RV-Archive.digest.vol-nq

October 17, 2002 - October 23, 2002



      
      Hi All,
      
      Get one of Bob Archer's wingtip Marker Beacon Antenna kits.
      
      BTW, the marker beacon antenna NEEDS to be a poor antenna.  Something that 
      "works" and does not do more than just barely "work".
      Who wants to receive an outer marker signal miles away from the outer marker?
      
      Just my thoughts.
      
      Jim Ayers
      PS Bob Archer's phone number is (310) 316-8796.  Give him a call.  He loves 
      to talk antenna's.
      
      
      
________________________________________________________________________________
From: Edcarris(at)aol.com
Date: Oct 17, 2002
Subject: Re: RV9-List: Re: posting (To Forward or Not to Forward...)
Don"t Forward, keep the RV-9 list pure. ________________________________________________________________________________
Date: Oct 17, 2002
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: DAR Listing ??? (with apologies to Jim)
I can understand the frustration of paying $500 for a 2 minute visit & a slip of paper, especially if you had to wait weeks or months for the appointment. Maybe it would feel better if you thought of it as a doctor visit. OK,OK, I'm joking. Sort of. The truth is, at the few FSDO's still willing to do inspections you would have likely gotten the same treatment, but your (and my) tax money would have footed the bill. As things now stand, many FAA inspectors consider the 'inspection' a paperwork check and have no interest in checking the plane for safe workmanship. The FAA is shifting responsibility for safety almost totally to the builder/owner. Consider the latest version of homebuilt operating limitations, which allow the owner to make major alterations to a homebuilt, place it in 'phase one' testing with a logbook entry, fly 5 hours of test time and restore the plane to normal operational status again with another logbook entry. In my view, it's a logical conclusion that the DAR is following standard FAA procedures. Our real complaint should be to FAA management and our congressmen/senators for allowing inspectors to ignore their duties to perform services that we as taxpayers have already paid for. Charlie Disclaimer: The first paragraph is intended to be funny. If you must flame, please flame me privately without wasting list bandwidth. ________________________________________________________________________________
From: "Gordon or Marge Comfort" <gcomfo(at)tc3net.com>
Subject: Re: Manual Trim Slop
Date: Oct 17, 2002
Subject: Re: RV-List: Manual Trim Slop > Interesting that you bring this up Paul, I have noticed that my manual trim > cable, not yet installed, seems to have about a half to three quarters of a > turn of slop (dead band) when I am playing with it on the bench. Does anyone > know if this is normal or should I see about getting another one from Van's > before I install it? > > Harry Crosby > Pleasanton, California > RV-6, electrical stuff Harry: It would be interesting to know how much slop is present when the cable is flexed to approximate the curves when it is installed. One could lay the cable out on the floor or a large bench and weight it down in a "S" curve and then measure the lost motion. My perception is that when straight, the system shows very little loss. But when curved, the clearance between the cable and its housing presents itself as lost motion. At least that is what it seems like on my -4. I suspect that the highest quality cables display less of it. Gordon Comfort N363GC ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Fuel pickup tube safetywire
Date: Oct 17, 2002
> > I am working on fuel tanks on my RV-7. In installing the fuel pickup > tube shouldn't the blue coupling nut be safety wired? Seems > like an a > lot of things we safety wired on military aircraft aren't > safety wired > on Experimental aircraft, or at least Van's aircraft. > Just gobber up the fitting with pro-seal after tightening. I did this both inside and out on the fuel fittings/nuts/etc. Alex Peterson Maple Grove, MN RV6-A N66AP 215 hours ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Fuel pickup tube safetywire
Date: Oct 17, 2002
Don't believe B-nuts need any safetying. Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org Always looking for articles for the Experimenter ----- Original Message ----- From: "Steve Eberhart" <newtech(at)newtech.com> Subject: RV-List: Fuel pickup tube safetywire > > I am working on fuel tanks on my RV-7. In installing the fuel pickup > tube shouldn't the blue coupling nut be safety wired? Seems like an a > lot of things we safety wired on military aircraft aren't safety wired > on Experimental aircraft, or at least Van's aircraft. > > Didn't find anything in the archives. > > Steve Eberhart > RV-7, working on fuel tanks > Old Air Force instrument systems technician > > > > > > > ________________________________________________________________________________
From: Smcm75(at)aol.com
Date: Oct 17, 2002
Subject: Re: RV9-List: Aux Fuel
In a message dated 10/17/02 6:06:12 PM Eastern Daylight Time, Ed_Cole(at)maximhq.com writes: > Scott, > it should be one Hell of a fire if you have to do an emergency > off-field landing and rupture the tank. > > Best case is that you leave a trail of underwear and t-shirts ! > I was wondering if you had retractable gear, or what about reputering your wing tanks?.....but just in case I designed a fuel dump in case of emergencies. Now let's hear from the EPA Scott ________________________________________________________________________________
From: Smcm75(at)aol.com
Date: Oct 17, 2002
Subject: Re: RV9-List: Aux Fuel
In a message dated 10/17/02 8:38:15 PM Eastern Daylight Time, rv7(at)b4.ca writes: > I've been thinking about this for my -7 as well, but would add true > "drop" capability. In the event of an emergency, you're right, I > wouldn't want it down there either. Some brightly marked release handle > in a location where you wouldn't kick it by accident would be a good thing. > It is not a true drop tank. can only be attached and removed on the ground ( for safety) it does have a fuel dump feature in case of an emergency landing. Scott ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Fuel pickup tube safetywire
Date: Oct 17, 2002
WHY? Why gobber up anything? Use the fittings as dry as designed. If they are properly supported, there shouldn't be any problem. Check most any military or commercial plane, they don't use anything. IF you are ANAL use some torque seal so you can see if they move at all. Torque seal also is useful if it is placed on a fitting, nut, or bolt head after you have done the final fastening. Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org Always looking for articles for the Experimenter ----- Original Message ----- From: "Alex Peterson" <alexpeterson(at)usjet.net> Subject: RE: RV-List: Fuel pickup tube safetywire > > > > > I am working on fuel tanks on my RV-7. In installing the fuel pickup > > tube shouldn't the blue coupling nut be safety wired? Seems > > like an a > > lot of things we safety wired on military aircraft aren't > > safety wired > > on Experimental aircraft, or at least Van's aircraft. > > > > Just gobber up the fitting with pro-seal after tightening. I did this > both inside and out on the fuel fittings/nuts/etc. > > Alex Peterson > Maple Grove, MN > RV6-A N66AP 215 hours > > ________________________________________________________________________________
From: "Gary Newsted" <fcs(at)jlc.net>
Subject: Re: RV9-List: Aux Fuel link
Date: Oct 17, 2002
Anyone thinking of adding tanks to their wing, would do well to read Vans article on this very subject in a recent RVator. Sorry I don't recall which issue, perhaps someone else has it handy. I'm reading all sorts of direct contradictions of the words from the man who designed the plane. He wrote this article for good reason. While I have to admire the creative ways people find for stuffing fuel in every pocket they can fill, I'd wait to see how these birds actually fly (in turbulence) before joining the flock. Of all the dangerous mods you can cook up, this has got to be near the top of the list. My two cents anyway... ________________________________________________________________________________
From: "Gary Newsted" <fcs(at)jlc.net>
Subject: Re: RV9-List: parking brake
Date: Oct 17, 2002
I went with the basic Matco parking brake for here on the windy east coast. I fab'ed a sturdy bracket to replace the hose-to-firewall bracket. Realizing how discouraging a failure of this baby would be (no steering, or locked wheels!), I took extra care to create a cable attachment that will withstand a gorilla at the helm. The only thing I changed from the photo ref'ed below, is I switched to 45-degree fittings to ease the routing of the metal lines. I've tugged on this thing a whole bunch of times and it works smoothly. http://www.jlc.net/~fcs/images/fuselage/f_brkbkt1.jpg ________________________________________________________________________________
Date: Oct 17, 2002
From: Jerry Springer <jsflyrv(at)earthlink.net>
Subject: Re: Fuel pickup tube safetywire
Steve Eberhart wrote: > > > I am working on fuel tanks on my RV-7. In installing the fuel pickup > tube shouldn't the blue coupling nut be safety wired? Seems like an a > lot of things we safety wired on military aircraft aren't safety wired > on Experimental aircraft, or at least Van's aircraft. > > Didn't find anything in the archives. > > Steve Eberhart > RV-7, working on fuel tanks > Old Air Force instrument systems technician > > Steve you are the manufacturer you can do it anyway you would like to. If you do not feel comfortable with it not being safty wired then find a way to do it. Jerry ________________________________________________________________________________
Date: Oct 17, 2002
Subject: Re: RV9-List: Aux Fuel
From: Tom Lutgring <tlutgring(at)juno.com>
Rob, sounds like a hell of an idea.... I'll bet Tom Ridge (homeland defense) would be really interested in a homebuilt with "bomb" dropping capability, in this post 9/11 era. Tom, RV-9A (36 gal) fuselage ________________________________________________________________________________
Date: Oct 17, 2002
From: Dave Bristol <bj034(at)lafn.org>
Subject: Re: RV9-List: Aux Fuel
John, There was some talk about aux fuel but it was on the RV list not the RV9 list. Also the folks that are considering drop tanks might want to check with the feds. The last I heard was that they arent even legal on an actual military plane (WWII type) they had to be safety wired so they couldn't be dropped. And, even if that's not so, I think maybe the FBI might want to talk to you about it! 8 ) Dave -6 So Cal (I don't even have the range of my stock tanks!) John Williams wrote: > > Keith: Good question. There was a chap on about ten days ago who is doing > a Mazda rotary in an RV-9, and who alluded to having added extra fuel. This > so piqued my interest that I asked him to share how he did it with me. > Haven't heard from him since! Musta' been something I said! ________________________________________________________________________________
From: "Karie Daniel" <karied4(at)attbi.com>
Subject: RV-7A Empennage Jig Question
Date: Oct 17, 2002
The plans for the 7A don't call for building a jig for the empennage (it's the same as a RV-9 empennage also) and I was pretty jazzed about not having to build one at first. Now that I'm up to my elbows in this I really would like to build a jig to make sure everything is straight before I start riveting. I went to Home Depot today and bought some 4x4's and built what looks like a jig from most RV-6 web sites I've seen but I'm not sure how to positively make sure the jig is plumb. Anyone have any jig plans or advice so that I make sure the jig is straight? BTW... If you have an RV web site with pictures of your building progress you have no idea how valuable it is to new builders like myself. Thank you! I hope to have a site of my own up soon. Karie Daniel Maple Valley, WA. RV-7A ________________________________________________________________________________
Date: Oct 17, 2002
From: Mark Schrimmer <mschrimmer(at)pacbell.net>
Subject: Re: RV9-List: parking brake
on 10/17/02 6:07 PM, Gary Newsted at fcs(at)jlc.net wrote: > --> RV9-List message posted by: "Gary Newsted" > > I went with the basic Matco parking brake for here on the windy east coast. I > fab'ed a sturdy bracket to replace the hose-to-firewall bracket. Gary, Cool bracket! Does it go in the exact same place as the hose-to-firewall bracket? What did you use for the cable? Where do you plan to mount the handle at the other end of the cable? Thanks, Mark Schrimmer ________________________________________________________________________________
From: Paulbaird(at)aol.com
Date: Oct 17, 2002
Subject: Re: DAR - Compensation?
I paid $250 in Ohio Paul 90355 ________________________________________________________________________________
From: Smcm75(at)aol.com
Date: Oct 17, 2002
Subject: Re: RV9-List: Aux Fuel
In a message dated 10/17/02 9:52:04 PM Eastern Daylight Time, bj034(at)lafn.org writes: > > There was some talk about aux fuel but it was on the RV list not the RV9 > list. > Also the folks that are considering drop tanks might want to check with the > feds. > The last I heard was that they arent even legal on an actual military plane > (WWII > type) they had to be safety wired so they couldn't be dropped. And, even if > that's not so, I think maybe the FBI might want to talk to you about it! > 8 > > Get a life I think we are all grown-ups. i don't think that anyone in their right mind would utilize a "real" drop tank that terminology was just used to describe how the aux tank looked, not operated. Scott Morrow RV-6A 90 % ________________________________________________________________________________
From: Smcm75(at)aol.com
Date: Oct 17, 2002
Subject: Re: RV9-List: Aux Fuel
In a message dated 10/17/02 9:11:46 PM Eastern Daylight Time, tlutgring(at)juno.com writes: > > Rob, sounds like a hell of an idea.... I'll bet Tom Ridge (homeland > defense) would be really interested in a homebuilt with "bomb" dropping > capability, in this post 9/11 era. > > Tom, RV-9A (36 gal) fuselage > Again get a life... The aux tank described was not a "drop" tank just looked like one. Scott Morrow RV-6A 90% ________________________________________________________________________________
From: Smcm75(at)aol.com
Date: Oct 17, 2002
Subject: Re: RV9-List: Aux Fuel
In a message dated 10/17/02 9:02:16 PM Eastern Daylight Time, jsflyrv(at)earthlink.net writes: > I heard that you cannot have inflight drop tanks on your airplane if you are > not > military. > You ought to read my response again. This is not a drop tank , but just looks like one. Scott Morrow RV-6A ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Fuel pickup tube safetywire
Date: Oct 17, 2002
Following the construction video, I covered the area you are concerned about with proseal. - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of > Steve Eberhart > Sent: Thursday, October 17, 2002 5:41 PM > To: rv-list(at)matronics.com > Subject: RV-List: Fuel pickup tube safetywire > > > > I am working on fuel tanks on my RV-7. In installing the fuel pickup > tube shouldn't the blue coupling nut be safety wired? Seems > like an a > lot of things we safety wired on military aircraft aren't > safety wired > on Experimental aircraft, or at least Van's aircraft. > > Didn't find anything in the archives. > > Steve Eberhart > RV-7, working on fuel tanks > Old Air Force instrument systems technician > > ________________________________________________________________________________
From: "Haywire" <haywire(at)telus.net>
Subject: RE: RV9-List: Aux Fuel
Date: Oct 17, 2002
Hi John; > > --> RV9-List message posted by: "John Williams" > > Keith: Good question. There was a chap on about ten days ago > who is doing > a Mazda rotary in an RV-9, and who alluded to having added extra > fuel. This > so piqued my interest that I asked him to share how he did it with me. > Haven't heard from him since! Musta' been something I said! > This would have been me, but I don't recall an e-mail from you. I try to answer all e-mails promptly, so maybe I accidentally deleted it or just didn't receive it. I see that someone has already given you my web address. Most of the info you want can be found there. I will one day finish writing the procedure for building the OB tanks. After you look over the info on my site if you have any further questions, don't hesitate to e-mail me. > I don't have my wing kit yet, nor the large drawings, but it sure looks to > me like you could switch the position of the tank outboard > end-ribs with the > adjacent wing nose ribs, and move the filler cap outboard to the next > chamber, and pick up about two gallons (estimated) capacity on I wouldn't go with this approach as you would either have to make a new longer IB leading edge skin or you would have a major seam on your tank. Easier to just convert the OB leading edge as a separate tank. > > From an aerodynamic standpoint, engineers say that extra fuel > carried as far > outboard as possible is beneficial to the wing spar with regard to the > bending moments and lessens stress on the spar. This is true as it improves span loading as well as stability. Unfortunately it also reduces spin recovery, but this should never be a problem with proper flight management. Hope this helps S. Todd Bartrim Turbo 13B rotary powered RV-9endurance (FWF) C-FSTB http://www3.telus.net/haywire/RV-9/C-FSTB.htm ________________________________________________________________________________
From: "Haywire" <haywire(at)telus.net>
Subject: RE: RV9-List: Aux Fuel link
Date: Oct 17, 2002
> --> RV9-List message posted by: "Gary Newsted" > > Anyone thinking of adding tanks to their wing, would do well to read Vans > article on this very subject in a recent RVator. Sorry I don't > recall which > issue, perhaps someone else has it handy. I'm reading all sorts > of direct > contradictions of the words from the man who designed the plane. > He wrote this > article for good reason. While I have to admire the creative > ways people find > for stuffing fuel in every pocket they can fill, I'd wait to see > how these birds > actually fly (in turbulence) before joining the flock. Of all > the dangerous > mods you can cook up, this has got to be near the top of the list. > My two cents anyway... Hi Gary; This isn't something I just came up with on a whim. It took alot of careful planning & consideration, not just to build it correctly but also to have a plan to use it correctly. Just as building a mod like this is not for the faint of heart, neither is flying over vast distances of water and inhospitable terrain. Some people are most comfortable flying in areas where you couldn't throw a rock without hitting a suitable place to land, equipped with fuel pumps. Others are drawn to the wilder, rugged corners of this rock we call earth. Fortunately those areas have no fuel service so it keeps out the riff raff. You must remember that Van is subject to liability issues so it is not in his interest to encourage anyone to modify his design. However there is at least one of his employees that has been encouraging in his remarks about my fuel mods. Although he always chooses his words carefully, implying that he his in no way endorsing it. I recently acquired 8 hrs flight time in an RV-6 with OB leading edges tanks, very similar to mine. This plane has been flying for more than 10 years, travelling from the Canadian arctic to South America (not in one trip'-)) and it has done it very well. While he was being told that he couldn't do it, he didn't hear them because he was busy doing it. Now, I'm not saying that anyone should do this. It takes allot of careful thought and I would encourage anyone considering this to think it through fully, asking yourself "do I really need that much?"; "will I really use it?" & most importantly "can I do this? - safely?" But I certainly would never discourage anyone based upon my own personal limits or the liability concerns of it's designer. Now I'm not saying that I won't ever have an accident caused by this, but I have done my best to anticipate any problems. I do know that I will die. I just don't know how or where, but I'm sure not going to sit and wait for it. All Men Dream: But Not Equally Those Who Dream By Night In The Dusty Recesses Of Their Minds Wake To Find That It Was Vanity: But The Dreamers Of The Day Are Dangerous Men, For They May Act Their Dreams With Open Eyes To Make It Possible T.E. Lawrence S. Todd Bartrim Turbo 13B rotary powered RV-9endurance (FWF) C-FSTB http://www3.telus.net/haywire/RV-9/C-FSTB.htm ________________________________________________________________________________
Date: Oct 17, 2002
From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)mcleodusa.net>
Subject: Re: RV9-List: Aux Fuel
Smcm75(at)aol.com wrote: > > In a message dated 10/17/02 8:38:15 PM Eastern Daylight Time, rv7(at)b4.ca > writes: > > > I've been thinking about this for my -7 as well, but would add true > > "drop" capability. In the event of an emergency, you're right, I > > wouldn't want it down there either. Some brightly marked release handle > > in a location where you wouldn't kick it by accident would be a good thing. > > > > It is not a true drop tank. can only be attached and removed on the ground ( > for safety) it does have a fuel dump feature in case of an emergency landing. > > Scott > Belly tanks have been used on Pitt's for more than a quarter century. They are not drop tanks, as such, They can only be removed manually from the ground. There is one in my hangar now, belongs to a friend. He uses it all the time for long ferry to contests. I have one out in my garage that needs finish welding on. They hold about 16 .5 gallons as we make them. I have flown his on a ferry back from Dennison, TX to Central IL. In the air I couldnt tell it was on the plane. It affected airspeed and handling little if any. When in flight we burn it out first, Then go to the inside tank. When landing with it on, it is hardly noticeable. Taxi-ing and takeoffs are something else. With his plane( was Bob Herendeen's Pitt's that he flew in Oshkosh), I taxied it slow and very careful, tool off almost 3 point to get in air soon as possible, then it was ok. Loaded with fuel, the CG point is moved very downward and with the extra 100 lbs, it affects tracking and is very squirrelly for a plane that is normally a pussycat. A lot of guys used two of them, they would make one end slip off from one and they would stuff clothes in it, rolled in a long cigar roll. As for an RV, I am thinking of aux fuel, but I will probably not go with a belly tank. Phil ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Fuel pickup tube safetywire
Date: Oct 17, 2002
Cy is right here. B nuts don't technically "have" to be safetied. Many B nuts on high pressure hydraulic systems on 747's, 757's, DC-10's, etc.. are not saftied, and they are operating at thousands of PSI! If you really want, you can buy B nuts which have a hole drilled in it for safety. Usually these are only used on AN-10 and larger lines. Just my experience with the jet-liners. Cheers, Stein Bruch -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Cy Galley Subject: Re: RV-List: Fuel pickup tube safetywire Don't believe B-nuts need any safetying. Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org Always looking for articles for the Experimenter ----- Original Message ----- From: "Steve Eberhart" <newtech(at)newtech.com> Subject: RV-List: Fuel pickup tube safetywire > > I am working on fuel tanks on my RV-7. In installing the fuel pickup > tube shouldn't the blue coupling nut be safety wired? Seems like an a > lot of things we safety wired on military aircraft aren't safety wired > on Experimental aircraft, or at least Van's aircraft. > > Didn't find anything in the archives. > > Steve Eberhart > RV-7, working on fuel tanks > Old Air Force instrument systems technician > > ________________________________________________________________________________
From: "Gary Newsted" <fcs(at)jlc.net>
Subject: Re: RV9-List: parking brake
Date: Oct 17, 2002
> Cool bracket! Does it go in the exact same place as the hose-to-firewall > bracket? Yep. I added another row of rivets along with the existing ones. Used the old bracket as a pattern for the new one. It's super strong. The cable is a standard locking tee-handle cable from AC Spruce, cut down to about 24" long. The swivel end is just a piece of hex steel stock about 1" long. I drilled it part way through so the cable shell fits into it, then a smaller center hole for the wire to pass through. The wire actually passes through a hole in the clevis pin which is just floating in the assembly. Two pointed set-screws clamp the cable shell into place. There's a small "Z" shaped bracket that serves to prevent the valve lever from going over-center. The valve is mounted at a slight downward angle to reduce cable bend and make it work smooth. Couldn't be happier with it! > Where do you plan to mount the handle at the other end of the cable? I made a small rounded "A" shaped bracket out of angle stock that is bolted to the vertical side rib where the fuel vent lines run (sorry I don't have the part number, those plans were put away long ago). It's just far enough away from the pilot so you have to reach for it and won't accidentally kick it or hit your knee on it. Anyway, if you go with the Matco valve, this is one proven way to mount the sucker. Steering by brakes always struck me as a wierd concept, but it's time proven. Adding a parking brake into your steering system is equally wierd, but it beats running after your plane! It's windy around here. Gary ________________________________________________________________________________
From: "Gary Newsted" <fcs(at)jlc.net>
Subject: Re: RV9-List: Aux Fuel
Date: Oct 17, 2002
> Get a life I think we are all grown-ups. Hey, be nice. I got a chuckle out of that reply. Although the keywords were certain to light up a few monitors down in Jersey if you know what I mean. ________________________________________________________________________________
From: "James E. Clark" <jclark(at)conterra.com>
Subject: Re: RV9-List: Aux Fuel
Date: Oct 17, 2002
Hmmm ... Is this right behind the exhausts? (that sometimes spit fire)???? Or do I have the wrong image in mind?. Why not put the tank in the baggage compartment given that you are willing to make the trade-off. From a weight standpoint you could have about the same capacity. Of course you would have a bit of a problem if there was an off-field landing and it ruptured. But that's another matter altogether. James > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Smcm75(at)aol.com > Sent: Thursday, October 17, 2002 5:33 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Re: RV9-List: Aux Fuel > > > I am developing an external "drop tank/cargo pod" that would have > only about > a 2 lb penalty (attach points and plumbing) when the tank is not > attached. > The tank will have a capacity of approx. 18 gal and will attach directly > under the belly onto the front and rear spar. A couple of pins > will make for > easy attach detach. The point is when you need extra fuel you can put the > tank on, When you need extra baggage capacity you can put the > baggage pod on. > when you don't need either you can remove them and they is literally no > weight or drag penalty. This tank/pod will fit RV-6, RV-6A, RV-7, RV-7A, > RV-8, RV-8A. This thing looks neat (WW II style) and it is right on the > center of gravity. > > Scott Morrow > RV-6A 90% > > ________________________________________________________________________________
From: "Gary Newsted" <fcs(at)jlc.net>
Subject: Re: RV9-List: Aux Fuel link
Date: Oct 17, 2002
Todd, I appreciate experimentation and innovation as much as anyone, but I'll stand by my statement that anyone considering doing this would do well to witness a prior example first (in turbulence). Regardless of any liability issues Van may have, I don't believe for one second that he would intentionally lie about the mathematics of his wing design. And since I love quotes, and you offered such a nice one, let me add to it. "Even this brief history of aviation is already littered with failed experiments and experimenters." [Thomas Edison]. You're a bit further on the edge than I would dare to be, but I sincerely wish you good flying and safe landings. ________________________________________________________________________________
Date: Oct 17, 2002
From: Dave Bristol <bj034(at)lafn.org>
Subject: Re: RV-7A Empennage Jig Question
Karie, The jig doesn't have to be plumb, it's the part that has to be plumb. The jig is only there to hold the part in the position that you put it. Just make it as straight as practical and be sure that it doesn't move. Also, beware, there are those on the list that don't think that jigs are of any use! Dave -6 So Cal Karie Daniel wrote: > > The plans for the 7A don't call for building a jig for the empennage (it's the same as a RV-9 empennage also) and I was pretty jazzed about not having to build one at first. Now that I'm up to my elbows in this I really would like to build a jig to make sure everything is straight before I start riveting. > > I went to Home Depot today and bought some 4x4's and built what looks like a jig from most RV-6 web sites I've seen but I'm not sure how to positively make sure the jig is plumb. Anyone have any jig plans or advice so that I make sure the jig is straight? > > BTW... If you have an RV web site with pictures of your building progress you have no idea how valuable it is to new builders like myself. Thank you! I hope to have a site of my own up soon. > > Karie Daniel > > Maple Valley, WA. > > RV-7A > ________________________________________________________________________________
From: rv4joe(at)sofnet.com
Subject: RV4 Project for Sale
Date: Oct 17, 2002
Have a 4 project partially completed. Hoped to finish it, but life situation changed. If interested, it is drop me a line here or at rv4joe(at)sofnet.com. Located in southwest MO. email pics on request. ________________________________________________________________________________
Date: Oct 18, 2002
From: Jim Oke <wjoke(at)shaw.ca>
Subject: Re: RV-7A Empennage Jig Question
Hi; From my experience (assembling a RV-6A prepunched tail kit two years ago) there is no need to put much time and effort into a tail jig. Hmm, let's rephrase that - I feel the time and effort put into a fancy tail jig are probably better spent elsewhere... The prepunched skins and spar effectively take care of any warping or twist. The one area where some care is needed is to make sure the stabilizer aft spar is kept straight. I used a 2 x 6 on edge with four metal hardware store angle brackets drilled for 3/16" bolts that picked up the elevator hinge brackets. I used a piece of stretched nylon monofilament fishline to keep the 3/16 holes in the brackets a straight line. The 2 x 6 wasn't that straight so I used some note paper shims between the brackets and the 2 x 6 to keep the bolt holes line up vertically. Once the above is taken care of, the other role of the jig is to hold the parts in a convenient position for riveting. I added a couple of 2 x 6 cross pieces on the bottom to support the 2 x 6 and then a light 2 x 2 vertical in the centre to clamp the centre part of the forward spar to so the whole thing wouldn't flop over. The whole jig (fixture might be a better word) was reasonably portable and could be moved around which is an advantage compared to a massive jig solidly bolted to the floor or whatever. Jim Oke Winnipeg, MB RV-3 RV-6A (painting) ----- Original Message ----- From: "Karie Daniel" <karied4(at)attbi.com> Subject: RV-List: RV-7A Empennage Jig Question > > The plans for the 7A don't call for building a jig for the empennage (it's the same as a RV-9 empennage also) and I was pretty jazzed about not having to build one at first. Now that I'm up to my elbows in this I really would like to build a jig to make sure everything is straight before I start riveting. > > I went to Home Depot today and bought some 4x4's and built what looks like a jig from most RV-6 web sites I've seen but I'm not sure how to positively make sure the jig is plumb. Anyone have any jig plans or advice so that I make sure the jig is straight? > > BTW... If you have an RV web site with pictures of your building progress you have no idea how valuable it is to new builders like myself. Thank you! I hope to have a site of my own up soon. > > Karie Daniel > > Maple Valley, WA. > > RV-7A > > ________________________________________________________________________________
From: "Patrick Kelley" <webmaster(at)flion.com>
Subject: RV-7A Empennage Jig Question
Date: Oct 17, 2002
You can get the fixture plumb enough with a regular level; don't be a fanatic about it. As long as the parts are held immobile in good alignment the jig itself could be as crooked as Bill Clinton. My website has a diagram of a way-over-engineered jig I built so I could work indoors (www.flion.com); feel free to look it over and adapt as needed. By the way, I added a couple of pictures of moving to the site - not enough to go look if you've viewed it recently - and my fuselage kit has arrived so I hope to have more content added around Christmas time. I should invest in a digicam like Dan Checkowith, but then I'd never get anything done what with fiddling with the site. I agree, tho, that the builder's sites are a great source of inspiration and some original ideas. Pat Kelley - RV-6A - fuselage bulkheads nearly ready for primer and rivet -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Karie Daniel Subject: RV-List: RV-7A Empennage Jig Question The plans for the 7A don't call for building a jig for the empennage (it's the same as a RV-9 empennage also) and I was pretty jazzed about not having to build one at first. Now that I'm up to my elbows in this I really would like to build a jig to make sure everything is straight before I start riveting. I went to Home Depot today and bought some 4x4's and built what looks like a jig from most RV-6 web sites I've seen but I'm not sure how to positively make sure the jig is plumb. Anyone have any jig plans or advice so that I make sure the jig is straight? BTW... If you have an RV web site with pictures of your building progress you have no idea how valuable it is to new builders like myself. Thank you! I hope to have a site of my own up soon. Karie Daniel Maple Valley, WA. RV-7A ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: RV-7A Empennage Jig Question
Date: Oct 17, 2002
Hi Karie, Try this: Assuming that you have the basic pieces to assemble the typical 'H' shaped jig, use a plumb bob to get the two upright 4X4s (posts) straight vertically. This is done buy hanging the plumb bob along side the 4x4s on two adjacent sides of each post. When these posts are squared up and fixed firmly in place a wire will be strung tightly between the two posts. Some .032 stainless steel tie wire will do the job. To do this drill small diameter holes through the centers of the posts so that the wire will be on a center line between the posts. An alternate choice would be some screw eyes. You can use a hardware store turnbuckle to tighten the wire. Make a small 'S' hook that will slide along the length of the tightened wire. To this 'S' hook the plumb bob will be adjusted and tied so that it hangs almost touching the crossbar. The point of the plumb bob should now be very nearly if not exactly centered on the crossbar, close to center is good enough. After the next step the overhead wire and the centerline 'must' be in line with each other. Move the plumb bob to each end of the wire. After the plumb bob has stopped moving mark a dot on the crossbar at the pointed end of the plumb bob. Using the marks at the center of each end of the cross bar stretch a chalk line, a thread or a long straight edge to draw the base centerline. This line will be used to line up the elevator mount centers. You now have the basic structure in place for final assembly of your stabilizers. You will need an upright to one side of the crossbar at the center. This along with some C clamps or what have you will be used to hold the stab upright and centered. By changing the length of the plumb bob line and sliding it back and forth you can be sure all is true and square as assembly goes forward. I used three plumb bobs on mine, one stayed in the center throughout assembly, the other two were moved back and forth as needed. I hope this description works for you or at least helps get you on the right track. Have fun building, Jim in Kelowna ------ Original Message ----- From: "Karie Daniel" <karied4(at)attbi.com> Subject: RV-List: RV-7A Empennage Jig Question > > The plans for the 7A don't call for building a jig for the empennage (it's the same as a RV-9 empennage also) and I was pretty jazzed about not having to build one at first. Now that I'm up to my elbows in this I really would like to build a jig to make sure everything is straight before I start riveting. > > I went to Home Depot today and bought some 4x4's and built what looks like a jig from most RV-6 web sites I've seen but I'm not sure how to positively make sure the jig is plumb. Anyone have any jig plans or advice so that I make sure the jig is straight? > > BTW... If you have an RV web site with pictures of your building progress you have no idea how valuable it is to new builders like myself. Thank you! I hope to have a site of my own up soon. > > Karie Daniel > > Maple Valley, WA. > > RV-7A > > ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Oct 18, 2002
Subject: Re: DAR - Compensation?
Mine was $500 which he explained by saying "this also includes your repairman's certificate ". Len Leggette RV-8A N901LL (res) Greensboro, N.C. Ready to Fly !! ________________________________________________________________________________
From: "Jack Textor" <jack(at)iajobs.com>
Subject: Fuel pickup tube safetywire
Date: Oct 18, 2002
Steve, I used proseal on mine Steve Eberhart wrote: > > > I am working on fuel tanks on my RV-7. In installing the fuel pickup > tube shouldn't the blue coupling nut be safety wired? Seems like an a > lot of things we safety wired on military aircraft aren't safety wired > on Experimental aircraft, or at least Van's aircraft. > > Didn't find anything in the archives. > > Steve Eberhart > RV-7, working on fuel tanks > Old Air Force instrument systems technician > > Steve you are the manufacturer you can do it anyway you would like to. If you do not feel comfortable with it not being safty wired then find a way to do it. Jerry ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Fuel pickup tube safetywire
Date: Oct 18, 2002
> WHY? Why gobber up anything? Use the fittings as dry as > designed. If they are properly supported, there shouldn't be > any problem. Check most any military or commercial plane, > they don't use anything. IF you are ANAL use some torque seal > so you can see if they move at all. Torque seal also is > useful if it is placed on a fitting, nut, or bolt head after > you have done the final fastening. When I spoke of gobbering up the fitting, I was thinking specifically of the 90 degree fitting in an inverted fuel setup (the 90 degree part of the fitting is inside the tank, with a nut on the outside of the tank to hold it in place). The potential problem is with the bulkhead fitting rotating when the line from the fuselage is tightened. This bulkhead fitting has no anti-rotate protection, and it must seal. Alex Peterson Maple Grove, MN RV6-A N66AP 215 hours ________________________________________________________________________________
From: "John Huft" <rv8tor(at)lazy8.net>
Subject: RV pictures
Date: Oct 18, 2002
Hello listers So far, I have only received 4 pictures of RVs. None of these are nosedraggers. C'mon, where is your pride? Really, this could be a good resource. For those planning a paint job. For those trying to remember what someone's airplane looks like. Those curious about one of their list friends. Also, it is a nice diversion on a Saturday am when the weather is stinky. My favorite page of skywagons is the Alaska Wing http://www.lazy8.net/akwing.htm I am sure we RVers can do better. After all, we BUILT the things! Follow the link on this page to view the pics. http://www.lazy8.net/rv8.html Send me pics at webmaster(at)lazy8.net I will run them through Photoshop to compress etc. John Huft, Pagosa Springs, CO RV8 "Gypsy Tailwind" 2.6 hours ________________________________________________________________________________
From: "John Huft" <rv8tor(at)lazy8.net>
Subject: DAR - Compensation?
Date: Oct 18, 2002
An old friend was my DAR, and so I may have gotten a reduced price. He stopped on the way from his home in Denver, travelling to Phoenix to attend a DAR class required every two years. It is a three day class, and he pays all his expenses, plus $125/day for the class. He is required to attend a 1-day class in Denver on the off years. When you also consider the amount of liabilty a DAR takes on every time he signs an airplane off, I think the fees are mostly reasonable. I do think it is fair to expect him to inspect the airplane. It is good to have the local experts do it too. I had three inspectors, each caught things the others didn't. On my own final-final inspection before flight, I caught some more. Paperwork only reminds me of annual inspections I have heard of, where the real good one means you send him a picture of the airplane! Just like the "in the bar, BFR" I guess. John Huft Pagosa Springs,CO RV8 -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Lenleg(at)aol.com Subject: Re: RV-List: DAR - Compensation? Mine was $500 which he explained by saying "this also includes your repairman's certificate ". Len Leggette RV-8A N901LL (res) Greensboro, N.C. Ready to Fly !! ________________________________________________________________________________
Date: Oct 18, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: RV pictures
John Huft wrote: > > > Hello listers > > So far, I have only received 4 pictures of RVs. None of these are > nosedraggers. C'mon, where is your pride? > > Really, this could be a good resource. For those planning a paint job. For > those trying to remember what someone's airplane looks like. Those curious > about one of their list friends. > Also, it is a nice diversion on a Saturday am when the weather is stinky. > > My favorite page of skywagons is the Alaska Wing > http://www.lazy8.net/akwing.htm > > I am sure we RVers can do better. After all, we BUILT the things! > > Follow the link on this page to view the pics. > http://www.lazy8.net/rv8.html > > Send me pics at webmaster(at)lazy8.net I will run them through Photoshop to > compress etc. > > John Huft, Pagosa Springs, CO > RV8 "Gypsy Tailwind" 2.6 hours Another RV photo album is located here: http://home.hiwaay.net/~sbuc/journal/album_1.html It is a bit dated since you will notice there are no RV9A or RV-7 photos. Hopefully John's album will get many great new airplanes for us to view. Sam Buchanan "The RV Journal" http://thervjournal.com ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Fuel pickup tube safetywire
Date: Oct 18, 2002
Sorry, I thought you were applying something to make the tube seal. Bulkhead sealing is another matter. ----- Original Message ----- From: "Alex Peterson" <alexpeterson(at)usjet.net> Subject: RE: RV-List: Fuel pickup tube safetywire > > > > WHY? Why gobber up anything? Use the fittings as dry as > > designed. If they are properly supported, there shouldn't be > > any problem. Check most any military or commercial plane, > > they don't use anything. IF you are ANAL use some torque seal > > so you can see if they move at all. Torque seal also is > > useful if it is placed on a fitting, nut, or bolt head after > > you have done the final fastening. > > > When I spoke of gobbering up the fitting, I was thinking specifically of > the 90 degree fitting in an inverted fuel setup (the 90 degree part of > the fitting is inside the tank, with a nut on the outside of the tank to > hold it in place). The potential problem is with the bulkhead fitting > rotating when the line from the fuselage is tightened. This bulkhead > fitting has no anti-rotate protection, and it must seal. > > Alex Peterson > Maple Grove, MN > RV6-A N66AP 215 hours > > ________________________________________________________________________________
From: Imfairings(at)aol.com
Date: Oct 18, 2002
Subject: Re: RV6-List: RV6-N664SB FLIES--Finally!!!!!!!!!!!!!!!!!!!!!!
Stein, Congrats on the first flight! If the locals are any indication, that face controtion is going to be there for weeks and will return frequently. Bob Fairings-Etc. ________________________________________________________________________________
From: "John Williams" <frate.dawg(at)attglobal.net>
Subject: RE: RV9-List: Aux Fuel
Date: Oct 18, 2002
Todd: Thanx. I hadn't thought of that, but as I said, I don't have the wing kit yet, nor anything to look at other than the preview plans (which, at my advanced age, are damned hard to see, let alone read!) Regards, John -----Original Message----- From: owner-rv9-list-server(at)matronics.com [mailto:owner-rv9-list-server(at)matronics.com] On Behalf Of Haywire Subject: RE: RV9-List: Aux Fuel --> RV9-List message posted by: "Haywire" Hi John; > > --> RV9-List message posted by: "John Williams" > > Keith: Good question. There was a chap on about ten days ago > who is doing > a Mazda rotary in an RV-9, and who alluded to having added extra > fuel. This > so piqued my interest that I asked him to share how he did it with me. > Haven't heard from him since! Musta' been something I said! > This would have been me, but I don't recall an e-mail from you. I try to answer all e-mails promptly, so maybe I accidentally deleted it or just didn't receive it. I see that someone has already given you my web address. Most of the info you want can be found there. I will one day finish writing the procedure for building the OB tanks. After you look over the info on my site if you have any further questions, don't hesitate to e-mail me. > I don't have my wing kit yet, nor the large drawings, but it sure looks to > me like you could switch the position of the tank outboard > end-ribs with the > adjacent wing nose ribs, and move the filler cap outboard to the next > chamber, and pick up about two gallons (estimated) capacity on I wouldn't go with this approach as you would either have to make a new longer IB leading edge skin or you would have a major seam on your tank. Easier to just convert the OB leading edge as a separate tank. > > From an aerodynamic standpoint, engineers say that extra fuel > carried as far > outboard as possible is beneficial to the wing spar with regard to the > bending moments and lessens stress on the spar. This is true as it improves span loading as well as stability. Unfortunately it also reduces spin recovery, but this should never be a problem with proper flight management. Hope this helps S. Todd Bartrim Turbo 13B rotary powered RV-9endurance (FWF) C-FSTB http://www3.telus.net/haywire/RV-9/C-FSTB.htm ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: DAR - Compensation?
Date: Oct 18, 2002
You guys paying $500 should really look into finding a new DAR next time. Mine was $200, and included the repairman's certificate, 50 miles of driving (each way), and a return inspection prior to Phase 2. Paul Besing RV-6A Sold (Waiting on the RV-10) http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: <Lenleg(at)aol.com> Subject: Re: RV-List: DAR - Compensation? > > Mine was $500 which he explained by saying "this also includes your > repairman's certificate ". > > Len Leggette RV-8A > N901LL (res) > Greensboro, N.C. > Ready to Fly !! > > ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: Re: DAR Listing
Date: Oct 18, 2002
Personally, I'd prefer the DAR or FAA visit be nothing but 5 minutes of paperwork. In and out, pay the fee (whatever it is), and be done with it. It's not that I don't want people looking over my plane. I do!!!! Any time; any where. Anyone who knows airplanes or RVs are encouraged to go over my plane with as much criticism as you can find. And the more you find, the happier I am. But there is a big difference between that and the DAR. With a friend, any problems found are in the legal form of recommendations. When the DAR does it, they are in the form of authority. A friend can't ground me because of some misplaced placard, or because he doesn't like where my fuel gauges are. The DAR can, and often will because of the feeling that if he doesn't write up something, he's not doing his job. That's not safety. That's just politics. I understand the intent of the law, and of course we are all obliged to deal with it. But in the real world all that good intent is lost to the moment. I'll leave the real inspections to EAA advisors, other RV pilots, and any assortment of A&Ps. Find me a DAR who will eat a burger and pencil whip my log. Thats the one I'll hire. Andy > I can understand the frustration of paying $500 for a 2 minute visit & a slip of > paper, especially if you had to wait weeks or months for the appointment. Maybe ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: DAR Listing
Date: Oct 18, 2002
Andy, Real Nice. However, maybe not the greatest idea to be throwing lines like that around, makes people wonder...If you'd like to have someone pencil whip the inspection, then what else.......????????????? Cheers, Stein Bruch RV6, Minneapolis Flying, (used an "RV" experienced DAR who actually looked at the airplane - my mistake I guess)! >>>>"Find me a DAR who will eat a burger and pencil whip my log. Thats the one I'll hire."N<<<<< Andy ________________________________________________________________________________
From: "Geoff Evans" <gwevans(at)attbi.com>
Subject: Bevel the edge?
Date: Oct 18, 2002
Regarding the elevator construction on an RV-8... The instructions say to "bevel the inboard and aft edges of E-713 locally where E-713 overlaps the spar and rib flanges to provide a smooth transition between the counterbalance skin and the E-701-R elevator skin." I can't quite figure out how doing anything to the E-713 (short of removing it) will provide a smooth transition between it and the elevator skin. Does anyone have any suggestions, or perhaps pictures? Thanks. -Geoff Evans RV-8 elevators ________________________________________________________________________________
From: "Bill" <n8wv(at)hotmail.com>
Subject: Electric C/S Props
Date: Oct 18, 2002
Anyone have any experience with electric C/S props? I have read about the MT, but don't know much else... -Bill www.vondane.com ________________________________________________________________________________
From: "Ron Calhoun" <roncal(at)earthlink.net>
Subject: DAR Listing
Date: Oct 18, 2002
I'm with Andy. When I call the FAA or DAR to inspect my plane, I know it is ready to fly because I have had my A&P and all my builder friends look it over many times. And lastly, I am the final inspector because I am the pilot and its my life on the line. The required government inspection only confirms what I aready know. Ron Calhoun RV-4 (test flight soon) ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: Electric C/S Props
Date: Oct 18, 2002
Bill, Are you unhappy with your FP Sterba Wood Prop?? Electric CS-Props are relatively rare and therefore expen$$$ive. You get more bang for the buck on hydraulic one's (Assuming you have a hollow crank). Konrad > Anyone have any experience with electric C/S props? I have read about the > MT, but don't know much else... > > -Bill > www.vondane.com > > ________________________________________________________________________________
From: "Camille Hawthorne" <cammie(at)sunvalley.net>
Subject: I need tank dimple dies
Date: Oct 18, 2002
Does anyone have a set of tank dimple dies for sale? Please respond off list to: cammie(at)sunvalley.net Camille Hawthorne RV-7 wings ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: DAR Listing
Date: Oct 18, 2002
I guess it depends on the DAR. If they are fair, they will just be another set of eyes on your plane, which is fine by me. He had a few things that he wanted me to change. Nothing nitpicky, just a couple of brain farts I had. He still signed everything off, but attached a contingency list to it. Basically, he said, "fix this stuff before you fly, but here's your certificate". I don't mind a DAR pointing things out and finding something that maybe an EAA tech counselor missed. Just another set of eyes. As long as it is done in a non-controlling fashion, I don't see a problem with it. These guys generally are very well experienced people that deserve the authority of being a DAR. This is why I would be more than happy to have them review my aircraft thoroughly than just pencil whipping the log. Paul Besing RV-6A Sold (Waiting on the RV-10) http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com> Subject: Re: RV-List: DAR Listing > > > Personally, I'd prefer the DAR or FAA visit be nothing but 5 minutes of > paperwork. In and out, pay the fee (whatever it is), and be done with it. > > It's not that I don't want people looking over my plane. I do!!!! Any > time; any where. Anyone who knows airplanes or RVs are encouraged to go > over my plane with as much criticism as you can find. And the more you > find, the happier I am. > > But there is a big difference between that and the DAR. With a friend, any > problems found are in the legal form of recommendations. When the DAR does > it, they are in the form of authority. A friend can't ground me because of > some misplaced placard, or because he doesn't like where my fuel gauges are. > The DAR can, and often will because of the feeling that if he doesn't write > up something, he's not doing his job. That's not safety. That's just > politics. > > I understand the intent of the law, and of course we are all obliged to deal > with it. But in the real world all that good intent is lost to the moment. > > I'll leave the real inspections to EAA advisors, other RV pilots, and any > assortment of A&Ps. Find me a DAR who will eat a burger and pencil whip my > log. Thats the one I'll hire. > > Andy > > > > I can understand the frustration of paying $500 for a 2 minute visit & a > slip of > > paper, especially if you had to wait weeks or months for the appointment. > Maybe > > ________________________________________________________________________________
Date: Oct 18, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: DAR - Compensation?
Paul Besing wrote: > > > He does things a little differently. For his own satisfaction, really. > What he does is signs off a phase 1 inspection. You can't sign off for > phase 2 until he comes out and does a quick look over the airplane and your > test flight data. It keeps the builders honest, I guess. It really wasn't > a burden to me, because he came out to the airport, looked over the test > flight data and logbook, glanced at the airplane for a few minutes and > signed the rest off. All without an extra fee. He is just very thorough, > and lets it get one more check before it's signed off for good. > > Paul Besing > RV-6A Sold (Waiting on the RV-10) > http://www.lacodeworks.com/besing > Kitlog Pro Builder's Log Software > http://www.kitlog.com I bet the insurance company attornys would have a field day with this DAR's inspection procedure if an accident occurred btween the initial signoff and phase two! I am constantly amazed at how DARs can "interpret" the duties that are relegated to them via the FARs................ Sam Buchanan ________________________________________________________________________________
From: "Bill" <n8wv(at)hotmail.com>
Subject: Re: Hooker seat belt installation
Date: Oct 18, 2002
I have been thinking of putting some hookers in my -8A as well... ;-) Actually, I was looking at the Simpson harnesses... Has anyone put these in an -8? How long do they need to be? I was looking at the Std. Latch & Link setup: http://www.simpsonraceproducts.com/catalog/restraints/latch.html -Bill www.vondane.com ----- Original Message ----- From: "Dean Pichon" <deanpichon(at)msn.com> Subject: Re: RV-List: Hooker seat belt installation I have a Hooker 5 point harness in my -4. I don't recall what diameter bolts are used to attach the harness. Regarding the crotch strap anchor, I built a triangular tab from .063 steel (4130) with holes the three corners. Two holes were used to attach the tab to the 2 (top) center spar bolts. These are the same bolts that hold the bracket to which control tube is attached. I can't recall whether or not I had to buy longer bolts to to accept the tab. Finally, I put a small joggle in the tab (1/4") to place the top of the tab in the proper location to receive the crotch strap. So far it works well, though it is one more thing to disassemble to get into the "stick well". Good luck Dean Pichon RV-4 Morgantown, WV >From: "Mark McGee" <riveter(at)ix.netcom.com> >Reply-To: rv-list(at)matronics.com >To: >Subject: RV-List: Hooker seat belt installation >Date: Wed, 16 Oct 2002 18:02:21 -0400 > > >I plan on installing Hooker harnesses in my RV-4 and need someone to tell >me >the mounting requirements. Specifically, what bolt diameter is used for the >seat belt and harness attachments? And what type of mounting will the >crotch >strap need? I know some builders have just provided a slot for the strap to >go through. If just a slot, how wide? > >Thanks, >Mark McGee >RV-4 fuselage, skinning ________________________________________________________________________________
From: "Randy Compton" <rdcompton(at)earthlink.net>
Subject: Ready-to-install Spinner
Date: Oct 18, 2002
Listers: Does anyone know of anyone who sells ready-to-install-on-the-airplane spinner assemblies, specifically polished aluminum ones? I bought a polished spinner which would mate to the backplate/frontplate from Van's spinner kit. When I asked about how to go about cutting out the prop blade holes I was told to use a Dremel. Well, it's pretty thick material and the cutting was MUCH easier said than done. So, here I sit with a trashed expensive polished spinner. I don't have the money to keep buying 'em as I climb the learning curve. Or, if no one knows of a factory-made assembly, if someone out there is a "pro" at fabricating spinners please contact me off-list and maybe we can work something out. Randy Compton RV-3A N84VF Gulf Breeze, FL ________________________________________________________________________________
From: "Albert Gardner" <albert.gardner(at)worldnet.att.net>
Subject: Re: Ready-to-install Spinner
Date: Oct 18, 2002
These guys http://www.sensenich.com/ make a very nice spinner to fit their props. I got one and I'm happy as a clam. I don't know if they fit any other props. Albert Gardner, Yuma, AZ RV-9A: N872RV ________________________________________________________________________________
From: "Rick Jory" <rickjory(at)msn.com>
Subject: Re: Ready-to-install Spinner
Date: Oct 18, 2002
Not that it matters . . . I bought a polished aluminum spinner from George & Becky Orndorff (sp?) and it fits Van's backplate, etc. Cutting the "cut out" for the blade (in my case, a Hartzell C/S prop) was easy . . . mainly because somewhere on the net I got a pattern and used this as a start. Needless to say, the pattern gets you the rough "size" . . . which I cut using a Dremmel and cut-off wheel . . . then "final" sizing can be done with a die grinder and 2" (or 1") scotchbrite wheels (Avery, etc.). The process is really simple and it is hard to make a mistake. Anyway, don't know a source for a spinner that is pre-cut for the prop, but what I've explained above was fairly straightforward. Good luck. Rick Jory RV8A ----- Original Message ----- From: Randy Compton <rdcompton(at)earthlink.net> Subject: RV-List: Ready-to-install Spinner > > Listers: > > Does anyone know of anyone who sells ready-to-install-on-the-airplane > spinner assemblies, specifically polished aluminum ones? > > I bought a polished spinner which would mate to the backplate/frontplate > from Van's spinner kit. When I asked about how to go about cutting out the > prop blade holes I was told to use a Dremel. Well, it's pretty thick > material and the cutting was MUCH easier said than done. So, here I sit > with a trashed expensive polished spinner. I don't have the money to keep > buying 'em as I climb the learning curve. > > Or, if no one knows of a factory-made assembly, if someone out there is a > "pro" at fabricating spinners please contact me off-list and maybe we can > work something out. > > Randy Compton > RV-3A > N84VF > Gulf Breeze, FL > > ________________________________________________________________________________
From: "Don Mack" <don(at)dmack.net>
Subject: Cutout for Van's spinner when using Sensenich 72FM series propeller
Date: Oct 18, 2002
I just ran accross this and thought it would be handy for the archives: On Sensenich's site that have added: 72FM Series Propeller spinner cut-out pattern for the Van's 13 inch spinner dome. http://www.sensenich.com/new/72fmcut.htm Don Mack RV-6A finishing don(at)dmack.net www.dmack.net ________________________________________________________________________________
Date: Oct 18, 2002
From: k moak <ken_moak(at)yahoo.com>
Subject: HS 908 question
I am having trouble visualizing the HS 908s. If I understand the drawing it is narrower in L portion (non spar side) than at the ends. Seems like the area next to the spar does not taper? Does anybody know a WEB site where I can see what this piece of angle is going to look like. Not sure the tolerance, when they give dimensions in 32s I assume it will be a tight fit later. Sorry for being so dense, I'm a little embarrassed getting stuck of assembly step 2. Any help would be appreciated. Ken Moak empennage ==== Ken Moak ken_moak(at)yahoo.com Y! Web Hosting - Let the expert host your web site http://webhosting.yahoo.com/ ________________________________________________________________________________
From: "Votuc.com" <guy(at)votuc.com>
Subject: Re: RV9-List: HS 908 question
Date: Oct 18, 2002
Here's a good picture of "attach brackets" from Tim's site http://www.deru.com/~rv9a/ ...thank s Tim.. Mine aren't that good but maybe for something else try here. . http://www.votuc.com/my_hobbys.htm Guy ----- Original Message ----- From: "k moak" <ken_moak(at)yahoo.com> Subject: RV9-List: HS 908 question > --> RV9-List message posted by: k moak > > I am having trouble visualizing the HS 908s. If I > understand the drawing it is narrower in L portion > (non spar side) than at the ends. Seems like the area > next to the spar does not taper? Does anybody know a > WEB site where I can see what this piece of angle is > going to look like. Not sure the tolerance, when they > give dimensions in 32s I assume it will be a tight fit > later. > > Sorry for being so dense, I'm a little embarrassed > getting stuck of assembly step 2. > > Any help would be appreciated. > > Ken Moak > empennage > > ==== > Ken Moak > ken_moak(at)yahoo.com > > Y! Web Hosting - Let the expert host your web site > http://webhosting.yahoo.com/ > > > > > > ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: Reminder Coastal Georgia Fall Fly In
Date: Oct 18, 2002
Hi Richard, Regretfully, I will not make it to the flyin. Went out flying today and when I got back local airport bum notice that the sidewall of my front tire on my RV-6A had been erroded to the thread by a bolt which holds wheel pants bracket to the nose wheel yoke. The wheel pant was a bit loose and I tightened the bolt two flights ago which apparent caused it to stick throught its hole in the wheel yoke sufficient to rub on the tire. None of the local FBOs have tires that small, so had to order one from Spruce but won't get it until next week. Hope your flyin is a big success and hope to make the next one. Best Regards Ed Anderson ----- Original Message ----- From: "Richard Sipp" <rsipp(at)earthlink.net> Subject: RV-List: Reminder Coastal Georgia Fall Fly In > > A quick reminder: the Coastal Georgia Fall Fly-In is Oct 19. at Eagle Neck Airpark, 1GA0. We're located on the Georgia coast half way between Savannah and St. Simons. 5 RVs on the airport. > > Please RVSP off line and we'll send you a flyer and airport briefing. > > This airpark is featured on the cover of the current General Aviation News. > > Dick & Vicki Sipp > 912 832-4813 > rsipp(at)earthlink.net > > ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Erroded Front Tire
Date: Oct 18, 2002
I thought I would pass this one to RV-6/7/9A fliers as I have not hear of anybody reporting this type of thing. I notice two flights ago that my nose gear wheel pant was a little loose, so I checked and found the 3/8" hex bolts that holds the wheel pant bracket to the aluminum nose wheel yoke to be a bit loose. So I got out my hex wrench and tightened them down a bit. Coming back from a flight today, local airport bum notice that my nose gear had a path on the sidewall where it had been erroded to the thread! On closer examination, the thread was showing all along this circular path around the tire. It appears that by tightening the hex bolt, I screwed it in sufficently far that its nose stuck out past the inside of the yoke to where it rubbed against the sidewall. It may be that the split washers had lost their tension, perhaps the bolt is 1/8" longer than it should be, or perhaps that side of the tire (tire stem side) flexed out more to make contact OR perhaps if you tighten it down enough, you too can get it to stick out the other side. The other side of the tire had no such errosion. It was not that apparently until you got down and looked at the tire closely and then its clear the tire is shot. Fortunately, the sharp eyed airport bum spotted it before I had to wrestle with the possible consequent of a blow out on touch down. So thought I would pass this on. Ed Anderson Matthews, NC RV-6A N494BW eanderson(at)carolina.rr.com ________________________________________________________________________________
Date: Oct 18, 2002
From: Jerry Springer <jsflyrv(at)earthlink.net>
Subject: Re: DAR Listing ???
John wrote: > > > Mike, > > Does that mean I can send you the documentation necessary to have my 'old' > operations limitations changed to match those published in FAA Order > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes published in > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > Basically that would be so I can make a change to the aircraft, log it, stay > in Phase 1 for 5 hours, and if all is well, make the required log entry and > not have to pay someone $500? > > As it stands right now the man in the hangar right next to mine, with the > exact airplane, having received his airworthiness certificate under the new > order, can make changes himself, but me, only 15-feet away, has to pay some > guy $500 for 'help' I don't need if we make the precise same changes. > > What's possible? Would the upcoming Experimeintal DAR that goes into effect > the first of the year or so change what would be possible? > > John at Salida, CO > n1cxo320(at)salidaco.com > John you can do that now, make the changes send a letter to FAA saying what changes you made. Why would you have to pay someone $500.00? ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Fuel Sender Leak
Date: Oct 18, 2002
Hi All, Well, now that I've been flying for a few hours, I finally have a squawck. I had a fuel smell in the cockpit when I was taxiing, I found a leak around one of my "B"nuts on the API fuel pump. Tightened it up and it went away. The residual smell in my carpet took longer, but I thought I had it licked. The last couple of days, I thought the smell was getting stronger. I searched every inch of my fuel system in the cockpit and no leaks. I was satisfied that my smell wasn't coming from inside the plane, and externally I couldn't find any indications of a leak. No blue stains, no marks on my cement floor, etc.. Tonight while I had the seat pans up to install my new comm antenna, I noticed the smell was stronger. AHA! It was coming from the outside. Well, I stuck my nose down there and determined it was coming from the right wing. Removed the right wing root fairing and guess what! Found a LEAK. Actually not a leak, not even enough to create any blue stains or drops, but definately a seap! The seap is from the very center of the fuel level sender. I have the S/W senders in my plane, and the very center is what's leaking, not my screws, etc.. So....I scratched my head for awhile, looked at one of my spare senders and determined that there is no way to "tighten" anything. The center post is tacked in when they are manufactured. What am I to do??? Well, I decided that I'll schmutz the whole thing up with some PR-1435 sealant (it cures inside wet fuel tanks) this weekend. The only thing I'll leave exposed is the brass nut to screw in the sender wire, otherwise it'll be covered in 1435. Just an FYI. I never thought THAT would leak. I more expeceted something I did to leak. Cheers, Stein Bruch RV6, Minneapolis Grounded for a day! ________________________________________________________________________________
From: "Carl Froehlich" <carlfro(at)erols.com>
Subject: Eroded Front Tire
Date: Oct 18, 2002
Ed, I just got done doing the nose gear wheel pant on my 8A last weekend. The bolt is just a little too long. I added another washer in addition to the split lock washer to solve the problem. I know - you are not supposed to add washers when using split washers but I decided to check the hex nut from time to time instead of worrying about the tire going out on me when the side wall flexes. Carl Froehlich RV-8A flying Vienna, VA -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Ed Anderson Subject: RV-List: Erroded Front Tire I thought I would pass this one to RV-6/7/9A fliers as I have not hear of anybody reporting this type of thing. I notice two flights ago that my nose gear wheel pant was a little loose, so I checked and found the 3/8" hex bolts that holds the wheel pant bracket to the aluminum nose wheel yoke to be a bit loose. So I got out my hex wrench and tightened them down a bit. Coming back from a flight today, local airport bum notice that my nose gear had a path on the sidewall where it had been erroded to the thread! On closer examination, the thread was showing all along this circular path around the tire. It appears that by tightening the hex bolt, I screwed it in sufficently far that its nose stuck out past the inside of the yoke to where it rubbed against the sidewall. It may be that the split washers had lost their tension, perhaps the bolt is 1/8" longer than it should be, or perhaps that side of the tire (tire stem side) flexed out more to make contact OR perhaps if you tighten it down enough, you too can get it to stick out the other side. The other side of the tire had no such errosion. It was not that apparently until you got down and looked at the tire closely and then its clear the tire is shot. Fortunately, the sharp eyed airport bum spotted it before I had to wrestle with the possible consequent of a blow out on touch down. So thought I would pass this on. Ed Anderson Matthews, NC RV-6A N494BW eanderson(at)carolina.rr.com ________________________________________________________________________________
From: "Robert scott" <rscott(at)johnsonmfginc.com>
Subject: Re: RV9-List: HS 908 question
Date: Oct 18, 2002
You can check out a photo of mine at http://www.myrv9a.com/hs908.htm Robert ----- Original Message ----- From: "k moak" <ken_moak(at)yahoo.com> Subject: RV9-List: HS 908 question > --> RV9-List message posted by: k moak > > I am having trouble visualizing the HS 908s. If I > understand the drawing it is narrower in L portion > (non spar side) than at the ends. Seems like the area > next to the spar does not taper? Does anybody know a > WEB site where I can see what this piece of angle is > going to look like. Not sure the tolerance, when they > give dimensions in 32s I assume it will be a tight fit > later. > > Sorry for being so dense, I'm a little embarrassed > getting stuck of assembly step 2. > > Any help would be appreciated. > > Ken Moak > empennage > > ==== > Ken Moak > ken_moak(at)yahoo.com > > Y! Web Hosting - Let the expert host your web site > http://webhosting.yahoo.com/ > > > > > ________________________________________________________________________________
From: "Curt Reimer" <cgreimer(at)mb.sympatico.ca>
Subject: Re: Aux Fuel
Date: Oct 18, 2002
> Belly tanks have been used on Pitt's for more than a quarter century. ... Loaded > with fuel, the CG point is moved very downward and with the extra 100 lbs, it > affects tracking and is very squirrelly for a plane that is normally a pussycat. Wow, a Pitts is a pussycat? What's your definition of hard - a J-85 mounted on a unicycle? :-) Curt (no Pitts time, but they do have quite a bad rap in the ground handling department) ________________________________________________________________________________
Subject: H-1 (was DAR Listing ???)
Date: Oct 19, 2002
From: "Gannon, Terence" <Terence.Gannon(at)trican.ca>
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From: "Michael Pilla" <mpilla(at)maine.rr.com>
Subject: FS: RV-4 Project (Southern Coastal Maine)
Date: Oct 19, 2002
Reluctantly, I have decided that I must sell my RV-4 project. It is at the proverbial 90% done, 90% remaining stage; i.e., all the major construction has been finished. The fuse is on the gear, wings are finished and primed, engine hung. The cowling needs to be mounted and the final mating of the wings to the fuse needs to be done. Nothing has been done on the instrument panel, but there are several instruments waiting to be placed into the panel. I have a Vision Microsystem for the RPM/Manifold/Fuel, etc. I also have two brand new orphaned Terra units: the COM and XPNDR (with Mode S mod). The starter/alternator are installed along with the battery and starter solenoids following Electric Bob's instructions. The project is located in Southern Maine, about 70 miles North of Boston or 16 miles North of Portsmouth, NH. With about three to four months of full-time effort, this -4 can be flying. There are some minor cracks (stop drilled) in the canopy (pilot/builder errors, transportation and storage in a hangar while building a house). The local EAA Tech Counselor felt that the canopy was fine, as is, especially to get flying. The new Hartzel prop may need seals checked and the AD checked since it has sat in the shipping container for a few years. Asking $28K, or best offer for plane, prop, engine (O-320-E2D overhauled at Winchester Aero and converted to a -D1A), instruments, and radios, ELT. If interested, I can send photos of the project. It will fit in a 24' U-Haul truck. The project is located in Ogunquit, ME - about 70 miles North of Boston, 16 miles North of Portsmouth, NH. Michael Pilla ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: Eroded Front Tire
Date: Oct 19, 2002
----- Original Message ----- From: "Carl Froehlich" <carlfro(at)erols.com> Subject: RE: RV-List: Eroded Front Tire > > Ed, > > I just got done doing the nose gear wheel pant on my 8A last weekend. The > bolt is just a little too long. I added another washer in addition to the > split lock washer to solve the problem. I know - you are not supposed to > add washers when using split washers but I decided to check the hex nut from > time to time instead of worrying about the tire going out on me when the > side wall flexes. > > Carl Froehlich > RV-8A flying > Vienna, VA > Hi Carl, I think the additional washer is a wise idea, certainly better than having the bolt rub against the tire. It just never occured to me that the bolt might be too long until I saw the damage it did. How is your new bird flying - as if I need to ask {:>) Ed Anderson RV-6A ________________________________________________________________________________
From: "Chris Sudlow" <sudlow77(at)earthlink.net>
Subject: Re: RV10-List: Re: posting (To Forward or Not to Forward...)
Date: Oct 19, 2002
Matt, You're doing a great job managing this. Chris ----- Original Message ----- From: "Matt Dralle" <dralle(at)matronics.com> ; ; ; ; Subject: RV10-List: Re: posting (To Forward or Not to Forward...) > --> RV10-List message posted by: dralle(at)matronics.com (Matt Dralle) > > > Kevin's right, except for the RV7, RV9, and RV10 Lists. The way its > been set up is when someone posts to the RV3, RV4, RV6, and RV8 Lists > a copy is automatically sent to the RV-List too. For some reason, the > 7/9/10 lists weren't configured that way; probably because I added > them later and forgot that about the forwarding. > > In anycase, for now I've added the forward feature the 7/9/10 Lists to keep > everything consistant. > > However, I don't have a stong preference either way, actually. I can > see pros and cons to each. Would people prefer the not-forwarding > operation? Sounds like it they might... > > So let's vote! Drop me an email at: > > dralle(at)matronics.com > > with a simple: > > "Forward" > or > "Don't Forward" > > in the Subject Line. I'll added up the votes in a couple of days and > announce the new method. > > > Matt Dralle > List Admin. > > > >-------------- > > > >Gary, > > > >Sorry, I have to respectfully disagree here. I am a member of Matt's > >RV8-list and the RV-list. If I post a message to the RV8-list, I get > >two copies - one that comes from the RV8-list, and a copy that comes > >across on the main RV-list. > > > >I just checked my Out Box - my message to Steve was sent to the > >RV4-List only. The copy you replied too seems to have come from the > >main RV-List. > > > >Search the RV-List archives for the text " New Specific RV Lists Auto > >Forwarded to RV-List" (don't include the quote marks. You'll find > >Matt's description of how the system works. I believe it causes > >confusion, because a lot of people on the main RV-List don't > >understand that they need study the original message to see where it > >originated, and send their response to the message to the correct > >list. Otherwise, the original poster may not see the response. But, > >Matt likes it the way it is, and these are his lists. > > > >Kevin > > > >> > >>Kevin.....actually, messages posted to model-specific Matronics > >>lists do not automatically post to the RV list. You can post to any > >>list or combination of lists you like, but you have to send it to > >>the ones you want it to show up on. > >> > >>Gary > >> > >>From: Kevin Horton <khorto1537(at)rogers.com> > >>Subject: Re: RV-List: Re: RV4-List: Bleeding Brakes > >> > >> > >>Steve, > >> > >>.................. Any message posted to one of the RV model specific > >>list also gets posted to the main RV List. Any responses to the copy > >>of the message that goes to the main RV List only go to the main RV > >>List - they don't go back to the RV model specific list, ............... > > > > > >-------------- > > > -- > > > Matt G. Dralle | Matronics | P.O. Box 347 | Livermore | CA | 94551 > 925-606-1001 Voice | 925-606-6281 FAX | dralle(at)matronics.com Email > http://www.matronics.com/ W.W.W. | Featuring Products For Aircraft > > > They that can give up essential liberty to obtain a little > temporary safety deserve neither liberty nor safety. > > Benjamin Franklin > Historical Review of Pennsylvania, 1759 > > ________________________________________________________________________________
From: Knicholas2(at)aol.com
Date: Oct 19, 2002
Subject: static air question
I am installing the Gretz heated pitot in my RV9. This pitot has a static air port. Van's uses ports on the mid/aft fusealge as a source for static air. My (probably dumb) question is which pitot source should I use? The fuse source is easier to troubleshoot if there is a problem yet I can also argue advantages for using the wing-pitot static source. Can/should I use both and connect the wing & fuse static air together? Thanks Kim Nicholas RV9A (I can see the light.....) Seattle ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)jetstream.net>
Subject: Spinner cut out
Date: Oct 19, 2002
I have patterns for the cut outs for Van's fiberglass spinner for the Hartzell constant speed prop (0360) if anyone would like a copy. Eustace Bowhay Blind Bay, B.C. ________________________________________________________________________________
From: "Stucklen" <wstucklen1(at)cox.net>
Subject: Erroded Front Tire (RV-6A Nose Wheel)
Date: Oct 19, 2002
Listers, this is an old problem easily corrected with washers under the head of the hex bolt.Before you install the nose section of the nose wheel pant, you should inspect for clearance between these bolts and the tire.. Fred Stucklen RV-6A N925RV 2005 Hrs of safe flying in the RV-6A From: "Ed Anderson" <eanderson(at)carolina.rr.com> Subject: RV-List: Erroded Front Tire I thought I would pass this one to RV-6/7/9A fliers as I have not hear of anybody reporting this type of thing. I notice two flights ago that my nose gear wheel pant was a little loose, so I checked and found the 3/8" hex bolts that holds the wheel pant bracket to the aluminum nose wheel yoke to be a bit loose. So I got out my hex wrench and tightened them down a bit. Coming back from a flight today, local airport bum notice that my nose gear had a path on the sidewall where it had been erroded to the thread! On closer examination, the thread was showing all along this circular path around the tire. It appears that by tightening the hex bolt, I screwed it in sufficently far that its nose stuck out past the inside of the yoke to where it rubbed against the sidewall. It may be that the split washers had lost their tension, perhaps the bolt is 1/8" longer than it should be, or perhaps that side of the tire (tire stem side) flexed out more to make contact OR perhaps if you tighten it down enough, you too can get it to stick out the other side. The other side of the tire had no such errosion. It was not that apparently until you got down and looked at the tire closely and then its clear the tire is shot. Fortunately, the sharp eyed airport bum spotted it before I had to wrestle with the possible consequent of a blow out on touch down. So thought I would pass this on. Ed Anderson Matthews, NC RV-6A N494BW eanderson(at)carolina.rr.com ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: static air question
Date: Oct 19, 2002
Good question Kim, I don't see how too many static sources could be bad in any way, as long as they are in proven locations on the airframe? Actually combining different sources of "Acceptable Locations" would give a better average/balance on static pressure, now wouldn't it?? But then, I could be way wrong on this theory. Please correct me if so!! Konrad, ABQ-NM > I am installing the Gretz heated pitot in my RV9. This pitot has a static > air port. Van's uses ports on the mid/aft fusealge as a source for static > air. My (probably dumb) question is which pitot source should I use? The > fuse source is easier to troubleshoot if there is a problem yet I can also > argue advantages for using the wing-pitot static source. Can/should I use > both and connect the wing & fuse static air together? > > Thanks > > Kim Nicholas > RV9A (I can see the light.....) > Seattle > > ________________________________________________________________________________
From: "Vincent Welch" <welchvincent(at)hotmail.com>
Subject: Re: Spinner cut out
Date: Oct 19, 2002
Is this the same pattern for a Hartzell with an IO-360? If so, I would love one. Thanks, Vince >From: "Eustace Bowhay" <ebowhay(at)jetstream.net> >Reply-To: rv-list(at)matronics.com >To: "rv list" >Subject: RV-List: Spinner cut out >Date: Sat, 19 Oct 2002 08:51:49 -0700 > > >I have patterns for the cut outs for Van's fiberglass spinner for the >Hartzell constant speed prop (0360) if anyone would like a copy. > >Eustace Bowhay Blind Bay, B.C. > > Internet access plans that fit your lifestyle -- join MSN. http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
Date: Oct 19, 2002
rv7-list(at)matronics.com, rv8-list(at)matronics.com, rv9-list(at)matronics.com, rv10-list(at)matronics.com
From: Matt Dralle <dralle(at)matronics.com>
Subject: Re: posting (To Forward or Not to Forward...)
Thanks Scott! The votes are still trickling in and its a REALLY, REALLY close race. If you have a preference and haven't yet voted, it so close that one or two votes could actually make the difference. PLEASE only vote once, though! To be fair, multiple votes from the same email address will not be counted. Matt At 07:07 AM 10/19/2002 Saturday, you wrote: > >Matt, > >You're doing a great job managing this. > >Chris >----- Original Message ----- >From: "Matt Dralle" <dralle(at)matronics.com> >Subject: RV-List: Re: posting (To Forward or Not to Forward...) > > > > --> RV10-List message posted by: dralle(at)matronics.com (Matt Dralle) > > > > > > Kevin's right, except for the RV7, RV9, and RV10 Lists. The way its > > been set up is when someone posts to the RV3, RV4, RV6, and RV8 Lists > > a copy is automatically sent to the RV-List too. For some reason, the > > 7/9/10 lists weren't configured that way; probably because I added > > them later and forgot that about the forwarding. > > > > In anycase, for now I've added the forward feature the 7/9/10 Lists to >keep > > everything consistant. > > > > However, I don't have a stong preference either way, actually. I can > > see pros and cons to each. Would people prefer the not-forwarding > > operation? Sounds like it they might... > > > > So let's vote! Drop me an email at: > > > > dralle(at)matronics.com > > > > with a simple: > > > > "Forward" > > or > > "Don't Forward" > > > > in the Subject Line. I'll added up the votes in a couple of days and > > announce the new method. > > > > > > Matt Dralle > > List Admin. > > > > > > >-------------- > > > > > >Gary, > > > > > >Sorry, I have to respectfully disagree here. I am a member of Matt's > > >RV8-list and the RV-list. If I post a message to the RV8-list, I get > > >two copies - one that comes from the RV8-list, and a copy that comes > > >across on the main RV-list. > > > > > >I just checked my Out Box - my message to Steve was sent to the > > >RV4-List only. The copy you replied too seems to have come from the > > >main RV-List. > > > > > >Search the RV-List archives for the text " New Specific RV Lists Auto > > >Forwarded to RV-List" (don't include the quote marks. You'll find > > >Matt's description of how the system works. I believe it causes > > >confusion, because a lot of people on the main RV-List don't > > >understand that they need study the original message to see where it > > >originated, and send their response to the message to the correct > > >list. Otherwise, the original poster may not see the response. But, > > >Matt likes it the way it is, and these are his lists. > > > > > >Kevin > > > > > >> > > >>Kevin.....actually, messages posted to model-specific Matronics > > >>lists do not automatically post to the RV list. You can post to any > > >>list or combination of lists you like, but you have to send it to > > >>the ones you want it to show up on. > > >> > > >>Gary > > >> > > >>From: Kevin Horton <khorto1537(at)rogers.com> > > >>Subject: Re: RV-List: Re: RV4-List: Bleeding Brakes > > >> > > >> > > >>Steve, > > >> > > >>.................. Any message posted to one of the RV model specific > > >>list also gets posted to the main RV List. Any responses to the copy > > >>of the message that goes to the main RV List only go to the main RV > > >>List - they don't go back to the RV model specific list, ............... > > > > > > ________________________________________________________________________________
From: Knicholas2(at)aol.com
Date: Oct 19, 2002
Subject: routing the static tubing
I asked earlier about static sources in the aft. fuse (per Van's plans) and in the heated pitot tube. Thanks for the great input. I plan to tie together the static lines from the aft fuse and the heated pitot tube. The next question - when you guys run the static tubing from teh aft fuse, thru the bulkheads and along the pilot side cockpit to the panel, are you somehow stuffing the tube up under the longeron out of sight or just let it stay visable on the bottom of the longeron. If you are stuffing it up under the U shape channel, how are you keeping it there? ...so full of questions, so few answers... Kim Nicholas RV9A Seattle ________________________________________________________________________________
From: Knicholas2(at)aol.com
Date: Oct 19, 2002
Subject: forward
forward ________________________________________________________________________________
From: Smcm75(at)aol.com
Date: Oct 19, 2002
Subject: Re: Aux Fuel
In a message dated 10/19/02 10:35:43 AM Eastern Daylight Time, n5lp(at)carlsbad.net writes: > I have also found that the horror stories, almost invariably, come from > people that have not flown the airplane they are talking about. > Larry you speaketh the truth. Scott Morrow RV-6A 90% ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: static air question
Date: Oct 19, 2002
The more ports you use, the higher probability that you will have a leak in the system. I believe Piper also uses one on each side to balance the static pressure but adding a 3rd just adds weight without benefit. ----- Original Message ----- From: "Konrad Werner" <Connywerner(at)wans.net> Subject: Re: RV-List: static air question > > Good question Kim, > > I don't see how too many static sources could be bad in any way, as long as > they are in proven locations on the airframe? > Actually combining different sources of "Acceptable Locations" would give a > better average/balance on static pressure, now wouldn't it?? > But then, I could be way wrong on this theory. Please correct me if so!! > > Konrad, > ABQ-NM > > > > I am installing the Gretz heated pitot in my RV9. This pitot has a static > > air port. Van's uses ports on the mid/aft fusealge as a source for static > > air. My (probably dumb) question is which pitot source should I use? > The > > fuse source is easier to troubleshoot if there is a problem yet I can > also > > argue advantages for using the wing-pitot static source. Can/should I use > > both and connect the wing & fuse static air together? > > > > Thanks > > > > Kim Nicholas > > RV9A (I can see the light.....) > > Seattle > > > > > > ________________________________________________________________________________
From: DanJE(at)aol.com
Date: Oct 19, 2002
Subject: Re: RV6-List Digest: 2 Msgs - 10/18/02
Stan: RV-6 fuel leaks.... I've got one... I've got one rivet just in front of the right spar, about half way out the fuel tank, that seeps a bit of blue fuel all the time. A friend who's building an RV-6 in a pack of RV-6 builder/owners at Denver's Front Range Airport (See his web site: Singer's RV-6A ) suggests using a special version of Loctite. I forgot the specific number of the product, but I think its called Loctite C, or maybe B? Whatever, its very rare, hard to find. You have to go to those real industrial quality hardware stores to find it. I had a web site for it, but dumped it after I found it and bought it. Here's the important clue: Its GREEN. Loctite makes it just for seeping leaks and for holding screws and things that are already assembled. Its very very thin fluid, (not viscous or gummy at all) and can seep UP into bolt threads, loose rivets, tiny crevices, by capillary action. And, it works fine in an oily or fuel environment. It does seal up fuel leaks! As long as they are tiny seeps around things with very small openings. It can seal UP (against gravity) because it works by capillary action. Good stuff. But... very expensive! I think I paid about $7 for a very tiny plastic bottle of about 1/2 oz. That's the good news. Now, my bad news: I have been daubing the green loctite on that leaking rivet for a couple of weeks now, (about once a week), and it sucks right up around that rivet. But... I'm thinking it must be just getting washed away on the inside of the tank, or diluted with wet fuel, because its not doing anything to stop the leak, so far... Perhaps I'll have to drain the tank first, let it dry, and then do the locktite application to the bad rivet. That will no doubt allow the loctite to suck up, fill in the gaps around the rivet, and solidify and DRY. Then I'll be done with the leak. Dan Eikleberry Las Vegas .. RV-6 flying. ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: RV6-List Digest: 2 Msgs - 10/18/02
Date: Oct 19, 2002
PRODUCT DESCRIPTION LOCTITE Product 990 is a low viscosity, anaerobic sealant designed especially for wicking applications. It has the ability to penetrate porosities and cracks by capillary action, filling voids as large as .005". This sealant hardens by polymerization into a tough thermoset plastic, only when confined between surfaces such as a pore. Sealant exposed to air will remain liquid and is removed by washing with organic solvents or water based industrial wash solutions. Pressures and fluids may be retained, as well as corrosion or contamination eliminated. The sealant is suitable for continuous service at 300F. Typical weldments and castings can be sealed to their rupture pressure. Experience has shown that thin walled members exposed to temperatures above 225F and pressure cycling above 250 psig must be evaluated on an individual basis. This product withstands temperatures ranging from -65F to 400F. Parts may reach 400F intermittently without affecting the sealability of the sealant. Application of Sealant Sealant is applied directly to prepared surfaces. Metal temperature may range from 60F to 140F. Higher temperatures will open porosities, reduce the viscosity and speed up the cure. Brushing is the easiest and most economical means of application. 3 ml's (cc's) of sealant are required to seal 100 linear inches of weld when using a 1/2" brush. Manual or fully automatic spray equipment is available from Loctite Corporation for high production requirements. Loctite sealants cure between any metallic surface. PROPERTIES OF UNCURED MATERIAL Typical Value Chemical Type Dimethacrylate Appearance Clear tan Viscosity, Cannon Fenske #150 @ 25C, cP 11 - 20 Specific Gravity 1.07 Flash Point, COC, F >200 TYPICAL PROPERTIES OF CURED MATERIAL Coefficient of Thermal Expansion ASTM D 696, in/in/C 10-4 Product 990 is recommended for inactive surfaces, such as zinc or aluminum. It can also be used on iron or steel surfaces. However, its rapid cure speed may not allow for total penetration into porosity. Surface Preparation All surfaces must be free of dirt and excessive oil. If cleaning is necessary, only non-greasing solvents should be used. Cure Rate Adhesive should be allowed to cure to 50% strength before further processing or testing. Application to non-metallic surfaces may require heat curing. From www.loctite.com ----- Original Message ----- From: <DanJE(at)aol.com> Subject: RV-List: Re: RV6-List Digest: 2 Msgs - 10/18/02 > > Stan: > RV-6 fuel leaks.... I've got one... > I've got one rivet just in front of the right spar, about half way out the > fuel tank, that seeps a bit of blue fuel all the time. > > A friend who's building an RV-6 in a pack of RV-6 builder/owners at > Denver's Front Range Airport (See his web site:
Singer's RV-6A ) suggests > using a special version of Loctite. I forgot the specific number of the > product, but I think its called Loctite C, or maybe B? Whatever, its very > rare, hard to find. You have to go to those real industrial quality hardware > stores to find it. I had a web site for it, but dumped it after I found it > and bought it. > > Here's the important clue: Its GREEN. Loctite makes it just for seeping > leaks and for holding screws and things that are already assembled. Its very > very thin fluid, (not viscous or gummy at all) and can seep UP into bolt > threads, loose rivets, tiny crevices, by capillary action. And, it works > fine in an oily or fuel environment. It does seal up fuel leaks! As long as > they are tiny seeps around things with very small openings. It can seal UP > (against gravity) because it works by capillary action. Good stuff. But... > very expensive! I think I paid about $7 for a very tiny plastic bottle of > about 1/2 oz. > > That's the good news. Now, my bad news: I have been daubing the green > loctite on that leaking rivet for a couple of weeks now, (about once a week), > and it sucks right up around that rivet. But... I'm thinking it must be just > getting washed away on the inside of the tank, or diluted with wet fuel, > because its not doing anything to stop the leak, so far... Perhaps I'll > have to drain the tank first, let it dry, and then do the locktite > application to the bad rivet. That will no doubt allow the loctite to suck > up, fill in the gaps around the rivet, and solidify and DRY. Then I'll be > done with the leak. > > Dan Eikleberry > Las Vegas .. RV-6 flying. > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: RV6-List Digest: 2 Msgs - 10/18/02
Date: Oct 19, 2002
Maybe since it does not want air to set... apply and then cover with clear tape to exclude air. Might be helpful as you say to lower the fuel level below the rivet. Might raise or lower tail or block up a wheel to move the fuel level and reduce the pressure. ----- Original Message ----- From: <DanJE(at)aol.com> Subject: RV-List: Re: RV6-List Digest: 2 Msgs - 10/18/02 > > Stan: > RV-6 fuel leaks.... I've got one... > I've got one rivet just in front of the right spar, about half way out the > fuel tank, that seeps a bit of blue fuel all the time. > > A friend who's building an RV-6 in a pack of RV-6 builder/owners at > Denver's Front Range Airport (See his web site:
Singer's RV-6A ) suggests > using a special version of Loctite. I forgot the specific number of the > product, but I think its called Loctite C, or maybe B? Whatever, its very > rare, hard to find. You have to go to those real industrial quality hardware > stores to find it. I had a web site for it, but dumped it after I found it > and bought it. > > Here's the important clue: Its GREEN. Loctite makes it just for seeping > leaks and for holding screws and things that are already assembled. Its very > very thin fluid, (not viscous or gummy at all) and can seep UP into bolt > threads, loose rivets, tiny crevices, by capillary action. And, it works > fine in an oily or fuel environment. It does seal up fuel leaks! As long as > they are tiny seeps around things with very small openings. It can seal UP > (against gravity) because it works by capillary action. Good stuff. But... > very expensive! I think I paid about $7 for a very tiny plastic bottle of > about 1/2 oz. > > That's the good news. Now, my bad news: I have been daubing the green > loctite on that leaking rivet for a couple of weeks now, (about once a week), > and it sucks right up around that rivet. But... I'm thinking it must be just > getting washed away on the inside of the tank, or diluted with wet fuel, > because its not doing anything to stop the leak, so far... Perhaps I'll > have to drain the tank first, let it dry, and then do the locktite > application to the bad rivet. That will no doubt allow the loctite to suck > up, fill in the gaps around the rivet, and solidify and DRY. Then I'll be > done with the leak. > > Dan Eikleberry > Las Vegas .. RV-6 flying. > > ________________________________________________________________________________
From: "John" <n1cxo320(at)salidaco.com>
Subject: Re: DAR Listing ???
Date: Oct 19, 2002
Because basically your have to have the PERMISSION to make the change from the FSDO or a DAR. If you have the newer operations limitations you just do the change, log it, go to Phase 1 for 5 hours, and if all is well, just make the required log entry. With the old limitations you CANNOT just 'do it' - what ever happened to equal treatment under the law??? The DARs want to do a full plane inspection - just as if it had never been inspected and charge for the whole ball of wax, even though, as you point out, it is merely a paper work exercise. John at Salida, CO ----- Original Message ----- From: "Jerry Springer" <jsflyrv(at)earthlink.net> Subject: Re: RV-List: DAR Listing ??? > > John wrote: > > > > > > Mike, > > > > Does that mean I can send you the documentation necessary to have my 'old' > > operations limitations changed to match those published in FAA Order > > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes published in > > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > > > Basically that would be so I can make a change to the aircraft, log it, stay > > in Phase 1 for 5 hours, and if all is well, make the required log entry and > > not have to pay someone $500? > > > > As it stands right now the man in the hangar right next to mine, with the > > exact airplane, having received his airworthiness certificate under the new > > order, can make changes himself, but me, only 15-feet away, has to pay some > > guy $500 for 'help' I don't need if we make the precise same changes. > > > > What's possible? Would the upcoming Experimeintal DAR that goes into effect > > the first of the year or so change what would be possible? > > > > John at Salida, CO > > n1cxo320(at)salidaco.com > > > > John you can do that now, make the changes send a letter to FAA saying what > changes you made. Why would you have to pay someone $500.00? > > ________________________________________________________________________________
From: "Ken Stribling" <ken(at)soundsuckers.com>
Subject: Re: not forward
Date: Oct 19, 2002
> > > > > > ________________________________________________________________________________
Date: Oct 19, 2002
From: Jerry Springer <jsflyrv(at)earthlink.net>
Subject: Re: DAR Listing ???
My OL issued in 1989 just says FAA must be notified and their response received in writing. I suppose it is up to the individual if they want to do a complete inspection again. If you change your prop does that mean you are going to pay some guy for a complete inspection again? From what I understand that would be a major change and require a letter to FAA and a response from them in writing under old limitations. I wonder how many homebuilts of any kind out there have had changes such as prop change without notifying anyone? To take it a step farther I wonder how many engines have been changed from say an O-320 to an O-360 under old limitations without anyone being notified? It goes without saying this would make insurance people unhappy I am sure. I wish FAA had just grand fathered in all of the OLs and made them all the same. Jerry John wrote: > > > Because basically your have to have the PERMISSION to make the change from > the FSDO or a DAR. If you have the newer operations limitations you just do > the change, log it, go to Phase 1 for 5 hours, and if all is well, just make > the required log entry. With the old limitations you CANNOT just 'do it' - > what ever happened to equal treatment under the law??? The DARs want to do a > full plane inspection - just as if it had never been inspected and charge > for the whole ball of wax, even though, as you point out, it is merely a > paper work exercise. > > John at Salida, CO > > ----- Original Message ----- > From: "Jerry Springer" <jsflyrv(at)earthlink.net> > To: > Subject: Re: RV-List: DAR Listing ??? > > > > > John wrote: > > > > > > > > > Mike, > > > > > > Does that mean I can send you the documentation necessary to have my > 'old' > > > operations limitations changed to match those published in FAA Order > > > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes published > in > > > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > > > > > Basically that would be so I can make a change to the aircraft, log it, > stay > > > in Phase 1 for 5 hours, and if all is well, make the required log entry > and > > > not have to pay someone $500? > > > > > > As it stands right now the man in the hangar right next to mine, with > the > > > exact airplane, having received his airworthiness certificate under the > new > > > order, can make changes himself, but me, only 15-feet away, has to pay > some > > > guy $500 for 'help' I don't need if we make the precise same changes. > > > > > > What's possible? Would the upcoming Experimeintal DAR that goes into > effect > > > the first of the year or so change what would be possible? > > > > > > John at Salida, CO > > > n1cxo320(at)salidaco.com > > > > > > > John you can do that now, make the changes send a letter to FAA saying > what > > changes you made. Why would you have to pay someone $500.00? > > > > > ________________________________________________________________________________
From: "Sally and George" <aeronut58(at)hotmail.com>
Subject: Re: RV6-List Digest: 2 Msgs - 10/18/02
Date: Oct 19, 2002
Dan: The stuff you want is called Loctite Threadlocker Green. It's available at Auto Zone or other auto parts stores for about $5.00. You must drain the fuel tank before using it. It helps to apply a pool of the stuff under the weeping rivet and allow it to suck up over a period of abou 24 hours. I used flattened modellling clay,and put a cavity in it with the head of an AN5 bolt. I filled the cavity with Threadlocker Green and applied it to the rivet, then held it in place with duct tape. After 24 hours it is cured and will stop small leaks. It won't work for large ones. For large leaks, you'll neet to remove the tank, drill out the rivet and replace it with lots of tank sealer. George Kilishek RV-8 N888GK > > Stan: > > RV-6 fuel leaks.... I've got one... > > I've got one rivet just in front of the right spar, about half way out >the > > fuel tank, that seeps a bit of blue fuel all the time. > > > > A friend who's building an RV-6 in a pack of RV-6 builder/owners at > > Denver's Front Range Airport (See his web site:
HREF="http://www.jgsinger.com/rv">Singer's RV-6A ) suggests > > using a special version of Loctite. I forgot the specific number of the > > product, but I think its called Loctite C, or maybe B? Whatever, its >very > > rare, hard to find. You have to go to those real industrial quality >hardware > > stores to find it. I had a web site for it, but dumped it after I found >it > > and bought it. > > > > Here's the important clue: Its GREEN. Loctite makes it just for seeping > > leaks and for holding screws and things that are already assembled. Its >very > > very thin fluid, (not viscous or gummy at all) and can seep UP into bolt > > threads, loose rivets, tiny crevices, by capillary action. And, it >works > > fine in an oily or fuel environment. It does seal up fuel leaks! As >long >as > > they are tiny seeps around things with very small openings. It can seal >UP > > (against gravity) because it works by capillary action. Good stuff. >But... > > very expensive! I think I paid about $7 for a very tiny plastic bottle >of > > about 1/2 oz. > > > > That's the good news. Now, my bad news: I have been daubing the >green > > loctite on that leaking rivet for a couple of weeks now, (about once a >week), > > and it sucks right up around that rivet. But... I'm thinking it must be >just > > getting washed away on the inside of the tank, or diluted with wet fuel, > > because its not doing anything to stop the leak, so far... Perhaps >I'll > > have to drain the tank first, let it dry, and then do the locktite > > application to the bad rivet. That will no doubt allow the loctite to >suck > > up, fill in the gaps around the rivet, and solidify and DRY. Then I'll >be > > done with the leak. > > > > Dan Eikleberry > > Las Vegas .. RV-6 flying. > > > > > > Protect your PC - get McAfee.com VirusScan Online http://clinic.mcafee.com/clinic/ibuy/campaign.asp?cid=3963 ________________________________________________________________________________
From: "Dave Stewart" <davestewart(at)globalserve.net>
Subject: Re: routing the static tubing
Date: Oct 19, 2002
Kim Make a few clips (see static attach detail dwg 25) that rivet through longeron and keep line level along its run. Dave ----- Original Message ----- From: <Knicholas2(at)aol.com> Subject: RV-List: routing the static tubing > > I asked earlier about static sources in the aft. fuse (per Van's plans) and > in the heated pitot tube. Thanks for the great input. I plan to tie together > the static lines from the aft fuse and the heated pitot tube. > > The next question - when you guys run the static tubing from teh aft fuse, > thru the bulkheads and along the pilot side cockpit to the panel, are you > somehow stuffing the tube up under the longeron out of sight or just let it > stay visable on the bottom of the longeron. If you are stuffing it up under > the U shape channel, how are you keeping it there? > > ...so full of questions, so few answers... > > Kim Nicholas > RV9A > Seattle > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: DAR Listing ???
Date: Oct 19, 2002
Jerry, Just go to the FAA and have them give you the new limitations. Some say you win, some say you lose a bit. The FSDO might want to inspect your airplane. Strike that! Might want to look at your airplane, but since there is no urgency, they should be able to do it when they get around to it. If they won't, then stick with what you have until the VDARs come around. (Voluntary DAR) EAA is working on it and it is in the wings. You haven't had a problem with the old OLs since 1989, a few months more should not give you any heart-burn. Cy Galley Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org ----- Original Message ----- From: "Jerry Springer" <jsflyrv(at)earthlink.net> Subject: Re: RV-List: DAR Listing ??? > > My OL issued in 1989 just says FAA must be notified and their response > received in writing. I suppose it is up to the individual if they want to > do a complete inspection again. If you change your prop does that mean you > are going to pay some guy for a complete inspection again? From what > I understand that would be a major change and require a letter to FAA and > a response from them in writing under old limitations. I wonder how many > homebuilts of any kind out there have had changes such as prop change without > notifying anyone? To take it a step farther I wonder how many engines have > been changed from say an O-320 to an O-360 under old limitations without > anyone being notified? It goes without saying this would make insurance > people unhappy I am sure. I wish FAA had just grand fathered in all of the > OLs and made them all the same. > > Jerry > > John wrote: > > > > > > Because basically your have to have the PERMISSION to make the change from > > the FSDO or a DAR. If you have the newer operations limitations you just do > > the change, log it, go to Phase 1 for 5 hours, and if all is well, just make > > the required log entry. With the old limitations you CANNOT just 'do t' - > > what ever happened to equal treatment under the law??? The DARs want to do a > > full plane inspection - just as if it had never been inspected and charge > > for the whole ball of wax, even though, as you point out, it is merely a > > paper work exercise. > > > > John at Salida, CO > > > > ----- Original Message ----- > > From: "Jerry Springer" <jsflyrv(at)earthlink.net> > > To: > > Subject: Re: RV-List: DAR Listing ??? > > > > > > > > John wrote: > > > > > > > > > > > > Mike, > > > > > > > > Does that mean I can send you the documentation necessary to have my > > 'old' > > > > operations limitations changed to match those published in FAA Order > > > > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes published > > in > > > > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > > > > > > > Basically that would be so I can make a change to the aircraft, log it, > > stay > > > > in Phase 1 for 5 hours, and if all is well, make the required log entry > > and > > > > not have to pay someone $500? > > > > > > > > As it stands right now the man in the hangar right next to mine, with > > the > > > > exact airplane, having received his airworthiness certificate under the > > new > > > > order, can make changes himself, but me, only 15-feet away, has to pay > > some > > > > guy $500 for 'help' I don't need if we make the precise same changes. > > > > > > > > What's possible? Would the upcoming Experimeintal DAR that goes into > > effect > > > > the first of the year or so change what would be possible? > > > > > > > > John at Salida, CO > > > > n1cxo320(at)salidaco.com > > > > > > > > > > John you can do that now, make the changes send a letter to FAA saying > > what > > > changes you made. Why would you have to pay someone $500.00? > > > > > > > > > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: DAR Listing ???
Date: Oct 19, 2002
One of our chapter members just wrote our FSDO for permission to change rudder peddles from bottom mount to hanging type on his RV-6 He has the old OL and they wrote back and said it was fine with them. If I remember they even treated it as a minor alteration so he didn't have to re-inspect. Good figure. ----- Original Message ----- From: "John" <n1cxo320(at)salidaco.com> Subject: Re: RV-List: DAR Listing ??? > > Because basically your have to have the PERMISSION to make the change from > the FSDO or a DAR. If you have the newer operations limitations you just do > the change, log it, go to Phase 1 for 5 hours, and if all is well, just make > the required log entry. With the old limitations you CANNOT just 'do t' - > what ever happened to equal treatment under the law??? The DARs want to do a > full plane inspection - just as if it had never been inspected and charge > for the whole ball of wax, even though, as you point out, it is merely a > paper work exercise. > > > John at Salida, CO > > > ----- Original Message ----- > From: "Jerry Springer" <jsflyrv(at)earthlink.net> > To: > Subject: Re: RV-List: DAR Listing ??? > > > > > > John wrote: > > > > > > > > > Mike, > > > > > > Does that mean I can send you the documentation necessary to have my > 'old' > > > operations limitations changed to match those published in FAA Order > > > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes published > in > > > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > > > > > Basically that would be so I can make a change to the aircraft, log it, > stay > > > in Phase 1 for 5 hours, and if all is well, make the required log entry > and > > > not have to pay someone $500? > > > > > > As it stands right now the man in the hangar right next to mine, with > the > > > exact airplane, having received his airworthiness certificate under the > new > > > order, can make changes himself, but me, only 15-feet away, has to pay > some > > > guy $500 for 'help' I don't need if we make the precise same changes. > > > > > > What's possible? Would the upcoming Experimeintal DAR that goes into > effect > > > the first of the year or so change what would be possible? > > > > > > John at Salida, CO > > > n1cxo320(at)salidaco.com > > > > > > > John you can do that now, make the changes send a letter to FAA saying > what > > changes you made. Why would you have to pay someone $500.00? > > > > > > ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: Erroded Front Tire (RV-6A Nose Wheel)
Date: Oct 19, 2002
----- Original Message ----- From: "Stucklen" <wstucklen1(at)cox.net> Subject: RV-List: Erroded Front Tire (RV-6A Nose Wheel) > > Listers, > > this is an old problem easily corrected with washers under the head of the hex bolt.Before you install the nose section of the nose wheel pant, you should inspect for clearance between these bolts and the tire.. > > Fred Stucklen > RV-6A N925RV > 2005 Hrs of safe flying in the RV-6A > > Ok, thanks, Fred I had not heard about it before and could find nothing in the archives when I searched there. Checking is clearly the prudent thing to do and adding a washer where necessary. Ed Anderson ________________________________________________________________________________
From: "Doug Weiler" <dougweil(at)pressenter.com>
Subject: Re: RV6-List Digest: 2 Msgs - 10/18/02
Date: Oct 19, 2002
> > Maybe since it does not want air to set... apply and then cover with clear > tape to exclude air. Might be helpful as you say to lower the fuel level > below the rivet. Might raise or lower tail or block up a wheel to move the > fuel level and reduce the pressure. > ----- Original Message ----- > From: <DanJE(at)aol.com> > To: > Subject: RV-List: Re: RV6-List Digest: 2 Msgs - 10/18/02 > Hi Guys: Do you think this version of Locktite may stop a slowly seeping brake fitting on my RV-4. It is the brass fittings screwed into the aluminum master cylinders. I am about ready to remove the brass fittings and install AN fittings, but maybe this might work. Doug Weiler Hudson, WI ________________________________________________________________________________
From: TColeE(at)aol.com
Date: Oct 19, 2002
Subject: Re: RV10-List: Re: posting (To Forward or Not to Forward...)
forward Terry E. Cole ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Hung Up Flop Tube Previously RV Glider
Date: Oct 19, 2002
Some of you may recall my episode where I could not use the last 3 gallons or so of fuel from my right tank which has a flop tube installed. I concluded that the flop tube must have hung up on a lightening hole or some other obstruction which kept the end suspended approx 2 1/2" above the bottom of the tank. Well, today, I took the tank off the wing being careful not to disturb the flop tube as I wanted to see what it was hung up on. Well, much to my surprise when I unscrewed and opened up the access plate, the flop tube was laying exactly where it should be. Further I had never cut a lightening hole in that bays ribs which I thought it might have hung upon, plus I had all the guards that Van's recommends for the flop tube tank (I had forgotten the details over the past 6 years). Well, I was really perplexed in that the flop tube was not hung up on anything and reached in and grabbed the flop tube and much to my surprise it came out the access door in my hand! The flop tube had not hung up, the flare nut holding to the bulkhead fitting had come unscrewed. The only thing I can conclude (as I flew approx 150 hours before having the fuel problem) is that I must have not torque it on sufficiently and the vibration eventually loosened and unscrewed the flare nut and flop tube. So I was only picking fuel up that rose as high as the bulkhead fitting. So flop tube fitting is torque firmly and hopefully finally. Best Regards Ed Anderson Ed Anderson Matthews, NC RV-6A N494BW eanderson(at)carolina.rr.com ________________________________________________________________________________
Date: Oct 19, 2002
From: "Harry Hawkins" <hawkbud(at)mail.speednetllc.com>
Subject: Re: RV6-List: Fuel Sender Leak
3M makes a product called "structural adhesive" p/n 08101. it would seal your mother in laws mouth. Work fast it has only two minutes till it hardens. You will like it for gas leaks. ---------- Original Message ---------------------------------- From: "Stein Bruch" <stein(at)steinair.com> Date: Fri, 18 Oct 2002 21:37:56 -0500 >--> RV6-List message posted by: "Stein Bruch" > >Hi All, > >Well, now that I've been flying for a few hours, I finally have a squawck. >I had a fuel smell in the cockpit when I was taxiing, I found a leak around >one of my "B"nuts on the API fuel pump. Tightened it up and it went away. >The residual smell in my carpet took longer, but I thought I had it licked. >The last couple of days, I thought the smell was getting stronger. I >searched every inch of my fuel system in the cockpit and no leaks. I was >satisfied that my smell wasn't coming from inside the plane, and externally >I couldn't find any indications of a leak. No blue stains, no marks on my >cement floor, etc.. > >Tonight while I had the seat pans up to install my new comm antenna, I >noticed the smell was stronger. AHA! It was coming from the outside. >Well, I stuck my nose down there and determined it was coming from the right >wing. Removed the right wing root fairing and guess what! Found a LEAK. >Actually not a leak, not even enough to create any blue stains or drops, but >definately a seap! The seap is from the very center of the fuel level >sender. I have the S/W senders in my plane, and the very center is what's >leaking, not my screws, etc.. > >So....I scratched my head for awhile, looked at one of my spare senders and >determined that there is no way to "tighten" anything. The center post is >tacked in when they are manufactured. What am I to do??? Well, I decided >that I'll schmutz the whole thing up with some PR-1435 sealant (it cures >inside wet fuel tanks) this weekend. The only thing I'll leave exposed is >the brass nut to screw in the sender wire, otherwise it'll be covered in >1435. > >Just an FYI. I never thought THAT would leak. I more expeceted something I >did to leak. > >Cheers, >Stein Bruch >RV6, Minneapolis >Grounded for a day! > > ________________________________________________________________________________
Date: Oct 19, 2002
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: DAR Listing ???
You can get your old op lims changed to the new ones by calling the fsdo & explaining what you want, then taking your old op lims to them along with the completed application they mailed to you. They then issue the new paperwork in the office. Been there, done that with an RV-4 built in '92. If the fsdo resists, call EAA & ask for their assistance in educating the guys at the fsdo. Charlie John wrote: > > > Because basically your have to have the PERMISSION to make the change from > the FSDO or a DAR. If you have the newer operations limitations you just do > the change, log it, go to Phase 1 for 5 hours, and if all is well, just make > the required log entry. With the old limitations you CANNOT just 'do it' - > what ever happened to equal treatment under the law??? The DARs want to do a > full plane inspection - just as if it had never been inspected and charge > for the whole ball of wax, even though, as you point out, it is merely a > paper work exercise. > > John at Salida, CO > > ----- Original Message ----- > From: "Jerry Springer" <jsflyrv(at)earthlink.net> > To: > Subject: Re: RV-List: DAR Listing ??? > > > > > John wrote: > > > > > > > > > Mike, > > > > > > Does that mean I can send you the documentation necessary to have my > 'old' > > > operations limitations changed to match those published in FAA Order > > > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes published > in > > > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > > > > > Basically that would be so I can make a change to the aircraft, log it, > stay > > > in Phase 1 for 5 hours, and if all is well, make the required log entry > and > > > not have to pay someone $500? > > > > > > As it stands right now the man in the hangar right next to mine, with > the > > > exact airplane, having received his airworthiness certificate under the > new > > > order, can make changes himself, but me, only 15-feet away, has to pay > some > > > guy $500 for 'help' I don't need if we make the precise same changes. > > > > > > What's possible? Would the upcoming Experimeintal DAR that goes into > effect > > > the first of the year or so change what would be possible? > > > > > > John at Salida, CO > > > n1cxo320(at)salidaco.com > > > > > > > John you can do that now, make the changes send a letter to FAA saying > what > > changes you made. Why would you have to pay someone $500.00? > > > > ________________________________________________________________________________
Date: Oct 19, 2002
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: static air question
Konrad Werner wrote: > see below... > > Good question Kim, > > I don't see how too many static sources could be bad in any way, as long as > they are in proven locations on the airframe? > Actually combining different sources of "Acceptable Locations" would give a > better average/balance on static pressure, now wouldn't it?? > But then, I could be way wrong on this theory. Please correct me if so!! > > Konrad, > ABQ-NM > > > I am installing the Gretz heated pitot in my RV9. This pitot has a static > > air port. Van's uses ports on the mid/aft fusealge as a source for static > > air. My (probably dumb) question is which pitot source should I use? > The > > fuse source is easier to troubleshoot if there is a problem yet I can > also > > argue advantages for using the wing-pitot static source. Can/should I use > > both and connect the wing & fuse static air together? > > > > Thanks > > > > Kim Nicholas > > RV9A (I can see the light.....) > > Seattle > > > > > Konrad, On my RV-4 with 2 flush static ports in Van's recommended fuse. location, I had ~ 10 kt (slow) error in indicated airspeed at cruise & ~ 150 ft (low) indicated altitude at full speed. If you are wondering how I knew, the alt. was set to field elevation & indicated ~150 ft *below* field elevation when making a high speed pass down the runway. Adding pop-rivet heads over the ports (thanks, Kevin) corrected both the airspeed error & the altimeter error. Would adding another port have changed things again? I don't know, but I'd bet yes. Charlie ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Oct 19, 2002
Subject: Re: RV 6 list digest:2msgs-10-18-02
The weeping brake fitting can be fixed by emoving it and using ,"Fuel Lube " to re-install it .You need something like this when installing any aluminum or dissimilar metal fittings. As a lubricant and sealer. RV-4 , N1191X , Flying Now Charleston, Arkansas ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: RE: RV6-List: Fuel Sender Leak
Date: Oct 19, 2002
Hi Harry, I'm very familiar with that stuff! It's great for many applications, but I hesitate to use it on my fuel tanks. I don't think it has the flexibility of the PRC sealants, and since I'm not going to drain the tank to fix this, I need to use a purpose made sealant that will cure with fuel present, this is where PR-1435 is excellent. I'm using B1/2 so it sets up in no-time, and doesn't care about the seaping fuel that is present. Clean the area with some MEK, and schmutz away! Thanks for the suggestion, the 3M product has many great uses on RV's! Cheers, Stein Bruch RV6, Minneapolis. Flying...except the weather won't cooperate! -----Original Message----- From: owner-rv6-list-server(at)matronics.com [mailto:owner-rv6-list-server(at)matronics.com]On Behalf Of Harry Hawkins Subject: Re: RV6-List: Fuel Sender Leak --> RV6-List message posted by: "Harry Hawkins" 3M makes a product called "structural adhesive" p/n 08101. it would seal your mother in laws mouth. Work fast it has only two minutes till it hardens. You will like it for gas leaks. ________________________________________________________________________________
From: Ewinne(at)aol.com
Date: Oct 20, 2002
Subject: do not forward!
do not forward! Ed Winne RV9A Hershey PA ________________________________________________________________________________
From: "Rick Galati" <rick07x(at)earthlink.net>
Subject: FW: Spinner Assembly
Date: Oct 20, 2002
----- Original Message ----- From: Rick Galati Subject: FW: Spinner Assembly ----- Original Message ----- From: Rick Galati Subject: Spinner Assembly I purchased the Sensenich bolt-on spinner assembly for my under construction 6A. None of its parts are interchangeable with the Van's kit supplied spinner assembly. The front and rear bulkheads are of a completely different design. There is nothing you have to do to this assembly other than bolt it to the engine. I upgraded because I want the option of plating the spinner. Interestingly, Sensenich expressed some concern about "hydrogen embrittlement" and did not recommend it. They suggest polishing it to a high luster from time to time. All I know is 12 years ago I plated the spinner on my C150 and it has held up very well. Anyway, go to Sensenichs' website for more information. --- Rick Galati --- rick07x(at)earthlink.net --- EarthLink: It's your Internet. --- Rick Galati --- rick07x(at)earthlink.net --- EarthLink: It's your Internet. --- Rick Galati --- rick07x(at)earthlink.net --- EarthLink: It's your Internet. ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: static air question
Date: Oct 20, 2002
Extra ports means more tubing, more fittings, more weight, and the possibility of more leaks and less accuracy. Use either the dual fuselage ports or the port on the pitot tube. Won't make much difference until you go to certify your static system. Remember, the tech charges by the hour to find and seal the leaks to certify. P.S. Why stop at just 3 if you think additional ports increases accuracy??? Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org Always looking for articles for the Experimenter original Message ----- From: "Charlie and Tupper England" <cengland(at)netdoor.com> Subject: Re: RV-List: static air question > > Konrad Werner wrote: > > > > see below... > > > > > Good question Kim, > > > > I don't see how too many static sources could be bad in any way, as long as > > they are in proven locations on the airframe? > > Actually combining different sources of "Acceptable Locations" would give a > > better average/balance on static pressure, now wouldn't it?? > > But then, I could be way wrong on this theory. Please correct me if so!! > > > > Konrad, > > ABQ-NM > > > > > I am installing the Gretz heated pitot in my RV9. This pitot has a static > > > air port. Van's uses ports on the mid/aft fusealge as a source for static > > > air. My (probably dumb) question is which pitot source should I use? > > The > > > fuse source is easier to troubleshoot if there is a problem yet I can > > also > > > argue advantages for using the wing-pitot static source. Can/should I use > > > both and connect the wing & fuse static air together? > > > > > > Thanks > > > > > > Kim Nicholas > > > RV9A (I can see the light.....) > > > Seattle > > > > > > > > > Konrad, > > On my RV-4 with 2 flush static ports in Van's recommended fuse. location, I had > ~ 10 kt (slow) error in indicated airspeed at cruise & ~ 150 ft (low) indicated > altitude at full speed. If you are wondering how I knew, the alt. was set to > field elevation & indicated ~150 ft *below* field elevation when making a high > speed pass down the runway. > > Adding pop-rivet heads over the ports (thanks, Kevin) corrected both the > airspeed error & the altimeter error. > > Would adding another port have changed things again? I don't know, but I'd bet > yes. > > Charlie > > ________________________________________________________________________________
From: "Austin" <6430(at)axion.net>
Subject: Van's regulator
Date: Oct 20, 2002
Listers, I seem to recall some instances of builders having problems with a Van's voltage regulator.........anyone have any experience with that ? My regulator was putting out 16.8 V and the small adjustment dealy on the back gives a TINY adjustment and reduced output hardly at all....... My regulator may be an older one with a tin box and one field wire attached to a screw on top, and one other wire out the back......my alternator ( 30 amp ) also has different color and number of wires than my pal has who also has a Van's kit.... This reg. causes my o/v breaker to pop even during a ground idle...I pulled the unit out for now, to replace it.....any other incidents out there ? Austin. ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: static air question
Date: Oct 20, 2002
Thanks Charlie & Cy for your respective inputs. Konrad > > Extra ports means more tubing, more fittings, more weight, and the > possibility of more leaks and less accuracy. > Use either the dual fuselage ports or the port on the pitot tube. Won't make > much difference until you go to certify your static system. Remember, the > tech charges by the hour to find and seal the leaks to certify. > > P.S. Why stop at just 3 if you think additional ports increases accuracy??? > Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh > > Editor, EAA Safety Programs > cgalley(at)qcbc.org or experimenter(at)eaa.org > > > > Konrad, > > On my RV-4 with 2 flush static ports in Van's recommended fuse. location, > I had ~ 10 kt (slow) error in indicated airspeed at cruise & ~ 150 ft (low) > indicated altitude at full speed. If you are wondering how I knew, the alt. was set > to field elevation & indicated ~150 ft *below* field elevation when making a > high speed pass down the runway. > > Adding pop-rivet heads over the ports (thanks, Kevin) corrected both the > airspeed error & the altimeter error. > Would adding another port have changed things again? I don't know, but I'd > bet yes. > Charlie ________________________________________________________________________________
Date: Oct 20, 2002
From: Bobby Hester <bhester(at)apex.net>
Subject: Re: DAR Listing ???
John wrote: > > Because basically your have to have the PERMISSION to make the change from > the FSDO or a DAR. If you have the newer operations limitations you just do > the change, log it, go to Phase 1 for 5 hours, and if all is well, just make > the required log entry. With the old limitations you CANNOT just 'do it' - > what ever happened to equal treatment under the law??? The DARs want to do a > full plane inspection - just as if it had never been inspected and charge > for the whole ball of wax, even though, as you point out, it is merely a > paper work exercise. > > John at Salida, CO All you have to do is send a copy of your current operation limitations to you state FAA office and request it be updated with the new wording. They will create a new operation limitations and send it to you. I did that with my current experimental (Rans S12xl). No problem! -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
From: "John" <n1cxo320(at)salidaco.com>
Subject: Re: DAR Listing ???
Date: Oct 20, 2002
I wish that were the case. I did exactly that. I sent the local FSDO office the complete package. They returned it, said they don't do experimental stuff anymore, and I should go to a DAR....I felt as if I had been told to go to h--- ! The FAA FSDO offices all operate differently, largely depending on staffing levels. I doubt some will ever to back to handling experimental inspections or anything else connected to experimental. How nice it is to take tax money and then tell the tax-payers to pay someone else for the work they are being paid to do. John at Salida, CO ----- Original Message ----- From: "Bobby Hester" <bhester(at)apex.net> Subject: Re: RV-List: DAR Listing ??? > > John wrote: > > > > > Because basically your have to have the PERMISSION to make the change from > > the FSDO or a DAR. If you have the newer operations limitations you just do > > the change, log it, go to Phase 1 for 5 hours, and if all is well, just make > > the required log entry. With the old limitations you CANNOT just 'do t' - > > what ever happened to equal treatment under the law??? The DARs want to do a > > full plane inspection - just as if it had never been inspected and charge > > for the whole ball of wax, even though, as you point out, it is merely a > > paper work exercise. > > > > John at Salida, CO > > All you have to do is send a copy of your current operation limitations to you > state FAA office and request it be updated with the new wording. They will > create a new operation limitations and send it to you. I did that with my > current experimental (Rans S12xl). No problem! > > > -- > Surfing the Web from Hopkinsville, KY > Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ > RV7A Working on the wings :-) > > ________________________________________________________________________________
From: "John" <n1cxo320(at)salidaco.com>
Subject: Re: DAR Listing ???
Date: Oct 20, 2002
I DID contact the EAA and the AOPA and neither were much help. The EAA said they understood my circumstance, but doubted that anything could be done. They also added that they definately believed the FAA would NEVER issue a blanket change to operations limitatons to update the older restrictions on major changes to the newer ones that allow changes in the new simplified manner. We are just screwed I guess. The Denver FSDO refuses to do anything for experimental aircraft. AOPA responded but couldn't offer anything helpful. John at Salida, CO ----- Original Message ----- From: "Charlie and Tupper England" <cengland(at)netdoor.com> Subject: Re: RV-List: DAR Listing ??? > > You can get your old op lims changed to the new ones by calling the fsdo & > explaining what you want, then taking your old op lims to them along with the > completed application they mailed to you. They then issue the new paperwork in > the office. Been there, done that with an RV-4 built in '92. > > If the fsdo resists, call EAA & ask for their assistance in educating the guys > at the fsdo. > > Charlie > > > John wrote: > > > > > > Because basically your have to have the PERMISSION to make the change from > > the FSDO or a DAR. If you have the newer operations limitations you just do > > the change, log it, go to Phase 1 for 5 hours, and if all is well, just make > > the required log entry. With the old limitations you CANNOT just 'do t' - > > what ever happened to equal treatment under the law??? The DARs want to do a > > full plane inspection - just as if it had never been inspected and charge > > for the whole ball of wax, even though, as you point out, it is merely a > > paper work exercise. > > > > John at Salida, CO > > > > ----- Original Message ----- > > From: "Jerry Springer" <jsflyrv(at)earthlink.net> > > To: > > Subject: Re: RV-List: DAR Listing ??? > > > > > > > > John wrote: > > > > > > > > > > > > Mike, > > > > > > > > Does that mean I can send you the documentation necessary to have my > > 'old' > > > > operations limitations changed to match those published in FAA Order > > > > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes published > > in > > > > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > > > > > > > Basically that would be so I can make a change to the aircraft, log it, > > stay > > > > in Phase 1 for 5 hours, and if all is well, make the required log entry > > and > > > > not have to pay someone $500? > > > > > > > > As it stands right now the man in the hangar right next to mine, with > > the > > > > exact airplane, having received his airworthiness certificate under the > > new > > > > order, can make changes himself, but me, only 15-feet away, has to pay > > some > > > > guy $500 for 'help' I don't need if we make the precise same changes. > > > > > > > > What's possible? Would the upcoming Experimeintal DAR that goes into > > effect > > > > the first of the year or so change what would be possible? > > > > > > > > John at Salida, CO > > > > n1cxo320(at)salidaco.com > > > > > > > > > > John you can do that now, make the changes send a letter to FAA saying > > what > > > changes you made. Why would you have to pay someone $500.00? > > > > > > > > ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: DAR Listing ???
Date: Oct 20, 2002
FWIW, the Scottsdale FSDO is pretty helpful. Their inspector there is an RV-4 builder. He even does inspections and such. Bet he could help you out. Gary Towner is his name at the Scottsdale, Arizona FSDO. Paul Besing RV-6A Sold (Waiting on the RV-10) http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "John" <n1cxo320(at)salidaco.com> Subject: Re: RV-List: DAR Listing ??? > > I DID contact the EAA and the AOPA and neither were much help. The EAA said > they understood my circumstance, but doubted that anything could be done. > They also added that they definately believed the FAA would NEVER issue a > blanket change to operations limitatons to update the older restrictions on > major changes to the newer ones that allow changes in the new simplified > manner. We are just screwed I guess. > The Denver FSDO refuses to do anything for experimental aircraft. AOPA > responded but couldn't offer anything helpful. > > John at Salida, CO > > > ----- Original Message ----- > From: "Charlie and Tupper England" <cengland(at)netdoor.com> > To: > Subject: Re: RV-List: DAR Listing ??? > > > > > > > You can get your old op lims changed to the new ones by calling the fsdo & > > explaining what you want, then taking your old op lims to them along with > the > > completed application they mailed to you. They then issue the new > paperwork in > > the office. Been there, done that with an RV-4 built in '92. > > > > If the fsdo resists, call EAA & ask for their assistance in educating the > guys > > at the fsdo. > > > > Charlie > > > > > > John wrote: > > > > > > > > > Because basically your have to have the PERMISSION to make the change > from > > > the FSDO or a DAR. If you have the newer operations limitations you just > do > > > the change, log it, go to Phase 1 for 5 hours, and if all is well, just > make > > > the required log entry. With the old limitations you CANNOT just 'do > t' - > > > what ever happened to equal treatment under the law??? The DARs want to > do a > > > full plane inspection - just as if it had never been inspected and > charge > > > for the whole ball of wax, even though, as you point out, it is merely a > > > paper work exercise. > > > > > > John at Salida, CO > > > > > > ----- Original Message ----- > > > From: "Jerry Springer" <jsflyrv(at)earthlink.net> > > > To: > > > Subject: Re: RV-List: DAR Listing ??? > > > > > > > > > > > John wrote: > > > > > > > > > > > > > > > Mike, > > > > > > > > > > Does that mean I can send you the documentation necessary to have my > > > 'old' > > > > > operations limitations changed to match those published in FAA Order > > > > > 8310.2D, Pagagraph 134 (dated 9/30/99), including the changes > published > > > in > > > > > Change 1 to FAA Order 8130.2D (dated 2/15/99) ? > > > > > > > > > > Basically that would be so I can make a change to the aircraft, log > it, > > > stay > > > > > in Phase 1 for 5 hours, and if all is well, make the required log > entry > > > and > > > > > not have to pay someone $500? > > > > > > > > > > As it stands right now the man in the hangar right next to mine, > with > > > the > > > > > exact airplane, having received his airworthiness certificate under > the > > > new > > > > > order, can make changes himself, but me, only 15-feet away, has to > pay > > > some > > > > > guy $500 for 'help' I don't need if we make the precise same > changes. > > > > > > > > > > What's possible? Would the upcoming Experimeintal DAR that goes into > > > effect > > > > > the first of the year or so change what would be possible? > > > > > > > > > > John at Salida, CO > > > > > n1cxo320(at)salidaco.com > > > > > > > > > > > > > John you can do that now, make the changes send a letter to FAA saying > > > what > > > > changes you made. Why would you have to pay someone $500.00? > > > > > > > > > > > > > > ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Oct 20, 2002
Subject: Re: routing the static tubing
In a message dated 10/19/02 12:01:14 PM Pacific Daylight Time, Knicholas2(at)aol.com writes: << when you guys run the static tubing from teh aft fuse, thru the bulkheads and along the pilot side cockpit to the panel, are you somehow stuffing the tube up under the longeron out of sight or just let it stay visable on the bottom of the longeron. If you are stuffing it up under the U shape channel, how are you keeping it there? >> Kim: I drilled holes as high as I could in the seatback bulkhead and the wing spar carry thru bulkhead (I don't know what these are called in the -9) for plastic bushings that fit the static tubing snugly. When I pulled the static tubing through the bushings, with some difficulty because of the tight fit, there is no tendency for the tubing to sag and it is completely out of sight under the canopy deck. I used an angle drill with a small head to reach as high as possible to drill the bushing holes. Hope this helps. Harry Crosby Pleasanton, California RV-6, electrical stuff ________________________________________________________________________________
From: "Dean Pichon" <DeanPichon(at)msn.com>
Subject: Looking for IFR RV-4 pilots
Date: Oct 20, 2002
Hi Listers, I'm considering upgrading my -4 to be IFR capable and would like to talk with someone who actually flies a -4 in instrument conditions. If one of you guys wouldn't mind chatting with me briefly, please contact me off-line. ________________________________________________________________________________
From: "Ernest Kells" <ernest.kells(at)sympatico.ca>
Subject: Re: Van's regulator
Date: Oct 20, 2002
>> I seem to recall some instances of builders having problems with a Van's voltage regulator...anyone have any experience with that ? > My regulator was putting out 16.8 V and the small adjustment dealy on the back gives a TINY adjustment and reduced output hardly at all....... This discussion confuses me somewhat. Vans offers two voltage regulators. One only at 13.8 volts, and one that is adjustable. I asked Vans as to which is appropriate for me. He said that the standard unit would be set to 13.8 only. If I wanted to adjust it to something else sometimes I should get the variable one. I said that I was only interested in 13.8. He said "buy it". Are you talking about the apple or the orange????? If you got the "other" one - is it the one you should adjust??? Ernest Kells - RV-9A O235-N2C, Wood Prop Finish Kit 70% Complete ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: DAR Listing ???
Date: Oct 20, 2002
Make an appointment to see a FSDO airworthiness inspector. Carry your packet in and discuss it. They might just do it on the spot. OR wait until the Vdar is in place. ----- Original Message ----- From: "John" <n1cxo320(at)salidaco.com> Subject: Re: RV-List: DAR Listing ??? > > I wish that were the case. I did exactly that. I sent the local FSDO office > the complete package. They returned it, said they don't do experimental > stuff anymore, and I should go to a DAR....I felt as if I had been told to > go to h--- ! The FAA FSDO offices all operate differently, largely > depending on staffing levels. I doubt some will ever to back to handling > experimental inspections or anything else connected to experimental. How > nice it is to take tax money and then tell the tax-payers to pay someone > else for the work they are being paid to do. > > John at Salida, CO > > > ----- Original Message ----- > From: "Bobby Hester" <bhester(at)apex.net> > To: > Subject: Re: RV-List: DAR Listing ??? > > > > > > John wrote: > > > > > > > > Because basically your have to have the PERMISSION to make the change > from > > > the FSDO or a DAR. If you have the newer operations limitations you just > do > > > the change, log it, go to Phase 1 for 5 hours, and if all is well, just > make > > > the required log entry. With the old limitations you CANNOT just 'do > t' - > > > what ever happened to equal treatment under the law??? The DARs want to > do a > > > full plane inspection - just as if it had never been inspected and > charge > > > for the whole ball of wax, even though, as you point out, it is merely a > > > paper work exercise. > > > > > > John at Salida, CO > > > > All you have to do is send a copy of your current operation limitations to > you > > state FAA office and request it be updated with the new wording. They will > > create a new operation limitations and send it to you. I did that with my > > current experimental (Rans S12xl). No problem! > > > > > > -- > > Surfing the Web from Hopkinsville, KY > > Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ > > RV7A Working on the wings :-) > > > > > > ________________________________________________________________________________
Date: Oct 20, 2002
From: "Richard E. Tasker" <retasker(at)optonline.net>
Subject: Elevator trailing edges...
I am ready to drill my elevator trailing edges and have a question. According to the directions for drilling, one is supposed to mark a line 7/32 - 1/4 inch back from the leading edge of the wedge. If I do this and then line it up with the predrilled holes on teh elevator, the wedge sticks out from the trailing edge of the skin about 0.050". The rudder was predrilled and it doesn't stick out at all. Is this correct? The elevators trailing edge sticks out past the skin but the rudder doesn't?? Or am I interperting something wrong? Also, what sort of corrosion prevention is to be used on the trim tab hinge (if any)? It sort of looks like it is anodized which would need no additional coating. Dick, 90573 ________________________________________________________________________________
From: "Jim Cimino" <jcimino(at)echoes.net>
Subject: Re: Van's regulator
Date: Oct 20, 2002
I have had both on my RV-8 with Van's 35 amp alternator. I got the preset one first and it worked for about 10 hrs and then went crazy. I talked to some other people who had it and they also experienced problems with it. I purchased the adjustable one and set it to 14.1V and have been flying with it for about 80hrs without a problem. Jim Jim Cimino RV-8 sn 80039 N7TL 85+ Hrs. http://www.geocities.com/jcimino.geo/ (570)842-4057 ----- Original Message ----- From: "Ernest Kells" <ernest.kells(at)sympatico.ca> Subject: Re: RV-List: Van's regulator > > >> I seem to recall some instances of builders having problems with a Van's > voltage regulator...anyone have any experience with that ? > > My regulator was putting out 16.8 V and the small adjustment dealy on > the back gives a TINY adjustment and reduced output hardly at all....... > > This discussion confuses me somewhat. Vans offers two voltage regulators. > One only at 13.8 volts, and one that is adjustable. I asked Vans as to > which is appropriate for me. He said that the standard unit would be set to > 13.8 only. If I wanted to adjust it to something else sometimes I should > get the variable one. I said that I was only interested in 13.8. He said > "buy it". Are you talking about the apple or the orange????? If you got > the "other" one - is it the one you should adjust??? > Ernest Kells - RV-9A O235-N2C, Wood Prop > Finish Kit 70% Complete > > ________________________________________________________________________________
Date: Oct 20, 2002
From: barry pote <barrypote(at)comcast.net>
Subject: do not forward
do not forward Barry Pote RV9a finishing ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: DAR Listing ???
Date: Oct 20, 2002
John at Salida, CO > > All you have to do is send a copy of your current operation limitations to you > state FAA office and request it be updated with the new wording. They will > create a new operation limitations and send it to you. I did that with my > current experimental (Rans S12xl). No problem! > > > -- > Surfing the Web from Hopkinsville, KY > Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ > RV7A Working on the wings :-) > Actually, it much depends on your local FSDO. When I had my operating limitations changed to permit me to make and sign off major changes, the local FSDO came out and inspected my aircraft again, this was down in NC. I could not get the FAA FSDO in Washington area to do the original inspection despite months of effort, so finally hired a DAR. Ed Anderson Matthews, NC ________________________________________________________________________________
From: "Sally and George" <aeronut58(at)hotmail.com>
Subject: Re: Van's regulator
Date: Oct 20, 2002
My experience, for what it's worth: I built my RV-8 with the adjustable Van's regulator. It worked for about 25 hours, then failed (in safe mode, not catastrophically). I replaced it with a Ford automotive regulator, as recommended by Electric Bob Nuckolls and have had no problems for about 75 hours. George Kilishek N888GK >----- Original Message ----- >From: "Ernest Kells" <ernest.kells(at)sympatico.ca> >To: >Subject: Re: RV-List: Van's regulator > > > > > > > >> I seem to recall some instances of builders having problems with a >Van's > > voltage regulator...anyone have any experience with that ? > > > My regulator was putting out 16.8 V and the small adjustment >dealy >on > > the back gives a TINY adjustment and reduced output hardly at all....... > > > > This discussion confuses me somewhat. Vans offers two voltage >regulators. > > One only at 13.8 volts, and one that is adjustable. I asked Vans as to > > which is appropriate for me. He said that the standard unit would be >set >to > > 13.8 only. If I wanted to adjust it to something else sometimes I >should > > get the variable one. I said that I was only interested in 13.8. He >said > > "buy it". Are you talking about the apple or the orange????? If you >got > > the "other" one - is it the one you should adjust??? > > Ernest Kells - RV-9A O235-N2C, Wood Prop > > Finish Kit 70% Complete > > > > > > http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: DAR Listing ???
Date: Oct 20, 2002
First I've heard of the VDAR. Where can I find out more info? - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Cy Galley > Sent: Sunday, October 20, 2002 6:10 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: DAR Listing ??? > > > > Make an appointment to see a FSDO airworthiness inspector. > Carry your packet in and discuss it. They might just do it > on the spot. OR wait until the Vdar is in place. > > ----- Original Message ----- > From: "John" <n1cxo320(at)salidaco.com> > To: > Subject: Re: RV-List: DAR Listing ??? > > > > > > I wish that were the case. I did exactly that. I sent the local FSDO > office > > the complete package. They returned it, said they don't do > > experimental stuff anymore, and I should go to a DAR....I > felt as if I had been told to > > go to h--- ! The FAA FSDO offices all operate differently, largely > > depending on staffing levels. I doubt some will ever to back to > > handling experimental inspections or anything else connected to > > experimental. How nice it is to take tax money and then tell the > > tax-payers to pay someone else for the work they are being > paid to do. > > > > John at Salida, CO > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: DAR Listing ???
Date: Oct 20, 2002
Sorry, I called it V Dar for volunteer DAR but it has been changed again. EAA-DEVELOPED AMATEUR-BUILT DAR PROGRAM BEGINS IN DECEMBER Program Aims to Unclog Logjam of Inspection Requests A new amateur-built aircraft DAR (Designated Airworthiness Representative) program, designed to ease the current backlog of airworthiness inspection requests, will become effective on December 30, 2002. The program, a product of three years of collaboration between EAA and FAA, will increase the number of inspectors authorized to issue airworthiness certificates for amateur-built aircraft. "EAA was eager to help develop and participate in this program, which will significantly strengthen support for homebuilders by increasing their access to aircraft inspectors," EAA President Tom Poberezny said. "Increasing the number of DARs will shorten the time needed for inspection, enabling builders to fly their aircraft sooner and encourage the continued growth of homebuilding." The demand for amateur-built aircraft certification has outgrown FAA inspector resources in recent years, causing waits of three to six months in some cases for initial inspections. The amateur-built DAR program addresses the shortage by creating a new DAR designation for amateur-built (AB) aircraft certification. EAA, long recognized for providing technical assistance and training to homebuilders, is a designated sponsoring organization that may recommend qualified individuals for AB DAR appointment. AB DAR candidates must possess current knowledge on fabrication, assembly and operating characteristics of amateur-built aircraft; speak and write English; and have three technical and three character references, including one from the sponsoring organization when applicable. In addition, DAR candidates must hold an FAA A have built and received certification for an amateur-built airplane that has flown a minimum of 100 hours; and performed at least three condition inspections on such aircraft. DAR candidates without A&P certificates must have a minimum of five years experience as a field technical representative or as an FAA inspector. New AB DARs are required to attend Transportation Safety Institute (TSI) amateur-built training (currently being developed by TSI with help from EAA and FAA) as well as FAA initial standardization training before performing certifications. For more information on AB DAR certification, contact your local MIDO (Manufacturing Inspection District Office) or the MIDO satellite office (MISO). Current DARs wishing to maintain amateur-built authority should contact their managing offices in writing to revise their certificates. DARs can also expand their authority to include amateur-built aircraft by completing the corresponding TSI training. The program allows DARs to work outside of their assigned geographic area after contacting their MIDO and receiving an endorsement. For more information, contact the EAA Government Relations Office at 888/EAA-INFO, ext. 6522, or govt(at)eaa.org. ----- Original Message ----- From: "Larry Bowen" <Larry(at)bowenaero.com> Subject: RE: RV-List: DAR Listing ??? > > First I've heard of the VDAR. Where can I find out more info? > > - > Larry Bowen > Larry(at)BowenAero.com > http://BowenAero.com > > > > -----Original Message----- > > From: owner-rv-list-server(at)matronics.com > > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Cy Galley > > Sent: Sunday, October 20, 2002 6:10 PM > > To: rv-list(at)matronics.com > > Subject: Re: RV-List: DAR Listing ??? > > > > > > > > Make an appointment to see a FSDO airworthiness inspector. > > Carry your packet in and discuss it. They might just do it > > on the spot. OR wait until the Vdar is in place. > > > > ----- Original Message ----- > > From: "John" <n1cxo320(at)salidaco.com> > > To: > > Subject: Re: RV-List: DAR Listing ??? > > > > > > > > > > I wish that were the case. I did exactly that. I sent the local FSDO > > office > > > the complete package. They returned it, said they don't do > > > experimental stuff anymore, and I should go to a DAR....I > > felt as if I had been told to > > > go to h--- ! The FAA FSDO offices all operate differently, largely > > > depending on staffing levels. I doubt some will ever to back to > > > handling experimental inspections or anything else connected to > > > experimental. How nice it is to take tax money and then tell the > > > tax-payers to pay someone else for the work they are being > > paid to do. > > > > > > John at Salida, CO > > > > > ________________________________________________________________________________
Date: Oct 20, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: static air question
> > >I have the Gretz heated pitot in my RV8 and fuselage static ports. I ran >them separately with a selector valve. I found the static source from the >pitot accurate, whereas the fuselage ports off by 150' or so and 5 to 10 kts. > >Mike Robbins >RV8Q N88Mj 115 hours >Seattle area Mike - just curious - did you use Van's pop rivet static ports, or flush static ports? -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
Date: Oct 20, 2002
From: "Michael J. Robbins" <michael.j.robbins(at)verizon.net>
Subject: Re: static air question
Kevin; I did use Van's pop rivet ports, but I did not locate them per the RV8 drawings. I failed to see the drawing depicting the proper location for the ports on the 8, and instead used the location on the instruction sheet, which is for the -6. I naively thought that if they were different for the 8 then Van would have included separate instructions for the 8. I know better now. So in my case they aren't in the right place, so I guess that's why they don't work. Mike Robbins >Mike - just curious - did you use Van's pop rivet static ports, or >flush static ports? >-- >Kevin Horton RV-8 (cowling, wing tip lights) >Ottawa, Canada ________________________________________________________________________________
From: "Dave von Linsowe" <davevon(at)tir.com>
Subject: constant speed prop diameters
Date: Oct 20, 2002
Hi guys, I have a couple of questions concerning constant speed prop diameters. First, is there anyone out there running a Hartzell clipped to 68"? I would think that the smaller diameter would allow more pitch in cruise and more speed. An engineer at Hartzell says no. He says to run the largest diameter possible for more speed. He claims that the effect of the increased parasitic drag of the fuselage goes up more with the smaller diameter prop. Although it doesn't seem to really hold true from the results seen with fix pitch props. I would think that there would be an ideal diameter for each airplane based on parasitic drag of the fuselage and cruise speed. The lower drag of a RV as compared to a Cessna I think would lend itself to a smaller diameter. It is obvious that the larger diameter would have a big effect on climb. Second question, has anyone tried different diameter Hartzell C/S props on the same airplane? (apples to apples comparison) Thanks, Dave RV-6 O-360 C/S, tip up ________________________________________________________________________________
Date: Oct 20, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Van's regulator
Sally and George wrote: > > > My experience, for what it's worth: > > I built my RV-8 with the adjustable Van's regulator. It worked for about 25 > hours, then failed (in safe mode, not catastrophically). I replaced it with > a Ford automotive regulator, as recommended by Electric Bob Nuckolls and > have had no problems for about 75 hours. > > George Kilishek > N888GK > I have been flying the mid-70's Ford regulator for 430 hrs with no hiccups (I hope I didn't just jinx it....). Neat thing about the Ford regulator is that I can replace it at any airport where I can bum a ride to the nearest auto parts store, and, it costs less than ten dollars. I also use 'Lectric Bob's overvoltage module. Sam Buchanan http://thervjournal.com ________________________________________________________________________________
Date: Oct 20, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: static air question
Yeah, the accuracy of aft fuselage static ports varies greatly depending on where they are located. So this could be why they aren't accurate in your case. Kevin > > > >Kevin; > >I did use Van's pop rivet ports, but I did not locate them per the RV8 >drawings. I failed to see the drawing depicting the proper location for >the ports on the 8, and instead used the location on the instruction sheet, >which is for the -6. I naively thought that if they were different for the >8 then Van would have included separate instructions for the 8. I know >better now. So in my case they aren't in the right place, so I guess >that's why they don't work. > >Mike Robbins > > >>Mike - just curious - did you use Van's pop rivet static ports, or >>flush static ports? >>-- >>Kevin Horton RV-8 (cowling, wing tip lights) > >Ottawa, Canada > ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: primer sealer/filler
Date: Oct 20, 2002
On Fiberglass , what primer sealer or filler is compatible with Sherwin Williams Jet Glow paint? Jerry Calvert Edmond Ok -6 N296JC (res) ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: F804N side channel cap - when?
Date: Oct 20, 2002
When is it too soon or too late to install the F804N side channel cap? Thats the cover that is pop rivetted on the side of the center section. I was going to install the throttle quad tonight, but realized a couple of the pop rivets in the channel cap would not be able to be pulled with the quadrant in the way. Thus I concluded the channel cap must be installed before the quadrant. Right? The rear quadrant is installed. I haven't fit my wings yet -- not sure if that's a factor or not. What a puzzle! Thanks. - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com ________________________________________________________________________________
Date: Oct 20, 2002
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: Full-swivel tailwheel
After only 35 hours of use, my full-swivel tailwheel is refusing to relock after a tight turn. Eventually does when I get out and wiggle the rudder gently either side of straight-ahead. Every thing appears to work properly, but I wonder if the grease I added at the 25hr oilchange and service may have compressed or jammed up the spring behind the locking pin. Anyone have any experience with this? Thanks, Scott in VAncouver still learnin' ________________________________________________________________________________
Date: Oct 20, 2002
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: Van's oil temp gauge
Just a heads' up for those using the Van's oil temp gauge. A colleague called last week for help in troubleshooting a sudden 30-degree rise in oil temperature. We tried the usual" remove the sender and immerse in boiling water" routine and the gauge indicated about 205F without the engine running. Put it back together and went flying on a 20C day. Sure enough, the oil temp climbed to about 225F before stabilizing. This RV has over 800hrs on it using this same engine and it has never behaved like this. Orbiting within gliding distance of the airport, the owner and I scratched our heads. I finally realized that the only difference now from when we tested it on the ground was the bus voltage. I turned off the alternator and the oil temperature immediately fell about 30F back to a more normal reading. Re-energizing the alternator caused the temp to climb back up again. To their credit, Van's immediately shipped out another gauge. Something to consider before ordering a larger oil cooler or something even more drastic. SCott in Vancouver ________________________________________________________________________________
Date: Oct 20, 2002
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: Removing bugs
Re: the recent thread about Simple Green or Fantastic Orange to remove bugs from the painted surfaces: I've been trying out a new product here in Canada which is an automotive windshield-washing fluid with something called "Bug Wash" added. I just wipe it on the leading edges using a small synthetic sponge and, when reaching the other end of the wing, start over again with a light scrubbing action and the remains just wipe off. Might be kinder to the paint than the above products... Scott in Vancouver ________________________________________________________________________________
From: LeastDrag93066(at)aol.com
Date: Oct 21, 2002
Subject: Re: constant speed prop diameters
Hi All, I have flown the same three propeller blades at the original 76" diameter, and gradually trimmed them equally to the smallest diameter of 66" diameter. I have flown these blades as both a three blade prop and as a two blade prop. On my RV-3, I can make the following generalizations: The largest diameter allowing the max 2700 RPM gave the best climb rate. The smallest diameter (down to 66") gave the highest speed. For the prop I was testing, a 6" smaller diameter three blade prop gave the same speed as a two blade prop. BTW, The prop I was running was NOT a metal prop. The manufacturer gave me special instructions for my installation, so it would be legal for me to make the prop modifications. Jim Ayers RV-3 N47RV Maroon Marauder ________________________________________________________________________________
From: "Robert scott" <rscott(at)johnsonmfginc.com>
Subject: Re: RV9-List: Elevator trailing edges...
Date: Oct 20, 2002
Mine extended out aprox. .025/.040. I just filed, block sanded and scotch brighted the AEX flush with the skin after assembly. Robert Scott N472RV Reserved ----- Original Message ----- From: "Richard E. Tasker" <retasker(at)optonline.net> Subject: RV9-List: Elevator trailing edges... > --> RV9-List message posted by: "Richard E. Tasker" > > I am ready to drill my elevator trailing edges and have a question. > According to the directions for drilling, one is supposed to mark a > line 7/32 - 1/4 inch back from the leading edge of the wedge. If I do > this and then line it up with the predrilled holes on teh elevator, the > wedge sticks out from the trailing edge of the skin about 0.050". The > rudder was predrilled and it doesn't stick out at all. > > Is this correct? The elevators trailing edge sticks out past the skin > but the rudder doesn't?? Or am I interperting something wrong? > > Also, what sort of corrosion prevention is to be used on the trim tab > hinge (if any)? It sort of looks like it is anodized which would need > no additional coating. > > Dick, 90573 > > ________________________________________________________________________________
From: "flyseaplane" <flyseaplane(at)netzero.net>
Subject: RV6-List GREEN LOCTITE
Date: Oct 21, 2002
Dear Dan Eikleberry, Green Loctite is not rare at all. Any AutoZone auto parts store carries it, It is $4.99 plus tax in central Texas. Let us know if it works. I tried Super Glue once (the really thin stuff) and it stopped about 95% of the leak. There was still a tiny little weep left where a few molecules of gas were getting through, but for the most part stopped it. Good Luck, Linc ------------------------------------------- Introducing NetZero Long Distance Unlimited Long Distance only $29.95/ month! Sign Up Today! www.netzerolongdistance.com ________________________________________________________________________________
From: "Gary" <rv9er(at)3rivers.net>
Subject: Re: RV9-List: Elevator trailing edges...
Date: Oct 20, 2002
I would say line the wedge up where you like the fit, and don't worry about the dimension. .050 sticking out is not going to look too good. Just make sure you don't go too far the other way, or your holes will be in a portion of the wedge that is too thin. The hinges are anodized. I didn't prime them. You can determine whether aluminum is anodized with an ohmmeter. Anodizing is Aluminum Oxide, and non-conductive......but very thin. Gary 90263 --> RV9-List message posted by: "Richard E. Tasker" I am ready to drill my elevator trailing edges and have a question. According to the directions for drilling, one is supposed to mark a line 7/32 - 1/4 inch back from the leading edge of the wedge. If I do this and then line it up with the predrilled holes on teh elevator, the wedge sticks out from the trailing edge of the skin about 0.050". The rudder was predrilled and it doesn't stick out at all. Is this correct? The elevators trailing edge sticks out past the skin but the rudder doesn't?? Or am I interperting something wrong? Also, what sort of corrosion prevention is to be used on the trim tab hinge (if any)? It sort of looks like it is anodized which would need no additional coating. Dick, 90573 ________________________________________________________________________________
From: "Robert scott" <rscott(at)johnsonmfginc.com>
Subject: Re: RV9-List: Elevator trailing edges...
Date: Oct 20, 2002
Mine extended out aprox. .025/.040. I just filed, block sanded and scotch brighted the AEX flush with the skin after assembly. Robert Scott N472RV Reserved ----- Original Message ----- From: "Richard E. Tasker" <retasker(at)optonline.net> Subject: RV9-List: Elevator trailing edges... > --> RV9-List message posted by: "Richard E. Tasker" > > I am ready to drill my elevator trailing edges and have a question. > According to the directions for drilling, one is supposed to mark a > line 7/32 - 1/4 inch back from the leading edge of the wedge. If I do > this and then line it up with the predrilled holes on teh elevator, the > wedge sticks out from the trailing edge of the skin about 0.050". The > rudder was predrilled and it doesn't stick out at all. > > Is this correct? The elevators trailing edge sticks out past the skin > but the rudder doesn't?? Or am I interperting something wrong? > > Also, what sort of corrosion prevention is to be used on the trim tab > hinge (if any)? It sort of looks like it is anodized which would need > no additional coating. > > Dick, 90573 > > ________________________________________________________________________________
Date: Oct 21, 2002
From: Nouj <nouj(at)compuserve.com>
Subject: RV7-List Digest: 1 Msgs - 10/19/02
Not forward ________________________________________________________________________________
Date: Oct 21, 2002
From: P M Condon <pcondon(at)mitre.org>
Subject: PDA EFIS
http://www.mountainscope.com/ Another handheld PDA based electronic flight instrument/maping (EFIS) option. Has some kept a list of all of these new toys/offerings. There is more then a handfull of these offerings now; which is great. Don'r forget the garman 196 too..... ________________________________________________________________________________
From: "Sally and George" <aeronut58(at)hotmail.com>
Subject: Re: Van's regulator
Date: Oct 21, 2002
Forgot to mention: the Ford alternator cost less than $10 at Auto Zone. George >From: "Sally and George" <aeronut58(at)hotmail.com> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: Re: RV-List: Van's regulator >Date: Sun, 20 Oct 2002 18:54:01 -0500 > > >My experience, for what it's worth: > >I built my RV-8 with the adjustable Van's regulator. It worked for about >25 >hours, then failed (in safe mode, not catastrophically). I replaced it >with >a Ford automotive regulator, as recommended by Electric Bob Nuckolls and >have had no problems for about 75 hours. > >George Kilishek >N888GK > > > >----- Original Message ----- > >From: "Ernest Kells" <ernest.kells(at)sympatico.ca> > >To: > >Subject: Re: RV-List: Van's regulator > > > > > > > > > > > > >> I seem to recall some instances of builders having problems with a > >Van's > > > voltage regulator...anyone have any experience with that ? > > > > My regulator was putting out 16.8 V and the small adjustment > >dealy > >on > > > the back gives a TINY adjustment and reduced output hardly at >all....... > > > > > > This discussion confuses me somewhat. Vans offers two voltage > >regulators. > > > One only at 13.8 volts, and one that is adjustable. I asked Vans as >to > > > which is appropriate for me. He said that the standard unit would be > >set > >to > > > 13.8 only. If I wanted to adjust it to something else sometimes I > >should > > > get the variable one. I said that I was only interested in 13.8. He > >said > > > "buy it". Are you talking about the apple or the orange????? If you > >got > > > the "other" one - is it the one you should adjust??? > > > Ernest Kells - RV-9A O235-N2C, Wood Prop > > > Finish Kit 70% Complete > > > > > > > > > > > > >http://resourcecenter.msn.com/access/plans/default.asp > > http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
Date: Oct 21, 2002
From: Mark Phillips <ripsteel(at)edge.net>
Subject: Re: constant speed prop diameters
Dave von Linsowe wrote: > I would think that the smaller diameter would allow more pitch in cruise and > more speed. An engineer at Hartzell says no. He says to run the largest > diameter possible for more speed. He claims that the effect of the > increased parasitic drag of the fuselage goes up more with the smaller > diameter prop. ...and I would assume the ratio of disc area vs. fuse frontal area would favor the tandem models. Considering a fixed pitch 3-blade pitched for cruise on a -6/6A, does anyone have any actual experience on top speed performance for this combination vs. fixed pitch 2-blade, assuming well designed and built props are part of the equation? (Performance Props and Catto as examples) I am buying soon and interested in a 3-blade, primarily for noise reduction, provided cruise speed does not suffer- I have seen references to reduced climb rate, but this would be an acceptable trade off. Thanks for any thoughts before I cut another big check! Mark Phillips - Columbia, TN - dusting off the engine mount, looking for bolts... ________________________________________________________________________________
From: "Tim Andres" <tim2542(at)charter.net>
Subject: Mitchell (VDO)
Date: Oct 21, 2002
In searching for a new oil temp sender for my 0-360, I found a Mitchell sender # ps 211-8045 with the correct thread (5/8-18) and resistance. The Approved Piper part is not available, (it's made from "Unobtainium") These senders seal via a flange and gasket (AN copper washer), not via the thread like Pipe thread does. My concern is that the old sender has a significantly larger sealing surface (flange) than the new one. The new sender just barely overlaps the sealing washer, however it does not leak. I have talked to Mitchell about it but they seemed unconcerned or interested. He did tell me that they have never had a problem with it and it is correct for Lycoming engines. Anybody run into this? Any ideas? heres a picture of it, http://www.chiefaircraft.com/Aircraft/Aircraft.html ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: Full-swivel tailwheel
Date: Oct 21, 2002
> After only 35 hours of use, my full-swivel tailwheel is refusing to > relock after a tight turn. [snip] > Anyone have any experience with this? I haven't had that specific problem but I have found that I need to service the swivel mechanism every 40-50 hours or so. It generally dries out and starts sticking by then, progressively getting worse as time goes on, and if I let it go very long rust sets in that needs to be polished out. Greasing through the zerk fitting doesn't seem to be adequate; I need to take it apart and clean it all out and smear new grease on by hand. It is hangared, and no I don't fly off non-paved strips all that often (well there was that beach this summer, and the gravel quarry, and... well, thats another story.) May sound like a pain but I must say that its become kind of a nice ritual for me. One of those "tailwheel guy" quirks I guess... :-) Randall Henderson, RV-6 N6R (~400 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
From: "Bill" <n8wv(at)hotmail.com>
Subject: Power Chart...
Date: Oct 21, 2002
I have been thinking of ways to get better performance out of my 150 HP -8A, and this morning put together a page on my web site with some power info... Please have a look and let me know if I screwed anything up... Also, as always your comments are welcome... http://vondane.com/flightdata/powerinfo.htm -Bill www.vondane.com ________________________________________________________________________________
Date: Oct 21, 2002
From: "Michael J. Robbins" <michael.j.robbins(at)verizon.net>
Subject: Re: Removing bugs
Buy some RejeX. Just use water to remove bugs. Works great. Covered my whole plane with it. Mike Robbins RV8 N88MJ 115 hrs do not achive > >Re: the recent thread about Simple Green or Fantastic Orange to remove >bugs from the painted surfaces: > > I've been trying out a new product here in Canada which is an > automotive windshield-washing fluid with something called "Bug Wash" added. >I just wipe it on the leading edges using a small synthetic sponge and, >when reaching the other end of the wing, start over again with a light >scrubbing action and the remains just wipe off. >Might be kinder to the paint than the above products... >Scott in Vancouver > ________________________________________________________________________________
From: Larry Hawkins <lhawkins(at)giant.com>
Subject: Full-swivel tailwheel
Date: Oct 21, 2002
Come on Randall we want to hear about the beach..... and the gravel quarry. -----Original Message----- From: Randall Henderson [mailto:randallh(at)attbi.com] Subject: Re: RV-List: Full-swivel tailwheel > After only 35 hours of use, my full-swivel tailwheel is refusing to > relock after a tight turn. [snip] > Anyone have any experience with this? I haven't had that specific problem but I have found that I need to service the swivel mechanism every 40-50 hours or so. It generally dries out and starts sticking by then, progressively getting worse as time goes on, and if I let it go very long rust sets in that needs to be polished out. Greasing through the zerk fitting doesn't seem to be adequate; I need to take it apart and clean it all out and smear new grease on by hand. It is hangared, and no I don't fly off non-paved strips all that often (well there was that beach this summer, and the gravel quarry, and... well, thats another story.) May sound like a pain but I must say that its become kind of a nice ritual for me. One of those "tailwheel guy" quirks I guess... :-) Randall Henderson, RV-6 N6R (~400 hrs) Portland, OR www.vanshomewing.org RE: RV-List: Full-swivel tailwheel Come on Randall we want to hear about the beach..... and the gravel quarry. -----Original Message----- From: Randall Henderson [<A HREF"mailto:randallh(at)attbi.com">mailto:randallh(at)attbi.com] Subject: Re: RV-List: Full-swivel tailwheel -- RV-List message posted by: Randall Henderson randallh(at)attbi.com After only 35 hours of use, my full-swivel tailwheel is refusing to relock after a tight turn. [snip] Anyone have any experience with this? I haven't had that specific problem but I have found that I need to service the swivel mechanism every 40-50 hours or so. It generally dries out and starts sticking by then, progressively getting worse as time goes on, and if I let it go very long rust sets in that needs to be polished out. Greasing through the zerk fitting doesn't seem to be adequate; I need to take it apart and clean it all out and smear new grease on by hand. It is hangared, and no I don't fly off non-paved strips all that often (well there was that beach this summer, and the gravel quarry, and... well, thats another story.) May sound like a pain but I must say that its become kind of a nice ritual for me. One of those tailwheel guy quirks I guess... :-) Randall Henderson, RV-6 N6R (~400 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
From: "Randy Lervold" <randy@rv-8.com>
Subject: Re: Full-swivel tailwheel
Date: Oct 21, 2002
After 250 hrs or so mine showed galling on the post surface in spite of keeping it fairly well greased with hi-temp disc brake grease. Tom Green says oil is the best lubricant because the bronze bushing is Oil-Lite (spelling?) which is impregnated with oil. He says grease will not penetrate the pores like oil will. So I bought a new fork/post assembly and have been using oil since then... too soon for any results. FWIW, Randy Lervold, RV-8, 273 hrs. > > After only 35 hours of use, my full-swivel tailwheel is refusing to > > relock after a tight turn. > [snip] > > Anyone have any experience with this? > > I haven't had that specific problem but I have found that I need to service > the swivel mechanism every 40-50 hours or so. It generally dries out and > starts sticking by then, progressively getting worse as time goes on, and if > I let it go very long rust sets in that needs to be polished out. Greasing > through the zerk fitting doesn't seem to be adequate; I need to take it > apart and clean it all out and smear new grease on by hand. It is hangared, > and no I don't fly off non-paved strips all that often (well there was that > beach this summer, and the gravel quarry, and... well, thats another story.) > > May sound like a pain but I must say that its become kind of a nice ritual > for me. One of those "tailwheel guy" quirks I guess... :-) > > Randall Henderson, RV-6 N6R (~400 hrs) > Portland, OR > www.vanshomewing.org ________________________________________________________________________________
From: "Dave von Linsowe" <davevon(at)tir.com>
Subject: comm antenna
Date: Oct 21, 2002
Hi guys, At one of the dawn patrols this summer, a RV-6 was there that had the comm antennas in the leading edge of each gear leg (fiber glass fairings). The owner said it worked great. We did some air to air and he sounded fine even when he was out ahead of me. Has anyone had any experience with trying this? Thanks, Dave RV-6, 180hp, tip-up ________________________________________________________________________________
From: CRomine656(at)aol.com
Date: Oct 21, 2002
Subject: W-730 Bellcrank Jig
It looks like the jig stays in the wing until after the wings are completely finished (it is mentioned again when fitting the wing tip). What about the second wing and aileron alignment? Do we make another jig, or is everyone removing the supplied piece and reinstalling it when necessary? Chris Romine RV-7A Wings ________________________________________________________________________________
From: "Russ Werner" <russ(at)maui.net>
Subject: Electric Aileron Trim RV8 style
Date: Oct 21, 2002
Can anyone having experience with the RV8 electric aileron trim kit using the "sliding tube" comment on the spring pressures? Specifically I am interested in the springs Vans sent in your kit. Mine are quite strong and appear (contrary to earlier list posts) that they will impart excessive pressures on the controls. Mine are each 3 inches long (total) and the kit preloads them to about 4 inches. On the bench that is a very hard pull. At full aileron deflection, (my wings aren't on so I have to guess how far the stick needs to move to get there) they will be stretched to about 5 or more inches. I guess if they are too stiff I can get lighter ones of the same length but I thought I'd get comments from those with experience. Thanks, Russ Werner HRII Maui ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: W-730 Bellcrank Jig
Date: Oct 21, 2002
I set the bellcrank-to-aileron pushrod length on each wing with the alignment tool and that's it for now. The inner pushrods will get attached and rigged later (they're up on the wall for now). No sense in doing all this rigging now when it has to happen later anyway. Just an opinion, though. )_( Dan RV-7 N714D (fuselage) http://www.rvproject.com ----- Original Message ----- From: <CRomine656(at)aol.com> Subject: RV-List: W-730 Bellcrank Jig > > It looks like the jig stays in the wing until after the wings are completely > finished (it is mentioned again when fitting the wing tip). What about the > second wing and aileron alignment? Do we make another jig, or is everyone > removing the supplied piece and reinstalling it when necessary? > > Chris Romine > RV-7A Wings > > ________________________________________________________________________________
Date: Oct 21, 2002
Subject: Re: primer sealer/filler
From: Don R Jordan <dons6a(at)juno.com>
Jerry: I would stay with the SW line. I used a lower cost line i found in the Dupont store. They said it was the same as Dupont's line, but a lot cheaper. It was Eurocoat. I really like it. Don Jordan - RV6A - N6DJ Arlington, Tx > > On Fiberglass , what primer sealer or filler is compatible with > Sherwin Williams Jet Glow paint? > > Jerry Calvert > Edmond Ok > -6 N296JC (res) ________________________________________________________________________________
From: "Joe Hine" <joehine(at)nbnet.nb.ca>
Subject: Another good engine scorce
Date: Oct 21, 2002
Listers I just thought I would pass along another good engine shop that would be worth getting a quote from if you are looking for an engine. This is a canadian shop in Halifax Nova Scotia and he has a number of engines in stock that he would build up for homebuilts. He is calling them homebuilt engines because he has a stock of engine parts he has bought at auctions and cannot legally put them in certified engines. This is a shop that also builds certified engines and all his engines come with a warrenty. I have delt with the owner myself and have no reservations in directing you to him. If I was looking for an engine this is where I would be going. I have no connection with this business other than customer. The shop is Aerotec Engines, the owner is Jason Crowell. Their numbers are 902-873-3100,phone 902-873-3101 fax and their email address is aerotec(at)dbis.ns.ca. Good Luck. Joe Hine RV4 C-FYTQ aerotec(at)dbis.ns.ca ________________________________________________________________________________
From: "Tim Greene" <timgreene@go-concepts.com>
Subject: Re: RV7-List: RV7-List Digest: 1 Msgs - 10/19/02
Date: Oct 21, 2002
?? ----- Original Message ----- From: "Nouj" <nouj(at)compuserve.com> Subject: RV7-List: RV7-List Digest: 1 Msgs - 10/19/02 > --> RV7-List message posted by: Nouj > > Not forward > > > > > > > ________________________________________________________________________________
From: "Rob W M Shipley" <Rob(at)RobsGlass.com>
Subject: Manual trim
Date: Oct 21, 2002
I've been waiting for this thread to die but it's proven quite durable. My 2 cents. I've put a MAC electric trim servo in the stab on my 9A and been planning a dual voltage supply switched by a microswitch on the flap mechanism in order to give two different rates of adjustment. This was as a result of the experiences reported on the list with difficulty at higher speeds in getting accurate trim settings. I will not be bothering with this unless I find it necessary. I flew the factory 9A at Copperstate and found no difficulty at all in getting the trim where I wanted it. A nudge one way or the other was all that was needed. Much better than my previous experience with cable operated trim systems. Rob Rob W M Shipley. RV9A fuselage. N919RV resvd. ________________________________________________________________________________
From: Parker43rp(at)aol.com
Date: Oct 21, 2002
Subject: Re: Electric Aileron Trim RV8 style
Russ---- I am concerned also that the aileron trim springs are excessively strong,although I have yet to mount them. Let us know what you find out. ---Ray ________________________________________________________________________________
From: DFCPAC(at)aol.com
Date: Oct 21, 2002
Subject: ivo propeller
has anyone tried the ivo in flight magnum propeller unit on an rv-4? dan carley ________________________________________________________________________________
From: "Carl Froehlich" <carlfro(at)erols.com>
Subject: Electric Aileron Trim RV8 style
Date: Oct 21, 2002
Russ, These are the correct springs - and they work as advertised. You will not notice the spring pressure when flying. You need to make sure you zero (center) the trim when you go to rig your ailerons. I am currently chasing a rigging problem with mine (adjust one side, screw up the other, etc.). Of interest, I flew the first 20 hours or so without touching the aileron trim. Once I started testing with one tank full, the other near empty and such it came in handy. I also have the Navaid Wing leveler - if you have this installed you may want to forgo the trim kit altogether. I like having both however. Carl Froehlich RV8A (flying - 40 hour flyoff completed Saturday) Vienna, VA -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Russ Werner Subject: RV-List: Electric Aileron Trim RV8 style Can anyone having experience with the RV8 electric aileron trim kit using the "sliding tube" comment on the spring pressures? Specifically I am interested in the springs Vans sent in your kit. Mine are quite strong and appear (contrary to earlier list posts) that they will impart excessive pressures on the controls. Mine are each 3 inches long (total) and the kit preloads them to about 4 inches. On the bench that is a very hard pull. At full aileron deflection, (my wings aren't on so I have to guess how far the stick needs to move to get there) they will be stretched to about 5 or more inches. I guess if they are too stiff I can get lighter ones of the same length but I thought I'd get comments from those with experience. Thanks, Russ Werner HRII Maui ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: leak
Date: Oct 21, 2002
Stein, My right tank did the same thing, I just cleaned and covered the whole sending unit with proseal. Now there's a wire coming out of a blob on the side of the tank, but no fuel. If I ever have to service it the tank is coming off, but it probably would have to anyway. W ________________________________________________________________________________
Date: Oct 21, 2002
From: Dan DeNeal <rv6apilot(at)yahoo.com>
Subject: How do you start an engine thats been sitting a long time?
I have an engine that was overhauled in 1994 and has been pickled all this time. We took off the sump and looked inside. Everything looked great. So now that I have drained all the oil out and put mineral oil in, what else do I need to do to make sure theirs no metal against metal? Their is not much comprassion, as I am told the rings are not set yet. Dan DeNeal Y! Web Hosting - Let the expert host your web site http://webhosting.yahoo.com/ ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: Vreg
Date: Oct 21, 2002
Lead acid battery's do not do well with any voltage source that is more than one volt over fully charged which is 12.68v or 2.11v per cell. It is a function of the galvanic response between lead and lead oxide. The adjustable V-reg is the only way to be sure you are at 13.68V. I have never seen a fixed V-reg sit at this in thirty years of working on charging systems. Anything more than 13.68V will shorten the life of your battery as the extra voltage causes extra current which translates into extra heat which dries out the battery. It also tends to sulfate the plates faster than normal. And finally, the extra voltage will shorten the life of all your light bulbs and electric motors as they are also not designed to work at higher voltages. Most digital circuits correct for this so they will be OK. W ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)jetstream.net>
Subject: Re: Power Chart...
Date: Oct 21, 2002
Bill: Looks good to me. Eustace ----- Original Message ----- From: "Bill" <n8wv(at)hotmail.com> Subject: RV-List: Power Chart... > > I have been thinking of ways to get better performance out of my 150 HP -8A, and this morning put together a page on my web site with some power info... Please have a look and let me know if I screwed anything up... > > Also, as always your comments are welcome... > > http://vondane.com/flightdata/powerinfo.htm > > -Bill > www.vondane.com > > ________________________________________________________________________________
From: "William Davis" <rvpilot(at)mpinet.net>
Subject: Re: Electric Aileron Trim RV8 style
Date: Oct 21, 2002
Russ, Install it as designed, it will work fine. You will not even notice the spring loads when flying and hardly notice them when on the ground due to the leverage of the stick. That much tension is necessary in order to balance out unequal fuel quantities. Bill, RV-8 N48WD ----- Original Message ----- From: "Russ Werner" <russ(at)maui.net> Subject: RV-List: Electric Aileron Trim RV8 style > > Can anyone having experience with the RV8 electric aileron trim kit using > the "sliding tube" comment on the spring pressures? Specifically I am > interested in the springs Vans sent in your kit. Mine are quite strong and > appear (contrary to earlier list posts) that they will impart excessive > pressures on the controls. Mine are each 3 inches long (total) and the kit > preloads them to about 4 inches. On the bench that is a very hard pull. At > full aileron deflection, (my wings aren't on so I have to guess how far the > stick needs to move to get there) they will be stretched to about 5 or more > inches. > > I guess if they are too stiff I can get lighter ones of the same length but > I thought I'd get comments from those with experience. > > Thanks, > > Russ Werner > HRII > Maui > > ________________________________________________________________________________
From: "Eustace Bowhay" <ebowhay(at)jetstream.net>
Subject: Re: How do you start an engine thats been sitting a long time?
Date: Oct 21, 2002
Hi Dan: I would not start it without preoiling it. This is done by forcing oil (preferable warm oil) through the entire oil system.The inside of the cylinders will also need preoiling. I would give Bart Lalonde a call at 250 376 1223 and get his instructions on how to handle a situation such as yours. I was in Aero Sport Power's facility today and saw the results of starting an engine that had not been properly cared for while in long term storage. It will probably cost in the area of $5000.00 to repair the damage. Eustace Bowhay Blind Bay, B.C. ----- Original Message ----- From: "Dan DeNeal" <rv6apilot(at)yahoo.com> Subject: RV-List: How do you start an engine thats been sitting a long time? > > I have an engine that was overhauled in 1994 and has > been pickled all this time. We took off the sump and > looked inside. Everything looked great. So now that I > have drained all the oil out and put mineral oil in, > what else do I need to do to make sure theirs no metal > against metal? > > Their is not much comprassion, as I am told the rings > are not set yet. > > Dan DeNeal > > http://webhosting.yahoo.com/ > > ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Oct 21, 2002
Subject: Re:Vreg
You don't have to use 30's lead-acid battery technology in your experimental aircraft. The Odyssey battery is hunreds of percent better and it doesn't spill. See : odysseybattery.com RV-4 , N1191X , Flying Now Charleston, Arkansas ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: How do you start an engine thats been sitting a long time?
Date: Oct 21, 2002
I pre oiled mine by using a garden sprayer. I put oil in the sprayer, and connected it to the oil return fitting on the back of the engine. Pump up the sprayer and let it slowly creep it's way through the engine. Put a few squirts of oil in the spark plug holes, and crank the engine a few times with the plugs removed to get oil pressure up. Then fire her up and get the grin! Paul Besing RV-6A Sold (Waiting on the RV-10) http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "Dan DeNeal" <rv6apilot(at)yahoo.com> Subject: RV-List: How do you start an engine thats been sitting a long time? > > I have an engine that was overhauled in 1994 and has > been pickled all this time. We took off the sump and > looked inside. Everything looked great. So now that I > have drained all the oil out and put mineral oil in, > what else do I need to do to make sure theirs no metal > against metal? > > Their is not much comprassion, as I am told the rings > are not set yet. > > Dan DeNeal > > http://webhosting.yahoo.com/ > > ________________________________________________________________________________
From: "Ed Bundy" <ebundy(at)velocitus.net>
Subject: Re: constant speed prop diameters
Date: Oct 21, 2002
Generally speaking, a 3 bladed prop is not as efficient as a 2 blade. I believe it has something to do with each blade hitting the disturbed air from the previous blade sooner, and with less forward travel before it hits it. I'm not positive on this however. I do know from personal experience changing from a 2 blade to a 3 blade on a C182 lowered the climb rate very slightly, and cruise/top speed was also slightly less. However, there was a BIG improvement in smoothness. 3 blades smoothed out the firing pulses on the engine much better than 2. IIRC, the climb rate suffered something less than 100fpm, and cruise was a few knots. Ed Bundy RV6A 500+ hours Boise, ID > the tandem models. Considering a fixed pitch 3-blade pitched for cruise on a > -6/6A, does anyone have any actual experience on top speed performance for this > combination vs. fixed pitch 2-blade, assuming well designed and built props are > part of the equation? (Performance Props and Catto as examples) I am buying > soon and interested in a 3-blade, primarily for noise reduction, provided cruise > speed does not suffer- I have seen references to reduced climb rate, but this > would be an acceptable trade off. ________________________________________________________________________________
From: "Bill VonDane" <n8wv(at)hotmail.com>
Subject: Re: ivo propeller
Date: Oct 21, 2002
I just sent an email to IVO this morning, and they told there was NO chance that they would sell an IVO for a Lycoming... -Bill www.vondane.com ----- Original Message ----- From: <DFCPAC(at)aol.com> Subject: RV-List: ivo propeller has anyone tried the ivo in flight magnum propeller unit on an rv-4? dan carley ________________________________________________________________________________
From: JDaniel343(at)aol.com
Date: Oct 21, 2002
Subject: Re:Vreg
Maybe I'm wrong, but I thought the sealed batteries required something like 14.5 volts of charging power or they won't last but a couple of years. John Danielson N106WP 90 Hrs ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: TruTrak control stops
Date: Oct 22, 2002
For those using the TruTrak APs: Are you using the stops that come with, and mount to, the servos, or relying on the control stops on your RV? If both, wouldn't they have to be calibrated to be equal -- both allowing exactly xx.x degrees of travel, for example? Seems like that would be hard to do accomplish... - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com ________________________________________________________________________________
Date: Oct 21, 2002
From: David Aronson <aronsond(at)pacbell.net>
Subject: Re: TruTrak control stops
Listers: Concerning the stops. I have installed a Trutrack in my RV4. No way could I use the stock stops. I fabricated new ones out of angle stock. The stops prevent an over-center condition. I do not see them needing to be exactly equal distant in range. Your built in stops are probably going to be about the same, maybe a little outside the perameters of the stops on the Trutrak. The installation instructions advise that it is OK to use your built in control stops if you cannot fit stops on the unit. Just set them up as directed and it seems to work fine. Dave Aronson RV4 N504RV ----- Original Message ----- From: "Larry Bowen" <Larry(at)bowenaero.com> Subject: RV-List: TruTrak control stops > > For those using the TruTrak APs: > > Are you using the stops that come with, and mount to, the servos, or > relying on the control stops on your RV? If both, wouldn't they have to > be calibrated to be equal -- both allowing exactly xx.x degrees of > travel, for example? Seems like that would be hard to do accomplish... > > - > Larry Bowen > Larry(at)BowenAero.com > http://BowenAero.com > > ________________________________________________________________________________
From: LessDragProd(at)aol.com
Date: Oct 22, 2002
Subject: Re: RV4-List: ivo propeller
Hi Dan, I've been flying the Ivoprop Magnum electric prop since Dec. 1995 on my RV-3. Is that close enough to a RV-4? I don't believe Ivo is selling their prop for four cylinder four cycle engines, and engines with certain gear boxes. Check with them at http://www.ivoprop.com Jim Ayers RV-3 N47RV LOM M332A engine 140 HP at 2700RPM and 35"MP (Love that supercharger! :-) ) ________________________________________________________________________________
From: "flyseaplane" <flyseaplane(at)netzero.net>
Subject: Re: RV4-List: ivo propeller
Date: Oct 22, 2002
As far as the Ivo Prop goes, the LOM inline engine is a great candidate. It seems to run a lot smoother than the Lycomings. I seem to remember talking to a guy in Montana a few years ago that had the Ivo electric prop on an Avid Magnum and was having problems with it. Just to much engine for a flimsy prop design. I love my Warp Drive 72" 3-blade ground adjustable. Lots of Murphy Rebel guys run them on 150-160 HP. Its great for STOL planes, I wonder if anyone has ever put one on an RV???? ------------------------------------------------------ ------------------------------------------------------ I don't believe Ivo is selling their prop for four cylinder four cycle > engines, and engines with certain gear boxes. Check with them at > http://www.ivoprop.com > > Jim Ayers > RV-3 N47RV LOM M332A engine 140 HP at 2700RPM and 35"MP > (Love that supercharger! :-) ) ------------------------------------------- Introducing NetZero Long Distance Unlimited Long Distance only $29.95/ month! Sign Up Today! www.netzerolongdistance.com ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re:Vreg
Date: Oct 22, 2002
Hi John, That was true of the Gell Cell types. The newer RG batteries look the same but don't require the higher charge Rate. Go to http://www.aeroelectric.com/ and root around till you find Bob's info on RG battery technology and lots of other stuff. Jim in Kelowna ----- Original Message ----- From: <JDaniel343(at)aol.com> Subject: Re: RV-List: Re:Vreg > > Maybe I'm wrong, but I thought the sealed batteries required something like > 14.5 volts of charging power or they won't last but a couple of years. > > John Danielson > N106WP 90 Hrs > > ________________________________________________________________________________
From: "Pat Hatch" <pat_hatch(at)msn.com>
Subject: Re:Vreg
Date: Oct 22, 2002
John, I recently purchased a 32 AH, sealed lead-acid battery from B & C and the flyer that came with it recommended re-setting regulator voltage to 14.2 to 14.6 volts for charging operations. Hope this helps, Pat Hatch RV-4, N17PH, 700 hrs O-320, Hartzell C/S RV-6, N44PH, 30 hrs O-360, Hartzell C/S Vero Beach, FL ----- Original Message ----- From: <JDaniel343(at)aol.com> Subject: Re: RV-List: Re:Vreg > > Maybe I'm wrong, but I thought the sealed batteries required something like > 14.5 volts of charging power or they won't last but a couple of years. > > John Danielson > N106WP 90 Hrs > > ________________________________________________________________________________
From: "Rick Jory" <rickjory(at)msn.com>
Subject: FAA DAR Checklist
Date: Oct 22, 2002
FYI, my FSDO sent me a list that they suggest the DAR uses as part of an amateur-built aircraft inspection. This is lengthy, if not interested delete: 1. Does the builder have FAA Form 8050-3 (aircraft registration documentation, obtained via Aircraft Registry in Oklahoma City)? 2. Is the registration number affixed on the aircraft in compliance with FAR's 45.21 through 45.29 [personal note: this is supposed to be "permanent" . . . if you haven't painted your plane one technique which I think is deemed okay is to have a sign shop cut your N-numbers via vinyl. These can be applied and then removed prior to painting.] 3. Does the builder have an airplane and engine logbook? Do logbook entries, data plate, and information on FAA forms have the same builder, model, and serial number? 4. Is the current weight and balance recorded in legible format? 5. Is the word "EXPERIMENTAL" at least 2" minimum height and affixed onto the aircraft in compliance with FAR 45.23(b)? 6. Are required instruments installed and properly marked? 7. Are cockpit controls identified as to function and position? Examples: fuel, throttle, carburetor heat, flaps, trim, etc. 8. Is the aircraft data plate attached to the aircraft in accordance with FAR's 45.11 and 45.13? 9. Is the passenger warning placard installed? 10. Have records been maintained and recorded in compliance with FAR 91.417? 11. Is the aircraft equipped with an Emergency Locator Transmitter (ELT) in compliance with the requirements of FAR 91.207? 12. If applicable, ahs a radio station license been issued for the aircraft? 13. Are approved seat belts installed at all seating locations? 14. Have an original and one copy of the letter of request for experimental, FAA Form 8130-6 and FAA Form 8130-12, a three-view drawing or photos with aircraft dimensions been prepared? 15. Is there a checklist schedule of proposed flight test or aircraft operating instructions for FAA review at the time of aircraft release for flight? 16. Has the aircraft flight, engine, and landing gear been rigged and checked for proper operation to the satisfaction of manufacturer's instruction? 17. Has the aircraft fuel system(s) been leak, vent, pressure and flow checked and found satisfactory? 18. Is the aircraft considered complete in every detail by the builder? 19. Has the applicant made application in accordance with AC 20-27D paragraph 10d? Rick Jory, RV8A ________________________________________________________________________________
From: "Wiethe, Philip (P.J.)" <pwiethe(at)ford.com>
Subject: Trim tab question
Date: Oct 22, 2002
I have had to bend the bottom forward flange (non hinged side) on my trim tab up at quite an angle to clear the elevator skin enough to allow the trim tab to rotate down 35 degrees for max nose up trim. It doesn't look like it will have any negative effect, I just wondered it this was common, or if my clearance between the tab and elevator skin was too tight. Phil 8A - emp complete, wings started. ________________________________________________________________________________
Subject: Trim tab question
Date: Oct 22, 2002
From: "Todd Wenzel" <TWenzel@heartland-software.com>
I don't remember having to do anything to the trim tab to get the proper deflection. Todd Wenzel Delafield, WI USA RV-8AQB - Finish Kit N900TW - Reserved TWenzel@Heartland-Software.com -----Original Message----- From: Wiethe, Philip (P.J.) [mailto:pwiethe(at)ford.com] Subject: RV-List: Trim tab question --> I have had to bend the bottom forward flange (non hinged side) on my trim tab up at quite an angle to clear the elevator skin enough to allow the trim tab to rotate down 35 degrees for max nose up trim. It doesn't look like it will have any negative effect, I just wondered it this was common, or if my clearance between the tab and elevator skin was too tight. Phil 8A - emp complete, wings started. ________________________________________________________________________________
From: "Bill" <n8wv(at)hotmail.com>
Subject: Re: Rudder Pedal Return Springs
Date: Oct 22, 2002
Hey Joe... I tried this and it worked! I am going to work on it a little bit more, but the little bit of tweaking I did do seems to have works wonders... What I did was make some 6" extensions out of .032 for my hand seamers, and just went up the trailing edge of the rudder, squeezing it in a bit each time until I got a good even edge... -Bill www.vondane.com ----- Original Message ----- From: "Joe Hine" <joehine(at)nbnet.nb.ca> Subject: RE: RV-List: Rudder Pedal Return Springs I can remember reading about someone with this problem and it was cured by squeezing down the trialing edge of the rudder. The same way you do to correct a heavy wing, very gently and progressively until the problem gets better. If the radius of the bend is a bit large, it seems to cause the tail wag. Joe Hine C-FYTQ ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: Las Cruces Saturday
Date: Oct 22, 2002
Anyone from the Denver area and south wanting to join up Saturday morning for a group arrival at Las Cruces contact, write back so we can set up a flight plan. Our tentative plans are for 3 planes to depart Granby, CO at 7:00am, pick up some people at Centeniel in Denver at about 7:30, then head south for fuel and breakfast at Belen, NM, around 9:30, then on to Cruces arriving around 11:00. Andy winterland(at)rkymtnhi.com ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: Flight simulator survey
Date: Oct 22, 2002
We are considering setting up a web catalog to sell discounted Jeppesen Flight Simulators. Since I don't know much about these or how popular they'd be, I thought I'd get some feedback from the group. After all, all of us here are folks that 1] like airplanes, 2] like computers, and 3] can afford toys. I can't think of a better source of information. As a very brief description, these things come in Basic, Advanced, and FAA Approved models ranging from about $700 - $2000. They include all the gadgets, controls, and software, and are designed to help you practice navigation and instrument approaches all over the world. (I'm not sure if you could bomb Bagdad, but you definitely can land there - even in the SMOKE and haze.) So, in an as anonymous a fashion as possible (considering your sending me an e-mail), please check which statement applies and reply to me at agold(at)buildersbooks.com ___ I have no interest in flight simulators ___ I may be interested if the price was right ___ I've always wanted one. Write back when your ready ___ I've got one and I use it often ___ I've got one; its in the closet full of dust Thank you, Andy ________________________________________________________________________________
Date: Oct 22, 2002
Subject: Control stops/ autopilot servos
From: czechsix(at)juno.com
Regarding the thread on servo control stops, keep in mind that the primary control stops for any axis should be at the control surface...aileron, elevator, etc. The stops on the Tru Trak servos should not even make contact at full control deflections. They are there as a backup to make sure the servo control arm never goes over-center and jams the controls (i.e. on the RV-8, if the collet were to slip, etc.) --Mark Navratil Cedar Rapids, Iowa RV-8A N2D sanding fiberglass...main wheel pants and gear leg fairings... Sign Up for Juno Platinum Internet Access Today Only $9.95 per month! Visit www.juno.com ________________________________________________________________________________
Date: Oct 22, 2002
From: P M Condon <pcondon(at)mitre.org>
Subject: Re: How do you start an engine thats been sitting a long time
Pre-oiler I used a metal weed sprayer from the garden store, put in 6 qts of hot oil, drained the oil in the engine so I could verify all 6 qts of hot oil went into the engine (checked the dip stick). Pumped up sprayer and pushed oil in via the oil cooler line into the engine. I did this on both oil lines (intake to the cooler and return). Fogged the cylinders with oil before I started. I also cranked the engine with the elect. starter for a few minutes to get oil pressure reading (40 lbs) before re-installing the plugs for the first start. Can't be certain I did any good, but I felt much ($$$) beter...... Hi Dan: I would not start it without preoiling it. This is done by forcing oil (preferable warm oil) through the entire oil system.The inside of the cylinders will also need preoiling. I would give Bart Lalonde a call at 250 376 1223 and get his instructions on how to handle a situation such as yours. I was in Aero Sport Power's facility today and saw the results of starting an engine that had not been properly cared for while in long term storage. It will probably cost in the area of $5000.00 to repair the damage. Eustace Bowhay Blind Bay, B.C. ----- Original Message ----- From: "Dan DeNeal" <rv6apilot(at)yahoo.com> Subject: RV-List: How do you start an engine thats been sitting a long time? ________________________________________________________________________________
Date: Oct 22, 2002
From: Larry Bowen <lcbowen(at)yahoo.com>
Subject: Re: TruTrak control stops
See below: --- David Aronson wrote: > > Listers: > Concerning the stops. I have installed a Trutrack in my RV4. No way could > I use the stock stops. I fabricated new ones out of angle stock. The stops > prevent an over-center condition. I do not see them needing to be exactly > equal distant in range. I meant the servos-mounted stops must allow equal travel as the airplane-mounted stops. If the servos are allowing 10` travel, but the 'normal' stops allow 20`, the TruTrak stops are 'robbing' you of 10` of travel. Thus they should be equal -- both 20` in this example. Right? I'll leave the servo-mounted stops off for now and see if things are still within spec using the other control stops. Thanks. -LB > Your built in stops are probably going to be about > the same, maybe a little outside the perameters of the stops on the Trutrak. > The installation instructions advise that it is OK to use your built in > control stops if you cannot fit stops on the unit. Just set them up as > directed and it seems to work fine. > Dave Aronson > RV4 N504RV > ----- Original Message ----- > From: "Larry Bowen" <Larry(at)bowenaero.com> > To: > Subject: RV-List: TruTrak control stops > > > > > > For those using the TruTrak APs: > > > > Are you using the stops that come with, and mount to, the servos, or > > relying on the control stops on your RV? If both, wouldn't they have to > > be calibrated to be equal -- both allowing exactly xx.x degrees of > > travel, for example? Seems like that would be hard to do accomplish... > > > > - > > Larry Bowen > > Larry(at)BowenAero.com > > http://BowenAero.com http://webhosting.yahoo.com/ ________________________________________________________________________________
Date: Oct 22, 2002
From: Larry Bowen <lcbowen(at)yahoo.com>
Subject: Re: Control stops/ autopilot servos
Ah....I guess that makes sense. I only received one stop - it was mounted on the pitch servo. Sounds like I'm missing a stop. There is also a rivet in the collet, in my plans, to act a safety against slipping. -LB --- czechsix(at)juno.com wrote: > > Regarding the thread on servo control stops, keep in mind that the primary > control stops for any axis should be at the control surface...aileron, > elevator, etc. The stops on the Tru Trak servos should not even make contact > at full control deflections. They are there as a backup to make sure the > servo control arm never goes over-center and jams the controls (i.e. on the > RV-8, if the collet were to slip, etc.) > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D sanding fiberglass...main wheel pants and gear leg fairings... > http://webhosting.yahoo.com/ ________________________________________________________________________________
From: "Jack Textor" <jack(at)iajobs.com>
Subject: Flight simulator survey
Date: Oct 22, 2002
Jack Textor PERSONNEL INCORPORATED Established 1963 515-243-7687 www.iaJobs.com www.personneliowa.com -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Aircraft Technical Book Company Subject: RV-List: Flight simulator survey We are considering setting up a web catalog to sell discounted Jeppesen Flight Simulators. Since I don't know much about these or how popular they'd be, I thought I'd get some feedback from the group. After all, all of us here are folks that 1] like airplanes, 2] like computers, and 3] can afford toys. I can't think of a better source of information. As a very brief description, these things come in Basic, Advanced, and FAA Approved models ranging from about $700 - $2000. They include all the gadgets, controls, and software, and are designed to help you practice navigation and instrument approaches all over the world. (I'm not sure if you could bomb Bagdad, but you definitely can land there - even in the SMOKE and haze.) So, in an as anonymous a fashion as possible (considering your sending me an e-mail), please check which statement applies and reply to me at agold(at)buildersbooks.com ___ I have no interest in flight simulators _x__ I may be interested if the price was right ___ I've always wanted one. Write back when your ready ___ I've got one and I use it often ___ I've got one; its in the closet full of dust Thank you, Andy ________________________________________________________________________________
Date: Oct 22, 2002
From: David Wentzell <wntzl(at)execpc.com>
Subject: Re: do not forward
Do Not Forward ________________________________________________________________________________
Date: Oct 22, 2002
From: rob ray <smokyray(at)yahoo.com>
Subject: Re: RV4-List: ivo propeller
Several years ago I seriously researched buying an IVO Magnum for my RV4. I found Four guys who had bought and flown them on RV's and all four had cracks in the gelcoat after 25 hours. I called IVO and asked if the problem was solved and never heard back. There is an RV3 with a LOM engine and IVO electric C/S prop flying, I spoke to him at Van's. I compromised and bought a Catto Composite... RR --- flyseaplane wrote: > --> RV4-List message posted by: "flyseaplane" > > > As far as the Ivo Prop goes, the LOM inline engine > is a great candidate. It > seems to run a lot smoother than the Lycomings. I > seem to remember talking > to a guy in Montana a few years ago that had the Ivo > electric prop on an > Avid Magnum and was having problems with it. Just to > much engine for a > flimsy prop design. > > I love my Warp Drive 72" 3-blade ground adjustable. > Lots of Murphy Rebel > guys run them on 150-160 HP. Its great for STOL > planes, I wonder if anyone > has ever put one on an RV???? > ------------------------------------------------------ > ------------------------------------------------------ > > I don't believe Ivo is selling their prop for four > cylinder four cycle > > engines, and engines with certain gear boxes. > Check with them at > > http://www.ivoprop.com > > > > Jim Ayers > > RV-3 N47RV LOM M332A engine 140 HP at 2700RPM and > 35"MP > > (Love that supercharger! :-) ) > > > ------------------------------------------- > Introducing NetZero Long Distance > Unlimited Long Distance only $29.95/ month! > Sign Up Today! www.netzerolongdistance.com > > > > Contributions of > any other form > > latest messages. > other List members. > > http://www.matronics.com/subscription > http://www.matronics.com/photoshare > http://www.matronics.com/search > http://www.matronics.com/archives > http://www.matronics.com/emaillists > > > > > http://webhosting.yahoo.com/ ________________________________________________________________________________
From: Imfairings(at)aol.com
Date: Oct 22, 2002
Subject: Re: Just can't get this smile off of my face
Congratulations Fran, That smile will continue to return time and time again to your face. Bob Fairings-Etc. ________________________________________________________________________________
From: LessDragProd(at)aol.com
Date: Oct 23, 2002
Subject: Re(2): RV4-List: ivo propeller
In a message dated 10/22/2002 7:50:57 PM Pacific Daylight Time, smokyray(at)yahoo.com writes: > There is an > RV3 with a LOM engine and IVO electric C/S prop > flying, I spoke to him at Van's. I compromised and > bought a Catto Composite... > > RR > Sounds like a good choice. Jim Ayers RV-3 N47RV LOM M332A engine Ivoprop Magnum electric prop flown since Dec. 1995 very nervously. I believe Ivo hasn't sold his prop for Lycoming engines for a couple years. Warp drive wasn't successful on a Lycoming, either. Makes me wonder about the new CS props using Warp drive blades. Anyone have any history on the new CS props with the Warp drive blades on a Lycoming? ________________________________________________________________________________
From: RV8DRIVER(at)aol.com
Date: Oct 23, 2002
Subject: Re: RV-List Digest: 43 Msgs - 10/21/02
UN/SUBSCRIBE: http://www.matronics.com/subscription ________________________________________________________________________________
Subject: Affordable Turbine Power Engine
From: Don.Alexander(at)AstenJohnson.com
Date: Oct 23, 2002
10/23/2002 07:36:45 AM Have any of you heard any news from ATP regarding their turboprop engine. There have been no updates to the website recently and was wondering if they had tanked. I saw them at SunNFun with the RV-4 rigged with the turboprop and it looked interesting. RV-8A Fuel Tanks Loving every minute of it! ________________________________________________________________________________
Date: Oct 23, 2002
From: Virgil Young <vwyoung(at)comcast.net>
Subject: RV7 quickbuild slider
I'm interested in a 180hp Lycoming which does not require air induction scoop on the lower cowling. My understanding is this requires a forward sump and horizontal induction. Would appreciate anyone's research along with recommended prop governor and constant speed prop.Virgil Young.#1017 ________________________________________________________________________________
From: "Sluggo" <rdcompton(at)earthlink.net>
Subject: Re: Ready-to-install Spinner
Date: Oct 23, 2002
> I bought a polished aluminum spinner from George & > Becky Orndorff (sp?) and it fits Van's backplate, etc. Cutting the "cut > out" for the blade (in my case, a Hartzell C/S prop) was easy . . . mainly > because somewhere on the net I got a pattern and used this as a start. Yep, been down this route. I bought the Orndorff polished spinner, too. Real pretty, I might add. Had a template, too, from an existing fitted fiberglass spinner. So far, so good. > Needless to say, the pattern gets you the rough "size" . . . which I cut > using a Dremmel and cut-off wheel . . . then "final" sizing can be done with > a die grinder and 2" (or 1") scotchbrite wheels (Avery, etc.). The process > is really simple and it is hard to make a mistake. Ah, here was the "rub", as they say. The Orndorff's also said that a Dremel was the way to go and should be "simple and hard to make a mistake." Well, maybe for you all. Ham-fisted me let the Dremel get away and walk nicely across the spinner, leaving a lovely etched trail, as well as a ruined pricey polished spinner, in its wake. >Anyway, don't know a source for a spinner that is pre-cut for the prop, but what I've explained > above was fairly straightforward. Good luck. > Rick Jory RV8A Well, my search will go on. The polished spinner fabrication learning curve might get too expensive to risk buying them 'till I get it right. Thanks for the info, though. Randy Compton RV-3A (with a trashed polished spinner) N84VF Gulf Breeze, FL ________________________________________________________________________________
Subject: Calgary Hangar Opportunity
Date: Oct 23, 2002
From: "Gannon, Terence" <Terence.Gannon(at)trican.ca>
A quick message to those building in and around the Calgary/Southern Alberta area that will eventually need hangar space for their finished aircraft, and/or workspace for their project, and would like to be located at Springbank (CYBW). Some new hangars are going up, and I'm investigating whether there is sufficient interest in some sort of arrangement to share space in one or two of the newly constructed bays. Please contact me directly, off list, to discuss further. Best regards... Terry in Calgary RV-6 S/N 24414 "Wings, Fuselage Arriving Today!" terence.gannon(at)trican.ca ________________________________________________________________________________
Date: Oct 23, 2002
From: Larry Bowen <lcbowen(at)yahoo.com>
Subject: Re: Ready-to-install Spinner
You can't buff it out? -LB --- Sluggo wrote: > > > Ah, here was the "rub", as they say. The Orndorff's also said that a Dremel > was the way to go and should be "simple and hard to make a mistake." Well, > maybe for you all. Ham-fisted me let the Dremel get away and walk nicely > across the spinner, leaving a lovely etched trail, as well as a ruined > pricey polished spinner, in its wake. ________________________________________________________________________________
Date: Oct 23, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Ready-to-install Spinner
Sluggo wrote: > > Ah, here was the "rub", as they say. The Orndorff's also said that a Dremel > was the way to go and should be "simple and hard to make a mistake." Well, > maybe for you all. Ham-fisted me let the Dremel get away and walk nicely > across the spinner, leaving a lovely etched trail, as well as a ruined > pricey polished spinner, in its wake. Randy, don't trash the spinner yet! Use 320 grit wet/dry paper with water to sand out the trail. Once the trail is sanded out (I assume the "trail" is largely cosmetic and not deep enough to create structural problems) follow the 320 with 600, then 1200, then a buffing wheel with polishing compound. Sam Buchanan ________________________________________________________________________________
From: "John Starn" <jhstarn(at)earthlink.net>
Subject: Re: Ready-to-install Spinner
Date: Oct 23, 2002
Duct tape.... use several layers of good ole duct tape to outline the openning on the spinner. It may not be perfect against the "ham fisted" but it gives protection for the little slip of the wheel. Warning: Cut the same day you put it on and take it off as soon as the cut is completed. (works witth fibreglas and plastic too). KABONG ----- Original Message ----- From: "Larry Bowen" <lcbowen(at)yahoo.com> Subject: Re: RV-List: Ready-to-install Spinner > > You can't buff it out? > > -LB > > --- Sluggo wrote: > > > > > > Ah, here was the "rub", as they say. The Orndorff's also said that a Dremel > > was the way to go and should be "simple and hard to make a mistake." Well, > > maybe for you all. Ham-fisted me let the Dremel get away and walk nicely > > across the spinner, leaving a lovely etched trail, as well as a ruined > > pricey polished spinner, in its wake. > > ________________________________________________________________________________
From: "Meier, George" <George.Meier(at)goodrich.com>
Subject: Another good engine scorce
Date: Oct 23, 2002
I just thought I would pass along another good engine shop that would be worth getting a quote from if you are looking for an engine. This is a canadian shop in Halifax Nova Scotia and he has a number of engines in stock that he would build up for homebuilts. He is calling them homebuilt engines because he has a stock of engine parts he has bought at auctions and cannot legally put them in certified engines. This is a shop that also builds certified engines and all his engines come with a warrenty. I have delt with the owner myself and have no reservations in directing you to him. If I was looking for an engine this is where I would be going. I have no connection with this business other than customer. The shop is Aerotec Engines, the owner is Jason Crowell. Their numbers are 902-873-3100,phone 902-873-3101 fax and their email address is aerotec(at)dbis.ns.ca. This shop did a great job on the IO360 in my Pitts. I concur with this recommendation. With the current exchange rate, they offer prices that can't be beat. George Meier RV6A wings Pitts S-1D N61BY ________________________________________________________________________________
From: "Jack Textor" <jack(at)iajobs.com>
Subject: Affordable Turbine Power Engine
Date: Oct 23, 2002
Don, They were at OSH, I was at the flight line at their published times to fly, but never caught the 4 in the air. There was a nice air-to-air photo in this months Sport Aviation. The fellow I talked with from ATP said the improvements should be ready in 2003. Jack Textor RV8, wings forever DSM Have any of you heard any news from ATP regarding their turboprop engine. There have been no updates to the website recently and was wondering if they had tanked. I saw them at SunNFun with the RV-4 rigged with the turboprop and it looked interesting. RV-8A Fuel Tanks Loving every minute of it! ________________________________________________________________________________
From: "Phil Birkelbach" <phil(at)petrasoft.net>
Subject: Re: RV7-List: RV7 quickbuild slider
Date: Oct 23, 2002
I talked to Superior Air Parts last week and they are developing a "cool air" induction system for the O-360 (acutally it would be for their XP-360, but it should fit the O) The system will keep the induction path outside the sump so the oil does not warm it up. This should increase power and efficiency. You will not be able to install a carb though. The sump would have the forward induction placement which would require a fuel injection servo because of the orientation. The carb would not work very well mounted at a 90 deg angle. If I understand it correctly you wouldn't want the fuel/air mixture from the carb to go straight to the jug anyway for carb ice reasons. I believe that was the reason for routing the fuel/air mixture through the sump in the first place. I am no engine expert so don't quote me on this! Just for reference moving to the Airflow Performance fuel injection system will be about a $2500 - $3000 net increase in the price of the engine. The sump is supposed to be ready sometime early next year. The Ellison TBI might work but you may still have to deal with a carb ice issue. Anyway to make a short story long this new sump would allow you to use the cowl from Van's that doesn't have the bottom scoop on it. Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB (Reserved) - Fuselage http://www.myrv7.com ----- Original Message ----- From: "Virgil Young" <vwyoung(at)comcast.net> Subject: RV7-List: RV7 quickbuild slider > --> RV7-List message posted by: Virgil Young > > I'm interested in a 180hp Lycoming which does not require air induction scoop on the lower cowling. My understanding is this requires a forward sump and horizontal induction. Would appreciate anyone's research along with recommended prop governor and constant speed prop.Virgil Young.#1017 > > ________________________________________________________________________________
Date: Oct 23, 2002
From: RV9 <rv9(at)charter.net>
Subject: New Builder introduction
Hello, My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit number 609 which I received on the 10th of October. I've finished all of the prep work on the HS and I'm awaiting better weather here in North Texas (Granbury) before priming my HS parts. I've also begun work on the VS. I have a very crude (in comparison to some of you guys) website that's intended to allow my non-builder friends and relatives to track my progress. You are, of course, welcome to visit. Comments, suggestions, motiviations, etc. are all welcome. http://webpages.charter.net/smottin Steve Mottin RV-9A Empennage Granbury, Texas mailto:rv9(at)charter.net ________________________________________________________________________________
From: "flyseaplane" <flyseaplane(at)netzero.net>
Subject: RV4-List: ivo propeller
Date: Oct 23, 2002
Jim Ayers - - - Sorry to all that this is the RV list - I have never heard of anyone having problems with their Warp Drive on a Lycoming. That is, the ground adjustable ones. What have you heard?? I know a guy who has one on a 160 HP and has had no problems for the six years that it has been flying (about 800 hours now) Thanks, Linc > RV-3 N47RV > LOM M332A engine > Ivoprop Magnum electric prop flown since Dec. 1995 very nervously. > I believe Ivo hasn't sold his prop for Lycoming engines for a couple years. > Warp drive wasn't successful on a Lycoming, either. Makes me wonder about > the new CS props using Warp drive blades. Anyone have any history on the new > CS props with the Warp drive blades on a Lycoming? ------------------------------------------- ________________________________________________________________________________
From: "Albert Gardner" <albert.gardner(at)worldnet.att.net>
Subject: Re: RV9-List: New Builder introduction
Date: Oct 23, 2002
Hey Steve, welcome to the list. You may or may not know but many builders of the pre-punched kits are skipping the step of putting the parts together and then opening up the 3/32" holes with a #40 drill. They first dimple the individual parts (which opens up the holes slightly) and then clecoe it up and set the rivets. I know of several guys who built wings without even thinking about twist while building. After the skins were riveted on they checked and found out there was zero twist. In any case you are going to have fun. Albert Gardner, Yuma, AZ RV-9A: N872RV (After 2 years I can see the end from here.) ----- Original Message ----- From: "RV9" <rv9(at)charter.net> Subject: RV9-List: New Builder introduction > --> RV9-List message posted by: RV9 > > > Hello, > > My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit > number 609 which I received on the 10th of October. I've finished all > of the prep work on the HS and I'm awaiting better weather here in > North Texas (Granbury) before priming my HS parts. I've also begun work > on the VS. > > I have a very crude (in comparison to some of you guys) website that's > intended to allow my non-builder friends and relatives to track my > progress. You are, of course, welcome to visit. Comments, suggestions, > motiviations, etc. are all welcome. > > http://webpages.charter.net/smottin > > Steve Mottin > RV-9A Empennage > Granbury, Texas mailto:rv9(at)charter.net > > ________________________________________________________________________________
From: Larry Hawkins <lhawkins(at)giant.com>
Subject: Inverted oil system
Date: Oct 23, 2002
Does anyone have any experience with this inverted oil system built by Raven aircraft (Pitts). Check it out at; http://www.ravenaircraft.com/raven_001.htm Larry Hawkins, RV-4 Farmington, NM, N-345SL, finishing. ________________________________________________________________________________
From: "Randy Compton" <rdcompton(at)earthlink.net>
Subject: Re: Ready-to-install Spinner
Date: Oct 23, 2002
> Randy, don't trash the spinner yet! Use 320 grit wet/dry paper with > water to sand out the trail. Once the trail is sanded out (I assume the > "trail" is largely cosmetic and not deep enough to create structural > problems) follow the 320 with 600, then 1200, then a buffing wheel with > polishing compound. > > Sam Buchanan No, I've still got it. I was so bummed that I didn't think about any "salvage" work. The marring is not very deep, so I don't think there is a structural problem. I'll go ahead and give sanding/scotchbriting a try. Thanks for tip! Randy Compton N84VF RV-3A Gulf Breeze, FL ________________________________________________________________________________
From: "Steve Struyk" <rv8striker(at)hotmail.com>
Subject: fiberglass information
Date: Oct 23, 2002
I have put off, far too long now, all my fiberglass work. I guess what I need is an introduction to the basics. Is there a video or perhaps or book to explain fiberglass for the beginner? Any advice would be appreciated. Thanks in advance Steve Struyk St. Charles MO RV-8 N842S (Res.) ________________________________________________________________________________
Date: Oct 23, 2002
From: Richard Tasker <retasker(at)optonline.net>
Subject: Drill and dimple vs just dimple (was:New Builder introduction)
I am currently finishing up my RV9 empennage kit and expect to get the wing kit in a few weeks. I have noticed while building the empennage that the pre-punched holes always line up so all you are really seem to be doing is just enlarging the holes with the "match" drilling. Furthermore, when you dimple the drilled hole, the resulting hole is actually a little oversize for the rivet (per standard rivet specifications). Dimpling the existing holes would actually create a better fit to the rivet. I would like to solicit opinions as to the procedure noted below. That is, what are the advantages and drawbacks of following the instructions to drill then dimple vs just dimple as is. Of course, it goes without saying that your dimple tool should fit into the existing holes before dimpling (which might require slight grinding of the dimple tool pilot shaft). Dick Tasker, 90573 Albert Gardner wrote: >--> RV9-List message posted by: "Albert Gardner" > >Hey Steve, welcome to the list. You may or may not know but many builders of >the pre-punched kits are skipping the step of putting the parts together and >then opening up the 3/32" holes with a #40 drill. They first dimple the >individual parts (which opens up the holes slightly) and then clecoe it up >and set the rivets. I know of several guys who built wings without even >thinking about twist while building. After the skins were riveted on they >checked and found out there was zero twist. In any case you are going to >have fun. >Albert Gardner, Yuma, AZ >RV-9A: N872RV >(After 2 years I can see the end from here.) > >----- Original Message ----- >From: "RV9" <rv9(at)charter.net> >To: >Subject: RV9-List: New Builder introduction > > > > >>--> RV9-List message posted by: RV9 >> >> >>Hello, >> >>My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit >>number 609 which I received on the 10th of October. I've finished all >>of the prep work on the HS and I'm awaiting better weather here in >>North Texas (Granbury) before priming my HS parts. I've also begun work >>on the VS. >> >>I have a very crude (in comparison to some of you guys) website that's >>intended to allow my non-builder friends and relatives to track my >>progress. You are, of course, welcome to visit. Comments, suggestions, >>motiviations, etc. are all welcome. >> >>http://webpages.charter.net/smottin >> >>Steve Mottin >>RV-9A Empennage >>Granbury, Texas mailto:rv9(at)charter.net >> >> >> >> > > > > ________________________________________________________________________________
From: "Dane Sheahen" <dane(at)mutualace.com>
Subject: RV Fuel Injection Help
Date: Oct 23, 2002
My problem is this. While flying near Sylvania Airport in Wisconsin in my new RV8a (50 hrs) I had a total loss of power. The engine (IO-360a, Bendix Servo) was coughing, sputtering backfiring & wind milling all the way down to airport that I just happened to be near. As I rolled out on the runway the prop quit turning. I tried to restart on the runway and flooded it. In the air I did the following: Fly the plane & head for airport (alt. 1500 agl) Fuel pump on Circuit breaker check Full power throttle on Full rich Did not switched tanks but it was full Missed Semi-Truck on highway near the approach and landed the plane. On the ground the mechanic at Sylvania came out on a Sunday and check spark (mag & LightSpeed) not a problem. Cleaned the bottom plugs and we restarted the engine. It ran fine. I came back Monday and checked the complete fuel system from the tank to the filter to the lines plenty of fuel. We put I back together and it ran fine. Ran it up to 2000 rpm switched tanks, boost pump on & off, mixture rich to lean, turned off fuel while running until she stared to quit then turned fuel back on. It ran fine. Pulled the plane back in the hanger and scratched our heads. We did an oil change since the engine was warm. When we took the plane out to test for oil leaks it would not run over 1600rpm and it coughed, backfired and ran extremely rough. Here is the clue as soon as I leaned the mixture about halfway back run smooth. (elevation is about 775 ft) So I suspect the Bendix servo is the problem. Anyone have any ideas that could shed some light on the subject . Oh by the way I bought the engine used at OSH and the servo has not been overhauled. ???????????? RV8a Flying (was flying) ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: fiberglass information
Date: Oct 23, 2002
Sam James has a fiberglass 101 video. You can get it from Builder's Bookstore I think. Paul Besing RV-6A Sold (Waiting on the RV-10) http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "Steve Struyk" <rv8striker(at)hotmail.com> Subject: RV-List: fiberglass information > > I have put off, far too long now, all my fiberglass work. I guess what I need is an introduction to the basics. Is there a video or perhaps or book to explain fiberglass for the beginner? > > Any advice would be appreciated. > Thanks in advance > > Steve Struyk > St. Charles MO > RV-8 N842S (Res.) > > ________________________________________________________________________________
Date: Oct 23, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: LOE wx so far
The DCU RV gang is agonizing (well.......confused!?!.......) about whether or not to plan on launching a gaggle of planes westward Friday morning. Unfortunately, it seems an unseasonable and unusual weather pattern has plopped down directly on top of our route of flight all the way to LRU. It would be EXTREMELY helpful for us (and I am sure a host of other RVers) to get periodic reports such as Brian's from pilots who live in the Arkansas, Texas, and New Mexico areas. We need to know about the visibility, ceilings, presence of showers, etc, all the stuff that a bunch of VFR RV pilots of various skill levels will be concerned about. Yes, we are devouring all the weather products available on the web, but Brian's "real world" report is invaluable in trying to make plans. Thanks in advance for the ground-based PIREPS! Sam Buchanan (RV-6 at DCU) =============================== Brian Denk wrote: > > > Since I live in Albuquerque, I thought I'd mention what "the view out the > window" is today for your wx planning if flying down from northern areas to > Las Cruces. It's quite nice, but much wetter than usual. We have low > scattered clouds, providing some mountain obscuration this morning. Had > some intense showers mixed with hail yesterday evening. (The weather gods > must have known I just had my shop roof redone!) > > Forecast calls for similar conditions for the next few days...scattered > showers, highs upper 60's for Albuquerque and a bit warmer down south at > Cruces. > > Copied off the local news channel website: > > Middle Rio Grande Valley > Today: mostly cloudy with scattered showers and thunderstorms. Highs 64 to > 70. > Tonight: mostly cloudy with scattered showers and thunderstorms. Developing > east canyon winds 10 to 20 mph during the evening. Lows 35 to 43. > Thursday: partly cloudy with isolated showers and thunderstorms. Highs 63 to > 70. > Thursday Night: partly cloudy with isolated showers and thunderstorms. Lows > 33 to 41. > Friday: partly cloudy. Highs 63 to 70. > Saturday And Sunday: mostly cloudy with a chance of showers and > thunderstorms. Lows 38 to 48. Highs 58 to 68. > Monday And Tuesday: partly cloudy. Lows 34 to 45. Highs 59 to 68. > > Ya'll bring a jacket and be prepared to dodge some showers along the way. > > Brian Denk > RV8 N94BD > ________________________________________________________________________________
From: "Scott W. Hatten" <ScottHatten(at)columbus.rr.com>
Subject: RV9A - Plans / Empennage
Date: Oct 23, 2002
Wanting to Purchase? Looking for anyone who might have purchased the RV9A plans, or the Empennage and have changed thier mind, or decided the project is too big? Scott W. Hatten Pataskala, OH N6153K ________________________________________________________________________________
Date: Oct 23, 2002
From: Scott Bilinski <bilinski(at)qcpi.com>
Subject: Re: RV7-List: Drill and dimple vs just dimple (was:New Builder
introduction) Your are correct about the hole size. I looked up the MIL SPEC and it showed something a little different than what we are getting. I called the factory, and to keep this short, just build it, it is way over built for the rivet hole size to be an issue. To be perfect it should be dimpled with the smallest pilot hole possible and then reamed to size. So do you want to build the rest of your life or do you want to fly in the near future? >--> RV7-List message posted by: Richard Tasker > >I am currently finishing up my RV9 empennage kit and expect to get the >wing kit in a few weeks. > >I have noticed while building the empennage that the pre-punched holes >always line up so all you are really seem to be doing is just enlarging >the holes with the "match" drilling. Furthermore, when you dimple the >drilled hole, the resulting hole is actually a little oversize for the >rivet (per standard rivet specifications). Dimpling the existing holes >would actually create a better fit to the rivet. > >I would like to solicit opinions as to the procedure noted below. That >is, what are the advantages and drawbacks of following the instructions >to drill then dimple vs just dimple as is. Of course, it goes without >saying that your dimple tool should fit into the existing holes before >dimpling (which might require slight grinding of the dimple tool pilot >shaft). > >Dick Tasker, 90573 > >Albert Gardner wrote: > >>--> RV9-List message posted by: "Albert Gardner" > >> >>Hey Steve, welcome to the list. You may or may not know but many builders of >>the pre-punched kits are skipping the step of putting the parts together and >>then opening up the 3/32" holes with a #40 drill. They first dimple the >>individual parts (which opens up the holes slightly) and then clecoe it up >>and set the rivets. I know of several guys who built wings without even >>thinking about twist while building. After the skins were riveted on they >>checked and found out there was zero twist. In any case you are going to >>have fun. >>Albert Gardner, Yuma, AZ >>RV-9A: N872RV >>(After 2 years I can see the end from here.) >> >>----- Original Message ----- >>From: "RV9" <rv9(at)charter.net> >>To: >>Subject: RV9-List: New Builder introduction >> >> >> >> >>>--> RV9-List message posted by: RV9 >>> >>> >>>Hello, >>> >>>My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit >>>number 609 which I received on the 10th of October. I've finished all >>>of the prep work on the HS and I'm awaiting better weather here in >>>North Texas (Granbury) before priming my HS parts. I've also begun work >>>on the VS. >>> >>>I have a very crude (in comparison to some of you guys) website that's >>>intended to allow my non-builder friends and relatives to track my >>>progress. You are, of course, welcome to visit. Comments, suggestions, >>>motiviations, etc. are all welcome. >>> >>>http://webpages.charter.net/smottin >>> >>>Steve Mottin >>>RV-9A Empennage >>>Granbury, Texas mailto:rv9(at)charter.net >>> >>> >>> >>> >> >> >> >> > > Scott Bilinski Eng dept 8220 Phone (858) 657-2536 Pager (858) 502-5190 ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Ready-to-install Spinner
Date: Oct 23, 2002
Hello Randy, Examine the marks carefully. If the "marring" is very shallow start with a very fine grit wet and dry sandpaper. If possible omit the 320 and try first with 600 grit or 400 grit. Use water and a flexable sanding pad Good luck, Jim in Kelowna ----- Original Message ----- From: "Randy Compton" <rdcompton(at)earthlink.net> Subject: Re: RV-List: Ready-to-install Spinner > > > Randy, don't trash the spinner yet! Use 320 grit wet/dry paper with > > water to sand out the trail. Once the trail is sanded out (I assume the > > "trail" is largely cosmetic and not deep enough to create structural > > problems) follow the 320 with 600, then 1200, then a buffing wheel with > > polishing compound. > > > > Sam Buchanan > > No, I've still got it. I was so bummed that I didn't think about any > "salvage" work. The marring is not very deep, so I don't think there is a > structural problem. I'll go ahead and give sanding/scotchbriting a try. > > Thanks for tip! > > Randy Compton > N84VF > RV-3A > Gulf Breeze, FL > > > ________________________________________________________________________________
Date: Oct 23, 2002
From: Richard Tasker <retasker(at)optonline.net>
Subject: Re: RV7-List: Drill and dimple vs just dimple (was:New Builder
introduction) Well, your last question is what mine is related to. Just dimpling would save substantial time over clecoing together, match drilling, then dimpling vs just dimpling it. If there are no drawbacks to this approach, then it would get us flying sooner! Dick Tasker, 90573 Scott Bilinski wrote: >--> RV7-List message posted by: Scott Bilinski > >Your are correct about the hole size. I looked up the MIL SPEC and it >showed something a little different than what we are getting. I called the >factory, and to keep this short, just build it, it is way over built for >the rivet hole size to be an issue. To be perfect it should be dimpled with >the smallest pilot hole possible and then reamed to size. So do you want to >build the rest of your life or do you want to fly in the near future? > > > > >>--> RV7-List message posted by: Richard Tasker >> >>I am currently finishing up my RV9 empennage kit and expect to get the >>wing kit in a few weeks. >> >>I have noticed while building the empennage that the pre-punched holes >>always line up so all you are really seem to be doing is just enlarging >>the holes with the "match" drilling. Furthermore, when you dimple the >>drilled hole, the resulting hole is actually a little oversize for the >>rivet (per standard rivet specifications). Dimpling the existing holes >>would actually create a better fit to the rivet. >> >>I would like to solicit opinions as to the procedure noted below. That >>is, what are the advantages and drawbacks of following the instructions >>to drill then dimple vs just dimple as is. Of course, it goes without >>saying that your dimple tool should fit into the existing holes before >>dimpling (which might require slight grinding of the dimple tool pilot >>shaft). >> >>Dick Tasker, 90573 >> >>Albert Gardner wrote: >> >> >> >>>--> RV9-List message posted by: "Albert Gardner" >>> >>> >> >> >> >>>Hey Steve, welcome to the list. You may or may not know but many builders of >>>the pre-punched kits are skipping the step of putting the parts together and >>>then opening up the 3/32" holes with a #40 drill. They first dimple the >>>individual parts (which opens up the holes slightly) and then clecoe it up >>>and set the rivets. I know of several guys who built wings without even >>>thinking about twist while building. After the skins were riveted on they >>>checked and found out there was zero twist. In any case you are going to >>>have fun. >>>Albert Gardner, Yuma, AZ >>>RV-9A: N872RV >>>(After 2 years I can see the end from here.) >>> >>>----- Original Message ----- >>>From: "RV9" <rv9(at)charter.net> >>>To: >>>Subject: RV9-List: New Builder introduction >>> >>> >>> >>> >>> >>> >>>>--> RV9-List message posted by: RV9 >>>> >>>> >>>>Hello, >>>> >>>>My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit >>>>number 609 which I received on the 10th of October. I've finished all >>>>of the prep work on the HS and I'm awaiting better weather here in >>>>North Texas (Granbury) before priming my HS parts. I've also begun work >>>>on the VS. >>>> >>>>I have a very crude (in comparison to some of you guys) website that's >>>>intended to allow my non-builder friends and relatives to track my >>>>progress. You are, of course, welcome to visit. Comments, suggestions, >>>>motiviations, etc. are all welcome. >>>> >>>>http://webpages.charter.net/smottin >>>> >>>>Steve Mottin >>>>RV-9A Empennage >>>>Granbury, Texas mailto:rv9(at)charter.net >>>> >>>> >>>> >>>> >>>> >>>> >>> >>> >>> >>> >> >> > > >Scott Bilinski >Eng dept 8220 >Phone (858) 657-2536 >Pager (858) 502-5190 > > > > ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: Inverted oil system
Date: Oct 23, 2002
Hi Larry, Looks like the Raven System is a copy of the tried and true "Christen" Inverted Oil System. I have seen this system advertised on Ebay a few times. Other than that, don't know much else about this one. P.S. Will you be at LRU on the weekend?? Konrad ABQ ----- Original Message ----- From: "Larry Hawkins" <lhawkins(at)giant.com> Subject: RV-List: Inverted oil system > > Does anyone have any experience with this inverted oil system built by Raven > aircraft (Pitts). Check it out at; > http://www.ravenaircraft.com/raven_001.htm > > Larry Hawkins, RV-4 Farmington, NM, N-345SL, > finishing. > > ________________________________________________________________________________
Date: Oct 23, 2002
From: Scott Bilinski <bilinski(at)qcpi.com>
Subject: Re: RV7-List: Drill and dimple vs just dimple (was:New Builder
introduction) If I had to do it over again (rivetiing 99% done at this time) I would consider not match drill, but at least deburr, which is very important. I would not even consider not doing it. Now I say this, and am no expert by any means. So that is why I always run my ideas past experts which is what I suggest to anyone deviating from the directions. >--> RV7-List message posted by: Richard Tasker > >Well, your last question is what mine is related to. Just dimpling >would save substantial time over clecoing together, match drilling, then >dimpling vs just dimpling it. If there are no drawbacks to this >approach, then it would get us flying sooner! > >Dick Tasker, 90573 > >Scott Bilinski wrote: > >>--> RV7-List message posted by: Scott Bilinski >> >>Your are correct about the hole size. I looked up the MIL SPEC and it >>showed something a little different than what we are getting. I called the >>factory, and to keep this short, just build it, it is way over built for >>the rivet hole size to be an issue. To be perfect it should be dimpled with >>the smallest pilot hole possible and then reamed to size. So do you want to >>build the rest of your life or do you want to fly in the near future? >> >> >> >> >>>--> RV7-List message posted by: Richard Tasker >>> >>>I am currently finishing up my RV9 empennage kit and expect to get the >>>wing kit in a few weeks. >>> >>>I have noticed while building the empennage that the pre-punched holes >>>always line up so all you are really seem to be doing is just enlarging >>>the holes with the "match" drilling. Furthermore, when you dimple the >>>drilled hole, the resulting hole is actually a little oversize for the >>>rivet (per standard rivet specifications). Dimpling the existing holes >>>would actually create a better fit to the rivet. >>> >>>I would like to solicit opinions as to the procedure noted below. That >>>is, what are the advantages and drawbacks of following the instructions >>>to drill then dimple vs just dimple as is. Of course, it goes without >>>saying that your dimple tool should fit into the existing holes before >>>dimpling (which might require slight grinding of the dimple tool pilot >>>shaft). >>> >>>Dick Tasker, 90573 >>> >>>Albert Gardner wrote: >>> >>> >>> >>>>--> RV9-List message posted by: "Albert Gardner" >>>> >>>> >>> >>> >>> >>>>Hey Steve, welcome to the list. You may or may not know but many builders of >>>>the pre-punched kits are skipping the step of putting the parts together and >>>>then opening up the 3/32" holes with a #40 drill. They first dimple the >>>>individual parts (which opens up the holes slightly) and then clecoe it up >>>>and set the rivets. I know of several guys who built wings without even >>>>thinking about twist while building. After the skins were riveted on they >>>>checked and found out there was zero twist. In any case you are going to >>>>have fun. >>>>Albert Gardner, Yuma, AZ >>>>RV-9A: N872RV >>>>(After 2 years I can see the end from here.) >>>> >>>>----- Original Message ----- >>>>From: "RV9" <rv9(at)charter.net> >>>>To: >>>>Subject: RV9-List: New Builder introduction >>>> >>>> >>>> >>>> >>>> >>>> >>>>>--> RV9-List message posted by: RV9 >>>>> >>>>> >>>>>Hello, >>>>> >>>>>My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit >>>>>number 609 which I received on the 10th of October. I've finished all >>>>>of the prep work on the HS and I'm awaiting better weather here in >>>>>North Texas (Granbury) before priming my HS parts. I've also begun work >>>>>on the VS. >>>>> >>>>>I have a very crude (in comparison to some of you guys) website that's >>>>>intended to allow my non-builder friends and relatives to track my >>>>>progress. You are, of course, welcome to visit. Comments, suggestions, >>>>>motiviations, etc. are all welcome. >>>>> >>>>>http://webpages.charter.net/smottin >>>>> >>>>>Steve Mottin >>>>>RV-9A Empennage >>>>>Granbury, Texas mailto:rv9(at)charter.net >>>>> >>>>> >>>>> >>>>> >>>>> >>>>> >>>> >>>> >>>> >>>> >>> >>> >> >> >>Scott Bilinski >>Eng dept 8220 >>Phone (858) 657-2536 >>Pager (858) 502-5190 >> >> >> >> > > Scott Bilinski Eng dept 8220 Phone (858) 657-2536 Pager (858) 502-5190 ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Drill and dimple vs just dimple (was:New Builder introduction)
Date: Oct 23, 2002
Hello Richard, The pre-punched holes will fit the clekoes and should assure exact parts alignments during the drilling stage. The pre-drilling of assembled parts that will receive flush rivets is (in my opinion) a must!. The suggested pre-drilling removes enough material from the hole center to allow the dimpling process to take place without excess stretching around the hole. Excess stretch in this area 'could' translate out as minute stress relief cracks. This might not happen, but the extra drilling effort helps to preclude such eventualities Keep in mind that the procedure described has been more than Seventy years in development. You can bet that a lot of attention has been paid in the past to the area we are discussing here. I seriously doubt that this is an area that needs any fine tuning by aircraft kit builders such as us. As for messing with the design of the dimple dies grinding or otherwise modifying such tools...I would not go there! Sometimes short cuts tend to leave one just a bit short of the desired goal. There are books aplenty on the tools and procedures used in stressed skin monocoque (sp) designs. They are not exiting to read, just very informative. Happy drilling, Jim in Kelowna ----- Original Message ----- From: "Richard Tasker" <retasker(at)optonline.net> Subject: RV-List: Drill and dimple vs just dimple (was:New Builder introduction) > > I am currently finishing up my RV9 empennage kit and expect to get the > wing kit in a few weeks. > > I have noticed while building the empennage that the pre-punched holes > always line up so all you are really seem to be doing is just enlarging > the holes with the "match" drilling. Furthermore, when you dimple the > drilled hole, the resulting hole is actually a little oversize for the > rivet (per standard rivet specifications). Dimpling the existing holes > would actually create a better fit to the rivet. > > I would like to solicit opinions as to the procedure noted below. That > is, what are the advantages and drawbacks of following the instructions > to drill then dimple vs just dimple as is. Of course, it goes without > saying that your dimple tool should fit into the existing holes before > dimpling (which might require slight grinding of the dimple tool pilot > shaft). > > Dick Tasker, 90573 > > Albert Gardner wrote: > > >--> RV9-List message posted by: "Albert Gardner" > > > >Hey Steve, welcome to the list. You may or may not know but many builders of > >the pre-punched kits are skipping the step of putting the parts together and > >then opening up the 3/32" holes with a #40 drill. They first dimple the > >individual parts (which opens up the holes slightly) and then clecoe it up > >and set the rivets. I know of several guys who built wings without even > >thinking about twist while building. After the skins were riveted on they > >checked and found out there was zero twist. In any case you are going to > >have fun. > >Albert Gardner, Yuma, AZ > >RV-9A: N872RV > >(After 2 years I can see the end from here.) > > > >----- Original Message ----- > >From: "RV9" <rv9(at)charter.net> > >To: > >Subject: RV9-List: New Builder introduction > > > > > > > > > >>--> RV9-List message posted by: RV9 > >> > >> > >>Hello, > >> > >>My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit > >>number 609 which I received on the 10th of October. I've finished all > >>of the prep work on the HS and I'm awaiting better weather here in > >>North Texas (Granbury) before priming my HS parts. I've also begun work > >>on the VS. > >> > >>I have a very crude (in comparison to some of you guys) website that's > >>intended to allow my non-builder friends and relatives to track my > >>progress. You are, of course, welcome to visit. Comments, suggestions, > >>motiviations, etc. are all welcome. > >> > >>http://webpages.charter.net/smottin > >> > >>Steve Mottin > >>RV-9A Empennage > >>Granbury, Texas mailto:rv9(at)charter.net > >> > >> > >> > >> > > > > > > > > > > ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: LOE wx so far
Date: Oct 23, 2002
> . . . climb up into the dessert of NM, it should be OK. < * Hi Brian, What kind of "dessert" are you talking? Anything with strawberry's I hope! About our desert weather: Keep up the good job and I'll see you for a sweet dessert at LRU! > Las Cruces: > Currently: 57F Cloudy > Wind: Southeast at 6.0 MPH > Humidity: 94.0% > Dewpoint: 55 F * Ninety four percent wet air in Cruces?? Wow, now that is humid! C.U.@ LRU Konrad ________________________________________________________________________________
From: MeangreenRV4(at)aol.com
Date: Oct 23, 2002
Subject: Re: Inverted oil system
In a message dated 10/23/2002 9:29:18 AM Pacific Daylight Time, lhawkins(at)giant.com writes: > Does anyone have any experience with this inverted oil system built by Raven > aircraft (Pitts). Check it out at; > http://www.ravenaircraft.com/raven_001.htm > > Larry Hawkins, RV-4 Farmington, NM, N-345SL, > I have the Christian setup on my 4 and it looks very simular I can't see it not working the same way. Tim Barnes Meangreen RV4 ________________________________________________________________________________
Date: Oct 23, 2002
From: rob ray <smokyray(at)yahoo.com>
Subject: Re: RV4-List: ivo propeller
MT and Hoffman both had enough doubts about the hubs on Warp Drive props holding up on Lycomings early on. They invested a ton o' money on research on the crankshaft before they built props for them. Something about Pulse rate frequencies on Lycomings being severe. When you're over trees or water or mountains, you don't need other problems... RR --- flyseaplane wrote: > --> RV4-List message posted by: "flyseaplane" > > > Jim Ayers - - - > > Sorry to all that this is the RV list - I have never > heard of anyone having > problems with their Warp Drive on a Lycoming. That > is, the ground adjustable > ones. What have you heard?? I know a guy who has one > on a 160 HP and has had > no problems for the six years that it has been > flying (about 800 hours now) > > Thanks, > Linc > > > > RV-3 N47RV > > LOM M332A engine > > Ivoprop Magnum electric prop flown since Dec. 1995 > very nervously. > > I believe Ivo hasn't sold his prop for Lycoming > engines for a couple > years. > > Warp drive wasn't successful on a Lycoming, > either. Makes me wonder about > > the new CS props using Warp drive blades. Anyone > have any history on the > new > > CS props with the Warp drive blades on a Lycoming? > > > ------------------------------------------- > > > > Contributions of > any other form > > latest messages. > other List members. > > http://www.matronics.com/subscription > http://www.matronics.com/photoshare > http://www.matronics.com/search > http://www.matronics.com/archives > http://www.matronics.com/emaillists > > > > > ________________________________________________________________________________
From: MeangreenRV4(at)aol.com
Date: Oct 23, 2002
Subject: Re: RV Fuel Injection Help
In a message dated 10/23/2002 9:55:27 AM Pacific Daylight Time, dane(at)mutualace.com writes: > > My problem is this. While flying near Sylvania Airport in Wisconsin in my > new RV8a (50 hrs) I had a total loss of power. The engine (IO-360a, Bendix > Servo) was coughing, sputtering backfiring & wind milling all the way down > to airport that I just happened to be near. As I rolled out on the runway > the prop quit turning. I tried to restart on the runway and flooded it. > > In the air I did the following: > > Fly the plane & head for airport (alt. 1500 agl) > Fuel pump on > Circuit breaker check > Full power throttle on > Full rich > Did not switched tanks but it was full > Missed Semi-Truck on highway near the approach and landed the plane. > > On the ground the mechanic at Sylvania came out on a Sunday and check spark > (mag & LightSpeed) not a problem. Cleaned the bottom plugs and we restarted > the engine. It ran fine. > I came back Monday and checked the complete fuel system from the tank to > the > filter to the lines plenty of fuel. We put I back together and it ran fine. > Ran it up to 2000 rpm switched tanks, boost pump on & off, mixture rich to > lean, turned off fuel while running until she stared to quit then turned > fuel back on. It ran fine. Pulled the plane back in the hanger and > scratched our heads. We did an oil change since the engine was warm. When > we took the plane out to test for oil leaks it would not run over 1600rpm > and it coughed, backfired and ran extremely rough. Here is the clue as soon > as I leaned the mixture about halfway back run smooth. (elevation is about > 775 ft) > So I suspect the Bendix servo is the problem. Anyone have any ideas that > could shed some light on the subject . Oh by the way I bought the engine > used at OSH and the servo has not been overhauled. > > > ???????????? > RV8a Flying (was flying) > Nothing like having an experience like that to blow your confidence and make you smarter all at the same time. Tim Barnes Meangreen RV4 ________________________________________________________________________________
Date: Oct 23, 2002
From: Rob Prior <rv7(at)b4.ca>
Subject: Re: RV7-List: Drill and dimple vs just dimple (was:New Builder
introduction) One downside, that has been discussed here before, is the problem of leaving potential crack forming locations. When the holes are punched, the machining marks left are parallel to the axis of the hole, i.e. across the edge of the sheet inside the hole. Dimpling this edge will stretch it a little bit, and place these machining marks in tension. Age, vibration, flight stresses, etc. *may* cause these marks to turn into microscopic cracks that could propagate into the skins. I say may, because the loads at those edges are likely to be extremely small. When you drill the holes before dimpling, you rotate the machining marks so they are now perpendicular to the axis of the hole, or parallel to the edge of the skins inside the hole. When these marks are stretched by dimpling, they are much less likely to cause microscopic stress fractures that could propagate into the skins at a later date. I agree that the risk is low of any of these microscopic cracks propagating into the skins. But at the same time, I would prefer not to leave myself open to any potential problems, when it takes such a short time to remove them. It's not *that* much of an inconvenience to assemble, drill, and then disassemble. Oh, and finally, the last time I heard someone ask the factory about this, they said to assemble, drill, and disassemble before dimpling. -RB4 Richard Tasker wrote: > --> RV7-List message posted by: Richard Tasker > > Well, your last question is what mine is related to. Just dimpling > would save substantial time over clecoing together, match drilling, then > dimpling vs just dimpling it. If there are no drawbacks to this > approach, then it would get us flying sooner! > > Dick Tasker, 90573 > > Scott Bilinski wrote: > > >>--> RV7-List message posted by: Scott Bilinski >> >>Your are correct about the hole size. I looked up the MIL SPEC and it >>showed something a little different than what we are getting. I called the >>factory, and to keep this short, just build it, it is way over built for >>the rivet hole size to be an issue. To be perfect it should be dimpled with >>the smallest pilot hole possible and then reamed to size. So do you want to >>build the rest of your life or do you want to fly in the near future? >> >> >> >> >> >>>--> RV7-List message posted by: Richard Tasker >>> >>>I am currently finishing up my RV9 empennage kit and expect to get the >>>wing kit in a few weeks. >>> >>>I have noticed while building the empennage that the pre-punched holes >>>always line up so all you are really seem to be doing is just enlarging >>>the holes with the "match" drilling. Furthermore, when you dimple the >>>drilled hole, the resulting hole is actually a little oversize for the >>>rivet (per standard rivet specifications). Dimpling the existing holes >>>would actually create a better fit to the rivet. >>> >>>I would like to solicit opinions as to the procedure noted below. That >>>is, what are the advantages and drawbacks of following the instructions >>>to drill then dimple vs just dimple as is. Of course, it goes without >>>saying that your dimple tool should fit into the existing holes before >>>dimpling (which might require slight grinding of the dimple tool pilot >>>shaft). >>> >>>Dick Tasker, 90573 >>> >>>Albert Gardner wrote: >>> >>> >>> >>> >>>>--> RV9-List message posted by: "Albert Gardner" >>>> >>>> >>> >>> >>> >>> >>> >>>>Hey Steve, welcome to the list. You may or may not know but many builders of >>>>the pre-punched kits are skipping the step of putting the parts together and >>>>then opening up the 3/32" holes with a #40 drill. They first dimple the >>>>individual parts (which opens up the holes slightly) and then clecoe it up >>>>and set the rivets. I know of several guys who built wings without even >>>>thinking about twist while building. After the skins were riveted on they >>>>checked and found out there was zero twist. In any case you are going to >>>>have fun. >>>>Albert Gardner, Yuma, AZ >>>>RV-9A: N872RV >>>>(After 2 years I can see the end from here.) >>>> >>>>----- Original Message ----- >>>>From: "RV9" <rv9(at)charter.net> >>>>To: >>>>Subject: RV9-List: New Builder introduction >>>> >>>> >>>> >>>> >>>> >>>> >>>> >>>>>--> RV9-List message posted by: RV9 >>>>> >>>>> >>>>>Hello, >>>>> >>>>>My name is Steve Mottin and I'm the proud owner of RV-9 empennage kit >>>>>number 609 which I received on the 10th of October. I've finished all >>>>>of the prep work on the HS and I'm awaiting better weather here in >>>>>North Texas (Granbury) before priming my HS parts. I've also begun work >>>>>on the VS. >>>>> >>>>>I have a very crude (in comparison to some of you guys) website that's >>>>>intended to allow my non-builder friends and relatives to track my >>>>>progress. You are, of course, welcome to visit. Comments, suggestions, >>>>>motiviations, etc. are all welcome. >>>>> >>>>>http://webpages.charter.net/smottin >>>>> >>>>>Steve Mottin >>>>>RV-9A Empennage >>>>>Granbury, Texas mailto:rv9(at)charter.net >>>>> >>>>> >>>>> >>>>> >>>>> >>>>> >>>> >>>> >>>> >>>> >>> >>> >>> >> >> >>Scott Bilinski >>Eng dept 8220 >>Phone (858) 657-2536 >>Pager (858) 502-5190 >> >> >> >> > > > > > > > ________________________________________________________________________________
Date: Oct 23, 2002
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Drill and dimple vs just dimple (was:New Builder
introduction) Jim Jewell wrote: > > > Hello Richard, > > The pre-punched holes will fit the clekoes and should assure exact parts > alignments during the drilling stage. > The pre-drilling of assembled parts that will receive flush rivets is (in my > opinion) a must!. > The suggested pre-drilling removes enough material from the hole center to > allow the dimpling process to take place without excess stretching around > the hole. Excess stretch in this area 'could' translate out as minute stress > relief cracks. This might not happen, but the extra drilling effort helps to > preclude such eventualities I'm feeling grumpy this afternoon.......since my 6-month plans for LRU may get flushed away by rogue low pressure systems..... > Keep in mind that the procedure described has been more than Seventy years > in development. You can bet that a lot of attention has been paid in the > past to the area we are discussing here. I seriously doubt that this is an > area that needs any fine tuning by aircraft kit builders such as us. > Maybe folks have been drilling holes in metal skins for seventy years, but they have been riveting together CAD designed and punched RV kits for only a couple of years! I have to wonder how far back in the past it would have been deemed "acceptable" to skip the drilling stage if drills were not necessary to make the holes in the first place. Would we have seen "undrilled" B-17's or P-51's??? I bet the folks trying to force every plane possible into the sky during WWII would have gladly skipped the drilling process if CAD punched skins were available. And..........if that had happened, would it now be "acceptable" to skip the drilling step without fear of "stretching" the holes??? Just tryin' to stir up a rip-roarin', flat-out flame-throwin' war on this here list...... Sam Buchanan ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Ready-to-install Spinner
Date: Oct 23, 2002
Bet you can't see it while flying! AND if you turn the prop right when parked, no one will see it. ----- Original Message ----- From: "Larry Bowen" <lcbowen(at)yahoo.com> Subject: Re: RV-List: Ready-to-install Spinner > > You can't buff it out? > > -LB > > --- Sluggo wrote: > > > > > > Ah, here was the "rub", as they say. The Orndorff's also said that a Dremel > > was the way to go and should be "simple and hard to make a mistake." Well, > > maybe for you all. Ham-fisted me let the Dremel get away and walk nicely > > across the spinner, leaving a lovely etched trail, as well as a ruined > > pricey polished spinner, in its wake. > > ________________________________________________________________________________
From: "Stephen Johnson" <spjohnsn(at)ix.netcom.com>
Subject: Re: RV7-List: Drill and dimple vs just dimple (was:New Builder
introduction)
Date: Oct 23, 2002
The drilling and deburring process is needed to eliminate stress risers which can cause cracks later. For a very good discussion on fatigue failure caused by stress concentrations see "Sky Ranch Engineering Manual" by John Schwaner. It's available from http://www.sacskyranch.com/index.htm and is must reading before engine selection time. If I were building a matched hole kit, I would drill holes #41 rather than #40. This eliminates the stress risers and is just large enough for the pilots in the dimple dies and countersink. Steve Johnson RV-8 #80121 fuse ----- Original Message ----- From: "Richard Tasker" <retasker(at)optonline.net> Subject: RV-List: Re: RV7-List: Drill and dimple vs just dimple (was:New Builder introduction) > > Well, your last question is what mine is related to. Just dimpling > would save substantial time over clecoing together, match drilling, then > dimpling vs just dimpling it. If there are no drawbacks to this > approach, then it would get us flying sooner! > > Dick Tasker, 90573 > > Scott Bilinski wrote: > > >--> RV7-List message posted by: Scott Bilinski > > > >Your are correct about the hole size. I looked up the MIL SPEC and it > >showed something a little different than what we are getting. I called the > >factory, and to keep this short, just build it, it is way over built for > >the rivet hole size to be an issue. To be perfect it should be dimpled with > >the smallest pilot hole possible and then reamed to size. So do you want to > >build the rest of your life or do you want to fly in the near future? ________________________________________________________________________________
From: "flyseaplane" <flyseaplane(at)netzero.net>
Subject: RV4-List: ivo propeller
Date: Oct 23, 2002
Rob Ray, "MT and Hoffman both had enough doubts about the hubs on Warp Drive props holding up on Lycomings early on." All the guys I know with Warp Drive Props on Lycomings have the "High Horse Power" blade hub. Maybe "early on" there was an issue, I think Warp fixed it with the HHP hub. Later, Linc ------------------------------------------- ________________________________________________________________________________
From: SportAV8R(at)aol.com
Date: Oct 23, 2002
Subject: transponder antenna inside wheelpant
Listers: an update on my experiment with relocating the transponder antenna from the belly to the wheelpant- This summer, as I finished installing the 2-piece pressure-recovery wheelpants, I decided to take a gamble and remove the old belly-mounted transponder antenna and replace it with a new one located inside the aft compartment of the right main wheel pant. The little antenna is quite short, and can't be but so draggy, but it was always getting an oil film on it and becoming intermittently unreliable. Besides, it was one more thing to bump my head on or poke my eye with while working or cleaning underneath the plane. The installation involved fabricating a ground-plane from .032 aluminum sheet, cut as large as would fit inside the compartment formed by the rear bulkhead in Van's 2-piece wheel pant. A T-shaped slot was cut in the bulkhead fiberglass, allowing the antenna with ground-plane to be inserted in its final location, pointing straight downwards. The edges of the roughly-trapezoidal ground plane touched the sides of the wheel pant at some points, but the antenna tip was in free space, as installed. Pop rivets secured the forward flange of the ground plane to the bulkhead, and a coax bulkhead BNC fitting terminated the short run of coax (RG-200 from Electric Bob) from the antenna feedpoint to the bulkhead. The T-hole was closed with a layer of glass-epoxy, covering the pop rivet heads as well, and weatherproofing everything. Coax was run down the gear leg inside the fairing, to mate with this bulkhead fitting, so everything is removable if needed. Coax connections were sealed with wraps of self-fusing silicone tape. I now have a totally concealed, zero-drag, environmentally protected antenna which seems to hear and be heard just as well as the former belly installation. Total coax length is just over what the transponder book says is okay for RG-200, but I don't really care since it seems to perform to specs. No shielding effects are evident despite the proximity of the wheel and gear leg; I get "pinged" by approach radar throughout a 360 turn from a good distance away. Now I am wondering what sort of results we would see using a rubber duck antenna for aircraft comm and /or 2-meter ham frequencies in the opposite wheel pant. Obviously, the ground plane would be a compromise at these lower frequencies, whereas at 1260 MHz, a full quarter wave ground plane was able to fit inside the wheel pant. If I ever get around to trying this second experiment, I will post results here. More likely, I will fab a wingtip antenna for a low drag comm, using Bob Nuckolls' gamma-matched design. Disclaimer: any speed increase from this mod is sure to be unmeasurable in actual practice, but might make you feel better. Bill Boyd RV-6A ________________________________________________________________________________
From: "John Huft" <rv8tor(at)lazy8.net>
Subject: Re: RV7-List: RV7 quickbuild slider
Date: Oct 23, 2002
Sky Dynamics http://www.skydynamics.com/ has had a cool air system for some time. You still need to use fuel injection of some type, Bendix works too. See my setup at http://www.lazy8.net/fwf.html , it just goes through the sump like a carb. John Huft, Pagosa Springs, CO RV8 4.9 hours -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Phil Birkelbach Subject: RV-List: Re: RV7-List: RV7 quickbuild slider I talked to Superior Air Parts last week and they are developing a "cool air" induction system for the O-360 (acutally it would be for their XP-360, but it should fit the O) The system will keep the induction path outside the sump so the oil does not warm it up. This should increase power and efficiency. You will not be able to install a carb though. The sump would have the forward induction placement which would require a fuel injection servo because of the orientation. The carb would not work very well mounted at a 90 deg angle. If I understand it correctly you wouldn't want the fuel/air mixture from the carb to go straight to the jug anyway for carb ice reasons. I believe that was the reason for routing the fuel/air mixture through the sump in the first place. I am no engine expert so don't quote me on this! Just for reference moving to the Airflow Performance fuel injection system will be about a $2500 - $3000 net increase in the price of the engine. The sump is supposed to be ready sometime early next year. The Ellison TBI might work but you may still have to deal with a carb ice issue. Anyway to make a short story long this new sump would allow you to use the cowl from Van's that doesn't have the bottom scoop on it. Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB (Reserved) - Fuselage http://www.myrv7.com ----- Original Message ----- From: "Virgil Young" <vwyoung(at)comcast.net> Subject: RV7-List: RV7 quickbuild slider > --> RV7-List message posted by: Virgil Young > > I'm interested in a 180hp Lycoming which does not require air induction scoop on the lower cowling. My understanding is this requires a forward sump and horizontal induction. Would appreciate anyone's research along with recommended prop governor and constant speed prop.Virgil Young.#1017 > > ________________________________________________________________________________
Date: Oct 23, 2002
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: Re: Inverted oil system
I tried to save money back in the early seventies by buying an inverted system that looked like a homemade version of the Christen system. On every flight of the Pitts, the oil pressure would drop to almost nothing as the oil temperature climbed. Turned out the three-way valve had dissimilar metals for the ball and the seat; as they heated up, they changed dimension and wouldn't seal. I got what I paid for. didn't someone once say," There's nothing made that someone can't make cheaper"? Scott in Vancouver ----- Original Message ----- From: <meangreenrv4(at)aol.com> Subject: Re: RV-List: Inverted oil system > > In a message dated 10/23/2002 9:29:18 AM Pacific Daylight Time, > lhawkins(at)giant.com writes: > > > > Does anyone have any experience with this inverted oil system built by Raven > > aircraft (Pitts). Check it out at; > > http://www.ravenaircraft.com/raven_001.htm > > > > Larry Hawkins, RV-4 Farmington, NM, N-345SL, > > > > I have the Christian setup on my 4 and it looks very simular I can't see it > not working the same way. > > Tim Barnes > Meangreen RV4 > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Drill and dimple vs just dimple (was:New Builder introduction)
Date: Oct 23, 2002
Hi Sam, WasamaterSamduh%$#kofyemakerbroke?!! :-)! Jim in Kelowna ----- Original Message ----- From: "Sam Buchanan" <sbuc(at)hiwaay.net> Subject: Re: RV-List: Drill and dimple vs just dimple (was:New Builder introduction) > > > Jim Jewell wrote: > > > > > > Hello Richard, > > > > The pre-punched holes will fit the clekoes and should assure exact parts > > alignments during the drilling stage. > > The pre-drilling of assembled parts that will receive flush rivets is (in my > > opinion) a must!. > > The suggested pre-drilling removes enough material from the hole center to > > allow the dimpling process to take place without excess stretching around > > the hole. Excess stretch in this area 'could' translate out as minute stress > > relief cracks. This might not happen, but the extra drilling effort helps to > > preclude such eventualities > > I'm feeling grumpy this afternoon.......since my 6-month plans for LRU > may get flushed away by rogue low pressure systems..... > > > Keep in mind that the procedure described has been more than Seventy years > > in development. You can bet that a lot of attention has been paid in the > > past to the area we are discussing here. I seriously doubt that this is an > > area that needs any fine tuning by aircraft kit builders such as us. > > > > Maybe folks have been drilling holes in metal skins for seventy years, > but they have been riveting together CAD designed and punched RV kits > for only a couple of years! > > I have to wonder how far back in the past it would have been deemed > "acceptable" to skip the drilling stage if drills were not necessary to > make the holes in the first place. Would we have seen "undrilled" B-17's > or P-51's??? I bet the folks trying to force every plane possible into > the sky during WWII would have gladly skipped the drilling process if > CAD punched skins were available. > > And..........if that had happened, would it now be "acceptable" to skip > the drilling step without fear of "stretching" the holes??? > > Just tryin' to stir up a rip-roarin', flat-out flame-throwin' war on > this here list...... > > Sam Buchanan > > ________________________________________________________________________________
From: "Bill" <n8wv(at)hotmail.com>
Subject: Re: Drill and dimple vs just dimple (was:New Builder introduction)
Date: Oct 23, 2002
I talked to someone at Van's about this once, and they said it would be "no problem" to skip the match drilling, as the dimpling process would open the holes up enough to accept the rivets... I also recall reading in one of the RVators that VANS built the first matched hole "kit" wings for the 9 "without picking up a drill"... FWIW -Bill VonDane RV-8A ~ 71 hours www.vondane.com ----- Original Message ----- From: "Jim Jewell" <jjewell(at)telus.net> Subject: Re: RV-List: Drill and dimple vs just dimple (was:New Builder introduction) Hi Sam, WasamaterSamduh%$#kofyemakerbroke?!! :-)! Jim in Kelowna ----- Original Message ----- From: "Sam Buchanan" <sbuc(at)hiwaay.net> Subject: Re: RV-List: Drill and dimple vs just dimple (was:New Builder introduction) > > > Jim Jewell wrote: > > > > > > Hello Richard, > > > > The pre-punched holes will fit the clekoes and should assure exact parts > > alignments during the drilling stage. > > The pre-drilling of assembled parts that will receive flush rivets is (in my > > opinion) a must!. > > The suggested pre-drilling removes enough material from the hole center to > > allow the dimpling process to take place without excess stretching around > > the hole. Excess stretch in this area 'could' translate out as minute stress > > relief cracks. This might not happen, but the extra drilling effort helps to > > preclude such eventualities > > I'm feeling grumpy this afternoon.......since my 6-month plans for LRU > may get flushed away by rogue low pressure systems..... > > > Keep in mind that the procedure described has been more than Seventy years > > in development. You can bet that a lot of attention has been paid in the > > past to the area we are discussing here. I seriously doubt that this is an > > area that needs any fine tuning by aircraft kit builders such as us. > > > > Maybe folks have been drilling holes in metal skins for seventy years, > but they have been riveting together CAD designed and punched RV kits > for only a couple of years! > > I have to wonder how far back in the past it would have been deemed > "acceptable" to skip the drilling stage if drills were not necessary to > make the holes in the first place. Would we have seen "undrilled" B-17's > or P-51's??? I bet the folks trying to force every plane possible into > the sky during WWII would have gladly skipped the drilling process if > CAD punched skins were available. > > And..........if that had happened, would it now be "acceptable" to skip > the drilling step without fear of "stretching" the holes??? > > Just tryin' to stir up a rip-roarin', flat-out flame-throwin' war on > this here list...... > > Sam Buchanan ________________________________________________________________________________
From: "John Huft" <rv8tor(at)lazy8.net>
Subject: Drill and dimple vs just dimple (was:New Builder introduction)
Date: Oct 23, 2002
Wondering about this...are the pre-punched holes large enough to admit the pilot shaft of the dimple die, or does the pilot have to be "forced" through the hole? John Huft, RV8 (drilled em all) -----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: Drill and dimple vs just dimple (was:New Builder introduction) Jim Jewell wrote: > > > Hello Richard, > > The pre-punched holes will fit the clekoes and should assure exact parts > alignments during the drilling stage. > The pre-drilling of assembled parts that will receive flush rivets is (in my > opinion) a must!. > The suggested pre-drilling removes enough material from the hole center to > allow the dimpling process to take place without excess stretching around > the hole. Excess stretch in this area 'could' translate out as minute stress > relief cracks. This might not happen, but the extra drilling effort helps to > preclude such eventualities I'm feeling grumpy this afternoon.......since my 6-month plans for LRU may get flushed away by rogue low pressure systems..... > Keep in mind that the procedure described has been more than Seventy years > in development. You can bet that a lot of attention has been paid in the > past to the area we are discussing here. I seriously doubt that this is an > area that needs any fine tuning by aircraft kit builders such as us. > Maybe folks have been drilling holes in metal skins for seventy years, but they have been riveting together CAD designed and punched RV kits for only a couple of years! I have to wonder how far back in the past it would have been deemed "acceptable" to skip the drilling stage if drills were not necessary to make the holes in the first place. Would we have seen "undrilled" B-17's or P-51's??? I bet the folks trying to force every plane possible into the sky during WWII would have gladly skipped the drilling process if CAD punched skins were available. And..........if that had happened, would it now be "acceptable" to skip the drilling step without fear of "stretching" the holes??? Just tryin' to stir up a rip-roarin', flat-out flame-throwin' war on this here list...... Sam Buchanan ________________________________________________________________________________
From: "Jim Norman" <jnorman(at)intermapsystems.com>
Subject: Inverted oil system
Date: Oct 23, 2002
Konrad, If you don't know much about this system, why did you write back to give advise? He asked for advise, so if you don't have any, don't give any. Jim (cranky today). Tampa No not archive. -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Konrad Werner Subject: Re: RV-List: Inverted oil system Hi Larry, Looks like the Raven System is a copy of the tried and true "Christen" Inverted Oil System. I have seen this system advertised on Ebay a few times. Other than that, don't know much else about this one. P.S. Will you be at LRU on the weekend?? Konrad ABQ ----- Original Message ----- From: "Larry Hawkins" <lhawkins(at)giant.com> Subject: RV-List: Inverted oil system > > Does anyone have any experience with this inverted oil system built by Raven > aircraft (Pitts). Check it out at; > http://www.ravenaircraft.com/raven_001.htm > > Larry Hawkins, RV-4 Farmington, NM, N-345SL, > finishing. > > ________________________________________________________________________________
From: "Gary" <rv9er(at)3rivers.net>
Subject: Re: RV9-List: Drill and dimple vs just dimple (was:New Builder
introduction)
Date: Oct 23, 2002
Why do you guys want to second-guess the experts in sheet metal aircraft construction, and the tool and die makers? Van's has made itself clear on this point in the manual. The proceedures and fit are the way they are for good reasons, which have been discussed (beat to death) on the list. Check the archives. If it is too much work for you to match drill, I dont see how you will get very far in the construction of an RV. There was another long thread on the RV list about skipping deburring. It amazes me. Why not just do it right? It is not difficult. Gary From: Richard Tasker --> RV9-List message posted by: Richard Tasker I am currently finishing up my RV9 empennage kit and expect to get the wing kit in a few weeks. I have noticed while building the empennage that the pre-punched holes always line up so all you are really seem to be doing is just enlarging the holes with the "match" drilling. Furthermore, when you dimple the drilled hole, the resulting hole is actually a little oversize for the rivet (per standard rivet specifications). Dimpling the existing holes would actually create a better fit to the rivet. I would like to solicit opinions as to the procedure noted below. That is, what are the advantages and drawbacks of following the instructions to drill then dimple vs just dimple as is. Of course, it goes without saying that your dimple tool should fit into the existing holes before dimpling (which might require slight grinding of the dimple tool pilot shaft).


October 17, 2002 - October 23, 2002

RV-Archive.digest.vol-nq