smart Level: 1) Line up flat with aileron pinned to neutral. 2) Calibrate Smart Level to "zero" at this position 3) Rotate flap until you have 40 degrees of travel. Something will probably interfere and you will have to deal with it. NOTE: A recent RVAtor (I think) had a comment that the flaps should have 42 degrees of travel stationary because the wind forece will deflect them to 40 in flight! My plans and instructions don't say anything about that! Dennis 6A fusellage in jig ---------- > From: kevin lane <worldnet.att.net!n3773(at)matronics.com> > To: rv-list(at)matronics.com > Subject: RV-List: degrees of flap > Date: Saturday, July 05, 1997 11:04 PM > > > What actually is "degree of flap"? I recently started setting mine up and > couldn't find what angle was actually supposed to be measured. Since the > flaps hinge from the bottom skin the pivot point of the flap cord and the > fixed wing cord move aft as the flap lowers, different from the elevators. > Is 40 degrees an angle formed between the bottom skins? Is it close enough? > But, it seems that the travel down of the flap is already determined by the > geometry of the weldment and the travel of the electric flap motor. The > length of the linkage determines where the flaps stop in the up > position(zero degrees). Am I missing something? > kevin 6A -engine permanent this week! (Randall, don't read this, I know > how it upsets you--brand new engine huh? wish I was a programmer instead of > a carpenter, wait, hey, I used to be, I forgot-money or time, take your pick!) > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ ________________________________________________________________________________
Date: Jul 06, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Wire routing thru main spar
There are several points where you can run wires and lines through the spar. The most logical is near the center of the fuselage where you can open up a three sided hole, the fourth side being at the end on the spar. This would allow your wiring to remain intact as you install/remove your wings. If you choose to do this, just tie the wire bundles over so they will not interfere with the control column. You can put holes through the spar web, as long as you avoid the bars, both horizontal and vertical. I put a 2" hole through mine to run warm/cool air to the back seat, with Van's approval. The point of the highest stress is just outside the fuselage. There is a vertical bar in the spar just inside the fuselage with two bolts attaching it to the fuse. We refer to this as the shear bar and you can loosely think of it as a fulcrum (remember, I'm an EE, not an ME nor an English major). The points just outboard from this shear bar are receiving the highest stress. One of the purposes of the wing walk ribs is to support the skin when you step on the wing, but an even more important function is to support the spar bars at the highest stress point where they are under a high level of compression and are trying to buckle forward (the top bars when pulling +g's) or aft. Now that we have gone through this exercise, don't think that you need to reinforce this area. There has never been a case of spar failure in a -4 or -6/6A. These spars are so over designed that you (the pilot) will pass out long before the spar yields. Bill > >I'm in the seemingly never-ending phase of wiring my RV-4 and I have a >question, or perhaps more of a "survey." > >Where have most of you 4 builders routed the wire bundles through the >main spar?? My original plan was just inboard of the fuselage skin, near >an existing tooling-hole. My concern however is the size of the holes >required,, which in my case, are fairly large because of my use of QD's. >I am thinking I will require one hole on each side, one of which would >have to be 1" dia, the other 1 1/4". Of course I am referring to the spar >web and not interfering with any stiffeners, straps, etc. > >I have seen many different configurations including a few incorporating >the setup I have already described, but the thought of removing ANY >material from the main spar is rather scary to me :/ > >Thanks in advance,,, > > >Derrick L. Aubuchon >n184da(at)cctrap.com > > > > > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours. These opinions are mine and do not necessarily represent the opinions or position of my employer. ________________________________________________________________________________
Date: Jul 06, 1997
From: Bill Benedict <billb(at)europa.com>
Subject: Re: Vans in Indy?
Frank, You are correct. Van will be there, but I do not know about the topic. Bill > >I heard that Van is going to be addressing the Indianapolis Aero Club on >July 8th at Eagle Creek Airport. Maybe Bill Benedict can confirm this >and give us a little more details. > >Frank Smidler > > > > +-- --+ > | Visit the Matronics & RV-List Web Sites at http://www.matronics.com | > | --- | > | To [un]subscribe from the RV-List, email "rv-list-request(at)matronics.com" | > | & put the word "[un]subscribe" in the *body*. No other text or subject. | > +-- --+ > > Bill RV-4-180 soon. N894RV with over 400 hours behind a O-320, Over 1000 RV flying hours.


June 26, 1997 - July 06, 1997

RV-Archive.digest.vol-db