RV-Archive.digest.vol-pr

August 19, 2004 - August 30, 2004



      
      
      > Mr. Hester,
      > While driving to the airport this evening, I realized the sketch should
      > show the
      > transition zone in the middle of the travel.  I'll correct it and send 
      > you the
      > update tomorrow.
      
      Actually, you need to show the acceptable range on both sides of 
      center.  For example, the drawing shows the 45 degree angle - what 
      happens beyond this angle?  There should be a travel range shown for 
      "released" and a range shown for "locked".
      
      Jim Daniels
      
      
      
________________________________________________________________________________
From: Laird Owens <owens(at)aerovironment.com>
Subject: Re: Propeller balance
Date: Aug 19, 2004
If you don't mind heading South, there is a shop at Whiteman, WHP, (under Burbanks airspace) that will do balancing on homebuilts. I'll try to get some info for you. I'll also pass this on to the SoCal list to see what comes up. Laird RV-6 WHP On Aug 19, 2004, at 2:54 PM, David L Ahrens wrote: > > Hello all, I need some help in finding someone to Dynamic balance my > propeller and engine. I have a RV-6A with about 75 hrs., 0-320 > engine,conical mounts, sensenich propeller. The local shops do not show > much interest in doing the work. One doesn't want to touch a homebuilt > and the other can't work me into his schedule. I live in Bakersfield, > Ca. > Anyone have a favorite shop within an hours flight time of Bakersfield? > Thanks, David Ahrens > > > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > > > > ________________________________________________________________________________
From: JusCash(at)aol.com
Date: Aug 19, 2004
Subject: Re: Propeller balance
Sullivan Propeller Specialties, 510-782-0920, located on the Hayward Airport. They just did mine and I am totally satisfied. Cash Copeland RV6 Hayward, Ca In a message dated 8/19/2004 3:01:18 PM Pacific Daylight Time, daviddla(at)juno.com writes: Hello all, I need some help in finding someone to Dynamic balance my propeller and engine. I have a RV-6A with about 75 hrs., 0-320 engine,conical mounts, sensenich propeller. The local shops do not show much interest in doing the work. One doesn't want to touch a homebuilt and the other can't work me into his schedule. I live in Bakersfield, Ca. Anyone have a favorite shop within an hours flight time of Bakersfield? Thanks, David Ahrens ________________________________________________________________________________
Date: Aug 19, 2004
From: Bobby Hester <bhester(at)hopkinsville.net>
Subject: Re: [Fwd: Re: Parking brake info (PVPV-1)]
Jim Daniels wrote: > > > >>Mr. Hester, >>While driving to the airport this evening, I realized the sketch should >>show the >>transition zone in the middle of the travel. I'll correct it and send >>you the >>update tomorrow. >> >> > >Actually, you need to show the acceptable range on both sides of >center. For example, the drawing shows the 45 degree angle - what >happens beyond this angle? There should be a travel range shown for >"released" and a range shown for "locked". > >Jim Daniels > > The drawing I received from George R. Happ at Matco Mfg. does show this. I sent the drawing into the RV-List but it has not showed up yet. So I put it on my web site: http://members.hopkinsville.net/bhester/pvpv1page.htm -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse :-) ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Aug 19, 2004
Subject: Re: Propeller balance
In a message dated 8/19/2004 3:01:22 PM Pacific Daylight Time, daviddla(at)juno.com writes: I need some help in finding someone to Dynamic balance my propeller and engine. I have a RV-6A with about 75 hrs., 0-320 engine,conical mounts, sensenich propeller. The local shops do not show much interest in doing the work. One doesn't want to touch a homebuilt and the other can't work me into his schedule. I live in Bakersfield, Ca. Anyone have a favorite shop within an hours flight time of Bakersfield? ========================================== Dave Morss did mine. He's based at San Carlos (KSQL) and you may be able to track him down on the web. GV (RV-6A N1GV O-360-A1A C/S, flying 708 hrs) ________________________________________________________________________________
From: "Bob 1" <rv3a(at)comcast.net>
Subject: Re: Saw this engine on Ebay
Date: Aug 20, 2004
> > Great for a low budget bird: > > http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?viewItem&rd=1&item=2487056705&category=26437 > > if the link doesn't work, go to ebay and put the item number into the search > window: > > 2487056705 > ++++++++++++++++++++++++++++++++ The H2AD series of engines have a less than stellar history. Let the buyer beware. Bob ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Question for the aerodynamycists
Date: Aug 20, 2004
I am going to install a NACA vent on the side of the forward fuselage on the RV-4 I am rebuilding. I am thinking of installing it right below the cowl cheek angled downward so that the longitudinal axis of the vent is parallel to the logitudnal axis of the cowl cheek extension. My thought is the pressure will be positive in this area and will result in good positive airflow into the vent (this will be for fresh air ventilation to the front cockpit). I assume that the left side will be best for airflow given the vortex generated by the propeller but the right side would be best for internal routing of the scat tubing as there is no throttle and mixture control cables to avoid. Does it make an appreciable difference? As in most things the best idea would be to try it to find out but that is not practical given the hole I need to cut in the fuselage skin. I'm looking for opinions and/or experience with this location. Is my thinking sound or am I missing something? Net, net - I'd like to install on the right but the left seems like a better location. Which is best and will either work? Richard RV-4 N144KT - rising from he ashes of a 1998 landing in the trees at IGX. ________________________________________________________________________________
From: "Steve & Denise" <sjhdcl(at)kingston.net>
Subject: Re: Saw this engine on Ebay
Date: Aug 21, 2004
3.3 DATE_IN_FUTURE_12_24 Date: is 12 to 24 hours after Received: date Exactly. Why anybody would build a $60,000 airplane and finish it off with a $4000 engine is beyond my reasoning. The most important piece of the puzzle and I see way too many builders trying to find the cheapest they can get. If I have to spend $35,000 to get a good engine either new or a very well documented log books then so be it. Wheres the checkbook? If anyone buys an engine like this the amateur built warning sign should include the price paid for the engine in large capital letters. As the saying goes: If you can't afford a good engine, you can't afford an airplane. Ebay is for digital camera batteries, not aircraft engines. Steve RV7A #2 70015 71629 > Subject: Re: RV-List: Saw this engine on Ebay > From: "Jamie Painter" <jdpainter(at)jpainter.org> > > > Just an FYI on this Engine: > > It appears to have been involved in the following accident (based on the > N-number on the aircraft logbook). > > http://www2.ntsb.gov/ntsb/brief.asp?ev_id 040803X01125&key=1 > > On July 4, 2004, about 1700 eastern daylight time, a Cessna 172N, N10DJ, > received substantial damage during the landing roll out at the Grand Canyon > Airport, Wellsboro, Pennsylvania. The certificated private pilot was not > injured. Visual meteorological conditions prevailed, and the airplane was not > operating on a flight plan. The local personal flight, which departed Cherry > Springs Airport (5G6), Galeton, Pennsylvania, was conducted under 14 CFR Part > 91. > > According to a Federal Aviation Administration (FAA) inspector, the pilot > elected to perform a precautionary landing at Grand Canyon Airport due to > deteriorating weather conditions in the area. While landing on runway 28, the > airplane veered off the right side of the runway and impacted a hay bail. > > ... > > > > > > > Great for a low budget bird: > > > > http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?viewItem&rd=1&item=2487056705&category=26437 > > > > if the link doesn't work, go to ebay and put the item number into the search > > window: > > > > 2487056705 ________________________________________________________________________________
From: "Ronnie Brown" <romott(at)adelphia.net>
Subject: Re: Saw this engine on Ebay
Date: Aug 20, 2004
Please don't perpetuate the myths about this engine. I ran two of these O320-H2AD engines to TBO on our 1977 Cessna 172N with ABSOLUTELY NO internal problems. There were indeed problems with the early engines at a time when these engines were not flying much due to the oil embargos of the 70's. I also have a friend with this engine installed on his RV-7A, with over 500 trouble free hours and he is very happy with it. See the bottom of page http://www.prime-mover.org/Aviation/C172.ENGINES.html for more info on the truth (not myths) about this engine. ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: Saw this engine on Ebay
Date: Aug 20, 2004
> > Exactly. > > Why anybody would build a $60,000 airplane and finish it off with a $4000 > engine is > beyond my reasoning. > A couple of reasons. The $3,500 is probably less than the value of the good parts on the engine. Its less than the cost of a case alone, for example. The H2D had a bad reputation as early versions had problems (can't remember what they were but I think CAM and/or lifter related. Later serial numbers fixed those problems and it became a very reliable engine. For $3,500 youcould buy this engine and overhaul it by having the parts sent out for yellow tag inpection and refurb/replace for 5-$15,000 depending on what needed to be scrapped. I'd have a hard time buying it sight unseen and would want to at least pull the cylinders to get a look at the cam and dial the crank but it is a good deal if anything major is salvageble. But if you would rather convert cash to an new engine that is also a very wise choice, maybe even a preferable one. There has been a lot of talk on how much it cost to build one of these things. That is inversely proportional to the amount of work you want to do scrounging for deals on used stuff versus buying brand new out of the box. Of course new is better, but a flying aircraft can be done safely and a heck of a lot less cash out the door. Of course this assumes you pay yourself the kind of wages tyrants the world over pay their minions... ________________________________________________________________________________
Subject: RV-8 Canopy Track Question
From: Don.Alexander(at)AstenJohnson.com
Date: Aug 20, 2004
08/20/2004 09:12:07 AM I am in the process of putting my C-804 / C-805 rear slide track together and have run into a question that I can't seem to find the answer to. The plans indicate that the 805 should be countersunk on both sides for the AN 426 rivets. I don't understand what this means. How does one go about driving the rivets on this assembly? I imagine that the shop head of the rivet somehow nests inside the bottom countersink, but I don't see how to drive the rivet down into a "funnel" shaped hole. Don Alexander RV-8 Half way there...seeing the light at the end of the dark tunnel ________________________________________________________________________________
Date: Aug 20, 2004
From: Bill VonDane <bill(at)vondane.com>
Subject: Re: Saw this engine on Ebay
Agreed... He had three (now just two) H2AD's running on RV's here and have not had any problems with any of them... Use aeroshell oil (has the additives) and fly regularly and you will not have any trouble... -Bill VonDane RV-8A - Colorado Springs EAA Tech Counselor www.vondane.com www.rv8a.com www.creativair.com www.epanelbuilder.com ----- Original Message ----- From: "Ronnie Brown" <romott(at)adelphia.net> Subject: Re: RV-List: Saw this engine on Ebay > > Please don't perpetuate the myths about this engine. I ran two of these O320-H2AD engines to TBO on our 1977 Cessna 172N with ABSOLUTELY NO internal problems. There were indeed problems with the early engines at a time when these engines were not flying much due to the oil embargos of the 70's. I also have a friend with this engine installed on his RV-7A, with over 500 trouble free hours and he is very happy with it. > > See the bottom of page http://www.prime-mover.org/Aviation/C172.ENGINES.html for more info on the truth (not myths) about this engine. > > ________________________________________________________________________________
From: Tailgummer(at)aol.com
Date: Aug 20, 2004
Subject: Re: RV-8 Canopy Track Question
Don, it's reffered to as " double countersinking". Just countersink each side as usual then select a rivet length shorter than you would use to produce a shop head and squeeze. Try it out on scrap to get a feel for the correct length. The final result is a smooth surface on both sides. It might not be perfect, but it will work. John D'Onofrio ________________________________________________________________________________
Subject: RV8 one piece wings skins
Date: Aug 20, 2004
From: "Stewart, Michael (ISS Atlanta)" <mstewart(at)iss.net>
I just found out from Charlie Kuss, builder in Fl., that Vans now can make for you single piece wing skins, .032 in stead of 025, for the RV8. I am a little upset (OK A LOT) I did not know about this. Up charge is some $50 or something, negligible shipping charge change. Many of you probably know that when you sight down the wing of any RV with 025 skins, you see the dip between the ribs. Unsightly. Weight penalty is about 4lbs total for the plane using the 4 new skins. Im no aerodynamicist but Ill bet that the speed increase is more than negligible with the lack of distortion using the 032 skins. I sure would have liked to have known this on the Super 8. I'd of taken that penalty for strength in a heartbeat. Thought you all would find this interesting. I have not spoken to Vans yet about this so I can not confirm the cost or availability. I would also be interested in knowing what strength increase could be expected from a change from 025 to 032 skins if anyone happens to know (or swag) this off the top of their heads. Regards, Michael Stewart All my list watching did not turn up this info. ARGH! ________________________________________________________________________________
Date: Aug 20, 2004
From: "David E. Nelson" <david.nelson(at)pobox.com>
Subject: Re: RV-8 Canopy Track Question
Hi Don, This same technique was used to make the TE on the rudder (at least on my 7A). The plans/instructions walked my through the procedure. The rivet was basically back riveted to fill in the countersink. Regards, /\/elson Austin, TX RV-7A - Got the goo, ready to finish the tank On Fri, 20 Aug 2004 Don.Alexander(at)AstenJohnson.com wrote: > > > I am in the process of putting my C-804 / C-805 rear slide track together > and have run into a question that I can't seem to find the answer to. The > plans indicate that the 805 should be countersunk on both sides for the AN > 426 rivets. I don't understand what this means. How does one go about > driving the rivets on this assembly? I imagine that the shop head of the > rivet somehow nests inside the bottom countersink, but I don't see how to > drive the rivet down into a "funnel" shaped hole. > > Don Alexander > RV-8 Half way there...seeing the light at the end of the dark tunnel > > -- ~~ ** ~~ If you didn't learn anything when you broke it the 1st ~~ ** ~~ time, then break it again. ________________________________________________________________________________
From: WFACT01(at)aol.com
Date: Aug 20, 2004
Subject: Re: RV8 one piece wings skins
MIKE-VANS MADE MINE 6 YEARS AGO-WHAT IS A SUPER 8-TOM Tom Whelan Whelan Farms Airport President EAA Chapter 1097 wfact01(at)aol.com 249 Hard Hill Road North PO Box 426 Bethlehem, CT 06751 Tel: 203-266-5300 Fax: 202-266-5140 EAA Technical/Flight Advisor RV-8 540 LYC (Engine Runs, Taxi-Tests) S-51 Mustang Turbine (Under Construction) ________________________________________________________________________________
From: Laird Owens <owens(at)aerovironment.com>
Subject: Re: Propeller balance
Date: Aug 20, 2004
David, Hummingbird Rotorwing Services will do it at Whiteman (WHP). John Balkin 818 897 1995 $155, and he says he has about a week lead time. Also one at Cable (CCB). Mike Hartman (909) 624-5022 Don't know what his cost or availability is. Good luck, Laird On Aug 19, 2004, at 2:54 PM, David L Ahrens wrote: > > Hello all, I need some help in finding someone to Dynamic balance my > propeller and engine. I have a RV-6A with about 75 hrs., 0-320 > engine,conical mounts, sensenich propeller. The local shops do not show > much interest in doing the work. One doesn't want to touch a homebuilt > and the other can't work me into his schedule. I live in Bakersfield, > Ca. > Anyone have a favorite shop within an hours flight time of Bakersfield? > Thanks, David Ahrens > > > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > > > > ________________________________________________________________________________
Date: Aug 20, 2004
From: Phil Birkelbach <phil(at)petrasoft.net>
Subject: Re: Saw this engine on Ebay
Wow, beyond reasoning? I don't think I'd consider a $4,000 engine much more than a core but if it's a good core and the crank, cam and case are good you're only about $8,000 away from a good rebuilt engine. If I had been able to find an engine for $12,000 then I wouldn't have a $60,000 airplane I'd have a $40,000 airplane. If it were me I think I'd start looking east. There are about to be a bunch of perfectly good engines coming out of bent up airplanes in Florida. A guy here in Houston built a $28,000 RV-6 (8 years ago) and part of his secret was a hurricane engine. Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB (Reserved) - Panel http://www.myrv7.com Steve & Denise wrote: > >Exactly. > >Why anybody would build a $60,000 airplane and finish it off with a $4000 >engine is >beyond my reasoning. > > ________________________________________________________________________________
From: "Greg Milner" <tldrgred(at)execpc.com>
Subject: Re: Question for the aerodynamycists
Date: Aug 20, 2004
My -4 has one on the left side and works good until backing off the throttle. Red Milner RV-4 N79KM based @ UES ----- Original Message ----- From: "Richard Bibb" <rebibb(at)comcast.net> Subject: RV-List: Question for the aerodynamycists > > I am going to install a NACA vent on the side of the forward fuselage on the > RV-4 I am rebuilding. I am thinking of installing it right below the cowl > cheek angled downward so that the longitudinal axis of the vent is parallel > to the logitudnal axis of the cowl cheek extension. My thought is the > pressure will be positive in this area and will result in good positive > airflow into the vent (this will be for fresh air ventilation to the front > cockpit). > > I assume that the left side will be best for airflow given the vortex > generated by the propeller but the right side would be best for internal > routing of the scat tubing as there is no throttle and mixture control > cables to avoid. > > Does it make an appreciable difference? As in most things the best idea > would be to try it to find out but that is not practical given the hole I > need to cut in the fuselage skin. > > I'm looking for opinions and/or experience with this location. Is my > thinking sound or am I missing something? > > Net, net - I'd like to install on the right but the left seems like a better > location. Which is best and will either work? > > Richard > RV-4 N144KT - rising from he ashes of a 1998 landing in the trees at IGX. > > > _____________________________________________________ > ________________________________________________________________________________
From: "RV_8 Pilot" <rv_8pilot(at)hotmail.com>
Subject: Parachutes, any record
Date: Aug 20, 2004
I feel totally confident I could get out in the event of a fire. An -8 canopy can be opened in flight - not sure about any others. What would be bad enough? Not sure. If there was fire in the cockpit, it wouldn't take much to get me out. Inside the cowling - probably depends on how hot my feet are getting and what kind of emergency landing spots are or the ground below. As for someone actually able to get out of the plane (RV-8), it is possible and has happened. Unfortunately, a contributor to the list, Mr. Von Alexander, exited the plane without a parachute and did not survive. As I remember the discussions, it wasn't exactly clear as to why he had the canopy open and was unstrapped. Check the archives here and NTSB records for more info. http://www2.ntsb.gov/ntsb/brief.asp?ev_id 001212X19358&key=1 Bryan Jones -8 www.LoneStarSquadron.com Houston, Texas > > Bryant: Thnaks for the reply, however, two things, what do you do >in >case of fire, as you said, how can one open the canopy in flight, and when >is >the fire bad enough to get to this situation? > >Second I really would like to know if there is any record anywhere, as to >has any one ever, to use the word, egressed, from an rv in flight? > > >Thnaks > >Bert > ________________________________________________________________________________
From: "Matthew Brandes" <matthew(at)n523rv.com>
Subject: Compass liquid
Date: Aug 20, 2004
I picked up a used compass that has a low liquid level. What can I use to replenish/replace it? Matthew Brandes, Van's RV-9A (Fuselage) EAA Chapter 868/91/1329 www.n523rv.com <http://www.n523rv.com/> ________________________________________________________________________________
From: Hopperdhh(at)aol.com
Date: Aug 20, 2004
Subject: Re: Compass liquid
In a message dated 8/20/04 2:56:34 PM US Eastern Standard Time, matthew(at)n523rv.com writes: > > > I picked up a used compass that has a low liquid level. What can I use to > replenish/replace it? > > Matthew Brandes, > Van's RV-9A (Fuselage) > EAA Chapter 868/91/1329 > www.n523rv.com <http://www.n523rv.com/> > > I used "Ultra-pure smokeless and odorless candle and lamp oil" which you can buy at any of the big home improvement stores. There used to be a compass factory near here, and they just used a high grade of kerosene. Much cheaper than AC$pruce. Dan Hopper RV-7A (Flying about 37 hours now) ________________________________________________________________________________
Date: Aug 20, 2004
From: Chuck <chuck515tigger(at)yahoo.com>
Subject: Re: Compass liquid
Matthew, I think I've still got a few compass overhaul kits and a pint of compass fluid kickin' around. If you're interested I go search. If I find 'em you can have 'em, just reimburse me for the shipping. Chuck don't archive Matthew Brandes wrote: I picked up a used compass that has a low liquid level. What can I use to replenish/replace it? Matthew Brandes, Van's RV-9A (Fuselage) EAA Chapter 868/91/1329 www.n523rv.com --------------------------------- ________________________________________________________________________________
From: "Rhett Westerman" <Rhettwesterman(at)cox.net>
Subject: Compass liquid
Date: Aug 20, 2004
Use Naptha -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Chuck Subject: Re: RV-List: Compass liquid Matthew, I think I've still got a few compass overhaul kits and a pint of compass fluid kickin' around. If you're interested I go search. If I find 'em you can have 'em, just reimburse me for the shipping. Chuck don't archive Matthew Brandes wrote: I picked up a used compass that has a low liquid level. What can I use to replenish/replace it? Matthew Brandes, Van's RV-9A (Fuselage) EAA Chapter 868/91/1329 www.n523rv.com --------------------------------- ________________________________________________________________________________
Date: Aug 20, 2004
From: "Matt Johnson" <matt(at)n559rv.com>
Subject: Floor Standing Pneumatic Dimpler...
(not processed: message from valid local sender) One of the guys at Sierra Skypark here in Fresno has a dimpler that is a floor standing pnuematic dimpler with a foot pedal that he uses to dimple skins. I noticed that his finished control surfaces has no light distortion around the rivets at all (showing a slight dimpling that extends past the rivet head). When you look at his rivets, you would think they were countersunk in the skin not riveted. My question is, is that from his technique at dimpling skins or is it because he has the pneumatic dimpler? My rivets look pretty good, but not that good and I use the standard bench top one that you pound with the hammer... By the way, were do you even get a floor unit like that? I looked online and cant find one. - Matt ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Aug 20, 2004
Subject: Re: Compass liquid
The Rec. Aviation Homebuilt site on Google had quite a discussion on this some time back. One party finally settled on Toner for copy machine. He said it is slightly more viscous than the original and was clear. Maybe easier on gaskets too ? I intend to use it in mine,soon. Bob Olds RV-4 , N1191X A&P , EAA Tech. Counselor Charleston,Arkansas Real Aviators Fly Taildraggers ________________________________________________________________________________
From: "David Burton" <dburton(at)nwlink.com>
Subject: Re: Compass liquid
Date: Aug 20, 2004
I'd give a call to an avionics shop and ask them what they use now. We used to use acid free white kerosene in the past. ----- Original Message ----- From: "Matthew Brandes" <matthew(at)n523rv.com> Subject: RV-List: Compass liquid > > I picked up a used compass that has a low liquid level. What can I use to > replenish/replace it? > > Matthew Brandes, > Van's RV-9A (Fuselage) > EAA Chapter 868/91/1329 > www.n523rv.com <http://www.n523rv.com/> > > ________________________________________________________________________________
From: "Fred Kunkel" <rvator(at)socal.rr.com>
Subject: Re: Floor Standing Pneumatic Dimpler... (not processed:
message from valid local sender)
Date: Aug 20, 2004
It's the riveter & you're probably referring to a CP-450 style cold riveter - 24,000 Lbs. of force @ 90 PSI - rated for 1/2" solid aluminum rivets. You can probably find a rebuilt one from different dealers for the $5-6,000 range. If your rivets look pretty good, you might want to save your money for the next engine core that comes up on Ebay :). ----- Original Message ----- From: "Matt Johnson" <matt(at)n559rv.com> Subject: RV-List: Floor Standing Pneumatic Dimpler... (not processed: message from valid local sender) > > One of the guys at Sierra Skypark here in Fresno has a dimpler that is a floor standing pnuematic dimpler with a foot pedal that he uses to > dimple skins. I noticed that his finished control surfaces has no light distortion around the rivets at all (showing a slight dimpling that extends > past the rivet head). When you look at his rivets, you would think they were countersunk in the skin not riveted. My question is, is that from > his technique at dimpling skins or is it because he has the pneumatic dimpler? My rivets look pretty good, but not that good and I use the > standard bench top one that you pound with the hammer... > > By the way, were do you even get a floor unit like that? I looked online and cant find one. > > - Matt > > ________________________________________________________________________________
From: "Wayne R. Couture" <commando@cox-internet.com>
Subject: Re: Compass liquid
Date: Aug 20, 2004
I used Varsol in mine! Wayne ----- Original Message ----- From: "David Burton" <dburton(at)nwlink.com> Subject: Re: RV-List: Compass liquid > > I'd give a call to an avionics shop and ask them what they use now. We used > to use acid free white kerosene in the past. > > ----- Original Message ----- > From: "Matthew Brandes" <matthew(at)n523rv.com> > To: > Subject: RV-List: Compass liquid > > > > > > I picked up a used compass that has a low liquid level. What can I use to > > replenish/replace it? > > > > Matthew Brandes, > > Van's RV-9A (Fuselage) > > EAA Chapter 868/91/1329 > > www.n523rv.com <http://www.n523rv.com/> > > > > > > ________________________________________________________________________________
Date: Aug 20, 2004
From: "Richard E. Tasker" <retasker(at)optonline.net>
Subject: Re: Park brake
Okay guys, let's not get too carried away. If you look at the operation drawing on the website, you will notice that the operational arc of "on" and the operational arc of "off" is everything except the middle 45 degrees where it is transitioning. In other words, all this discussion about 45 or 90 degrees is just smoke. If you look at the drawing you will see that the valves are fully open everywhere from about 27 degrees above horizontal to completely vertical. They are fully closed from about 25 degrees below horizontal to completely vertical (down). So, as long as you don't leave the valve in the central position (approximately +/- 25 degrees) you are fine. With the way it works, you cannot turn it on when you really want it off. Unless you have some really funky linkage you can only pull or push to the vertical positions and all is well. I suppose you could overcenter the lever and have a problem, but even there, assuming you have the clearance for the lever movement, the valve would still work properly. Stops are nice but not really necessary for the proper functioning of the valve. Dick Tasker Wheeler North wrote: > >The matco park brake valves have two spring loaded poppet valves (one for >each side) that are pushed open by two cam lobes on a rotating shaft. > >When the cams are pushed on them they are stuck open, when the cam is >rotated off they act like check valves and allow pressure to build up from >the master cyls but not return. > >If the lever rotates too far it will cause the cam to come back off the >valves and reengage the parking brake. > >If I remember correctly 90degs is too much lever travel, its more like 45 >degs. > >As stated in other posts, if the compensating valves in the master cylinders >don't open up at the top end of the MC piston travel this will also keep the >brakes on. > >W > > ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)jetstream.net>
Subject: Buying a used engine
Date: Aug 20, 2004
0.3 SUBJ_BUY Subject line starts with Buy or Buying I have bought used engines in the past and have had fairly good luck. From experience I have set myself some guide lines and will pass them on to the list hoping it will help someone and maybe save some heart-ache. I divide the engines into three categories, part time first run that can be put into service without overhaul, part time second run and high time. My first choice is first run part time with good logs that can be verified and the same for second run but must have been overhauled by a reputable overhaul facility and the logs to include a work sheet and parts list for the overhaul. The high time engine is a core only and will be overhauled. The value of the part time engines is based on time on the engine. The value of the high time engine is a guess, it may make a good core or could be a good boat anchor. When I bye a part time engine I take it to a reputable overhaul facility (in my case this would be Aero Sport Power) and have it checked out and run in their test stand. For me this is a must, for safety sake and fairness to your passengers you have to know you have a safe reliable engine up front. In years gone by I have worked in a engine overhaul facility and understand the overhaul process, but am a firm believer in getting my engines overhauled in a good facility. This becomes even more important now with the RV 10 since we will be carrying three passengers. Van' choice of the I0 540 for the 10 has to be the very best as it is one of the most reliable engines ever built. Eustace Bowhay RV 10 40030 Working on the fuselage ________________________________________________________________________________
Date: Aug 20, 2004
From: "thomas a. sargent" <sarg314(at)earthlink.net>
Subject: don't want the engine to fall off.
I'm surprised that the manual says very little about attaching the Dynafocal II engine mount (for RV-6A) to the fuselage. I could use a little guidance here. The pre-drilled bolt holes in my QB fuselage are 1/4", intentionally undersized for the 3/8" bolts in the engine mount. My plan is to get a couple sholder bolts that are 1/4" in the threaded section and 3/8" in the shank and see if I can use those to center the mount on the plane, or at least find a resaonable compromise position. Then using the engine mount as a drill guide, drill the holes out to size with a drill slightly less than 3/8". Then ream the hole out to 3/8". (My mechanical engineer co-workers tell me that reamed holes are significantly stronger.) Is this what most folks do? Or am I missing something obvious? Proceeding carefully here... botching these holes would be REAL BAD. -- Tom Sargent, RV-6A, Landing gear ________________________________________________________________________________
Date: Aug 21, 2004
From: Charlie Kuss <chaztuna(at)adelphia.net>
Subject: Re: RV8 one piece wings skins
Tom Was your set pre-punched? I know that Vans has offered 1 piece main skins with no pre-punching for quite a few years. Charlie Kuss > >MIKE-VANS MADE MINE 6 YEARS AGO-WHAT IS A SUPER 8-TOM > >Tom Whelan >Whelan Farms Airport >President EAA Chapter 1097 >wfact01(at)aol.com >249 Hard Hill Road North >PO Box 426 >Bethlehem, CT 06751 >Tel: 203-266-5300 >Fax: 202-266-5140 >EAA Technical/Flight Advisor >RV-8 540 LYC (Engine Runs, Taxi-Tests) >S-51 Mustang Turbine (Under Construction) > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: don't want the engine to fall off.
Date: Aug 20, 2004
Hi Tom, I built the slow built 6a and did pretty much what you describe. Instead of shoulder bolts I used some bushings on 1/4" bolts. I centered the mount over the two holes that gave me the best average fit for the rest of the holes and bolted the engine mount down. I then used some more bushings to re-center drill the remaining slightly off center firewall mount holes. Next I used the mount itself as a guide to drill the fierwall holes to final size. The reammer sure can't hurt, weather or not it is needed in this case I'll leave up to the experts to have fun with.{[B-)! HuH!, quick build EH! (;-)! Jim in Kelowna ----- Original Message ----- From: "thomas a. sargent" <sarg314(at)earthlink.net> Subject: RV-List: don't want the engine to fall off. > > I'm surprised that the manual says very little about attaching the > Dynafocal II engine mount (for RV-6A) to the fuselage. I could use a > little guidance here. > > The pre-drilled bolt holes in my QB fuselage are 1/4", intentionally > undersized for the 3/8" bolts in the engine mount. My plan is to get a > couple sholder bolts that are 1/4" in the threaded section and 3/8" in > the shank and see if I can use those to center the mount on the plane, > or at least find a resaonable compromise position. > > Then using the engine mount as a drill guide, drill the holes out to > size with a drill slightly less than 3/8". Then ream the hole out to > 3/8". (My mechanical engineer co-workers tell me that reamed holes are > significantly stronger.) > > Is this what most folks do? Or am I missing something obvious? > > Proceeding carefully here... botching these holes would be REAL BAD. > > -- > Tom Sargent, RV-6A, Landing gear > > ________________________________________________________________________________
Date: Aug 21, 2004
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: RV8 one piece wings skins
> > >I would also be interested in knowing what strength increase could be >expected from a change from 025 to 032 skins if anyone happens to know >(or swag) this off the top of their heads. Sure, the outboard wing would be a bit stronger, but the inboard wing would be the same as before. The extra strength in the outboard wing is irrelevant, as a chain is only as strong as the weakest link. If you want one piece wing skins, go ahead. But don't use extra strength as an argument for the mod. -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Wing Twist
Date: Aug 21, 2004
I am at the stage of drilling the rear wing attachment bolts on my RV-4 and have discovered I have about a 1/4" wash out in the left wing. Dont know how I got that and it doesn't matter at this point but I am seeking the list's collective wisdom on the best remedy for this. I am thinking that perhaps the best thing to do is to "average" the twist's effect by lessening the incidence on the side with the twist. In other words, if the tip has in effect 1/4"more incidence when the root has the same incidence as the other straight wing I would drill the hole such that the twisted wing has 1/8" less incidence at the root so that the "average" along the span is the same. Not optimal, of course but there is no way to straighten the wing with the skins now on it.. I realize that measuring this is difficult and I may have some measurement errors as well so I don't want to get too anal on this. Van's instructions suggest getting the wings square and the sweep alignment within 1/2" or so is OK (their "get real" statement in the supplementary instructions) but I am sure I will have some slight rolling moment if the wings are not straight in incidence. This is a pain and I have no idea how the twist crept into the wing while riveting the skins. The twist seems to be gradual along the entire length of the wing panel as opposed to localized at the tip region. Thoughts? ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: Compass liquid
Date: Aug 21, 2004
Naphtha is another name for white Gasoline. You certainly don't want highly flammable gas in your compass and cockpit. Cy Galley Safety Programs Editor Always looking for ideas and articles for EAA Sport Pilot ----- Original Message ----- From: "Rhett Westerman" <Rhettwesterman(at)cox.net> Subject: RE: RV-List: Compass liquid > > Use Naptha > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Chuck > To: rv-list(at)matronics.com > Subject: Re: RV-List: Compass liquid > > > Matthew, > > I think I've still got a few compass overhaul kits and a pint of compass > fluid kickin' around. If you're interested I go search. If I find 'em you > can have 'em, just reimburse me for the shipping. > > Chuck > > don't archive > > Matthew Brandes wrote: > > I picked up a used compass that has a low liquid level. What can I use to > replenish/replace it? > > Matthew Brandes, > Van's RV-9A (Fuselage) > EAA Chapter 868/91/1329 > www.n523rv.com > > > --------------------------------- > > ________________________________________________________________________________
From: WFACT01(at)aol.com
Date: Aug 21, 2004
Subject: Re: RV8 one piece wings skins
CHARLIE-Yes they were pre punched-TOM Tom Whelan Whelan Farms Airport President EAA Chapter 1097 wfact01(at)aol.com 249 Hard Hill Road North PO Box 426 Bethlehem, CT 06751 Tel: 203-266-5300 Fax: 202-266-5140 EAA Technical/Flight Advisor RV-8 540 LYC (Engine Runs, Taxi-Tests) S-51 Mustang Turbine (Under Construction) ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: Wing Twist
Date: Aug 21, 2004
Once upon a time, someone from Van's (perhaps Bill Benedict, when he used to post to the list), suggested choosing a reference point at 2/3 span to set incidence. A good search of the archives might (or might not) find this note. KB ----- Original Message ----- From: "Richard Bibb" <rebibb(at)comcast.net> Subject: RV-List: Wing Twist > > I am at the stage of drilling the rear wing attachment bolts on my RV-4 and > have discovered I have about a 1/4" wash out in the left wing. Dont know > how I got that and it doesn't matter at this point but I am seeking the > list's collective wisdom on the best remedy for this. > > I am thinking that perhaps the best thing to do is to "average" the twist's > effect by lessening the incidence on the side with the twist. In other > words, if the tip has in effect 1/4"more incidence when the root has the > same incidence as the other straight wing I would drill the hole such that > the twisted wing has 1/8" less incidence at the root so that the "average" > along the span is the same. Not optimal, of course but there is no way to > straighten the wing with the skins now on it.. > > I realize that measuring this is difficult and I may have some measurement > errors as well so I don't want to get too anal on this. Van's instructions > suggest getting the wings square and the sweep alignment within 1/2" or so > is OK (their "get real" statement in the supplementary instructions) but I > am sure I will have some slight rolling moment if the wings are not straight > in incidence. This is a pain and I have no idea how the twist crept into > the wing while riveting the skins. > > The twist seems to be gradual along the entire length of the wing panel as > opposed to localized at the tip region. > > Thoughts? > > ________________________________________________________________________________
Date: Aug 21, 2004
From: Jim Streit <wooody04(at)bellsouth.net>
Subject: Re: Compass liquid
kerosene is "liquid" used in compasses Matthew Brandes wrote: > >I picked up a used compass that has a low liquid level. What can I use to >replenish/replace it? > >Matthew Brandes, >Van's RV-9A (Fuselage) >EAA Chapter 868/91/1329 >www.n523rv.com <http://www.n523rv.com/> > > > > ________________________________________________________________________________
From: Bluecavu(at)aol.com
Date: Aug 21, 2004
Subject: Question for the aerodynamycists
>I am going to install a NACA vent on the side of the forward fuselage on the RV-4 I am rebuilding.=A0 I am thinking of installing it right below the cowl cheek angled downward so that the longitudinal axis of the vent is parallel to the logitudnal axis of the cowl cheek extension.=A0 My thought is the pressure will be positive in this area < I have one there on my -4 on the left side for the reasons you stated. Works *very* well (you could style your hair in front of it). I am thinking of adding another on the right side -but haven't gotten around to it. My vent is level with the longitudinal axis of the fuse (I squared it to the lower cowl/fuse line as I recall). It also looks good this way -as the vent angle goes the opposite direction from the cheek angles. Scott N4ZW ________________________________________________________________________________
Date: Aug 21, 2004
From: Skylor Piper <skylor4(at)yahoo.com>
Subject: Re: RV8 one piece wings skins
--- Kevin Horton wrote: > Sure, the outboard wing would be a bit stronger, but > the inboard wing > would be the same as before. The extra strength in > the outboard wing > is irrelevant...snip... > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada > http://go.phpwebhosting.com/~khorton/rv8/ Are you sure about that? The two RV-8's that had in-flight structural failures (that I know about) had the wings fail right at the inboard edge of the aileron. __________________________________ ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: RV8 one piece wings skins
Date: Aug 21, 2004
Two? I think we're all aware of the factory aircraft crashing, but what was the other one? KB ----- Original Message ----- From: "Skylor Piper" <skylor4(at)yahoo.com> Subject: Re: RV-List: RV8 one piece wings skins > > > --- Kevin Horton wrote: > > > Sure, the outboard wing would be a bit stronger, but > > the inboard wing > > would be the same as before. The extra strength in > > the outboard wing > > is irrelevant...snip... > > > Kevin Horton RV-8 (finishing kit) > > Ottawa, Canada > > http://go.phpwebhosting.com/~khorton/rv8/ > > Are you sure about that? The two RV-8's that had > in-flight structural failures (that I know about) had > the wings fail right at the inboard edge of the aileron. > > > __________________________________ > > ________________________________________________________________________________
Date: Aug 21, 2004
From: Jerry Springer <jsflyrv(at)earthlink.net>
Subject: Re: RV8 one piece wings skins
Skylor Piper wrote: > > >--- Kevin Horton wrote: > > > >>Sure, the outboard wing would be a bit stronger, but >>the inboard wing >>would be the same as before. The extra strength in >>the outboard wing >>is irrelevant...snip... >> >> > > > >>Kevin Horton RV-8 (finishing kit) >>Ottawa, Canada >>http://go.phpwebhosting.com/~khorton/rv8/ >> >> > >Are you sure about that? The two RV-8's that had >in-flight structural failures (that I know about) had >the wings fail right at the inboard edge of the aileron. > > > > > Skylor what were the deaails of the second in flight failure? Jerry ________________________________________________________________________________
Date: Aug 21, 2004
Subject: [ Pat Long ] : New Email List Photo Share Available!
From: Email List Photo Shares <pictures(at)matronics.com>
A new Email List Photo Share is available: Poster: Pat Long Subject: Vernatherm http://www.matronics.com/photoshare/PGLong@aol.com.08.21.2004/index.html o Main Photo Share Index http://www.matronics.com/photoshare o Submitting a Photo Share If you wish to submit a Photo Share of your own, please include the following information along with your email message and files: 1) Email List or Lists that they are related to: 2) Your Full Name: 3) Your Email Address: 4) One line Subject description: 5) Multi-line, multi-paragraph description of topic: 6) One-line Description of each photo or file: Email the information above and your files and photos to: pictures(at)matronics.com ________________________________________________________________________________
Date: Aug 21, 2004
Subject: [ Bobby Hester ] : New Email List Photo Share Available!
From: Email List Photo Shares <pictures(at)matronics.com>
A new Email List Photo Share is available: Poster: Bobby Hester Subject: Matco Parking Brake http://www.matronics.com/photoshare/bhester@hopkinsville.net.08.21.2004/index.html o Main Photo Share Index http://www.matronics.com/photoshare o Submitting a Photo Share If you wish to submit a Photo Share of your own, please include the following information along with your email message and files: 1) Email List or Lists that they are related to: 2) Your Full Name: 3) Your Email Address: 4) One line Subject description: 5) Multi-line, multi-paragraph description of topic: 6) One-line Description of each photo or file: Email the information above and your files and photos to: pictures(at)matronics.com ________________________________________________________________________________
Date: Aug 19, 2004
Subject: Re: Compass liquid
From: Bruce Green <mailindex(at)juno.com>
Years ago, I used some baby oil. Didn't freeze and damped the compass somewhat. > > The Rec. Aviation Homebuilt site on Google had quite a discussion on > this > some time back. One party finally settled on Toner for copy > machine. He said it > is slightly more viscous than the original and was clear. Maybe > easier on > gaskets too ? > I intend to use it in mine,soon. > > > Bob Olds RV-4 , N1191X > A&P , EAA Tech. Counselor > Charleston,Arkansas > Real Aviators Fly Taildraggers > > > > > > > > > > > ________________________________________________________________________________
Date: Aug 21, 2004
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Wing Twist
You definitely should use a reference point further out than mid-span. A left-to-right difference in incidence will have more effect on the outboard wing than the inboard wing, as it has a longer moment to work with. I don't feel like crunching the math, but Kyle's 2/3 span number feels correct intuitively to me. Kevin Horton > >Once upon a time, someone from Van's (perhaps Bill Benedict, when he used to >post to the list), suggested choosing a reference point at 2/3 span to set >incidence. A good search of the archives might (or might not) find this >note. > >KB >----- Original Message ----- >From: "Richard Bibb" <rebibb(at)comcast.net> >To: >Subject: RV-List: Wing Twist > > >> >> I am at the stage of drilling the rear wing attachment bolts on my RV-4 >and >> have discovered I have about a 1/4" wash out in the left wing. Dont know >> how I got that and it doesn't matter at this point but I am seeking the >> list's collective wisdom on the best remedy for this. >> >> I am thinking that perhaps the best thing to do is to "average" the >twist's >> effect by lessening the incidence on the side with the twist. In other >> words, if the tip has in effect 1/4"more incidence when the root has the >> same incidence as the other straight wing I would drill the hole such that >> the twisted wing has 1/8" less incidence at the root so that the "average" >> along the span is the same. Not optimal, of course but there is no way to >> straighten the wing with the skins now on it.. >> >> I realize that measuring this is difficult and I may have some measurement >> errors as well so I don't want to get too anal on this. Van's >instructions >> suggest getting the wings square and the sweep alignment within 1/2" or so >> is OK (their "get real" statement in the supplementary instructions) but I >> am sure I will have some slight rolling moment if the wings are not >straight >> in incidence. This is a pain and I have no idea how the twist crept into >> the wing while riveting the skins. >> >> The twist seems to be gradual along the entire length of the wing panel as >> opposed to localized at the tip region. >> > > Thoughts? >> > > ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: RV8 one piece wings skins
Date: Aug 21, 2004
WELL SAID KEVIN!!!! I see this all to often in a growing number of homebuilders lately. For example (and one I see quite a bit).....If AWG16 wire is sufficient to the wingtip, why don't I go ahead and run AWG14, AWG12 or even AWG10 wire out there?!?!? If I need AWG18 for master relay power, why not run AWG16 or AWG14?!? Far too many people are making "improvements" based on something they hear 3rd hand, or just simply assume that "if some is good, more must be better, and most must be best"! I'm really not harping here, just relating a fact that I'm seeing more and more in the past year or two. Airplane structures, systems, electronics, etc.. are not simple "linear equations" where more of everything is better, sometimes yes, but certainly not always. Now I'm not saying you should abandon any improvements. Certainly there are a some areas where people have learned by experience that additional metal, thicker wire, etc.. are better. That being said, just because you "heard it from some old guy who used to work on airplanes in the 40's", doesn't mean it applies to these RV's exactly. Another reason I see people doing "things" is that they saw or heard of someone else doing it and think by association that therefore it must be good. Once again, sometimes yes, but not always. Anyway, just be smart about it and happy building. Lot's of smart people out there building lot's of nice airplane. Many of them better than mine (but not all)!! Cheers, Stein Bruch RV6's, Minneapolis -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Kevin Horton Subject: RE: RV-List: RV8 one piece wings skins Well, the problem is we don't know what was going on in that accident, so it is very hard to know what loads the wing experienced. How fast were they going, what was the aircraft weight and CG, how many g were pulled, were the ailerons deflected, etc. Yes, maybe thicker lower wing skins could have allowed that part of the wing to carry the loads that were applied to it. Or maybe not. And even if that part of the wing could carry those loads, we have now changed the way the loads are distributed on the wing, so we don't know where the weak link is, and how much load the weakest part of the wing could carry before it fails. I'm aware of at least two incidents where RV-8s have had landing gear box failure during landing, and one case where an RV-8A had a nose wheel leg collapse. Should builders arbitrarily beef up the landing gear box and nose landing gear legs too? Where does it end? A heavier aircraft is less safe than a lighter aircraft, as the stall speed is higher, which means the lowest possible touchdown speed is higher. The structure of the heavier aircraft has to carry higher loads for a given manoeuvre, so it is more likely to fail. The best answer is to carefully design the aircraft to be just strong enough to withstand the design loads, and to operate the aircraft so the design loads are not exceeded. Just adding structure on the "That Looks About Right" principle just changes the stress distribution, and puts higher loads somewhere else. I'm not a structures engineer, so all the above is worth what you paid for it. I do have a mechanical engineering degree, but have never really used it in anger. Kevin Horton ________________________________________________________________________________
From: "RV_8 Pilot" <rv_8pilot(at)hotmail.com>
Subject: RV8 one piece wings skins
Date: Aug 21, 2004
When was the second RV-8 structural (in-flight) failure?? IMVHO, as a non-practicing engineer, I believe there would be some small structural benefit from single piece and/or thicker wing skins. But I also couldn't agree more that lighter airplanes are better all the way around - more efficient, faster, less damage with hard or crash landings. I feel very comfortable flying my -8 the way I do with standard lap-jointed skins. 2 Bryan ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Aug 21, 2004
Subject: Re: Compass liquid
In a message dated 8/21/2004 11:57:47 AM Pacific Daylight Time, mailindex(at)juno.com writes: Years ago, I used some baby oil. Didn't freeze and damped the compass somewhat. ============================================= I've always wondered whether DOT 5 brake fluid wouldn't be the most ideal compass fluid. GV (RV-6A N1GV O-360-A1A C/S, flying 708 hrs) ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Aug 21, 2004
Subject: Re: Camping at Copperstate
In a message dated 8/21/2004 5:04:12 PM Pacific Daylight Time, svanarts(at)yahoo.com writes: Anyone on the list ever tent camped at Copperstate? How's access to food? (It's dismal if you arrive early at OSH) What's the weather like that time of year? Would I be better off in a hotel? ============================================ Weather is still warm. The grounds there were messy due to blowing dirt and hay last year. We had a motel in Casa Grande and would recommend this again, although they indicated that they were going to be planting grass thruout. GV (RV-6A N1GV O-360-A1A C/S, flying 708 hrs) ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: Camping at Copperstate
Date: Aug 21, 2004
Hot and cool. Could be too hot, depending on the year. They do NOT have grass throughout. Most of it is dead, but they are trying to bring it back. I'd recommend the motels in Casa Grande as well. I fly over (and land at) PRA just about every day. I'll keep checking it out. Paul Besing RV-6A Sold (RV-10 Soon) http://www.lacodeworks.com/besing Kitlog Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: <Vanremog(at)aol.com> Subject: Re: RV-List: Camping at Copperstate > > > In a message dated 8/21/2004 5:04:12 PM Pacific Daylight Time, > svanarts(at)yahoo.com writes: > > Anyone on the list ever tent camped at Copperstate? How's access to food? > (It's dismal if you arrive early at OSH) What's the weather like that time of > year? Would I be better off in a hotel? > > > ============================================ > > Weather is still warm. The grounds there were messy due to blowing dirt and > hay last year. We had a motel in Casa Grande and would recommend this > again, although they indicated that they were going to be planting grass thruout. > > > GV (RV-6A N1GV O-360-A1A C/S, flying 708 hrs) > > ________________________________________________________________________________
From: DOUGPFLYRV(at)aol.com
Date: Aug 22, 2004
Subject: Re: Fortune Magazine - Nice article on Vans!
In a message dated 8/12/2004 1:31:21 PM Central Standard Time, jhelms(at)i1.net writes: http://www.fortune.com/fortune/smallbusiness/roi/articles/0,15114,654762,00. html HAS ANYONE DOWNLOADED THIS ARTICLE ? I AM UNABLE TO LOCATE IT ON THE WEBSITE. WOULD GREATLY APPRECIATE A COPY OFF LIST. THANKS, DOUG PRESTON DOUGPFLYRV(at)AOL.COM ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: Fortune Magazine - Nice article on Vans!
Date: Aug 22, 2004
After the down load fails, select the address, right arrow and type ".html" on the end without the quotes. Works fine. ----- Original Message ----- From: <DOUGPFLYRV(at)aol.com> Subject: Re: RV-List: Fortune Magazine - Nice article on Vans! > > In a message dated 8/12/2004 1:31:21 PM Central Standard Time, jhelms(at)i1.net > writes: > http://www.fortune.com/fortune/smallbusiness/roi/articles/0,15114,654762,00. > html > HAS ANYONE DOWNLOADED THIS ARTICLE ? I AM UNABLE TO LOCATE IT ON THE > WEBSITE. WOULD GREATLY APPRECIATE A COPY OFF LIST. > > THANKS, > > DOUG PRESTON > DOUGPFLYRV(at)AOL.COM > > ________________________________________________________________________________
Date: Aug 22, 2004
Subject: [ Gary Gunn ] : New Email List Photo Share Available!
From: Email List Photo Shares <pictures(at)matronics.com>
A new Email List Photo Share is available: Poster: Gary Gunn Subject: Grand Canyon http://www.matronics.com/photoshare/ggunn@qwest.net.08.22.2004/index.html o Main Photo Share Index http://www.matronics.com/photoshare o Submitting a Photo Share If you wish to submit a Photo Share of your own, please include the following information along with your email message and files: 1) Email List or Lists that they are related to: 2) Your Full Name: 3) Your Email Address: 4) One line Subject description: 5) Multi-line, multi-paragraph description of topic: 6) One-line Description of each photo or file: Email the information above and your files and photos to: pictures(at)matronics.com ________________________________________________________________________________
Date: Aug 22, 2004
From: "thomas a. sargent" <sarg314(at)earthlink.net>
Subject: Flight Grip stick grips
Has any one on the list installed Flight Grip stick grips in their plane? Even if you just checked one out at Oshkosh, I'd be interested to hear opinions about how it fit your hand and how the switches felt, etc.. Thanks, -- Tom Sargent, RV-6A, Landing gear ________________________________________________________________________________
From: DOUGPFLYRV(at)aol.com
Date: Aug 22, 2004
Subject: Re: Fortune Magazine - Nice article on Vans!
Thanks ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
"'owner-rv-list-server(at)matronics.com '"(at)matronics.com
Subject: wing wash out
Date: Aug 22, 2004
In my opinion the most important aspect of setting the wing is to be dang sure there is proper edge distance on the rear spar flanges. Having measured a number of aurplanes and RVs for general rigging I can assure that its amazing what will fly relatively straight. A 1/4" washout won't do anything, most likely. If it does introduce anything it would be most likely only be noticed during a stall, translated to a general preference to go one way over the other. If you ran your riveting process from one end to the other, then that is what probably introduced the shift, as the metal surrounding the rivet holes is stretched, and will introduce accumlative shift over a long run. The worst case would be to do one side (top or bottom) one way, then the other side the opposite way, then do something different on the other wing. As a general rule though, during rigging shoot for symetry, and average out where its not possible to get exact symetry. Using the span point of 1/2 or 2/3s will do, and I doubt one could ever tell the difference in performance effects using one vs the other. Get it close without going nutso on it, as you will need to make final adjustments by flying it rather than measuring things no matter how much you measure it now. Just think about the difference in relative angle of wind on the left side vs the right side in the prop influence area, yet they all seem to fly just fine even if they are perfectly symetrical. Robust structure is far more important on these aircraft than is precise rigging. W ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
"'owner-rv-list-server(at)matronics.com '"(at)matronics.com
Subject: engine timing vs CHTs/EGTs
Date: Aug 22, 2004
Well, once again the list provided a useful jog to my rapidly degrading mental faculties. After a recent discussion with Andre B. re his fuel injection problems he reminded me of an old Lycoming service letter which allows most of the IO-360s to have their timing retarded to 20 degs from the normal factory setting of 25 degs used for most Lycoming engines. Although the SL doesn't fully explain this, it is an option for those engine installations where detonation and cooling are an issue. For some strange reason this finally gelled in my head with the previous thirty years of experience floating around in there and answered the question I have had in my head as to why many RVs have such a wide range of CHTs from one aircraft to the next given they all have the same relative engines(mostly). Years ago I worked in a shop where we had this strange little Mercedes two seater with a big ass engine in it. The engine was fairly high time and the owner was always complaining about how hot the thing ran. So we eventually went through everything including a complete teardown overhaul, reteardown and I finally ended up calling up the old guy in Germany who said the timing specs for that engine were wrong and to back them off two degrees. I whined about this until as it couldn't possibly have that much effect. He promtly reminded me who the old guy was and told me to just shut up and do it. Dang old guy was right, two degrees of timing retard had a major effect on the operating temperature of that engine. Then later on I had a few customers who regularly got stuck in border traffic so I retarded their timing a few degrees and voila, same thing, cooler temps. So, having had several conversations with many of you about CHTs being kinda cold, or hot, once this re-epiphany fired from my left neuron to my right neuron I decided to give it a try. At 26 degs BTDC my CHTs are about 440 during a long climb out, and on a hot day will go beyond 450 if I don't drop the nose. EGTs tend to stay about 1250 when leaned to short of peak. After a couple of initial flights yesterday with the timing set at 22.5 degs BTDC my CHTs were in the 325 to 350 range and the EGTs were up around 1425. Now this jives with what I would think would happen as the heat, being started later, is now getting more rejection through the exhaust, but I am very suprised at how much change occured between a shift of 3.5 degrees. Since I have the cheapo CHT/EGT gauge with the funcky switches I am not very confident in any hard numbers I am listing here, but the relative change does seem to be significant. Now, with all that said one might then want to discuss the effect retarding or advancing timing will have on power. In general retarding timing away from that maximum point where the engine will begin to misfire or detonate will reduce power as it shifts the maximum centroid of pressure away from that optimum range where the pressure cycle will be fully utilized converting to the most rotational power into the crankshaft. (energy conversion cyclically changes from 0% at 0degsTDC to 100% at 90degsATDC) But this would only be noticed at full power since aircraft engines don't vary timing with engine RPM or load as cars do. Well I didn't notice any loss at full blast going down the runway, which is the only time I ever plow around at that power setting. In fact it seemed to me that the engine was running a tad bit smoother so may have actually felt a little more powerful. (truely a subjective comment based upon not one schred of empirical evidence) In truth what has happened is this. There is some RPM value to which Lycoming's setting of 25 degs causes the most efficeint conversion of pressure into torque, (I would guess roughly 2300 to 2400 RPM) By changing the timing one is just shifting where this occurs on the RPM scale. Since reciprocating engines will vary power output with changes in timing at max RPM, but if you don't fly at that RPM much, than your power really won't be effected by a small change in timing. You might notice a slight change in control knob position for a known MAP/RPM setting, but if you set it to that MAP/RPM it will still produce the same power as before, or at least so close that you wouldn't be able to tell the difference. I'm thinking the same will be true for fuel efficiency, but will have to fly awhile to prove that. So, if your CHTS are very low, or too hgh, check your timing and try moving it few degrees(retard for cooler, advanced for hotter). I would not recommend going over 25 degs though as these aircooled engines are low RPM, large piston, thermally critical assemblies, just looking for a detonation to happen. The last thing I want to say is that I played with getting the timing exact between the mags vs being about a deg off from each other. Although I never flew with them at very different settings, it did ground run noticeably smoother with them set as close to each other as possible. (one degree off was amazingly rougher at 1500 RPM) So if some of y'all with them fancy recording engine things wanted to try this I would love to see the hard EGT/CHT data from say 25 degs vs 22.5 degs at max effort and cruise climb. (I know its a total pain to get the cowl off and change this a few times, particularly if the gasket tears as it did on my left mag, but if you're in there tinkering, it would be way cool to see hard accurate data) W ________________________________________________________________________________
Date: Aug 22, 2004
From: Scott Vanartsdalen <svanarts(at)yahoo.com>
Subject: Re: Camping at Copperstate
Ah... Never trust a picture on a website. I'll be there too. Shuttling between Holiday Inn and the airport. Thanks for the 411. Besing" Hot and cool. Could be too hot, depending on the year. They do NOT have grass throughout. Most of it is dead, but they are trying to bring it back. I'd recommend the motels in Casa Grande as well. I fly over (and land at) PRA just about every day. I'll keep checking it out. Paul Besing RV-6A Sold (RV-10 Soon) http://www.lacodeworks.com/besing Kitlog Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: Subject: Re: RV-List: Camping at Copperstate > > > In a message dated 8/21/2004 5:04:12 PM Pacific Daylight Time, > svanarts(at)yahoo.com writes: > > Anyone on the list ever tent camped at Copperstate? How's access to food? > (It's dismal if you arrive early at OSH) What's the weather like that time of > year? Would I be better off in a hotel? > > > ============================================ > > Weather is still warm. The grounds there were messy due to blowing dirt and > hay last year. We had a motel in Casa Grande and would recommend this > again, although they indicated that they were going to be planting grass thruout. > > > GV (RV-6A N1GV O-360-A1A C/S, flying 708 hrs) > > -- Scott VanArtsdalen RV-4 N311SV, FLYING!! When a man does all he can though it succeeds not well, blame not him that did it." -- George Washington ________________________________________________________________________________
Date: Aug 22, 2004
From: Charlie Kuss <chaztuna(at)adelphia.net>
Subject: Re: engine timing vs CHTs/EGTs
Wheeler, What the hell is wrong with you! You one of them damned radicals who actually thinks that one repeatable test is worth a thousand expert opinions??? :-) You hit the nail on the head, as usual. Charlie Kuss > >Well, > >once again the list provided a useful jog to my rapidly degrading mental >faculties. After a recent discussion with Andre B. re his fuel injection >problems he reminded me of an old Lycoming service letter which allows most >of the IO-360s to have their timing retarded to 20 degs from the normal >factory setting of 25 degs used for most Lycoming engines. Although the SL >doesn't fully explain this, it is an option for those engine installations >where detonation and cooling are an issue. > >For some strange reason this finally gelled in my head with the previous >thirty years of experience floating around in there and answered the >question I have had in my head as to why many RVs have such a wide range of >CHTs from one aircraft to the next given they all have the same relative >engines(mostly). > >Years ago I worked in a shop where we had this strange little Mercedes two >seater with a big ass engine in it. The engine was fairly high time and the >owner was always complaining about how hot the thing ran. So we eventually >went through everything including a complete teardown overhaul, reteardown >and I finally ended up calling up the old guy in Germany who said the timing >specs for that engine were wrong and to back them off two degrees. I whined >about this until as it couldn't possibly have that much effect. He promtly >reminded me who the old guy was and told me to just shut up and do it. Dang >old guy was right, two degrees of timing retard had a major effect on the >operating temperature of that engine. > >Then later on I had a few customers who regularly got stuck in border >traffic so I retarded their timing a few degrees and voila, same thing, >cooler temps. > >So, having had several conversations with many of you about CHTs being kinda >cold, or hot, once this re-epiphany fired from my left neuron to my right >neuron I decided to give it a try. > >At 26 degs BTDC my CHTs are about 440 during a long climb out, and on a hot >day will go beyond 450 if I don't drop the nose. EGTs tend to stay about >1250 when leaned to short of peak. > >After a couple of initial flights yesterday with the timing set at 22.5 degs >BTDC my CHTs were in the 325 to 350 range and the EGTs were up around 1425. > >Now this jives with what I would think would happen as the heat, being >started later, is now getting more rejection through the exhaust, but I am >very suprised at how much change occured between a shift of 3.5 degrees. > >Since I have the cheapo CHT/EGT gauge with the funcky switches I am not very >confident in any hard numbers I am listing here, but the relative change >does seem to be significant. > >Now, with all that said one might then want to discuss the effect retarding >or advancing timing will have on power. In general retarding timing away >from that maximum point where the engine will begin to misfire or detonate >will reduce power as it shifts the maximum centroid of pressure away from >that optimum range where the pressure cycle will be fully utilized >converting to the most rotational power into the crankshaft. (energy >conversion cyclically changes from 0% at 0degsTDC to 100% at 90degsATDC) > >But this would only be noticed at full power since aircraft engines don't >vary timing with engine RPM or load as cars do. Well I didn't notice any >loss at full blast going down the runway, which is the only time I ever plow >around at that power setting. In fact it seemed to me that the engine was >running a tad bit smoother so may have actually felt a little more powerful. >(truely a subjective comment based upon not one schred of empirical >evidence) > >In truth what has happened is this. There is some RPM value to which >Lycoming's setting of 25 degs causes the most efficeint conversion of >pressure into torque, (I would guess roughly 2300 to 2400 RPM) By changing >the timing one is just shifting where this occurs on the RPM scale. Since >reciprocating engines will vary power output with changes in timing at max >RPM, but if you don't fly at that RPM much, than your power really won't be >effected by a small change in timing. You might notice a slight change in >control knob position for a known MAP/RPM setting, but if you set it to that >MAP/RPM it will still produce the same power as before, or at least so close >that you wouldn't be able to tell the difference. I'm thinking the same will >be true for fuel efficiency, but will have to fly awhile to prove that. > >So, > >if your CHTS are very low, or too hgh, check your timing and try moving it >few degrees(retard for cooler, advanced for hotter). I would not recommend >going over 25 degs though as these aircooled engines are low RPM, large >piston, thermally critical assemblies, just looking for a detonation to >happen. > >The last thing I want to say is that I played with getting the timing exact >between the mags vs being about a deg off from each other. Although I never >flew with them at very different settings, it did ground run noticeably >smoother with them set as close to each other as possible. (one degree off >was amazingly rougher at 1500 RPM) > >So if some of y'all with them fancy recording engine things wanted to try >this I would love to see the hard EGT/CHT data from say 25 degs vs 22.5 degs >at max effort and cruise climb. (I know its a total pain to get the cowl off >and change this a few times, particularly if the gasket tears as it did on >my left mag, but if you're in there tinkering, it would be way cool to see >hard accurate data) > >W > > ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: Navaid problem
Date: Aug 22, 2004
I am asking this for a friend who is having problems with his Navaid. He has the Navaid coupled to a Garmin 296. When he is intercepting a course, he feels a bump in the stick when he reaches the new course line, but instead of turning on course, it stays on heading and doesn't make the turn. Has anyone had this problem and resolved it? Jerry Calvert Edmond Ok RV6 N296JC ________________________________________________________________________________
From: "Albert Gardner" <spudnut(at)worldnet.att.net>
Subject: Re: Navaid problem
Date: Aug 22, 2004
I'm using a ControlVision to drive my Navaid. If I have the Navaid trim knob set so that I'm offset from the center line of the course, at an intersection the Navaid will sometimes turn the wrong way to intercept the new leg or seem ottherwise confused but if I hold the stick for a few moments it will work OK. Is this your case or will it never intercept the new leg? Albert Gardner RV-9A 872RV Yuma, AZ ----- Original Message ----- From: "Jerry Calvert" <rv6(at)cox.net> Subject: RV-List: Navaid problem > > I am asking this for a friend who is having problems with his Navaid. He has the Navaid coupled to a Garmin 296. When he is intercepting a course, he feels a bump in the stick when he reaches the new course line, but instead of turning on course, it stays on heading and doesn't make the turn. > > Has anyone had this problem and resolved it? > > Jerry Calvert > Edmond Ok > RV6 N296JC ________________________________________________________________________________
Date: Aug 22, 2004
From: "Tim Bryan" <rv6flyer(at)improvementteam.com>
Subject: Wheel Fairings - Balancing Act
Hello Listers, Today I decided to start on my main wheel fairings. (RV-6) I have raised the tail so the plane is in level flight. I snapped a chalk line on the floor right down the center of the fuselage using a plumb at the tail and one at the front center of the firewall. I have a couple of questions about this process. First I am wishing I had done this prior to installing the engine because of the weight. Without the wings installed the plane doesn't seem too terribly stable when the tail is lifted this high. I attached some weight at the tail and tied it down to my lifted plateform. Should be OK. On the other hand, in front the manual says to lift the plane so the main wheels are off the ground 0-1/16th of an inch so the the mains will swing into "no load" free position. I have a cherry picker connected to the engine hook only for stability as I raised the tail but can I effectively and safely pick up the front of the plane with this hook? Second, using my chalk line and trying to get a measurement of the center line on the wheel pants while they are resting unattached on a 1" block of wood sitting on the tire and the tail resting on a coffee can at 8 5/8" off the floor seems like a pretty shakey way to get these things within the 1/4" the plans call for. Does somebody have a suggestion for an easier way to accomplish this process? Trying to get this accomplished reasonably without having a wreck. Any ideas, comments, etc. would be appreciated. Tim Bryan RV-6 N616TB Getting Done This Year! ________________________________________________________________________________
Date: Aug 22, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Navaid problem
Jerry Calvert wrote: > > I am asking this for a friend who is having problems with his Navaid. > He has the Navaid coupled to a Garmin 296. When he is intercepting a > course, he feels a bump in the stick when he reaches the new course > line, but instead of turning on course, it stays on heading and > doesn't make the turn. > > Has anyone had this problem and resolved it? My Navaid *usually* worked quite well at tracking a course if the nose of the plane was pointed nearly at the waypoint when the autopilot was engaged and the trims set properly, but it never was able to consistently intercept a course. From my 450 hrs of experience with the Navaid, I found reliable course intercepts was beyond the capabilities of my Navaid. There is a way to absolutely fix this problem, but it involves leaving the Navaid at home......... :-) Sam Buchanan (RV-6, AlTrak and EZ-Pilot autopilots) ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Aug 22, 2004
Subject: Re: Wheel Fairings - Balancing Act
In a message dated 8/22/2004 8:08:45 PM Pacific Daylight Time, rv6flyer(at)improvementteam.com writes: Today I decided to start on my main wheel fairings. (RV-6) I have raised the tail so the plane is in level flight. I snapped a chalk line on the floor right down the center of the fuselage using a plumb at the tail and one at the front center of the firewall. I have a couple of questions about this process. First I am wishing I had done this prior to installing the engine because of the weight. Without the wings installed the plane doesn't seem too terribly stable when the tail is lifted this high. I attached some weight at the tail and tied it down to my lifted platform. Should be OK. On the other hand, in front the manual says to lift the plane so the main wheels are off the ground 0-1/16th of an inch so the mains will swing into "no load" free position. I have a cherry picker connected to the engine hook only for stability as I raised the tail but can I effectively and safely pick up the front of the plane with this hook? ================================== I would encourage you to use cables or straps to some other portion of the engine mount rather than risk carrying to much mass with the engine hook. Some rope or nylon straps would be better and more stabilizing as you can connect to several more outboard members. GV (RV-6A N1GV O-360-A1A C/S, flying 710 hrs) ________________________________________________________________________________
Date: Aug 22, 2004
From: Skylor Piper <skylor4(at)yahoo.com>
Subject: Re: RV8 one piece wings skins
It's been awhile since I've read the report of the "other" structural failure, and I must admit that I don't recall all the details. I'll see if I can find it this week. I do recall that it was an RV-8 in California on its way to a fly in several years ago. I believe it was VFR into IMC by a non IFR pilot, and a witness saw it come spinning out of the clouds without part of a wing. Like N58RV, the wing failed around the inboard end of the aileron (I recall). I agree with Kevin's point of view that you can't arbitrarily install a heavier one piece skin and expect that will strengthen the wing under all conditions. Lighter planes are definitely better. My only point was that there "may" be some benefit of the heavier one piece skin, at list in the two instances where the wing failed mid span. Ultimately, the answer to the that question lies with a knowledgeable structural engineer or the aircraft designer. Skylor --- Jerry Springer wrote: > > > Skylor Piper wrote: > > > > > > > >--- Kevin Horton wrote: > > > > > > > >>Sure, the outboard wing would be a bit stronger, > but > >>the inboard wing > >>would be the same as before. The extra strength > in > >>the outboard wing > >>is irrelevant...snip... > >> > >> > > > > > > > >>Kevin Horton RV-8 (finishing kit) > >>Ottawa, Canada > >>http://go.phpwebhosting.com/~khorton/rv8/ > >> > >> > > > >Are you sure about that? The two RV-8's that had > >in-flight structural failures (that I know about) > had > >the wings fail right at the inboard edge of the > aileron. > > > > > > > > > > > Skylor what were the deaails of the second in flight > failure? > > Jerry > > > > Contributions > any other > Forums. > > http://www.matronics.com/chat > > http://www.matronics.com/subscription > http://www.matronics.com/FAQ/RV-List.htm > http://www.matronics.com/archives > http://www.matronics.com/photoshare > http://www.matronics.com/emaillists > > > > > > _______________________________ ________________________________________________________________________________
Date: Aug 22, 2004
From: Jerry Springer <jsflyrv(at)earthlink.net>
Subject: Re: RV8 one piece wings skins
Skylor Piper wrote: > >It's been awhile since I've read the report of the >"other" structural failure, and I must admit that I >don't recall all the details. I'll see if I can find >it this week. > > http://www2.ntsb.gov/ntsb/brief.asp?ev_id 031009X01690&key=1 If this is the one you are referring to I do not believe wing skins would have made a difference, nor was it in anyway the fault of the aircraft. If you read the entire report the wings were still attached and both wing leading edges were crushed back. I really hate it when misinformation gets spread around about the airplanes we build and fly. If you have other information I would love to see the report. Jerry ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: Re: Navaid problem
Date: Aug 23, 2004
The virtues of early technology! Thanks Sam, Jerry Calvert Edmond Ok RV6 N296JC ----- Original Message ----- From: "Sam Buchanan" <sbuc(at)hiwaay.net> Subject: Re: RV-List: Navaid problem > > Jerry Calvert wrote: > > > > > I am asking this for a friend who is having problems with his Navaid. > > He has the Navaid coupled to a Garmin 296. When he is intercepting a > > course, he feels a bump in the stick when he reaches the new course > > line, but instead of turning on course, it stays on heading and > > doesn't make the turn. > > > > Has anyone had this problem and resolved it? > > > My Navaid *usually* worked quite well at tracking a course if the nose > of the plane was pointed nearly at the waypoint when the autopilot was > engaged and the trims set properly, but it never was able to > consistently intercept a course. From my 450 hrs of experience with the > Navaid, I found reliable course intercepts was beyond the capabilities > of my Navaid. > > There is a way to absolutely fix this problem, but it involves leaving > the Navaid at home......... :-) > > Sam Buchanan (RV-6, AlTrak and EZ-Pilot autopilots) > > ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: Re: Navaid problem
Date: Aug 23, 2004
It never intercepts the course. Just a twitch in the stick as it goes by the course.Thanks for the input. Jerry Calvert Edmond Ok RV6 N29JC ----- Original Message ----- From: "Albert Gardner" <spudnut(at)worldnet.att.net> Subject: Re: RV-List: Navaid problem > > I'm using a ControlVision to drive my Navaid. If I have the Navaid trim knob > set so that I'm offset from the center line of the course, at an > intersection the Navaid will sometimes turn the wrong way to intercept the > new leg or seem ottherwise confused but if I hold the stick for a few > moments it will work OK. Is this your case or will it never intercept the > new leg? > Albert Gardner > RV-9A 872RV > Yuma, AZ > > ----- Original Message ----- > From: "Jerry Calvert" <rv6(at)cox.net> > To: > Subject: RV-List: Navaid problem > > > > > > I am asking this for a friend who is having problems with his Navaid. He > has the Navaid coupled to a Garmin 296. When he is intercepting a course, > he feels a bump in the stick when he reaches the new course line, but > instead of turning on course, it stays on heading and doesn't make the turn. > > > > Has anyone had this problem and resolved it? > > > > Jerry Calvert > > Edmond Ok > > RV6 N296JC > > ________________________________________________________________________________
From: Mlfred(at)aol.com
Date: Aug 23, 2004
Subject: Re:2nd RV8 breakup??
In a message dated 8/23/2004 1:59:48 AM Central Daylight Time, rv-list-digest(at)matronics.com writes: From: Jerry Springer <jsflyrv(at)earthlink.net> Subject: Re: RV-List: RV8 one piece wings skins Skylor Piper wrote: > >It's been awhile since I've read the report of the >"other" structural failure, and I must admit that I >don't recall all the details. I'll see if I can find >it this week. > > http://www2.ntsb.gov/ntsb/brief.asp?ev_id 031009X01690&key=1 If this is the one you are referring to I do not believe wing skins would have made a difference, nor was it in anyway the fault of the aircraft. If you read the entire report the wings were still attached and both wing leading edges were crushed back. I really hate it when misinformation gets spread around about the airplanes we build and fly. If you have other information I would love to see the report. Jerry Hi All: This accident involved my friends Earnest & Marketta Woodard (Falcon 2). I heard nothing of any structural problems, and I seriously doubt any were a factor -- it was yet another case of VFR flight into IMC....ugh... Jerry: If you're going to be the 'Misinformation Cop', you'll have a lot of job security. Regards Mark ________________________________________________________________________________
From: "Ronnie Brown" <romott(at)adelphia.net>
Subject: Re: Navaid problem
Date: Aug 23, 2004
The Navaid Autopilot course tracking mode is a relatively simple automatic controller having only gain control - no integral or derivative control incorporated. It took me a while to figure this out, but here's the deal: The error correction output of the Navaid for course deviation is proportional to the amount of error off course. It does not have any thing to get you completely back on course over time (integral control does this). You have to do provide your own "integral control" with the trim knob. At first, I thought my Navaid was not doing a very good job of tracking course. But after using the trim knob to eliminate course deviation, I have found the Navaid does an excellent job. It just isn't as sophisticated as newer autopilots. But it does do a good job if you understand how to use it. The Navaid manual also states that it is not designed to intercept a course, you have to point your plane in the desired heading before engaging the course tracking mode. Try using the trim knob (left knob) more, you'll be a lot happier with your Navaid. Oh and by the way, the accuracy of GPS makes the Navaid appear less capable - if you were only tracking VOR's and didn't see the course error with such great accuracy (1 degree), you'd not notice the problem so much. Ronnie Brown ________________________________________________________________________________
Date: Aug 23, 2004
From: Skylor Piper <skylor4(at)yahoo.com>
Subject: Re: RV8 one piece wings skins
No, this was not the accident that I was referring. In fact, the texas crash involved a plane that both of my parents had flown in, but that was before it was sold to the owners involved in the accident. --- Jerry Springer wrote: > > > Skylor Piper wrote: > > > > > >It's been awhile since I've read the report of the > >"other" structural failure, and I must admit that I > >don't recall all the details. I'll see if I can > find > >it this week. > > > > > http://www2.ntsb.gov/ntsb/brief.asp?ev_id 031009X01690&key=1 > > > If this is the one you are referring to I do not > believe wing skins > would have made a difference, nor was it in anyway > the fault > of the aircraft. If you read the entire report the > wings were still > attached and both wing leading edges were crushed > back. > I really hate it when misinformation gets spread > around about the > airplanes we build and fly. > > If you have other information I would love to see > the report. > > Jerry > > > > Contributions > any other > Forums. > > http://www.matronics.com/chat > > http://www.matronics.com/subscription > http://www.matronics.com/FAQ/RV-List.htm > http://www.matronics.com/archives > http://www.matronics.com/photoshare > http://www.matronics.com/emaillists > > > > > > __________________________________ ________________________________________________________________________________
Date: Aug 23, 2004
From: Skylor Piper <skylor4(at)yahoo.com>
Subject: Re: RV8 one piece wings skins
OK, this will teach me to "keep my mouth shut" until I have all my facts together. The accident that I was referring to was an RV-3, and the wing separated at the fuselage. Oh well... --- Skylor Piper wrote: > > > It's been awhile since I've read the report of the > "other" structural failure, and I must admit that I > don't recall all the details. I'll see if I can > find > it this week. > > I do recall that it was an RV-8 in California on its > way to a fly in several years ago. I believe it was > VFR into IMC by a non IFR pilot, and a witness saw > it > come spinning out of the clouds without part of a > wing. Like N58RV, the wing failed around the > inboard > end of the aileron (I recall). > > I agree with Kevin's point of view that you can't > arbitrarily install a heavier one piece skin and > expect that will strengthen the wing under all > conditions. Lighter planes are definitely better. > > My only point was that there "may" be some benefit > of > the heavier one piece skin, at list in the two > instances where the wing failed mid span. > Ultimately, > the answer to the that question lies with a > knowledgeable structural engineer or the aircraft > designer. > > Skylor > > --- Jerry Springer wrote: > > > > > > > Skylor Piper wrote: > > > > > > > > > > > > >--- Kevin Horton wrote: > > > > > > > > > > > >>Sure, the outboard wing would be a bit stronger, > > but > > >>the inboard wing > > >>would be the same as before. The extra strength > > in > > >>the outboard wing > > >>is irrelevant...snip... > > >> > > >> > > > > > > > > > > > >>Kevin Horton RV-8 (finishing kit) > > >>Ottawa, Canada > > >>http://go.phpwebhosting.com/~khorton/rv8/ > > >> > > >> > > > > > >Are you sure about that? The two RV-8's that had > > >in-flight structural failures (that I know about) > > had > > >the wings fail right at the inboard edge of the > > aileron. > > > > > > > > > > > > > > > > > Skylor what were the deaails of the second in > flight > > failure? > > > > Jerry > > > > > > > > Contributions > > any other > > Forums. > > > > http://www.matronics.com/chat > > > > http://www.matronics.com/subscription > > http://www.matronics.com/FAQ/RV-List.htm > > http://www.matronics.com/archives > > http://www.matronics.com/photoshare > > http://www.matronics.com/emaillists > > > > > > > > > > > > > > > > _______________________________ > > > > Contributions > any other > Forums. > > http://www.matronics.com/chat > > http://www.matronics.com/subscription > http://www.matronics.com/FAQ/RV-List.htm > http://www.matronics.com/archives > http://www.matronics.com/photoshare > http://www.matronics.com/emaillists > > > > > > __________________________________ ________________________________________________________________________________
Date: Aug 23, 2004
From: Scott Bilinski <bilinski@kyocera-wireless.com>
Subject: Re: RV8 one piece wings skins
Can you be more specific? A accident like you mentioned would have been all over the E-mail lists. > >No, this was not the accident that I was referring. >In fact, the texas crash involved a plane that both of >my parents had flown in, but that was before it was >sold to the owners involved in the accident. >--- Jerry Springer wrote: > > > > > > > Skylor Piper wrote: > > > > > > > > > >It's been awhile since I've read the report of the > > >"other" structural failure, and I must admit that I > > >don't recall all the details. I'll see if I can > > find > > >it this week. > > > > > > > > >http://www2.ntsb.gov/ntsb/brief.asp?ev_id 031009X01690&key=1 > > > > > > If this is the one you are referring to I do not > > believe wing skins > > would have made a difference, nor was it in anyway > > the fault > > of the aircraft. If you read the entire report the > > wings were still > > attached and both wing leading edges were crushed > > back. > > I really hate it when misinformation gets spread > > around about the > > airplanes we build and fly. > > > > If you have other information I would love to see > > the report. > > > > Jerry > > > > > > > > Contributions > > any other > > Forums. > > > > http://www.matronics.com/chat > > > > http://www.matronics.com/subscription > > http://www.matronics.com/FAQ/RV-List.htm > > http://www.matronics.com/archives > > http://www.matronics.com/photoshare > > http://www.matronics.com/emaillists > > > > > > > > > > > > > > >__________________________________ > > Scott Bilinski Eng dept 305 Phone (858) 657-2536 Pager (858) 502-5190 ________________________________________________________________________________
From: "Matthew Brandes" <matthew(at)n523rv.com>
Subject: RE: Compass liquid
Date: Aug 23, 2004
Thanks for all the responses. I'm kind of surprised at the number of responses and options. I found some compass fluid at ACS but if Chuck can find his overhaul kits, I'll take his offer. Thanks! Matthew Brandes, Van's RV-9A (Fuselage) EAA Chapter 868/91/1329 www.n523rv.com <http://www.n523rv.com/> ________________________________________________________________________________
Date: Aug 23, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Navaid problem
Ronnie Brown wrote: > > The Navaid manual also states that it is not designed to intercept a > course, you have to point your plane in the desired heading before > engaging the course tracking mode. > > Try using the trim knob (left knob) more, you'll be a lot happier > with your Navaid. The advice to use the Navaid trim knob properly is indeed crucial to getting the Navaid to track accurately. A feature that I found few Navaid users that I've talked with using is the ability of the unit to track an offset course. Usually you must have the trim set just right to get the Navaid to hold a tight course, but it the trim is intentionally cranked to one side after the Navaid is tracking properly, it will track a parallel course offset up to a mile or so. This is helpful if you are approaching a area you wish to avoid flying over (power plant, tower, C172, etc) but don't want to disengage the Navaid and have to set it up again. Just rack the trim full over and the unit will wander off in that direction and eventually return to the original heading while flying a parallel course to the original courseline. After passing the 172, recenter the trim and the Navaid will return, more or less, to the original course. The Navaid generally works quite well for simply tracking a course, but it's kinda like the old analog TV set; you must tweak the tuning knob just right and some chewing gum foil on the rabbit ears sometimes helps as well. :-) The feature set and performance of the digital autopilots is far beyond what the venerable Navaid is capable of providing. Technology marches on! Sam Buchanan http://thervjournal.com ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: RV8 one piece wings skins
Date: Aug 23, 2004
Van has already modified the RV-3 spar to prevent such happenings. Cy Galley Safety Programs Editor Always looking for ideas and articles for EAA Sport Pilot ----- Original Message ----- From: "Skylor Piper" <skylor4(at)yahoo.com> Subject: Re: RV-List: RV8 one piece wings skins > > OK, this will teach me to "keep my mouth shut" until I > have all my facts together. The accident that I was > referring to was an RV-3, and the wing separated at > the fuselage. Oh well... > --- Skylor Piper wrote: > > > > > > > It's been awhile since I've read the report of the > > "other" structural failure, and I must admit that I > > don't recall all the details. I'll see if I can > > find > > it this week. > > > > I do recall that it was an RV-8 in California on its > > way to a fly in several years ago. I believe it was > > VFR into IMC by a non IFR pilot, and a witness saw > > it > > come spinning out of the clouds without part of a > > wing. Like N58RV, the wing failed around the > > inboard > > end of the aileron (I recall). > > > > I agree with Kevin's point of view that you can't > > arbitrarily install a heavier one piece skin and > > expect that will strengthen the wing under all > > conditions. Lighter planes are definitely better. > > > > My only point was that there "may" be some benefit > > of > > the heavier one piece skin, at list in the two > > instances where the wing failed mid span. > > Ultimately, > > the answer to the that question lies with a > > knowledgeable structural engineer or the aircraft > > designer. > > > > Skylor > > > > --- Jerry Springer wrote: > > > > > > > > > > > Skylor Piper wrote: > > > > > > > > > > > > > > > > > >--- Kevin Horton wrote: > > > > > > > > > > > > > > > >>Sure, the outboard wing would be a bit stronger, > > > but > > > >>the inboard wing > > > >>would be the same as before. The extra strength > > > in > > > >>the outboard wing > > > >>is irrelevant...snip... > > > >> > > > >> > > > > > > > > > > > > > > > >>Kevin Horton RV-8 (finishing kit) > > > >>Ottawa, Canada > > > >>http://go.phpwebhosting.com/~khorton/rv8/ > > > >> > > > >> > > > > > > > >Are you sure about that? The two RV-8's that had > > > >in-flight structural failures (that I know about) > > > had > > > >the wings fail right at the inboard edge of the > > > aileron. > > > > > > > > > > > > > > > > > > > > > > > Skylor what were the deaails of the second in > > flight > > > failure? > > > > > > Jerry > > > > > > > > > > > > Contributions > > > any other > > > Forums. > > > > > > http://www.matronics.com/chat > > > > > > http://www.matronics.com/subscription > > > http://www.matronics.com/FAQ/RV-List.htm > > > http://www.matronics.com/archives > > > http://www.matronics.com/photoshare > > > http://www.matronics.com/emaillists > > > > > > > > > > > > > > > > > > > > > > > > > > _______________________________ > > > > > > > > Contributions > > any other > > Forums. > > > > http://www.matronics.com/chat > > > > http://www.matronics.com/subscription > > http://www.matronics.com/FAQ/RV-List.htm > > http://www.matronics.com/archives > > http://www.matronics.com/photoshare > > http://www.matronics.com/emaillists > > > > > > > > > > > > > > > __________________________________ > > ________________________________________________________________________________
Subject: excess cylinder flashing
Date: Aug 23, 2004
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
Guys, Online chatter has accused excess cylinder flashing of causing high CHT's. Some have said that they used several hours and several drill bits to clean it out. Here's how I did it. Takes about an hour to do. http://www.usi.edu/science/chemistry/vfrazier/Engine%20and%20Prop.htm I can't say if it helps cooling, but it certainly looks like it would. Vince Frazier 3965 Caborn Road Mount Vernon, IN 47620 812-464-1839 work 812-985-7309 home F-1H Rocket, N540VF http://www.usi.edu/science/chemistry/vfrazier/page1.html ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Aug 23, 2004
Subject: Re:Wheel Fairings-Balancing Act
When I did the main gear fairings on our RV-4 I used wing jacks to lift the plane. My jacks lift via 3/8" bolts, screwed into the wing tie-down fittings ,and they sit in a pipe socket welded atop the jack. ( NO slipping here) I placed the tailwheel on a table, with appropiate blocking, to level the plane. I had to put weight on the horizontal stabilizer to keep the tail down. Place the weight close to the verticle fin. With the plane supported off the floor and level I had the proper flight attitude for aligning the fairings. I can email pic's of my jacks if that would help. Bob Olds RV-4 , N1191X A&P , EAA Tech. Counselor Charleston,Arkansas Real Aviators Fly Taildraggers ________________________________________________________________________________
From: "John Furey" <john(at)fureychrysler.com>
Subject: excess cylinder flashing
Date: Aug 23, 2004
I agree with all that is said. I used a dremmel with a file in the chuck-same rules apply. No scientific data but I think I could back up a 20 degree drop on the worst ones. John Furey RV6A O-320 ________________________________________________________________________________
From: "sdellangelo(at)netzero.com" <sdellangelo(at)netzero.com>
Date: Aug 23, 2004
Subject: Anybody with experience with both Trutrak and Trio?
I am looking to install either the pictoral pilot (the 3 1/8" one with the ball incorporated into it, which they claimed at Oshkosh would be out soon for "another $50") or the EZ pilot II. Can anybody who has experience with both give me any pros or cons one way or the other between them. I know the EZ pilot is ~$300 cheaper. Both look to come with installation hardware (the tru trak stuff "looks" nicer and the setup would be at the wing bellcrank, and the EZ pilot would attach to the control tube probably under the seats?). I definitely want the turn coordinator function to backup the Dynon, but they both do that and both have (will have) a ball. How about the performance difference or anything else? Thanks, Scott DellAngelo #90598 fuselage Plainfield, IL Only $14.95/ month -visit www.netzero.com to sign up today! ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Anybody with experience with both Trutrak and Trio?
Date: Aug 23, 2004
-----Original Message----- Subject: RV-List: Anybody with experience with both Trutrak and Trio? Both look to come with installation hardware (the tru trak stuff "looks" nicer and the setup would be at the wing bellcrank, and the EZ pilot would attach to the control tube probably under the seats?). Scott DellAngelo Scott, TruTrak now has an under the seat installation. Call them for details. Ross Mickey N9PT ________________________________________________________________________________
Date: Aug 23, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Anybody with experience with both Trutrak and Trio?
sdellangelo(at)netzero.com wrote: > > > > I am looking to install either the pictoral pilot (the 3 1/8" one > with the ball incorporated into it, which they claimed at Oshkosh > would be out soon for "another $50") or the EZ pilot II. Can anybody > who has experience with both give me any pros or cons one way or the > other between them. I know the EZ pilot is ~$300 cheaper. Both look > to come with installation hardware (the tru trak stuff "looks" nicer > and the setup would be at the wing bellcrank, and the EZ pilot would > attach to the control tube probably under the seats?). I definitely > want the turn coordinator function to backup the Dynon, but they both > do that and both have (will have) a ball. > > How about the performance difference or anything else? > > Thanks, Scott DellAngelo #90598 fuselage Plainfield, IL Even though I can't address the request for a comparison between the pictorial pilot and the EZ-Pilot since I have never flown the TruTrak unit, there are a couple of other issues raised in the above post that are worthy of comment. The EZ-Pilot servo can be mounted in a variety of locations since it is a Navaid servo that has faithfully served the experimental market many years in a wide range of installations. The servo can be located under seat pans, at mid-wing, or at the wing tip. Fabricating mounting hardware and actuating stuff for servo installations is fairly simple and limited only by the builder's imagination. The TruTrak servo is a step-motor which is considerably heavier than the EZ-Pilot unit but it likewise is suitable for various locations in the plane, even though I would be reluctant to mount it at the wing tip due to the weight of the servo. No doubt what I am now about to state will be subject to disagreement by many pilots, but in my opinion the presence or lack of a turn coordinator display (analog or digital) in a panel with an autopilot is vastly overblown. I can assure you that if the Dynon were to go belly-up in my RV-6 while I was flying on instruments, whether or not I have a T/C in the panel will be the last of my concerns. Before you can say "Vertigo" I will have the autopilot flying the plane (if it isn't already) and will let the EZ-Pilot direct the plane to any vectors I input. There is NO WAY I am going to rely on flying partial panel via a T/C when there is a functioning autopilot on board!!!! I frequently conduct practice flights using just the AnywhereMap, the AlTrak, and the EZ-Pilot for all maneuvers except takeoffs and very short final. It is easy to conduct 500 fpm climbs and descents while the EZ-Pilot holds heading, and the AlTrak will hold altitude while the EZ-Pilot changes headings. I can even shoot a "virtual" ILS approach into ANY paved runway using the AnyWhereMap system (keeping in mind possible obstructions near the airport) and letting the autopilot slide the plane down final. This is not condoned by any experimental single-axis autopilot manufacturer, but I practice it so I can receive full benefit of ALL the equipment in the panel should things get ugly. During all the above, the turn coordinator is a non-issue. So if having a T/C display is still important to you, so be it. But if there is an operable autopilot in the panel, I just can't see where the presence of a T/C display is a factor. Remember, if you have staked your flight on an autopilot based T/C, it will be dead if the autopilot is off-line. But if the electrical system is well-designed, it is unlikely both the EFIS and autopilot will expire simultaneously. Sam Buchanan ________________________________________________________________________________
From: LeastDrag93066(at)aol.com
Date: Aug 23, 2004
Subject: CS Propeller
Hi All, The first propellers ordered from MT Propellers are just now starting to be delivered. I can still accept addition propeller orders for an MT Propeller at the special price. MT Propeller manufactures a very nice electric CS propeller for the solid crankshaft Lycoming. There are electric CS propellers designed for the Lycoming 320, 360 and 540 engine. MT Propeller custom designs their propeller for the engine/airframe and expected performance. They have electric CS propellers available to match the alternative engines which have the standard SAE (and some other) propeller flanges. Of course, hydraulic CS propellers are also available. 2 blade CS propellers. 3 blade CS propellers. (2nd order harmonic removed. Much smoother running than 2 blade.) 4 blade CS propeller. (John Harmon said that the four blade MT Propeller he tried was the smoothest running propeller he has ever flown. And he had previously flown the 3 blade MT Propeller.) Regards, Jim Ayers _jim(at)lessdrag.com_ (mailto:jim(at)lessdrag.com) RV-3 LOM M332A engine 3 blade electric CS MT propeller Less Drag Products, Inc. _www.lessdrag.com_ (http://www.lessdrag.com) ________________________________________________________________________________
Date: Aug 23, 2004
From: Jeff Point <jpoint(at)mindspring.com>
Subject: UHMW temperature rating
Howdy, Does anyone know what the temperature rating for UHMW tape (the kind used for flaps) is? I'd like to use some on the cowl, where it is rubbing on the camlocks, but I don't know if it'll take the heat. Thanks Jeff Point RV-6 Milwaukee WI ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: UHMW temperature rating
Date: Aug 23, 2004
I wouldn't hesitate at least to test it at first on an inconspicuous spot. According to McMaster's web site, the UHMW polyethylene tape they sell (go to http://www.mcmaster.com and enter "76445A761" in the Find box) is rated -40F to +220F. I don't know if this is comparable to the stuff Van's sells. One of these days I want to temp probe my cowl after shutdown on a hot day in the sun and see how high those under-cowl temps get. )_( Dan RV-7 N714D http://www.rvproject.com ----- Original Message ----- From: "Jeff Point" <jpoint(at)mindspring.com> Subject: RV-List: UHMW temperature rating > > Howdy, > > Does anyone know what the temperature rating for UHMW tape (the kind > used for flaps) is? I'd like to use some on the cowl, where it is > rubbing on the camlocks, but I don't know if it'll take the heat. > > Thanks > Jeff Point > RV-6 > Milwaukee WI > > ________________________________________________________________________________
Date: Aug 23, 2004
From: Scott Bilinski <bilinski@kyocera-wireless.com>
Subject: Re: UHMW temperature rating
Mine is holding up just fine, exactly where you want to use it, 190 Hrs, going strong. > >Howdy, > >Does anyone know what the temperature rating for UHMW tape (the kind >used for flaps) is? I'd like to use some on the cowl, where it is >rubbing on the camlocks, but I don't know if it'll take the heat. > >Thanks >Jeff Point >RV-6 >Milwaukee WI > > Scott Bilinski Eng dept 305 Phone (858) 657-2536 Pager (858) 502-5190 ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: UHMW temperature rating
Date: Aug 23, 2004
Hi Jeff, I believe the UHMW tape that I sell has a temp range of: -40oF to 225oF. My tape sheets say that should be accurate for most UHWM tape, but I can't say for sure. I think Van's sells the same stuff I do. I have UHMW tape all over the place (it's the best thing since sliced cheese) to keep anything that "rubs" from making a mark. I also have some on my cowl along the camlock strips, as well as the intersection fairings, canopy slider tracks, flaps, etc.. Hope this helps! Cheers, Stein Bruch RV6's, Minneapolis http://www.steinair.com -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Jeff Point Subject: RV-List: UHMW temperature rating Howdy, Does anyone know what the temperature rating for UHMW tape (the kind used for flaps) is? I'd like to use some on the cowl, where it is rubbing on the camlocks, but I don't know if it'll take the heat. Thanks Jeff Point RV-6 Milwaukee WI ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: io-360-a1b6d
Date: Aug 23, 2004
io-360-a1b6d Not sure, but this is the one excluded, and the last 6 refers to a 6th order counterweight and the D refers to a dual magneto. I expect the counter weight was found to be needed with the dual mag to prevent some harmonic problem, to which changing the timing negatively impacted the fix. But that is a guess on my part as I wasn't there when they designed this one. W ________________________________________________________________________________
From: "Donald Mei" <don_mei(at)hotmail.com>
Subject: H2AD series engines
Date: Aug 23, 2004
Steve, Your thought: **Why anybody would build a $60,000 airplane and finish it off with a $4000 engine is beyond my reasoning. ** Is a little ignorant of the financial realities for some builders. There are RV builders whose total aircraft budget is roughly equivalent to the total cost of an AEIO-360 . There's fewer of these kinds of builders than there used to be, but they are out there. (I would even venture that if Van himself were a builder, that is the way he'd think - light, cheap and simple) In fact, one of the attractions of the RV series, historically has been that you could build a nice simple VFR airplane for $35K that handled great and cruised at 150 kts. The problems with the O320-H2AD are well documented, as are the fixes to those problems. Espescially with the choices we have in the Experimental class, this may be a good base for someone who is handy and on a budget. Don "All of us need to be reminded that the federal government did not create the states; the states created the federal government!"---Ronald Reagan ________________________________________________________________________________
From: Laird Owens <owens(at)aerovironment.com>
Subject: Re: UHMW temperature rating
Date: Aug 23, 2004
The UHMW is good for most applications under the cowl, but it's the adhesive that gives up first. I put some on the baffles where they rub on the cylinder. After I pulled the engine some repairs, the UHMW was still on the baffles (worse for the wear) but the adhesive was a mess to clean off. I wouldn't hesitate to use it as a rub strip anywhere on the cowl. Laird RV-6 950hrs SoCal On Aug 23, 2004, at 1:55 PM, Dan Checkoway wrote: > > I wouldn't hesitate at least to test it at first on an inconspicuous > spot. > According to McMaster's web site, the UHMW polyethylene tape they sell > (go > to http://www.mcmaster.com and enter "76445A761" in the Find box) is > rated -40F to +220F. I don't know if this is comparable to the stuff > Van's > sells. > > One of these days I want to temp probe my cowl after shutdown on a hot > day > in the sun and see how high those under-cowl temps get. > > )_( Dan > RV-7 N714D > http://www.rvproject.com > > ----- Original Message ----- > From: "Jeff Point" <jpoint(at)mindspring.com> > To: "RV List" ; > Subject: RV-List: UHMW temperature rating > > >> >> Howdy, >> >> Does anyone know what the temperature rating for UHMW tape (the kind >> used for flaps) is? I'd like to use some on the cowl, where it is >> rubbing on the camlocks, but I don't know if it'll take the heat. >> >> Thanks >> Jeff Point >> RV-6 >> Milwaukee WI >> >> > > > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > > > > ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: io-360-a1b6d
Date: Aug 23, 2004
> io-360-a1b6d > > Not sure, but this is the one excluded, and the last 6 refers to a 6th order > counterweight and the D refers to a dual magneto. I expect the counter > weight was found to be needed with the dual mag to prevent some harmonic > problem, to which changing the timing negatively impacted the fix. Not quite...the "D" only means dual mag and is irrespective of counterweights. Likewise the "6" is independent of mag style, and just means the crankshaft is "equipped with one 6.3 order and one 8th order counterweights." (I'm quoting the TCDS) You can find the dual mag on some "D" model engines that don't have the "6" counterweights, i.e. the -E1AD or -E1BD. What the "6" model counterweights achieve is *no RPM operating limitations* on a typical Hartzell prop. Take a look at the Hartzell TCDS and you'll see that a Hartzell C2YK or C2YR with the "7666" series blade has the following placards required: IO-360-A1A or -A1B: "Avoid continuous operation between 2000 and 2250 RPM" IO-360-A1B6 or -A1B6D: "none" The counterweights have more to do with propeller dynamics than anything else, to the best of my knowledge. )_( Dan RV-7 N714D http://www.rvproject.com ________________________________________________________________________________
From: "Shemp" <shempdowling(at)earthlink.net>
Subject: Re: Anybody with experience with both Trutrak and Trio?
Date: Aug 23, 2004
What about FAR's? What qualifies for your turn and bank? Shemp ----- Original Message ----- From: "Sam Buchanan" <sbuc(at)hiwaay.net> Subject: Re: RV-List: Anybody with experience with both Trutrak and Trio? > > sdellangelo(at)netzero.com wrote: > > > > > > > > I am looking to install either the pictoral pilot (the 3 1/8" one > > with the ball incorporated into it, which they claimed at Oshkosh > > would be out soon for "another $50") or the EZ pilot II. Can anybody > > who has experience with both give me any pros or cons one way or the > > other between them. I know the EZ pilot is ~$300 cheaper. Both look > > to come with installation hardware (the tru trak stuff "looks" nicer > > and the setup would be at the wing bellcrank, and the EZ pilot would > > attach to the control tube probably under the seats?). I definitely > > want the turn coordinator function to backup the Dynon, but they both > > do that and both have (will have) a ball. > > > > How about the performance difference or anything else? > > > > Thanks, Scott DellAngelo #90598 fuselage Plainfield, IL > > > Even though I can't address the request for a comparison between the > pictorial pilot and the EZ-Pilot since I have never flown the TruTrak > unit, there are a couple of other issues raised in the above post that > are worthy of comment. > > The EZ-Pilot servo can be mounted in a variety of locations since it is > a Navaid servo that has faithfully served the experimental market many > years in a wide range of installations. The servo can be located under > seat pans, at mid-wing, or at the wing tip. Fabricating mounting > hardware and actuating stuff for servo installations is fairly simple > and limited only by the builder's imagination. The TruTrak servo is a > step-motor which is considerably heavier than the EZ-Pilot unit but it > likewise is suitable for various locations in the plane, even though I > would be reluctant to mount it at the wing tip due to the weight of the > servo. > > No doubt what I am now about to state will be subject to disagreement by > many pilots, but in my opinion the presence or lack of a turn > coordinator display (analog or digital) in a panel with an autopilot is > vastly overblown. I can assure you that if the Dynon were to go belly-up > in my RV-6 while I was flying on instruments, whether or not I have a > T/C in the panel will be the last of my concerns. Before you can say > "Vertigo" I will have the autopilot flying the plane (if it isn't > already) and will let the EZ-Pilot direct the plane to any vectors I > input. There is NO WAY I am going to rely on flying partial panel via a > T/C when there is a functioning autopilot on board!!!! > > I frequently conduct practice flights using just the AnywhereMap, the > AlTrak, and the EZ-Pilot for all maneuvers except takeoffs and very > short final. It is easy to conduct 500 fpm climbs and descents while the > EZ-Pilot holds heading, and the AlTrak will hold altitude while the > EZ-Pilot changes headings. I can even shoot a "virtual" ILS approach > into ANY paved runway using the AnyWhereMap system (keeping in mind > possible obstructions near the airport) and letting the autopilot slide > the plane down final. This is not condoned by any experimental > single-axis autopilot manufacturer, but I practice it so I can receive > full benefit of ALL the equipment in the panel should things get ugly. > > During all the above, the turn coordinator is a non-issue. So if having > a T/C display is still important to you, so be it. But if there is an > operable autopilot in the panel, I just can't see where the presence of > a T/C display is a factor. Remember, if you have staked your flight on > an autopilot based T/C, it will be dead if the autopilot is off-line. > But if the electrical system is well-designed, it is unlikely both the > EFIS and autopilot will expire simultaneously. > > Sam Buchanan > > ________________________________________________________________________________
Date: Aug 23, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Anybody with experience with both Trutrak and Trio?
Shemp wrote: > > What about FAR's? What qualifies for your turn and bank? > > Shemp The Navaid, DigiTrak and EZ-Pilot all have turn coordinator displays. My point was that if forced into a partial panel situation, I would let the autopilot keep the shiny side up instead of hand flying with a turn coordinator. Sam Buchanan ============================== > > ----- Original Message ----- > From: "Sam Buchanan" <sbuc(at)hiwaay.net> > To: > Subject: Re: RV-List: Anybody with experience with both Trutrak and Trio? > > > >> >>sdellangelo(at)netzero.com wrote: >> >>> >>> >>> >>>I am looking to install either the pictoral pilot (the 3 1/8" one >>>with the ball incorporated into it, which they claimed at Oshkosh >>>would be out soon for "another $50") or the EZ pilot II. Can anybody >>>who has experience with both give me any pros or cons one way or the >>>other between them. I know the EZ pilot is ~$300 cheaper. Both look >>>to come with installation hardware (the tru trak stuff "looks" nicer >>>and the setup would be at the wing bellcrank, and the EZ pilot would >>>attach to the control tube probably under the seats?). I definitely >>>want the turn coordinator function to backup the Dynon, but they both >>>do that and both have (will have) a ball. >>> >>>How about the performance difference or anything else? >>> >>>Thanks, Scott DellAngelo #90598 fuselage Plainfield, IL >> >> >>Even though I can't address the request for a comparison between the >>pictorial pilot and the EZ-Pilot since I have never flown the TruTrak >>unit, there are a couple of other issues raised in the above post that >>are worthy of comment. >> >>The EZ-Pilot servo can be mounted in a variety of locations since it is >>a Navaid servo that has faithfully served the experimental market many >>years in a wide range of installations. The servo can be located under >>seat pans, at mid-wing, or at the wing tip. Fabricating mounting >>hardware and actuating stuff for servo installations is fairly simple >>and limited only by the builder's imagination. The TruTrak servo is a >>step-motor which is considerably heavier than the EZ-Pilot unit but it >>likewise is suitable for various locations in the plane, even though I >>would be reluctant to mount it at the wing tip due to the weight of the >>servo. >> >>No doubt what I am now about to state will be subject to disagreement by >>many pilots, but in my opinion the presence or lack of a turn >>coordinator display (analog or digital) in a panel with an autopilot is >>vastly overblown. I can assure you that if the Dynon were to go belly-up >>in my RV-6 while I was flying on instruments, whether or not I have a >>T/C in the panel will be the last of my concerns. Before you can say >>"Vertigo" I will have the autopilot flying the plane (if it isn't >>already) and will let the EZ-Pilot direct the plane to any vectors I >>input. There is NO WAY I am going to rely on flying partial panel via a >>T/C when there is a functioning autopilot on board!!!! >> >>I frequently conduct practice flights using just the AnywhereMap, the >>AlTrak, and the EZ-Pilot for all maneuvers except takeoffs and very >>short final. It is easy to conduct 500 fpm climbs and descents while the >>EZ-Pilot holds heading, and the AlTrak will hold altitude while the >>EZ-Pilot changes headings. I can even shoot a "virtual" ILS approach >>into ANY paved runway using the AnyWhereMap system (keeping in mind >>possible obstructions near the airport) and letting the autopilot slide >>the plane down final. This is not condoned by any experimental >>single-axis autopilot manufacturer, but I practice it so I can receive >>full benefit of ALL the equipment in the panel should things get ugly. >> >>During all the above, the turn coordinator is a non-issue. So if having >>a T/C display is still important to you, so be it. But if there is an >>operable autopilot in the panel, I just can't see where the presence of >>a T/C display is a factor. Remember, if you have staked your flight on >>an autopilot based T/C, it will be dead if the autopilot is off-line. >>But if the electrical system is well-designed, it is unlikely both the >>EFIS and autopilot will expire simultaneously. >> >>Sam Buchanan ________________________________________________________________________________
From: <groves(at)epix.net>
Subject: Unheated Pitot
Date: Aug 23, 2004
Hello everyine!! I was wondering can you get gretz pitot tubes unheated? Thanks, Kirk RV-8 Wings ________________________________________________________________________________
From: Sam Knight <knightair(at)lv.rmci.net>
Subject: Knight Aircraft Interiors/Upholstery
Date: Aug 23, 2004
RV Builders: I have been in the upholstery business for 30 years and have been making upholstery products for kitplanes for 18 years. I have interior kits available for RV-4, RV-6, RV-6A, and RV-8. I also have cabin covers and other items. I am the supplier of upholstery products for several kitplane manufacturers. A list of other kitplane interior products available upon request. For more information, call Knight Aircraft Interiors, Inc., at (702) 207-6681 or e mail me at knightair(at)lv.rmci.net. If you e-mail for information, please mention either "Knight" or "Upholstery" in your reference line so I can give your request my immediate attention. Photos available upon request. Sincerely, KNIGHT AIRCRAFT INTERIORS, INC. "Fly by Knight" Upholstery Products Sam Knight ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Aug 23, 2004
Subject: Re: UHMW temperature rating
In a message dated 8/23/2004 1:12:37 PM Pacific Daylight Time, jpoint(at)mindspring.com writes: Does anyone know what the temperature rating for UHMW tape (the kind used for flaps) is? I'd like to use some on the cowl, where it is rubbing on the camlocks, but I don't know if it'll take the heat. ======================================= We have found that the loop (soft) side of self-stick Velcro is really good as an anti-chafe strip. It was the only material that would hold up to the constant vibration and didn't come unstuck, even in high temp areas. GV (RV-6A N1GV O-360-A1A C/S, flying 710 hrs) ________________________________________________________________________________
From: "James E. Clark" <james(at)nextupventures.com>
Subject: Attachment showing up in RV List (or do I have a virus)????????
Date: Aug 23, 2004
Anyone else out there getting mail from the RV-List with an "attachment"? Hope I don't have a virus or something. (Should be protected by virus protection s/w) James ________________________________________________________________________________
From: "Gordon and Marge" <gcomfo(at)tc3net.com>
Subject: Question for the aerodynamycists
Date: Aug 24, 2004
Subject: RV-List: Question for the aerodynamycists I am going to install a NACA vent on the side of the forward fuselage on the RV-4 I am rebuilding. I am thinking of installing it right below the cowl cheek angled downward so that the longitudinal axis of the vent is parallel to the logitudnal axis of the cowl cheek extension. My thought is the pressure will be positive in this area and will result in good positive airflow into the vent (this will be for fresh air ventilation to the front cockpit). Does it make an appreciable difference? As in most things the best idea would be to try it to find out but that is not practical given the hole I need to cut in the fuselage skin. I'm looking for opinions and/or experience with this location. Is my thinking sound or am I missing something? Net, net - I'd like to install on the right but the left seems like a better location. Which is best and will either work? Richard RV-4 N144KT - rising from he ashes of a 1998 landing in the trees at IGX. Richard: I cannot say which side is best, but I can tell you that the right side works very well. Mine is located on the right, vertical placement is about midway between the cowl cheek extension and the wing, inclined roughly paralleling the cheek extension and the incoming air will blow a chart out of your hands at speeds above the stall. Not much flow on the ground. Gordon Comfort N363GC ________________________________________________________________________________
Date: Aug 24, 2004
From: Finn Lassen <finn.lassen(at)verizon.net>
Subject: Re: Your Big Mistake - Your Big Chance
I started this thread and I'm actually still waiting for an answer to my questions of "how strong are the tiedown hardpoints on an RV-3?", how strong winds will they handle (assuming ropes and ground anchors stay put)? Finn Robert Hansen wrote: > >There is good information on this list much of the time, but it seems too >often loaded down with the chit chat of folks who want to use it as a forum >to offer opinions that have nothing to do with RVs. Like many others, I >hate it that I have to wade through tons of, "Hurricane and tie-down" >dribble to find RV stuff. > > ________________________________________________________________________________
From: "Eric Parlow" <ericparlow(at)hotmail.com>
Subject: RVs at KTOA
Date: Aug 24, 2004
Looking for info on RVs, more specifically RV-8s, at KTOA. Or surrounding airports: KSMO, KLGB, KHHR. I'm considering moving there and RV's / Airports will weigh heavily into my decision. ERic-- RV-8 Wings ________________________________________________________________________________
Date: Aug 24, 2004
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Your Big Mistake - Your Big Chance
> >I started this thread and I'm actually still waiting for an answer to my >questions of "how strong are the tiedown hardpoints on an RV-3?", how >strong winds will they handle (assuming ropes and ground anchors stay put)? > >Finn > Finn, Your original post said "I think only two 3/16" bolts hold the tie-down pipe to the spar web." Wicks catalog gives a rated strength in shear of 2,125 lb for an AN3 bolt. It isn't clear at first glance whether this is an allowable design strength (i.e. it is acceptable to have normal design loads up to this value), or whether it is a guaranteed ultimate strength. Some other references give lower values, so I assume that 2,125 is an ultimate strength, and the other references are providing allowable design loads. Assuming 2,125 lb is an ultimate strength, two bolts would be 4,250 lb, but that assumes that the load is shared equally between the two bolts. In practice I suspect the lower bolt would get more than 50% of the load, as the tie-down pipe might stretch a bit. So you probably shouldn't count on the bolts taking more than 3,000 lb load, maybe even less. This assumes that the load is perfectly aligned with the tie down pipe. A misaligned load would probably increase the stress on the lower bolt even further. The limiting factor might be somewhere else. Depending on the thread size of the hole, and material of the tie down ring, you might find that it breaks first. Or, depending on the material and cross sectional area of the tie down pipe, perhaps it is the weak link. Or, maybe the spar itself will be the first thing damaged (hopefully not - a good design would have something else fail before the spar incurred damaging loads). What is the thread size and pitch of the tie down hole? What is the material and cross sectional area of the tie down pipe? What is the spar material and dimensions where the tie down pipe attaches to it? -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ ________________________________________________________________________________
Subject: "Super RV-8" web sites or drawings?
Date: Aug 24, 2004
From: "Stewart, Michael (ISS Atlanta)" <mstewart(at)iss.net>
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From: dmedema(at)att.net
Subject: Safety wiring bolts for wheel pants
Date: Aug 24, 2004
I finished installing my wheel pants last night and have one question: The plans say to safety wire the bolt head that holds the outside bracket to the large axle nut. However, the bolts supplied in my wheel pants kit don't have drilled heads. Also, the bolts go into a nutplate that has the usual anti-vibration crimp. Do I need to buy new drilled head bolts or is the nutplate crimp sufficient? Have others received drilled head bolts or are regular un-drilled bolts now standard? Thanks, Doug Medema RV-6A N276DM I finished installing my wheel pants last night and have one question: The plans say to safety wire the bolt head that holds the outside bracket to the large axle nut. However, the bolts supplied in my wheel pants kit don't have drilled heads. Also, the bolts go into a nutplate that has the usual anti-vibration crimp. Do I need to buy new drilled head bolts or is the nutplate crimp sufficient? Have others received drilled head bolts or are regular un-drilled bolts now standard? Thanks, Doug Medema RV-6A N276DM ________________________________________________________________________________
From: "Jack Blomgren" <jackanet(at)hotmail.com>
Subject: Aluminum matching paints
Date: Aug 24, 2004
Painting Gurus, Say you only wanted to paint your RV's fairings, tips, pants, skirt, you know, the glass parts, to sort of fool the non-RV world that it's all aluminum, what paint would you choose, and maybe why? I see PPG has all those "Mist" names for what-- on the computer screen-- look to be aluminum-like paints for Audi, Jaguar, Mercedes, etc.. But some of you must already have worked out this not-as-easy-as-it-looks problem. [No pun intended] Thanks, Jack -8 ________________________________________________________________________________
Date: Aug 24, 2004
From: Skylor Piper <skylor4(at)yahoo.com>
Subject: Re: RVs at KTOA
Eric, The RV population at Torrance is growing rapidly. I'm building an 8 QB with my father, and there is another flying 8A based there. There are also several 6's and 4's on the field, and at least 1 F1 Rocket under construction. Skylor Piper RV-8 QB Under Construction N808SJ Reserved --- Eric Parlow wrote: > > > Looking for info on RVs, more specifically RV-8s, > at KTOA. > > Or surrounding airports: KSMO, KLGB, KHHR. > > I'm considering moving there and RV's / Airports > will weigh heavily into my > decision. > > ERic-- > RV-8 Wings > > > > Contributions > any other > Forums. > > http://www.matronics.com/chat > > http://www.matronics.com/subscription > http://www.matronics.com/FAQ/RV-List.htm > http://www.matronics.com/archives > http://www.matronics.com/photoshare > http://www.matronics.com/emaillists > > > > > > _______________________________ ________________________________________________________________________________
Date: Aug 24, 2004
From: Chris W <1qazxsw23edcvfr45tgbnhy67ujm(at)cox.net>
Subject: Re: Tie Down Strength
Finn Lassen wrote: > >I started this thread and I'm actually still waiting for an answer to my >questions of "how strong are the tiedown hardpoints on an RV-3?", how >strong winds will they handle (assuming ropes and ground anchors stay put)? > > I'm not sure there is an answer to you question, but I can make a guess. According to the McMaster catalog a plain steel 3/8 inch eyebolt has a load rating of 1,300 lbs. Since on the RV the eyebolt is screwed into aluminum alloy threads, and a good aluminum alloy is close to the strength of a plain unalloyed steel, I would tend the think the load ratting would be at most that of the plain steel eyebolt, 1,300 lbs. Now the question becomes how much wind do you need to produce 1300 lbs of lift on each wing with the plane in tail wheel attitude. Just a wild guess here but I am pretty sure that it would be less than 100 mph. Of course if you attach some kind of stall strip to the top of the wing it would help. That brings up an idea I had for people who commonly tie down their RV in high winds. Why not modify the tie down hard point so you can screw into it from the bottom and top of the wing, then add a second one some distance away from the first. It would then be very easy to bolt an aluminum angle or just a 2 x 4 to the top of the wing to kill the lift from strong winds. -- Chris W Bring Back the HP 15C http://hp15c.org Not getting the gifts you want? The Wish Zone can help. ________________________________________________________________________________
Date: Aug 24, 2004
From: "Tim Bryan" <rv6flyer(at)improvementteam.com>
Subject: Re: RVs at KTOA
Hi Eric, Check out this fantastic tool that Dan put together. It is at: http://www.rvproject.com/registry/rvfinder.jsp Tim Bryan RV-6 N616TB -------Original Message------- From: rv-list(at)matronics.com Date: 08/24/04 09:28:25 Subject: RV-List: RVs at KTOA Looking for info on RVs, more specifically RV-8s, at KTOA. Or surrounding airports: KSMO, KLGB, KHHR. I'm considering moving there and RV's / Airports will weigh heavily into my decision. ERic-- RV-8 Wings ________________________________________________________________________________
From: "Doug Weiler" <dcw(at)nomadwi.com>
Subject: Re: Safety wiring bolts for wheel pants
Date: Aug 24, 2004
I do not have these bolts safetied and have never had them come loose. You are going into a locking nutplate anyway. Doug Weiler RV-4 120 hours.. still in the paint shop in Tuscaloosa. > > I finished installing my wheel pants last night and have one question: > The plans say to safety wire the bolt head that holds the outside > bracket to the large axle nut. However, the bolts supplied in my > wheel pants kit don't have drilled heads. Also, the bolts go into > a nutplate that has the usual anti-vibration crimp. Do I need to > buy new drilled head bolts or is the nutplate crimp sufficient? > Have others received drilled head bolts or are regular un-drilled > bolts now standard? > > Thanks, > Doug Medema ________________________________________________________________________________
Date: Aug 24, 2004
From: Mickey Coggins <mick-matronics(at)rv8.ch>
Subject: "Super RV-8" web sites or drawings?
local> Hi Alan, Michael Stewart has some good information on the web here: http://www.mstewart.net/michael/rv/ Mickey >A quick search through archives didn't yeild anything... > >I've heard mention of the Super -8. Is there a web site/sites or drawings >on what this entails? > >- Alan -- Mickey Coggins http://www.rv8.ch/ #82007 QB Wings/Fuselage ________________________________________________________________________________
From: Grenwis(at)aol.com
Date: Aug 24, 2004
Subject: EZ Pilot Display Choice
For those that have used them, which display (LCD or VFD) is more readable in an RV cockpit? Rick Grenwis RV6A QB - Panel - CoSpgs, CO ________________________________________________________________________________
From: "Ollie Washburn" <ollie-6a(at)prodigy.net>
Subject: Re: EZ Pilot Display Choice
Date: Aug 24, 2004
Rick, I have RV6A with the sun shade and I first had the LCD as many RVers said that was best with all the light in the RV.However with the sun shade my poor old eyes couldn't see the display so I called them and they put the vfd display in for me which while not perfect is much better than before. Ollie ----- Original Message ----- From: <Grenwis(at)aol.com> Subject: RV-List: EZ Pilot Display Choice > > For those that have used them, which display (LCD or VFD) is more readable > in an RV cockpit? > > Rick Grenwis > RV6A QB - Panel - CoSpgs, CO > > ________________________________________________________________________________
Date: Aug 24, 2004
From: Louis Willig <larywil(at)comcast.net>
Subject: Re: Safety wiring bolts for wheel pants
At 11:41 AM 8/24/2004, you wrote: > >I finished installing my wheel pants last night and have one question: >The plans say to safety wire the bolt head that holds the outside >bracket to the large axle nut. However, the bolts supplied in my >wheel pants kit don't have drilled heads. Also, the bolts go into >a nutplate that has the usual anti-vibration crimp. Do I need to >buy new drilled head bolts or is the nutplate crimp sufficient? >Have others received drilled head bolts or are regular un-drilled >bolts now standard? Doug, The hex head bold that held the wheel pant onto the outside bracket on my RV-4 used to come loose all the time. I disregarded it one time too many, and upon landing one day, the bolt fell out completely, and the wheel pant was twisted around by the tire and the backing plate was destroyed. I have a new backing plate and repaired the cosmetic damage to the wheel pant, BUT I now use a simple split lock washer. 350 additional hours and no problem. I don't know where you would secure a safety wire to. Louis - Louis I Willig 1640 Oakwood Dr. Penn Valley, PA 19072 610 668-4964 RV-4, N180PF 190HP IO-360, C/S prop ________________________________________________________________________________
From: "David Carter" <dcarter(at)datarecall.net>
Subject: Re: EZ Pilot Display Choice
Date: Aug 24, 2004
What is a VFD display? David ----- Original Message ----- From: "Ollie Washburn" <ollie-6a(at)prodigy.net> Subject: Re: RV-List: EZ Pilot Display Choice > > Rick, I have RV6A with the sun shade and I first had the LCD as many RVers > said that was best with all the light in the RV.However with the sun shade > my poor old eyes couldn't see the display so I called them and they put the > vfd display in for me which while not perfect is much better than before. > Ollie > > ----- Original Message ----- > From: <Grenwis(at)aol.com> > To: > Subject: RV-List: EZ Pilot Display Choice > > > > > > For those that have used them, which display (LCD or VFD) is more readable > > in an RV cockpit? > > > > Rick Grenwis > > RV6A QB - Panel - CoSpgs, CO > > > > > > ________________________________________________________________________________
From: "LarryRobertHelming" <lhelming(at)sigecom.net>
Subject: Re: Safety wiring bolts for wheel pants
Date: Aug 24, 2004
My kit came with bolts to be safeywired. Indiana Larry, RV7 TipUp "SunSeeker" The sincerest satisfactions in life come in doing and not dodging duty; in meeting and solving problems, in facing facts, in being a dependable person. - Richard L. Evans ----- Original Message ----- From: "Doug Weiler" <dcw(at)nomadwi.com> Subject: Re: RV-List: Safety wiring bolts for wheel pants > > I do not have these bolts safetied and have never had them come loose. You > are going into a locking nutplate anyway. > > Doug Weiler > RV-4 120 hours.. still in the paint shop in Tuscaloosa. > > > > > > I finished installing my wheel pants last night and have one question: > > The plans say to safety wire the bolt head that holds the outside > > bracket to the large axle nut. However, the bolts supplied in my > > wheel pants kit don't have drilled heads. Also, the bolts go into > > a nutplate that has the usual anti-vibration crimp. Do I need to > > buy new drilled head bolts or is the nutplate crimp sufficient? > > Have others received drilled head bolts or are regular un-drilled > > bolts now standard? > > > > Thanks, > > Doug Medema > > ________________________________________________________________________________
Date: Aug 24, 2004
From: linn walters <lwalters2(at)cfl.rr.com>
Subject: Re: Safety wiring bolts for wheel pants
To answer the question that Louis posed: Drill a hole in the wheel pant near the bolt and put a cotter pin in there with the loop on the inside. Safety the bolt to the cotter pin. Linn Louis Willig wrote: > >At 11:41 AM 8/24/2004, you wrote: > > >> >>I finished installing my wheel pants last night and have one question: >>The plans say to safety wire the bolt head that holds the outside >>bracket to the large axle nut. However, the bolts supplied in my >>wheel pants kit don't have drilled heads. Also, the bolts go into >>a nutplate that has the usual anti-vibration crimp. Do I need to >>buy new drilled head bolts or is the nutplate crimp sufficient? >>Have others received drilled head bolts or are regular un-drilled >>bolts now standard? >> >> > >Doug, > >The hex head bold that held the wheel pant onto the outside bracket on my >RV-4 used to come loose all the time. I disregarded it one time too many, >and upon landing one day, the bolt fell out completely, and the wheel pant >was twisted around by the tire and the backing plate was destroyed. I have >a new backing plate and repaired the cosmetic damage to the wheel pant, BUT >I now use a simple split lock washer. 350 additional hours and no problem. >I don't know where you would secure a safety wire to. > >Louis > > >- >Louis I Willig >1640 Oakwood Dr. >Penn Valley, PA 19072 >610 668-4964 >RV-4, N180PF >190HP IO-360, C/S prop > > > > ________________________________________________________________________________
Date: Aug 24, 2004
From: linn walters <lwalters2(at)cfl.rr.com>
Subject: Re: Safety wiring bolts for wheel pants
I apologize for the multiple posts ...... but put the cotter pin loop on the OUTSIDE. 'Course you probably already knew that! ;-) Linn linn walters wrote: > >To answer the question that Louis posed: Drill a hole in the wheel pant >near the bolt and put a cotter pin in there with the loop on the >inside. Safety the bolt to the cotter pin. >Linn >Louis Willig wrote: > > > >> >>At 11:41 AM 8/24/2004, you wrote: >> >> >> >> >>> >>>I finished installing my wheel pants last night and have one question: >>>The plans say to safety wire the bolt head that holds the outside >>>bracket to the large axle nut. However, the bolts supplied in my >>>wheel pants kit don't have drilled heads. Also, the bolts go into >>>a nutplate that has the usual anti-vibration crimp. Do I need to >>>buy new drilled head bolts or is the nutplate crimp sufficient? >>>Have others received drilled head bolts or are regular un-drilled >>>bolts now standard? >>> >>> >>> >>> >>Doug, >> >>The hex head bold that held the wheel pant onto the outside bracket on my >>RV-4 used to come loose all the time. I disregarded it one time too many, >>and upon landing one day, the bolt fell out completely, and the wheel pant >>was twisted around by the tire and the backing plate was destroyed. I have >>a new backing plate and repaired the cosmetic damage to the wheel pant, BUT >>I now use a simple split lock washer. 350 additional hours and no problem. >>I don't know where you would secure a safety wire to. >> >>Louis >> >> >>- >>Louis I Willig >>1640 Oakwood Dr. >>Penn Valley, PA 19072 >>610 668-4964 >>RV-4, N180PF >>190HP IO-360, C/S prop >> >> >> >> >> >> > > > > ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: Attachment showing up in RV List (or do I have a virus)????????
Date: Aug 24, 2004
If you have an attachment then the sending address is spoofed. All attachments on the Matronics list are stripped. ----- Original Message ----- From: "James E. Clark" <james(at)nextupventures.com> Subject: RV-List: Attachment showing up in RV List (or do I have a virus)???????? > > Anyone else out there getting mail from the RV-List with an "attachment"? > > Hope I don't have a virus or something. (Should be protected by virus > protection s/w) > > James > > ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)earthlink.net>
Subject: Minnesota Wing Campin/Flyin
Date: Aug 24, 2004
Just a reminder to all of you - our fall picnic/flyin/campin is only a little more than two weeks away. The date of the picnic is Saturday, September 11th. For those interested, there will be camping also Friday and Saturday nights. We are holding it a beautiful 3800' grass strip just into Wisconsin from Minneapolis. For details see: http://www.pressenter.com/~dougweil/mnwing/id18.htm This is a really fun group, and we hope to see you there!!! Alex Peterson Maple Grove, MN RV6-A N66AP 516 hours http://www.home.earthlink.net/~alexpeterson/ ________________________________________________________________________________
From: "Noel & Yoshie Simmons" <noel(at)blueskyaviation.net>
"rvyahoo"
Subject: 153MC flies today
Date: Aug 24, 2004
Had a great day today, took RV-6A 153MC off the ground for the fist time today. Subsequently put 7 hours on it with out a hitch, god I love VAN'S stuff. O-360-A1A Holy Cowl with plenum NACA scoop for oil cooler Fixed pitch basic panel after 4 RV's I still get that RV grin :>))))))))))))))))))))))))))))))))))))) Sincerely, Noel Simmons Blue Sky Aviation, Inc. Phone & Fax: 406-538-6574 noel(at)blueskyaviation.net <http://www.blueskyaviation.net/> www.blueskyaviation.net ________________________________________________________________________________
Date: Aug 24, 2004
From: Dave Bristol <bj034(at)lafn.org>
Subject: Re: RVs at KTOA
on zoot.lafn.org Eric, You left out CPM. We've got a 6, 6A, 3 - 4's and a just minted Rocket. The 8's seem to be at TOA... maybe they need the longer runway? 8 > ) Dave RV6 Eric Parlow wrote: > >Looking for info on RVs, more specifically RV-8s, at KTOA. > >Or surrounding airports: KSMO, KLGB, KHHR. > >I'm considering moving there and RV's / Airports will weigh heavily into my >decision. > >ERic-- >RV-8 Wings > > > > ________________________________________________________________________________
From: "Dean Psiropoulos" <deanpsir(at)easystreet.com>
Subject: Navaid VS EZ Pilot!
Date: Aug 25, 2004
Ok Sam Buchanan: After not bothering to respond to the email I sent you off list, you've finally answered part of my questions to you. Specifically that the Navaid works "OK" if you understand how it operates and use it to its full potential. Great, that's good to hear. NOW..could you please tell me and the rest of the people on the list about the EZ Pilot electronics that you've mated to your Navaid servo???? You say that the digital autopilots are light years beyond the Navaid, great generalization, everybody else says that too!!! How bout some good solid opinion on the EZ Pilot II by someone who's used it quit a bit lately??? Don't worry about stirring up a hornets nest with the Tru Track people, I'm counting on that to get the rest of the information I'm seeking. Now come on.cough it up!!!! Dean Psiropoulos RV-6A N197DM Panel and wiring ________________________________________________________________________________
Date: Aug 24, 2004
From: Jeff Bertsch <noms1reqd(at)yahoo.com>
Subject: Re: H2AD series engines
I had an O-320H2AD engine in my C-172. I had it overhauled and ran it for 2400 hours with absolutely no significant problems. The only thing that gave me problems was the dual mag, which is a pain to work on and I don't think is a good idea. The engine compression was still in the mid to low 70's when I sold it. It was a great engine. We used Aeroshell 15w-50 which is required by AD (or you can use the Lyc additive). But I believe the real key is the plane flew frequently and never sat for more than 2 or 3 days without being flown. Jeff Bertsch lonestarsquadron.com --------------------------------- ________________________________________________________________________________
From: "James E. Clark" <james(at)nextupventures.com>
Subject: Attachment showing up in RV List (or do I have a virus)????????
Date: Aug 25, 2004
Thanks. It seems to have stopped after a few emails. Hmmmm, James > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of cgalley > Sent: Tuesday, August 24, 2004 8:56 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Attachment showing up in RV List (or do I have a > virus)???????? > > > If you have an attachment then the sending address is spoofed. All > attachments on the Matronics list are stripped. > > > ----- Original Message ----- > From: "James E. Clark" <james(at)nextupventures.com> > To: > Subject: RV-List: Attachment showing up in RV List (or do I have a > virus)???????? > > > > > > > Anyone else out there getting mail from the RV-List with an > "attachment"? > > > > Hope I don't have a virus or something. (Should be protected by virus > > protection s/w) > > > > James > > > > > > ________________________________________________________________________________
Date: Aug 25, 2004
From: linn walters <lwalters2(at)cfl.rr.com>
Subject: Re: H2AD series engines
Jeff Bertsch wrote: > >I had an O-320H2AD engine in my C-172. I had it overhauled and ran it for 2400 hours with absolutely no significant problems. The only thing that gave me problems was the dual mag, which is a pain to work on and I don't think is a good idea. > Aha! I'm a little slow. Couldn't figure out what all the fuss was about with the dual mag ..... it's missing the 's'!!! Until the electronic ignitions came along they all had dual mags :-D . I thought it was a typo! I've known them as 'siamese mags' ..... and there really is still two. And I agree ..... not my first choice .... nor second ;-) . However, they still have a good track record for failures ..... can't really compare them with separate mags ...... no data ...... but AFAIK, after the initial problems were addressed, the O-320-H2AD is just as solid as it's bretheren. Linn > The engine compression was still in the mid to low 70's when I sold it. It was a great engine. We used Aeroshell 15w-50 which is required by AD (or you can use the Lyc additive). But I believe the real key is the plane flew frequently and never sat for more than 2 or 3 days without being flown. > >Jeff Bertsch >lonestarsquadron.com > > >--------------------------------- > > > > ________________________________________________________________________________
From: "Shemp" <shempdowling(at)earthlink.net>
Subject: Re: Navaid VS EZ Pilot!
Date: Aug 25, 2004
I cant reply about the ez pilot but I sure can add some praise for the venerable old Nav-aid. Once I got the servo arm length adjusted to match the trim knob, it has worked great. I so far haven't found a need for using a course intercept function yet. The only feature that I would say is better in the new digital a/p's is the pictorial display for your turn coordinator if you ever really get in a pinch. However, considering the amount of planes out there now with some kind of EFIS and a backup vacuum system, I dont see the need to upgrade to one of the new systems. If you're starting from scratch, you'll have to weigh the cost differences yourself. It may be worth the extra bucks to get current technology. Shemp RV-6a/ 100 hours Chicago/ Louisville ----- Original Message ----- From: "Dean Psiropoulos" <deanpsir(at)easystreet.com> Subject: RV-List: Navaid VS EZ Pilot! > > Ok Sam Buchanan: > > > After not bothering to respond to the email I sent you off list, you've > finally answered part of my questions to you. Specifically that the Navaid > works "OK" if you understand how it operates and use it to its full > potential. Great, that's good to hear. NOW..could you please tell me and > the rest of the people on the list about the EZ Pilot electronics that > you've mated to your Navaid servo???? You say that the digital autopilots > are light years beyond the Navaid, great generalization, everybody else says > that too!!! How bout some good solid opinion on the EZ Pilot II by someone > who's used it quit a bit lately??? Don't worry about stirring up a hornets > nest with the Tru Track people, I'm counting on that to get the rest of the > information I'm seeking. Now come on.cough it up!!!! > > > Dean Psiropoulos > > RV-6A N197DM > > Panel and wiring > > ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)earthlink.net>
Subject: Attachment showing up in RV List (or do I have a virus)????????
Date: Aug 25, 2004
James is not the only one - since yesterday, all the messages from the list have a text attachment, which is simply a copy of the message. This has happened in the past, no clue what is going on. Other emails I have received, not from the list, also have the attachment occasionally, so it is likely not anything the list is generating. No clue. Alex Peterson Maple Grove, MN RV6-A N66AP 516 hours http://www.home.earthlink.net/~alexpeterson/ > > If you have an attachment then the sending address is > spoofed. All attachments on the Matronics list are stripped. > > > ----- Original Message ----- > From: "James E. Clark" <james(at)nextupventures.com> > To: > Subject: RV-List: Attachment showing up in RV List (or do I > have a virus)???????? > > > > --> > > > > Anyone else out there getting mail from the RV-List with an > > "attachment"? > > > > Hope I don't have a virus or something. (Should be > protected by virus > > protection s/w) > > > > James ________________________________________________________________________________
Date: Aug 25, 2004
From: Rick Galati <rick6a(at)yahoo.com>
Subject: Re: Aluminum matching paints
Judging from the underwhelming response to your interesting query I too must, (for the moment at least) conclude attaining such a polished look with paint is not quite as easy as we may want. Like you Jack, I have often wondered about the very same issue. AirVenture past, I approached an RV with some fairings that seemed to sport the closest match I had ever seen that attained the look of polished aluminum. I tipped my cap to the builder but was a bit crestfallen to discover the shiny new fairings were indeed aluminum! Bear with me for a brief wild-eyed and quixotic moment. Has anyone ever successfully CLAD the fairings with some suitable material......maybe something sharing similiar qualities with the shiny self adhesive heat reflective shielding some of us apply to the interior of the lower cowl? Does some shrinkable and long lasting material exist (perhaps known within in the RC world) that can be successfully applied to the complex surfaces of fiberglass fairings that matches the look of polished aluminum, but will over the long term, withstand the environment in which it will serve? To date, I have simply not observed a paint application that convincingly matches the look of polished aluminum. I only want to do this once. Short of carving form blocks, mastering 3003 alloy, dollys, and an english wheel, what's a simple homebuilder to do? Rick Galati RV-6A "finishing" Painting Gurus, Say you only wanted to paint your RV's fairings, tips, pants, skirt, you know, the glass parts, to sort of fool the non-RV world that it's all aluminum, what paint would you choose, and maybe why? I see PPG has all those "Mist" names for what-- on the computer screen-- look to be aluminum-like paints for Audi, Jaguar, Mercedes, etc.. But some of you must already have worked out this not-as-easy-as-it-looks problem. [No pun intended] Thanks, Jack -8 ________________________________________________________________________________
Subject: super 8
Date: Aug 25, 2004
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
SNIP Michael Stewart has some good information on the web here: http://www.mstewart.net/michael/rv/ SNIP From the website above: SNIP The Rockets are sexy and look great, but... I dont like the steel tube round gear. Wiggly wobblySNIP Ahem, the Rocket gear is not steel tube. Nor is it any more wiggly, wobbly than an RV-4, 6,or 7 gear. Wood stiffeners are required and will add about 37 cents to the cost of this project. SNIP But, if you fly the plane within the standard RV envelope for acro, and cruise around at 220, then it has been demonstrated you will probably not die. Your results may vary. SNIP All I can say is that no Rocket has ever shed its wings. Why would anyone want to put a 6 cylinder on an RV-8? Geez, put on an IO-360 and live with the measely 200HP. Super sixers, I hope your wings always arrive at the same place as your airframe. This is a penny-wise, pound-foolish project if I ever saw one. If money is your motivation to do this, then buy a SLOW BUILD Harmon kit from John and the cost will still be as cheap as an RV. Sorry for the flames... but better to have flames online than at the crash site!!! Vince Frazier F-1H Rocket, N540VF http://www.usi.edu/science/chemistry/vfrazier/page1.html ________________________________________________________________________________
Date: Aug 25, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Navaid VS EZ Pilot!
Dean Psiropoulos wrote: > > Ok Sam Buchanan: > > > After not bothering to respond to the email I sent you off list, you've > finally answered part of my questions to you. Good morning, Dean! I don't know what happened to the email you sent me since I never received it, but I am glad some (or maybe all as you will see shortly) of your questions have been answered. Specifically that the Navaid > works "OK" if you understand how it operates and use it to its full > potential. Great, that's good to hear. The Navaid does indeed work well most of the time once you figure it out but the key is "full potential". The full potential of the analog Navaid falls way short of the capabilities of the digital units. This isn't a slam against Navaid or its manufacturer, just a reflection of analog vs digital technology. NOW..could you please tell me and > the rest of the people on the list about the EZ Pilot electronics that > you've mated to your Navaid servo???? You say that the digital autopilots > are light years beyond the Navaid, great generalization, everybody else says > that too!!! How bout some good solid opinion on the EZ Pilot II by someone > who's used it quit a bit lately??? Dean, an archive search of the list will pull up several posts I have made concerning the EZ-Pilot. Or you can just hit this page on my web site to see some of the earliest posts: http://home.hiwaay.net/~sbuc/journal/EZ_Pilot.htm Hopefully you will consider these posts to be "good solid information". :-) The Navaid servo, even though designed many years ago, works beautifully with the digital control heads. It is an elegantly simple design that has proved to be reliable in many, many experimental planes. However, its days are numbered since all the digital manufacturers have either released their own modern servos or soon will. But for pilots who already have a Navaid installation, the old servo will deliver fine performance with the new autopilots that are designed to interface with it. Don't worry about stirring up a hornets > nest with the Tru Track people, I'm counting on that to get the rest of the > information I'm seeking. Now come on.cough it up!!!! I'm not worried in the least about stirring up the TruTrak folks; they are very capable of presenting their line of fine equipment on their own. Remember, I am a TruTrak customer since I fly their excellent AlTrak. TruTrak approached me about doing some beta testing of their Navaid version of the DigiTrak but since I already had the EZ-Pilot installed and was very pleased with it and the fine support of Trio Avionics I didn't see any point in getting in the middle of a competitive situation. Dean, you can download the installation and user manuals of both the EZ-Pilot and the DigiTrak from the respective websites. There are no secrets or black magic involved with these units; the info is right out in the open to anybody who does their homework. I'm not sure what other information you are seeking but I think a careful reading of the manuals will answer your questions. If not, don't hesitate to reply and I and other autopilot users, regardless of brand, will attempt to fill in the gaps. Now.....maybe I coughed up a bib-full..... ;-) Sam Buchanan ________________________________________________________________________________
From: "Eric Parlow" <ericparlow(at)hotmail.com>
Subject: Re: RVs at KTOA
Date: Aug 25, 2004
Tim, Thanks for the link. I had forgotten about it. I found 20 within 25 miles! ERic- RV-8 Wings ----Original Message Follows---- From: "Tim Bryan" <rv6flyer(at)improvementteam.com> Subject: Re: RV-List: RVs at KTOA Date: Tue, 24 Aug 2004 10:44:49 -0700 (Pacific Daylight Time) Hi Eric, Check out this fantastic tool that Dan put together. It is at: http://www.rvproject.com/registry/rvfinder.jsp Tim Bryan RV-6 N616TB -------Original Message------- From: rv-list(at)matronics.com Date: 08/24/04 09:28:25 Subject: RV-List: RVs at KTOA Looking for info on RVs, more specifically RV-8s, at KTOA. Or surrounding airports: KSMO, KLGB, KHHR. I'm considering moving there and RV's / Airports will weigh heavily into my decision. ERic-- RV-8 Wings ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: H2AD series engines
Date: Aug 25, 2004
NO! The dual MAG (no s) is a single unit with two mags inside. One drive but two mags (2000 series Bendix) Cy Galley - Chair, Emergency Aircraft Repair Safety Programs Editor - TC EAA Sport Pilot ----- Original Message ----- From: "linn walters" <lwalters2(at)cfl.rr.com> Subject: Re: RV-List: Re: H2AD series engines > > Jeff Bertsch wrote: > > > > >I had an O-320H2AD engine in my C-172. I had it overhauled and ran it for 2400 hours with absolutely no significant problems. The only thing that gave me problems was the dual mag, which is a pain to work on and I don't think is a good idea. > > > Aha! I'm a little slow. Couldn't figure out what all the fuss was > about with the dual mag ..... it's missing the 's'!!! Until the > electronic ignitions came along they all had dual mags :-D . I thought > it was a typo! I've known them as 'siamese mags' ..... and there really > is still two. And I agree ..... not my first choice .... nor second ;-) > . However, they still have a good track record for failures ..... can't > really compare them with separate mags ...... no data ...... but AFAIK, > after the initial problems were addressed, the O-320-H2AD is just as > solid as it's bretheren. > Linn > > > The engine compression was still in the mid to low 70's when I sold it. It was a great engine. We used Aeroshell 15w-50 which is required by AD (or you can use the Lyc additive). But I believe the real key is the plane flew frequently and never sat for more than 2 or 3 days without being flown. > > > >Jeff Bertsch > >lonestarsquadron.com > > > > > >--------------------------------- > > > > > > > > > > ________________________________________________________________________________
From: "David Carter" <dcarter(at)datarecall.net>
Subject: Re: Attachment showing up in RV List (or do I have a virus)????????
Date: Aug 25, 2004
On my computer, I get an "html attachment" IF the sender sent his e-mail in HTML format (to show color, photos, etc). That is due to a setting in Inbox-Outlook Express e-mail pgm - click Format, and see if Plain Text has a dot to left of it. That blocks display of the html content. If you click "HTML" then any e-mail sent in html format will display normally. However, none of the e-mails I get from RV-list or AeroElectric list have this "html attachment" because I believe Matt does not allow attachments and I suppose he sends out all the e-mails in txt format. I keep HTML turned off as a security precaution due to a security vulnerability of Microsoft's e-mail pgm wherein malicious code can be embedded in an HTML format e-mai. So, I suspect that the address is spoofed and it is malicious e-mail, as someone below explained. David ----- Original Message ----- From: "Alex Peterson" <alexpeterson(at)earthlink.net> Subject: RE: RV-List: Attachment showing up in RV List (or do I have a virus)???????? > > James is not the only one - since yesterday, all the messages from the > list have a text attachment, which is simply a copy of the message. > This has happened in the past, no clue what is going on. Other emails I > have received, not from the list, also have the attachment occasionally, > so it is likely not anything the list is generating. No clue. > > Alex Peterson > Maple Grove, MN > RV6-A N66AP 516 hours > http://www.home.earthlink.net/~alexpeterson/ > > > > > > If you have an attachment then the sending address is > > spoofed. All attachments on the Matronics list are stripped. > > > > > > ----- Original Message ----- > > From: "James E. Clark" <james(at)nextupventures.com> > > To: > > Subject: RV-List: Attachment showing up in RV List (or do I > > have a virus)???????? > > > > > > > --> > > > > > > Anyone else out there getting mail from the RV-List with an > > > "attachment"? > > > > > > Hope I don't have a virus or something. (Should be > > protected by virus > > > protection s/w) > > > > > > James > > ________________________________________________________________________________
Subject: super 8
Date: Aug 25, 2004
From: "Stewart, Michael (ISS Atlanta)" <mstewart(at)iss.net>
All good points Vince. Let me work em. 1. Perhaps "steel tube" was the wrong choice of words. I was trying to differentiate between the flat stock 8 gear that does not shake the plane at any speeds, and the solid tube steel round gear of the F-1 which exhibits the same gear leg shake as does the other RV series planes of the same design. The F-1 does have longer gear which I think exacerbates the problem. Having flown next to, section take off and landed with, played airborn next to the F-1, I have experienced this for myself. 2. You said " Why would anyone want to put a 6 cylinder on an RV-8? Geez, put on an IO-360 and live with the measely 200HP." My response is I don't want to live with 200. I want to live with 260 and have the many attributes of the 8 which I listed on my website that clearly spell out my reasons for doing such a thing so I wont rehash them here. 3. You said " If money is your motivation to do this, then buy a SLOW BUILD Harmon kit from John and the cost will still be as cheap as an RV." My response is I want the attributes of the 8, not 4, plain and simple. And I don't want to slow build a Harmon 4. 5. You said "All I can say is that no Rocket has ever shed its wings." And you are correct. Although the sample size if small. 4. And finally you said " Sorry for the flames... but better to have flames online than at the crash site!!!" No flames seen and all good comments Vince. I do respect your thoughts and they are all very worthy of consideration of my self and others risk/reward management. This Super 8 is not for the masses. Kind Regards, Mike Stewart -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Frazier, Vincent A Subject: RV-List: super 8 SNIP Michael Stewart has some good information on the web here: http://www.mstewart.net/michael/rv/ SNIP From the website above: SNIP The Rockets are sexy and look great, but... I dont like the steel tube round gear. Wiggly wobblySNIP Ahem, the Rocket gear is not steel tube. Nor is it any more wiggly, wobbly than an RV-4, 6,or 7 gear. Wood stiffeners are required and will add about 37 cents to the cost of this project. SNIP But, if you fly the plane within the standard RV envelope for acro, and cruise around at 220, then it has been demonstrated you will probably not die. Your results may vary. SNIP All I can say is that no Rocket has ever shed its wings. Why would anyone want to put a 6 cylinder on an RV-8? Geez, put on an IO-360 and live with the measely 200HP. Super sixers, I hope your wings always arrive at the same place as your airframe. This is a penny-wise, pound-foolish project if I ever saw one. If money is your motivation to do this, then buy a SLOW BUILD Harmon kit from John and the cost will still be as cheap as an RV. Sorry for the flames... but better to have flames online than at the crash site!!! Vince Frazier F-1H Rocket, N540VF http://www.usi.edu/science/chemistry/vfrazier/page1.html = = = = ________________________________________________________________________________
From: "Eric Irwin" <rv6eric(at)myacc.net>
Subject: Re: Aluminum matching paints
Date: Aug 25, 2004
Hey guys. I came across a paint product that is being marketed to custom motorcycle builders that you might be interested in. This company has a paint with a chrome finish and one with an aluminum finish (plus a lot of other cool paints). I have never seen it myself, but you can check out some pictures on their web site. Here is a link directly to the page with their chrome paints: http://www.alsacorp.com/chrome.htm Maybe this can give you the finish you are looking for. If you end up trying it, let me know how it works out. Eric -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Rick Galati Subject: RV-List: Re: Aluminum matching paints Judging from the underwhelming response to your interesting query I too must, (for the moment at least) conclude attaining such a polished look with paint is not quite as easy as we may want. Like you Jack, I have often wondered about the very same issue. AirVenture past, I approached an RV with some fairings that seemed to sport the closest match I had ever seen that attained the look of polished aluminum. I tipped my cap to the builder but was a bit crestfallen to discover the shiny new fairings were indeed aluminum! Bear with me for a brief wild-eyed and quixotic moment. Has anyone ever successfully CLAD the fairings with some suitable material......maybe something sharing similiar qualities with the shiny self adhesive heat reflective shielding some of us apply to the interior of the lower cowl? Does some shrinkable and long lasting material exist (perhaps known within in the RC world) that can be successfully applied to the complex surfaces of fiberglass fairings that matches the look of polished aluminum, but will over the long term, withstand the environment in which it will serve? To date, I have simply not observed a paint application that convincingly matches the look of polished aluminum. I only want to do this once. Short of carving form blocks, mastering 3003 alloy, dollys, and an english wheel, what's a simple homebuilder to do? Rick Galati RV-6A "finishing" Painting Gurus, Say you only wanted to paint your RV's fairings, tips, pants, skirt, you know, the glass parts, to sort of fool the non-RV world that it's all aluminum, what paint would you choose, and maybe why? I see PPG has all those "Mist" names for what-- on the computer screen-- look to be aluminum-like paints for Audi, Jaguar, Mercedes, etc.. But some of you must already have worked out this not-as-easy-as-it-looks problem. [No pun intended] Thanks, Jack -8 = direct advertising on the Matronics Forums. = = = ________________________________________________________________________________
From: "RV_8 Pilot" <rv_8pilot(at)hotmail.com>
Subject: super 8
Date: Aug 25, 2004
>SNIP The Rockets are sexy and look great, but... I dont like the >steel tube round gear. Wiggly wobblySNIP I've heard comments about the longer, tubular/round stock gear legs on F-1's and HR's being more bouncy or spongy than std RV's. >Ahem, the Rocket gear is not steel tube. Nor is it any more wiggly, >wobbly than an RV-4, 6,or 7 gear. Wood stiffeners are required and will >add about 37 cents to the cost of this project. That is the point - these all have tubular/round stock gear legs. and the Rocket legs are even longer. >Why would anyone want to put a 6 cylinder on an RV-8? For the same reasons Mike mentioned, plus a few others. O-540's are relatively cheap per hp (for now), particularly as compared to -360's. the weight of a -540/hp is attractive also IMO. I've already built an -8, so installing a -540 would be relatively painless as compared to building a Harmon Rocket or a much more expensive F-1 Rocket. >Geez, put on an IO-360 and live with the measely 200HP. I don't follow this point. >This is a penny-wise, pound-foolish project if I ever saw >one. If money is your motivation to do this, then buy a SLOW BUILD >Harmon kit from John and the cost will still be as cheap as an RV. >Sorry for the flames... but better to have flames online than at the >crash site!!! The overall risk of a -540 powered RV is probably higher than that of a -320 or -360 powered plane, but I believe it could be well managed. Seems to me there are roughly four factors to consider with a -540 powered RV. 1. Additional torque - not a major issue except when low, slow or in a botched takeoff/landing adding power. But still not a significant airframe issue. 2. Additional thrust - The additional thrust force on the airframe itself is not a significant issue either. Additional - yes, but not enough to cause concern IMO. 3. Additional dynamic flight loads - This one is the only one which would cause me concern. The Vne would be something that concerned me. But as Mike says - there are quite a few others pushing the RV envelope which might help raise the confidence level with this item. When doing acro, the load factors and entry speeds would have to be looked at closely. I'm pretty conservative with my acro, not regularly seeing anything more than about 3.2 g's anyway. You'd have to look at the motor mount and fuselage attachment to be sure the -540 and RV combo would be suitable at your chosed load factor. But most of this answers could be reverse engineered from the load factors RV's are seeing with -360's on the firewall. 4. Additional weight - The engine and prop would probably add 75 or 100-lbs over a 200-hp combo, just guessing. This is going to change stall speeds, maneuvering speeds, dynamics of flying, etc. Landings would have to be rethought a little, reducing the rough field and short field landing capability somewhat. changed speeds could be determined pretty accurately versus current when you know the new weight. Good discussions, particularly since I'd like to make this conversion one fo these days myself. Bryan Jones -8 www.LoneStarSquadron.com Houston, Texas ________________________________________________________________________________
Date: Aug 25, 2004
From: "Tim Bryan" <rv6flyer(at)improvementteam.com>
Subject: Re: Navaid VS EZ Pilot!
Listers and Dean, I spoke with Trio last week and was told the Navaid servo is what ships when you purchase the EZ pilot. It isn't a matter of matting the Navaid servo just because you have it. If you purchase a new EZ Pilot, you will still be using a Navaid servo. I don't know about the future of their own servos. Tim Bryan RV-6 N616TB -------Original Message------- From: rv-list(at)matronics.com Date: 08/25/04 07:10:32 Subject: Re: RV-List: Navaid VS EZ Pilot! Dean Psiropoulos wrote: com> > > Ok Sam Buchanan: > > > After not bothering to respond to the email I sent you off list, you've > finally answered part of my questions to you. Good morning, Dean! I don't know what happened to the email you sent me since I never received it, but I am glad some (or maybe all as you will see shortly) of your questions have been answered. Specifically that the Navaid > works "OK" if you understand how it operates and use it to its full > potential. Great, that's good to hear. The Navaid does indeed work well most of the time once you figure it out but the key is "full potential". The full potential of the analog Navaid falls way short of the capabilities of the digital units. This isn't a slam against Navaid or its manufacturer, just a reflection of analog vs digital technology. NOW..could you please tell me and > the rest of the people on the list about the EZ Pilot electronics that > you've mated to your Navaid servo???? You say that the digital autopilots > are light years beyond the Navaid, great generalization, everybody else says > that too!!! How bout some good solid opinion on the EZ Pilot II by someone > who's used it quit a bit lately??? Dean, an archive search of the list will pull up several posts I have made concerning the EZ-Pilot. Or you can just hit this page on my web site to see some of the earliest posts: http://home.hiwaay.net/~sbuc/journal/EZ_Pilot.htm Hopefully you will consider these posts to be "good solid information". :-) The Navaid servo, even though designed many years ago, works beautifully with the digital control heads. It is an elegantly simple design that has proved to be reliable in many, many experimental planes. However, its days are numbered since all the digital manufacturers have either released their own modern servos or soon will. But for pilots who already have a Navaid installation, the old servo will deliver fine performance with the new autopilots that are designed to interface with it. Don't worry about stirring up a hornets > nest with the Tru Track people, I'm counting on that to get the rest of the > information I'm seeking. Now come on.cough it up!!!! I'm not worried in the least about stirring up the TruTrak folks; they are very capable of presenting their line of fine equipment on their own. Remember, I am a TruTrak customer since I fly their excellent AlTrak. TruTrak approached me about doing some beta testing of their Navaid version of the DigiTrak but since I already had the EZ-Pilot installed and was very pleased with it and the fine support of Trio Avionics I didn't see any point in getting in the middle of a competitive situation. Dean, you can download the installation and user manuals of both the EZ-Pilot and the DigiTrak from the respective websites. There are no secrets or black magic involved with these units; the info is right out in the open to anybody who does their homework. I'm not sure what other information you are seeking but I think a careful reading of the manuals will answer your questions. If not, don't hesitate to reply and I and other autopilot users, regardless of brand, will attempt to fill in the gaps. Now.....maybe I coughed up a bib-full..... ;-) Sam Buchanan ________________________________________________________________________________
Date: Aug 25, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Navaid VS EZ Pilot!
Tim Bryan wrote: > > Listers and Dean, > > I spoke with Trio last week and was told the Navaid servo is what ships when > you purchase the EZ pilot. It isn't a matter of matting the Navaid servo > just because you have it. If you purchase a new EZ Pilot, you will still be > using a Navaid servo. I don't know about the future of their own servos. Whoa here! Let me nip this in the bud before it gets out of hand. I may have made an inference where it was unintended. I am privy to no information as to the future availability of the Navaid servo, but have heard absolutely nothing about its immediate demise. My point was about the inevitable replacement of analog servos with digital. The change will certainly occur eventually, but for now, the Navaid/Trio servo works fine, and pilots who install it should expect many years of reliable service. Sam Buchanan ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: Re: Aluminum matching paints
Date: Aug 25, 2004
I didn't see any replies to this do I'll take a shot. If you take a piece of polished aluminum to your local Sherwin Williams or other auto paint store, they will have a device that can mix a custom color to match. This approach is used with excellent results to match faded paints for collision damage repair. That said, everyone I've talked to advises me against this course because of the problems keeping bare aluminum looking good and the difficulty of reproducing the same shinyness. I'd paint the whole thing some aluminum color you like to keep from emphasizing the fiberglass parts. Dave Reel - RV8A ________________________________________________________________________________
Date: Aug 25, 2004
From: Bob Japundza <bjapundza(at)yahoo.com>
Subject: super 8
>I've heard comments about the longer, tubular/round >stock gear legs on F-1's >and HR's being more bouncy or spongy than std RV's. Absolutely not true. I recently had Mark Frederick's F1 and flew it for a dozen or so hours and found it handled better on the ground, had a better ride on the ground, and had LESS of a tendency to bounce compared to my -6. In fact it took some getting used to not knowing that you've actually touched down, you can grease it in that smooth. I have several friends with HR2's and have closely observed gear movement. It is more noticeable because these airplanes have longer wheelpants, but in reality the movement you see is just slightly more than you see on RV's. In formation you will see a little movement of the gear in the bumps when flying with a rocket, but only if you're looking for it. I've never really looked for it with RV's. In my experience the ti gear on the rockets is leaps and bounds better (no pun intended) than the gear on any RV-4-6-8 I've flown, and that's coming from my experience, not conjecture. As you could probably tell I like it. :) Why would anyone want a big motor?...efficiency. 195kts three-way gps runs burning 10.5gph running 2100rpm 23". Climbs from 700msl to 10.5K in under five minutes running max 340cht in the climb on a hot day. With a friend flying my 180c/s RV-6 next to me in the F1 at the same speed I was burning 1 gph less in the F1 running ROP. The super-8's in my area don't do nearly as well as the rockets, but they do better than the 200hp RV's. My only beef with the super 8 is that it is not supported by Van's. Regards, Bob Japundza RV-6 flying, F1 under const. Indy __________________________________ ________________________________________________________________________________
Date: Aug 25, 2004
From: Matt Dralle <dralle(at)matronics.com>
Subject: Re: Attachment showing up in RV List (or do I have a
virus)???????? David's assertions below are right on the mark. If you receive a message from the "RV-List" that has an attachment, then it is a spoof and not from Matronics. It likely has a virus, too, and should be deleted immediately. Matt Dralle Matronics Email List Admin At 07:17 AM 8/25/2004 Wednesday, you wrote: > >On my computer, I get an "html attachment" IF the sender sent his e-mail in >HTML format (to show color, photos, etc). That is due to a setting in >Inbox-Outlook Express e-mail pgm - click Format, and see if Plain Text has a >dot to left of it. That blocks display of the html content. If you click >"HTML" then any e-mail sent in html format will display normally. > >However, none of the e-mails I get from RV-list or AeroElectric list have >this "html attachment" because I believe Matt does not allow attachments and >I suppose he sends out all the e-mails in txt format. > >I keep HTML turned off as a security precaution due to a security >vulnerability of Microsoft's e-mail pgm wherein malicious code can be >embedded in an HTML format e-mai. > >So, I suspect that the address is spoofed and it is malicious e-mail, as >someone below explained. > >David > >----- Original Message ----- >From: "Alex Peterson" <alexpeterson(at)earthlink.net> >To: >Subject: RE: RV-List: Attachment showing up in RV List (or do I have a >virus)???????? > > > > > > > James is not the only one - since yesterday, all the messages from the > > list have a text attachment, which is simply a copy of the message. > > This has happened in the past, no clue what is going on. Other emails I > > have received, not from the list, also have the attachment occasionally, > > so it is likely not anything the list is generating. No clue. > > > > Alex Peterson > > Maple Grove, MN > > RV6-A N66AP 516 hours > > http://www.home.earthlink.net/~alexpeterson/ > > > > > > > > > > If you have an attachment then the sending address is > > > spoofed. All attachments on the Matronics list are stripped. > > > > > > > > > ----- Original Message ----- > > > From: "James E. Clark" <james(at)nextupventures.com> > > > To: > > > Subject: RV-List: Attachment showing up in RV List (or do I > > > have a virus)???????? > > > > > > > > > > --> > > > > > > > > Anyone else out there getting mail from the RV-List with an > > > > "attachment"? > > > > > > > > Hope I don't have a virus or something. (Should be > > > protected by virus > > > > protection s/w) > > > > > > > > James > > > > > > Matt G Dralle | Matronics | PO Box 347 | Livermore | CA | 94551 925-606-1001 V | 925-606-6281 F | dralle(at)matronics.com Email http://www.matronics.com/ WWW | Featuring Products For Aircraft ________________________________________________________________________________
From: "Doug Rozendaal" <dougr(at)petroblend.com>
Subject: Re: super 8
Date: Aug 25, 2004
All, This is an excellent discussion, exactly the kind that needs to occur in a forum like this. The RVs are great designs. Everything in the design of an airplane is a compromise. Most elements in the design of an airplane are inter-related. Aspect ratio vs spar strength vs wing area vs stall speed etc..... My question is in flying a Super-8, what do you give up???? And how do you operate it within it's enevelope? I have a helluva time operating my IO-320 -4 within it's envelope. I blow the recommended aerobatic gross weight nearly every time I fly. I give up G-loading, I use +4/-2 as my aerobatic limits. It is hard to stay below redline in a descent. I try not to break the redline, but still hear my RMencoder bitching at me about Vne more frequently than I should. There is really nothing I can give up to raise Vne. I would have to redesign the airplane. If operated at +4/-2 (at aerobatic gross weight) and with a healthy respect for Vno and Vne a Super-8 might work fine, but a Super-8 is going to be a challenge to fly within those limits. I did a presentation at the MN RV forum called "The Wing Removal Lever, and how Not to use it" It studied the V-N diagram of the RV-8. At Vne the RV-8 has 18 G available......... Twice its failure limit......... These are not fragile airplanes, but because the stall speed is so low, they awesome power available to break themselves. A Super-8 would be a GREAT airplane for high altitude cruise, becasue more displacement is a much easier cheaper and safer solution than a turbo charger. But a Super-8 is not an idiot proof airplane, and needs to be flown carefully. Tailwinds, Doug Rozendaal ________________________________________________________________________________
From: "Kathleen (rv7)" <Kathleen(at)rv7.us>
Subject: Aluminum matching paints
Date: Aug 25, 2004
You can try 20209 MONOKOTE CHROME. It can be laid up over your fairings and can be shrunk with a heat gun. It is very chrome like and may be too reflective to match the polished aluminum unless you have the gloss level way up there. I don't think the aluminum Monokote looks like anything other than brushed aluminum... Kathleen Evans Folsom, CA www.rv7.us -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of DAVID REEL Subject: Re: RV-List: Aluminum matching paints I didn't see any replies to this do I'll take a shot. If you take a piece of polished aluminum to your local Sherwin Williams or other auto paint store, they will have a device that can mix a custom color to match. This approach is used with excellent results to match faded paints for collision damage repair. That said, everyone I've talked to advises me against this course because of the problems keeping bare aluminum looking good and the difficulty of reproducing the same shinyness. I'd paint the whole thing some aluminum color you like to keep from emphasizing the fiberglass parts. Dave Reel - RV8A advertising on the Matronics Forums. ________________________________________________________________________________
Subject: super 8
Date: Aug 25, 2004
From: "Stewart, Michael (ISS Atlanta)" <mstewart(at)iss.net>
I was hoping you would weigh in Bob since you clearly have lots of experience around all these items. I have absolutely no issue with the bounce factor personally. It was the taxi wobble, shake, braking shimmy noticeable in the all the rv tail draggers and more noticeable in the various "rockets." Bob what is the issue around the "Unsupported by Vans" that bothers you? Vans does not support all kinds of things. Why is that a factor? I have as a top 3 list of reasons why I chose the Super 8 the fact that IS a Vans plane first. What would you like them to support that they don't already? The idea? You know that's never happening. Mike -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Bob Japundza Subject: RE: RV-List: super 8 >I've heard comments about the longer, tubular/round >stock gear legs on F-1's >and HR's being more bouncy or spongy than std RV's. Absolutely not true. I recently had Mark Frederick's F1 and flew it for a dozen or so hours and found it handled better on the ground, had a better ride on the ground, and had LESS of a tendency to bounce compared to my -6. In fact it took some getting used to not knowing that you've actually touched down, you can grease it in that smooth. I have several friends with HR2's and have closely observed gear movement. It is more noticeable because these airplanes have longer wheelpants, but in reality the movement you see is just slightly more than you see on RV's. In formation you will see a little movement of the gear in the bumps when flying with a rocket, but only if you're looking for it. I've never really looked for it with RV's. In my experience the ti gear on the rockets is leaps and bounds better (no pun intended) than the gear on any RV-4-6-8 I've flown, and that's coming from my experience, not conjecture. As you could probably tell I like it. :) Why would anyone want a big motor?...efficiency. 195kts three-way gps runs burning 10.5gph running 2100rpm 23". Climbs from 700msl to 10.5K in under five minutes running max 340cht in the climb on a hot day. With a friend flying my 180c/s RV-6 next to me in the F1 at the same speed I was burning 1 gph less in the F1 running ROP. The super-8's in my area don't do nearly as well as the rockets, but they do better than the 200hp RV's. My only beef with the super 8 is that it is not supported by Van's. Regards, Bob Japundza RV-6 flying, F1 under const. Indy __________________________________ = = = = ________________________________________________________________________________
Date: Aug 25, 2004
From: Garey Wittich <gareywittich2000(at)yahoo.com>
Subject: "Need Extra Hands" in building a RV-8A QB - Santa Monica, Calif
rv8-list(at)matronics.com, rv9-list(at)matronics.com, rv-list(at)matronics.com Greetings: Any Builders who live in the Santa Monica, Calif area. Building a RV-8A QB in my garage 5 minutes from Santa Monica Airport and "need extra hands". Willing to help somebody with their project TOO. My wife does not want to get involved and the local EAA Chapter is all composite builders. At the rate I am making progress it will take me 5 life times to complete !!!!! Thanks, Garey Wittich (310) 392-1682 __________________________________ ________________________________________________________________________________
Date: Aug 25, 2004
From: Skylor Piper <skylor4(at)yahoo.com>
Subject: super 8
> -----Original Message----- > > > Why would anyone want a big motor?...efficiency. > 195kts three-way gps runs burning 10.5gph running > 2100rpm 23". Climbs from 700msl to 10.5K in under > five minutes running max 340cht in the climb on a > hot > day. With a friend flying my 180c/s RV-6 next to me > in the F1 at the same speed I was burning 1 gph less > in the F1 running ROP. > I'm going to ask a somewhat obvious question here: Why is the IO-540 more efficient than the 360? Pardon my ignorance, but this doesn't make that much sense to me. The parallel valve 540's and 360's use the same cylinders (right?). For a given horsepower smaller engines are usually more efficient, especially when the two are of nearly identical designs. It should also take the same amount of horsepower to fly similar airframes at the same speed (actually slightly more for a Super 8 vs. standard 8 because of more weight and drag). Perhaps the larger engine can turn a larger prop, and gain some efficiency there, but I still don't see this as making a significant difference in this case. Maybe the F1 is just a more efficient airframe than the -6. In this case, I think those hoping for an increase in efficiency by going to a Super 8 are going to be disappointed. Comments? _______________________________ ________________________________________________________________________________
From: Laird Owens <owens(at)aerovironment.com>
Subject: Re: "Need Extra Hands" in building a RV-8A QB - Santa Monica,
Calif
Date: Aug 25, 2004
Garey, You should also post your note at: http://groups.yahoo.com/group/SoCAL-RVlist/ Lots of folks on our SoCal list that might be able to help. I always wondered why I started to itch every time I drove by Santa Monica...... Laird - Simi Valley RV-6 @ Whiteman On Aug 25, 2004, at 12:04 PM, Garey Wittich wrote: > > > Greetings: > > Any Builders who live in the Santa Monica, Calif area. > Building a RV-8A QB in my garage 5 minutes from Santa > Monica Airport and "need extra hands". Willing to > help somebody with their project TOO. My wife does > not want to get involved and the local EAA Chapter is > all composite builders. At the rate I am making > progress it will take me 5 life times to complete > !!!!! > > Thanks, > Garey Wittich (310) 392-1682 > > > __________________________________ > > > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > _- > ======================================================================= > > > > ________________________________________________________________________________
From: "Albert Gardner" <spudnut(at)worldnet.att.net>
Subject: Re: Need Compass
Date: Aug 25, 2004
I put the OAT probe from my EI gage in the NACA vent and the readings always agree with those reported from other planes so it works for me. Albert Gardner RV-9A 872RV Yuma, AZ ----- Original Message ----- From: "Chuck Weyant" <cweyant(at)chuckdirect.com> Subject: Re: RV-List: Need Compass > > I've found, in my Grumman AA1a, that the OAT sensor located in the NACA vent > on the side of the fuselage, is inaccurate in flight. Seems it gets radiant > heat from the engine and registers about 20 degrees too high. Could this be > a problem with the RV NACA vent install? > Chuck ________________________________________________________________________________
Date: Aug 25, 2004
From: Bob Japundza <bjapundza(at)yahoo.com>
Subject: super 8
>I have absolutely no issue with the bounce factor >personally. It was the taxi wobble, shake, braking >shimmy noticeable in the all the rv tail draggers >and more noticeable in the various "rockets." My opinion here is that the more freedom of movement allowed at the axle, the less stress will be transmitted to the airframe where the gearleg joins. The wheel is free to move in more than one axis so it can absorb/rebound loads. With the flat design, you essentially only have one axis of movement (up/down) and rely on a rigid attachment to the airframe (gearbox) to provide dampening of any loads at the axle (fore/aft). >Bob what is the issue around the "Unsupported by >Vans" that bothers you? Vans does not support all >kinds of things. Why is that a factor? I have as a >top 3 list of reasons why I chose the Super 8 the >fact that IS a Vans plane first. What would you like >them to support that they don't already? The idea? >You know that's never happening. Yes you are correct that they don't like lots of things and in some respects I don't blame them given the legal environment in our country. On the other hand, if this sort of experimentation never happened (super 8's, rockets, etc.), we'd all be flying stits playboys right now. That 'e' word written in 2" high letters is a great thing, isn't it? I don't in any way put anyone down for hanging a 540 on an -8. But there are some unknowns with the wing being operated at higher gross weights and higher airspeeds that limit the advantages you gain with hanging a big motor up front. I'm pretty certain Van's won't give you any analysis on that. Unless you know those limits, you'll have to operate somewhere well under what you think those limits are, that's gonna take some fun factor out of the equation. Regards, Bob Japundza RV-6 180c/s flying "weenie motor" F1 under const. Indy __________________________________ ________________________________________________________________________________
Subject: IFR instruments
Date: Aug 25, 2004
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
, , , 1.7 SUSPICIOUS_RECIPS Similar addresses in recipient list Hi Guys, I was almost convinced the Garmin GNS 430 hooked to a Dynon and a Digitrack A/P was the almost perfect base to a light weight IFR setup for an RV-7, then I see that BMA has come out with the EFIS Lite G3 which has the GPS, and an electronic version of the VOR/GS receiver that can be driven by an SL30 Navcom. Apparently this system drives a BMA 2 axis autopilot. Looking at all of this gives me aN IFR panel for about $11k including the transponder and 2 axis A/P. The similar setup using the GNS 430 comes in at about $14.5K with single axis A/P. Anyone have any experience or thoughts on this set up? I haven't started IFR training yet so I'm fumbling a little on all the requirements...Not sure about the "indicator lights" (marker beacon?) that are apparently built into the Nav head that the GNS 430 would drive. Frank ________________________________________________________________________________
Date: Aug 25, 2004
From: Kevin Horton <khorton01(at)rogers.com>
Subject: super 8
> >I don't in any >way put anyone down for hanging a 540 on an -8. But >there are some unknowns with the wing being operated >at higher gross weights and higher airspeeds that >limit the advantages you gain with hanging a big motor >up front. I'm pretty certain Van's won't give you any >analysis on that. Unless you know those limits, >you'll have to operate somewhere well under what you >think those limits are, that's gonna take some fun >factor out of the equation. Just curious - has anyone done static load testing on the HR wing? If so, who did it and what gross weight and g did the testing simulate? Also, how do the HR and F-1 wing designs compare? -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ ________________________________________________________________________________
Date: Aug 25, 2004
From: Bob Japundza <bjapundza(at)yahoo.com>
Subject: super 8
>Just curious - has anyone done static load testing >on the HR wing? If so, who did it and what gross >weight and g did the testing simulate? It is my understanding that John Harmon had an engineering evaluation done on the HR wing sometime in the mid-90's. I don't know if any static load testing has been done. To that end I don't know if its ever been done on the RV-4 either. There's never been a in-flight failure that I'm aware of. >Also, how do the HR and F-1 wing designs compare? Nearly identical. Regards, Bob __________________________________ ________________________________________________________________________________
Date: Aug 25, 2004
From: "Stein Bruch" <stein(at)steinair.com>
Subject: super 8
Used to be, but not anymore... The F-1 wing couldn't be further from an RV wing if you tried. The new EVO wing is a tapered wing, both in chord and span. It's really an amazing piece of work and comes finished from Tearm Rocket/HPA...the work looks top notch from what I've seen, and I really scrutinzed it at OSH. If you saw it at OSH you'd know what I mean. Also, it "apparantly" has resulted in higher cruise speed and slightly lowered stall speed. Plus....it looks like a piece of a rocket!! Last thing...about that gear argument. They really aren't that similar, other than being tapered rods. The rockets are Titanium, machined flat for a lot of the length, and attache via a tapered cone (like the CNC Morris Taper bits), and the Van's are steel (or can be AL2 on the -8's). If and when I build something with a 6 banger on the front, I'd love a rocket. That being said, the $46K entry price is a lot more than the Van's planes...so that -10 is also pretty attractive at $10K less (slow build vs. fast build). Cheers, Stein Bruch Minneapolis ---------- Original Message ---------------------------------- From: Bob Japundza <bjapundza(at)yahoo.com> Date: Wed, 25 Aug 2004 15:36:18 -0700 (PDT) > >>Also, how do the HR and F-1 wing designs compare? > >Nearly identical. > >Regards, >Bob > > > >__________________________________ > > ________________________________________________________________________________
From: "Jerry Hansen" <jerry-hansen(at)cox.net>
Subject: RE: RV8-List: IFR instruments
Date: Aug 25, 2004
Many newer digital autopilots aimed at the experimental market find their best reference for navigation in a properly configured GPS data stream. The NMEA 0183 data stream and the AVLINK data stream (from Garmin and others) adhere to strict standards. Such digital autopilots are designed to accept data that adheres to these standards, and they typically work remarkably well when using such precise digital data. EFIS systems must also get their navigation information from outside sources, such as GPS. They may then process this information and provide an output for use by autopilots. If you are going to attach an autopilot to these systems, you MUST know what processes are being performed to the NMEA 0183 or AVLINK data streams once the EFIS digests it and provides an output to an autopilot. Some EFIS systems can get a little tricky in their "Heading" mode. When you select a heading on the EFIS, they might create a "phantom" waypoint some distance ahead of the aircraft at the heading that was selected. They then put this in the data stream, replacing the GPS BTW (Bearing to Waypoint) data with BTW of the phantom waypoint. The autopilot will then track to this course if the data is in the correct format. There can be some unknown parameters here... how far away is the "phantom" waypoint - is the autopilot capable of tracking to the output data as configured - are all of the required data passed through from the NMEA information (typically the RMB and RMC sentences) - and a whole host of other questions that must be addressed by the EFIS and autopilot manufacturers to assure fail safe operation. This is not to say that these systems won't work together. Just a "heads up" to prompt questions that might be asked of potential suppliers of such equipment - to be sure that you don't find yourself in a dark cumulus cloud someday with these questions left unanswered. Check with the systems manufacturers to get absolute assurance of compatibility. Remember that many of the EFIS and autopilot systems that are directed to experimental aircraft are not "certified" and therefore have not been subjected to the rigorous testing that is demanded by certification. This should create a huge question mark above your head. Jerry -----Original Message----- From: owner-rv8-list-server(at)matronics.com [mailto:owner-rv8-list-server(at)matronics.com] On Behalf Of Tony Johnson Subject: RE: RV8-List: IFR instruments --> RV8-List message posted by: "Tony Johnson" Frank, I am also interested in learning more about the BMA EFIS lite 3. I do have some concerns about using it for IFR applications. Let me preface this by saying that I am no expert, and I am not even IFR rated at this point. It is my understanding that for a GPS to be approved for IFR it must have a left-right indication and annunciators. The G3 seems to have the left-right indication, but I did not see any indication that it had the annuciators. That would add about $750 to the package. The other issue is that I think, but do not know, that a GPS used for IFR work would have to be certified (or meet the TSO requirements) for IFR, either enroute or approach even in an experimental aircraft. I have not seen any indication that the G3 meets these requirements. The G3 is an impressive unit, although it lacks some of the features of the dynon, it has adds more. I did not see any indication that the G3 has AOA information, OAT, or density altitude. It does have winds aloft information, both speed and direction. I am wondering if it will interface with a NAVAID, and take VOR info from a NARCO Nav radio. I emailed BMA today with those questions. I will be interested in the observations and knowledge of other listers. Tony Johnson RV8A Orlando -----Original Message----- From: owner-rv8-list-server(at)matronics.com [mailto:owner-rv8-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) rv8-list(at)matronics.com; rv9-list(at)matronics.com; rv-list(at)matronics.com Subject: RV8-List: IFR instruments --> RV8-List message posted by: "Hinde, Frank George (Corvallis)" Hi Guys, I was almost convinced the Garmin GNS 430 hooked to a Dynon and a Digitrack A/P was the almost perfect base to a light weight IFR setup for an RV-7, then I see that BMA has come out with the EFIS Lite G3 which has the GPS, and an electronic version of the VOR/GS receiver that can be driven by an SL30 Navcom. Apparently this system drives a BMA 2 axis autopilot. Looking at all of this gives me aN IFR panel for about $11k including the transponder and 2 axis A/P. The similar setup using the GNS 430 comes in at about $14.5K with single axis A/P. Anyone have any experience or thoughts on this set up? I haven't started IFR training yet so I'm fumbling a little on all the requirements...Not sure about the "indicator lights" (marker beacon?) that are apparently built into the Nav head that the GNS 430 would drive. Frank ________________________________________________________________________________
From: "Jim Anglin" <jlanglin44(at)earthlink.net>
Subject: Re: super 8
Date: Aug 25, 2004
I almost have my HR II finished - the last thing I will have to buy is paint. I have less than $55K in it. I would like to see anyone build an IFR RV of any kind for less than that. I bought the 4 kit and John's kit and if that is what you call an entry price it's nowhere near $46K. Plus it is a better looking plane than the F 1 IMHO. Jim ----- Original Message ----- From: "Stein Bruch" <stein(at)steinair.com> Subject: RE: RV-List: super 8 > > Used to be, but not anymore... > > The F-1 wing couldn't be further from an RV wing if you tried. The new EVO wing is a tapered wing, both in chord and span. It's really an amazing piece of work and comes finished from Tearm Rocket/HPA...the work looks top notch from what I've seen, and I really scrutinzed it at OSH. If you saw it at OSH you'd know what I mean. Also, it "apparantly" has resulted in higher cruise speed and slightly lowered stall speed. Plus....it looks like a piece of a rocket!! > > Last thing...about that gear argument. They really aren't that similar, other than being tapered rods. The rockets are Titanium, machined flat for a lot of the length, and attache via a tapered cone (like the CNC Morris Taper bits), and the Van's are steel (or can be AL2 on the -8's). > > If and when I build something with a 6 banger on the front, I'd love a rocket. That being said, the $46K entry price is a lot more than the Van's planes...so that -10 is also pretty attractive at $10K less (slow build vs. fast build). > > Cheers, > Stein Bruch > Minneapolis > > > ---------- Original Message ---------------------------------- > From: Bob Japundza <bjapundza(at)yahoo.com> > Date: Wed, 25 Aug 2004 15:36:18 -0700 (PDT) > > > >>Also, how do the HR and F-1 wing designs compare? > > > >Nearly identical. > > > >Regards, > >Bob > > > > > > > >__________________________________ > > > > > > ________________________________________________________________________________
Date: Aug 25, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: A peek into the future??
This is not related to RV-dom in its present form, but who knows what we will have in the panel a decade from now? What would our electronic flight instruments look like if they were not mimicking mechanical gyros? What if there was a way to portray all flight parameters in a format that didn't require an instrument scan? The following link is to a study that is investigating these questions. I do not make any claims to understand even half of what is discussed in the paper, but I find it fascinating to consider how our flight instruments may appear at some time in the future. Maybe those instrument panels on Star Trek weren't that outrageous after all! http://www.ihmc.us/research/projects/OZ_UCAV/downloads/OzHumanCenteredComputing.pdf No doubt if something along the lines of the above study ever happens, it will be available commercially first in the realm of experimental aviation. Sam Buchanan ________________________________________________________________________________
Date: Aug 25, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Temporary hangar space in Birmingham
Doug, check with Doug Preston. He is a corporate pilot and TVRVBGer based at Bessemer and he may be able to find room for you. dougpflyrv(at)aol.com Sam =========================== Doug Weiler wrote: > > Fellow Listers: > > There is a chance that I may be in desperate need of hangar space for my > RV-4 in the Birmingham, AL area from Aug 29 - Sep 3. My recourse is to > hangar with one of the big FBO's at the BHM airport which could get rather > pricey. Anyone have any ideas? > > Please contact off list or call my cell at 651-398-1184 > > Many thanks, > > Doug Weiler, pres MN Wing ________________________________________________________________________________
From: "Jaye and Scott Jackson" <jayeandscott(at)telus.net>
Subject: Re: A peek into the future??
Date: Aug 25, 2004
The ultimate goal would be to make all flying, including night, in-cloud, etc., just like day, CAVU flying. How the environment outside is detected and generated, either by radar, infrared sensors, or GPS/terrain database interface, with the resulting image projected either on a head-up display, or holographically, remains to be seen. Flight directors, then, become not unlike driving along a winding, coastal road, with rises and falls, with the commanded path looking either like a road with a centreline, or a series of windows to steer through. Surrounded here by coastal mountains on three sides, imagine flying through a mountain pass in the dark, or solid cloud...... Scott in Vancouver ----- Original Message ----- From: "Sam Buchanan" <sbuc(at)hiwaay.net> Subject: RV-List: A peek into the future?? > > This is not related to RV-dom in its present form, but who knows what we > will have in the panel a decade from now? > > What would our electronic flight instruments look like if they were not > mimicking mechanical gyros? What if there was a way to portray all > flight parameters in a format that didn't require an instrument scan? > > The following link is to a study that is investigating these questions. > I do not make any claims to understand even half of what is discussed in > the paper, but I find it fascinating to consider how our flight > instruments may appear at some time in the future. Maybe those > instrument panels on Star Trek weren't that outrageous after all! > > http://www.ihmc.us/research/projects/OZ_UCAV/downloads/OzHumanCenteredComputing.pdf > > No doubt if something along the lines of the above study ever happens, > it will be available commercially first in the realm of experimental > aviation. > > Sam Buchanan > > ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: A peek into the future??
Date: Aug 25, 2004
Sam, I read through that report last night after reading about it on the Blue Mountain discussion board. My first reaction was to wonder what all those weird symbols were all about, but it's pretty hard to deny the results of their experiments. In essence, they found that using the Oz symbols, inexperienced pilots were much more capable of controlling the airplane (actually, flight simulator) under varying conditions of turbulence and distraction (reading text) than they were with conventional instrumentation. I can easily imagine a time in the near future when part of the start-up process for your EFIS system is to choose Oz or conventional symbology. It would seem that it would be a relatively simple matter with a glass cockpit to choose how you wanted the information presented. Oh, and Greg at Blue Mountain is onto it. Terry RV-8 still wiring -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Sam Buchanan Subject: RV-List: A peek into the future?? This is not related to RV-dom in its present form, but who knows what we will have in the panel a decade from now? What would our electronic flight instruments look like if they were not mimicking mechanical gyros? What if there was a way to portray all flight parameters in a format that didn't require an instrument scan? The following link is to a study that is investigating these questions. I do not make any claims to understand even half of what is discussed in the paper, but I find it fascinating to consider how our flight instruments may appear at some time in the future. Maybe those instrument panels on Star Trek weren't that outrageous after all! http://www.ihmc.us/research/projects/OZ_UCAV/downloads/OzHumanCenteredComput ing.pdf No doubt if something along the lines of the above study ever happens, it will be available commercially first in the realm of experimental aviation. Sam Buchanan ________________________________________________________________________________
From: "sheldon barrett" <sheldonb(at)frontiernet.net>
Subject: Any RV builders/flyers in New Zealand?
Date: Aug 26, 2004
Going to New Zealand Oct 3rd to Oct 15th.. Was wondering if there are any RV guys/gals there for a looksee visit monitoring the list? Sheldon Barrett RV6A (Champ RV6 at LOE3). sheldon(at)frontiernet.net ________________________________________________________________________________
From: "Doug Weiler" <dcw(at)nomadwi.com>
Subject: Re: Temporary hangar space in Birmingham
Date: Aug 26, 2004
Thanks Sam ----- Original Message ----- From: "Sam Buchanan" <sbuc(at)hiwaay.net> Subject: RV-List: Temporary hangar space in Birmingham > > Doug, check with Doug Preston. He is a corporate pilot and TVRVBGer > based at Bessemer and he may be able to find room for you. > > dougpflyrv(at)aol.com > > Sam > > =========================== > > Doug Weiler wrote: > > > > > Fellow Listers: > > > > There is a chance that I may be in desperate need of hangar space for my > > RV-4 in the Birmingham, AL area from Aug 29 - Sep 3. My recourse is to > > hangar with one of the big FBO's at the BHM airport which could get rather > > pricey. Anyone have any ideas? > > > > Please contact off list or call my cell at 651-398-1184 > > > > Many thanks, > > > > Doug Weiler, pres MN Wing > > ________________________________________________________________________________
Subject: more Rocket/Super 8 comments
Date: Aug 26, 2004
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
He he he.... I have to laugh because the Rocket list never gets this much action on any topic. LOL Also Michael Stewart has been a real gentleman throughout this thread. We had emailed back and forth several times yesterday before my pea-brain made the connection that it was his website comments that I was tromping on! Some guys aren't so gracious and I take my hat off to Michael for putting up with our well intended barbs. I would not have any qualms about the Super 8s (or Super 6s either)if some simple strengthening mods were done. It would be very easy to copy what John Harmon has done on the Rocket and apply that to the RV airframe. Most of the mods would involve a relatively simple increase in skin thickness. Adding length to the tail would get a bit more involved but is still reasonably straightforward. For anyone who doesn't know what John Harmon did to Rocketize an RV-4, here's a brief overview: the wings are shortened about 7" per side and the rib spacing is decreased, the tail is lengthened about 7" with 4" of that length added between the seats, several skins in the forward fuselage are thickened, a different cowl, motor mount, canopy, and several widened bulkheads are needed due to widening of the fuselage. (Obviously the 8 wouldn't need to be widened.) And, of course, a big IO-540-C4B5 motor and HUGE Hartzell prop are installed...don't kid yourself here... this is why it's a 1200# Rocket and not a 950# RV-4 anymore. Please do the math for yourself.... 250# difference and most of it is on the nose! The gear geometry on the Rockets is changed to accommodate the weight on the nose, with the Harmons tending to be more nose heavy on the ground. The F-1 wheels are slightly farther forward to put more weight on the tail. I'd be leary of simply leaving the RV-8 gear "as is" while adding all of that weight up front. But I have no knowledge of the Super 8s ground manners. Perhaps Bob J. will chime in again. I've had the opportunity to ride in 3 different Harmons. The gear never misbehaved whatsoever. Bob Japundza had a very good description of the titanium gear yesterday. (I hate to say it in public, but I have a high regard for Bob's opinions. He usually has it right.) Incidentally, the titatium gear legs are without a doubt, the single most expensive part of the entire airframe. I think I paid $850 apiece!!! If money makes it good, these gear legs must be awesome! ;-) There was discussion of cost also. My half breed Harmon/F1 Rocket has a 0-time Lyc and brand new prop, fully painted and upholstered, Grand Rapids EFIS based panel with brand new avionics, etc, etc,... ALL new everything, and I have all of the receipts to prove that I've not popped the $50,000 barrier yet. I have taken exactly 5 years of spare time to build it. So, IMHO, a Super 8 with the Rocket mods listed above, and a Rocket gear instead of the gear towers crowding your thighs would be "da bomb". There's even a turtledeck mod for the RV-8 that a local RV-8 builder (and others) have done. Looks nice. Regards, Vince Frazier F-1H Rocket, N540VF http://www.usi.edu/science/chemistry/vfrazier/page1.html ________________________________________________________________________________
From: "RV_8 Pilot" <rv_8pilot(at)hotmail.com>
Subject: Firewall color
Date: Aug 26, 2004
>I understand paint will not stick to the stainless so Sure it will. Just needs to be clean and have an anchor pattern. >sheet of 24 gold plate plate, gold foil, gold whatever. Remember, my >firewall is already attached awaiting the install of my engine mount for >the >rotary but only after figuring out how to "gold" the firewall. I'm not thinking very creatively this morning, so I can't offer much advice on making it gold right now. But you do realize that nice, shiny stainless steel will reflect radiant energy (heat) better than any color, helping to keep your feet cool. If I just had to have it gold, I'd buff the outer surface of the firewall or maybe use a portable grit blaster to rough it up a little. Clean it/degrease it really well, then shoot it with a gold metallic flake automotive paint (urethane, acrylic). IMO, it's a little late for electroplating. 2 cents Bryan ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: 153MC flies today
Date: Aug 26, 2004
Noel, CONGRATULATIONS and WELL DONE - Again !!!!! Chuck & Dave Rowbotham RV-8A >From: "Noel & Yoshie Simmons" <noel(at)blueskyaviation.net> >Reply-To: rv-list(at)matronics.com >To: "Rv-List(at)Matronics. Com" , "rvyahoo" > >Subject: RV-List: 153MC flies today >Date: Tue, 24 Aug 2004 20:28:35 -0600 > > > >Had a great day today, took RV-6A 153MC off the ground for the fist time >today. Subsequently put 7 hours on it with out a hitch, god I love VAN'S >stuff. > >O-360-A1A >Holy Cowl with plenum >NACA scoop for oil cooler >Fixed pitch >basic panel > >after 4 RV's I still get that RV grin >:>))))))))))))))))))))))))))))))))))))) > >Sincerely, > >Noel Simmons >Blue Sky Aviation, Inc. >Phone & Fax: 406-538-6574 >noel(at)blueskyaviation.net > <http://www.blueskyaviation.net/> www.blueskyaviation.net ________________________________________________________________________________
From: "Greg Young" <gyoung@cs-sol.com>
Subject: A peek into the future??
Date: Aug 26, 2004
One issue I've never seen debated is the risk management/tolerance of these systems, be it OZ, SATS, HITS or ??. The NASA SATS program seemingly wants to hand the airplane keys to anyone checked out on a Game Boy. Great concept - make it super easy to fly in all weather and the flying population will grow enough to support the ground infrastructure. Except what happens when the electrowizzies die and the "pilot/console operator" has never flown anything else? The old timers (and FAA?) will say everyone needs to be able to fly the old way, partial panel, needle-ball-airspeed, just like Lindy. That destroys the benefit of the shallow learning curve. It's kind of a bank loan approach - you only get the benefits if you don't need them. Accepting that an occasional SATS airplane will fall out of the sky is likely not politically (or insurance) acceptable. Maybe the answer is in higher redundancy or recovery chutes ala Cirrus (OMG I can't believe I wrote that) or anti-gravity belts or something else. Personally, I'd like to see the OZ/SATS/HITS concepts flourish. I won't have any steam gauges in the Phoenix and I'll manage the risk. But I'd sure like to hear how the visionaries propose to manage the risk for their ab initio OZ/SATS pilots. If anyone has seen such a discussion please pass it along. Regards, Greg Young - Houston (DWH) RV-6 N6GY ...project Phoenix Navion N5221K - just an XXL RV-6A > In essence, they found that using the Oz symbols, > inexperienced pilots were much more capable of controlling > the airplane (actually, flight simulator) under varying > conditions of turbulence and distraction (reading text) than > they were with conventional instrumentation. > ________________________________________________________________________________
Date: Aug 26, 2004
From: SportAV8R(at)aol.com
Subject: Re: Looking for an RV'er with mode s
>>Looking for real world RV experience with this mode S stuff. Prices are down to almost reasonableness now and I am wanting to pull the trigger. << Here's a related plea: someone tell me who makes a serial-altitude-data transponder that would be compatible with the Dynon "new model." Google is not proving much help... I want to pull some triggers of my own on a glass panel overhaul, but ditching my almost new Garmin GTX-320 xpdr isn't appealing; I'm even thinking of going over to the dark side and looking at BMA, Grand Rapids, & so forth. -Bill B ________________________________________________________________________________
Date: Aug 26, 2004
From: Mickey Coggins <mick-matronics(at)rv8.ch>
Subject: Re: Looking for an RV'er with mode s
Hi, I'm not flying with a mode s, but I wonder why you want to spend more money so "big brother" can track you? Rhetorical question, BTW. If you want to get the truth of mode s, this is a good place to start: http://www.collisionavoidance.org/ Mickey >... >Prices are down to almost reasonableness now and I am wanting to pull >the trigger. Someone please push me over the edge so's I have a good >excuse and can hold you accountable later:-) -- Mickey Coggins http://www.rv8.ch/ #82007 QB Wings/Fuselage ________________________________________________________________________________
Date: Aug 26, 2004
From: "Ken Simmons" <ken(at)truckstop.com>
Subject: Re: Looking for an RV'er with mode s
The GTX 327 is one. That's what I have and plan on using. They're not bad on the used market. That's how I got mine. This is the transponder Doug Medema at Dynon is using so he made sure this one was compatible. Ken ---------- Original Message ---------------------------------- From: SportAV8R(at)aol.com Date: Thu, 26 Aug 2004 14:39:20 -0400 > >>>Looking for real world RV experience with this mode S stuff. > >Prices are down to almost reasonableness now and I am wanting to pull >the trigger. << > >Here's a related plea: someone tell me who makes a serial-altitude-data transponder that would be compatible with the Dynon "new model." Google is not proving much help... I want to pull some triggers of my own on a glass panel overhaul, but ditching my almost new Garmin GTX-320 xpdr isn't appealing; I'm even thinking of going over to the dark side and looking at BMA, Grand Rapids, & so forth. > >-Bill B > ________________________________________________________________________________
Date: Aug 26, 2004
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Looking for an RV'er with mode s
SportAV8R(at)aol.com wrote: > Here's a related plea: someone tell me who makes a > serial-altitude-data transponder that would be compatible with the > Dynon "new model." Google is not proving much help... I want to pull > some triggers of my own on a glass panel overhaul, but ditching my > almost new Garmin GTX-320 xpdr isn't appealing; I'm even thinking of > going over to the dark side and looking at BMA, Grand Rapids, & so > forth. Couldn't you just buy an altitude encoder for your existing xsponder? Sam Buchanan ________________________________________________________________________________
From: "RV_8 Pilot" <rv_8pilot(at)hotmail.com>
Subject: Firewall color
Date: Aug 26, 2004
I've never painted a firewall but we've painted stainless piping and vessels regularly here in the petrochem plants. why paint a perfect good, new piece of SS piping or vessel? It keeps the atmospheric contaminants from causing external environmental and chloride stress corrosion cracking. Also, you might (just guessing here) be able to offset some of the loss of reflectivity by adding bulk/thickness to the layer of paint being applied in order to provide some degree of thermal insulation. For example, apply generous amount of primer then a couple of build or top coats. Might even help a little with noise. I'm shooting from the hip on this one. Don't forget - it'll also add weight and probably (!) be more flammable than polished stainless steel. Bryan ________________________________________________________________________________
From: "Randy Lervold" <randy(at)romeolima.com>
Subject: Re: Firewall color
Date: Aug 26, 2004
> Just want to make sure..........................paint WILL stick to > stainless?? Dana, I painted the BACK of my firewall with Concept, after thoroughly Scotchbriting it, and it stuck just fine for 368 hrs. Randy Lervold ________________________________________________________________________________
From: owner-rv-list-server(at)matronics.com
Subject: RE: more Rocket/Super 8 comments
Date: Aug 26, 2004
Tromping on? I surely did not see it that way. I put my thoughts out there for all to see, and debate. It is quite fun if you ask me. Ego's get left at the door. This is serious business and lightweights should stay home. I expect the S8 to weigh in at 60lbs heavier than my 6A does. How am I gonna do that? Well the current S8's weigh in at 1250 empty. That is 60lbs over my heavy 6A which is loaded to the gills with stuff that I love. And these 1250lbs numbers are on the std gear. I have the Grove gear (sitting idlely waiting on the fuse to arrive next week) shaving 18lbs. I hope to not eat up all that savings with the increase weight of smoke system, big tanks, and the ever tantalizing glass cockpit, but I might. IF I get in at <=1250 Ill be one happy happy camper. That is the power to weight Im after. And thanks to all that have chimed in on the S8 issue. One of the best threads I have seen in quite some time. Bring it on. Keep it coming. Mike Stewart S8 mounting tips. -----Original Message----- From: Frazier, Vincent A [mailto:VFrazier(at)usi.edu] Subject: more Rocket/Super 8 comments He he he.... I have to laugh because the Rocket list never gets this much action on any topic. LOL Also Michael Stewart has been a real gentleman throughout this thread. We had emailed back and forth several times yesterday before my pea-brain made the connection that it was his website comments that I was tromping on! Some guys aren't so gracious and I take my hat off to Michael for putting up with our well intended barbs. I would not have any qualms about the Super 8s (or Super 6s either)if some simple strengthening mods were done. It would be very easy to copy what John Harmon has done on the Rocket and apply that to the RV airframe. Most of the mods would involve a relatively simple increase in skin thickness. Adding length to the tail would get a bit more involved but is still reasonably straightforward. For anyone who doesn't know what John Harmon did to Rocketize an RV-4, here's a brief overview: the wings are shortened about 7" per side and the rib spacing is decreased, the tail is lengthened about 7" with 4" of that length added between the seats, several skins in the forward fuselage are thickened, a different cowl, motor mount, canopy, and several widened bulkheads are needed due to widening of the fuselage. (Obviously the 8 wouldn't need to be widened.) And, of course, a big IO-540-C4B5 motor and HUGE Hartzell prop are installed...don't kid yourself here... this is why it's a 1200# Rocket and not a 950# RV-4 anymore. Please do the math for yourself.... 250# difference and most of it is on the nose! The gear geometry on the Rockets is changed to accommodate the weight on the nose, with the Harmons tending to be more nose heavy on the ground. The F-1 wheels are slightly farther forward to put more weight on the tail. I'd be leary of simply leaving the RV-8 gear "as is" while adding all of that weight up front. But I have no knowledge of the Super 8s ground manners. Perhaps Bob J. will chime in again. I've had the opportunity to ride in 3 different Harmons. The gear never misbehaved whatsoever. Bob Japundza had a very good description of the titanium gear yesterday. (I hate to say it in public, but I have a high regard for Bob's opinions. He usually has it right.) Incidentally, the titatium gear legs are without a doubt, the single most expensive part of the entire airframe. I think I paid $850 apiece!!! If money makes it good, these gear legs must be awesome! ;-) There was discussion of cost also. My half breed Harmon/F1 Rocket has a 0-time Lyc and brand new prop, fully painted and upholstered, Grand Rapids EFIS based panel with brand new avionics, etc, etc,... ALL new everything, and I have all of the receipts to prove that I've not popped the $50,000 barrier yet. I have taken exactly 5 years of spare time to build it. So, IMHO, a Super 8 with the Rocket mods listed above, and a Rocket gear instead of the gear towers crowding your thighs would be "da bomb". There's even a turtledeck mod for the RV-8 that a local RV-8 builder (and others) have done. Looks nice. Regards, Vince Frazier F-1H Rocket, N540VF http://www.usi.edu/science/chemistry/vfrazier/page1.html ________________________________________________________________________________
Subject: Was Mode S, now Dynon serial output.
Date: Aug 26, 2004
From: "Stewart, Michael (ISS Atlanta)" <mstewart(at)iss.net>
That is exactly what they(Dynon) recommend. From their website: Altitude Encoder Output The new EFIS-D10A outputs altitude encoder data via serial communications using an ASCII formatted message. The change from parallel gray code used by the EFIS-D10 model was to free up connection pins for other features and be compatible with newer transponders coming out on the market. Dynon does not have a listing of serial equipped/compatible transponders available in the market. You'll need to purchase an altitude encoder if the transponder you currently own or are considering only accepts a parallel input. There are no serial to parallel converters that we know about. The new EFIS-D10A provides a setup menu that allows you to select from one of 4 possible protocols and an altimeter resolution of either 10 or 100 feet. The combination of these two selections should make the EFIS-D10A compatible with most serial input capable transponders. Protocol 1 Used By Garmin AT (formerly UPS Aviation Technologies) Baud rate 1200 Format #AL, space, +/-sign, five altitude bytes, the letter "T" and the number "25", two checksum bytes, and a carriage return Example message # AL +05200T+25D7[CR] Protocol 2 Used By Magellan Baud rate 1200 Format $MGL, +/- sign, five altitude digits, T+25, checksum, carriage return Example message $MGL+05200T+25D7[CR] Protocol 3 Used By Northstar, Garmin Baud rate 2400 Format ALT, space, five altitude bytes, carriage return Example message ALT 05200[CR] Protocol 4 Used By Trimble, Garmin Baud rate 9600 Format ALT, space, five altitude bytes, carriage return Example message ALT 05200[CR] When purchasing a new transponder or looking to see if your existing unit is compatible, please check with your owners manual, manufacturer's representative or local avionics shop - please do not call Dynon. Mike -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Sam Buchanan Subject: Re: RV-List: Looking for an RV'er with mode s SportAV8R(at)aol.com wrote: > Here's a related plea: someone tell me who makes a > serial-altitude-data transponder that would be compatible with the > Dynon "new model." Google is not proving much help... I want to pull > some triggers of my own on a glass panel overhaul, but ditching my > almost new Garmin GTX-320 xpdr isn't appealing; I'm even thinking of > going over to the dark side and looking at BMA, Grand Rapids, & so > forth. Couldn't you just buy an altitude encoder for your existing xsponder? Sam Buchanan = = = = ________________________________________________________________________________
From: "John" <n1cxo320(at)salidaco.com>
Subject: What's a fair price?
Date: Aug 26, 2004
I am replacing my Orndorff RV6A seat cushions and seat backs with Oregon Aero units. A friend offered to buy the Orndorff seats, but I am not settled on what a fair price would be. I only paid $300 for them 9 years ago, and they are in like-new condition. I see Orndorff now gets $600 for them...same units. What you consider a fair price...I don't want to take advantage of a friend, nor do I want to "give" them away. John ________________________________________________________________________________
From: "Greg Young" <gyoung@cs-sol.com>
Subject: Was Mode S, now Dynon serial output.
Date: Aug 26, 2004
The Garmin/UPSAT SL-70 takes both serial and gray code inputs. Has serial output too which goes to my GX-60. I still mourn the buyout:-( Greg > > Yup, been there, read that... not exactly helpful! It's been > a pain trying to research the input compatibility of various > transponders online. No mention in Garmin's web pages about > the input of the GTX series, but I know from the install > manual that my GTX 320 is parallel only. I was just hoping > for a research shortcut, since Dynon says not to bother them > with this inquiry. > ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: GA Scare Piece
Date: Aug 26, 2004
There is a very scary trend occuring that seems to be gaining momentum - namely attacks like this on General Aviation. To wit: Aviation Week has an article on the DC area ADIZ and the wonderful job the Customs and Immigration people are doing keeping all the nasty little planes from being a threat to our sacred national capital. Included was the gem that these security folks want a 60 mile radius (its now 30) permanent ADIZ in DC where they require folks wanting to fly into it to land at "gateway" airports for search and clearance before being allowed to fly into the ADIZ. Also, TSA Inspectors would be located at all of these airports and the users would pay a fee to support this force. WTOP radio, a Washington DC area all news radio station has a terrorism expert on this morning talking about the grave threat of attack via GA....to their credit WTOP is inviting him back to ask him some questions tommorow after being besieged commetns debunking his analysis from local aviators and will have AOPA on as well for a counter view. The Boston Globe thing.... This is scary because the tactics remind me of those who oppose guns. No matter where you are on the gun issue you have to admit that the opposition to guns uses a tactic that, at times, seems to want to make the gun owners the problem and that if we just eliminated them the problem would go away. Luckily for gun owners they have the NRA to fight for them and they are a much larger segment of the populace. Not taking a side in that issue here just pointing out the similarities to the issue we face. Do not think it does not effect you because you are not in DC because if they suceed in getting these sort of draconian measures in place here in the name of security how long do you think it will be before the Senator Schumer's and the Mayor Daley's of the world start clamoring for the same level of protection for their cities. If you think they (these security types) will never get what they want consider this: In DC they recently closed streets around the Capitol Building and set up checkpoints (like Nazi Germany!) based on some intelligence they got that AL Queda was planning on blowing up buildings in DC. After the fact they admited the intelligence was vague and there was no specific information. The relevent point is they did it in the middle of the night and didnt inform a single elected official (not the Mayor or the Speaker of the House, no one) they were going to do it. City officails are livid and have been calling for them to open back the streets as it plays havoc with local traffic to no avail. When the time comes they will make the same kind of airspace grab and nothing will be done about it. BTW - the streets are stilled closed..... I am not some sort of right wing or left wing nut but this scares the hell out of me. If we continue this way we are letting the damn terrorists win by default. Sorr this is not directly RV related but it effects your right to fly in a very real way. Write your Congressman and send money to AOPA - they are the only ones fighting for us... ________________________________________________________________________________
Date: Aug 26, 2004
From: Skylor Piper <skylor4(at)yahoo.com>
Subject: Re: GA Scare Piece
ALL of us as Aviators need to stand up for our rights. The reason that vans haven't become targets after multiple world trade center attack attempts and Oklahoma City is because the pure number of people that rely on vans is huge, especially compared to the size of the GA population. On the other hand, GA is a relatively easy target for the media and public, because the number of people affected is only a tiny percentage of the population. That is why it is important for Aviators to be very vocal (but not obnoxious or unreasonable) about supporting our rights and educating the general public. In a addition, it's important to support our most influential advocacy group, AOPA! Skylor --- Richard Bibb wrote: > > > There is a very scary trend occuring that seems to > be gaining momentum - > namely attacks like this on General Aviation. > _______________________________ ________________________________________________________________________________
From: "BRUCE GRAY" <brucerv84us(at)hotmail.com>
Subject: What's a fair price?
Date: Aug 26, 2004
Fair would be sell them for the same price you payed. Consider you using the seat's for 9 year's for free. >From: "John" <n1cxo320(at)salidaco.com> >Reply-To: rv-list(at)matronics.com >To: >Subject: RV-List: What's a fair price? >From: contains numbers mixed in with letters > > >I am replacing my Orndorff RV6A seat cushions and seat backs with Oregon >Aero units. A friend offered to buy the Orndorff seats, but I am not >settled >on what a fair price would be. I only paid $300 for them 9 years ago, and >they are in like-new condition. I see Orndorff now gets $600 for >them...same >units. > >What you consider a fair price...I don't want to take advantage of a >friend, >nor do I want to "give" them away. > >John > > http://search.msn.click-url.com/go/onm00200636ave/direct/01/ ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: GA Scare Piece
Date: Aug 26, 2004
> Come on. It's the Boston Globe. Fit for fish wrap and hampster cage lining. > The problemis it gets picked up and repeated over and over. The WTOP radio piece was because they read the Globe thing, saw a good (as in sensational) item to report on, called the "expert" and he was more than willing to fill the drive time airways around the nations capital with this drivel letting literally several million commuters hear this crap and be scared about little planes. You know its crap, I know its crap, but some innocent out there is now thinking they better ban those little planes from coming anywhere near a stadium lest 90,000 God fearing NFL fans be put at risk. Unfortunately the logical argument against this sort of thing gets lost in the shuffle, sort of like the correction to the story where you are accused of beating your wife gets put on page 24 in fine print. The "damage" has already been done. I'm not try9ing to be alarmist but to approriate those immortal words for a new application - "Houston, we ahve a problem..." ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: What's a fair price?
Date: Aug 26, 2004
Hmm - what a willing buyer and a willing seller agree it to be. I'd ask him to make an offer and if it seems oK take it - if not counter. Sounds like the american, well not exactly american as its practiced in every corner of the globe, way. ________________________________________________________________________________
From: plaurence@the-beach.net
Date: Aug 26, 2004
Subject: Re: GA Scare Piece
Come ya'all. nough of this useless bandwidth. Let's all keep the subject about building airplanes. And if you insist, at least don't take up Matt's drive space . DO NOT ARCHIVE! Peter Laurence On 26 Aug 2004 at 19:11, Richard Bibb wrote: > > > > Come on. It's the Boston Globe. Fit for fish wrap and hampster > > cage > lining. > > > The problemis it gets picked up and repeated over and over. The WTOP > radio > piece was because they read the Globe thing, saw a good (as in > sensational) item to report on, called the "expert" and he was more > than willing to fill the drive time airways around the nations capital > with this drivel letting literally several million commuters hear this > crap and be scared about little planes. You know its crap, I know its > crap, but some innocent out there is now thinking they better ban > those little planes from coming anywhere near a stadium lest 90,000 > God fearing NFL fans be put at risk. Unfortunately the logical > argument against this sort of thing gets lost in the shuffle, sort of > like the correction to the story where you are accused of beating your > wife gets put on page 24 in fine print. The "damage" has already been > done. > > I'm not try9ing to be alarmist but to approriate those immortal words > for a new application - "Houston, we ahve a problem..." > > > advertising on the Matronics Forums. > http://www.matronics.com/chat > === > > > > ________________________________________________________________________________
From: "Jim Cimino" <jcimino(at)echoes.net>
Subject: Lyle Hefel
Date: Aug 26, 2004
Does anyone know how to get in touch with Lyle Hefel? A good friend of mine is interested in buying an -8 and heard he might be willing to sell his. He called Lyle's phone number and left a few messages for him, but has not heard back. If anyone can help, I would sure appreciate it. James Cimino RV-8 SN 80039 100+ Hours 570-842-4057 http://www.geocities.com/jcimino.geo/ ________________________________________________________________________________
From: plaurence@the-beach.net
Date: Aug 26, 2004
Subject: Cad 3 view
Can anyone point me to a cad 3 view drawing of a RV9A? Thanks peter ________________________________________________________________________________
From: Elrod3794(at)aol.com
Date: Aug 26, 2004
Subject: Re: Temporary hangar space in Birmingham
Doug I have space in my hanger at Bessemer (eky)call me. mike at 205 3691103 or Bob at 205 5414103 m. elrod ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: Lyle Hefel
Date: Aug 26, 2004
Lyle is building a new house and is quite busy. You might try rvbuilder(at)dubuque.net Cy Galley Safety Programs Editor Always looking for ideas and articles for EAA Sport Pilot ----- Original Message ----- From: "Jim Cimino" <jcimino(at)echoes.net> Subject: RV-List: Lyle Hefel > > Does anyone know how to get in touch with Lyle Hefel? A good friend of mine is interested in buying an -8 and heard he might be willing to sell his. He called Lyle's phone number and left a few messages for him, but has not heard back. If anyone can help, I would sure appreciate it. > James Cimino > RV-8 SN 80039 > 100+ Hours > 570-842-4057 > http://www.geocities.com/jcimino.geo/ > > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Aug 26, 2004
Subject: Re: GA Scare Piece
In a message dated 8/26/2004 3:23:40 PM Pacific Daylight Time, RV8ter(at)aol.com writes: Folks that read that pathetic excuse of a news paper have long since given up their common sense and that rag merely reflects their liberal stupidity. ==================================== Unfortunately the liberals have no monopoly on stupidity. Just choose your subject matter (religion, sex, violence, guns,energy, immigration, drugs, corporate finance, etc.) and there is certainly stupidity aplenty across the board. GV (RV-6A N1GV O-360-A1A C/S, flying 710 hrs) ________________________________________________________________________________
From: BrooksRV6(at)webtv.net (Chris Brooks)
Date: Aug 26, 2004
Subject: First Flight
After 10+ years of construction RV-6 Ser. 22935 N164CB flew from MQY in Smyrna TN today. It may not look like much, but at least it doesn't fly too bad. Both wings are heavy, and you have to hold right rudder going up and left rudder coming down :-) The planes not bent, and my pants are still dry so I consider the flight a success. Chris Brooks DNA ________________________________________________________________________________
Date: Aug 27, 2004
Subject: RV-7A Tipup Install suggestion
From: Sebastian Trost <sebastian.trost(at)sbcglobal.net>
Been a lurker and massive user of Dan Checkoway and Walter Tondu's web sites and this forum to speed my progress, but I think I have a good suggestion for aligning the tipup canopy frame I haven't read before. I used Dan's notes on interference to trim the alum spacers to allow the frame to move forward. I had a really hard time getting the skin to sit flat and flush to the subpanel flange. I couldn't get the duct tape to hold well enough to keep the skin in place. I decided to use tape for the top center portion of the skin. Then I put a ratcheting tiedown strap around the entire fuselage along the forward part of the canopy frame skin. After snugging it down, I was able to make some final adjustments to the skin to get it evenly aligned relative to the forward top skin. The strap kept the skin flush to the flanges and also kept the alignment in place. I was able to drill the splice plate and hinge flange with no problem with this setup. I hope this idea helps someone else. I have certainly saved a lot of time with the Matronics forum. Many thanks to all! Sebastian Trost RV-7A Tipup QB Working on Canopy Cameron Airpark, CA (O61) ________________________________________________________________________________
From: "Ronnie Brown" <romott(at)adelphia.net>
Subject: GA Scare Piece
Date: Aug 27, 2004
I urge all of us to respond to this threat against our GA freedoms by the sensationalist media. This tripe will lead to more TFR's, restricted areas, security at our small airports (have you noticed the miles of fences being put up around the mid size airports?????). Eventually we will lose the freedom to fly our airplanes anywhere. http://www.boston.com/news/nation/articles/2004/08/26/analysts_warn_of_small_plane_terrorism_threat/ Take a few minutes and let the editor (unfortunately, Karen Schaler, the writer doesn't have the guts to list her email address) know what you think of this piece of journalism. letter(at)globe.com ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: First Flight
Date: Aug 27, 2004
Chris, CONGRATULATIONS and WELL DONE !! Chuck & Dave Rowbotham RV-8A >From: BrooksRV6(at)webtv.net (Chris Brooks) >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: First Flight >Date: Thu, 26 Aug 2004 22:58:21 -0500 > > >After 10+ years of construction RV-6 Ser. 22935 N164CB flew from MQY in >Smyrna TN today. It may not look like much, but at least it doesn't fly >too bad. Both wings are heavy, and you have to hold right rudder going >up and left rudder coming down :-) The planes not bent, and my pants are >still dry so I consider the flight a success. >Chris Brooks Get ready for school! Find articles, homework help and more in the Back to ________________________________________________________________________________
Date: Aug 27, 2004
From: Hal / Carol Kempthorne <kempthornes(at)earthlink.net>
Subject: GA Scare Piece
At 06:29 AM 8/27/2004, you wrote: > >Take a few minutes and let the editor (unfortunately, Karen Schaler, the >writer doesn't have the guts to list her email address) know what you >think of this piece of journalism. I read the piece. Wasn't Karen just reporting on what some commission said? I didn't see anything like editorializing on her part. What will we say to her? Should we damn her for reporting something we didn't want to hear? Would it matter if we found out she is a very religious pilot with a BUSH button? Let's get some facts. hal ________________________________________________________________________________
Date: Aug 27, 2004
From: Rick Galati <rick6a(at)yahoo.com>
Subject: Re: Nationair insurance news
For something over 4 years of building now, I have been virtually "self insured" all along including the potentially risky move to the airport. Very recently, I installed a Garmin stack (thank you, John Stark) which in one fell swoop dramatically increased the total investment in my unfinished RV-6A. After insistent prodding (nagging) from my wife, I finally called the AOPA inquiring about "builders insurance." Hard to believe, but after the initial telephone inquiry, it took the AOPA more than 2 weeks to get back with the news that such coverage was unfamiliar and not available through their good offices. Upon the recommendation of a fellow RV builder, I called Nationair which happens to be located right here (I had no idea) in River City and immediately secured 80K in non-motion Vanguard coverage for $413. Recently hired Aaron Wedge handled the whole thing. Relatively small premium, considerable coverage, and some welcomed peace of mind, especially considering all t he late afternoon thunderstorms we've had around here lately. Rick Galati RV-6A "finishing" N307R (reserved) "Darla" ________________________________________________________________________________
From: "Darwin Barrie" <ktlkrn(at)cox.net>
Subject: Re: Looking for an RV'er with mode s
Date: Aug 27, 2004
Oh, give me a break about the "big brother" paranoia. I am putting in a 330 for the collision avoidance so I can live to see another fly-in. I live in a very congested area and the safety benefits far out weigh the costs. I have nothing to hide so I don't care if they track me or not. Secondly, how long until they are mandatory? If you don't live in a congested area don't even consider it. GOTTA GO, there's a black helicopter landing out back. Oh no, black Suburbans with guys in suits!!!! Darwin N. Barrie Chandler AZ ________________________________________________________________________________
Subject: Mode S response
Date: Aug 27, 2004
From: "Stewart, Michael (ISS Atlanta)" <mstewart(at)iss.net>
Well believe it or not, I actually did get a response from an RV guy who actually has a flying airplane(RV), and mode S. I thought the list might find it interesting. Since he did not reply to the lis, I have kept him anonymous. Yep got that GNS430 and the GTX330 and I think its the best $2000 I spent since that hooker in Vegas. We can go up for a demo at GEZ, I'm planning on being there tomorrow. The 330 is really great for crowded airspace (your around ATL right?) and during formation it provides real peace of mind for protection. While the mode S can transmit N # it doesn't have to...my has never beeen program to do that. Its a better system then the airlines TCAS because you also get a vector line of traffic movement. Course when you don't want to be tracked, there is always the stby button. I cant think of a good reason during normal flight why I would not want to have this in my airplane. Now when I have my hotdog hat on, that's what the power switch is for I guess. I am as fearful of big brother as the next guy believe me (well maybe not as bad as some of you), but for my every days runnings around under my busy class B, and the handful of hours I fly cross country, this sure seems like cheap tcas to me. Regards Michael Stewart ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: GA Scare Piece
Date: Aug 27, 2004
The sin in this case was not presenting both sides of the argument and taking the yet incomplete report out of context. Journalists have a responsibility to get the facts straight before scaring the hell out of everybody. See: http://www.aopa.org/whatsnew/newsitems/2004/040827security.html for the rest of the story.... > I read the piece. Wasn't Karen just reporting on what some commission > said? I didn't see anything like editorializing on her part. What will we > say to her? Should we damn her for reporting something we didn't want to hear? > > Would it matter if we found out she is a very religious pilot with a BUSH > button? Let's get some facts. > > hal > ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: Nationair insurance news
Date: Aug 27, 2004
Not unless you got a rider on the policy..... ----- Original Message ----- From: <dfiggins(at)es.com> Subject: RE: RV-List: Re: Nationair insurance news > > As long as I am building in my garage I assume I am covered by my > homeowners policy, is this a valid assumption? > > Dave Figgins RV-7A empennage ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: Aug 27, 2004
Subject: Re: Nationair insurance news
In a message dated 8/27/04 1:01:15 PM Central Daylight Time, dfiggins(at)es.com writes: > As long as I am building in my garage I assume I am covered by my > homeowners policy, is this a valid assumption? Not from most homeowners policies. Call Aaron Wedge @ 877-475-5860 for VERY reasonable rates & great service- "builders" policy upgraded to "flying" in January '04! (I too was dissapointed our RV-list resident agent wouldn't be handling my policy, but that's the price you pay for success!) No commision, just a happy Nation Air customer........... Mark Phillips -6A ________________________________________________________________________________
From: "Cory Emberson" <bootless(at)earthlink.net>
Subject: Re: Nationair insurance news
Date: Aug 27, 2004
Dave, Unfortunately, it's not a valid assumption. Builders coverage varies from one company/underwriter to another. And it can be complex. For instance, with Rotorway's agent of choice (Willis Caroon in Texas), they offer coverage for physical damage during construction, and third-party liability insurance one it's flying. But if someone watches you build and cracks their head on part of the project, your insurance won't coverage them. Generally, homeowner's insurance won't cover the project even if you're building it in your garage. How did I find all this out? The upcoming Kitplanes magazine (October) has an article I wrote about insuring homebuilts. I had to admit that the subject of insurance generally makes my eyes glaze over, but the people who provided information, including JT Helms (thank you!) made it interesting and understandable. thanks, Cory > > As long as I am building in my garage I assume I am covered by my > homeowners policy, is this a valid assumption? > > Dave Figgins RV-7A empennage ________________________________________________________________________________
Date: Aug 27, 2004
From: "Rob Prior" <rv7(at)b4.ca>
Subject: Re: Nationair insurance news
On 10:59 27/08/2004 wrote: > As long as I am building in my garage I assume I am covered by my > homeowners policy, is this a valid assumption? As you'll hear about any insurance question that starts with "am I covered...", the answer is "it depends". Some builders have discussed their projects with their insurers and found them to be quite amenable to insuring it. In some cases additional coverage was added to cover the increased equity in the tools or in the kit materials. Others found that their existing coverage was adequate for their tools, and that the kit parts were covered under "contents." Other builders were told flat out that their complete homeowner's policy was null and void the day they mentioned they were building an aircraft in the basement. I still don't know what those people did to work out their insurance. If you don't tell your insurer that you're building, you run the risk of being denied coverage in the event of the claim for not providing full disclosure. If you do tell them, you run the risk of having coverage denied up front because you are building. So unless you can self-insure (as some do), you're better off discussing the situation up-front with your insurer and making sure you're covered. If you're concerned about having your coverage pulled if you bring up the topic, shop around first and find one or two insurers who *will* cover you while you're building. Then you're in a much stronger bargaining position with your current insurer if they try to pull your coverage. And you have a place to go if it doesn't work out. -Rob (currently building under normal homeowner's coverage only) ________________________________________________________________________________
Subject: Re: Nationair insurance news
Date: Aug 27, 2004
From: <dfiggins(at)es.com>
Interesting set of comments, obviously my assumption is invalid but I fail to see the difference between building a plane in the garage from building a hot-rod or dragster or boat etc in the garage with respect to the comment about "invalidating" the entire home owners policy. At this point the major investment is in tools which I think would be covered but I guess I need to make some calls. Thanks Dave -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Rob Prior Subject: RE: RV-List: Re: Nationair insurance news On 10:59 27/08/2004 wrote: > As long as I am building in my garage I assume I am covered by my > homeowners policy, is this a valid assumption? As you'll hear about any insurance question that starts with "am I covered...", the answer is "it depends". Some builders have discussed their projects with their insurers and found them to be quite amenable to insuring it. In some cases additional coverage was added to cover the increased equity in the tools or in the kit materials. Others found that their existing coverage was adequate for their tools, and that the kit parts were covered under "contents." Other builders were told flat out that their complete homeowner's policy was null and void the day they mentioned they were building an aircraft in the basement. I still don't know what those people did to work out their insurance. If you don't tell your insurer that you're building, you run the risk of being denied coverage in the event of the claim for not providing full disclosure. If you do tell them, you run the risk of having coverage denied up front because you are building. So unless you can self-insure (as some do), you're better off discussing the situation up-front with your insurer and making sure you're covered. If you're concerned about having your coverage pulled if you bring up the topic, shop around first and find one or two insurers who *will* cover you while you're building. Then you're in a much stronger bargaining position with your current insurer if they try to pull your coverage. And you have a place to go if it doesn't work out. -Rob (currently building under normal homeowner's coverage only) = direct advertising on the Matronics Forums. = = = ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: Nationair insurance news
Date: Aug 27, 2004
Think of it as a fur coat. Such items are not covered either unless you add them specifically to the policy. It will not invalidate your policy if you dont but if your house burns to the ground they won't pay for the plane.... ----- Original Message ----- From: <dfiggins(at)es.com> Subject: RE: RV-List: Re: Nationair insurance news > > Interesting set of comments, obviously my assumption is invalid but I > fail to see the difference between building a plane in the garage from > building a hot-rod or dragster or boat etc in the garage with respect to > the comment about "invalidating" the entire home owners policy. At this > point the major investment is in tools which I think would be covered > but I guess I need to make some calls. > Thanks > > Dave > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Rob Prior > To: rv-list(at)matronics.com > Subject: RE: RV-List: Re: Nationair insurance news > > > On 10:59 27/08/2004 wrote: > > As long as I am building in my garage I assume I am covered by my > > homeowners policy, is this a valid assumption? > > As you'll hear about any insurance question that starts with "am I > covered...", the answer is "it depends". > > Some builders have discussed their projects with their insurers and > found them to be quite amenable to insuring it. In some cases > additional coverage was added to cover the increased equity in the tools > or in the kit materials. Others found that their existing coverage was > adequate for their tools, and that the kit parts were covered under > "contents." > > Other builders were told flat out that their complete homeowner's policy > was null and void the day they mentioned they were building an aircraft > in the basement. I still don't know what those people did to work out > their insurance. > > If you don't tell your insurer that you're building, you run the risk of > being denied coverage in the event of the claim for not providing full > disclosure. If you do tell them, you run the risk of having coverage > denied up front because you are building. So unless you can self-insure > (as some do), you're better off discussing the situation up-front with > your insurer and making sure you're covered. > > If you're concerned about having your coverage pulled if you bring up > the topic, shop around first and find one or two insurers who *will* > cover you while you're building. Then you're in a much stronger > bargaining position with your current insurer if they try to pull your > coverage. And you have a place to go if it doesn't work out. > > -Rob > (currently building under normal homeowner's coverage only) > > > = > direct advertising on the Matronics Forums. > = > = > = > > ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: new books and cheap old ones
Date: Aug 27, 2004
Here's a couple new items and some discounted old ones. Order these by return e-mail or phone at 800 780-4115. These are all first come first serve, so call or e-mail back by Monday if you want one. Thanks Andy Builder's Bookstore www.buildersbooks.com 800 780-4115 1] JEPPESEN INSTRUMENT TEXTBOOK Revision 6 of the big Jeppesen Instrument/Commercial Manual was just released today. The price is $84.49. However, we have about a dozen left of revision 5 which is less than a year old. (little has changed) On Monday afternoon we will return our old #5s to Jeppesen. So if you want to grab one before then, we'll discount the price to $60. (a $25 savings) 2] The FAA's AIRPLANE FLYING HANDBOOK Revised about a week ago and twice the size of the old one. This is everything the FAA thinks you ought to know about flying your airplane in easy to understand full color graphics. We got a special "new release" price on our opening order, so also till Monday, the RV list price for this book is $20, instead of the normal $29.95. 3] HOW TO PAINT AN AIRPLANE. By Ron Alexander. Finally an up to date and easy to understand book on painting a homebuilt (with a nice RV on the cover) It's produced by SportAir Workshops and EAA $19.95 ...and a couple of one left of bargain basement items Advanced Composites $15.00 (was $29.95) Physics for Aviation $10.00 (slightly damaged, was $22.00) Everything Explained for Pilots $25.00 (normally $59.95) an evaluation copy of something we're not going to carry Stress Without Tears $15.00 (normally $25.00) another evaluation copy of something we're not going to carry Introduction To Aircraft Maintenance $15.00 (normally $44.50) an "prototype" edition of a new A&P General Textbook Airplane PDQ software $25.00 (normally $99.95) the previous edition from 2002 FAR/AIM 2003 on CD $10.00 also includes current AC 43.13 Getting Started in Electronics $10.00 An evaluation copy of something we're not going to carry Simplified Aircraft Design For Homebuilders $20.00 an evaluation copy of a design book thats too expansive at $60, bot a good deal at $20 ________________________________________________________________________________
From: "S Hamer" <s.hamer(at)verizon.net>
Subject: Navaid Autopilot
Date: Aug 27, 2004
I have a new Navaid Autopilot I'm considering selling in order to upgrade to one of the newer models available from Trio or Digitrak. Mine has never been used though it has been installed. I have the external Smart Coupler which may or may not be of use to whoever may buy the unit. The prices haven't changed since I bought this one, they're $1300 the last I looked. The external Smart Coupler was around $200. If anyone wants it, make me an offer. If the offer is good enough it may entice me to spend the extra money to upgrade. Hey Gummo, if you buy it I'll deliver it for nothing on my next walk. Steve Hamer Apple Valley, Ca s.hamer(at)verizon.net (760)486-5950 ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Aug 28, 2004
Subject: Re: Nationair insurance news
In a message dated 8/27/04 11:01:12 AM Pacific Daylight Time, dfiggins(at)es.com writes: << As long as I am building in my garage I assume I am covered by my homeowners policy, is this a valid assumption? >> Not if your homeowners insurance is like any that I have ever had. Better check the fine print> Harry Crosby Pleasanton, California RV-6, final assembly ________________________________________________________________________________
From: "Bob 1" <rv3a(at)comcast.net>
Subject: Re: Nationair insurance news
Date: Aug 28, 2004
> So he hired someone to take care of that part of the program that he felt he > could off-load to a subordinate. > > So, I think it is simply a sign of success (a good thing!) and JT is still > there. > > I have spoken to BOTH JT and the person that handles my policies. JT was > just the same phone call away and the new (additional person ... sorry I > don't remember his name at the moment) was very helpful and responsive. > > > James ================================ AFAIK..... Aaron is a_replacement_for the fine gal that handled my policies before succumbing to cancer. Bob ________________________________________________________________________________
Date: Aug 28, 2004
From: Glenn Brasch <gbrasch(at)earthlink.net>
Subject: Vans Shipping a Crate to you in the Future?
VERY long story short. Van's current "discount" shipper, Bullet Freight just shipped a QB fuselage to me. They told Van's, who in turn told me, the had a terminal where I live, in Tucson. They do not, nor do they share an inter-line terminal with any other company here. Nor do they own a terminal in Phoenix, which they also say they do. At the last minute, I had to arrange a terminal, workers, fork lifts, and further delivery of the crate to my shop. Anne at Van's was great, she called the logistics company and had the extra money taken off the bill before I finished writing my letter of complaint. The moral is: pay very close attention to detail and ask a lot of question about your shipment before hand. After the fact, Anne confirmed Bullet Freight's brochure showed 3 terminals in Arizona, which don't exist. Glenn in Tucson, -9A about to start fuselage. ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Aug 28, 2004
Subject: Re: First Flight
In a message dated 8/28/2004 7:51:36 AM Pacific Daylight Time, shempdowling(at)earthlink.net writes: How can both wings be heavy? ================================================ If they're both built of lead? GV (RV-6A N1GV O-360-A1A C/S, flying 710 hrs) ________________________________________________________________________________
From: "Ernest Kells" <ernest.kells(at)sympatico.ca>
Subject: Production Status of the XCOM760
Date: Aug 28, 2004
I would like to have a status report from someone who has successfully installed and fully tested an XCOM760. Unit must truly be from "regular production" - - not a factory/lab or other prototype. I have been following this product for nearly a year. I know that they have had rollout problms with suppliers, etc. They haven't finalised the software update capability yet - although it is probably not an issue. I retired from the computer industry - I am used to the 100% completion rule. Thanks for any help. Ernest Kells - RV-9A O235-N2C, Wood Prop 95% Complete - Preparing for Paint ________________________________________________________________________________
From: "Randy Compton" <thecomptons(at)bellsouth.net>
Subject: RV-3 vs. RV-3A
Date: Aug 28, 2004
Listers: I'm familiar with the rear spar mod, CN-1, 1-4, for early 80's and older RV-3's, which when reworked allowed for the "A" designation. What I'm trying to find out is when/if this mod was incorporated into the RV-3 kit. In other words, was there a certain time after which all RV-3 kits sold had the fork-type rear spar and carry-through attach structure and no retro-work was needed? I've searched the archives and have found little help, although I did read a post about the "A" designation later being dropped. Is that because the kits being produced had the upgraded structure? Thanks. Randy Compton Gulf Breeze, FL ________________________________________________________________________________
From: "Amit Dagan" <amitdagan(at)hotmail.com>
Subject: The RV takes to the sky!!
Date: Aug 28, 2004
First album: http://checkoway.com/url/?s=43f9eb3f Second album: http://checkoway.com/url/?s=d23319d Enjoy!! ________________________________________________________________________________
From: BBreckenridge(at)att.net
Subject: Rozendaal/Oct.Kitplanes RV-4 & Corsair
Date: Aug 28, 2004
Doug; Thanks for a great article! The title caught my eye on the front cover so well, I don't have any clue what else is in the latest issue!! Bruce Breckenridge 40018 Slowwwwbuilddd ________________________________________________________________________________
Date: Aug 28, 2004
From: Tedd McHenry <tedd(at)vansairforce.org>
Subject: Re: RV-3 vs. RV-3A
> In other words, was there a certain time after which all RV-3 kits sold had > the fork-type rear spar and carry-through attach structure and no retro-work > was needed? Here are some quotes from Van's RVator that shed some light on the situation. "We have prepared modification kits which we are sending out to all RV-3 owners requesting it. Modification kits for Type II RV-3s have already been sent out. We are now in the process of designing a new spar for use on all future RV-3s, and for retro-fit on under construction RV-3s." [1996] "We are now working on redrawing the wing plans and getting the new spar into production." [1998] "RV-3B wing kits are being prepared for market and we will again be able to offer complete RV-3 kits. The new kits have a redesigned, simplified, and strengthened main spar and 30 gallon wing tanks." [1999] --- Tedd McHenry Surrey, BC, Canada ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Aug 28, 2004
Subject: Re:RV-3 vs. RV3A
Why not do the obvious and call Van's or email them ????????? Bob Olds RV-4 , N1191X A&P , EAA Tech. Counselor Charleston,Arkansas Real Aviators Fly Taildraggers ________________________________________________________________________________
From: "Heinrich Gerhardt" <hgerhardt(at)earthlink.net>
Subject: Re: RV-List homeowner's insurance
Date: Aug 28, 2004
My homeowner's policy (AAA Insurance) covers my airplane within my city-owned hangar! That is, only as long as the airplane is being constructed and is deemed unairworthy. Reason why is that until the time the airplane is flying, in their eyes it's just a collection of parts that are considered my personal property and that is covered no matter where it's stored. My city even stipulated that my insurance has to cover the "city council members and all the officers of the city" as part of the policy, so I got AAA to add that phrase to my homeowner's policy. ________________________________________________________________________________
From: "Richard Suffoletto" <rsuffoletto(at)hotmail.com>
Subject: Wire routing
Date: Aug 29, 2004
I wasn't able to find anything on this in the archives. I'm looking for suggestions on how to route the wiring from behind the panel through or behind the spare on a RV-7A. I'd like to keepthem out of view as best I can. I don't have a great number of wires, just antenna andlights and flaps... Any photo's or suggestions would be appreciated. Thanks Richard Check out Election 2004 for up-to-date election news, plus voter tools and more! ________________________________________________________________________________
From: "james frierson" <tn3639(at)hotmail.com>
Subject: Wire routing
Date: Aug 29, 2004
I used the center piece for the throttle and elevator trim and was able to hide all the wiring including the 1/4" pitot polyflow behind it. Scott RV6-A Slider N162RV Flying..... 17hrs >From: "Richard Suffoletto" <rsuffoletto(at)hotmail.com> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: Wire routing >Date: Sun, 29 Aug 2004 08:14:04 -0700 > > > > >I wasn't able to find anything on this in the archives. I'm looking for >suggestions on how to route the wiring from behind the panel through or >behind the spare on a RV-7A. I'd like to keepthem out of view as best I >can. I don't have a great number of wires, just antenna andlights and >flaps... Any photo's or suggestions would be appreciated. > > >Thanks > > >Richard > > > Check out Election 2004 for up-to-date election news, plus voter tools >and more! > > Get ready for school! Find articles, homework help and more in the Back to ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)new.rr.com>
Subject: Re: Wire routing
Date: Aug 29, 2004
Richard: You can route your wires through a conduit mounted on the firewall stiffener adjacent to the firewall recess with adel clamps and then under the center floor cover. At the Spar, drill another hole similar to the one that is predrilled for the trim cable to pass through, only do it in the other wing spar. I ran my conduit under the floor cover and then just through the hole in the spar. Keeps the wires bundled nicely. I will send you what pictures I have to you directly. Regards, Jeff Orear RV6A N782P (reserved) firewall forward Peshtigo, WI ----- Original Message ----- From: "Richard Suffoletto" <rsuffoletto(at)hotmail.com> Subject: RV-List: Wire routing > > > I wasn't able to find anything on this in the archives. I'm looking for suggestions on how to route the wiring from behind the panel through or behind the spare on a RV-7A. I'd like to keepthem out of view as best I can. I don't have a great number of wires, just antenna andlights and flaps... Any photo's or suggestions would be appreciated. > > > Thanks > > > Richard > > > Check out Election 2004 for up-to-date election news, plus voter tools and more! > > ________________________________________________________________________________
From: "Michel" <rv8ter(at)rogers.com>
Subject: RV-3 vs. RV-3A
Date: Aug 29, 2004
I purchased my RV 3 kit in 1979 and was confused with the extra ribs and angles that were different from what was required in the plans. When I inquired to Van's they said oh! Silly us we forgot to put the updated instruction for the extra ribs and angles that we included in the kit. Michel RV3 & RV8 -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Randy Compton Subject: RV-List: RV-3 vs. RV-3A Listers: I'm familiar with the rear spar mod, CN-1, 1-4, for early 80's and older RV-3's, which when reworked allowed for the "A" designation. What I'm trying to find out is when/if this mod was incorporated into the RV-3 kit. In other words, was there a certain time after which all RV-3 kits sold had the fork-type rear spar and carry-through attach structure and no retro-work was needed? I've searched the archives and have found little help, although I did read a post about the "A" designation later being dropped. Is that because the kits being produced had the upgraded structure? Thanks. Randy Compton Gulf Breeze, FL ________________________________________________________________________________
Date: Aug 27, 2004
rv7-list(at)matronics.com, rv10-list(at)matronics.com, rv8-list(at)matronics.com, rv3-list(at)matronics.com, rv4-list(at)matronics.com
From: Richard Scott <rscott(at)cascadeaccess.com>
Subject: Van's Homecoming-- Where to eat
1.70 SUSPICIOUS_RECIPS Similar addresses in recipient list Scrumptous breakfast both Saturday & Sunday will be served right at Van's--pancakes, eggs, ham, sausage, bacon, coffee & orange juice. And lunch on Saturday, burgers, corn on the cob. Served by EAA Chapter 902. Don't miss out! ________________________________________________________________________________
From: "ed " <ed_88(at)hotmail.com>
Subject: Liability when you sell an RV?
Date: Aug 30, 2004
From: "ed \240" <ed_88@hotmai... So one of the reasons they say that homebuilt planes are so much cheaper is that the builder is on the hook instead of vans for liability reasons. So I assume that means if you sell your plane, that anyone who ever touches it after you can sue you if they are in an accident? Has a homebuilder ever actually been sued in a situation like this? Any thoughts on how to protect yourself? I imagine having the buyer sign something saying he understands it is a homebuilt wouldn't help. If nothing else he could sell it to a 3rd party who never signed such paperwork. Given all the insurance related talk recently I was wondering if this is something that people are thinking about. --Eddie ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: Enjoying my RV6
Date: Aug 29, 2004
Today featured a clear blue sky and a northerly breeze. A little bumpy, but the fun of flying the RV6 overshadowed that. I base at Sundance Airpark in Oklahoma City and was heading back in and made a mid field cross-wind at 175mph to check the sock(ok, showing off).....oh what the heck...a low pass(more showing off) to wrap up a good day. Swing around into a left downwind for 35 and set up for a smooth descending left turn to final. We're looking good...a little head wind... but GPS indicating 204mph ground speed...pull up...yee haw! Not bad for 160hp fixed pitch metal prop! I park in front of the hanger and another RVer who was watching comes over grinning and says...Looks and sounds great in flight...do you have 200hp? Nope, 160hp. He says ....NO WAY! I grin and say, YES WAY. I am having fun! Jerry Calvert Edmond Ok N296JC RV6 ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Liability when you sell an RV?
Date: Aug 30, 2004
> So one of the reasons they say that homebuilt planes are so much >cheaper is that the builder is on the hook instead of vans for liability >reasons. So I assume that means if you sell your plane, that anyone who >ever >touches it after you can sue you if they are in an accident? Has a >homebuilder ever actually been sued in a situation like this? > > Any thoughts on how to protect yourself? I imagine having the buyer >sign >something saying he understands it is a homebuilt wouldn't help. If nothing >else he could sell it to a 3rd party who never signed such paperwork. > > Given all the insurance related talk recently I was wondering if >this >is something that people are thinking about. > > >--Eddie > Oh certainly. There are disclaimer forms, basically a hold harmless release that is commonly used. I think EAA has one and I have a copy stached away on my harddrive somewhere. It basically tries to completely separate the builder from any and all possible liability once the airplane changes hands. It's only a piece of paper though, and I'm sure it could be whittled away by a savvy shyster to next to nothing if pursued hard enough. I'll be dealing with this soon enough when I sell my RV8. Yikes. Brian Denk RV8 N94BD RV10 '51 tailcone/empennage rigging time. ________________________________________________________________________________
Date: Aug 29, 2004
From: Dave Bristol <bj034(at)lafn.org>
Subject: Re: Liability when you sell an RV?
on zoot.lafn.org Ed, A few years ago when my wife was selling her Mustang II, she contacted EAA on this subject and their answer was that there had never been a "successful suit" against a homebuilder. The lawyers are looking for "deep pockets" and homebuilders generally don't have them. If they squeezed me for every penny I have they wouldn't get enough to make it worth their time. Dave -6 So Cal EAA Technical Counselor ed wrote: > > > So one of the reasons they say that homebuilt planes are so much >cheaper is that the builder is on the hook instead of vans for liability >reasons. So I assume that means if you sell your plane, that anyone who ever >touches it after you can sue you if they are in an accident? Has a >homebuilder ever actually been sued in a situation like this? > > Any thoughts on how to protect yourself? I imagine having the buyer sign >something saying he understands it is a homebuilt wouldn't help. If nothing >else he could sell it to a 3rd party who never signed such paperwork. > > Given all the insurance related talk recently I was wondering if this >is something that people are thinking about. > > >--Eddie > > > > > ________________________________________________________________________________
Date: Aug 29, 2004
Subject: grass runway length for RV's?
From: czechsix(at)juno.com
Guys, For those of you with experience flying RV's off grass strips, what would you consider the minimum safe runway length? I know, it depends on a variety of factors, so in this case lets assume no obstacles at either end higher than 6' (i.e. a cornfield in August) and no higher terrain or obstacles beyond that, relatively level & smooth runway surface, operating at gross weight with 180hp / CS, on a hot/humid day (say 95 F) at 880' msl, with no headwind. Maybe throw in a bit of dew or post-rain moisture on the grass to reduce braking effectiveness, and this would be about the worst case scenario for me here in Iowa. Would 1700' be adequate under these conditions? I imagine takeoff would be a non-event, so landing and getting stopped without too much pucker factor would be my main concern.... Thanks, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D finishing.... ________________________________________________________________________________
Date: Aug 29, 2004
From: Scott Vanartsdalen <svanarts(at)yahoo.com>
Subject: Re: grass runway length for RV's?
Sounds like plenty to me. See how short you can land at your home airport. I bet it's less than 1700 feet. Guys, For those of you with experience flying RV's off grass strips, what would you consider the minimum safe runway length? I know, it depends on a variety of factors, so in this case lets assume no obstacles at either end higher than 6' (i.e. a cornfield in August) and no higher terrain or obstacles beyond that, relatively level & smooth runway surface, operating at gross weight with 180hp / CS, on a hot/humid day (say 95 F) at 880' msl, with no headwind. Maybe throw in a bit of dew or post-rain moisture on the grass to reduce braking effectiveness, and this would be about the worst case scenario for me here in Iowa. Would 1700' be adequate under these conditions? I imagine takeoff would be a non-event, so landing and getting stopped without too much pucker factor would be my main concern.... Thanks, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D finishing.... -- Scott VanArtsdalen RV-4 N311SV, FLYING!! When a man does all he can though it succeeds not well, blame not him that did it." -- George Washington ________________________________________________________________________________
From: "Jaye and Scott Jackson" <jayeandscott(at)telus.net>
Subject: Re: grass runway length for RV's?
Date: Aug 29, 2004
Years ago, I practiced spot landing with maximum effort stops on a grass runway prior to going into a one-way, 1700' strip with tall trees at one end and a fruit orchard on the approach end, plus it was uphill( a plus) with the wind above the trees occasionally a tailwind for departure( not a plus). The first time I actually landed on the strip I had been practicing for, in a 180 hp, fixed-pitch wooden prop RV-4, two-up( owner in the back), it sure looked short while we were on final, but the slope contributed to that appearance. We actually aimed for the treetops on the approach end as the lift of the wings will keep our flight path slightly above that, and practically drove the machine right onto the ground with only a slight flare to preclude a bounce.A wheel landing was used to eliminate float, followed by raising the tail to kill the lift while coming on the brakes moderately until an overrun was not in the cards, and we used less than half the runway. This was at sea level, on a summer day, which on the Pacific Coast means around 20C. Add a little lift from the extra bouyancy of both of us holding our breaths during the latter stages of teh approach and landing..... The departure was equally impressive due to the performance of these machines, and that's without a constant-speed prop. Taxi up against the tall trees, swing the tail almost into the trunks, full power, minimum-drag attitude for acceleration, hold it level after liftoff for a little extra airspeed when encountering that slight tailwind at the treetop level and there's plenty of room left. Which is a long way of saying that you should be fine within the parameters you describe. Walk off the distance on a longer runway, then perhaps practice to see how it feels and performs for you before committing yourself. SCott in VAncouver ----- Original Message ----- From: <czechsix(at)juno.com> Subject: RV-List: grass runway length for RV's? > > Guys, > > For those of you with experience flying RV's off grass strips, what would > you consider the minimum safe runway length? I know, it depends on a > variety of factors, so in this case lets assume no obstacles at either > end higher than 6' (i.e. a cornfield in August) and no higher terrain or > obstacles beyond that, relatively level & smooth runway surface, > operating at gross weight with 180hp / CS, on a hot/humid day (say 95 F) > at 880' msl, with no headwind. Maybe throw in a bit of dew or post-rain > moisture on the grass to reduce braking effectiveness, and this would be > about the worst case scenario for me here in Iowa. Would 1700' be > adequate under these conditions? I imagine takeoff would be a non-event, > so landing and getting stopped without too much pucker factor would be my > main concern.... > > Thanks, > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D finishing.... > > ________________________________________________________________________________
From: "Dave Mader" <davemader(at)bresnan.net>
Subject: new near vision procedure
Date: Aug 29, 2004
Guys, > After 10 years of keeping reading glasses by my easy chair, around my neck, in my pocket, & > losing on the average of one pair per week, I was excited to hear about this new procedure > for the improvement of near vision. The procedure is fairly new and was just approved by > the FDA in Feb. So excited, in fact, that I went to one of the few places in the country that > does the procedure and had a preliminary consult. Everything sounded good and I was > ready to proceed. > This procedure is CK (conductive keratoplasty) It uses, as I understand it, radiofrequency energy > instead of a laser and reshapes the cornea to help your near vision. > All is well and I am ready to do it when last night I get a call from my brother, who is a commercial > pilot, and he tells me that his doctor said that if this procedure is ever done you will never get > a pilots license renewed. He said to try and find out if this is true. I thought I would post the question > here and see if anybody knows if this is true or not. > Anybody familiar with this procedure or it's consequences as far as a license renewal?? > > Dave Mader > 2nd slowbuild 6 > rebuilding the engine ________________________________________________________________________________
Date: Sep 30, 2004
From: Jim Oke <wjoke(at)shaw.ca>
Subject: Re: RV-3 vs. RV-3A
Randy; As a point of reference, I purchased my RV-3 kits in fall 1980 (gosh, that's 24 years ago now!) and there were no CN-1 related materials or components in the kits. No surprise, since CN-1 was issued in Feb of 1982. Reading the text of CN-1 there is mention of several mishaps between July 1978 and March 1981 which led to the Van's aircraft detailed analysis of the RV-3 wing structure and the eventual issue of CN-1. One of the issues Van's had to deal with was an FAA document (which was enclosed with CN-1) that placed a blanket prohibition on aerobatics on "any RV-3 designated model aircraft". About the only around this blanket ban was to redesignate the aircraft as a different model of aircraft presumably after incorporating certain wing modifications and apply for a new airworthiness certificate as a type other than an RV-3. This was, in fact, the solution proposed by the FAA. CN-1 was essentially a recommended mod or set of actions to designate an existing RV-3 to an RV-3A to work around this FAA prohibition. As you may be aware, CN-1 laid out four methods for modifying the root rib depending on the exact nature of the root rib. The changeover date of Sept 1980 is mentioned as when .032 thickness root ribs were supplied vice the earlier .020 root ribs. An RV-3 owner/builder was expected to decide which version of the mod to incorporate depending on nature of the root rib installed and the state of completion of the wing, etc. At the same time the aft spar carry through structure was changed from a 1 x 1 x 1/8 angle to a 11/4 x 11/4 x 3/6 angle; the earlier small angle required some additional reinforcement via a bolted on angle. The larger angle was OK but the aft spar still required a doubler plate to put the spar bolt in double shear vice single shear. Keep in mind that in those days, Vans kits were rather basic compared to what they are now and a lot more "components" were actually supplied as raw sheet for the builder to cut out. The directions and plans were also a lot simpler and so an RV-3 kit may well have included a set of CN-1 instructions and some stock vice detailed plans and pre-cut parts. Sometime later on, Vans started introducing nosewheel versions of his aircraft line which used the "A" designator, the RV-6A being the first in perhaps 1987 or so. That would be when the RV-3A designator sort of faded away. I still fly my RV-3 with the CN-1 wing mods incorporated in the later stages of construction but the authorities in Canada didn't care much whether I called it an RV-3 or RV-3A so I didn't bother complicating the issue. Jim Oke Winnipeg, Man. RV-3, C-FIZM RV-6A, C-GKGZ ----- Original Message ----- From: "Randy Compton" <thecomptons(at)bellsouth.net> Subject: RV-List: RV-3 vs. RV-3A > > Listers: > > I'm familiar with the rear spar mod, CN-1, 1-4, for early 80's and older > RV-3's, which when reworked allowed for the "A" designation. What I'm > trying to find out is when/if this mod was incorporated into the RV-3 kit. > In other words, was there a certain time after which all RV-3 kits sold had > the fork-type rear spar and carry-through attach structure and no retro-work > was needed? > > I've searched the archives and have found little help, although I did read a > post about the "A" designation later being dropped. Is that because the > kits being produced had the upgraded structure? > > Thanks. > > Randy Compton > Gulf Breeze, FL > > ________________________________________________________________________________
Date: Aug 30, 2004
From: Doug Shenk <dshenk3(at)bresnan.net>
Subject: Re: Van's Homecoming
I may get a chance to get to Portland this weekend and go the homecoming for the first time. My question is how Saturday and Sunday compare with respect to amount of activity and to how many RV's are likely to be available for inspection (read: get a much needed dose of inspiration!). I suspect I will have to leave fairly early Sunday and wondering how much of the event I'll miss. Any info appreciated and you can let me know off list. Thanks. Do not archive. dshenk3(at)bresnan.net rv6a quickbuild kit but slowbuild technique! ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: grass runway length for RV's?
Date: Aug 30, 2004
Just go over to Amana and practice! You can always go to the Colony Inn between attempts and increase your gross! Cy Galley - Chair, Emergency Aircraft Repair Safety Programs Editor - TC EAA Sport Pilot ----- Original Message ----- From: <czechsix(at)juno.com> Subject: RV-List: grass runway length for RV's? > > Guys, > > For those of you with experience flying RV's off grass strips, what would > you consider the minimum safe runway length? I know, it depends on a > variety of factors, so in this case lets assume no obstacles at either > end higher than 6' (i.e. a cornfield in August) and no higher terrain or > obstacles beyond that, relatively level & smooth runway surface, > operating at gross weight with 180hp / CS, on a hot/humid day (say 95 F) > at 880' msl, with no headwind. Maybe throw in a bit of dew or post-rain > moisture on the grass to reduce braking effectiveness, and this would be > about the worst case scenario for me here in Iowa. Would 1700' be > adequate under these conditions? I imagine takeoff would be a non-event, > so landing and getting stopped without too much pucker factor would be my > main concern.... > > Thanks, > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D finishing.... > > ________________________________________________________________________________
From: Rvsearey(at)aol.com
Date: Aug 30, 2004
Subject: Re: grass runway length for RV's?
Mark, I flew my RV-4 off a 1400' private grass runway (1000' elev) all the time I had it. You are right, takeoff is no problem at any weight. Landing is no problem either as long as you are experienced in short field procedures and don't get excessive speed on final. There were a couple of times I did a go-around because I let the speed get too high and then floated down the runway. In my 4 I calculated that 70mph was a good short field speed for me based on what MY stall speed was. Yours may be different. Dan Decker RV-4 built, flown and regrettably sold SeaRey getting inspected today RV-7 ordered and waiting ________________________________________________________________________________
From: "Dean Pichon" <deanpichon(at)msn.com>
Subject: Results of Annual Inspection on my -4
Date: Aug 30, 2004
I just finished the 3rd annual inspection on my -4 and thought I make a quick post summarizing the more interesting findings. Thankfully, there were few interesting findings. The aircraft now has 221 hours. It has a 180hp A1A with Lasar ignition and Performance Airflow fuel injection. The prop is a CS Hartzell. The airframe presented no problems save for the rudder which now has small cracks on 3 of the forward rivets on 3 skin stiffeners on the starboard side. My rudder has an 0.016 skin and has RTV in the trailing edge per Van's original recommendation. I have stop-drilled the cracks and have started a new rudder with an 0.020 skin. On these stiffeners, I will use ProSeal in addition to rivets. Both the fuel injection system and the electronic ignition continue to perform flawlessly. I can't tell that I save any fuel or gain any power with the Lasar system - I'm just happy to have everything working. Again, I found a severly cracked plate that mounts the airbox to the air induction/fuel metering system. This same part was found cracked and replaced at last year's annual. My current hypothesis is that the lower cowl pre-loads the airbox via the rubber snout at the air intake. I have cut away a small portion of the snout in an attempt to relieve the preload without sacraficing seal quality. Clearly, I will have to keep an eye on this. I also noticed I have lost a single eyelet on one of the hinge strips on the cowl. At this point, I will simply keep an eye on the eyelets, as I don't have a good long-term strategy. The tires still have another year of tread remaining. I have 2 years on these Aero Trainers and will end up with 3 years if they make it to the next annual. The brake pads are still the orginal set. Some wear is evident, but still well above the minimum thickness requirement. I usually land on long, paved runways, so the brakes don't get much hard use. I have 3 years on the orginal Concorde gel cell and see no reason to replace it. For the first time, I had a compression test done on the engine. I don't have tools and have never done one, so I had the field FBO do this for me. The lowest cylinder was 76psi. All told, this annual cost me 6 quarts of oil, one oil filter, and an airbox mouting plate. Plus about 3 days of my labor with my Dad's help. The rudder cost, however, has yet to tallied. Dean Pichon Bolton, MA ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: elevator play
Date: Aug 30, 2004
My -6A elevators, after about 200 hours, have developed about 1/2 of play (1/4" up and down) relative to each other at the trailing edge. I'm guessing at the number, as I haven't actually measured it yet. I find this when, on pre-flight, I grap both trailing edges, and pull one up while pushing the other down. Has anyone else noticed this "problem"? I'm not sure what could cause this other than a slight (very slight) elongation of the hole in the control horns. Perhaps there is a better way to tie the 2 horns together than just the single bolt from the push/pull tube bearing. Andy ________________________________________________________________________________
From: "Pat Hatch" <pat_hatch(at)msn.com>
Subject: Re: elevator play
Date: Aug 30, 2004
Andy, If the bolt between the horns was loose or not torqued properly, this could cause the play you described. This would be the first thing I check. Pat ----- Original Message ----- From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com> Subject: RV-List: elevator play > > My -6A elevators, after about 200 hours, have developed about 1/2 of play (1/4" up and down) relative to each other at the trailing edge. I'm guessing at the number, as I haven't actually measured it yet. I find this when, on pre-flight, I grap both trailing edges, and pull one up while pushing the other down. > > Has anyone else noticed this "problem"? I'm not sure what could cause this other than a slight (very slight) elongation of the hole in the control horns. Perhaps there is a better way to tie the 2 horns together than just the single bolt from the push/pull tube bearing. > > Andy > > ________________________________________________________________________________
Date: Aug 30, 2004
From: Scott Bilinski <bilinski@kyocera-wireless.com>
Subject: Re: elevator play
Its the bolt that goes through both elevator horns, most likely. I sure would not fly until it is fixed. > > >My -6A elevators, after about 200 hours, have developed about 1/2 of play >(1/4" up and down) relative to each other at the trailing edge. I'm >guessing at the number, as I haven't actually measured it yet. I find >this when, on pre-flight, I grap both trailing edges, and pull one up >while pushing the other down. > >Has anyone else noticed this "problem"? I'm not sure what could cause >this other than a slight (very slight) elongation of the hole in the >control horns. Perhaps there is a better way to tie the 2 horns together >than just the single bolt from the push/pull tube bearing. > >Andy > > Scott Bilinski Eng dept 305 Phone (858) 657-2536


August 19, 2004 - August 30, 2004

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