RV-Archive.digest.vol-ns

October 28, 2002 - November 02, 2002



      I hope this thread dies soon.
      
      Gary
      
From: "Peter H. Blake" <pblake(at)epix.net>
Subject: Match drilling etc.
Does anyone know what manufacturing practices are used in building the quick-build kits? Do they drill, deburr, dimple, then rivet? Or do they just dimple and rivet? Whatever they do, I'd be comfortable doing on my plane (if I were lucky enough to have predrilled parts!!!). Peter Blake RV6 New O-360 mounted! --- Checked by AVG anti-virus system (http://www.grisoft.com). ________________________________________________________________________________
From: <etech(at)ucnsb.net>
, , , ,
Subject: GI-106A for sale
Date: Oct 28, 2002
Hello Everyone, We have an extra GI-106A that belongs to a customer for sale. Has never been installed or used. Still in original box with install kit and install manual. Customer was going to get two CDIs, but decided to get an HSI and a CDI. Customer asking $1398.37 plus S&H. We can pre-wire for a small additonal fee. If interested, please call or email. Rick Case Electronic Technologies 1501 Airway Circle New Smyrna Beach, FL 32168 (386) 426-1213 www.electronictechnologies.net ________________________________________________________________________________
Date: Oct 28, 2002
From: Jeff Point <jpoint(at)mindspring.com>
Subject: Re: . and engine horsepower mods.
Stein Bruch wrote: >our little 4 bangers. You will reach a point where you've done so much to >the engine that it will only last for a couple of hours. Case in point, > > There's another side to this that few seem to consider, that Stein just brought up. Everything you do to these engines to get more HP is going to reduce the life of the engine. I, too had dreams of high compression pistons, polished and ported, custom induction, etc. to get the most speed out of my bird. Until July 31 this year, when I was involved in an engine failure accident at very low altitude (200 feet- take off) over very unhospitable terrain (city.) I wasn't flying, just a passenger, and except for quick thinking and excellent airmanship on the part of the pilot, it could well have been five fatalities. As it was we all walked away with minor injuries. After some soul searching, I decided to stick with my project, but I resolved that I would not do ANYTHING which would decrease engine reliability. No fuel system mods, no souped up anything. These planes fly great on a box-stock engine. Sure, you may get another 5 or even 10 mph by tricking them out, but at what cost? It's just not worth the risk, IMHO. Jeff Point RV-6 finish kit Milwaukee WI ________________________________________________________________________________
Date: Oct 28, 2002
From: Laird Owens <owens(at)aerovironment.com>
Subject: LOE2 report: more wacky ramblings
>----Original Message Follows---- >From: "Brian Denk" <akroguy(at)hotmail.com> snipped stuff about LOE2 > >And on a lighter note, there was a report of a toilet papering, bestowed >upon Laird "Fowling Piece" Owens' RV-6 after receiving the much coveted, >lauded and lusted after Grand Champion award. Witnesses were interviewed, >interrogated and bought off as necessary to find the most likely suspect, >who goes by the name of "NORDO ROSIE". > >More news at eleven. :) > >Brian "don't let him lead or #4 will end up in the dirt" Denk >RV8 N94BD I uploaded a picture of what my RV looked like the morning after getting the award. See it at: http://members3.clubphoto.com/socal230330/974070/owner-9b41.phtml I had a great time hanging out at LOE2 with Brian and Larry and everybody else this past weekend. I'm sure it'll be HUGE next year! I just wish everyone else around the country could have made. I'm sure the award would have gone to someone else if everybody could have made it...but I'll take it anyway ;-) The award was just icing on the cake of a great weekend. For the new guys on the list who probably don't know, the "Fowling Piece" comment Brian made was because of the Hawk strike I took in the RV a couple of years ago. (If your interested about how a how a RV windshield holds up to a hawk, just check the archives searching Laird & Hawk, and some pictures at: http://members3.clubphoto.com/socal230330/429051/guest.phtml Laird RV-6 SoCal ________________________________________________________________________________
Date: Oct 28, 2002
From: Miller Robert <rmiller3(at)earthlink.net>
Subject: Not really RV related
Sorry for the "not RV" post. ... But I'd like to ask the eminently logical bunch of RV builders and flyers on this list which handheld GPS you are using? Which model is the best value? I don't want to spend much right now....(need the money for my RV 9a builder's fund). I apologize again for the off-topic topic. Robert ________________________________________________________________________________
From: "MARSHALL,STEPHANIE (HP-Corvallis,ex1)" <stephanie.marshall(at)hp.com>
Subject: Not really RV related
Date: Oct 28, 2002
We _rely_ on the Magellan Gold, a driving trip wasn't really a trip (without the Magellan) unless I either got us lost or took us 4 hours out of the way. My hubby said enough and got the gold. I haven't got us lost since, I have tried my hardest though....the darn thing just won't let me. :) Stephanie Marshall -----Original Message----- From: Miller Robert [mailto:rmiller3(at)earthlink.net] Subject: RV-List: Not really RV related Sorry for the "not RV" post. ... But I'd like to ask the eminently logical bunch of RV builders and flyers on this list which handheld GPS you are using? Which model is the best value? I don't want to spend much right now....(need the money for my RV 9a builder's fund). I apologize again for the off-topic topic. Robert ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: RV-6A airspeed problem
Date: Oct 28, 2002
I am helping a friend fly off the restrictions of his RV-6A. He has an O-320 with a Sensenich metal prop sold by Van's. I don't know the pitch, but it was ordered from Van's as the prop for the RV-6 and a 160 HP O-320. We can't seem to get more than about 145 KIAS out of this airplane. Have checked it with GPS, and it is close enough. Here is what we have so far: Max RPM we can get out of it is about 2650. (8000' 75%) Manifold pressure is good. Climb is very good. 1500 FPM 80 KIAS All fairings and pants are installed Could there be a pitch problem here? 140 KIAS seems pretty slow for an O-320. Anyone else flying a Sensenich have this problem? All signs are pointing to the prop. 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 ________________________________________________________________________________
From: "Bartrim, Todd" <sbartrim(at)mail.canfor.ca>
Subject: Freedom and right
Date: Oct 28, 2002
> And thanks to Robert McCallum for reminding us that our neighbors to the > North get along very well with a less arrogant attitude than we often have > in the US. The Canadians stand up for their freedoms, too, but they don't > have half the world pissed off at them. > Actually, we had a TFR last summer, IIRC it was 75 nm radius around Kananaskis Alberta, during the G-8 summit, while we were being visited by...... you guessed it. George W. Bush. S. Todd Bartrim Turbo 13B rotary powered RX-9endurance (FWF) C-FSTB (reserved) http://www3.telus.net/haywire/RV-9/C-FSTB.htm RE: RV-List: Freedom and right And thanks to Robert McCallum for reminding us that our neighbors to the North get along very well with a less arrogant attitude than we often have in the US. The Canadians stand up for their freedoms, too, but they don't have half the world pissed off at them. Actually, we had a TFR last summer, IIRC it was 75 nm radius around Kananaskis Alberta, during the G-8 summit, while we were being visited by...... you guessed it. George W. Bush. S. Todd Bartrim Turbo 13B rotary powered RX-9endurance (FWF) C-FSTB (reserved) http://www3.telus.net/haywire/RV-9/C-FSTB.htm ________________________________________________________________________________
From: "John Huft" <rv8tor(at)lazy8.net>
Subject: Hi-EGT's
Date: Oct 28, 2002
A fouled or misfiring spark plug will defiantly make the EGT go up (the fuel is still burning as it exits the cylinder). It is also common that a plug will misfire at full power (higher combustion pressure) but not after you pull the power back. So you should check the plugs, maybe try another set. Check your harness too. John -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of MeangreenRV4(at)aol.com Subject: RV-List: Hi-EGT's This is somthing that has started in the last month or so. My engine is a IO 360 A1B Angle Valve 200 + hp. On take off my # 1 cycinder goes to 1400 degrees. # 2 1375 degrees. # 3 & 4 1275 degrees. the problem is it never went past 1300 degrees in the first 200 hrs. Once I climb out, level off everything seems fine. Something has cause the EGT' on # 1 to go higher. My problem is I don't understand why. Things that I have done; 1. Cleaned the injectors 2. Look at and make sure that all hoses & fittings were tight 3. Cleaned all screens ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
Paul, Does he have the gear pants, gear leg fairings and intersection fairings installed? We picked up almost 20 kts when we installed ours. Chuck & Dave Rowbotham RV-A >From: "Paul Besing" <azpilot(at)extremezone.com> >Reply-To: rv-list(at)matronics.com >To: >Subject: RV-List: RV-6A airspeed problem >Date: Mon, 28 Oct 2002 15:11:07 -0700 > > >I am helping a friend fly off the restrictions of his RV-6A. He has an >O-320 with a Sensenich metal prop sold by Van's. I don't know the pitch, >but it was ordered from Van's as the prop for the RV-6 and a 160 HP O-320. > >We can't seem to get more than about 145 KIAS out of this airplane. Have >checked it with GPS, and it is close enough. Here is what we have so far: > >Max RPM we can get out of it is about 2650. (8000' 75%) >Manifold pressure is good. >Climb is very good. 1500 FPM 80 KIAS >All fairings and pants are installed > >Could there be a pitch problem here? 140 KIAS seems pretty slow for an >O-320. > >Anyone else flying a Sensenich have this problem? All signs are pointing >to the prop. > > >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 > > http://resourcecenter.msn.com/access/plans/2monthsfree.asp ________________________________________________________________________________
From: "Donald Mei" <don_mei(at)hotmail.com>
Subject: Cleaning Out the Hangar
Date: Oct 28, 2002
Dear All, I have a couple of items that I don't need. Hope the bandwidth use isn't offensive. 1) Fumoto Valve. Quick oil change valve. The version for the Lycoming costs 31.95 delivered. This is brand new version with the optional nipple to attach a hose to. I'll even include the hose. It doesn't clear my Vetterman 4 header exhaust. (damn!!) $25 - I'll pay shipping. 2) Flightcom IIsx portable intercom. About $120 new from discounter. Good condition. $40+shipping. Thanks. Don Mei RV-4 N92CT 3B9 - Chester, CT http://resourcecenter.msn.com/access/plans/2monthsfree.asp ________________________________________________________________________________
Date: Oct 28, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: RV-6A airspeed problem
> >I am helping a friend fly off the restrictions of his RV-6A. He has >an O-320 with a Sensenich metal prop sold by Van's. I don't know >the pitch, but it was ordered from Van's as the prop for the RV-6 >and a 160 HP O-320. > >We can't seem to get more than about 145 KIAS out of this airplane. >Have checked it with GPS, and it is close enough. Here is what we >have so far: > >Max RPM we can get out of it is about 2650. (8000' 75%) >Manifold pressure is good. >Climb is very good. 1500 FPM 80 KIAS >All fairings and pants are installed > >Could there be a pitch problem here? 140 KIAS seems pretty slow for an O-320. > >Anyone else flying a Sensenich have this problem? All signs are >pointing to the prop. > >Paul Besing Paul, I assume all the fairings are installed, but you didn't mention that. Please confirm. Airspeed Accuracy - You say the airspeed was checked with the GPS - which method did you use? Was this checked at the same time the 145 mph speed was determined, or did you check the airspeed accuracy some other time? I would like to nail down the accuracy of this speed, to make sure that we aren't looking at an inaccuracy in the IAS. I like Doug Gray's method, as modified by the National Test Pilot School. See: http://members.rogers.com/khorton/rvlinks/doug_gray/TASCALC.ZIP http://www.ntps.com/GPS_SpeedTrack.XLS If you want, I would be happy to run the calculations, if you will gather the data. Go to 8000 ft, with the altimeter set to 29.92. Record the outside air temperature. Do four runs, every 90 deg (track or heading - it doesn't matter for this method). Let the aircraft stabilize on speed. Record the IAS, GPS ground speed, and GPS track for each run. All runs must be at the same IAS, even if this means you need to do a very slight climb or descent on some runs. Reset the altimeter after the tests are complete. Prop pitch - if you get 2650 rpm at 8000 ft with full throttle, the prop pitch is probably not the reason why you are so slow. If 2650 is with less than full throttle, then the prop pitch may be to blame. Mind you, I think the redline with that prop is 2600 rpm, so you may need a different pitch to avoid going over redline. Tachometer accuracy - find a prop tach, and verify the tach is accurate. Engine - How many hours on the engine? Is there perhaps a problem with the mixture, carb or air filter? Wing twist - find a digital level (Smart Level) and check the incidence of each wing at several stations. Do you have a wing twist? Flaps and ailerons - check the rigging when they are retracted. If they are rigged so that they don't come all the way up to zero, that could slow you down a bit. According to Van's web site, that aircraft should be able to do about 188 mph TAS at 8000 ft. The numbers you mention are certainly well short of that, if the IAS is accurate. 145 mph CAS at 8000 ft, standard day, is about 163 mph TAS. Keep us posted, -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
All fairings are installed. The airplane is trimmed out, painted, clean, etc. I'm going to do some extensive GPS tests tomorrow, as well as noting the MAP and Fuel Flow to make sure that it is inline with engine performance. As far as the prop is concerned, I was under the impression that Sensenich has removed the 2600 RPM restriction on the 160 HP models. Only the 180 HP has the 2600 restriction. 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: "Kevin Horton" <khorto1537(at)rogers.com> Subject: Re: RV-List: RV-6A airspeed problem > > > > >I am helping a friend fly off the restrictions of his RV-6A. He has > >an O-320 with a Sensenich metal prop sold by Van's. I don't know > >the pitch, but it was ordered from Van's as the prop for the RV-6 > >and a 160 HP O-320. > > > >We can't seem to get more than about 145 KIAS out of this airplane. > >Have checked it with GPS, and it is close enough. Here is what we > >have so far: > > > >Max RPM we can get out of it is about 2650. (8000' 75%) > >Manifold pressure is good. > >Climb is very good. 1500 FPM 80 KIAS > >All fairings and pants are installed > > > >Could there be a pitch problem here? 140 KIAS seems pretty slow for an O-320. > > > >Anyone else flying a Sensenich have this problem? All signs are > >pointing to the prop. > > > >Paul Besing > > Paul, > > I assume all the fairings are installed, but you didn't mention that. > Please confirm. > > Airspeed Accuracy - You say the airspeed was checked with the GPS - > which method did you use? Was this checked at the same time the 145 > mph speed was determined, or did you check the airspeed accuracy some > other time? I would like to nail down the accuracy of this speed, to > make sure that we aren't looking at an inaccuracy in the IAS. I like > Doug Gray's method, as modified by the National Test Pilot School. > See: > > http://members.rogers.com/khorton/rvlinks/doug_gray/TASCALC.ZIP > http://www.ntps.com/GPS_SpeedTrack.XLS > > If you want, I would be happy to run the calculations, if you will > gather the data. Go to 8000 ft, with the altimeter set to 29.92. > Record the outside air temperature. Do four runs, every 90 deg > (track or heading - it doesn't matter for this method). Let the > aircraft stabilize on speed. Record the IAS, GPS ground speed, and > GPS track for each run. All runs must be at the same IAS, even if > this means you need to do a very slight climb or descent on some > runs. Reset the altimeter after the tests are complete. > > Prop pitch - if you get 2650 rpm at 8000 ft with full throttle, the > prop pitch is probably not the reason why you are so slow. If 2650 > is with less than full throttle, then the prop pitch may be to blame. > Mind you, I think the redline with that prop is 2600 rpm, so you may > need a different pitch to avoid going over redline. > > Tachometer accuracy - find a prop tach, and verify the tach is accurate. > > Engine - How many hours on the engine? Is there perhaps a problem > with the mixture, carb or air filter? > > Wing twist - find a digital level (Smart Level) and check the > incidence of each wing at several stations. Do you have a wing twist? > > Flaps and ailerons - check the rigging when they are retracted. If > they are rigged so that they don't come all the way up to zero, that > could slow you down a bit. > > According to Van's web site, that aircraft should be able to do about > 188 mph TAS at 8000 ft. The numbers you mention are certainly well > short of that, if the IAS is accurate. 145 mph CAS at 8000 ft, > standard day, is about 163 mph TAS. > > Keep us posted, > -- > Kevin Horton RV-8 (cowling, wing tip lights) > Ottawa, Canada > http://members.rogers.com/khorton/rv8.html > > ________________________________________________________________________________
From: "Doug Weiler" <dougweil(at)pressenter.com>
Subject: Re: . and engine horsepower mods.
Date: Oct 28, 2002
> > > There's another side to this that few seem to consider, that Stein just > brought up. Everything you do to these engines to get more HP is going > to reduce the life of the engine. I, too had dreams of high compression > pistons, polished and ported, custom induction, etc. to get the most > speed out of my bird. Until July 31 this year, when I was involved in > an engine failure accident at very low altitude (200 feet- take off) > over very unhospitable terrain (city.) I wasn't flying, just a > passenger, and except for quick thinking and excellent airmanship on the > part of the pilot, it could well have been five fatalities. As it was > we all walked away with minor injuries. After some soul searching, I > decided to stick with my project, but I resolved that I would not do > ANYTHING which would decrease engine reliability. No fuel system mods, > no souped up anything. These planes fly great on a box-stock engine. > Sure, you may get another 5 or even 10 mph by tricking them out, but at > what cost? It's just not worth the risk, IMHO. > > Jeff Point > RV-6 finish kit > Milwaukee WI Jeff brings up a very good point (and I am also glad he is here to discuss it). Many folks do "soup" up their engines, but when I decided to have Bart LeLond build up my engine, I told him I wanted the safest, most reliable engine he could build. Thus it is a rather plain Jane, 0-360-A1A, carb, mags, etc... just standard everything. Just my two cents worth. Doug Weiler Hudson, WI Flying RV-4 Under construction RV-4 ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
Dear Paul, I think it is the other way around regarding Sensenich's Prop Limitation: I believe the 160hp is limited to 2600 RPM, but the 180hp is not. But then I may be wrong (again?) Konrad > I was under the impression that Sensenich has removed the 2600 RPM restriction on the 160 HP models. > Only the 180 HP has the 2600 restriction. > > Paul Besing > RV-6A Sold (Waiting on the RV-10) ________________________________________________________________________________
Date: Oct 28, 2002
From: Art Glaser <airplane(at)megsinet.net>
Subject: Re: RV-6A airspeed problem
I just rechecked the site and 2600 is still the red line for the 320 prop. Konrad Werner wrote: > > Dear Paul, > I think it is the other way around regarding Sensenich's Prop Limitation: > I believe the 160hp is limited to 2600 RPM, but the 180hp is not. > But then I may be wrong (again?) > Konrad > > > I was under the impression that Sensenich has removed the 2600 RPM > restriction on the 160 HP models. > > Only the 180 HP has the 2600 restriction. > > > > Paul Besing > > RV-6A Sold (Waiting on the RV-10) > ________________________________________________________________________________
From: "Larry Pardue" <n5lp(at)carlsbad.net>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
> > All fairings are installed. The airplane is trimmed out, painted, clean, > etc. I'm going to do some extensive GPS tests tomorrow, as well as noting > the MAP and Fuel Flow to make sure that it is inline with engine > performance. As far as the prop is concerned, I was under the impression > that Sensenich has removed the 2600 RPM restriction on the 160 HP models. > Only the 180 HP has the 2600 restriction. > Just the opposite. No restriction on the 180 HP but the 2600 restriction is still in effect for the 160 HP. http://www.sensenich.com/new/70cmprop.htm Larry Pardue Carlsbad, NM RV-6 N441LP Flying http://www.carlsbadnm.com/n5lp/index.htm ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
145 KIAS (knots) is 167 IAS (mph) there is also a correction addition for 8000' altitude so the True is above 170mph. Might check timing and induction. Does the engine when the mixture is slowly pulled exhibit the 25 to 50 rpm expected rise? 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: "Paul Besing" <azpilot(at)extremezone.com> Subject: Re: RV-List: RV-6A airspeed problem > > All fairings are installed. The airplane is trimmed out, painted, clean, > etc. I'm going to do some extensive GPS tests tomorrow, as well as noting > the MAP and Fuel Flow to make sure that it is inline with engine > performance. As far as the prop is concerned, I was under the impression > that Sensenich has removed the 2600 RPM restriction on the 160 HP models. > Only the 180 HP has the 2600 restriction. > > 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: "Kevin Horton" <khorto1537(at)rogers.com> > To: > Subject: Re: RV-List: RV-6A airspeed problem > > > > > > > > > >I am helping a friend fly off the restrictions of his RV-6A. He has > > >an O-320 with a Sensenich metal prop sold by Van's. I don't know > > >the pitch, but it was ordered from Van's as the prop for the RV-6 > > >and a 160 HP O-320. > > > > > >We can't seem to get more than about 145 KIAS out of this airplane. > > >Have checked it with GPS, and it is close enough. Here is what we > > >have so far: > > > > > >Max RPM we can get out of it is about 2650. (8000' 75%) > > >Manifold pressure is good. > > >Climb is very good. 1500 FPM 80 KIAS > > >All fairings and pants are installed > > > > > >Could there be a pitch problem here? 140 KIAS seems pretty slow for an > O-320. > > > > > >Anyone else flying a Sensenich have this problem? All signs are > > >pointing to the prop. > > > > > >Paul Besing > > > > Paul, > > > > I assume all the fairings are installed, but you didn't mention that. > > Please confirm. > > > > Airspeed Accuracy - You say the airspeed was checked with the GPS - > > which method did you use? Was this checked at the same time the 145 > > mph speed was determined, or did you check the airspeed accuracy some > > other time? I would like to nail down the accuracy of this speed, to > > make sure that we aren't looking at an inaccuracy in the IAS. I like > > Doug Gray's method, as modified by the National Test Pilot School. > > See: > > > > http://members.rogers.com/khorton/rvlinks/doug_gray/TASCALC.ZIP > > http://www.ntps.com/GPS_SpeedTrack.XLS > > > > If you want, I would be happy to run the calculations, if you will > > gather the data. Go to 8000 ft, with the altimeter set to 29.92. > > Record the outside air temperature. Do four runs, every 90 deg > > (track or heading - it doesn't matter for this method). Let the > > aircraft stabilize on speed. Record the IAS, GPS ground speed, and > > GPS track for each run. All runs must be at the same IAS, even if > > this means you need to do a very slight climb or descent on some > > runs. Reset the altimeter after the tests are complete. > > > > Prop pitch - if you get 2650 rpm at 8000 ft with full throttle, the > > prop pitch is probably not the reason why you are so slow. If 2650 > > is with less than full throttle, then the prop pitch may be to blame. > > Mind you, I think the redline with that prop is 2600 rpm, so you may > > need a different pitch to avoid going over redline. > > > > Tachometer accuracy - find a prop tach, and verify the tach is accurate. > > > > Engine - How many hours on the engine? Is there perhaps a problem > > with the mixture, carb or air filter? > > > > Wing twist - find a digital level (Smart Level) and check the > > incidence of each wing at several stations. Do you have a wing twist? > > > > Flaps and ailerons - check the rigging when they are retracted. If > > they are rigged so that they don't come all the way up to zero, that > > could slow you down a bit. > > > > According to Van's web site, that aircraft should be able to do about > > 188 mph TAS at 8000 ft. The numbers you mention are certainly well > > short of that, if the IAS is accurate. 145 mph CAS at 8000 ft, > > standard day, is about 163 mph TAS. > > > > Keep us posted, > > -- > > Kevin Horton RV-8 (cowling, wing tip lights) > > Ottawa, Canada > > http://members.rogers.com/khorton/rv8.html > > > > > > ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
I may have missed it in earlier posts, but what kind of elevator trim is required at cruise? I did notice that she likes to climb and was wondering if she needs a lot of nose down trim. If so, check the incidence at the horizontal. I am not an engineer, but I believe a horizontal out of spec will cost you airspeed. Just a thought, Jerry Calvert N296JC -6 ----- Original Message ----- From: "Paul Besing" <azpilot(at)extremezone.com> Subject: Re: RV-List: RV-6A airspeed problem > > All fairings are installed. The airplane is trimmed out, painted, clean, > etc. I'm going to do some extensive GPS tests tomorrow, as well as noting > the MAP and Fuel Flow to make sure that it is inline with engine > performance. As far as the prop is concerned, I was under the impression > that Sensenich has removed the 2600 RPM restriction on the 160 HP models. > Only the 180 HP has the 2600 restriction. > > 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: "Kevin Horton" <khorto1537(at)rogers.com> > To: > Subject: Re: RV-List: RV-6A airspeed problem > > > > > > > > > >I am helping a friend fly off the restrictions of his RV-6A. He has > > >an O-320 with a Sensenich metal prop sold by Van's. I don't know > > >the pitch, but it was ordered from Van's as the prop for the RV-6 > > >and a 160 HP O-320. > > > > > >We can't seem to get more than about 145 KIAS out of this airplane. > > >Have checked it with GPS, and it is close enough. Here is what we > > >have so far: > > > > > >Max RPM we can get out of it is about 2650. (8000' 75%) > > >Manifold pressure is good. > > >Climb is very good. 1500 FPM 80 KIAS > > >All fairings and pants are installed > > > > > >Could there be a pitch problem here? 140 KIAS seems pretty slow for an > O-320. > > > > > >Anyone else flying a Sensenich have this problem? All signs are > > >pointing to the prop. > > > > > >Paul Besing > > > > Paul, > > > > I assume all the fairings are installed, but you didn't mention that. > > Please confirm. > > > > Airspeed Accuracy - You say the airspeed was checked with the GPS - > > which method did you use? Was this checked at the same time the 145 > > mph speed was determined, or did you check the airspeed accuracy some > > other time? I would like to nail down the accuracy of this speed, to > > make sure that we aren't looking at an inaccuracy in the IAS. I like > > Doug Gray's method, as modified by the National Test Pilot School. > > See: > > > > http://members.rogers.com/khorton/rvlinks/doug_gray/TASCALC.ZIP > > http://www.ntps.com/GPS_SpeedTrack.XLS > > > > If you want, I would be happy to run the calculations, if you will > > gather the data. Go to 8000 ft, with the altimeter set to 29.92. > > Record the outside air temperature. Do four runs, every 90 deg > > (track or heading - it doesn't matter for this method). Let the > > aircraft stabilize on speed. Record the IAS, GPS ground speed, and > > GPS track for each run. All runs must be at the same IAS, even if > > this means you need to do a very slight climb or descent on some > > runs. Reset the altimeter after the tests are complete. > > > > Prop pitch - if you get 2650 rpm at 8000 ft with full throttle, the > > prop pitch is probably not the reason why you are so slow. If 2650 > > is with less than full throttle, then the prop pitch may be to blame. > > Mind you, I think the redline with that prop is 2600 rpm, so you may > > need a different pitch to avoid going over redline. > > > > Tachometer accuracy - find a prop tach, and verify the tach is accurate. > > > > Engine - How many hours on the engine? Is there perhaps a problem > > with the mixture, carb or air filter? > > > > Wing twist - find a digital level (Smart Level) and check the > > incidence of each wing at several stations. Do you have a wing twist? > > > > Flaps and ailerons - check the rigging when they are retracted. If > > they are rigged so that they don't come all the way up to zero, that > > could slow you down a bit. > > > > According to Van's web site, that aircraft should be able to do about > > 188 mph TAS at 8000 ft. The numbers you mention are certainly well > > short of that, if the IAS is accurate. 145 mph CAS at 8000 ft, > > standard day, is about 163 mph TAS. > > > > Keep us posted, > > -- > > Kevin Horton RV-8 (cowling, wing tip lights) > > Ottawa, Canada > > http://members.rogers.com/khorton/rv8.html > > > > > > ________________________________________________________________________________
Date: Oct 28, 2002
From: Gary & Carolyn Zilik <zilik(at)direcpc.com>
Subject: Re: RV-6A airspeed problem
> I was under the impression > that Sensenich has removed the 2600 RPM restriction on the 160 HP models. > Only the 180 HP has the 2600 restriction According to Sensenich (http://www.sensenich.com/direct/vans.htm) the 70CM series propeller has a placard required to avoid operation above 2600 RPM. The 72FM series propeller restriction is set at 2700 RPM. Also at http://www.sensenich.com/misc/faq70cm.htm Q) How important is the 2600 RPM restriction? A) Extremely important! The propeller has a tenth order, third mode vibration when operated above 2600 RPM. Q) What if I accidentally exceed the 2600 RPM restriction? A) You absolutely must not exceed the 2600 RPM restriction! We have pitched the propeller so that at altitude, you will max out at 2600 full throtle level. Every aircraft and engine will be a little different; so a slight pitch adjustment at the local prop shop may be in order. Q) I heard a rumor that you are going to remove the 2600 RPM restriction. Any truth to that? A) You should assume that the placard will always be there! Gary ________________________________________________________________________________
Subject: RV7A Empennage Options
From: "" <tx_jayhawk(at)excite.com>
Date: Oct 28, 2002
All, After "watching" the list for the last three years, I am finally ready to order the empennage. I resisted for so long on the basis of three things that I promised to do first: 1) Finish instrument rating, 2) Sell Cherokee, and 3) Finish garage. The last of the three got close enough this weekend, and I am filling out the forms. I have chosen the RV7A, and I have a question: What difference is there in the kit if you check the "no lights in wingtips" option? I assume that means different fiberglass tips? What lights are they designed to accomadate? If I am semi-undecided now, is it hard to change one way or another with either set on down the road? I like the "lights in the wingtips" design...is there something like that for the tail? Thanks in advance,Scott Join Excite! - http://www.excite.com The most personalized portal on the Web! ________________________________________________________________________________
From: "Ken Stribling" <ken(at)soundsuckers.com>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
I was just curious but I was under the impression that the gps read the planes airspeed from the satellites and barometer and other factors should not matter KEN S. ----- Original Message ----- From: "Jerry Calvert" <rv6(at)cox.net> Subject: Re: RV-List: RV-6A airspeed problem > > I may have missed it in earlier posts, but what kind of elevator trim is > required at cruise? I did notice that she likes to climb and was wondering > if she needs a lot of nose down trim. If so, check the incidence at the > horizontal. I am not an engineer, but I believe a horizontal out of spec > will cost you airspeed. > > Just a thought, > Jerry Calvert > N296JC -6 > > > ----- Original Message ----- > From: "Paul Besing" <azpilot(at)extremezone.com> > To: > Subject: Re: RV-List: RV-6A airspeed problem > > > > > > All fairings are installed. The airplane is trimmed out, painted, clean, > > etc. I'm going to do some extensive GPS tests tomorrow, as well as noting > > the MAP and Fuel Flow to make sure that it is inline with engine > > performance. As far as the prop is concerned, I was under the impression > > that Sensenich has removed the 2600 RPM restriction on the 160 HP models. > > Only the 180 HP has the 2600 restriction. > > > > 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: "Kevin Horton" <khorto1537(at)rogers.com> > > To: > > Subject: Re: RV-List: RV-6A airspeed problem > > > > > > > > > > > > > > >I am helping a friend fly off the restrictions of his RV-6A. He has > > > >an O-320 with a Sensenich metal prop sold by Van's. I don't know > > > >the pitch, but it was ordered from Van's as the prop for the RV-6 > > > >and a 160 HP O-320. > > > > > > > >We can't seem to get more than about 145 KIAS out of this airplane. > > > >Have checked it with GPS, and it is close enough. Here is what we > > > >have so far: > > > > > > > >Max RPM we can get out of it is about 2650. (8000' 75%) > > > >Manifold pressure is good. > > > >Climb is very good. 1500 FPM 80 KIAS > > > >All fairings and pants are installed > > > > > > > >Could there be a pitch problem here? 140 KIAS seems pretty slow for an > > O-320. > > > > > > > >Anyone else flying a Sensenich have this problem? All signs are > > > >pointing to the prop. > > > > > > > >Paul Besing > > > > > > Paul, > > > > > > I assume all the fairings are installed, but you didn't mention that. > > > Please confirm. > > > > > > Airspeed Accuracy - You say the airspeed was checked with the GPS - > > > which method did you use? Was this checked at the same time the 145 > > > mph speed was determined, or did you check the airspeed accuracy some > > > other time? I would like to nail down the accuracy of this speed, to > > > make sure that we aren't looking at an inaccuracy in the IAS. I like > > > Doug Gray's method, as modified by the National Test Pilot School. > > > See: > > > > > > http://members.rogers.com/khorton/rvlinks/doug_gray/TASCALC.ZIP > > > http://www.ntps.com/GPS_SpeedTrack.XLS > > > > > > If you want, I would be happy to run the calculations, if you will > > > gather the data. Go to 8000 ft, with the altimeter set to 29.92. > > > Record the outside air temperature. Do four runs, every 90 deg > > > (track or heading - it doesn't matter for this method). Let the > > > aircraft stabilize on speed. Record the IAS, GPS ground speed, and > > > GPS track for each run. All runs must be at the same IAS, even if > > > this means you need to do a very slight climb or descent on some > > > runs. Reset the altimeter after the tests are complete. > > > > > > Prop pitch - if you get 2650 rpm at 8000 ft with full throttle, the > > > prop pitch is probably not the reason why you are so slow. If 2650 > > > is with less than full throttle, then the prop pitch may be to blame. > > > Mind you, I think the redline with that prop is 2600 rpm, so you may > > > need a different pitch to avoid going over redline. > > > > > > Tachometer accuracy - find a prop tach, and verify the tach is accurate. > > > > > > Engine - How many hours on the engine? Is there perhaps a problem > > > with the mixture, carb or air filter? > > > > > > Wing twist - find a digital level (Smart Level) and check the > > > incidence of each wing at several stations. Do you have a wing twist? > > > > > > Flaps and ailerons - check the rigging when they are retracted. If > > > they are rigged so that they don't come all the way up to zero, that > > > could slow you down a bit. > > > > > > According to Van's web site, that aircraft should be able to do about > > > 188 mph TAS at 8000 ft. The numbers you mention are certainly well > > > short of that, if the IAS is accurate. 145 mph CAS at 8000 ft, > > > standard day, is about 163 mph TAS. > > > > > > Keep us posted, > > > -- > > > Kevin Horton RV-8 (cowling, wing tip lights) > > > Ottawa, Canada > > > http://members.rogers.com/khorton/rv8.html > > > > > > > > > > > > ________________________________________________________________________________
Date: Oct 28, 2002
From: Tedd McHenry <tedd(at)vansairforce.org>
Subject: Re: Not really RV related
I used an amazon.com gift certificate last year to buy bottom-end Garmin GPS III Plus, and I've found it quite useful. It's not even an aviation unit, and of course it has no aviation database. But I enter in the various airports and waypoints manuall (and share them with a couple of friends), and it makes a useful little unit I can take in any of the planes I rent, for not much money. Tedd McHenry -6 wings Surrey, BC ________________________________________________________________________________
From: "Larry Pardue" <n5lp(at)carlsbad.net>
Subject: Re: RV-6A airspeed problem
Date: Oct 28, 2002
> > I was just curious but I was under the impression that the gps read the > planes airspeed from the satellites and barometer and other factors should > not matter > GPS does not read airspeed at all. GPS is capable of displaying groundspeed, and from that there are various ways to derive true airspeed. This is very handy because it lets us figure out if the airspeed system in the airplane is accurate. This can be done by converting the indicated airspeed in the airplane to true airspeed by applying the altitude, pressure and temperature corrections and comparing it to the GPS derived TAS or by working in reverse from the known TAS. It is also a very very common misconception that GPS shows heading. It does not and if the track information that it does display is treated as heading it can cause problems for ATC. They do expect heading information, both when they ask and when they give a heading to fly. Everything you might want to know, and more, about his kind of stuff is on Kevin Horton's website. http://members.rogers.com/khorton/rv8.html You can count on the flight test stuff on this site. He knows what he is talking about. Larry Pardue Carlsbad, NM RV-6 N441LP Flying http://www.carlsbadnm.com/n5lp/index.htm ________________________________________________________________________________
Date: Oct 28, 2002
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: Re: Not really RV related
Glad to see that "-6 wings" in your post-way to go! Spirit! Drive da' boddy! Determination! Focus! Take you meals in that garage-cum-RV nest! Notice you've got a wife and friends at Christmas-that's what holiays are for, anyways. You better not be reading this until tomorrow at work... Scott ----- Original Message ----- From: "Tedd McHenry" <tedd(at)vansairforce.org> Subject: Re: RV-List: Not really RV related > > I used an amazon.com gift certificate last year to buy bottom-end Garmin GPS > III Plus, and I've found it quite useful. It's not even an aviation unit, and > of course it has no aviation database. But I enter in the various airports and > waypoints manuall (and share them with a couple of friends), and it makes a > useful little unit I can take in any of the planes I rent, for not much money. > > Tedd McHenry > -6 wings > Surrey, BC > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Ya Gotta Wonder
Date: Oct 28, 2002
And good night to you Austin. Great dreams and good mornings, From The RV list ----- Original Message ----- From: "Austin" <6430(at)axion.net> Subject: RV-List: Ya Gotta Wonder > > HIT DELETE IF YOU SEEK BUILDING HELP > ONLY SLIGHTLY RV RELATED.. > Hi listers, you rivet pounding ground bound bunch of dreamers,...with due > respect, > Yes, you do gotta wonder what kind of a world you enter when you get the old > bird flying and dream of what the hell you are going to do next to throw gas > on the fire of the dream that got you thinking about building and flying a > special hot rod like we have. > I have flown an RV before and sold the dream machine only that I may > go on to do more than I thought I could by building another with more stuff > and more snot than I think I could handle. > I do have a few snags to fix...I ain't an electrical genius or any other > kind if genius, but I have had to work through a few gremlins before I can > get the hours off and fling myself any place they have fuel.... > So I called my respected and awesome friend, who shall remain > nameless ere he gets embarrassed by knowing me....suffice to say he is well > respected and has mega hours on everything..and is getting grey and hard of > hearing from those radials by the day.....anyway, I lay on my sad story > about snags and how when this is done, I am going clawing for altitude to > get over the rocks and head out his way and carry on to farther reaches.... > He says."Great !..tell me when and we will hook up and fly up to the Arctic > circle just for the hell of it .....it is no bigee to just keep going ..the > RV is fast and comfortable..and we can have a great time...." > Now, I say, you just gotta wonder..this would never happen to me to fly up > to the Tundra in a magic carpet I built, if it wasn't for these > airplanes..in company with one of the most respected and fly savvy wonderful > guys you could ever hook up with......him and GPS..and the landscape will > look the same from windshield to past the horizon, where no man lives and > only Caribou call home....them and the bears.... > Floats would be as useful as wheels up here...cell phones might save your > a** if you get onto an ice floe that breaks off from the main pack....but > the sun will either shine forever or not at all, depending on when you go > there. > The hoot is, we are both senior citizens who forget to turn the turn > signal off and younger folk can't wait to pass when we are on the > road....with an RV, age is only a number....how lucky you 30 ish guys are > that you have so many more years to enjoy it !! > There are strips in the far North where it costs $500 to open the > hangar doors due to heat loss, and maybe $1500 to have some fuel cached for > you....but I don't think we will need our parkas and reindeer hide outfits > when we plan to see the Northern Lights.... > I looked at an airways map today which covers the whole country, coast > to coast...Man ! that is a long way...I wonder what the fuel bill will > be...money well spent just the same.. > Some one once told me that a long cross country was just a matter of a > few short, point to point trips...with that in mind, I know it can be > done... > There are many long distance stories about RV flights and most of them > never written about, but just think a while about the guy who flew around > the world twice in an RV4, and then almost pole to pole as well....about > another guy who flew to Costa Rica, and Claudio Tonnini who flew Purple > Passion down to Argentina..twice... > None of these guys let graft and red tape get in the way of a dream... > At least where I am headed one day, the wolves and Caribou only take a toll > on each other..no beaurocrats in shoulder brass to rush out and grab a fee > or stamp your papers.... > I see the fog and mist has lifted, and the sun is peeking out of the > Indian Summer sky, and there is daylight left to go fly a while before early > dusk ........ > Just up off the field at 1500, I can suddenly see all the red and gold > of the trees below...better than any other year, and I head off to the river > and point her down and watch the speed build and as the river twists and > sand bars catch the bends and the weary, beaten red bodies of the salmon > run, I have scarce time to watch it as I climb up over a Hemlock laden pass > with the first touches of snow and turn right and down again, still doing > 200, and there, at once, is the flood plain, green and civilized and safe, > and radio calls come into the headset to tell me the field below is open and > coffee and pie await...... > That's all there is time for as darkness is coming and although I > can see for 30 miles or so, and the horizon is still pink over black, the > home field is hard to find because all below is black and there is no > contrast..no feature to pick out in that time between twilight and when car > lights come on. > I have my strobes on and am trying out my wig-wag landing lights, and > I have found the ferry where it crosses the river and head straight South > from there....home is 3 miles away... > The tower folks are still there, but not for long, and they tell me they can > see my wig-wag very well and there is no other traffic. > I am cleared straight in and that is always nice and I get set up early and > all I have to do is wait and watch speed and descent....I can see a black > strip and silver roofed hangars and know I am lined up right and soon I > cross over the road above the roof of a pickup, just putting his lights on, > and Vasi lights look pretty and tell me I am high and I stop looking and > settle just past the numbers and hear " chirp chirp "..sounds like a decent > one, and taxi home... > Cowling feels good and smells good and ticking starts and I say " Goodnight > " and head out the gate......... > There is one flyer left, and he sits above on the lamp post and keeps his > perch since I am not stopping....he used to fly off when anything > approached, but now this big Hawk owns the field and is looking for other > types of movement..... > The wind sock is swinging a bit and is lit from within, and is so > different from daytime and because it is a beacon now....pretty lights > coming on and streams of light flow down the road to where home and hearth > await....time to fill in the logbook and try to drive a bit slower than 75, > now that I am on the ground...... > Ya gotta wonder....what can be better than this other than flying in > company with a pal ?? > Good night all, > Austin > > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Oct 28, 2002
Subject: Re: . and engine horsepower mods.
In a message dated 10/28/2002 11:54:49 AM Pacific Standard Time, jpoint(at)mindspring.com writes: > I resolved that I would not do > ANYTHING which would decrease engine reliability. No fuel system mods, > no souped up anything. These planes fly great on a box-stock engine. > Sure, you may get another 5 or even 10 mph by tricking them out, but at > what cost? It's just not worth the risk, IMHO. Well...hold on just a second. I agree with you to some degree that there is an inverse relationship between engine performance and longevity, but that's a far cry from saying that you can't safely get a little better performance without your engine stopping. Was the outage you mentioned actually and directly attributable to something done to that engine to increase performance or was it just bad karma? -GV (RV-6A N1GV 572hrs) ________________________________________________________________________________
From: "Jim Cimino" <jcimino(at)echoes.net>
Subject: S-Tech auto pilot buying
Date: Oct 28, 2002
Where is the best place to purchase an S-Tech 30? Jim Cimino RV-8 sn 80039 N7TL 75+ Hrs. http://www.geocities.com/jcimino.geo/ (570)842-4057 ________________________________________________________________________________
From: "Randy Compton" <rdcompton(at)earthlink.net>
Subject: Re: . and engine horsepower mods.
Date: Oct 28, 2002
----- Original Message ----- > Jeff brings up a very good point (and I am also glad he is here to discuss > it). Many folks do "soup" up their engines, but when I decided to have > Bart LeLond build up my engine, I told him I wanted the safest, most > reliable engine he could build. Thus it is a rather plain Jane, 0-360-A1A, > carb, mags, etc... just standard everything. Just my two cents worth. > > Doug Weiler > Hudson, WI > Flying RV-4 > Under construction RV-4 Boy, do I concur with Doug here. I went with all the "trick" stuff at my major overhaul on my stock 150hp O-320 back in the spring: high-compression pistons, "flow-matched" cylinders, electronic ignition, "blueprinting", blah,blah,blah; all "guaranteed" to have that O-320 puttin' out 180hp. Man, I was like a kid waiting on Christmas! Visions of eye-watering performance was dancing in my head.... Frankly, ain't seen much of a change in performance at all, other than what would be expected before/after from an engine that needed an overhaul due to a badly worn out camshaft. Sure, the overhaul work seems to have been done well, and the engine runs much smoother gives a bit better climb performance. But instead of finding that that cool toy under the tree, I feel like all I got from Santa was clothes. About the only thing I can absolutely quantify is that I now have an "experimental" engine. If I could do it over again, I'd save some money by just having my engine re-built (to new tolerances, of course) the way Lycoming made it in the first place. I doubt I'd notice any less ooomph out of it, and I'd have a lot more peace of mind about what I've got up there under the hood. And I'd still have a certified engine. Randy Compton RV-3A N84VF Gulf Breeze, FL ________________________________________________________________________________
Date: Oct 28, 2002
From: Robert McCallum <robert.mccallum2(at)sympatico.ca>
Subject: Re: . and engine horsepower mods.
Jeff Point wrote: > Everything you do to these engines to get more HP is going > to reduce the life of the engine. I, too had dreams of high compression > pistons, polished and ported, custom induction, etc. to get the most > speed out of my bird. Until July 31 this year, when I was involved in > an engine failure accident at very low altitude (200 feet- take off) > over very unhospitable terrain (city.) I wasn't flying, just a > passenger, and except for quick thinking and excellent airmanship on the > part of the pilot, it could well have been five fatalities. As it was > we all walked away with minor injuries. After some soul searching, I > decided to stick with my project, but I resolved that I would not do > ANYTHING which would decrease engine reliability. No fuel system mods, > no souped up anything. These planes fly great on a box-stock engine. > Sure, you may get another 5 or even 10 mph by tricking them out, but at > what cost? It's just not worth the risk, IMHO. > > Jeff Point > RV-6 finish kit > Milwaukee WI Although these statements contain a good deal of truth they are not necessarily 100% true. One thing to consider is that some "hot-rodding" modifications do as much or more for longevity and reliability as they do for HP gains. Things like balancing and minor porting & polishing make an engine run smoother and more evenly match the horsepower of each of the cylinders to one another. Both good things! If you don't do these mods with the view to achieving the most HP gain but only to equalize the stresses within the engine then "modifications" can create increased reliability and be a good thing. (with a small HP gain and possibly a slightly improved fuel economy as a free bonus) If you modify with the purpose of achieving the most HP possible then Jeff's statements above apply and you will definitely end up with a less reliable and shorter lived engine and you would be well advised to remain "stock." -- Bob McC ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Oct 28, 2002
Subject: Re: RV-6A airspeed problem
In a message dated 10/28/2002 6:03:55 PM Pacific Standard Time, ken(at)soundsuckers.com writes: > I was just curious but I was under the impression that the GPS read the > planes airspeed from the satellites Huh? -GV (RV-6A N1GV 572hrs) ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Oct 28, 2002
Subject: Re: Hi-EGT's
In a message dated 10/28/2002 3:02:12 PM Pacific Standard Time, rv8tor(at)lazy8.net writes: > A fouled or misfiring spark plug will defiantly make the EGT go up (the fuel > is still burning as it exits the cylinder). I traded my defiant plugs for compliant ones and that helped. -GV (RV-6A N1GV 572hrs) ________________________________________________________________________________
Date: Oct 28, 2002
From: David Aronson <aronsond(at)pacbell.net>
Subject: microair 760/T-2000 for sale
Listers: I have two Microair units, one each 760 com and one T-2000 transponder for sale. Both are new, in box. I ordered two of each as my hanger buddy wanted the same units for his RV-8. He waited and waited and lost interest, ordered a Becker and is still waiting. These arrived and I will "give them away" for: 760------$675 T-2000--$1400 I'll pay for ground shipping in the USA. Get back to me aronsond(at)pacbell.net Dave Aroson RV4 N504RV ________________________________________________________________________________
From: Larygagnon(at)aol.com
Date: Oct 29, 2002
Subject: EC 100 checklist
Does anyone using the Vision Micro System VM1000 with EC100 checklist have a sample of the items programed into the EC100 for a carburated O360. I can't find anything in the archives and want to see if I'm forgetting anything. Thanks in advance. Larry Gagnon RV6/O-360 N6LG (getting close) ________________________________________________________________________________
From: "Amit Dagan" <amitdagan(at)hotmail.com>
Subject: RV7 floor stiffeners, ATC fuse holders
Date: Oct 29, 2002
Listers, In the past (looked it up in the archives) there were many cases of smoking rivets in the forward floor area, the ones that hold the floor to the firewall and stiffeners. It was attributed to the engine vibrations, and several methods of stiffening the area even more were raised, including using more rivets, larger (1/8") rivets, both, more stiffeners, double floor boards etc. In the RV7, I am not sure that this issue has been adressed, as one still needs to use 3/32" rivets, same number of stiffeners etc. I DO see that the rivet spacing is ~1" and not 1.25", and that there is a double floor in the center of the cabin (between the two inboard stiffeners). 1. Is that enough ? 2. If the answer to 1. is no, has anyone else done anything about this ? What ? Should I add more stiffeners ? double the floor ? On a totally different subject, if you like the fuse block idea used by the "Aero Electric Connection", check out the "new products" at http://www.pegasusautoracing.com/newproducts.htm and scroll down to Fuse Blocks for ATC Style Fuses. They have good prices for single quantities. And another thing: Heads up, when you are done drilling the stiffeners to the cabin floor, you might want to cleco them to the firewall and F-704 bulkhead, and with the floor off drill the 4 holes for the center section cover (This is the "double floor" between the two middle stiffeners) with the cover in place of course, for the nutplates that go there later. I think it is very easy to reach then, rather then wait untill the floor is riveted. Ah yes, and don't forget to make and drill and dimple the air-vent support angles (0.032") to the side skins before you disassemble the forward fuse. Amit. ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: RV7A Empennage Options
Date: Oct 28, 2002
Yes, that's the tips. There is a blister in the rudder bottom fairing for an aft tail light. If you choose these, you could easily send them back to Van's for the standard ones later on. Just keep them in good shape. For me, I prefer the single nav/strobe/position light in the wingtip. Very visible, and less wiring. Congrats on your decision to move forward. I have an empty RV feeling inside that makes me cry sometimes. Especially since I am flying someone else's RV right now. I want my own again!! 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: <tx_jayhawk(at)excite.com> Subject: RV-List: RV7A Empennage Options > > > All, > After "watching" the list for the last three years, I am finally ready to order the empennage. I resisted for so long on the basis of three things that I promised to do first: 1) Finish instrument rating, 2) Sell Cherokee, and 3) Finish garage. The last of the three got close enough this weekend, and I am filling out the forms. I have chosen the RV7A, and I have a question: What difference is there in the kit if you check the "no lights in wingtips" option? I assume that means different fiberglass tips? What lights are they designed to accomadate? If I am semi-undecided now, is it hard to change one way or another with either set on down the road? I like the "lights in the wingtips" design...is there something like that for the tail? > Thanks in advance,Scott > > Join Excite! - http://www.excite.com > The most personalized portal on the Web! > > ________________________________________________________________________________
Date: Oct 28, 2002
From: mitchf(at)netscape.com (Mitchell Faatz)
Subject: Re: S-Tech auto pilot buying
Contact John Stark: jts7(at)mindspring.com . Tell him Mitch Faatz sent ya, and to give me my GI-106A for free. ;) Really though, John will simply give you the best price. His great service is just a bonus! Mitch Faatz San Mateo, CA RV-6A finish kit Jim Cimino wrote: > >Where is the best place to purchase an S-Tech 30? > > ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: Not really RV related
Date: Oct 28, 2002
> Sorry for the "not RV" post. ... > But I'd like to ask the eminently logical bunch of RV builders and flyers on > this list which handheld GPS you are using? > Which model is the best value? > I don't want to spend much right now....(need the money for my RV 9a builder's > fund). > I apologize again for the off-topic topic. > Robert I have a Garmin Pilot III. I really like it. Nice that it can be configured for horiz or vertical orientation too. I got it after my panel was done so I made a retro-fit clip on deal for it -- see http://www.edt.com/homewing/rhproject/instp.html.The color 295 is sweet but seems just awfully bulky for a handheld. Nice when installed in the panel though. I do think its important with handhelds to have them up close to your field of vision. There's just too much button pushing involved with these things to be doing it all down in your lap. (Funny how people feel they have to apologize for "not RV related" posts like this. Seems like since there's likely a GPS in nearly every RV flying, it would be relevant....Obviously there's a "line" somewhere but IMHO this question is well this side of it. What I'm wondering though is whether putting a GPS in my plane is a 'privelige' or a 'right'.... :-} ) Randall Henderson, RV-6 N6R (~400 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
From: "George McNutt" <gmcnutt(at)intergate.ca>
Subject: RV-6A airspeed problem
Date: Oct 29, 2002
> > > > > > > >I am helping a friend fly off the restrictions of his RV-6A. He has > > > >an O-320 with a Sensenich metal prop sold by Van's. I don't know > > > >the pitch, but it was ordered from Van's as the prop for the RV-6 > > > >and a 160 HP O-320. > > > > > > > >We can't seem to get more than about 145 KIAS out of this airplane. > > > >Have checked it with GPS, and it is close enough. Here is what we > > > >have so far: > > > > > > > >Max RPM we can get out of it is about 2650. (8000' 75%) > > > >Manifold pressure is good. > > > >Climb is very good. 1500 FPM 80 KIAS > > > >All fairings and pants are installed > > > > > > > >Could there be a pitch problem here? 140 KIAS seems pretty slow for an O-320. > > > > > > > >Anyone else flying a Sensenich have this problem? All signs are > > > >pointing to the prop. > > > > > > > >Paul Besing > > > Hi Paul For comparison info here are some numbers from my preliminary testing. RV-6A with 160 HP 0-320, (90TT) turning a Sensenich fixed pitch metal prop, 79" pitch. At 8000' pressure altitude (8300' density altitude) 1500 lbs, I indicate the following. Full Throttle RPM is 2570, Manifold Pressure 22.3" which according to Vans formula is about 75% power, IAS 175 MPH (152KT) this suggests a top speed (TAS) of 196 MPH however I believe this is optimistic by about 10 MPH. My climb rate may be lower than yours. During my climb test at 110 MPH (96 KT) we measured 966 FPM (200' to 3100' in 3 min.) temperature ISA +6 and slightly over the 1750 Lbs gross weight. Typically I see a climb rate of 1000 FPM at 135 MPH and find that the climb rate stays nearly the same for speeds between 110 and 140 MPH, higher speeds let the prop wind up producing more power. Disclaimer: all the instruments lie a little bit, my OAT is not accurate and I second guess it against the forecast air temp, also I believe my airspeed over-reads by 5+ MPH at high speeds, also my testing is near mountains with subtle rising or subsiding air. Observe the 2600 RPM limit. Hope this data helps, George McNutt Langley B.C. Coming up on first 100 hr inspection. ________________________________________________________________________________
Date: Oct 29, 2002
From: Doug Gray <dgra1233(at)bigpond.net.au>
Subject: Re: RV-6A airspeed problem
> > >Climb is very good. 1500 FPM 80 KIAS Vans quoted RoC is for sea level and is the result of an extrapolation of climb figures at various altitudes, to sea level. RoC decreases with density altitude so also needs correction at each point for pressure and temperature. Vy of course is also a function of aircraft weight and needs also to be evaluated before embarking on RoC testing. (Another procedure and spreadsheet required.......) Oh dear...did someone say 'zip it'? Is this is an off the dial figure? If so, and dependent upon calibration of the VSI you may have climb performance consistent with Vans published figures. From an early brochure Vans figures for RoC at sea level for an RV-6 was 1600 fpm at gross and 2000 fpm at 1160lbs. These figures will drop approx. 100 fpm for each 1000' above sea level. BTW from Van's graphs Vy seems to be about 110 mph. Without knowing the details I'll hazard to guess you may yet have another 100 fpm up your sleeve. > Wing twist - find a digital level (Smart Level) and check the > incidence of each wing at several stations. Do you have a wing twist? > Flaps and ailerons - check the rigging when they are retracted. If > they are rigged so that they don't come all the way up to zero, that > could slow you down a bit. Also, check that the slip ball is centered both on the ground (wings level I hope!!) and when you are doing your speed trials. An out of trim condition can inadvertently be corrected with yaw adding significantly to drag. Doug Gray NB new email address... ________________________________________________________________________________
Date: Oct 29, 2002
From: Jeff Point <jpoint(at)mindspring.com>
Subject: Re: . and engine horsepower mods.
Vanremog(at)aol.com wrote: >>I resolved that I would not do >>ANYTHING which would decrease engine reliability. No fuel system mods, >>no souped up anything. These planes fly great on a box-stock engine. >>Sure, you may get another 5 or even 10 mph by tricking them out, but at >>what cost? It's just not worth the risk, IMHO. >> >> > >Well...hold on just a second. I agree with you to some degree that there is >an inverse relationship between engine performance and longevity, but that's >a far cry from saying that you can't safely get a little better performance >without your engine stopping. > >Was the outage you mentioned actually and directly attributable to something >done to that engine to increase performance or was it just bad karma? > > > OK, I'm holding on;) Notice I did not say I would not do anything at all to the engine (one elec ignition and one mag for example) just nothing which would decrease reliability. I mentioned fuel system mods- Van himself has written about how many builders come to grief by modifying his fuel system design, so I used that as one example. Another lister mentioned that balancing/ blueprinting an engine could increase it's lifespan by making it run smoother. This is true, but how many engines are given such treatment with the goal of increasing engine reliability? I doubt very many. That usually accompanies high compression pistons, polished, lapped, ported, etc etc etc. with one goal in mind. As long as such "tricked out" engines are inspected and overhauled on a more frequent, as needed basis there will likely be no problems, but I'd hate to have a post-accident thread down the road, as we do after accidents, because someone took their souped up engine, never looked inside it and figured it was good for 2000 hours because Lycoming said so. I hate to sound preachy, but an engine failure right after takeoff will give you true religion in a hurry. And no, I don't believe the 73 year old Continental radial had been souped up. The investigation is still pending, but it definately quit from something. I'm certainly no engine expert so I won't give my .02, but I just wanted to point out the alternative view in this thread, which no one had yet mentioned. Jeff Point ________________________________________________________________________________
Date: Oct 29, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: RV-6A airspeed problem
> >> >> >Climb is very good. 1500 FPM 80 KIAS > >Vans quoted RoC is for sea level and is the result of an >extrapolation of climb >figures at various altitudes, to sea level. RoC decreases with >density altitude >so also needs correction at each point for pressure and temperature. >Vy of course >is also a function of aircraft weight and needs also to be evaluated before >embarking on RoC testing. (Another procedure and spreadsheet required.......) >Oh dear...did someone say 'zip it'? > >Is this is an off the dial figure? If so, and dependent upon >calibration of the >VSI you may have climb performance consistent with Vans published >figures. From >an early brochure Vans figures for RoC at sea level for an RV-6 was >1600 fpm at >gross and 2000 fpm at 1160lbs. These figures will drop approx. 100 >fpm for each >1000' above sea level. > One more note - VSIs can have errors too, so when doing climb tests you need to use a stop watch against the altimeter to get the data, and then correct for temperature. I got into a real fur ball a few years ago with a guy who published an article in one of the popular aviation magazines about engine upgrades. He had put a more powerful engine in his Debonair, and really liked the improved performance, especially the 5,000 ft/min rate of climb. I sent a letter to the editor suggesting that they should review the articles before publishing them, because this piece of info was obviously in error. The author got very bent out of shape at me, and we had a long and heated exchange of letters. He eventually sent me a video tape which showed a sustained climb at an indicated 5,000 ft/min. But way over in the corner of the screen you could see the altimeter, and I timed only 1,600 ft/min. He was quite embarrassed when I pointed that out. -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
Date: Oct 29, 2002
From: kempthornes <kempthornes(at)earthlink.net>
Subject: Exhaust Pipe Wrap...
> >I've ceramic coated my exhaust, and you can grab and hold onto them about 20 >seconds after the engine is turned off. If you study the theory behind >this Where do I find this theory, Jim? I'd like to try to study it. K. H. (Hal) Kempthorne RV6-a N7HK flying! PRB (El Paso de Robles, CA) ________________________________________________________________________________
Date: Oct 29, 2002
From: <towertoy(at)earthlink.net>
Subject: Re: thermocoupler options for micromonitor
From: Knicholas2(at)aol.com Subject: RV-List: thermocoupler options for micromonitor I built a RMI micromonitor for my 0-320 and now have the options for CHT sensors. The manufacturer sells the bayonet type thermocoupler but the also approve a washer type thermocoupler made by Westach. Any opinions? (...I guess that is a dumb question on THIS list, there are LOTS of opinions here....) Any recommendations? Kim Nicholas RV9A Seattle (trying to keep up with Andy....) From http://www.lycoming.textron.com/main.jsp?bodyPage=support/publications/keyReprints/operation/moreCylinderHeadTemp.html In Lycoming engines, all cylinders are drilled to accommodate a CHT bayonet type thermocouple. Some operators in the field have been using a spark plug gasket-type installation in order to get cylinder head temperature readings. Textron Lycoming Engineering does not currently approve this method of determining CHT. Not only is the method less accurate than the recommended thermocouple type, but the temperature readings differ noticeably from the approved installations. Dave Toy In the "thinking of building stage" ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: RV7 floor stiffeners, ATC fuse holders
Date: Oct 29, 2002
Amit, The main problem area on the RV-6 was the double row of rivets in the area of the spar. That was eventually changed from 3/32" to 1/8" rivets and dimpled skin/c-sunk under skin and spar. I think many problems were also due to the fact that a lot of people didn't attach the stiffeners to the spar or firewall or both (a result of really poorly drawn plans that don't clearly show those attachments). Assuming they are properly tied in fore and aft, the size rivets used on the stiffeners probably isn't as critical, but on the other hand why NOT use 1/8" rivets? Anyway I did. Randall Henderson, RV-6 N6R (~400 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
Date: Oct 29, 2002
From: John Allen <fliier(at)yahoo.com>
Subject: RV6A Airspeeds
In my RV-6A with a 160hp O-320 and a fixed pitch Sensenich I get between 155-160 kts true airspeed, depending on (density) altitude. That is with gear leg and intersection fairings and the old style wheelpants. Static RPM is about 2150. The prop typically maxes out at 2600 RPM below 5,000', and gets slower as altitude increases. John Allen --------------------------------- HotJobs - Search new jobs daily now ________________________________________________________________________________
Date: Jan 01, 2000
Subject: Re: Ya Gotta Wonder
From: lm4(at)juno.com
Thanks Austin Larry Mac Donald > >From: "Austin" <6430(at)axion.net> > >Hi listers, you rivet pounding ground bound bunch of > dreamers,...with due respect, Yes, you do gotta wonder what kind of a world you enter when you get the old bird flying ________________________________________________________________________________
From: "David Carter" <dcarter(at)datarecall.net>
Subject: Rate of climb - flt test (was RV-6A airspeed problem)
Date: Oct 29, 2002
> One more note - VSIs can have errors too, so when doing climb tests > you need to use a stop watch against the altimeter to get the data, > and then correct for temperature. -- > Kevin Horton RV-8 (cowling, wing tip lights) > Ottawa, Canada > http://members.rogers.com/khorton/rv8.html Here's another facet of this "rate of climb" and "change of altitude" thing: If you are flying on a standard day, i.e., with standard temperature at the surface, std temp lapse rate (i.e., std temp at every altitude above MSL) , and std pressure laps rate, then when the altimeter goes from, e.g., 1000' to 2000', then you have indeed climbed 1000' (as would be meaured with a 1000' surveyor's chain hung from a helicopter, for example) If it is hot summer, then none of the temperatures, temp lapse rate, & pressure lapse rates are standard - as you time a 1000' 'pressure altitude' change, you are not timing a "real altitude" change - because the atmosphere has expanded about 10%, for example. If it is expanded 10%, then a 1000' change in pressure altitude is really a change of 1100' "real" altitude (change in MSL). My fighter squadron used to us a "D value chart" and get the winter time shrinkage factors and summer time expansion factors for the atmosphere in the altitude range we were using for dive bombing - we then adjusted our manual dive bombing release altitudes so as to avoid releasing too low in cold Wisconsin winters and releasing too high in hot anywhere summers. We'd call Offutt weather every day and get the height of the 850mb level (about 4500' on a std day) - given that and the bombing range's altimeter setting, we used a special chart and plotted a line from sfc to 4500' or so. It sloped left in winter and right in summer (was straight up on a std day in Spring & Fall). We had to adjust our release altitudes up to 300' in winter and 200 to 300' in summer to avoid serious bomb impact errors. "D value" is just D for "delta" or "difference" - the delta or difference of actual altitude vs indicated altitude. Rather than try to teach everyone in the home built flight testing community about D values, I suggest you use the GPS altitude readout. GPS altitude is independent of pressure altitude - it is the actual altitude above the theoretical/calculated location of the earth's surface - as close to true MSL" as you are going to get. - On a slightly different note - flying in mountainous terrain instead of flight testing - all instrument pilots have heard the warning, "flying from high pressure to low, look out below" - as there can be up to a 2000 foot difference (d value) between your indicated altitude (pressure altitude, what you read on the altimeter with a surface altimeter setting dialed in) and your actual altitude (tops of mountains are at "actual altitudes" or "MSL altitudes", not pressure altitudes or indicated altitudes). - Now, with GPS, and if you program your display or select the correct "page" to display, you can see your "actual" or "MSL" altitude, as measured by the GPS system. So, just as you can use GPS altitude (as close to true or MSL altitude as you can get) to avoid mountains, so you can also measure "change in MSL altitude" (change in true altitude) by using the GPS instead of the altimeter when flight testing for rate of climb in hot and cold non-standard days. David Carter ________________________________________________________________________________
From: "Rick Galati" <rick07x(at)earthlink.net>
Subject: Oil Access Door
Date: Oct 29, 2002
After considering many options, I have decided that I would like to spring load the oil access door on my RV-6A upper cowl and hinge it from the bottom (as opposed to the top of the cowl per drawing) and swing it down and inward into the engine compartment. I have the Type S cowl which already has the oil access cutout area already defined on it. Since I have not yet hung the engine yet which will be an 0-320-D1A on order, I am wondering if I am opening up to myself possible conflicts with the engine mount or oil filler neck or any other obstruction by swinging the door inward. Without an engine in place, it is difficult for me to envision possible conflicts. Can I go ahead and do this subassembly work now and get it over with or should I wait? Any thoughts? --- Rick Galati --- rick07x(at)earthlink.net --- EarthLink: It's your Internet. ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Oil Access Door
Date: Oct 29, 2002
>After considering many options, I have decided that I would like to spring >load the oil access door on my RV-6A upper cowl and hinge it from the >bottom (as opposed to the top of the cowl per drawing) and swing it down >and inward into the engine compartment. I have the Type S cowl which >already has >the oil access cutout area already defined on it. Since I have not yet >hung the engine yet which will be an 0-320-D1A on order, I am wondering if >I am opening up to myself possible conflicts with the engine mount or oil >filler >neck or any other obstruction by swinging the door inward. Without an >engine in place, it is difficult for me to envision possible conflicts. >Can I go ahead and do this subassembly work now and get it over with or >should I >wait? Any thoughts? > > >--- Rick Galati > Will it be latched down in some way so you can still get your arm in there to reach the firewall/cowl hinge pins? Otherwise, that door will be grabbing at your arm the whole time. Get the firewall forward installation done, then check your ergonomics and clearances. Brian Denk RV8 N94BD 310 hrs. http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
From: "Bill VonDane" <n8wv(at)hotmail.com>
Subject: Exxon Elite
Date: Oct 29, 2002
What are the ramifications of switching from Aeroshell 20W-50 to Exxon Elite 20W-50? What other oils are "OK" for use in a Lycosaur? What about automotive synthetic blends? -Bill VonDane RV-8A ~ 74 hours www.vondane.com ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Oct 29, 2002
Subject: TFR solutions
Maybe if the FAA would give more advance notice with some means of identifying boundries for VFR guys. Some of the TFR's have not even had NOTAMS. How can we be expected to comply? Maybe some semi perment TFR's could be placed on Sectionals with times of use in the map cover like MOA's. The real solution lies in getting back to normal, small aircraft Simply do not represent a real and present danger to national security (no way--no how---simply, competely rediculous). Yeah, I suppose some evil genious could put a suitcase nuke in an RV4 (but that is what we have James Bond 007 for) and fly it to a stadium full of people but is that a realistic threat, wouldn't it be easier to just put the nuke in a Yugo and drive it to the target? The whole problem with this TFR thing is that it is an extreme over reaction. Maybe transponder codes on large aircraft could be tracked--they are the ones that need to be kept at a distance from "targets" not our bug smashers. I also fear that eventually someone will get trigger happy and shoot a family down, that is a whole lot more likely than terrorists using a C150 to attack a nucleor reactor. Our military guys and equipment probably also have better things to do than intercept ultralights. We know who the bad guys are, let's go get them and leave our freedoms intact. We might start with asking the Malvo's of the world to please leave our country--NOW. Does anyone remember the Boston Tea Party, it has implications here. Do Not Archive. JR ________________________________________________________________________________
From: "Rick Galati" <rick07x(at)earthlink.net>
Subject: Re:Oil Access Door
Date: Oct 29, 2002
Good point Brian. I should have mentioned that I have already made plans for and have partially installed a doubler strap to accommodate floating nut plates and screws in lieu of the piano hinge option for the curved portion of the upper cowl/firewall attach. So accessing hinge pins is not a concern. --- Rick Galati --- rick07x(at)earthlink.net --- EarthLink: It's your Internet. ________________________________________________________________________________
Date: Oct 29, 2002
From: KAKlewin(at)aol.com
Subject: Freebie...First Come...
Howdy... If anyone is looking for a Nomex flight suit..I have one to give away....I was issued it by the Air Force a few months ago and realized it was too small. It is the tan desert flight suit (not the standard green one). It is a size 40 Short...Im 5'9" and its about an inch too short for me...so would fit someone about 5'8" or smaller and normal build. Only put it on once to find out it wasn't going to work. Im currently serving in the middle east, but the first one that replies (off list please) who this could work for drop me a note. I have access to US post, but it takes about 10 days to get it to you..sometimes a few days longer. I would ask for about $10 to cover the shipping. Let me know if you are interested. Thanks.. Kurt Klewin RV6A Finishing Maj, USAFR, Incirlik AB, TU ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Oil Access Door
Date: Oct 29, 2002
Might make the oil filler oil a little low because the door has to clear. This will make it hard to see the filler hole in poor lighting and more difficult to insert the oil spout without dumping oil all over the place. I'd vote no! 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: "Rick Galati" <rick07x(at)earthlink.net> Subject: RV-List: Oil Access Door > > > After considering many options, I have decided that I would like to spring > load the oil access door on my RV-6A upper cowl and hinge it from the > bottom (as opposed to the top of the cowl per drawing) and swing it down > and inward into the engine compartment. I have the Type S cowl which already has > the oil access cutout area already defined on it. Since I have not yet > hung the engine yet which will be an 0-320-D1A on order, I am wondering if > I am opening up to myself possible conflicts with the engine mount or oil filler > neck or any other obstruction by swinging the door inward. Without an > engine in place, it is difficult for me to envision possible conflicts. > Can I go ahead and do this subassembly work now and get it over with or should I > wait? Any thoughts? > > > --- Rick Galati > > --- rick07x(at)earthlink.net > > --- EarthLink: It's your Internet. > > ________________________________________________________________________________
Date: Oct 29, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Rate of climb - flt test (was RV-6A airspeed
problem) > > >> One more note - VSIs can have errors too, so when doing climb tests >> you need to use a stop watch against the altimeter to get the data, >> and then correct for temperature. -- >> Kevin Horton RV-8 (cowling, wing tip lights) >> Ottawa, Canada > > http://members.rogers.com/khorton/rv8.html > > >Rather than try to teach everyone in the home built flight testing community >about D values, I suggest you use the GPS altitude readout. GPS altitude is >independent of pressure altitude - it is the actual altitude above the >theoretical/calculated location of the earth's surface - as close to true >MSL" as you are going to get. > - On a slightly different note - flying in mountainous terrain instead >of flight testing - all instrument pilots have heard the warning, "flying >from high pressure to low, look out below" - as there can be up to a 2000 >foot difference (d value) between your indicated altitude (pressure >altitude, what you read on the altimeter with a surface altimeter setting >dialed in) and your actual altitude (tops of mountains are at "actual >altitudes" or "MSL altitudes", not pressure altitudes or indicated >altitudes). > - Now, with GPS, and if you program your display or select the correct >"page" to display, you can see your "actual" or "MSL" altitude, as measured >by the GPS system. > >So, just as you can use GPS altitude (as close to true or MSL altitude as >you can get) to avoid mountains, so you can also measure "change in MSL >altitude" (change in true altitude) by using the GPS instead of the >altimeter when flight testing for rate of climb in hot and cold non-standard >days. > >David Carter David is correct that GPS altitude is probably more accurate than barometric altitude most of the time, if we are more than a few thousand feet above the location where the altimeter setting came from. If our altitude is close to the site where the altimeter setting came from, the altimeter is likely more accurate than the GPS. I'm not sure I would agree with the suggestion to time the GPS altitude change instead of timing the barometric altitude change though. In my experience, GPS altitude fluctuates quite a bit, so I'm not sure that timing the rate of change of GPS altitude will lead to an accurate result. GPS is much less accurate vertically than it is horizontally. I believe that we can get more accurate results by timing the rate of barometric altitude change, and then correcting for non-standard temperature. Take care, -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
Date: Oct 29, 2002
From: Brian Huffaker <bifft(at)xmission.com>
Subject: Re: Rate of climb - flt test (was RV-6A airspeed problem)
version=2.43 On Tue, 29 Oct 2002, David Carter wrote: > Rather than try to teach everyone in the home built flight testing community > about D values, I suggest you use the GPS altitude readout. GPS altitude is > independent of pressure altitude - it is the actual altitude above the > theoretical/calculated location of the earth's surface - as close to true > MSL" as you are going to get. > - On a slightly different note - flying in mountainous terrain instead > of flight testing - all instrument pilots have heard the warning, "flying > from high pressure to low, look out below" - as there can be up to a 2000 > foot difference (d value) between your indicated altitude (pressure > altitude, what you read on the altimeter with a surface altimeter setting > dialed in) and your actual altitude (tops of mountains are at "actual > altitudes" or "MSL altitudes", not pressure altitudes or indicated > altitudes). > - Now, with GPS, and if you program your display or select the correct > "page" to display, you can see your "actual" or "MSL" altitude, as measured > by the GPS system. > Are GPS's that accurate? I haven't used one in the plane much, but I had a hiking model that I played with a bit before leaving in a canyon somewhere in southern utah :(. It would show a difference of about 1000' or so just sitting at the kitchen table. Comparing altitude with topo maps showed similar errors. The rate of change for the error would be fairly slow, so useable for rate measurements, but I wouldn't want to try to avoid mountains based on it. (Another excuse just to fly VFR around here). Brian Huffaker, DSWL (bifft(at)xmission.com) RV-8A 80091 Delayed by another project. 1/4 Starduster II N23UT flying ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: Exxon Elite
Date: Oct 29, 2002
Dear Bill, Do you mean Aeroshell 15W-50 (Phillips-XC has 20W-50), versus the Exxon Elite 20W-50? *Should be O.K., if you are going from an oil with high detergent to an oil with a lower detergent content, but not the other way around, as it could loosen up crud that might travel into the oil galleries and block of some (or all) of the oil flow. *DO use one of the major brands (Aeroshell / Phillips / Exxon), Single- or Multi Viscosity is up to you. I'd go the modern Multi Viscosity Route (costs a little more, but then, how much did my new engine cost?) *DO NOT use Automotive oil of any kind. Please check in the Archives AS TO WHY NOT, or talk to Doug Rozendaal (spelling?) about his opinion on the subject. He really is an Expert on it, that actually earns a living with it!! Good Luck on your Quest! Sincerely, Konrad Werner ABQ-NM Subject: RV-List: Exxon Elite > > What are the ramifications of switching from Aeroshell 20W-50 to Exxon Elite 20W-50? > > What other oils are "OK" for use in a Lycosaur? What about automotive synthetic blends? > > -Bill VonDane > RV-8A ~ 74 hours > www.vondane.com > > ________________________________________________________________________________
From: "Marcus Ward" <marcus@f-64.org>
Subject: Re: TFR solutions
Date: Oct 29, 2002
We should dump tea into TFRs? Maybe we should dress up as Mohawks and violate TFRs. In 1773, Britain's East India Company was sitting on large stocks of tea that it could not sell in England. It was on the verge of bankruptcy. In an effort to save it, the government passed the Tea Act of 1773, which gave the company the right to export its merchandise directly to the colonies without paying any of the regular taxes that were imposed on the colonial merchants, who had traditionally served as the middlemen in such transactions. With these privileges, the company could undersell American merchants and monopolize the colonial tea trade. The act proved inflammatory for several reasons. First, it angered influential colonial merchants, who feared being replaced and bankrupted by a powerful monopoly. The East India Company's decision to grant franchises to certain American merchants for the sale of their tea created further resentments among those excluded from this lucrative trade. More important, however, the Tea Act revived American passions about the issue of taxation without representation. The law provided no new tax on tea. Lord North assumed that most colonists would welcome the new law because it would reduce the price of tea to consumers by removing the middlemen. But the colonists responded by boycotting tea. Unlike earlier protests, this boycott mobilized large segments of the population. It also helped link the colonies together in a common experience of mass popular protest. Particularly important to the movement were the activities of colonial women, who were one of the principal consumers of tea and now became the leaders of the effort to the boycott. Various colonies made plans to prevent the East India Company from landing its cargoes in colonial ports. In ports other than Boston, agents of the company were "persuaded" to resign, and new shipments of tea were either returned to England or warehoused. In Boston, the agents refused to resign and, with the support of the royal governor, preparations were made to land incoming cargoes regardless of opposition. After failing to turn back the three ships in the harbor, local patriots led by Samuel Adams staged a spectacular drama. On the evening of December 16, 1773, three companies of fifty men each, masquerading as Mohawk Indians, passed through a tremendous crowd of spectators, went aboard the three ships, broke open the tea chests, and heaved them into the harbor.As the electrifying news of the Boston "tea party" spread, other seaports followed the example and staged similar acts of resistance of their own.' ----- Original Message ----- From: <JRWillJR(at)aol.com> Subject: RV-List: TFR solutions > > Maybe if the FAA would give more advance notice with some means of > identifying boundries for VFR guys. Some of the TFR's have not even had > NOTAMS. How can we be expected to comply? Maybe some semi perment TFR's could > be placed on Sectionals with times of use in the map cover like MOA's. The > real solution lies in getting back to normal, small aircraft Simply do not > represent a real and present danger to national security (no way--no > how---simply, competely rediculous). Yeah, I suppose some evil genious could > put a suitcase nuke in an RV4 (but that is what we have James Bond 007 for) > and fly it to a stadium full of people but is that a realistic threat, > wouldn't it be easier to just put the nuke in a Yugo and drive it to the > target? The whole problem with this TFR thing is that it is an extreme over > reaction. Maybe transponder codes on large aircraft could be tracked--they > are the ones that need to be kept at a distance from "targets" not our bug > smashers. I also fear that eventually someone will get trigger happy and > shoot a family down, that is a whole lot more likely than terrorists using a > C150 to attack a nucleor reactor. Our military guys and equipment probably > also have better things to do than intercept ultralights. We know who the bad > guys are, let's go get them and leave our freedoms intact. We might start > with asking the Malvo's of the world to please leave our country--NOW. Does > anyone remember the Boston Tea Party, it has implications here. Do Not > Archive. JR > > ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: RV-6A airspeed update
Date: Oct 29, 2002
Ok. I did some more concrete tests today. Here is what I came up with: 2 methods. 3 way and 4 way track for the GPS. Both came up with 154 KTS Groundspeed. Not as bad as I had thought, but still about 10 Kts low. Here is the data on the engine performance: 8000' 22.7"MAP 2600 RPM 8.2GPH I suspect there are a few possible drag sources here. Perhaps the baffles. Haven't checked to see how tight they are. Also, he has the Team Rocket wheel pants. Don't know any performance differences than Van's wheel pants. He had a pretty heavy wing, and had to do considerable blocking and squeezing of the ailerons to make them level. One aileron is up a little, and one is down a little. I imagine there could be a seperate RV-List for the different theories on speed enhancement of RV's. Too many variables to know off hand. Either way, he has a 177 MPH RV-6A. I'd like to see closer to 185 or so, but not too far off. Thanks for all the advice, 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 ________________________________________________________________________________
From: "David Carter" <dcarter(at)datarecall.net>
Subject: Re: Rate of climb - flt test (was RV-6A airspeed problem)
Date: Oct 29, 2002
Kevin's observation about GPS being less accurate in the vertical than horizontal is good info. I have never noticed it vary while I was at a constant barometric altitude - but wasn't really looking for that, either. I'll keep a closer watch. Might be "an individual" thing, or a "day to day" thing - maybe depends on relative position to satellites, etc? Maybe the "iffy-ness" will go away when FAA gets off its hindside and implements WAAS so we get really accurate info. Meanwhile, might be useful and informative to note both baro altitude change and GPS altitude change, just to see if they correlate, given that you are flying on a cold or hot day and know what to expect (less altitude change on GPS than Baro in winter, more altitude change than Baro in summer). Anyone wanting a "D Value Chart" e-mail me privately and I'll go dig one out of my USAF archive boxes in the attic. Two refinements on my original post: 1) "We called the wx man. . ." - now you can access the balloon sounding data on the internet and look up the height of the 850mb level yourself; 2) I wasn't precise in saying what you plot: You plot "height (msl altitude) of the 850 mb level" - it rises above std in summer, sinks below in winter. Once plotted, the special D Value chart makes it easy to get the error (d value) to apply to baro altitude anywhere between sfc and the "approx" 4500' level. David ----- Original Message ----- From: "Kevin Horton" <khorto1537(at)rogers.com> Subject: Re: RV-List: Rate of climb - flt test (was RV-6A airspeed problem) > > > > > > >> One more note - VSIs can have errors too, so when doing climb tests > >> you need to use a stop watch against the altimeter to get the data, > >> and then correct for temperature. -- > >> Kevin Horton RV-8 (cowling, wing tip lights) > >> Ottawa, Canada > > > http://members.rogers.com/khorton/rv8.html > > > > > >Rather than try to teach everyone in the home built flight testing community > >about D values, I suggest you use the GPS altitude readout. GPS altitude is > >independent of pressure altitude - it is the actual altitude above the > >theoretical/calculated location of the earth's surface - as close to true > >MSL" as you are going to get. > > - On a slightly different note - flying in mountainous terrain instead > >of flight testing - all instrument pilots have heard the warning, "flying > >from high pressure to low, look out below" - as there can be up to a 2000 > >foot difference (d value) between your indicated altitude (pressure > >altitude, what you read on the altimeter with a surface altimeter setting > >dialed in) and your actual altitude (tops of mountains are at "actual > >altitudes" or "MSL altitudes", not pressure altitudes or indicated > >altitudes). > > - Now, with GPS, and if you program your display or select the correct > >"page" to display, you can see your "actual" or "MSL" altitude, as measured > >by the GPS system. > > > >So, just as you can use GPS altitude (as close to true or MSL altitude as > >you can get) to avoid mountains, so you can also measure "change in MSL > >altitude" (change in true altitude) by using the GPS instead of the > >altimeter when flight testing for rate of climb in hot and cold non-standard > >days. > > > >David Carter > > David is correct that GPS altitude is probably more accurate than > barometric altitude most of the time, if we are more than a few > thousand feet above the location where the altimeter setting came > from. If our altitude is close to the site where the altimeter > setting came from, the altimeter is likely more accurate than the GPS. > > I'm not sure I would agree with the suggestion to time the GPS > altitude change instead of timing the barometric altitude change > though. In my experience, GPS altitude fluctuates quite a bit, so > I'm not sure that timing the rate of change of GPS altitude will lead > to an accurate result. GPS is much less accurate vertically than it > is horizontally. I believe that we can get more accurate results by > timing the rate of barometric altitude change, and then correcting > for non-standard temperature. > > Take care, > -- > Kevin Horton RV-8 (cowling, wing tip lights) > Ottawa, Canada > http://members.rogers.com/khorton/rv8.html > > ________________________________________________________________________________
Date: Oct 29, 2002
From: Louis Willig <larywil(at)comcast.net>
Subject: Re: Exxon Elite
> >What are the ramifications of switching from Aeroshell 20W-50 to Exxon >Elite 20W-50? > >What other oils are "OK" for use in a Lycosaur? What about automotive >synthetic blends? Bill, Don't even think about using automotive oils in your Lycoming. Period. Aircraft engines are designed to consume oil when they run. Aircraft oils are formulated to be consumed and leave a residue that is relatively harmless. Automotive oil residue (whether natural or synthetic oil) will leave harmful residues and will kill you or you wallet. Did I say that gently enough? Now, the question about Exxon Elite vs. Aeroshell 20W-50 was asked about a year ago. I think my answer then was a safe one. "No one really knows." There is not a great deal of history with the Elite. I have been using Elite for over 200 hours. I used the Aeroshell 20W-50 prior to that. I see no difference whatsoever. Why? Because it would take a few thousand hours to see a statistically significant difference. My RV-4 flies about twice per week. Most other aircraft fly a lot less. I'll bet that the frequency of flying has a lot more to do with engine health and performance than does the type of oil. Both of the oils you asked about are considered great products, and both are premium priced. But the cost of oil is insignificant over the life of an engine. You will probably spend $1000 over a 2000 hour engine life for premium oil. Cheap aero oils will still cost $500 for that same period.....If they even let you get to that TBO. Both the Elite and the A/S 20W-50 are promoted as appropriate for engines that fly only occasionally. Neither has any known faults (so far). Both are great oils and Exxon told me they can be mixed if need be with no problem. Keep truckin' Louis ________________________________________________________________________________
Date: Oct 29, 2002
Subject: Re: RV7 floor stiffeners, ATC fuse holders
From: Michael D Hilger <rvsixer(at)juno.com>
writes: > > Listers, > In the past (looked it up in the archives) there were many cases of > smoking rivets in the forward floor area, the ones that hold the > floor to the firewall and stiffeners. > It was attributed to the engine vibrations, and several methods of > stiffening the area even more were raised, including using more > rivets, larger (1/8") rivets, both, more stiffeners, double floor > boards etc. > In the RV7, I am not sure that this issue has been adressed, as one > still needs to use 3/32" rivets, same number of stiffeners etc. I DO > see that the rivet spacing is ~1" and not 1.25", and that there is a > double floor in the center of the cabin (between the two inboard > stiffeners). That double floor in the RV-7 should help with a problem I had. On my -6, on takeoff as I accelerated through about 110 mph in the climb I would hear a "pop" and the exhaust note would change slightly. After landing I would hear another "pop". It turned out the bottom fwd skin was oil canning in about 10" fwd of the main spar. The change from flat at the firewall to curved at the spar created the problem. I made a stiffener and installed it between the inboard stiffeners, attaching it to those stiffeners. Fixed the problem. Mike Hilger RV-6, N207AM, 320 hrs Sign Up for Juno Platinum Internet Access Today Only $9.95 per month! Visit www.juno.com ________________________________________________________________________________
Date: Oct 29, 2002
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: vacuum system help
I've finally adjusted the vacuum regulator so that the suction needle sits in the middle of the green band at cruise power settings. But the regulator doesn't seem to be regulating-I get one-to-two inches of vacuum on the ground at runup and on the peg at eight inches during full power. One person told me these "Y" style regulators can be rebuilt and another told me they couldn't. A Forum search didn't reveal any information. Any ideas? Scott in Vancouver 40hrs, -6 ________________________________________________________________________________
Date: Oct 29, 2002
From: Laird Owens <owens(at)aerovironment.com>
Subject: Re: RV-6A airspeed update
Paul, Just to flog this a little more, were you taking into account OAT? When your saying 8000' was that pressure altitude, or density altitude? If it was hot and your flying at 8000' pressure altitude, your density altitude (the altitude at which your airplane/engine really thinks it's at) could be much higher, and the engine not putting out 75% power. When I do all my performance testing, I always fly at the density altitude which I'm trying to get the data. That way I can fly repeat tests the same way and be pretty sure I have close to the same power I had on the previous day. The other thing to think about is repeating the test several times on different days to average out the possible differences in air mass movement. If you happened to flying in slightly decending air, your groundspeeds would show low. I always fly at least 4 tests before I start to see a trend and believe the data. You wouldn't believe how hard it is to get GOOD data. Any data is easy, good data is much tougher. Have fun. Laird RV-6 630hrs SoCal > >Ok. I did some more concrete tests today. Here is what I came up with: > >2 methods. 3 way and 4 way track for the GPS. > >Both came up with 154 KTS Groundspeed. Not as bad as I had thought, >but still about 10 Kts low. > >Here is the data on the engine performance: > >8000' 22.7"MAP 2600 RPM 8.2GPH > >I suspect there are a few possible drag sources here. Perhaps the >baffles. Haven't checked to see how tight they are. Also, he has >the Team Rocket wheel pants. Don't know any performance differences >than Van's wheel pants. He had a pretty heavy wing, and had to do >considerable blocking and squeezing of the ailerons to make them >level. One aileron is up a little, and one is down a little. > >I imagine there could be a seperate RV-List for the different >theories on speed enhancement of RV's. Too many variables to know >off hand. Either way, he has a 177 MPH RV-6A. I'd like to see >closer to 185 or so, but not too far off. > >Thanks for all the advice, > >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 > > ________________________________________________________________________________
From: "Jim Sears" <sears(at)searnet.com>
Subject: Fw: RE: RV9-List: Drill and dimple vs just dimple (was:New Builder
introduction)
Date: Oct 29, 2002
I got this from Scott McDaniels, today. I know it's more of the same; but, it's nice to have a comment from an employee of Van's. I'll make a couple of comments below; but, it's good reading material for those of you who are interested in this thread and wanted an opinion from the source. > Hi Jim, I was cruising the archives of the RV list and saw your post. > I am responding to you directly because I am not a current subscriber of > the RV-list. > > The current construction manual does not say you don't have to drill. If > you read the manual for the kit you are helping your friend with I think > you will find just the opposite. Driving dimple dies through the > prepunch holes (even if you deburr first) is a very bad idea. I'm sure > you have noticed that the dimple die pilot doesn't fit in the undersized > hole. That means when you drive it home it is stretching the material to > make the hole larger (high probability of cracking) and the other problem > is that without final sizing the hole with a drill you are leaving the > ragged interior of the hole which would normally get removed by the > drilling process. This means that all of the hole interiors have a > surface finish similar to what the outer skin edges have before they have > been smoothed/deburred (more potential for cracks). > > I assure you that if we at Van's felt it an acceptable practice to just > dimple and then rivet the prepunched skins as supplied, we would punch > the holes to full size, and we would suggest it in the construction > manual. > > Please reconsider using the non drilling process, and pass the word to > other builders who may not be considering all of the issues related to > doing so. > > Give me a call at work if you need more info. > > Scott McDaniels > Scott used to be a subscriber; but, he got off some time ago. Actually, Van should have someone checking the list every day to catch things like this thread. It would sure help iron out some of our questions and would also help them correct problems. I know I've seen some problems that were still active five years after I reported them to Van's. Not good. You folks know that Van did advertise, or reported in the RVator, that they built the wings without ever picking up a drill. Well, folks, that tells me it's OK to do that if they don't say it's not when they advertise it that way. Maybe they did; but, I don't ever remember their doing it. Granted, the manual says to match drill; but, that's most likely told in the first few sections that a second time builder is not even going to look at. In fact, I'm betting a second, or more, timer is most likely going to just use the drawings to get started without ever looking at the manual. I'm just using the manual on the -9A to make sure I don't leave any parts out. That's it. We just got the finishing kit, today; and, we're ready for it. As for the dimple set's going through the hole, this is not a forced fit. It almost drops through the hole. I can push it in with very little pressure. As I said, I could tell no difference between holes/dimples I'd match drilled and ones I hadn't. I was using my sense of touch for the test, though. Maybe they have a better sense of touch than I do? Sure, I know they've probably done some testing; but, I can say I've never seen the skins crack on any RV, etc. As for my friend's RV-9A, it's a quick build that has left much of the building to Van's. We have done very little of the drilling and dimpling. With that, I'm not worried about what dimpling we've done without match drilling. As I said, another friend's RV-7A was built with no match drilling. I don't think he's going to ground his airplane and redo all of the rivet holes. He's going flying as soon as he's sure he's ready for the lift off. I'm expecting it at any time. I appreciate Scott's input on the subject and have passed it along to you. However, we got some good input on both sides of the discussion with documentation to back up each side. As for me, I'm not sure what I'll do on my next project. I may match drill. I may not. There is obviously good support for each method. You chose the method that gives you the warmest fuzzy. This is important enough to archive, I think. Jim Sears in KY RV-6A N198JS EAA Tech Counselor ________________________________________________________________________________
Date: Oct 29, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Rate of climb - flt test (was RV-6A airspeed
problem) > >Kevin's observation about GPS being less accurate in the vertical than >horizontal is good info. I have never noticed it vary while I was at a >constant barometric altitude - but wasn't really looking for that, either. >I'll keep a closer watch. > I've got a hand held Lowrance Air Map 100. I played with it quite a bit in our driveway when I was learning to use it. Usually it seemed to be fairly accurate on altitude. However, there was one occasion when I saw the altitude vary by about 600 ft over a period of less than a minute. I don't know how often such a variation could be expected to occur, as I stopped watching the altitude once I started flying with it. -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
Date: Oct 29, 2002
From: Gary & Carolyn Zilik <zilik(at)direcpc.com>
Subject: Re: Exxon Elite
None that I know of.. I use to run Aeroshell 15W-50 and have since switched to Phillips 20W-50. Price was my reason for switching. If bought in the gallon jugs the Phillips oil is only $1.87 qt. I dump two gallons in at oil change time and then 25 hours later drain the 6 remaining quarts out. Since I also change the filter at 25 hr intervals an oil change runs about 30 bucks. Some of the locals change the filter at 50 hr intervals and the oil at 25 hrs, just another way to save money. Gary Bill VonDane wrote: > > What are the ramifications of switching from Aeroshell 20W-50 to Exxon Elite 20W-50? > > What other oils are "OK" for use in a Lycosaur? What about automotive synthetic blends? > > -Bill VonDane > RV-8A ~ 74 hours > www.vondane.com > ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Date: Oct 29, 2002
Maybe it couldn't see the satellites from the kitchen table? Actually, an excellent article in an AOPA Air Safety Foundation publication about GPS says "...vertical accuracy is only about a sixth of its horizontal accuracy. When WAAS comes online, vertical accuracy will be greatly improved." In another place in the article, it says that horizontal accuracy with SA off (normal now) is 100 to 330 feet, so we are talking about vertical accuracy of maybe 600 to 1980 feet. Of course if it is consistently off by the same amount during the climb, the rate of climb numbers would be good. Terry Are GPS's that accurate? I haven't used one in the plane much, but I had a hiking model that I played with a bit before leaving in a canyon somewhere in southern utah :(. It would show a difference of about 1000' or so just sitting at the kitchen table. Comparing altitude with topo maps showed similar errors. The rate of change for the error would be fairly slow, so useable for rate measurements, but I wouldn't want to try to avoid mountains based on it. (Another excuse just to fly VFR around here). ________________________________________________________________________________
From: "Sally and George" <aeronut58(at)hotmail.com>
Subject: Re: Exxon Elite
Date: Oct 29, 2002
I know lots of guys change oil at 25 hour intervals, but my Lycoming manual says 50 hours with a full-flow filter. Any factual data, or is it all religious beliefs? George Kilishek N888GK ----- Original Message ----- From: Gary & Carolyn Zilik Subject: Re: RV-List: Exxon Elite None that I know of.. I use to run Aeroshell 15W-50 and have since switched to Phillips 20W-50. Price was my reason for switching. If bought in the gallon jugs the Phillips oil is only $1.87 qt. I dump two gallons in at oil change time and then 25 hours later drain the 6 remaining quarts out. Since I also change the filter at 25 hr intervals an oil change runs about 30 bucks. Some of the locals change the filter at 50 hr intervals and the oil at 25 hrs, just another way to save money. Gary Bill VonDane wrote: > > What are the ramifications of switching from Aeroshell 20W-50 to Exxon Elite 20W-50? > > What other oils are "OK" for use in a Lycosaur? What about automotive synthetic blends? > > -Bill VonDane > RV-8A ~ 74 hours > www.vondane.com > ________________________________________________________________________________
From: "Kyle Boatright" <kyle.boatright(at)adelphia.net>
Subject: Re: Oil Access Door
Date: Oct 29, 2002
You will have interference with the filler neck unless you really cut it short. If you cut it short, you'll make an even bigger mess when you go to add oil... Even with a long filler neck, I get a spill most of the time if I don't use a funnel... ----- Original Message ----- From: "Rick Galati" <rick07x(at)earthlink.net> Subject: RV-List: Oil Access Door > > > After considering many options, I have decided that I would like to spring > load the oil access door on my RV-6A upper cowl and hinge it from the > bottom (as opposed to the top of the cowl per drawing) and swing it down > and inward into the engine compartment. I have the Type S cowl which already has > the oil access cutout area already defined on it. Since I have not yet > hung the engine yet which will be an 0-320-D1A on order, I am wondering if > I am opening up to myself possible conflicts with the engine mount or oil filler > neck or any other obstruction by swinging the door inward. Without an > engine in place, it is difficult for me to envision possible conflicts. > Can I go ahead and do this subassembly work now and get it over with or should I > wait? Any thoughts? > > > --- Rick Galati ________________________________________________________________________________
From: "George McNutt" <gmcnutt(at)intergate.ca>
Subject: GPS Problem
Date: Oct 29, 2002
Anyone have avionics advice on the following, - it seems that my Comm radio is being picked up and re-radiated by the ELT which then shuts down the GPS. The Avionics Equipment installed is: - UPSAT SL60 GPS/COMM, Narco Nav 122D VOR/ILS, ACK E-01 ELT. Antennae locations are: - COMM on bottom under baggage compartment, ELT on top aft fuselage, GPS antennae just aft of the sliding canopy track and VOR/ILS cats whiskers on top of vertical stab. All antennae wires have good separation except the VOR and GPS. During initial installation tests of the GPS/COMM the ELT might not have been installed, the GPS/COMM tests went fine. Later, when I did practice ILS approaches at a local airport using tower frequency 121.0 I noticed that I would occasionally get a RAIM warning or a "unable to compute position" message. It finally dawned that I had a harmonic problem bothering the GPS, ground tests confirmed the problem. Disconnecting the ELT coax antennae at the ELT seemed to cure problem so I speculat that the ELT is picking up the COMM radio, then re-radiating the signal (harmonic) and bothering the GPS. The ELT manufacturer thought it might be the telephone cable to the remote switch but disconnecting that wire has no effect on the problem. I purchased a TED 4-70-54 notch filter yesterday and put it in the ELT antennae line at the ELT, ground testing seemed to indicate a major improvement but flight tests today confirm there is still a problem. My next plan is to try moving the notch filter around, should it be at the ELT antennae, COMM transmitter or? On the bright side - we had a clear sky with strong outflow winds today and the NavAid did a great job of tracking the localizer, 13 degrees of drift, and light turbulence, nice to see - keep pounding those rivets! George McNutt Langley B.C. 6-A ________________________________________________________________________________
From: "Randy Compton" <rdcompton(at)earthlink.net>
Subject: Refinishing wood props
Date: Oct 29, 2002
Dear fellow Listers: Anyone know of a shop that does good work, and in a fairly timely fashion, on refinishing a wood prop? The prop itself is in good shape mechanically, it's just starting to look a little...ok, maybe more than a little... worse for wear. Thanks, Randy Compton RV-3A N84VF Gulf Breeze, FL ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Fw: RE: RV9-List: Drill and dimple vs just dimple (was:New
Builder introduction) match drilling
Date: Oct 29, 2002
Hi Jim, Thank you for forwarding Scott's unsolicited informative email. Scott obviously sent it out of his concerns arising out of the recent emails in the archives. However it seems to me that the subject and tone of Scott's email might also have been meant to telegraph Vansaircraft's point of view all the while avoiding any direct contact etc. Legal circumstances etc.could be involved I suppose. His email sets it out well and clear enough for me: I quote; "Driving dimple dies through the pre-punch holes (even if you de-burr first) is a very bad idea". Scott then goes on to background that statement very clearly and concisely. Again I quote "Please reconsider using the non drilling process, and pass the word to other builders who may not be considering all of the issues related to doing so. It's clear to me that match drilling is firmly stated as a must step that is clearly indicated in the builder's instruction manual. In light of the fact that it is also an industry standard Scotts email should suffice to clear away any confusion created in the past by this at times confusing thread. Thank you for putting this information at the list's disposal. Happy building, Jim in Kelowna ----- Original Message ----- From: "Jim Sears" <sears(at)searnet.com> Subject: RV-List: Fw: RE: RV9-List: Drill and dimple vs just dimple (was:New Builder introduction) > > I got this from Scott McDaniels, today. I know it's more of the same; but, > it's nice to have a comment from an employee of Van's. I'll make a couple > of comments below; but, it's good reading material for those of you who are > interested in this thread and wanted an opinion from the source. > > > Hi Jim, I was cruising the archives of the RV list and saw your post. > > I am responding to you directly because I am not a current subscriber of > > the RV-list. > > > > The current construction manual does not say you don't have to drill. If > > you read the manual for the kit you are helping your friend with I think > > you will find just the opposite. Driving dimple dies through the > > prepunch holes (even if you deburr first) is a very bad idea . I'm sure > > you have noticed that the dimple die pilot doesn't fit in the undersized > > hole. That means when you drive it home it is stretching the material to > > make the hole larger (high probability of cracking) and the other problem > > is that without final sizing the hole with a drill you are leaving the > > ragged interior of the hole which would normally get removed by the > > drilling process. This means that all of the hole interiors have a > > surface finish similar to what the outer skin edges have before they have > > been smoothed/deburred (more potential for cracks). > > > > I assure you that if we at Van's felt it an acceptable practice to just > > dimple and then rivet the prepunched skins as supplied, we would punch > > the holes to full size, and we would suggest it in the construction > > manual. > > > > > > > > Give me a call at work if you need more info. > > > > Scott McDaniels > > > > Scott used to be a subscriber; but, he got off some time ago. Actually, Van > should have someone checking the list every day to catch things like this > thread. It would sure help iron out some of our questions and would also > help them correct problems. I know I've seen some problems that were still > active five years after I reported them to Van's. Not good. > > You folks know that Van did advertise, or reported in the RVator, that they > built the wings without ever picking up a drill. Well, folks, that tells me > it's OK to do that if they don't say it's not when they advertise it that > way. Maybe they did; but, I don't ever remember their doing it. Granted, > the manual says to match drill; but, that's most likely told in the first > few sections that a second time builder is not even going to look at. In > fact, I'm betting a second, or more, timer is most likely going to just use > the drawings to get started without ever looking at the manual. I'm just > using the manual on the -9A to make sure I don't leave any parts out. > That's it. We just got the finishing kit, today; and, we're ready for it. > > As for the dimple set's going through the hole, this is not a forced fit. > It almost drops through the hole. I can push it in with very little > pressure. As I said, I could tell no difference between holes/dimples I'd > match drilled and ones I hadn't. I was using my sense of touch for the > test, though. Maybe they have a better sense of touch than I do? Sure, I > know they've probably done some testing; but, I can say I've never seen the > skins crack on any RV, etc. > > As for my friend's RV-9A, it's a quick build that has left much of the > building to Van's. We have done very little of the drilling and dimpling. > With that, I'm not worried about what dimpling we've done without match > drilling. As I said, another friend's RV-7A was built with no match > drilling. I don't think he's going to ground his airplane and redo all of > the rivet holes. He's going flying as soon as he's sure he's ready for the > lift off. I'm expecting it at any time. > > I appreciate Scott's input on the subject and have passed it along to you. > However, we got some good input on both sides of the discussion with > documentation to back up each side. As for me, I'm not sure what I'll do on > my next project. I may match drill. I may not. There is obviously good > support for each method. You chose the method that gives you the warmest > fuzzy. > > This is important enough to archive, I think. > > Jim Sears in KY > RV-6A N198JS > EAA Tech Counselor > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Exxon Elite
Date: Oct 29, 2002
Hi George, The most accurate way to establish a user defined oil change interval is a series of lab analysis to establish a recommended average oil change frequency cycle. Most seem to settle for the less reliable thumb and finger and color test taken from the dip stick. Except in very extreme environmental cases, such as desert or arctic like conditions etc., it's doubtful that using Lycoming's standard guidelines will get you in any trouble. More frequent oil changes are optional. Jim in Kelowna ----- Original Message ----- From: "Sally and George" <aeronut58(at)hotmail.com> Subject: Re: RV-List: Exxon Elite > > I know lots of guys change oil at 25 hour intervals, but my Lycoming manual says 50 hours with a full-flow filter. > > Any factual data, or is it all religious beliefs? > > George Kilishek > N888GK > > ----- Original Message ----- > From: Gary & Carolyn Zilik > To: rv-list(at)matronics.com > Subject: Re: RV-List: Exxon Elite > > > None that I know of.. I use to run Aeroshell 15W-50 and have since switched to Phillips > 20W-50. Price was my reason for switching. If bought in the gallon jugs the Phillips oil is > only $1.87 qt. I dump two gallons in at oil change time and then 25 hours later drain the 6 > remaining quarts out. Since I also change the filter at 25 hr intervals an oil change runs > about 30 bucks. Some of the locals change the filter at 50 hr intervals and the oil at 25 > hrs, just another way to save money. > > Gary > > > Bill VonDane wrote: > > > > > What are the ramifications of switching from Aeroshell 20W-50 to Exxon Elite 20W-50? > > > > What other oils are "OK" for use in a Lycosaur? What about automotive synthetic blends? > > > > -Bill VonDane > > RV-8A ~ 74 hours > > www.vondane.com > > > > ________________________________________________________________________________
From: "Richard Sipp" <rsipp(at)earthlink.net>
Subject: Re: . and engine horsepower mods.
Date: Oct 29, 2002
To muddy the modification discussion waters further: I have just recieved Revision 7 (Oct 02) to the Hartzell Propeller Owner's Manual. Page 1-4 Par 3 (Airframe or Engine Modifications) contains a discussion regarding modifications. This full page is essentially a discussion of how propellers are tested with individual airframe and engine combinations to determine vibration characteristics prior to certification. It goes on to caution that airframe or engine modifications must be approved by the propeller manufacturer before being used on the aircraft. Among the sighted engine modifications are: "increased compression ratio, increased rpm, altered ignition timing, electronic ignition, full authority digital electronic controls (fadec), or tuned induction or exhaust." It is interesting that Unison gained approval for electronically controlled ignition on numerous certified applications while Hartzell says the modification must be appoved by them. It seems clear that Hartzell is going to some lengths to protect themselves and therefor must have some concerns. Hmmmm. Certainly, with our experimental certification, we are free to make these modifications, but as others have said the laws of physics still apply. There are, no doubt, a substantial number of RV and other experimentals using engines modified to one degree or another. So far, separated propeller blades do not seem to be raining down from the sky. The RV accident in Australia is the only recent one I have heard of. It seems the difficult question, without specific testing, is which modifications decrease vibration margins and which do not have a detremental or even positive effect. Dick Sipp RV4 N250DS ________________________________________________________________________________
From: "Richard Sipp" <rsipp(at)earthlink.net>
Subject: Re: Exxon Elite
Date: Oct 29, 2002
The last two issues of The Aviation Consumer compared the major aviation oil products for both wear and corrosion protection characteristics. Bottom line, Exon Elite and Shell multi-grade semi-synthetics were rated best and nearly equal. They gave a slight edge to the Shell product. Aviation Consumer cautioned against never using automotive oils in an aircraft engine. Exon responed questioning the validity of the test methods used. Dick Sipp RV4 N250DS ________________________________________________________________________________
From: "Ed Bundy" <ebundy(at)velocitus.net>
Subject: Re: vacuum system help
Date: Oct 29, 2002
It sounds like a bad regulator. I know the Rapco "Y" style regulators can't be rebuilt. I bought the Rapco kit that included the whole system and it worked fine when I installed it. The next flight it read really low. So I adjusted the regulator until it was back in the green again. The next flight it read really high. I finally got tired of playing with it and called Rapco. They said they thought the regulator was probably the culprit and sent me another one the next day. It worked great and has worked great ever since. I asked them if they wanted me to send the old one back and they told me to just destroy it (so it wouldn't accidentally end up on another airplane) because it was non-rebuildable. Mine reads 4.5" at idle and just a smidge over 5" at full throttle. It's just slightly under 5" at cruise. Ed Bundy RV6A 500+ hours Boise, ID > I've finally adjusted the vacuum regulator so that the suction needle sits in the middle of the green band at cruise power settings. But the regulator doesn't seem to be regulating-I get one-to-two inches of vacuum on the ground at runup and on the peg at eight inches during full power. > One person told me these "Y" style regulators can be rebuilt and another told me they couldn't. A Forum search didn't reveal any information. > Any ideas? > Scott in Vancouver ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: RV7 floor stiffeners, ATC fuse holders
Date: Oct 29, 2002
[snip] > That double floor in the RV-7 should help with a problem I had. .... I missed that part about the double floor. Thats standard on the -7? How about that! I guess I was ahead of my time. Floor vibration was in fact the reason I put in my own double floor in the -6. Lots about this in the archives but the gist is without the single floor there's a fair bit of HF vibration going on in that belly skin.The double floor not only helps from a comfort/fatigue standpoint but also helps avoid that old working rivet problem. Given that, bigger rivets in the stiffeners may not be needed, but again I doubt it would hurt to use them. Randall Henderson, RV-6 N6R (~400 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)attbi.com>
Subject: Re: RV7 floor stiffeners, ATC fuse holders
Date: Oct 29, 2002
[snip] > That double floor in the RV-7 should help with a problem I had. .... I missed that part about the double floor. Thats standard on the -7? How about that! I guess I was ahead of my time. Floor vibration was in fact the reason I put in my own double floor in the -6. Lots about this in the archives but the gist is without the single floor there's a fair bit of HF vibration going on in that belly skin.The double floor not only helps from a comfort/fatigue standpoint but also helps avoid that old working rivet problem. Given that, bigger rivets in the stiffeners may not be needed, but again I doubt it would hurt to use them. Randall Henderson, RV-6 N6R (~400 hrs) Portland, OR www.vanshomewing.org ________________________________________________________________________________
Date: Oct 29, 2002
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: Re: vacuum system help
Not the news I was hoping for but an answer nonetheless. Thanks, Ed. Scott in Vancouver ----- Original Message ----- From: "Ed Bundy" <ebundy(at)velocitus.net> Subject: Re: RV-List: vacuum system help > > It sounds like a bad regulator. I know the Rapco "Y" style regulators can't > be rebuilt. I bought the Rapco kit that included the whole system and it > worked fine when I installed it. The next flight it read really low. So I > adjusted the regulator until it was back in the green again. The next > flight it read really high. I finally got tired of playing with it and > called Rapco. They said they thought the regulator was probably the culprit > and sent me another one the next day. It worked great and has worked great > ever since. I asked them if they wanted me to send the old one back and > they told me to just destroy it (so it wouldn't accidentally end up on > another airplane) because it was non-rebuildable. > > Mine reads 4.5" at idle and just a smidge over 5" at full throttle. It's > just slightly under 5" at cruise. > > Ed Bundy RV6A 500+ hours > Boise, ID > > > I've finally adjusted the vacuum regulator so that the suction needle sits > in the middle of the green band at cruise power settings. But the regulator > doesn't seem to be regulating-I get one-to-two inches of vacuum on the > ground at runup and on the peg at eight inches during full power. > > One person told me these "Y" style regulators can be rebuilt and another > told me they couldn't. A Forum search didn't reveal any information. > > Any ideas? > > Scott in Vancouver > > ________________________________________________________________________________
Date: Oct 29, 2002
From: David Aronson <aronsond(at)pacbell.net>
Subject: Microair 760 and T-2000 sale
Listers: The 760 has been sold.... The Transponder is still available to the first person with a check. Thanks to all that showed interest. This list is great and FAST! Dave Aronson RV4 N504RV ________________________________________________________________________________
Date: Oct 30, 2002
From: Mark Phillips <ripsteel(at)edge.net>
Subject: Re: GPS for Altitude hold (was Rate of climb - flt test)
This being the case, is there a technical or practical argument against using GPS altitude data to drive an altitude hold device? Obviously useful course (or track or heading, but I don't want to start that up again !) data derived from GPS can keep the nose pointed toward a destination, why not do the same to control pitch trim? I sure don't possess the technical savvy to attempt such a device, but those who do might profit from such an offering. I had high hopes for the EZ-trim but it appears to be experiencing growing pains- any new developments here? From The PossumWorks in TN Mark Phillips Kevin Horton wrote: > David is correct that GPS altitude is probably more accurate than > barometric altitude most of the time, if we are more than a few > thousand feet above the location where the altimeter setting came > from. If our altitude is close to the site where the altimeter > setting came from, the altimeter is likely more accurate than the GPS. > > I'm not sure I would agree with the suggestion to time the GPS > altitude change instead of timing the barometric altitude change > though. In my experience, GPS altitude fluctuates quite a bit, so > I'm not sure that timing the rate of change of GPS altitude will lead > to an accurate result. GPS is much less accurate vertically than it > is horizontally. I believe that we can get more accurate results by > timing the rate of barometric altitude change, and then correcting > for non-standard temperature. ________________________________________________________________________________
From: BrownScottA(at)aol.com
Date: Oct 30, 2002
Subject: RV trip in need
Listers, Are there any guys out there that will be travelling soon from Fla to or thru the mid Texas area that wouldn't mind having their gas paid for? My father and I need a ride to the San Angelo, TX area and are wondering if we could get a ride there. We will pick up the tab. Scott ________________________________________________________________________________
From: <wstucklen1(at)cox.net>
Subject: Low Voltage Warning & Aux Batt management module
Date: Oct 30, 2002
Bob, Any chance you might make the .DWG file available for the Low Voltage Warning & Aux Batt management Module. I'd like to include it in my wiring documentation for the new plane... Are the PCB's available yet? IF so, where can I acquire one or more? Fred Stucklen RV-6A N925RV 2006 Hrs of safe flying! Working on 2'd RV-6A (Slow Build Version) ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Oct 30, 2002
Subject: Re: Refinishing wood props
I refinished my own Pacesetter wood prop. I sanded the entire prop evenly over the whole surface, with special attention to getting down far enough te remove any cracks in the finish,even if it meant sanding all the prop this much. I used three even coats of exterior Varithane ,being sure to keep it stirred all the time. There are ultraviolet inhibitors that must be kept in suspension to get them on the surface. I must cure for several days in a warm,dry place before use. Good Luck, RV-4 , N1191X , Flying Now Charleston, Arkansas ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: Re: GPS Problem
Date: Oct 30, 2002
I had a somewhat similar problem when I first set up. My com antenna is a copper strip attached to the canopy. The GPS antenna was mounted on top of the glare shield, only a couple inches from the com strip. Whenever I'd key the radio, the signal would overload the GPS which would then shut down and need to re-set itself. Moving the GPS antenna eliminated the problem. I now have it mounted to the back of the roll bar. Works fine. Hope that helps Andy > > Anyone have avionics advice on the following, - it seems that my Comm radio > is being picked up and re-radiated by the ELT which then shuts down the GPS. > > The Avionics Equipment installed is: - UPSAT SL60 GPS/COMM, Narco Nav 122D > VOR/ILS, ACK E-01 ELT. > Antennae locations are: - COMM on bottom under baggage compartment, ELT on > top aft fuselage, GPS antennae just aft of the sliding canopy track and > VOR/ILS cats whiskers on top of vertical stab. > All antennae wires have good separation except the VOR and GPS. > > During initial installation tests of the GPS/COMM the ELT might not have > been installed, the GPS/COMM tests went fine. Later, when I did practice ILS > approaches at a local airport using tower frequency 121.0 I noticed that I > would occasionally get a RAIM warning or a "unable to compute position" > message. It finally dawned that I had a harmonic problem bothering the GPS, > ground tests confirmed the problem. > > Disconnecting the ELT coax antennae at the ELT seemed to cure problem so I > speculat that the ELT is picking up the COMM radio, then re-radiating the > signal (harmonic) and bothering the GPS. The ELT manufacturer thought it > might be the telephone cable to the remote switch but disconnecting that > wire has no effect on the problem. > > I purchased a TED 4-70-54 notch filter yesterday and put it in the ELT > antennae line at the ELT, ground testing seemed to indicate a major > improvement but flight tests today confirm there is still a problem. > > My next plan is to try moving the notch filter around, should it be at the > ELT antennae, COMM transmitter or? > > On the bright side - we had a clear sky with strong outflow winds today and > the NavAid did a great job of tracking the localizer, 13 degrees of drift, > and light turbulence, nice to see - keep pounding those rivets! > > George McNutt > Langley B.C. > 6-A > > ________________________________________________________________________________
From: "Wiethe, Philip (P.J.)" <pwiethe(at)ford.com>
Subject: Re: . and engine horsepower mods.
Date: Oct 30, 2002
FWIW - Do an internet search on "cryogenic treating". Even though this process has not been approved by the aircraft engine manufacturers (why would they want to reduce their overhaul business), I am having it done on my engine parts. Phil 8A wings ________________________________________________________________________________
Date: Oct 30, 2002
From: SCOTT MORGAN <sdmorgan(at)prodigy.net>
Subject: Re: RV trip in need
Good morning Scott, When did you need a ride to San Angelo and what is your departure point? Regards, Scott Morgan League City, TX Listers, Are there any guys out there that will be travelling soon from Fla to or thru the mid Texas area that wouldn't mind having their gas paid for? My father and I need a ride to the San Angelo, TX area and are wondering if we could get a ride there. We will pick up the tab. Scott ________________________________________________________________________________
From: Dwpetrus(at)aol.com
Date: Oct 30, 2002
Subject: engine start and taxi test yesterday
rph(at)lainternet.com, cjohnson(at)jpjcpa.com, SIDLOVE(at)INU.NET, rentmoor(at)rochelle.net, capetrus(at)hotmail.com, claypetrus(at)msn.com, PRYORE(at)aol.com, RV-LIST(at)matronics.com, CSELF(at)PLYMOUTH.COM, DerFlieger(at)aol.com, miketerry(at)kjlo.com, WALLB(at)OIBANK.COM Cranked the engine on the RV8A airplane for the first time yesterday. After some minor adjustments I did some taxi testing. The engine ran great and the airplane handled properly on the ground. It is extremely powerful and will slide the airplane across the tarmac with the brakes locked at 3/4 throttle. Still have many details to finish before the first flight, but it should fly before the end of the year. Wayne Petrus RV8A finishing ________________________________________________________________________________
From: "Bob Hassel" <bob@hassel-usa.com>
Subject: Diesel Engine
Date: Oct 30, 2002
Wed, Oct 30 2002 Diesels In The Sky By ANN Correspondent Pete Combs When you think "diesel," you think 18-wheelers. Mercedes that seem to last forever. Generators. Airplanes. Airplanes? Yup. By the end of the year, Superior Air Parts hopes to have FAA certification for the Centurion TAE 125, a 135-hp diesel engine being retrofitted into Cessna 172s and Piper PA-28s. The Centurion is built by Thielert TAE, a manufacturer based in Lichtenstein, Germany, and is already certified by the JAA in Europe and the LBA in Germany. "We anticipate FAA approval in the very near future," says Superior's Terry Wood, as AOPA Expo wrapped up Saturday afternoon. The Centurion TAE 125 is a 1.7 liter engine that boasts a revolutionary engine management system. Forget fiddling with the mixture. No more complex prop controls. This engine employs FADEC (Full Authority Digital Engine Control). It's all digital. And every time you go in for an oil change or any other sort of engine maintenance, the A&P downloads data from the engine's onboard computer and sends it off in an e-mail to the factory. "There's just one lever to control the engine," boasts Wood. "There are two CPUs in the engine for redundancy." Wood predicts the TAE 125 will last a lot longer than the average 2000 hour time between overhauls for most normally aspirated aircraft prop engines. In fact, there is no TBO. "There is a 2400 hour TBR," says Wood. That's "To Be Replaced." This $20,000 engine is, for all intents and purposes, disposable. Replacing it, Wood claims, is cheaper than overhauling a $23,000 Lycoming IO-360. "People are starved for new technology," he says. "Lycoming and Continental [the two biggest manufacturers of general aviation piston engines] are based on 1940s technology." Superior claims there are other big-time advantages to this engine. The company says there are fewer emissions. Instead of running on 100LL, the only leaded gasoline still made in America, the TAE 125 runs on diesel fuel or Jet-A. "The 1.7 runs at 2300 rpm at cruise, versus 2800 rpm [sounds like a fast cruise to me --ed.] for normally-aspirated engines. There's less noise," says Wood. As Aero-News reported last Summer, Diamond Aircraft is planning to offer Theilert diesels in its forthcoming new DA-42 Twinstar, as well as in its single-engine four-place aircraft. FMI: www.superior-air-parts.com ---- Bob Hassel Email: bob @ hassel-usa.com URL: http://www.hassel-usa.com They that can give up essential liberty to obtain a little temporary safety deserve neither liberty nor safety - Benjamin Franklin ________________________________________________________________________________
From: "Marcus Ward" <marcus@f-64.org>
Subject: Re: RV trip in need
Date: Oct 30, 2002
You know I hate to be a party pooper or a rule monger but you guys know that taking any sort of compensation for a ride is considered to be a very bad thing by the FAA, mmmmkay? That includes covering gas. If they find out they'll come down on you like a load of bricks. (This rule was brought about not by the FAA but by the IRS leaning on the FAA - wouldn't want anyone making money they don't know about!) Marcus ----- Original Message ----- From: "SCOTT MORGAN" <sdmorgan(at)prodigy.net> Subject: Re: RV-List: RV trip in need > > > Good morning Scott, > When did you need a ride to San Angelo and what is your departure point? > Regards, > Scott Morgan > League City, TX BrownScottA(at)aol.com > > Listers, > > Are there any guys out there that will be travelling soon from Fla to or thru > the mid Texas area that wouldn't mind having their gas paid for? My father > and I need a ride to the San Angelo, TX area and are wondering if we could > get a ride there. We will pick up the tab. > > Scott > > ________________________________________________________________________________
From: BrownScottA(at)aol.com
Date: Oct 30, 2002
Subject: Re: RV trip in need
Marcus, Sharing expenses is not illegal in any way shape or form. The expense of owning and operating an RV far exceeds gas. I hardly think that it illegal. Scott ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: RV trip in need
Date: Oct 30, 2002
You can share the operating expenses. It doesn't say "how much" share you have to do. If one person buys 99% of the gas, and the other buys 1% of the gas, that is still technically "sharing" the operating expenses. 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: "Marcus Ward" <marcus@f-64.org> Subject: Re: RV-List: RV trip in need > > You know I hate to be a party pooper or a rule monger but you guys know that > taking any sort of compensation for a ride is considered to be a very bad > thing by the FAA, mmmmkay? That includes covering gas. If they find out > they'll come down on you like a load of bricks. (This rule was brought > about not by the FAA but by the IRS leaning on the FAA - wouldn't want > anyone making money they don't know about!) > > Marcus > > ----- Original Message ----- > From: "SCOTT MORGAN" <sdmorgan(at)prodigy.net> > To: > Subject: Re: RV-List: RV trip in need > > > > > > > > Good morning Scott, > > When did you need a ride to San Angelo and what is your departure point? > > Regards, > > Scott Morgan > > League City, TX > BrownScottA(at)aol.com > > > > Listers, > > > > Are there any guys out there that will be travelling soon from Fla to or > thru > > the mid Texas area that wouldn't mind having their gas paid for? My father > > and I need a ride to the San Angelo, TX area and are wondering if we could > > get a ride there. We will pick up the tab. > > > > Scott > > > > > > ________________________________________________________________________________
Date: Oct 30, 2002
From: Brian Armstrong <armstrbc(at)ucsub.colorado.edu>
Subject: Re: RV trip in need
i talked to a FSDO guy in denver about that. he said that while that is technically correct, an FAA inspector pursuing a violation is much more likely to believe you are "sharing expenses" if you split it closer to evenly. remember, even their own rules are still open to their own interpretation. brian armstrong englewood, co -- On Wed, 30 Oct 2002, Paul Besing wrote: > > You can share the operating expenses. It doesn't say "how much" share you > have to do. If one person buys 99% of the gas, and the other buys 1% of the > gas, that is still technically "sharing" the operating expenses. > > 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: "Marcus Ward" <marcus@f-64.org> > To: > Subject: Re: RV-List: RV trip in need > > > > > > You know I hate to be a party pooper or a rule monger but you guys know > that > > taking any sort of compensation for a ride is considered to be a very bad > > thing by the FAA, mmmmkay? That includes covering gas. If they find out > > they'll come down on you like a load of bricks. (This rule was brought > > about not by the FAA but by the IRS leaning on the FAA - wouldn't want > > anyone making money they don't know about!) > > > > Marcus > > > > ----- Original Message ----- > > From: "SCOTT MORGAN" <sdmorgan(at)prodigy.net> > > To: > > Subject: Re: RV-List: RV trip in need > > > > > > > > > > > > > Good morning Scott, > > > When did you need a ride to San Angelo and what is your departure point? > > > Regards, > > > Scott Morgan > > > League City, TX > > BrownScottA(at)aol.com > > > > > > Listers, > > > > > > Are there any guys out there that will be travelling soon from Fla to or > > thru > > > the mid Texas area that wouldn't mind having their gas paid for? My > father > > > and I need a ride to the San Angelo, TX area and are wondering if we > could > > > get a ride there. We will pick up the tab. > > > > > > Scott > > > > > > > > > > > > ________________________________________________________________________________
From: "Dave von Linsowe" <davevon(at)tir.com>
Subject: Re: RV-6A airspeed update
Date: Oct 30, 2002
I would really like to see a list devoted to speed enhancements of the RV's!!! I just finished reading "Speed with Economy" by Kent Paser. If you haven't read it and want to go faster, it's a must read! Kent started with a stock Mustang II and methodically made improvements that raised the cruise speed 60mph and lowered his fuel consumption. His O-320 powered Mustang will blow the doors off any RV and nearly match a Rocket. I realize speed isn't everything, just that if Van was satisfied with the Playboy none of us would be flying RV's and that all airplanes are compromises that can be improved upon in one way or another. And if we share what works and what doesn't we can reduce the cost and time it takes to dial in the improvements. It took Kent 23 years... Dave ----- Original Message ----- From: "Paul Besing" <azpilot(at)extremezone.com> Subject: RV-List: RV-6A airspeed update > > Ok. I did some more concrete tests today. Here is what I came up with: > > 2 methods. 3 way and 4 way track for the GPS. > > Both came up with 154 KTS Groundspeed. Not as bad as I had thought, but still about 10 Kts low. > > Here is the data on the engine performance: > > 8000' 22.7"MAP 2600 RPM 8.2GPH > > I suspect there are a few possible drag sources here. Perhaps the baffles. Haven't checked to see how tight they are. Also, he has the Team Rocket wheel pants. Don't know any performance differences than Van's wheel pants. He had a pretty heavy wing, and had to do considerable blocking and squeezing of the ailerons to make them level. One aileron is up a little, and one is down a little. > > I imagine there could be a seperate RV-List for the different theories on speed enhancement of RV's. Too many variables to know off hand. Either way, he has a 177 MPH RV-6A. I'd like to see closer to 185 or so, but not too far off. > > Thanks for all the advice, > > 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 > > ________________________________________________________________________________
Date: Oct 30, 2002
From: David Aronson <aronsond(at)pacbell.net>
Subject: Re: RV trip in need
Marcus: I believe you are mistaken. A passenger may "share expenses" with the pilot/AC owner. This doesn't emply a commercial ticket is necessary. FAR 61.118 (b) states: "A private pilot may share the operating expenses of a flight with his passengers." The gender mistake is taken as He/She....... Now this is stated out of my FAR that is two years out of date but I haven't heard anything about a major change in the FAA's position. Is there someone who can quote from the most recent FAR. Dave Aronson RV4 N504RV Marcus Ward wrote: > > You know I hate to be a party pooper or a rule monger but you guys know that > taking any sort of compensation for a ride is considered to be a very bad > thing by the FAA, mmmmkay? That includes covering gas. If they find out > they'll come down on you like a load of bricks. (This rule was brought > about not by the FAA but by the IRS leaning on the FAA - wouldn't want > anyone making money they don't know about!) > > Marcus > > ----- Original Message ----- > From: "SCOTT MORGAN" <sdmorgan(at)prodigy.net> > To: > Subject: Re: RV-List: RV trip in need > > > > > > > Good morning Scott, > > When did you need a ride to San Angelo and what is your departure point? > > Regards, > > Scott Morgan > > League City, TX > BrownScottA(at)aol.com > > > > Listers, > > > > Are there any guys out there that will be travelling soon from Fla to or > thru > > the mid Texas area that wouldn't mind having their gas paid for? My father > > and I need a ride to the San Angelo, TX area and are wondering if we could > > get a ride there. We will pick up the tab. > > > > Scott > > > > > ________________________________________________________________________________
From: "Camille Hawthorne" <cammie(at)sunvalley.net>
Subject: Re: RV trip in need
Date: Oct 30, 2002
I believe the verbage in the regs says "prorata share". In other words, the pilot must pay at least his/her percentage of the cost. ie. three occupants, 33%. That can mean rental cost or, if the aircraft is privately owned, fuel, oil, or airport expenses only. (FAR 61.113 (c)) I would be very careful with this one. If anything unusual happened it might read like one of those reports where all the dirt pertaining to the accident aircraft/pilot is reported even though a totally unrelated maintenance issue was the cause. There are other forms of compensation, I'd explore those options. (Need a new part?) Now, if the passengers are associated with a federal election campaign, that's a different story......(FAR 91.321) Sorry to bring this up, but I've heard lots of stories. Cammie Hawthorne, CFII ----- Original Message ----- From: "Paul Besing" <azpilot(at)extremezone.com> Subject: Re: RV-List: RV trip in need > > You can share the operating expenses. It doesn't say "how much" share you > have to do. If one person buys 99% of the gas, and the other buys 1% of the > gas, that is still technically "sharing" the operating expenses. > > 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: "Marcus Ward" <marcus@f-64.org> > To: > Subject: Re: RV-List: RV trip in need > > > > > > You know I hate to be a party pooper or a rule monger but you guys know > that > > taking any sort of compensation for a ride is considered to be a very bad > > thing by the FAA, mmmmkay? That includes covering gas. If they find out > > they'll come down on you like a load of bricks. (This rule was brought > > about not by the FAA but by the IRS leaning on the FAA - wouldn't want > > anyone making money they don't know about!) > > > > Marcus > > > > ----- Original Message ----- > > From: "SCOTT MORGAN" <sdmorgan(at)prodigy.net> > > To: > > Subject: Re: RV-List: RV trip in need > > > > > > > > > > > > > Good morning Scott, > > > When did you need a ride to San Angelo and what is your departure point? > > > Regards, > > > Scott Morgan > > > League City, TX > > BrownScottA(at)aol.com > > > > > > Listers, > > > > > > Are there any guys out there that will be travelling soon from Fla to or > > thru > > > the mid Texas area that wouldn't mind having their gas paid for? My > father > > > and I need a ride to the San Angelo, TX area and are wondering if we > could > > > get a ride there. We will pick up the tab. > > > > > > Scott > > > > > > > > > > > > ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: legal ride???
Date: Oct 30, 2002
A local non-profit group has an annual silent auction as a fund raiser. Recently I was asked to donate a sight seeing ride in my -6A to be bid on as part of the auction. The highest bidder makes the donation to the non-profit, and I then give the ride. I receive no compensation or shared expenses, either from the winning bidder or from the non-profit. Is this legal? Andy ________________________________________________________________________________
From: "Camille Hawthorne" <cammie(at)sunvalley.net>
Subject: Need flaring tool
Date: Oct 30, 2002
Anyone have a 37 degree flaring tool for sale? Or even better, one that I can borrow in the Boise area? Please respond offline. Cammie cammie(at)sunvalley.net ________________________________________________________________________________
Date: Oct 30, 2002
From: Rob Prior <rv7(at)b4.ca>
Subject: Re: legal ride???
It would be in Canada. I suspect the US regs are similar enough in spirit, if not in wording. Nobody is "making money" at this, someone is making a donation to a non-profit society, and you're taking a friend for a ride. Now, if the non-profit group was called "Andy's RV-6A Club" and had only one member (Andy), that might be a little questionable... 8-) -RB4 Aircraft Technical Book Company wrote: > > A local non-profit group has an annual silent auction as a fund raiser. > Recently I was asked to donate a sight seeing ride in my -6A to be bid on as > part of the auction. The highest bidder makes the donation to the > non-profit, and I then give the ride. I receive no compensation or shared > expenses, either from the winning bidder or from the non-profit. > > Is this legal? > > Andy ________________________________________________________________________________
Subject: legal ride???
Date: Oct 30, 2002
From: "Todd Wenzel" <TWenzel@heartland-software.com>
Yes, I believe there is an exception for this arrangement - there better be, I've been doing it this way! Todd Wenzel Delafield, WI USA RV-8AQB - Finish Kit N900TW - Reserved TWenzel@Heartland-Software.com -----Original Message----- From: Aircraft Technical Book Company [mailto:winterland(at)rkymtnhi.com] Subject: RV-List: legal ride??? --> A local non-profit group has an annual silent auction as a fund raiser. Recently I was asked to donate a sight seeing ride in my -6A to be bid on as part of the auction. The highest bidder makes the donation to the non-profit, and I then give the ride. I receive no compensation or shared expenses, either from the winning bidder or from the non-profit. Is this legal? Andy ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: legal ride???
Date: Oct 30, 2002
Andy, YES, Absolutely!! You are a private pilot giving a ride without being compensated for it in any way, shape or form! (The resulting RV-Grin is not considered compensation) Konrad ----- Original Message ----- From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com> Subject: RV-List: legal ride??? > > A local non-profit group has an annual silent auction as a fund raiser. > Recently I was asked to donate a sight seeing ride in my -6A to be bid on as > part of the auction. The highest bidder makes the donation to the > non-profit, and I then give the ride. I receive no compensation or shared > expenses, either from the winning bidder or from the non-profit. > > Is this legal? > > Andy > > ________________________________________________________________________________
From: "Joshua Siler" <joshs(at)ninatek.com>
Subject: legal ride???
Date: Oct 30, 2002
I believe FAR 61.118 allows it explicitly. Regards, Josh http://www.PilotDaily.com Daily news for general aviation pilots. -----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: legal ride??? A local non-profit group has an annual silent auction as a fund raiser. Recently I was asked to donate a sight seeing ride in my -6A to be bid on as part of the auction. The highest bidder makes the donation to the non-profit, and I then give the ride. I receive no compensation or shared expenses, either from the winning bidder or from the non-profit. Is this legal? Andy ________________________________________________________________________________
From: "John Helms" <jhelms(at)i1.net>
Subject: Re: legal ride???
Date: Oct 30, 2002
Are you really asking if it is LEGAL? I don't see how it would not be... I think what you may actually be asking is would it covered under your insurance policy. If so, you would have to ask your insurance agent specifically for an answer. I am not aware of any companies that would exclude coverage for a ride like that. So long as you are not being compensated for it. Under most policies, you could even accept $ for gas and oil and the like under most policies (must be equally shared by occupants.) The only thing most policies exclude would be fixed costs (maintenance/engine fund, hangar costs, insurance, etc.) John "JT" Helms Branch Manager NationAir Insurance Agency Pleasure and Business Branch ----- Original Message ----- From: "Todd Wenzel" <TWenzel@heartland-software.com> Subject: RE: RV-List: legal ride??? <TWenzel@Heartland-Software.com> Yes, I believe there is an exception for this arrangement - there better be, I've been doing it this way! Todd Wenzel Delafield, WI USA RV-8AQB - Finish Kit N900TW - Reserved TWenzel@Heartland-Software.com -----Original Message----- From: Aircraft Technical Book Company [mailto:winterland(at)rkymtnhi.com] Subject: RV-List: legal ride??? --> A local non-profit group has an annual silent auction as a fund raiser. Recently I was asked to donate a sight seeing ride in my -6A to be bid on as part of the auction. The highest bidder makes the donation to the non-profit, and I then give the ride. I receive no compensation or shared expenses, either from the winning bidder or from the non-profit. Is this legal? Andy ________________________________________________________________________________
From: "Joshua Siler" <joshs(at)ninatek.com>
Subject: RE: legal ride??
Date: Oct 30, 2002
You're right. Good catch - I found it referenced from Angel Flight here http://www.angelflight.org/articles/af00_010b.html , as well as a couple other links (search for 61.118 on google). Must be typo. Josh http://www.PilotDaily.com Daily news for general aviation pilots. -----Original Message----- From: Aircraft Technical Book Company [mailto:winterland(at)rkymtnhi.com] Subject: legal ride?? What is 61.118? According to the 2003 FARs, that number is still blank - reserved for future rules. Andy I believe FAR 61.118 allows it explicitly. Regards, Josh ________________________________________________________________________________
From: MeangreenRV4(at)aol.com
Date: Oct 30, 2002
Subject: Re: Exxon Elite
In a message dated 10/29/2002 11:51:51 AM Pacific Standard Time, n8wv(at)hotmail.com writes: > > What are the ramifications of switching from Aeroshell 20W-50 to Exxon > Elite 20W-50? > > What other oils are "OK" for use in a Lycosaur? What about automotive > synthetic blends? > > -Bill VonDane > RV-8A ~ 74 hours > www.vondane.com > I use Aero Shell 50 wt plus and I haven't used the multi viscosity oils such as Exxon or Shell but from what I have been told by the ones that have used it, unless you live were it gets very cold the multi viscosity oils will turn a perfectly good engine into a great boat anchor. This is from pilots that fly every week. I would call a Lycoming engine shop and ask them their opinion. Hope this helps Tim Barnes Meangreen RV-4 ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: legal ride???
Date: Oct 30, 2002
Sounds similar to Young Eagles to me.... - 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 Todd Wenzel > Sent: Wednesday, October 30, 2002 11:49 AM > To: rv-list(at)matronics.com > Subject: RE: RV-List: legal ride??? > > > --> <TWenzel@Heartland-Software.com> > > Yes, I believe there is an exception for this arrangement - > there better be, I've been doing it this way! > > Todd Wenzel > Delafield, WI USA > RV-8AQB - Finish Kit > N900TW - Reserved > TWenzel@Heartland-Software.com > > > -----Original Message----- > From: Aircraft Technical Book Company > [mailto:winterland(at)rkymtnhi.com] > To: rv-list(at)matronics.com > Subject: RV-List: legal ride??? > > > --> > > A local non-profit group has an annual silent auction as a > fund raiser. Recently I was asked to donate a sight seeing > ride in my -6A to be bid on as part of the auction. The > highest bidder makes the donation to the non-profit, and I > then give the ride. I receive no compensation or shared > expenses, either from the winning bidder or from the non-profit. > > Is this legal? > > Andy ________________________________________________________________________________
From: "zilik(at)direcpc.com" <zilik(at)direcpc.com>
Subject: Re: Exxon Elite
Date: Oct 30, 2002
Wow, this is really good information. No wonder I climb so slow, I got a boat anchor in the front and I did'nt know it. Gary >I use Aero Shell 50 wt plus and I haven't used the multi viscosity oils such >as Exxon or Shell but from what I have been told by the ones that have used >it, unless you live were it gets very cold the multi viscosity oils will >turn a perfectly good engine into a great boat anchor. This is from pilots >that fly every week. I would call a Lycoming engine shop and ask them their >opinion. >Hope this helps >Tim Barnes >Meangreen RV-4 ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: Oils
Date: Oct 30, 2002
Most aviation oils don't use detergents, they use dispersants, which are very different. The idea is to keep things suspended so that it either gets trapped by the filter or tossed during oil changes, rather than sticking to the inside. Common detergents found in automotive oils are ash based which, when introduced into the combustion chamber in small amounts, increase detonation = very bad. I only have my experience's from overhauling numerous automotive and aircraft engines where thin multi grade oils were used extensively. The rate of camshaft/lifter wear was far higher in these engines. Now that said, these engines were operating exclusively in the south south west west where it is normally 80 and above. In colder climates the multigrades are critical for the warmup phase. Best case to make TBO is to use single weight oils with a pre-heater and a pre-oiler, and fly it for at least one hour every day ;{) But do be aware, Multigrade oils are the specific viscosity of the lower number. They then have viscosity index enhancers that cause to oil to thin at a lower rate with increases in temperature. So at operating temperatures they "act" like the higher viscosity. This is an act that usually works ok at best, until the oil is old, either time wise or use wise. The idea of using 25 hr vs 50 hr is based upon the fact that oil really begins to get contaminted and certain features such as dispersants, anti-corrosive agents, and viscosity index enhancers begin to break down after about 25 hours, and are really failing after 50 hours. This is accelerated greatly in those areas where ambient temps are higher, and oil temps above 200-210 are common. So, do you want to change your oil before its worn out, or after its worn out. Additionally many folks don't collect 25 hours in 3 months so they ought not to be using the 50 hours "engine time" criteria for oil changes. Also, changing the filter, or the oil without the other is a waste of both given the cost and time is so low to just do it all every time. On a final note, although there is a lot of evidence that most engine wear occurs during start/warmup, there is now also a lot of evidence that micro-corrosion due to contaminants, including moisture, plays a major factor in this. The simplest way to remove those contaminants is to drain them out as often as you can afford. W ________________________________________________________________________________
From: "Randy Compton" <rdcompton(at)earthlink.net>
Subject: Re: Exxon Elite
Date: Oct 30, 2002
----- Original Message ----- From: <MeangreenRV4(at)aol.com> Subject: Re: RV-List: Exxon Elite > I use Aero Shell 50 wt plus and I haven't used the multi viscosity oils such > as Exxon or Shell but from what I have been told by the ones that have used > it, unless you live were it gets very cold the multi viscosity oils will > turn a perfectly good engine into a great boat anchor. This is from pilots > that fly every week. I would call a Lycoming engine shop and ask them their > opinion. > > Hope this helps > > Tim Barnes > Meangreen RV-4 Interesting, but now I'm really confused. Just had my engine overhauled, and ECI recommends Phillips X/C 20W-50, says it's good from break-in to TBO. And since it's completely mineral based, if you have to have some work done on a cylinder in the future you won't need to run a "break-in" oil. They also say it gives just as good a coating protection from corrosion on the innards while the engine just sits as 50W, but it flows quicker on start-up and thereby reduces wear as compared to a single weight. So, I think I'll follow ECI's recommendation and just keep my fingers crossed. Randy Compton RV-3A N84VF Gulf Breeze, FL ________________________________________________________________________________
Date: Oct 30, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: GPS Problem
> > >Anyone have avionics advice on the following, - it seems that my Comm radio >is being picked up and re-radiated by the ELT which then shuts down the GPS. > >The Avionics Equipment installed is: - UPSAT SL60 GPS/COMM, Narco Nav 122D >VOR/ILS, ACK E-01 ELT. >Antennae locations are: - COMM on bottom under baggage compartment, ELT on >top aft fuselage, GPS antennae just aft of the sliding canopy track and >VOR/ILS cats whiskers on top of vertical stab. >All antennae wires have good separation except the VOR and GPS. > >During initial installation tests of the GPS/COMM the ELT might not have >been installed, the GPS/COMM tests went fine. Later, when I did practice ILS >approaches at a local airport using tower frequency 121.0 I noticed that I >would occasionally get a RAIM warning or a "unable to compute position" >message. It finally dawned that I had a harmonic problem bothering the GPS, >ground tests confirmed the problem. > >Disconnecting the ELT coax antennae at the ELT seemed to cure problem so I >speculat that the ELT is picking up the COMM radio, then re-radiating the >signal (harmonic) and bothering the GPS. The ELT manufacturer thought it >might be the telephone cable to the remote switch but disconnecting that >wire has no effect on the problem. > >I purchased a TED 4-70-54 notch filter yesterday and put it in the ELT >antennae line at the ELT, ground testing seemed to indicate a major >improvement but flight tests today confirm there is still a problem. > >My next plan is to try moving the notch filter around, should it be at the >ELT antennae, COMM transmitter or? > >On the bright side - we had a clear sky with strong outflow winds today and >the NavAid did a great job of tracking the localizer, 13 degrees of drift, >and light turbulence, nice to see - keep pounding those rivets! > >George McNutt >Langley B.C. >6-A > George, I used to get involved in flight tests of IFR GPS installations a few years ago. I saw several cases where there was interference from the COM to the GPS. My recollection (which could be wrong) is that a couple of these problem cases were fixed by improving the bonding between the COM antenna and the air frame (i.e. make sure there is a very low resistance electrical bond between the antenna and the skin). I don't understand how this would help - I am simply saying that I recall that it was useful. Let us know how you get this resolved. Good luck, -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
Date: Oct 30, 2002
From: Mark Schrimmer <mschrimmer(at)pacbell.net>
Subject: RV7 floor stiffeners
I missed that part about the double floor. Thats standard on the -7? Does the 9A fuselage also have the double floor or is it just part of the 7 to handle the extra horsepower? Mark Schrimmer RV-9A Wings Irvine, CA ________________________________________________________________________________
Date: Oct 30, 2002
From: Mark Schrimmer <mschrimmer(at)pacbell.net>
Subject: Drill and dimple vs just dimple
You folks know that Van did advertise, or reported in the RVator, that they built the wings without ever picking up a drill. Well, folks, that tells me it's OK to do that if they don't say it's not when they advertise it that way. Maybe they did; but, I don't ever remember their doing it. Jim, I believe the story explained that the reason a prototype set of RV-9A wings was built without using a drill was to test the accuracy of the pre-punched holes. The same story also recommended that builders use a drill to minimize the possibility of cracks forming. Mark Schrimmer RV-9A Wings Irvine, CA ________________________________________________________________________________
Date: Oct 30, 2002
From: Mark Schrimmer <mschrimmer(at)pacbell.net>
Subject: Calibrated airspeed (Was RV-6A airspeed problem)
the number read off the ASI face is the "indicated a/s", which has to be corrected for both instrument error and pitot and (mostly) static port position error to get "calibrated A/S" Jim, What is the procedure for calibrating an airspeed indicator? Is this typically done during the first few test flights? Mark Schrimmer RV-9A Wings Irvine, CA ________________________________________________________________________________
Date: Oct 30, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: GPS for Altitude hold (was Rate of climb - flt test)
Two issues to wrestle with: 1. ATC wants us at particular barometric altitudes, which will not be the same as actual altitudes. So if we wanted to fly at 6,000 ft on our altimeter, we need to understand that the GPS altitude will differ from that. But, it should be practical to level off at the desired altitude using the altimeter, then tell your GPS altitude hold gizmo to memorize the current GPS altitude and hold it. The difference between GPS altitude and barometric altitude would slowly vary with time, as the satellite geometry changed (which would make the GPS altitude move up and down) and you travelled to areas with different local pressures and temperatures (which would make the barometric altitude move up and down). So you might have to reset the GPS altitude hold reference once in a while. 2. There is a certain amount of noise in the GPS altitude calculation - i.e. even if the actual altitude is constant, the GPS altitude may move up and down a bit. The amount of noise probably varies with different GPS units, satellite geometry, etc. I did an experiment with my hand held GPS a couple of nights ago - I went out in my driveway and stood there for a few minutes and watched the GPS altitude display. It varied in a range of about 30 ft total. If the altitude hold function was trying to keep the GPS altitude constant the aircraft would be moving up and down over a 30 ft range which might not be comfortable. I don't know whether a more expensive GPS box would have less noise in its GPS altitude or not. So this altitude noise may or may not be a problem. For extra points you could mount GPS antennae on the nose and tail, and use differential GPS techniques to develop an attitude hold function. The attitude information could be used to damp the system response to noise in the GPS altitude, and attitude hold would be a nice extra piece of functionality anyway. The use of differential techniques to calculate attitude has been done in a research setting, but I don't think anyone was developed an actual product that works this way. See: http://einstein.stanford.edu/gps/PDF/att_and_displ_4ga_akb96.pdf Kevin Horton > >This being the case, is there a technical or practical argument >against using GPS >altitude data to drive an altitude hold device? Obviously useful course (or >track or heading, but I don't want to start that up again !) data >derived from >GPS can keep the nose pointed toward a destination, why not do the same to >control pitch trim? I sure don't possess the technical savvy to >attempt such a >device, but those who do might profit from such an offering. I had high hopes >for the EZ-trim but it appears to be experiencing growing pains- any new >developments here? > >From The PossumWorks in TN >Mark Phillips > >Kevin Horton wrote: > >> David is correct that GPS altitude is probably more accurate than >> barometric altitude most of the time, if we are more than a few >> thousand feet above the location where the altimeter setting came >> from. If our altitude is close to the site where the altimeter >> setting came from, the altimeter is likely more accurate than the GPS. >> >> I'm not sure I would agree with the suggestion to time the GPS >> altitude change instead of timing the barometric altitude change >> though. In my experience, GPS altitude fluctuates quite a bit, so >> I'm not sure that timing the rate of change of GPS altitude will lead >> to an accurate result. GPS is much less accurate vertically than it >> is horizontally. I believe that we can get more accurate results by >> timing the rate of barometric altitude change, and then correcting > > for non-standard temperature. > ________________________________________________________________________________
Date: Oct 30, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Calibrated airspeed (Was RV-6A airspeed problem)
> >the number read off the ASI face is the "indicated a/s", which has to >be corrected for both instrument error and pitot and (mostly) static port >position error to get "calibrated A/S" > > >Jim, > >What is the procedure for calibrating an airspeed indicator? Is this >typically done during the first few test flights? > >Mark Schrimmer >RV-9A Wings >Irvine, CA > Mark, I've got quite a bit of info on the Flight Test Links part of my web site that deals with this issue. The old version of that page is at: http://members.rogers.com/khorton/ftlinks.html I'm working on a new version of that page at: http://go.phpwebhosting.com/~khorton/rv8/links.php See the Flight Test - Pitot-Static Cals section. In particular see: http://members.rogers.com/khorton/rvlinks/ssec.html Short version follows: The total error in the airspeed indication is the sum of a number of errors: 1. instrument error - the errors due to imperfections in the instrument itself. 2. static source position error - the static source is not located in a position that has the same pressure as the ambient pressure. This error will also affect the altimeter. 3. pitot source position error - the pitot source may be poorly located so that it is not sensing the correct pitot pressure. 4. errors due to leaks in the pitot or static system. The leaks should be found by a good leak check. Most people who do flight testing to determine the airspeed error don't really care about figuring out how much of the airspeed error is due to each source - they only want to know what the total amount of error is. This is probably OK for VFR flying, but for IFR I would want to know what the static source error was because this would affect the accuracy of the altimeter, which could be an issue during approaches. Also, if you every have to change the airspeed indicator you would want to do the flight tests again because you wouldn't know how the instrument error of the new ASI compared to the old one. It is possible to use a water manometer to determine the instrument error. See: http://www.eaa1000.av.org/technicl/instcal/instcal.htm http://members.rogers.com/khorton/rvlinks/asi.zip The pitot source error is normally negligible. Once you know the total error from flight tests, and the instrument error, you can calculate the static source error, which lets you figure out the effect on the altimeter. If anyone wants to do the proper testing I am prepared to work with them to help them do a good test and to analyze the data. -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
From: BrownScottA(at)aol.com
Date: Oct 30, 2002
Subject: RV ride
Guys, this is ridiculous...sorry that I asked. Scott ________________________________________________________________________________
Date: Oct 30, 2002
From: Rob Prior <rv7(at)b4.ca>
Subject: Re: Drill and dimple vs just dimple
My recollection from the first time this discussion came up: The article to which you refer had Van talking about the first RV-7 or -9 wing ever made. ie. The prototype. They didn't bother with the drilling for two reasons: One, to save time (which everyone seems to want to save now), and two, because the wing was only going to be used for static load tests, which I believe it was. It was never intended to be used on an aircraft. One of Van's engineers has sent an email that was copied to the forum, that says explicitly that "thou shalt drill and deburr before dimpling." I know that "did you match drill the holes before riveting?" will become one of the questions on my checklist if I ever buy a finished RV from someone. If the answer is "no," I won't be buying. -RB4 Mark Schrimmer wrote: > > You folks know that Van did advertise, or reported in the RVator, that they > built the wings without ever picking up a drill. Well, folks, that tells me > it's OK to do that if they don't say it's not when they advertise it that > way. Maybe they did; but, I don't ever remember their doing it. > > Jim, > > I believe the story explained that the reason a prototype set of RV-9A wings > was built without using a drill was to test the accuracy of the pre-punched > holes. The same story also recommended that builders use a drill to minimize > the possibility of cracks forming. ________________________________________________________________________________
From: "James E. Clark" <jclark(at)conterra.com>
Subject: Drill and dimple vs just dimple
Date: Oct 30, 2002
I don't have the article before me but didn't they also imply that they were doing a "worst-case build" for wing testing? Or was that another wing that they tested using "less than optimal" constuction techniques? Again, just asking for clarification. James > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Mark Schrimmer > Sent: Wednesday, October 30, 2002 6:18 PM > To: rv-list-matronics.com > Subject: RV-List: Drill and dimple vs just dimple > > > You folks know that Van did advertise, or reported in the RVator, > that they > built the wings without ever picking up a drill. Well, folks, > that tells me > it's OK to do that if they don't say it's not when they advertise it that > way. Maybe they did; but, I don't ever remember their doing it. > > Jim, > > I believe the story explained that the reason a prototype set of > RV-9A wings > was built without using a drill was to test the accuracy of the > pre-punched > holes. The same story also recommended that builders use a drill > to minimize > the possibility of cracks forming. > > Mark Schrimmer > RV-9A Wings > Irvine, CA > > ________________________________________________________________________________
Date: Oct 30, 2002
From: Mark Schrimmer <mschrimmer(at)pacbell.net>
Subject: Re: legal ride???
I was wrong. The FAR that were listed are correct and they state standard and that means factory certified. Experimental is a special airworthiness. Further you must be a commercial rated pilot AND in a drug testing program. The EAA in order to fly Young Eagles got a waiver from the drug testing requirement and cannot accept donations. Cy, This appears to mean you can't give a Young Eagles ride in a homebuilt and you have to have a commercial license. Is this correct, or did I miss something? Mark Schrimmer RV-9A Wings Irvine, CA ________________________________________________________________________________
Date: Oct 30, 2002
From: adrianchick <adrianchick(at)comcast.net>
Subject: wing dings
what is the best way to deal with dings from the rivet gun on the top wing surface? Filler? What kind? Adrian Chick rv6a finished wings ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Re: legal ride???
Date: Oct 30, 2002
My chapter's YE person told me I just need to be an EAA member and a current pilot to give YE rides. No mention of Comm. rating or drug tests..... - 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 Mark > Schrimmer > Sent: Wednesday, October 30, 2002 7:42 PM > To: rv-list-matronics.com > Subject: RV-List: Re: legal ride??? > > > > I was wrong. > > The FAR that were listed are correct and they state standard > and that means factory certified. Experimental is a special > airworthiness. > > Further you must be a commercial rated pilot AND in a drug > testing program. The EAA in order to fly Young Eagles got a > waiver from the drug testing requirement and cannot accept donations. > > Cy, > > This appears to mean you can't give a Young Eagles ride in a > homebuilt and you have to have a commercial license. Is this > correct, or did I miss something? > > Mark Schrimmer > RV-9A Wings > Irvine, CA > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: legal ride???
Date: Oct 30, 2002
No you are mixing apples and oranges. Since there aren't any donations, Young Eagles doesn't require a commercial nor standard certification. The EAA has a waiver for the drug testing program which would have been required for anyone giving rides. ----- Original Message ----- From: "Mark Schrimmer" <mschrimmer(at)pacbell.net> Subject: RV-List: Re: legal ride??? > > I was wrong. > > The FAR that were listed are correct and they state standard and that means > factory certified. Experimental is a special airworthiness. > > Further you must be a commercial rated pilot AND in a drug testing program. > The EAA in order to fly Young Eagles got a waiver from the drug testing > requirement and cannot accept donations. > > Cy, > > This appears to mean you can't give a Young Eagles ride in a homebuilt and > you have to have a commercial license. Is this correct, or did I miss > something? > > Mark Schrimmer > RV-9A Wings > Irvine, CA > > ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Control stick, S-bend
Date: Oct 30, 2002
I'm thinking of putting an 'S' bend in the forward stick. I though I saw a diagram of the dimensions on where to place the bends, but I don't remember where. Anybody know? I assume the powder-coat will chip off during the bending....? - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com ________________________________________________________________________________
From: Smcm75(at)aol.com
Date: Oct 30, 2002
Subject: Re: legal ride???
In a message dated 10/30/02 5:56:15 PM Eastern Standard Time, cgalley(at)qcbc.org writes: > > The FAR that were listed are correct and they state standard and that means > factory certified. Experimental is a special airworthiness. > > Further you must be a commercial rated pilot AND in a drug testing program. > The EAA in order to fly Young Eagles got a waiver from the drug testing > requirement and cannot accept donations. > > ----- Original Message ----- > From: "John Helms" <jhelms(at)i1.net> > Do you guys have anything better to do???....how about building airplanes. I have never seen so much BS on any topic! Scott Morrow RV-6A ________________________________________________________________________________
From: KDMIGAS(at)aol.com
Date: Oct 30, 2002
Subject: Re: wing dings
Used stuff called Super=Fil...Two part,light and fluffy and sands out (feathers) nicely.. Got mine locally (seattle) but wicks or aircraft spruce has it.. Also works for filling fiberglass parts and enclosing the ends of rudder and elevator openings when used with a fiberglassed in plate. hope this helps ________________________________________________________________________________
From: "Gary" <rv9er(at)3rivers.net>
Subject: floor stiffeners
Date: Oct 30, 2002
Amit.....one thing that Van's suggests on the floor stiffeners is to be sure and dimple rather than machine countersink those holes. Due to the thickness of the floor skin, some have opted to machine countersink, but Van's discourages it. The other thing I did on my -9A is to install sound deading insulation in the floor. With a thin carpet on top, it comes out about even with the tops of the stiffeners. Hopefully this will cut down on the drumming of the floor. We'll see when I fly. You might ask the techs at Van's whether they have seen any smoking rivets on the 7's or 9's. Good idea on drilling the nutplate holes in the stiffeners before riveting the floor. That would be easier. Gary From: "Amit Dagan" <amitdagan(at)hotmail.com> Subject: RV-List: RV7 floor stiffeners, ATC fuse holders Listers, In the past (looked it up in the archives) there were many cases of smoking rivets in the forward floor area, the ones that hold the floor to the firewall and stiffeners. It was attributed to the engine vibrations, and several methods of stiffening the area even more were raised, including using more rivets, larger (1/8") rivets, both, more stiffeners, double floor boards etc. In the RV7, I am not sure that this issue has been adressed, as one still needs to use 3/32" rivets, same number of stiffeners etc. I DO see that the rivet spacing is ~1" and not 1.25", and that there is a double floor in the center of the cabin (between the two inboard stiffeners). 1. Is that enough ? 2. If the answer to 1. is no, has anyone else done anything about this ? What ? Should I add more stiffeners ? double the floor ? On a totally different subject, if you like the fuse block idea used by the "Aero Electric Connection", check out the "new products" at http://www.pegasusautoracing.com/newproducts.htm and scroll down to Fuse Blocks for ATC Style Fuses. They have good prices for single quantities. And another thing: Heads up, when you are done drilling the stiffeners to the cabin floor, you might want to cleco them to the firewall and F-704 bulkhead, and with the floor off drill the 4 holes for the center section cover (This is the "double floor" between the two middle stiffeners) with the cover in place of course, for the nutplates that go there later. I think it is very easy to reach then, rather then wait untill the floor is riveted. Ah yes, and don't forget to make and drill and dimple the air-vent support angles (0.032") to the side skins before you disassemble the forward fuse. Amit. --- Checked by AVG anti-virus system (http://www.grisoft.com). ________________________________________________________________________________
From: "Bill VonDane" <n8wv(at)hotmail.com>
Subject: Re: Control stick, S-bend
Date: Oct 30, 2002
Larry... I have some info on my website, not sure if it will help though... http://www.vondane.com/tt&i/index.htm#bentcontrolsticks -Bill VonDane RV-8A ~ 74 hrs www.vondane.com ----- Original Message ----- From: "Larry Bowen" <Larry(at)bowenaero.com> Subject: RV-List: Control stick, S-bend I'm thinking of putting an 'S' bend in the forward stick. I though I saw a diagram of the dimensions on where to place the bends, but I don't remember where. Anybody know? I assume the powder-coat will chip off during the bending....? - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com ________________________________________________________________________________
From: "Amit Dagan" <amitdagan(at)hotmail.com>
Subject: double floor for RV-7
Date: Oct 31, 2002
[snip] That double floor in the RV-7 should help with a problem I had. .... I missed that part about the double floor. Thats standard on the -7? How about that! [snip] Sorry if I wasn't clear: Only the section between the two inboard floor stiffener is "doubled". This is done by a cover that runs from the fuel selector box, covering the fuel line, to the fire wall, where the auxiliary fuel pump is located. The cover is attached with screws and nutplates to the firewall recess, floor stiffeners and fuel selector valve box. Hope this clarifies it. Amit. ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Oct 30, 2002
Subject: Re: Wing Dings
On our RV-4 I used "Evercoat 'RAGE" auto body microlite filler on all the little metal dings. It has microballons to make it light and works well on all the fibreglas filling . It sands nice and is really handy to get at your local auto parts store. At about 28 bucks a gallon , maybe cheaper too. RV-4 , N1191X , Flying Now Charleston, Arkansas ________________________________________________________________________________
From: "Rob W M Shipley" <Rob(at)RobsGlass.com>
Subject: Boston tea party musings ....
Date: Oct 30, 2002
RV-List message posted by: "Marcus Ward" "In 1773, Britain's East India Company was sitting on large stocks of tea that it could not sell in England." How do you like taxation now there is representation? Heh! Heh! Rob ( the expat ) Rob W M Shipley. RV9A fuselage. N919RV resvd. ________________________________________________________________________________
Subject: Fuel Cap Deal Instructions
Date: Oct 30, 2002
From: "Brandon Dixon" <dixon(at)cs.ua.edu>
Sorry that you were disappointed. I got my caps back, and I was pleased. Maybe your "trophy shop" could have done the job just as well. I was glad to send mine to a shop that I KNEW would do the job right. I didn't have to explain to Steve Davis what I needed, or get him to do it again on new caps after a screw up. You can polish the caps to make them look like the photo on Paul's website, just a little elbow grease. Brandon Dixon RV-7A Finish Kit (Well ... almost) -----Original Message----- From: Wayne R. Couture [mailto:commando@cox-internet.com] Subject: Re: RV-List: Fuel Cap Deal Instructions <commando@cox-internet.com> Hey folks, Just an update on the fuel caps I received back from Steve this week. Unfortunately, I was not impressed. They did not look anything like the picture Paul posted to this list a few weeks ago and more like something I could have had done at a local trophy shop for a lot less money. I enjoy this list mostly for the information it provides on suppliers for RV related items. I just don't think this was such a great deal. Sorry Steve. Wayne RV-8a working on cabin ________________________________________________________________________________
Date: Oct 30, 2002
From: Bobby Hester <bhester(at)apex.net>
Subject: Re: Fuel Cap Deal Instructions
"Wayne R. Couture" wrote: > > Hey folks, > Just an update on the fuel caps I received back from Steve this week. > Unfortunately, I was not impressed. They did not look anything like the > picture Paul posted to this list a few weeks ago and more like something I > could have had done at a local trophy shop for a lot less money. > I enjoy this list mostly for the information it provides on suppliers > for RV related items. I just don't think this was such a great deal. Sorry > Steve. > > Wayne > RV-8a > working on cabin Mine looked just like the picture he posted except for the text being turned the right direction, like Paul said. I had mine done back in the spring and love the way they look, and the cost was just right! I'll try to remember to put a picture on my site so everyone can decide for their self. Here is the link Paul had in his message: http://www.lacodeworks.com/besing/wings.htm it looks as though he may have colored the letters to make them more visable. Can you show us a picture of your caps, so we can see how they are different? -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
From: "Mike" <mike(at)bmnellis.com>
Subject: Fuel Cap Deal Instructions
Date: Oct 31, 2002
I, too, am happy with how mine came out. Take a look at this picture to see how you can highlight the text to improve (in my opinion) the look of the caps. I will polish these caps later. Mike Nellis RV-6 Fuselage N699BM 1947 Stinson 108-2 NC9666K http://bmnellis.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Bobby Hester > Sent: Wednesday, October 30, 2002 11:16 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Fuel Cap Deal Instructions > > > "Wayne R. Couture" wrote: > > <commando@cox-internet.com> > > > > Hey folks, > > Just an update on the fuel caps I received back from Steve > this week. > > Unfortunately, I was not impressed. They did not look anything like the > > picture Paul posted to this list a few weeks ago and more like > something I > > could have had done at a local trophy shop for a lot less money. > > I enjoy this list mostly for the information it provides > on suppliers > > for RV related items. I just don't think this was such a great > deal. Sorry > > Steve. > > > > Wayne > > RV-8a > > working on cabin > > Mine looked just like the picture he posted except for the text > being turned the > right direction, like Paul said. > > I had mine done back in the spring and love the way they look, > and the cost was > just right! I'll try to remember to put a picture on my site so > everyone can > decide for their self. > > Here is the link Paul had in his message: > http://www.lacodeworks.com/besing/wings.htm it looks as though he may have > colored the letters to make them more visable. > > Can you show us a picture of your caps, so we can see how they > are different? > > > -- > 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 31, 2002
From: Jim Oke <wjoke(at)shaw.ca>
Subject: Re: Calibrated airspeed (Was RV-6A airspeed problem)
Mark; If you take your ASI to an instrument lab they will hook it up to a very accurate manometer and apply xx.xxx inches of water (or mercury) pressure to it and convert this pressure to an airspeed reading. See Kevin Horton's response - he has a nice page with all the mathematical intricacies of this worked out. The "quick and dirty" way would be to take a second ASI and tee the pitot side into your ASI and use some method of applying pressure (squeeze bulb, rolled up tubing, etc.) and see if the resulting readings agree. If they do, good. If not, then you know one or the other is bad and further investigation is needed. It is probably a good idea to do this before a first flight to make sure that your ASI is in the ball park - especially if you are going to base your flying technique on information (such as approach speeds) from other builders. Doing an inflight calibration to assess the pitot and static errors is actually a long drawn out process and can take a long series of flights to accomplish. Sometimes a "tower fly-by" is done - the idea being that if your fly precisely level with a feature (tower) of a known altitude, the altimeter should read the known altitude - if it doesn't (and the altimeter has been checked and precisely calibrated on it own) then the error is assumed to be in the static system. Alternatively, fly formation with another aircraft with a known altimeter - static error and see if the readings agree. Sometimes a "trailing bomb" (actually a weighted body with a static line running back to the aircraft) is towed inflight - the idea being that the test static source will be well clear of the aircraft's pressure flow field and be an accurate static pressure value. Any difference between the "bomb" static pressure and the aircraft's static pressure should then be due to static error in the aircraft. Often a test aircraft will be set up with a very long pitot tube extending well forward of the aircraft into presumably undisturbed air to get a "good" pitot pressure to compare with the aircraft's pitot system. Kevin also suggests a GPS based method to sort out the difference between CAS and IAS which is what most of us are interested in. One this is known and ASI error is known then you can work back and figure out the static pressure error for various airspeeds (and weights - often the error is dependant on angle of attack which changes with weight, etc. not a big factor for RV size aircraft though). Jim Oke RV-6A Winnipeg, MB ----- Original Message ----- From: "Mark Schrimmer" <mschrimmer(at)pacbell.net> Subject: RV-List: Calibrated airspeed (Was RV-6A airspeed problem) > > the number read off the ASI face is the "indicated a/s", which has to > be corrected for both instrument error and pitot and (mostly) static port > position error to get "calibrated A/S" > > > Jim, > > What is the procedure for calibrating an airspeed indicator? Is this > typically done during the first few test flights? > > Mark Schrimmer > RV-9A Wings > Irvine, CA > > ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Oct 31, 2002
Subject: Re: Exxon Elite
Modern synthetic oils and auto oils in general whether synthetic or not are not formulated to suspend lead in leaded fuels. The lead will precipitate out and form harmful deposits. Mobil discovered that even in a supposed Aviation formulation of Mobil 1 that this would happen. Synthetic oils could be engineered that could work with leaded fuels but the market is so small and the demise of 100LL being on the horizon that it would not be profitable. What if you run only unleaded auto fuel? well, I suspect Mobil 1 would work just fine but since these engines cost so much dinero and the consequences of failure so dramatic and the need to have a reliable engine to out manuver patroling F16's in No Fly Zones I would stick with an Aviation product. Do Not Archive. JR ________________________________________________________________________________
From: "Jim Sears" <sears(at)searnet.com>
Subject: Re: Drill and dimple vs just dimple
Date: Oct 31, 2002
> I know that "did you match drill the holes before riveting?" will become > one of the questions on my checklist if I ever buy a finished RV from > someone. If the answer is "no," I won't be buying. > > -RB4 Since I know of two airplanes that have either not been match drilled, or havn't been totally match drilled, I'll have two examples to form my own conclusions from. As for not buying one for that reason, I'm not sure I'd be that picky. I'd be more worried about such things as systems installations, engine installations, etc. I've seen some of that kind of thing that worries me a lot more than holes not being match drilled. In fact, some of those installations can get downright scarey. Some have killed some of our members. Now, if I see cracks forming all over the place, that's a different matter. With the low number of hours we put on our aircraft per year, I don't think that's going to be an issue. Jim Sears in KY ________________________________________________________________________________
Date: Oct 31, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Calibrated airspeed (Was RV-6A airspeed problem)
> >the number read off the ASI face is the "indicated a/s", which has to >be corrected for both instrument error and pitot and (mostly) static port >position error to get "calibrated A/S" > > >Jim, > >What is the procedure for calibrating an airspeed indicator? Is this >typically done during the first few test flights? > >Mark Schrimmer >RV-9A Wings >Irvine, CA > Second attempt - the first one still hasn't shown up after 11 hours. Mark, I've got quite a bit of info on the Flight Test Links part of my web site that deals with this issue. The old version of that page is at: http://members.rogers.com/khorton/ftlinks.html I'm working on a new version of that page at: http://go.phpwebhosting.com/~khorton/rv8/links.php See the Flight Test - Pitot-Static Cals section. In particular see: http://members.rogers.com/khorton/rvlinks/ssec.html Short version follows: The total error in the airspeed indication is the sum of a number of errors: 1. instrument error - the errors due to imperfections in the instrument itself. 2. static source position error - the static source is not located in a position that has the same pressure as the ambient pressure. This error will also affect the altimeter. 3. pitot source position error - the pitot source may be poorly located so that it is not sensing the correct pitot pressure. 4. errors due to leaks in the pitot or static system. The leaks should be found by a good leak check. Most people who do flight testing to determine the airspeed error don't really care about figuring out how much of the airspeed error is due to each source - they only want to know what the total amount of error is. This is probably OK for VFR flying, but for IFR I would want to know what the static source error was because this would affect the accuracy of the altimeter, which could be an issue during approaches. Also, if you every have to change the airspeed indicator you would want to do the flight tests again because you wouldn't know how the instrument error of the new ASI compared to the old one. It is possible to use a water manometer to determine the instrument error. See: http://www.eaa1000.av.org/technicl/instcal/instcal.htm http://members.rogers.com/khorton/rvlinks/asi.zip The pitot source error is normally negligible. Once you know the total error from flight tests, and the instrument error, you can calculate the static source error, which lets you figure out the effect on the altimeter. If anyone wants to do the proper testing I am prepared to work with them to help them do a good test and to analyze the data. -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
Date: Oct 31, 2002
From: Doug Gray <dgra1233(at)bigpond.net.au>
Subject: Re: Calibrated airspeed (Was RV-6A airspeed problem)
Kevin Horton wrote: > > If anyone wants to do the proper testing I am prepared to work with > them to help them do a good test and to analyze the data. > Hey guys this is a generous offer and a golden opportunity to have a highly qualified test pilot advise and crunch your flight test numbers. If we were in the commercial world you might buy an engine for what this offer is worth. Thanks Kevin, Doug Gray RV6 Fuselage, goes on forever... ________________________________________________________________________________
Date: Oct 31, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: GPS for Altitude hold (was Rate of climb - flt test)
Second attempt - the first one still hasn't shown up after 11 hours. Two issues to wrestle with: 1. ATC wants us at particular barometric altitudes, which will not be the same as actual altitudes. So if we wanted to fly at 6,000 ft on our altimeter, we need to understand that the GPS altitude will differ from that. But, it should be practical to level off at the desired altitude using the altimeter, then tell your GPS altitude hold gizmo to memorize the current GPS altitude and hold it. The difference between GPS altitude and barometric altitude would slowly vary with time, as the satellite geometry changed (which would make the GPS altitude move up and down) and you travelled to areas with different local pressures and temperatures (which would make the barometric altitude move up and down). So you might have to reset the GPS altitude hold reference once in a while. 2. There is a certain amount of noise in the GPS altitude calculation - i.e. even if the actual altitude is constant, the GPS altitude may move up and down a bit. The amount of noise probably varies with different GPS units, satellite geometry, etc. I did an experiment with my hand held GPS a couple of nights ago - I went out in my driveway and stood there for a few minutes and watched the GPS altitude display. It varied in a range of about 30 ft total. If the altitude hold function was trying to keep the GPS altitude constant the aircraft would be moving up and down over a 30 ft range which might not be comfortable. I don't know whether a more expensive GPS box would have less noise in its GPS altitude or not. So this altitude noise may or may not be a problem. For extra points you could mount GPS antennae on the nose and tail, and use differential GPS techniques to develop an attitude hold function. The attitude information could be used to damp the system response to noise in the GPS altitude, and attitude hold would be a nice extra piece of functionality anyway. The use of differential techniques to calculate attitude has been done in a research setting, but I don't think anyone was developed an actual product that works this way. See: http://einstein.stanford.edu/gps/PDF/att_and_displ_4ga_akb96.pdf Kevin Horton > >This being the case, is there a technical or practical argument >against using GPS >altitude data to drive an altitude hold device? Obviously useful course (or >track or heading, but I don't want to start that up again !) data >derived from >GPS can keep the nose pointed toward a destination, why not do the same to >control pitch trim? I sure don't possess the technical savvy to >attempt such a >device, but those who do might profit from such an offering. I had high hopes >for the EZ-trim but it appears to be experiencing growing pains- any new >developments here? > >From The PossumWorks in TN >Mark Phillips > >Kevin Horton wrote: > >> David is correct that GPS altitude is probably more accurate than >> barometric altitude most of the time, if we are more than a few >> thousand feet above the location where the altimeter setting came >> from. If our altitude is close to the site where the altimeter >> setting came from, the altimeter is likely more accurate than the GPS. >> >> I'm not sure I would agree with the suggestion to time the GPS >> altitude change instead of timing the barometric altitude change >> though. In my experience, GPS altitude fluctuates quite a bit, so >> I'm not sure that timing the rate of change of GPS altitude will lead >> to an accurate result. GPS is much less accurate vertically than it >> is horizontally. I believe that we can get more accurate results by >> timing the rate of barometric altitude change, and then correcting > > for non-standard temperature. > ________________________________________________________________________________
From: "Jim Nolan" <JimNolan(at)kconline.com>
Subject: Digitrak
Date: Oct 31, 2002
Just a note to express my satisfaction with the TruTrak Digitrak Autopilot. It will track anything that my gps has in it and it doesn't care if it's 180 degrees in back of you. It'll turn around and be locked on within a couple miles going at a speed of 160. It's great for Radar vectors to an approach because it has the magnetic headings stored in memory. ATC tells me what direction to take, I lean on the direction button, stop it when I get to the direction they want and go back to reading my approach plate until they give me another heading. You never re-level the airplane because that's stored in memory also. I turn mine on after liftoff while in a turn and it'll keep a standard rate turn going, then, level the wings and intercept the radial to my gps destination. It's also nice to know that with the gps off, the heading displayed in track mode of the autopilot is the actual magnetic heading you're on. It's easier to see the readout on the autopilot than it is to see the direction the whiskey compass has. I have a 2001 APOLLO, so on a VOR approach, you have to be close to the published inbound coarse for the autopilot to lock on. If you get too far off coarse the GPS will quit delivering information to the autopilot. The GPS automatically decreases course width from 5mi. to 1mi to .3mi. as you get further into the approach. If you stray out of these coarse widths the GPS information to the autopilot is cut off. I guess they don't want you shooting an approach to a particular airport if your not there. There isn't anything wrong with the autopilot, it's just that the signal to it is gone, so it reverts back to track mode. It's really a good thing that it does. Another benefit was the ability to talk to Jim and Chuck at Trutak and have them be patient with me while I was learning how to use the Digitrak. It's not that the Digitrak is hard to understand, it's just that as I get older I need more pictures to help me understand things. Hope this has been helpful to those considering an autopilot. Jim Nolan N444JN Warsaw, In. ________________________________________________________________________________
From: "Garrett Bray" <braygarrett(at)hotmail.com>
Subject: Re: wing dings
Date: Oct 31, 2002
One way to avoid dings in the top wing skins is to rivet them on first using the back riveting method, then rivet the bottom skins on by the "reach inside with bucking bar until your arm bleeds" method. The dings caused are then not visible except to very short people. Thats how I did it. Also there is probably some info in the archives about the method to do the last inboard ribs without using pop rivets. It worked well for me. Gary Bray RV-6 Get a speedy connection with MSN Broadband. Join now! http://resourcecenter.msn.com/access/plans/freeactivation.asp ________________________________________________________________________________
Subject: RV trip in need
Date: Oct 31, 2002
From: "Gannon, Terence" <Terence.Gannon(at)trican.ca>
While it is just possible that I haven't had all my synapses connecting for the last couple of years, and somehow the RV-10 has been kitted and completed by a few people already while I was 'sleeping', how is that anybody was planning on giving Scott **and his father** a ride anyway? I suspect that if you manage to get through the whether or not it's LEGAL to give him a ride, and whether or not you're INSURED to give him a ride, you might just get nailed on a bad weight and balance calculation, or, at the very least, the lack of one seatbelt. Just a thought...;-) Cheers... Terry in Calgary RV-6 S/N 24414 "Fuselage Inventory" -----Original Message----- From: BrownScottA(at)aol.com [mailto:BrownScottA(at)aol.com] Subject: RV-List: RV trip in need Listers, Are there any guys out there that will be travelling soon from Fla to or thru the mid Texas area that wouldn't mind having their gas paid for? My father and I need a ride to the San Angelo, TX area and are wondering if we could get a ride there. We will pick up the tab. Scott ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: Fuel Cap Deal Instructions
Date: Oct 31, 2002
Strange that you didn't like them. Last time we did them everyone was really impressed! Also, most trophy shops can't engrave with letters like that. They only engrave little brass plates with very shallow engraving, almost like an electric pencil type engraver you can get at Wal Mart. As for the letters are concerned, here is how it is done: Take some laquer paint and paint over and inside the letters. Then take some laquer thinner and soak it into the top of an old phone book. Rub the cap around flat on the phone book, and you will be left with paint inside the letters. Or, if this sounds to messy for you, get a black china pencil (grease pencil) and color them in. Then use alcohol to rub off the excess. We used to do this in the aerospace industry with launch control panels and such. Grease pencil stays inside the letters without a problem. As far as polishing is concerned, I used a micro mesh kit. You can get it from spruce. Basically it is steps of sandpaper starting at 1200 and going to 6000. A little polishing compound and you are done. The only problem with this process is, this alluminum will oxidize. It will not stay shiny for too long. It will dull over time. The other option is you could paint them, then fill with black grease pencil. This looks really nice, actually. I'm sorry if it appeared that Steve was going to polish and paint them. I guess I should have been more clear that he was just engraving them. It's only $24, so I don't know what else should be done for that price. 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: "Bobby Hester" <bhester(at)apex.net> Subject: Re: RV-List: Fuel Cap Deal Instructions > > "Wayne R. Couture" wrote: > <commando@cox-internet.com> > > > > Hey folks, > > Just an update on the fuel caps I received back from Steve this week. > > Unfortunately, I was not impressed. They did not look anything like the > > picture Paul posted to this list a few weeks ago and more like something I > > could have had done at a local trophy shop for a lot less money. > > I enjoy this list mostly for the information it provides on suppliers > > for RV related items. I just don't think this was such a great deal. Sorry > > Steve. > > > > Wayne > > RV-8a > > working on cabin ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Oct 31, 2002
Subject: Re: Calibrated airspeed (Was RV-6A airspeed problem)
Kevin: I am in the process right now trying to calibrate my two airspeed indicators ... one from Vans and the Rky Mtn uEncoder. I used the blood pressure bulb method last night and I am getting two different readings. At 35 in Hg on the blood pressure gauge I am getting 126 knots on the Vans gauge and 162 knots on the uEncoder. Not sure why I am getting such a big difference. Len Leggette RV-8A N901LL (res) Greensboro, N.C. Flying !! ________________________________________________________________________________
Subject: rivet dings and tricks
Date: Oct 31, 2002
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
********what is the best way to deal with dings from the rivet gun on the top wing surface? Filler? What kind?*********** Gosh, I'd really like to hop into the discussion about whether Scott is gonna be somebody's Prison Daisy for reimbursing somebody for gas, but I think I'll address Adrian's question instead. If the skin is simply recessed a bit from normal riveting, don't be afraid to use a block of wood (or long rivet set) and a hammer to tap it out from the back side. You can really improve the looks of your bird with this simple technique. If you've made a real live dent and it's just in the skin, but not over a flange, you can dolly it out a bit with your bucking bar and flush rivet set. If the dent is still offensive, drill a hole right in the middle of it where the dent is worst, take a scrap of .063 and match drill and countersink it, rivet it behind the dent. Use 2 rivets if necessary. The 063 will hold the skin flat and the dimpling operation will soak up some of the dent. Obviously this fix is not for the faint of heart, but it works. If somebody questions you later about the unusual placement of those rivets... tell them that those rivets hold the " altitude compensation solenoid for your beta version flight data transducing oscillator" or just beat them senseless. ;-) A neat trick to help make really flat rivet lines is to put a thin layer of JBWeld between your skins, cleco every hole, and drive the rivets after it sets. The JBWeld (3M makes a similar product) acts as a perfect shim to suck up any misfitting between the sheets. I can sense lots of flames coming.... no, I'm not advocating using JBWeld to make up for stupid building mistakes, only as a device to make properly fitting parts fit better. Filler... no thanks. I worked hard to put those dents there and there they will stay! Vince F-1H Rocket ________________________________________________________________________________
From: "Steve J Hurlbut" <sjhdcl(at)kingston.net>
Subject: Firewall fuel fittings
Date: Oct 31, 2002
Is there any concern mounting aluminum fuel fittings on the firewall? I know this is the standard in most aircraft and I've done it before on another aircraft but the stainless steel firewall holes are very sharp and may cause some chaffing on the fuel fittings. Any concerns from others here? Steve Hurlbut RV7A Subaru ________________________________________________________________________________
From: "Jordan, Mel" <jordan_mel(at)ti.com>
Subject: N6JX first flight
Date: Oct 31, 2002
I am very pleased to report that RV-6A N6JX flew for the first time this morning at KTUS (Tucson). N6JX is a QB kit, 60289, and the first builders log entry was on Oct. 15, 1998, so four years and 2K hours later, I have an airplane!! The plane flew great, no heavy wing, rudder half ball out at cruise, absolutely no squawks on the plane, systems or engine. After a post flight inspection, it will be ready to go again. N6JX has a new Lyc. O-360-A1A from Van's equipped with airflow performance Fuel Injection. Hartzell CS prop, Garmin GNC300XL and GTX327 radios, full gyro panel and Digitrak autopilot. She doesn't have paint or wheel pants yet, so speed was not yet up to par (145kts indicated), but she climbed like a rocket in the cool desert morning. What a kick. The tower was great and let me orbit right over the airport for the half hour duration of the flight. Did slow flight with half and full flaps and generally checked out handling, which was delightful. Landing was just like Mike Seager taught me, simple and easy. Everything was simply perfect! I had a lot of help from fellow builders here; Greg Johnson (RV-6), Gene Gaddis (RV-8), Alan Thomas (RV-6), and Paul Conn (Fairchild 24). It was definitely worth the time and effort. This has to be one of the best feelings a person can experience, having this machine you built take flight and carry you into such a beautiful blue sky. I think I'll go do it again after lunch! Mel Jordan RV-6A N6JX Tucson, AZ n6jx(at)earthlink.net ________________________________________________________________________________
Date: Oct 31, 2002
rv7-list(at)matronics.com, rv8-list(at)matronics.com, rv9-list(at)matronics.com, rv-list(at)matronics.com
From: Matt Dralle <dralle(at)matronics.com>
Subject: How To Wire a "Dual-Rate" Electric Trim System...
Hi Listers, I've recently received a number of requests from builders regarding how to wire up a "dual-rate" system for their electric trim installation. The concept is that in cruse configuration the trim speed would be slow and during flaps down configuration the trim speed would be fast. I've draw up a schematic diagram that shows how to accomplish this using two Matronics Governor MkIII units, a 12v relay, and an extra switch. With the flaps up, the "fast" Governor MkIII is switched in, and when the flaps are down, the "slow" Governor MkIII is switched in. I would recommend using the highest quality, sealed relay available for this installation. Here is the Dual-Rate PDF document: http://www.matronics.com/GovernorMkIII/DualRate-GovernorMkIII-Installation.pdf and here is the Governor MkIII website: http://www.matronics.com/GovernorMkIII If you have any questions on the wiring diagram, feel free to email me directly at: dralle(at)matronics.com Best regards, Matt Dralle Matt G Dralle | Matronics | PO Box 347 | Livermore | CA | 94551 925-606-1001 V | 925-606-6281 F | dralle(at)matronics.com Email http://www.matronics.com/ WWW | Featuring Products For Aircraft ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Oct 31, 2002
Subject: Re: N6JX first flight
Congrats Mel .. know how you feel ... I just flew my 8A last Sunday !!! Len Leggette RV-8A N901LL (res) Greensboro, N.C. Flying !! ________________________________________________________________________________
Date: Oct 31, 2002
From: P M Condon <pcondon(at)mitre.org>
Subject: Re: Fuel Cap Deal Instructions (Bad Work)
My caps were done poorly also. Looks like a grade-school helper did it. Took a long time to get done and didn't look professional. Poor letter edge defination, inconsistant depth, vise/tooling marks and poor letter allignment. Better then using a electric buzz pencil, but not by much. Very disappointed. <commando@cox-internet.com> Hey folks, Just an update on the fuel caps I received back from Steve this week. Unfortunately, I was not impressed. They did not look anything like the picture Paul posted to this list a few weeks ago and more like something I could have had done at a local trophy shop for a lot less money. I enjoy this list mostly for the information it provides on suppliers for RV related items. I just don't think this was such a great deal. Sorry Steve. Wayne RV-8a working on cabin ----- Original Message ----- ________________________________________________________________________________
From: "Gary" <rv9er(at)3rivers.net>
Subject: deburr
Date: Oct 31, 2002
They also tested that wing to destruction in the shop. No flight time was ever put on it. Gary From: Mark Schrimmer <mschrimmer(at)pacbell.net> Subject: RV-List: Drill and dimple vs just dimple You folks know that Van did advertise, or reported in the RVator, that they built the wings without ever picking up a drill. Well, folks, that tells me it's OK to do that if they don't say it's not when they advertise it that way. Maybe they did; but, I don't ever remember their doing it. Jim, I believe the story explained that the reason a prototype set of RV-9A wings was built without using a drill was to test the accuracy of the pre-punched holes. The same story also recommended that builders use a drill to minimize the possibility of cracks forming. Mark Schrimmer RV-9A Wings --- Checked by AVG anti-virus system (http://www.grisoft.com). ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Fuel cap labelling regs?
Date: Oct 31, 2002
Can somebody point me in the right direction...I'm looking for the FAR that states exactly how fuel filler caps should be labelled or placarded, and all I could find was mention in Part 23 that the word "Avgas" and the minimum acceptable octane must be specified. But I'm not sure if this applies to amateur-built aircraft. Plus, it looks like Steve Davis' engraving doesn't even say "Avgas" on it (I was basing that off this photo for reference: http://bmnellis.com/images/DCP01408.JPG). With all the confusion over the quality of having fuel caps engraved, I'm wondering if it's 100% required that the fuel caps be labelled in some form. I assume so, but what's the reg, and what's the simplest way of accomplishing this? )_( Dan RV-7 N714D (fuselage) http://www.rvproject.com ________________________________________________________________________________
From: "Cole, Ed" <Ed_Cole(at)maximhq.com>
Subject: Fuel Cap Deal Instructions (Bad Work)
Date: Oct 31, 2002
As I recall, the last time Steve did these he also painted the lettering. This was a couple of years ago, max. Mine looked great when they were returned. I believe the price was the same at the time. Ed Cole RV6A N2169D Flying RV6A N648RV Finishng > -----Original Message----- > From: P M Condon [SMTP:pcondon(at)mitre.org] > Sent: Thursday, October 31, 2002 11:05 AM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Fuel Cap Deal Instructions (Bad Work) > > > > My caps were done poorly also. Looks like a grade-school helper did it. > Took a long time to get done and didn't look professional. Poor letter > edge defination, inconsistant depth, vise/tooling marks and poor letter > allignment. Better then using a electric buzz pencil, but not by much. > Very disappointed. > > > <commando@cox-internet.com> > > Hey folks, > Just an update on the fuel caps I received back from Steve this > week. > Unfortunately, I was not impressed. They did not look anything like the > picture Paul posted to this list a few weeks ago and more like something > I > could have had done at a local trophy shop for a lot less money. > I enjoy this list mostly for the information it provides on > suppliers > for RV related items. I just don't think this was such a great deal. > Sorry > Steve. > > Wayne > RV-8a > working on cabin > ----- Original Message ----- > > > > > Maxim Home Page: http://www.maxim-ic.com Products Page: http://www.maxim-ic.com/MaximProducts/products.htm New Products: http://dbserv.maxim-ic.com/new_products.cfm Datasheets: http://dbserv.maxim-ic.com/l_datasheet3.cfm The information contained in this message is confidential and may be legally privileged. The message is intended solely for the addressee(s). If you are not the intended recipient, you are hereby notified that any use, dissemination, or reproduction is strictly prohibited and may be unlawful. If you are not the intended recipient, please contact the sender by return e-mail and destroy all copies of the original message. ________________________________________________________________________________
Date: Oct 31, 2002
From: Mark Phillips <ripsteel(at)edge.net>
Subject: Brake Fluid Reservoir Loc. on a tip-up
Howdy List- Anyone installed their reservoir on the rear of the subpanel so it can be accessed when the canopy is open? I see one less hole in the firewall, more space on firewall, easier to check level and detect leaks (why is my sock wet?) & the vent could be run off with a little tube to somewhere... Other pros & cons, please! From The PossumWorks in TN Mark ________________________________________________________________________________
From: "Mike Robertson" <mrobert569(at)hotmail.com>
Subject: Re: Fuel cap labelling regs?
Date: Oct 31, 2002
Dan, From a legal standpoint FAR Part 23 does not apply, BUT....your local inspector/DAR should not/will not issue your aircraft an Airworthiness Certificate unless somewhere in the near vicinity of the fuel filler cap (not necessarily on the cap itself) is the word "AVGAS", the minimum fuel octane and the tanks fuel capacity, in gallons. The closest FARs for this are 23.1557(c)(1), and parts of 23.1555(d) in that most inspectors will accept the fuel quantity to be marked near the fuel filler instead of at the fuel selector, as stated in the FAR. Mike Robertson Das Fed RV-8A, 6A and 9A >From: "Dan Checkoway" <dan(at)rvproject.com> >Reply-To: rv-list(at)matronics.com >To: , >Subject: RV-List: Fuel cap labelling regs? >Date: Thu, 31 Oct 2002 11:48:05 -0800 > > >Can somebody point me in the right direction...I'm looking for the FAR that >states exactly how fuel filler caps should be labelled or placarded, and >all >I could find was mention in Part 23 that the word "Avgas" and the minimum >acceptable octane must be specified. But I'm not sure if this applies to >amateur-built aircraft. Plus, it looks like Steve Davis' engraving doesn't >even say "Avgas" on it (I was basing that off this photo for reference: >http://bmnellis.com/images/DCP01408.JPG). > >With all the confusion over the quality of having fuel caps engraved, I'm >wondering if it's 100% required that the fuel caps be labelled in some >form. >I assume so, but what's the reg, and what's the simplest way of >accomplishing this? > >)_( Dan >RV-7 N714D (fuselage) >http://www.rvproject.com > > Choose an Internet access plan right for you -- try MSN! http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
Date: Oct 31, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Calibrated airspeed (Was RV-6A airspeed problem)
> >Kevin: > >I am in the process right now trying to calibrate my two airspeed indicators >... one from Vans and the Rky Mtn uEncoder. I used the blood pressure bulb >method last night and I am getting two different readings. > >At 35 in Hg on the blood pressure gauge I am getting 126 knots on the Vans >gauge and 162 knots on the uEncoder. Not sure why I am getting such a big >difference. > >Len Leggette RV-8A Len, We may have a units problem here. 35 inches of mercury would be over 700 knots. 35 mm of mercury would be about 168 kt. 162 kt would be about 32.4 in Hg. I'm not sure how accurate the gauge on the blood pressure cuff is, so it is pretty hard to say whether the uEncoder is accurate or not, but the Van's gauge certainly appears suspect. I think you would get better accuracy from a water manometer, as long as you can be sure to get all the little air bubbles out. -- Kevin Horton RV-8 (cowling, wing tip lights) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
Date: Oct 31, 2002
From: Tedd McHenry <tedd(at)vansairforce.org>
Subject: Re: deburr
> I believe the story explained that the reason a prototype set of RV-9A wings > was built without using a drill was to test the accuracy of the pre-punched > holes. The same story also recommended that builders use a drill to minimize > the possibility of cracks forming. That is exactly the story I got from an engineer at Van's who was involved in the testing. Tedd McHenry Surrey, BC -6 wings ________________________________________________________________________________
Date: Oct 31, 2002
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: GPS Accuracy Discussion - skip if you don't care to
read about it > >>it's a matter of satellite constellation geometry. all the >>satellites are above the horizon. that means that position measurement in >>the vertical is really only measured from one side. > >True, but what's the probablility that *all* the satellites are near the >horizon? Low. Actually, you stand a better chance of picking up the >satellites from ~30 elev up to 90, giving you little horiz vs verical >preference in my thinking. > >Lets assume one's directly overhead two are 60 and two are 30 above the >horizon, which is not that untypical from what I've observed. In this case, >the horizontal position would be almost as accurate as the vertical. > >Maybe I'm not seeing it, but I believe it's just basic geometry. In a very >simplified manner of discussion, you have 100% of the vertical component >from the 90, 86% of the 2 at 60 and 50% of the 2 at 30. I know, I >know... your measuring time differences, not distances. But it just seems >to me that horizontal is no more accurate than vertical, on average. > >if I'm still missing the boat, send me a link to something I can read. > >Bryan Jones -8 >Pearland, Texas > Bryan, First, there is no question that the vertical accuracy of GPS is worse than the horizontal accuracy. There have been many, many studies which collected GPS data, and they always clearly show that this is the case. So there is no point in trying to argue otherwise. GPS accuracy data: One years worth of data of horizontal and vertical accuracy: http://mywebpages.comcast.net/dmilbert/handacc/accur.htm More accuracy data - another GPS receiver: http://mywebpages.comcast.net/dmilbert/handacc/accur2.htm But, it is always instructive to try to understand why something is the way it is. I am not confident enough of my understanding of the issues vis-a-vis vertical vs horizontal accuracy to want to try to offer a better explanation than zilik(at)direcpc.com posted. So, I goggled the net, and found the following for your reading pleasure: Relatively simple explanation of why vertical accuracy is less than horizontal: http://www.eomonline.com/Common/Archives/May97/gilbert.htm How GPS accuracy is described: http://www.romdas.com/technical/gps/gps-acc.htm More than you ever wanted to know about GPS: http://www.edu-observatory.org/gps/gps.html Happy reading, -- Kevin Horton RV-8 (baffles, induction air, oil cooler) Ottawa, Canada http://members.rogers.com/khorton/rv8.html ________________________________________________________________________________
From: "Mike" <mike(at)bmnellis.com>
Subject: Fuel cap labeling regs?
Date: Oct 31, 2002
Hi Mike, What are the Subaru guys going to do who don't run AVGAS in their auto engines? Mike Nellis RV-6 Fuselage N699BM 1947 Stinson 108-2 NC9666K http://bmnellis.com > > Dan, > > From a legal standpoint FAR Part 23 does not apply, BUT....your local > inspector/DAR should not/will not issue your aircraft an Airworthiness > Certificate unless somewhere in the near vicinity of the fuel filler cap > (not necessarily on the cap itself) is the word "AVGAS", the minimum fuel > octane and the tanks fuel capacity, in gallons. The closest FARs > for this > are 23.1557(c)(1), and parts of 23.1555(d) in that most inspectors will > accept the fuel quantity to be marked near the fuel filler > instead of at the > fuel selector, as stated in the FAR. > > Mike Robertson > Das Fed > RV-8A, 6A and 9A > > > >From: "Dan Checkoway" <dan(at)rvproject.com> > >Reply-To: rv-list(at)matronics.com > >To: , > >Subject: RV-List: Fuel cap labelling regs? > >Date: Thu, 31 Oct 2002 11:48:05 -0800 > > > > > >Can somebody point me in the right direction...I'm looking for > the FAR that > >states exactly how fuel filler caps should be labelled or placarded, and > >all > >I could find was mention in Part 23 that the word "Avgas" and the minimum > >acceptable octane must be specified. But I'm not sure if this applies to > >amateur-built aircraft. Plus, it looks like Steve Davis' > engraving doesn't > >even say "Avgas" on it (I was basing that off this photo for reference: > >http://bmnellis.com/images/DCP01408.JPG). > > > >With all the confusion over the quality of having fuel caps engraved, I'm > >wondering if it's 100% required that the fuel caps be labelled in some > >form. > >I assume so, but what's the reg, and what's the simplest way of > >accomplishing this? > > > >)_( Dan > >RV-7 N714D (fuselage) > >http://www.rvproject.com > > > > > > > Choose an Internet access plan right for you -- try MSN! > http://resourcecenter.msn.com/access/plans/default.asp > > ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: Brake Fluid Reservoir Loc. on a tip-up
Date: Oct 31, 2002
Never thought about that, but sure makes sense to me. Just be real careful when filling or back bleeding the brakes so you don't ruin your interior! Also, brake fluid is a no-no around paint, so be sure the area isn't painted, or you are just real careful with the brake fluid. 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: "Mark Phillips" <ripsteel(at)edge.net> Subject: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > Howdy List- > > Anyone installed their reservoir on the rear of the subpanel so it can > be accessed when the canopy is open? I see one less hole in the > firewall, more space on firewall, easier to check level and detect leaks > (why is my sock wet?) & the vent could be run off with a little tube to > somewhere... Other pros & cons, please! > > >From The PossumWorks in TN > Mark > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Brake Fluid Reservoir Loc. on a tip-up
Date: Oct 31, 2002
Hi Mark, I'm trying to remember who it was that was offering a valve that was claimed to be effective for those negative G situations. Maybe someone out there will know. Jim ----- Original Message ----- From: "Mark Phillips" <ripsteel(at)edge.net> Subject: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > Howdy List- > > Anyone installed their reservoir on the rear of the subpanel so it can > be accessed when the canopy is open? I see one less hole in the > firewall, more space on firewall, easier to check level and detect leaks > (why is my sock wet?) & the vent could be run off with a little tube to > somewhere... Other pros & cons, please! > > From The PossumWorks in TN > Mark > > ________________________________________________________________________________
From: "Elsa & Henry" <elsa-henry@darlor-watch.com>
Subject: Fuel-cap labelling
Date: Oct 31, 2002
Greetings! I'm new to the Rv list subscription so bear with me if I don't know the ropes and correct protocol (yet). I'm Henry Hore and have an RV6-A that first flew in June this year. I have my RV in my own hangar at Cornwall Regional (CYCC) Ontario. I thought I would contribute what is required in Canada re Dan Chekoway's query on fuel cap labeling: The type of fuel and octane, plus the tank capacity in liters must be placarded next to the cap. I also have the capacity shown in USG. Reading the comments about cap engraving ,today, I would like to tell what I did.- I have done all my labeling using a Brother P-touch "handy" labeler, using the transparent "TZ" laminated tape. All my labels on the instrument panel, canopy opening instructions, "ELT HERE" etc,, were done with this unit and they look great. I have 2 labels by the fuel caps: The one behind the cap (rear): AVGAS 100LL ONLY and the one in front: CAPACITY 71.9 LIT- 19 USG. My final inspector liked it H. Hore. elsa-henry@darlor-watch.com ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: Brake Fluid Reservoir Loc. on a tip-up
Date: Oct 31, 2002
Alex Peterson is the guy who's producing these. alexpeterson(at)usjet.net )_( Dan ----- Original Message ----- From: "Jim Jewell" <jjewell(at)telus.net> Subject: Re: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > Hi Mark, > > I'm trying to remember who it was that was offering a valve that was claimed > to be effective for those negative G situations. > Maybe someone out there will know. > > Jim > > > ----- Original Message ----- > From: "Mark Phillips" <ripsteel(at)edge.net> > To: > Subject: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > > > > > Howdy List- > > > > Anyone installed their reservoir on the rear of the subpanel so it can > > be accessed when the canopy is open? I see one less hole in the > > firewall, more space on firewall, easier to check level and detect leaks > > (why is my sock wet?) & the vent could be run off with a little tube to > > somewhere... Other pros & cons, please! > > > > From The PossumWorks in TN > > Mark > > > > > > ________________________________________________________________________________
From: "sdavis12" <sdavis12(at)midsouth.rr.com>
Subject: Re: Fuel Cap Deal Instructions (Bad Work)
Date: Oct 31, 2002
Listers, If someone has a problem with the caps, Please contact me direct and at least give me a chance to correct the problem, Mr. Condon and Mr. Couture even a grade school helper would do that!. Most of the intelligent people I know would have enough sense to know that the caps were not in the best shape when they came from vans, anything I did wouldn't change that fact. If it took to long I apologize, some people were nice enough to e-mail me and ask If I would wait till they got theirs here for me to do, so I waited, can't win them all. But I never advertised that they were going to come back to you looking like a chrome bumper, those of you who polished theirs I'm sure wouldn't do it for 12 bucks each. ----- Original Message ----- From: "P M Condon" <pcondon(at)mitre.org> Subject: Re: RV-List: Fuel Cap Deal Instructions (Bad Work) > > > My caps were done poorly also. Looks like a grade-school helper did it. > Took a long time to get done and didn't look professional. Poor letter > edge defination, inconsistant depth, vise/tooling marks and poor letter > allignment. Better then using a electric buzz pencil, but not by much. > Very disappointed. > > > <commando@cox-internet.com> > > Hey folks, > Just an update on the fuel caps I received back from Steve this > week. > Unfortunately, I was not impressed. They did not look anything like the > picture Paul posted to this list a few weeks ago and more like something > I > could have had done at a local trophy shop for a lot less money. > I enjoy this list mostly for the information it provides on > suppliers > for RV related items. I just don't think this was such a great deal. > Sorry > Steve. > > Wayne > RV-8a > working on cabin > ----- Original Message ----- > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Fuel cap labeling regs?
Date: Oct 31, 2002
Or the turbine or diesel engine people? ----- Original Message ----- From: "Mike" <mike(at)bmnellis.com> Subject: RE: RV-List: Fuel cap labeling regs? > > Hi Mike, > > What are the Subaru guys going to do who don't run AVGAS in their auto > engines? > > Mike Nellis > RV-6 Fuselage N699BM > 1947 Stinson 108-2 NC9666K > http://bmnellis.com > > > > > > Dan, > > > > From a legal standpoint FAR Part 23 does not apply, BUT....your local > > inspector/DAR should not/will not issue your aircraft an Airworthiness > > Certificate unless somewhere in the near vicinity of the fuel filler cap > > (not necessarily on the cap itself) is the word "AVGAS", the minimum fuel > > octane and the tanks fuel capacity, in gallons. The closest FARs > > for this > > are 23.1557(c)(1), and parts of 23.1555(d) in that most inspectors will > > accept the fuel quantity to be marked near the fuel filler > > instead of at the > > fuel selector, as stated in the FAR. > > > > Mike Robertson > > Das Fed > > RV-8A, 6A and 9A > > > > > > >From: "Dan Checkoway" <dan(at)rvproject.com> > > >Reply-To: rv-list(at)matronics.com > > >To: , > > >Subject: RV-List: Fuel cap labelling regs? > > >Date: Thu, 31 Oct 2002 11:48:05 -0800 > > > > > > > > >Can somebody point me in the right direction...I'm looking for > > the FAR that > > >states exactly how fuel filler caps should be labelled or placarded, and > > >all > > >I could find was mention in Part 23 that the word "Avgas" and the minimum > > >acceptable octane must be specified. But I'm not sure if this applies to > > >amateur-built aircraft. Plus, it looks like Steve Davis' > > engraving doesn't > > >even say "Avgas" on it (I was basing that off this photo for reference: > > >http://bmnellis.com/images/DCP01408.JPG). > > > > > >With all the confusion over the quality of having fuel caps engraved, I'm > > >wondering if it's 100% required that the fuel caps be labelled in some > > >form. > > >I assume so, but what's the reg, and what's the simplest way of > > >accomplishing this? > > > > > >)_( Dan > > >RV-7 N714D (fuselage) > > >http://www.rvproject.com > > > > > > > > > > > > Choose an Internet access plan right for you -- try MSN! > > http://resourcecenter.msn.com/access/plans/default.asp > > > > > > ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: Brake Fluid Reservoir Loc. on a tip-up
Date: Oct 31, 2002
Mark, I thought about that idea a while back, and will incorporate a version of it in my Tipper as well. You might want to put a clear hose from the Aluminum Reservoir to a very small plastic "catch"-tank in case the reservoir overflows (or you are briefly inverted). Clear tube will give you signs of a arising problem, (or after the fact), but it should keep any spills contained and therefore doesn't ruin your interior. Konrad ----- Original Message ----- From: "Paul Besing" <azpilot(at)extremezone.com> Subject: Re: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > Never thought about that, but sure makes sense to me. Just be real careful > when filling or back bleeding the brakes so you don't ruin your interior! > Also, brake fluid is a no-no around paint, so be sure the area isn't > painted, or you are just real careful with the brake fluid. > > > > > Howdy List- > > > > Anyone installed their reservoir on the rear of the subpanel so it can > > be accessed when the canopy is open? I see one less hole in the > > firewall, more space on firewall, easier to check level and detect leaks > > (why is my sock wet?) & the vent could be run off with a little tube to > > somewhere... Other pros & cons, please! > > > > >From The PossumWorks in TN > > Mark ________________________________________________________________________________
Date: Oct 31, 2002
From: "Richard V. Reynolds" <rvreynolds(at)macs.net>
Subject: RV-9A Cowl Fitting
RV-9A with O-320-D1A engine w/ Hartzell C/S Propeller w/ new epoxy honeycomb cowl For the initial fitting of the cowl without the propeller install, we added a 9.0 inch diameter by 1.5 inch thick "plug" to forward face of the engine starter ring gear. Vans Dwg C4 says the aft face of the C/S hub to which the rear spinner bulkhead mounts is 2.25 inches forward of the forward face of the engine starter ring gear. The flange of the rear spinner bulkhead is 5/8 inch (.625) and the minimum clearance between the spinner and the cowl is 1/8 inch (.125). Thus, the "plug" should be 2.25 -.625 -.125 = 1.50 inches thick. The forward face of the cowl should be flush to the forward face of the plug to obtain equal spinner clearance (1/8 inch). With the forward face of the lower cowl mounted flush to the forward face of the plug, the right aft side of the cowl overlaps the fuselage bulkhead approximately 1.0 inches more than the left aft side and the right side hinge is very close to the raised honeycomb. Yes, we know there is an approximate 1.25 degree right thrust angle. If we decide to increase the spinner/cowl clearance, the interference with the honeycomb will be exasperated. I did not have this problem on my RV-6A cowl (ordered in 1998) The cowl is marked "RV-6 320 ". Do we have a "bad" cowl? Richard Reynolds, helping a RV-9A builder ________________________________________________________________________________
From: "C. Rabaut" <crabaut(at)coalinga.com>
"Dog Fighter-Terry Burch" , , "Alex Peterson" ,
Subject: Brake Fluid Reservoir Loc. on a tip-up
Date: Oct 31, 2002
Mark, How ya' doin' down there at "The Possum Works"? Funny ya'll mentioning the brake fluid reservoir. I was just talking/emailing with a fellow pilot about them. That's a good idea of yours, mounting it on the rear of the subpanel (for easy access), but if I might suggest a GREAT little stocking stuffer you could ask Old Saint Nick for.... the "Reservoir Dog" from Alex Peterson. Yep, you'll never have to worry about "why is my sock wet?" ever again. This handy dandy little cap/valve stops that red (pink or clear) caustic chemicals from dripping out; EVEN when you gets upside down. Now some of us don't wanna do flip flops or fancy smancy maneuvers, rolls, & loops, etc... ( though I ain't met that "someone" yet) but you know that even in steep turns and bounced landings that red stuff sloshes. So if ya' looking to keep your bird free from them kinda problems, contact Alex {off list at Alexpeterson(at)usjet.net } and he'll make you one too. Chuck p.s. There're "inexpensive", and I don't get nothin' for sayin' this... I just enjoy the one I installed (can you say 3 minute installation) and I like seeing one of our own list members succeed. ----- Original Message ----- From: Mark Phillips <ripsteel(at)edge.net> Subject: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > Howdy List- > > Anyone installed their reservoir on the rear of the subpanel so it can > be accessed when the canopy is open? I see one less hole in the > firewall, more space on firewall, easier to check level and detect leaks > (why is my sock wet?) & the vent could be run off with a little tube to > somewhere... Other pros & cons, please! > > From The PossumWorks in TN > Mark > > ________________________________________________________________________________
Date: Oct 31, 2002
From: Bobby Hester <bhester(at)apex.net>
RV-List
Subject: RV7A - Slider - Painted - picture
Hey guys wait untill you see this! It is Pat Patterson's RV7A, with sliding canopy, all painted up like Van's RV7. You can see it at the bottom of my home page! My server has a access limit so if you can access it check back later. It really makes me want to get mine done because it looks just like mine should. -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
From: "Steve J Hurlbut" <sjhdcl(at)kingston.net>
Subject: Re: Brake Fluid Reservoir Loc. on a tip-up
Date: Oct 31, 2002
The reservoir dog. Here is the guys email: Alex Peterson Peterson Innovation, LLC 17650 82nd Way North Maple Grove, MN 55311 alexpeterson(at)usjet.net 612-418-9710 ----- Original Message ----- From: "Jim Jewell" <jjewell(at)telus.net> Subject: Re: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > Hi Mark, > > I'm trying to remember who it was that was offering a valve that was claimed > to be effective for those negative G situations. > Maybe someone out there will know. > > Jim > > > ----- Original Message ----- > From: "Mark Phillips" <ripsteel(at)edge.net> > To: > Subject: RV-List: Brake Fluid Reservoir Loc. on a tip-up > > > > > > Howdy List- > > > > Anyone installed their reservoir on the rear of the subpanel so it can > > be accessed when the canopy is open? I see one less hole in the > > firewall, more space on firewall, easier to check level and detect leaks > > (why is my sock wet?) & the vent could be run off with a little tube to > > somewhere... Other pros & cons, please! > > > > From The PossumWorks in TN > > Mark > > > > > > ________________________________________________________________________________
From: "Konrad Werner" <Connywerner(at)wans.net>
Subject: Re: Fuel-cap labelling
Date: Oct 31, 2002
Dear Henry, A very warm "Welcome" to the RV-List! And Congratulations to finishing your RV-6A and flying it already! Happy Halloween! Sincerely, Konrad Werner ABQ-NM-USA ----- Original Message ----- From: "Elsa & Henry" <elsa-henry@darlor-watch.com> Subject: RV-List: Fuel-cap labelling <elsa-henry@darlor-watch.com> > > Greetings! I'm new to the Rv list subscription so bear with me if I don't know the ropes and correct protocol (yet). I'm Henry Hore and have an RV6-A that first flew in June this year. I have my RV in my own hangar at Cornwall Regional (CYCC) Ontario. ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Nov 01, 2002
Subject: Re: Fuel filler port labeling regs?
In a message dated 10/31/2002 11:54:52 AM Pacific Standard Time, dan(at)rvproject.com writes: > With all the confusion over the quality of having fuel caps engraved, I'm > wondering if it's 100% required that the fuel caps be labeled in some form. > I assume so, but what's the reg, and what's the simplest way of > accomplishing this? There are standard appliques available that surround the filler cap area on the wing tank. There are two types; type 1 is available from ACS and is a multilayer vinyl applique with a thin transparent coverlayer, Type 2 is a single layer vinyl applique I have found in the local flight accessories store (the Airport Shoppe at RHV has them). I went thru four of the ACS ones before I found the other type. The multilayer has a tendency to get air under the edge then starts to shed the clear layer. The now exposed markings are sticky with adhesive and not fuel/solvent resistant. The single layer type looks much better and outlasts the other about 5/1. -GV (RV-6A N1GV 572hrs) ________________________________________________________________________________
Subject: Brake Fluid Reservoir Location
Date: Nov 01, 2002
From: "Martin Hone" <martin.hone(at)tradergroup.com.au>
Hi Mark, I didn't like the look of the Van's brake reservoir on the firewall, so I ditched it in favour of a Ducati 996 front brake reservoir and mounted it above the pilot's rudder pedals, which, along with the master and starter relays etc, is accessed by a hatch built into the top skin of my RV6. The Ducati reservoir is opaque so I can easily check the level, and has a floating type of seal that moves with the fluid level and won't let the fluid leak when inverted. As far as potential for damage to upholstery and paint is concerned, I could use Dot 5 brake fluid, which I believe from a previous post, is compatible with the brake seals, or use Auto Trans Fluid. My AUD$0.02 worth Martin in Oz ________________________________________________________________________________
From: "Ted Lumpkin" <tlump(at)attbi.com>
Subject: Where to Buy Paint
Date: Oct 31, 2002
I know this seems like a silly question, but where can I buy paint for finishing my RV-4. I was going to buy Randolph paints from Aircraft Spruce, but their color choice is way too limited. I have looked at the Dupont and Sherwin Williams websites but they don't seem to have simple color charts. I know every color under the sun is available, but I was looking to buy a standard color from a paint color chart? Where have you guys purchased your paint? Ted ________________________________________________________________________________
From: "Sally and George" <aeronut58(at)hotmail.com>
Subject: Re: Where to Buy Paint
Date: Nov 01, 2002
Ted: In the Dallas area, Sherwin Williams is one good source. They have charts showing every auto make and model color for at least the last 10 years, and can mix your choice on the spot in polyurethane, lacquer or enamel. If the color you want isn't in their book, chances are it doesn't exist in the visible spectrum. George Kilishek >From: "Ted Lumpkin" <tlump(at)attbi.com> >Reply-To: rv-list(at)matronics.com >To: "RV List" >Subject: RV-List: Where to Buy Paint >Date: Thu, 31 Oct 2002 21:50:35 -0800 > > > I know this seems like a silly question, but where can I buy paint for >finishing my RV-4. I was going to buy Randolph paints from Aircraft >Spruce, >but their color choice is way too limited. I have looked at the Dupont and >Sherwin Williams websites but they don't seem to have simple color charts. >I know every color under the sun is available, but I was looking to buy a >standard color from a paint color chart? > > Where have you guys purchased your paint? > >Ted > > http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: huh
Date: Oct 31, 2002
Representation? What's that? Oh yeah, I'm a Republican living in California, duh, I forgot. ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.cc.ca.us>
Subject: Phillips
Date: Oct 31, 2002
The Philips XC is not pure mineral oil, can't be a multi-grade and be pure mineral oil. It is also an ashless dispersant oil. http://seweb1.phillips66.com/Lube/PRODUCTS.NSF/Products/0C30DC6094AF8A958625 64F3005D39AF?OpenDocument ECI is recommending this for break-in according to the recent post, but Lycoming and Contenintal don't, not sure about Superior. ________________________________________________________________________________
Date: Nov 01, 2002
From: Mark Phillips <ripsteel(at)edge.net>
Subject: Re: Fuel cap labeling regs?
Or plan to use mogas? If the tank is labelled for 100LL Avgas, will I be refused a fill-up at the BP station? Cy Galley wrote: > Or the turbine or diesel engine people? > > > What are the Subaru guys going to do who don't run AVGAS in their auto > > engines? > > ________________________________________________________________________________
From: "Wayne R. Couture" <commando@cox-internet.com>
Subject: Re: Fuel Cap Deal Instructions
Date: Nov 01, 2002
After looking at the picture of Paul's caps again(I had deleted them) I see that painting them made them appear deeper. I will do as you sugjest and I'm sure they will be just fine! Wayne ----- Original Message ----- From: "Paul Besing" <azpilot(at)extremezone.com> Subject: Re: RV-List: Fuel Cap Deal Instructions > snip > Strange that you didn't like them. 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: "Bobby Hester" <bhester(at)apex.net> > To: > Subject: Re: RV-List: Fuel Cap Deal Instructions > > > > > > "Wayne R. Couture" wrote: > > > <commando@cox-internet.com> > > > > > > Hey folks, > > > Just an update on the fuel caps I received back from Steve this > week. > > > Unfortunately, I was not impressed. They did not look anything like the > > > picture Paul posted to this list a few weeks ago and more like something > I > > > could have had done at a local trophy shop for a lot less money. > > > I enjoy this list mostly for the information it provides on > suppliers > > > for RV related items. I just don't think this was such a great deal. > Sorry > > > Steve. > > > > > > Wayne > > > RV-8a > > > working on cabin > > ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: Re: Phillips
Date: Nov 01, 2002
BTW the Cessna Owners group recommends XC for Lycoming break-in. Our experience with IO-360 (chrome cyl) was to start with staight 80 or 100 Aeroshell mineral and then switch to XC after the oil use stablized. Chuck & Dave Rowbotham RV-8A >From: Wheeler North <wnorth(at)sdccd.cc.ca.us> >Reply-To: rv-list(at)matronics.com >To: "'RV-List Digest Server '" >Subject: RV-List: Phillips >Date: Thu, 31 Oct 2002 23:23:19 -0800 > > >The Philips XC is not pure mineral oil, can't be a multi-grade and be pure >mineral oil. It is also an ashless dispersant oil. > >http://seweb1.phillips66.com/Lube/PRODUCTS.NSF/Products/0C30DC6094AF8A958625 >64F3005D39AF?OpenDocument > >ECI is recommending this for break-in according to the recent post, but >Lycoming and Contenintal don't, not sure about Superior. > > http://resourcecenter.msn.com/access/plans/freeactivation.asp ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: Where to Buy Paint
Date: Nov 01, 2002
You need to find a Sherwin Williams Automotive paint store. Call your local directory assistance and ask for the Automotive paint store. There is probably only one or two in your area. They don't advertise, and are usually located in an industrial area. They are there for body shops and such. But, when you go in, they have all you can imagine for painting your airplane. 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: "Ted Lumpkin" <tlump(at)attbi.com> Subject: RV-List: Where to Buy Paint > > I know this seems like a silly question, but where can I buy paint for > finishing my RV-4. I was going to buy Randolph paints from Aircraft Spruce, > but their color choice is way too limited. I have looked at the Dupont and > Sherwin Williams websites but they don't seem to have simple color charts. > I know every color under the sun is available, but I was looking to buy a > standard color from a paint color chart? > > Where have you guys purchased your paint? > > Ted > > ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: Re: N6JX first flight
Date: Nov 01, 2002
Mel, CONGRATULATIONS and WELL DONE !!!! Chuck & Dave Rowbotham RV-8A >From: "Jordan, Mel" <jordan_mel(at)ti.com> >Reply-To: rv-list(at)matronics.com >To: "'rv-list(at)matronics.com'" >Subject: RV-List: N6JX first flight >Date: Thu, 31 Oct 2002 11:30:46 -0600 > > >I am very pleased to report that RV-6A N6JX flew for the first time this >morning at KTUS (Tucson). N6JX is a QB kit, 60289, and the first builders >log entry was on Oct. 15, 1998, so four years and 2K hours later, I have an >airplane!! The plane flew great, no heavy wing, rudder half ball out at >cruise, absolutely no squawks on the plane, systems or engine. After a >post flight inspection, it will be ready to go again. N6JX has a new Lyc. >O-360-A1A from Van's equipped with airflow performance Fuel Injection. >Hartzell CS prop, Garmin GNC300XL and GTX327 radios, full gyro panel and >Digitrak autopilot. She doesn't have paint or wheel pants yet, so speed >was not yet up to par (145kts indicated), but she climbed like a rocket in >the cool desert morning. What a kick. The tower was great and let me >orbit right over the airport for the half hour duration of the flight. Did >slow flight with half and full flaps and generally checked out handling, >which was delightful. Landing was just like Mike Seager taught me, simple >and easy. Everything was simply perfect! I had a lot of help from fellow >builders here; Greg Johnson (RV-6), Gene Gaddis (RV-8), Alan Thomas (RV-6), >and Paul Conn (Fairchild 24). > >It was definitely worth the time and effort. This has to be one of the >best >feelings a person can experience, having this machine you built take flight >and carry you into such a beautiful blue sky. I think I'll go do it again >after lunch! > > >Mel Jordan >RV-6A N6JX >Tucson, AZ > >n6jx(at)earthlink.net > > http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
Subject: water manometers
Date: Nov 01, 2002
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
SNIP I think you would get better accuracy from a water manometer, as long as you can be sure to get all the little air bubbles out. SNIP To get all the little bubbles out all you need to do is boil the water for a few minutes prior to use. Boiling will drive out the dissolved gases that will otherwise form those zillion little bubbles in your manometer. This is a common lab practice. Of course you still have to watch for the bigger bubbles that you might form in your manometer by mechanical action. Manometer: a device for measuring WHAT!? Sorry, a little pun there based on that somewhat misleading name. ;-) Vince F-1H Rocket ________________________________________________________________________________
Subject: brake reservoir dribbles
Date: Nov 01, 2002
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
Aircraft Spruce sells a little reservoir that mounts directly on the brake cylinder. P/N A-600, $10.95 each and you'll need 2 for most installations. If you've already got Van's reservoir mounted, too bad, you could have eliminated several pesky brake fluid supply lines. To keep 5606 fluid dribbles from making a mess, get an eye dropper bulb that will fit over the fritted brake reservoir cap, make a small hole in it. Make sure the hole won't seal itself. When the brake fluid reservoir burps, most of the fluid will stay inside the bulb and get drawn back in. Seemed to work for me, but obviously won't keep you from overfilling it during brake bleeding operations. Most already know this, but I see it regularly, DON'T put automotive brake fluid in your airplane unless you want to crash into something! Most aircraft brake systems use Mil-H-5606 hydraulic fluid. Double check if you're not sure. Automotive (Dot 3,etc) fluids can soften your brake seals causing stained shorts at best, bent metal at worst! Vince F-1H Rocket ________________________________________________________________________________
From: MeangreenRV4(at)aol.com
Date: Nov 01, 2002
Subject: Re: Exxon Elite
In a message dated 10/30/2002 11:39:43 AM Pacific Standard Time, zilik(at)direcpc.com writes: > > Wow, this is really good information. No wonder I climb so slow, I got a > boat anchor in the front and I did'nt know it. > > Gary > Why Gary I am damm glad to help ya Tim Barnes ________________________________________________________________________________
From: "Mike" <mike(at)bmnellis.com>
Subject: Brake Fluid Reservoir Location
Date: Nov 01, 2002
A motorcycle reservoir is not a bad way to go. I don't know that I'd pick the most expensive model out there by going with a Ducati reservoir but any clear reservoir would probably work. It would be about $33 plus shipping to get one. You would have to design a mounting bracket though. Here is the one that fits my Yamaha YZF1000 and it's clear so it can be checked at a glance. http://216.37.204.206/xtremepowersports/Yamaha_OEM/YamahaMC.asp?Type=13&A=16 0&B=29 Mike Nellis RV-6 Fuselage N699BM 1947 Stinson 108-2 NC9666K http://bmnellis.com > > > > Hi Mark, > > I didn't like the look of the Van's brake reservoir on the > firewall, so I ditched it in favour of a Ducati 996 front brake > reservoir and mounted it above the pilot's rudder pedals, which, > along with the master and starter relays etc, is accessed by a > hatch built into the top skin of my RV6. The Ducati reservoir is > opaque so I can easily check the level, and has a floating type > of seal that moves with the fluid level and won't let the fluid > leak when inverted. > As far as potential for damage to upholstery and paint is > concerned, I could use Dot 5 brake fluid, which I believe from a > previous post, is compatible with the brake seals, or use Auto > Trans Fluid. > > My AUD$0.02 worth > > Martin in Oz > > ________________________________________________________________________________
From: "Mike Robertson" <mrobert569(at)hotmail.com>
Subject: Fuel cap labeling regs?
Date: Nov 01, 2002
OOps,..I guess I should have gone a bit further. The wording of the placarding of the fuel cap area will be dictated by the type of engine installed. But being an experimentor with an experimental aircraft you can pretty much put what you want around there provided you have some type of minimum fuel Quality (Octane) and the tanks capacity. Mike Robertson Das Fed >From: "Mike" <mike(at)bmnellis.com> >Reply-To: rv-list(at)matronics.com >To: >Subject: RE: RV-List: Fuel cap labeling regs? >Date: Thu, 31 Oct 2002 17:35:54 -0600 > > >Hi Mike, > >What are the Subaru guys going to do who don't run AVGAS in their auto >engines? > >Mike Nellis >RV-6 Fuselage N699BM >1947 Stinson 108-2 NC9666K >http://bmnellis.com > > > > > > Dan, > > > > From a legal standpoint FAR Part 23 does not apply, BUT....your local > > inspector/DAR should not/will not issue your aircraft an Airworthiness > > Certificate unless somewhere in the near vicinity of the fuel filler cap > > (not necessarily on the cap itself) is the word "AVGAS", the minimum >fuel > > octane and the tanks fuel capacity, in gallons. The closest FARs > > for this > > are 23.1557(c)(1), and parts of 23.1555(d) in that most inspectors will > > accept the fuel quantity to be marked near the fuel filler > > instead of at the > > fuel selector, as stated in the FAR. > > > > Mike Robertson > > Das Fed > > RV-8A, 6A and 9A > > > > > > >From: "Dan Checkoway" <dan(at)rvproject.com> > > >Reply-To: rv-list(at)matronics.com > > >To: , > > >Subject: RV-List: Fuel cap labelling regs? > > >Date: Thu, 31 Oct 2002 11:48:05 -0800 > > > > > > > > >Can somebody point me in the right direction...I'm looking for > > the FAR that > > >states exactly how fuel filler caps should be labelled or placarded, >and > > >all > > >I could find was mention in Part 23 that the word "Avgas" and the >minimum > > >acceptable octane must be specified. But I'm not sure if this applies >to > > >amateur-built aircraft. Plus, it looks like Steve Davis' > > engraving doesn't > > >even say "Avgas" on it (I was basing that off this photo for reference: > > >http://bmnellis.com/images/DCP01408.JPG). > > > > > >With all the confusion over the quality of having fuel caps engraved, >I'm > > >wondering if it's 100% required that the fuel caps be labelled in some > > >form. > > >I assume so, but what's the reg, and what's the simplest way of > > >accomplishing this? > > > > > >)_( Dan > > >RV-7 N714D (fuselage) > > >http://www.rvproject.com > > > > > > http://resourcecenter.msn.com/access/plans/default.asp ________________________________________________________________________________
From: "Randy Compton" <rdcompton(at)earthlink.net>
Subject: Ted Hendrickson props
Date: Nov 01, 2002
Fellow "Listers": Anyone out there know what happened to Ted Hendrickson props? Are they made under another name? Thanks, Randy Compton RV-3A N84VF Gulf Breeze, FL ________________________________________________________________________________
From: "Pete Bodie" <rv6apjb(at)attbi.com>
Subject: RV6A Wing attachment question
Date: Nov 01, 2002
I am finally getting to the point of attaching the wings on my RV6A. My question is; Should I support the fuselage when I remove the tempory spar or will the rest of the bolts in the main gear bracket support it until I get the wing installed and bolted? I will be working on one side at a time. If I should support the fuslage where is the best location. ________________________________________________________________________________
Date: Nov 01, 2002
From: Gary Liming <gary(at)liming.org>
Subject: Lightspeed Ignition vs mags
I think something is being overlooked here - Lightspeed has two ways to install one is with a unit that goes into where a mag would go that provides the timing info. The other way is drill small holes in the flywheel and replace the material with magnets, and then mount a sensor on the engine block to pick up the magnets rotation. The reason you would use the former is to make the installation simple. The reason you wouldn't is that you have yet another moving part that needs to be inspected every 50 hours, like your mags need. The latter method has no moving parts (other than the flywheel you need anyway) and therefore is more reliable and a lot more maintainable - that's what is hard to beat. It is completely your choice. My experience with customer support is that Klaus has answered my questions both times I called. As for performance of Lightspeed vs. mags, all you have to do is a "mag check" - I have one mag on the left, and Lightspeed on the right. When operating with one mag, there is the usual RPM drop. When operating with just Lightspeed and no mag, there is no RPM drop - the Lightspeed is completely burning the fuel mixture by itself. It does this at a lot less than 7000 ft. Gary Liming > > > Thanks for the info Randy. That is interesting for me. I have been >thinking of > > an electronic ignition on one side. > > I like the one from Chattanooga better because it has a machined part to >go in > > the mag hole instead of the way Light Speed does it. It looks a little >more > > "designed". > > > > Then when I weigh everything, a trusty old mag, new out of the box is >about half > > price of one of the electronic thingy's. They are pretty reliable for a >couple > > thousand hours... Hard to beat. > > > > Phil > >As you can see, some folks have a great experience with Lightspeed and it's >owner. Mine has been otherwise. I installed the Lightspeed as part of a >major overhaul. If I had it do over, I'd have gone with mags on both sides. >Since I don't routinely fly above 7500 feet msl, I haven't observed any >quantifiable pereformance gain. > >And I still stand by my observation that Lightspeed's customer support >stinks. Twice I tried to obtain a smidgen of info from them; both times the >response was "go to the web." Ain't practical when one is hanging over the >edge of the airplane tinkering with the innards. Probably took him longer >to tout the virtues of the web than it would to have just answered my >question. > >Randy Compton >RV-3A N84VF >Gulf Breeze, FL > > ________________________________________________________________________________
Date: Nov 01, 2002
From: Matt Dralle <dralle(at)matronics.com>
Subject: 2002 List Fund Raiser - Please Support Your Lists...
Dear Listers, During November of each year, I have a voluntary Email List Fund Raiser to support the continued operation, development, maintenance and upgrade of the Email Forums sponsored here. Your Contributions go directly into improvements in the systems that support the Lists and to pay for the Internet connectivity primarily dedicated to supporting the Lists. The traffic on the Lists continues to grow and the numbers are nothing short of impressive! Here are some statistics that show much traffic the Lists generated last year alone: 11/01/2001 - 10/31/2002 Web server hits: 8,700,000 (727,000/mo) Incoming Email Posts: 51,259 (4,271/mo) * * This number is multiplied by the total number of email addresses subscribed to the given List. The actual number of email message processed is in the 50,000,000 range for last year!! The new Internet provider, Speakeasy, has been providing extremely fast and reliable service over the last year, and this has certainly been a refreshing change from previous providers! There were a couple of new features added at the tail-end of last year including the new List Browse Feature ( http://www.matronics.com/listbrowse ), and the List Photoshare which have been both very popular. Many people have written to say how much they enjoy the on-line browsing capability of current week's messages. The 184 new Photoshares ( http://www.matronics.com/photoshare ) added over the last year attests to its acceptance and appreciation in the community as well. I have upgraded both the email and web server OS systems recently to the latest - well almost the latest - version of Redhat Linux and Kernel 2.4.19, both of which have been working very well and quite reliably. What does the future hold? Well, something pretty exciting I'm hoping... I am currently evaluating a new, commercially available software package that runs under Linux and provides a complete web-based Email List service akin to what those other guys use. The difference will be that there won't be any annoying advertisements and popup ads on the Matronics system!! The system will continue to be dedicated to furthering Lists activities and not trying to sell you something you don't want. My hope is to keep most if not all of the current functionality in place and add the new software system over the top. Some of the system will be replaced (like majordomo), but the lists will work much like they do today - only BETTER! As I mentioned, I am currently in the evaluation stage of this and have yet to select a final product. Suffice to say some facelifts are definitely on the way! Unlike many of the other "list servers" on the web these days, I have a strict no-commercial-advertisement policy on the Matronics Lists and associated List websites. I have been approached by a number of vendors recently with advertising deals that have been very tempting. However, my commitment to providing a grass-roots, non-commercial environment prevails! Commercialism on the Internet seems to be increasing exponentially every year with more and more SPAM and pop up ads, not to mention the ever increasing Virus attacks. My goal with the Matronics List Service is to provide my members with a commercial-free, safe, and high-performance system in which to share information, ideas, and camaraderie. I recoup my upgrade, maintenance, and operating costs by having a List Fund Raiser once a year during November. During this time, I ask List members to donate a small amount of money to support the continued operation of the Lists over the upcoming year. Contributions in the $20, $30, and $50 range are common. This year I have completely revamped the Contribution website, and have added the ability to use PayPal to make your Contribution in addition to the traditional Visa/MC and Personal Check Options. Its easier and faster than ever before to make your Contribution!! For those who are accustomed to using PayPal to make Internet purchases, will appreciate the ease and speed of using this handy method of payment to make their List Contribution. The best news this year, however, is that I have a couple of fantastic Gift offers to support the List Fund Raiser! Andy Gold of The Builder's Bookstore ( http://www.buildersbooks.com ) will be generously donating a FREE Jeppesen Flight Bag to anyone making a $50 or more List Contribution during the Fund Raiser! This is a great bag and something you'll surely what to get your hands on. Thanks Andy, for this great incentive!! In addition to the great Flight Bag, I will also be offering a FREE Matronics List Archive CDROM for a $50 or greater Contribution! This is a complete set of archives for all Email Lists currently hosted by Matronics. The Archives date back to the beginning of the each List. In the case of the RV-List, for example, this includes archives all the way back to 1990! That's about 133Mb alone! Also included on the CD is a copy of Chip Gibbion's Windows Archive Search Utility and a precompiled search-index for each archive on the CD. Better yet?! You can get BOTH the Flight Bag AND the Archive CD for a Contribution of $75 or more which is actually LESS than the combined retail price on the two items!!! How can you go wrong? Get some great stuff AND support your Lists at the same time! Over the next month I'll be posting a few reminder messages about the List Fund Raiser, and I ask for your patience and understanding during the process. Remember that the Lists are *completely* funded through the generous Contributions of its members. That's it! There's no support from a bloated advertising budget or deep pockets somewhere. Its all made possible through YOUR support! I would like to take this opportunity to thank everyone who supports the List this year. Your generosity contributes directly to the quality of the experience here. To make your List Contribution using a Visa or MasterCard, PalPal, or with a Personal Check, please go to the URL link below. Here you can find additional details on this year's great free Gifts as well as additional information on the various methods of payment. SSL Secure Contribution Web Site: http://www.matronics.com/contributions Again, I would like to thank everyone who supports the Lists this year! Your Contributions truly make it all possible!! Thank you! Matt Dralle Matronics Email List Administrator Matt G Dralle | Matronics | PO Box 347 | Livermore | CA | 94551 925-606-1001 V | 925-606-6281 F | dralle(at)matronics.com Email http://www.matronics.com/ WWW | Featuring Products For Aircraft ________________________________________________________________________________
From: Paulbaird(at)aol.com
Date: Nov 01, 2002
Subject: Re: RV ride
Scott, You are right it is ridiculous. You better drive. No one cares who buys the gas for your car. Paul PS the feds don't have the resources to care who paid for the gas (with cash!) ________________________________________________________________________________
From: "3 rotor" <rv8r300(at)attbi.com>
Subject: Re: Lightspeed Ignition vs mags
Date: Nov 01, 2002
inspect every 50 hours? gosh, i'm 800 hours overdue, of course they're Slicks so you just throw them away. I do change the oil every 50 hrs.... kevin > that you have yet another moving part that needs to be inspected every 50 > hours, like your mags need. ________________________________________________________________________________
From: "3 rotor" <rv8r300(at)attbi.com>
Subject: Re: RV6A Wing attachment question
Date: Nov 01, 2002
run some hardware store bolts thru the engine mount holes to a couple of 2x4 legs, put the tail on a stool, leave the gear off until the wing get some bolts in it. I don't understand how you thought you could attach the wing with the gear on since the gear socket attaches to the wing spar. kevin > My question is; > Should I support the fuselage when I remove the tempory spar or will the rest of the bolts in the main gear bracket support it until I get the wing installed and bolted? > ________________________________________________________________________________
Date: Nov 01, 2002
From: Bobby Hester <bhester(at)apex.net>
RV-List
Subject: Proseal use in cold weather
Ok, I am ready to start sealing my second tank. It is looks like the temps are going to be between 36-58 degrees F through the coming week. Is it ok to proseal in those temps? I'll be in my hanger with a karosene heater, but it does not help much. I do realize that it will take longer to cure, but is there any reason not to do it in these temps? -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
From: "RV6 Flyer" <rv6_flyer(at)hotmail.com>
Subject: Re: Lightspeed Ignition vs mags
Date: Nov 02, 2002
I have old 1961 vintage Bendix SL20 and SL21 mags. I overhauled both of them 1,200 hours ago. The only inspection required if all the ADs are complied with is 500 hours. I did pull the impulse coupled mag at 100 hours to do the 100 hour inspection that was required with the old riveted impulse coupling and replaced it with the snap ring coupling at that time. Now the inspection is required every 500 hours. At the 500 hour inspection, found no adjustments needed. At 1,000 hours, I did adjust the points. Relubricate the bearings both times but they looked as good before as they did after. Total time mags and engine over 4,300 hours the last time I looked in the engine log. What kind of mag do you have that needs 50 hour inspection? What does the inspection consist of? Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, 1,210 + Flying Hours So. CA, USA http://SoCAL_WVAF.rvproject.com ----Original Message Follows---- From: "3 rotor" <rv8r300(at)attbi.com> Subject: Re: RV-List: Lightspeed Ignition vs mags Date: Fri, 1 Nov 2002 20:05:15 -0800 inspect every 50 hours? gosh, i'm 800 hours overdue, of course they're Slicks so you just throw them away. I do change the oil every 50 hrs.... kevin > that you have yet another moving part that needs to be inspected every 50 > hours, like your mags need. http://resourcecenter.msn.com/access/plans/2monthsfree.asp ________________________________________________________________________________
From: "Sally and George" <aeronut58(at)hotmail.com>
Subject: Re: Proseal use in cold weather
Date: Nov 02, 2002
Bobby: I did one of my tanks in weather about that cold and it worked okay. I did, however, take the completed tank into my house where it could cure at 70 degrees F or so. I don't know how long it would take to cure at 50 degrees or lower, but I suspect it would be a long time. George Kilishek N888GK 100 hours and no leaks in fuel tanks >From: Bobby Hester <bhester(at)apex.net> >Reply-To: rv-list(at)matronics.com >To: RV7and7A , RV-List > >Subject: RV-List: Proseal use in cold weather >Date: Fri, 01 Nov 2002 23:04:51 -0600 > > >Ok, I am ready to start sealing my second tank. It is looks like the >temps are going to be between 36-58 degrees F through the coming week. >Is it ok to proseal in those temps? I'll be in my hanger with a karosene >heater, but it does not help much. I do realize that it will take longer >to cure, but is there any reason not to do it in these temps? > >-- >Surfing the Web from Hopkinsville, KY >Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ >RV7A Working on the wings :-) > > Protect your PC - get McAfee.com VirusScan Online http://clinic.mcafee.com/clinic/ibuy/campaign.asp?cid=3963 ________________________________________________________________________________
From: "Tom Gummo" <t.gummo(at)verizon.net>
Subject: manual
Date: Nov 01, 2002
I got the manual. I don't have the writer to go with Adobe Reader so I had to copy and pass it into MS Word a page at a time. Only then did I think I should ask if you have it in Word format. :-( There are a couple of things I will have to think about as they are different than I am used to. Tom ________________________________________________________________________________
From: "Jim Norman" <jnorman(at)intermapsystems.com>
Subject: Airport Problems
Date: Nov 02, 2002
OK Listers, here's a new problem... I'm putting my wings on my plane in a hanger that I rent. I have been based at this airport for almost 8 years (I have an Archer). The airport manager (without ANY warnings) shows up yesterday with eviction papers giving me 5 days to clean out the hangar. Why? Because we are "building an airplane" at the airport and this is not allowed. Of course, my plane was "built" at home, painted in a shop, and transported to the airport ready to bolt together. Its done except for wings, ailerons, and flaps. Also, of course, there are a dozen or more experimentals at this airport. Some, being built from scratch at the airport. Bottom line, after begging (and other distasteful measures) I was allowed to keep the hangar, but only for a "completed" airplane. They gave me 24 hours to get rid of the plane "parts". I have complied with this (what a pain in the butt). They even demanded that a work bench and all tools be removed. Their issue "insurance". "What happens if your plane falls on you and you get crushed and hold us liable?" Of course, of the $419 a month I pay for a hangar, $23.00 goes to "insurance" (its a line item). My plane is insured with builder's insurance (John Helms, are you reading this?). (I think there may be some more underlying issues, but I can't put my finger on them yet). Questions: 1) Has anybody heard of this before? 2) When is the plane a plane? When it has wings but not flaps? Wings and flaps but not ailerons? Fuselage and wings, but no avionics? They are quoting a clause that says "no airplane repairs shall be undertaken in areas not designated for such repairs, except for routine maintenance". Need some advice here... don't want to set a precedence for this airport that may spread. jim Tampa Vandenberg Airport VDF (near Sun-N-Fun, so don't come here on your way to Sun-n-Fun). ________________________________________________________________________________
Date: Nov 02, 2002
From: Bobby Hester <bhester(at)apex.net>
Subject: Re: Proseal use in cold weather
Sally and George wrote: > >Bobby: > >I did one of my tanks in weather about that cold and it worked okay. I did, >however, take the completed tank into my house where it could cure at 70 >degrees F or so. I don't know how long it would take to cure at 50 degrees >or lower, but I suspect it would be a long time. > >George Kilishek >N888GK >100 hours and no leaks in fuel tanks > > Didn't the smell about kill you? -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Working on the wings :-) ________________________________________________________________________________
Date: Nov 02, 2002
From: Ken Balch <kbalch1(at)attbi.com>
"rv8list(at)yahoogroups.com"
Subject: FS: RV-8
Well, the time has come to either conclude the sale of my RV, or give in and paint it this winter in the hope of selling it next year. I won't bore the list with the details, as everyone has seen them before, other than to say that it's still flying great. N118KB will go, as is, to the first guy who ponies up $96,000. Please email me off-list with any questions. Ken Balch RV-8 N118KB ________________________________________________________________________________
From: "Dan Ahearn" <dahearn(at)attbi.com>
Subject: Technical education
Date: Nov 02, 2002
Listers .... Were can I learn more about the A&P rating? I've been curious what goes into the A&P rating. While I recognize it's not necessary for what I'm about to embark upon, it seems to me that all this effort I intend to put into my airplane might allow me to apply work towards an A&P. Any advise or links greatly appreciated Dan Highland Village, TX ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Airport Problems
Date: Nov 02, 2002
Jim, This is classic police state mentality - have enough laws so that the "authorities" can bust anyone they want. This worked well in the 30's in various countries, and we are going fast towards that here in the US. I suspect most airports have such laws as you shared below. However, since there are thousands of experimental and certificated airplanes being built, assembled, etc., in this country at public airports in public hangers, most airport managers don't play rent-a-cop like yours is. Legally you may have no option, but AOPA's legal advisors might be able to help. EAA should be brought into the loop for sure, as this has large implications for all homebuilders. Is it likely that some FBO is playing hardball? If you had proof, there might be some market pressures that could be brought to bear. Can you get an A&P to write a letter saying that your assembly is quite routine, which it obviously is? It must be routine, since it is necessary and has happened thousands of times. It is obviously not a repair either. Play the words, shove them back in his face. Good luck, keep the list posted. Alex Peterson Maple Grove, MN RV6-A N66AP 221 hours at a friendly Anoka County Airport ANE in Minneapolis They are quoting a clause that says "no airplane > repairs shall be undertaken in areas not designated for such > repairs, except for routine maintenance". > > Need some advice here... don't want to set a precedence for > this airport that may spread. > > jim ________________________________________________________________________________
From: "Ron Calhoun" <roncal(at)earthlink.net>
Subject: Airport Problems
Date: Nov 02, 2002
Jim, if you have to go, so should all the other builders. Is this what the airport wants? Ron Calhoun RV4 Installling wings ________________________________________________________________________________
Date: Nov 02, 2002
From: Gert <gert(at)execpc.com>
Subject: Re: Proseal use in cold weather
Hi Bobby I did mine in low temps, it takes a looong time to cure so the tanks will have to be undisturbed a looong time...if you want to move them to a warmer place do it as soon as possible with the proseal as plyable as possible. Clean your parts **thoroughly**, and then even better. kerosine heaters do cause an minute oily film to built on things left in the neighbourhood. If you can smell anything when the kerosine heater is running, it's leaving a residu. if ya can't smell it, it is probably still contaminating. Proseal just does not adhere consistently to contaminated parts and just because you cleaned all parts yesterday before you went to bed, that does not mean a film has started to build overnite sufficient to make your tank leak down the line. Be safe and reclean all parts directly prior to use........ I did find the quality of kerosine has a tremendous effect here Gert Bobby Hester wrote: > > Ok, I am ready to start sealing my second tank. It is looks like the > temps are going to be between 36-58 degrees F through the coming week. > Is it ok to proseal in those temps? I'll be in my hanger with a karosene > heater, but it does not help much. I do realize that it will take longer > to cure, but is there any reason not to do it in these temps? > > -- is subject to a download and archival fee in the amount of $500 ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Lightspeed Ignition vs mags
Date: Nov 02, 2002
Slick and Bendix both recommend 500 hour inspections. 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: "3 rotor" <rv8r300(at)attbi.com> Subject: Re: RV-List: Lightspeed Ignition vs mags > > inspect every 50 hours? gosh, i'm 800 hours overdue, of course they're > Slicks so you just throw them away. I do change the oil every 50 hrs.... > kevin > > > that you have yet another moving part that needs to be inspected every 50 > > hours, like your mags need. > > ________________________________________________________________________________
Date: Nov 02, 2002
From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)mcleodusa.net>
Subject: Re: Airport Problems
Jim Norman wrote: > > OK Listers, here's a new problem... > > I'm putting my wings on my plane in a hanger that I rent. I have been based > at this airport for almost 8 years (I have an Archer). > > The airport manager (without ANY warnings) shows up yesterday with eviction > papers giving me 5 days to clean out the hangar. Why? Because we are > "building an airplane" at the airport and this is not allowed. Of course, > my plane was "built" at home, painted in a shop, and transported to the > airport ready to bolt together. Its done except for wings, ailerons, and > flaps. > > Also, of course, there are a dozen or more experimentals at this airport. > Some, being built from scratch at the airport. > > Bottom line, after begging (and other distasteful measures) I was allowed to > keep the hangar, but only for a "completed" airplane. They gave me 24 hours > to get rid of the plane "parts". I have complied with this (what a pain in > the butt). They even demanded that a work bench and all tools be removed. > > Their issue "insurance". "What happens if your plane falls on you and you > get crushed and hold us liable?" Of course, of the $419 a month I pay for a > hangar, $23.00 goes to "insurance" (its a line item). My plane is insured > with builder's insurance (John Helms, are you reading this?). (I think > there may be some more underlying issues, but I can't put my finger on them > yet). > > Questions: 1) Has anybody heard of this before? 2) When is the plane a > plane? When it has wings but not flaps? Wings and flaps but not ailerons? > Fuselage and wings, but no avionics? They are quoting a clause that says > "no airplane repairs shall be undertaken in areas not designated for such > repairs, except for routine maintenance". > > Need some advice here... don't want to set a precedence for this airport > that may spread. > > jim > Tampa > Vandenberg Airport VDF (near Sun-N-Fun, so don't come here on your way to > Sun-n-Fun). > I thought for a minute you were going to say you were in Illinois. The small city owned airprts around here pull the same stuff. Usually it is dictated to them from Illinois Deptartment of Transportation, Aeronautics.. The State wants to have the final say so in small airport management, I guess so they can justify their Fat State Paychecks....... Phil, Litchfield, IL building RV-6, flying Pitt's S1S ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: Re: Technical education
Date: Nov 02, 2002
Dan, If you are looking for info on whats involved in getting the rating itself then either call your local FSDO office or speak to the staff at a nearby part 147 AMT school. If you are looking for self study material (textbooks, test aids, ect.) then click into our "other" web catalog http://ACtechbooks.com. Also if you are looking for a nearby school, also click into the link above, and then into the "Part 147 Schools" link on the top of the page. It will display all the certificated schools by state and city with contact info. Andy > > Listers .... > > Were can I learn more about the A&P rating? > > I've been curious what goes into the A&P rating. While I recognize it's not necessary for what I'm about to embark upon, it seems to me that all this effort I intend to put into my airplane might allow me to apply work towards an A&P. > > Any advise or links greatly appreciated > > Dan > Highland Village, TX > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Airport Problems
Date: Nov 02, 2002
Phil, I don't think you comments about the Illinois Aeronautical Department are true. I am based at Moline, Illinois and have no problems and neither do any of the other many experimentals based as our class C airport. We have built, assembled, and test flown several in just this last year. Everything from a RV-4 to an L-29 Jet. No insurance requirement either. It all depends on the airport commissioner or board. Cy Galley Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org ----- Original Message ----- From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)mcleodusa.net> Subject: Re: RV-List: Airport Problems > > Jim Norman wrote: > > > > > OK Listers, here's a new problem... > > > > I'm putting my wings on my plane in a hanger that I rent. I have been based > > at this airport for almost 8 years (I have an Archer). > > > > The airport manager (without ANY warnings) shows up yesterday with eviction > > papers giving me 5 days to clean out the hangar. Why? Because we are > > "building an airplane" at the airport and this is not allowed. Of course, > > my plane was "built" at home, painted in a shop, and transported to the > > airport ready to bolt together. Its done except for wings, ailerons, and > > flaps. > > > > Also, of course, there are a dozen or more experimentals at this airport. > > Some, being built from scratch at the airport. > > > > Bottom line, after begging (and other distasteful measures) I was allowed to > > keep the hangar, but only for a "completed" airplane. They gave me 24 hours > > to get rid of the plane "parts". I have complied with this (what a pain in > > the butt). They even demanded that a work bench and all tools be removed. > > > > Their issue "insurance". "What happens if your plane falls on you and you > > get crushed and hold us liable?" Of course, of the $419 a month I pay for a > > hangar, $23.00 goes to "insurance" (its a line item). My plane is insured > > with builder's insurance (John Helms, are you reading this?). (I think > > there may be some more underlying issues, but I can't put my finger on them > > yet). > > > > Questions: 1) Has anybody heard of this before? 2) When is the plane a > > plane? When it has wings but not flaps? Wings and flaps but not ailerons? > > Fuselage and wings, but no avionics? They are quoting a clause that says > > "no airplane repairs shall be undertaken in areas not designated for such > > repairs, except for routine maintenance". > > > > Need some advice here... don't want to set a precedence for this airport > > that may spread. > > > > jim > > Tampa > > Vandenberg Airport VDF (near Sun-N-Fun, so don't come here on your way to > > Sun-n-Fun). > > > > I thought for a minute you were going to say you were in Illinois. The small > city owned airprts around here pull the same stuff. Usually it is dictated to > them from Illinois Deptartment of Transportation, Aeronautics.. > The State wants to have the final say so in small airport management, I guess so > they can justify their Fat State Paychecks....... > > Phil, Litchfield, IL building RV-6, flying Pitt's S1S > > ________________________________________________________________________________
From: "Carl Froehlich" <carlfro(at)erols.com>
Subject: Airport Problems
Date: Nov 02, 2002
Jim, We are fighting this in northern VA right now. The good news is if the airport gets any federal money, they cannot do what they did to you. Here is a note from the EAA we received when we asked for help. Good luck, Carl Froehlich RV-8A (flying) Vienna, VA Now to the basics: FAA AC 150/5190-5, dated June 10, 2002, http://www.faa.gov/arp/ACs/5190-5a1.pdf FAA Order 5190-6A, http://www.faa.gov/arp/publications/orders/5190-6a.pdf FAA Order 5100.38A - assurances extract - http://www.faa.gov/arp/pdf/assrnap.pdf Any airport developed under FAA granted federal funds signs a "grant of assurance" (FAA Order 5100.38A) that says two things: 1st. Grant 22a - "It will make its airport available as an airport for public use on fair and reasonable terms and without unjust discrimination, to all types, kinds, and classes of aeronautical activities."; and 2nd Grant 22f - "It will not exercise or grant any right or privilege which operates to prevent any person, firm, or corporation operating aircraft on the airport from performing any services on its own aircraft with its own employees (including, but not limited to maintenance, repair, and fueling) that it may choose to perform." FAA Order 5190.6A, paragraph 3-9(e)(1) - Restrictions on Self-Service - "Any unreasonable restriction imposed on the owners or operators of aircraft regarding the servicing of their own aircraft and equipment may be construed as a violation of this policy. Where no attempt has been made to perform such services for others, aircraft owners should be permitted to fuel, wash, repair, paint and otherwise take care of their own aircraft. A restriction which has the effect of diverting such business to a commercial operator amounts to an exclusive monopoly of an aeronautical activity contrary to law.": plus paragraph 3-9(3) - ..."With respect to fuel, the aircraft owner may assert the right to obtain fuel where he pleases and bring it onto the airport to service his own aircraft...This policy also applies to aircraft owners who have obtained FAA STC 's authorizing the use of auto gas in their aircraft and who wish to self service their aircraft with mogas." FAA AC 150/5190-5 paragraph 1-2 Agency Policy - "An exclusive rights violation occurs when the airport sponsor excludes others, either intentionally or unintentionally, from participating in an on-airport aeronautical activity." Bottom line - By the Airport management refusing to recognize the rights of the experimental amateur-built aircraft owners right to perform all his/her own maintenance per FAR 65.104 and failing to recognize that FAR 43.1(b) specifically excludes the owners of amateur-built aircraft from complying with all the maintenance procedures of FAR 43 the airport owner is "intentionally creating an exclusive rights violation" by requiring all experimental amateur-built aircraft owners to use A&P mechanics. One thing the airport needs to be made aware of is that because FAR 43.1(b) specifically excludes owners of experimental amateur-built aircraft from the maintenance requirements of FAR 43 - that in effect moves all experimental amateur-built aircraft maintenance into the "self-service" side of the on-airport maintenance issue. And FAA Order 5190.6A grants owners of aircraft the right to perform self-maintenance on their aircraft... For you, the self-maintenance rules does not automatically dedicate that you can bring a independent A&P on the airport to complete your annual condition inspections and major repairs to your experimental amateur-built aircraft. However, if the on-airport A&P's (at the FBO's, etc.) refuse to work on amateur-built aircraft, then the airport managers have to requirement to allow you to hire someone to do that work for you (FAA Order 5190.6A, para 3-9(e)(1)). Hope that helps. Randy Randy Hansen EAA Government & Industry Relations Specialist rhansen(at)eaa.org 920-426-6522 888-322-4636, extension 6522 920-426-6560 (fax) -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Jim Norman Subject: RV-List: Airport Problems OK Listers, here's a new problem... I'm putting my wings on my plane in a hanger that I rent. I have been based at this airport for almost 8 years (I have an Archer). The airport manager (without ANY warnings) shows up yesterday with eviction papers giving me 5 days to clean out the hangar. Why? Because we are "building an airplane" at the airport and this is not allowed. Of course, my plane was "built" at home, painted in a shop, and transported to the airport ready to bolt together. Its done except for wings, ailerons, and flaps. Also, of course, there are a dozen or more experimentals at this airport. Some, being built from scratch at the airport. Bottom line, after begging (and other distasteful measures) I was allowed to keep the hangar, but only for a "completed" airplane. They gave me 24 hours to get rid of the plane "parts". I have complied with this (what a pain in the butt). They even demanded that a work bench and all tools be removed. Their issue "insurance". "What happens if your plane falls on you and you get crushed and hold us liable?" Of course, of the $419 a month I pay for a hangar, $23.00 goes to "insurance" (its a line item). My plane is insured with builder's insurance (John Helms, are you reading this?). (I think there may be some more underlying issues, but I can't put my finger on them yet). Questions: 1) Has anybody heard of this before? 2) When is the plane a plane? When it has wings but not flaps? Wings and flaps but not ailerons? Fuselage and wings, but no avionics? They are quoting a clause that says "no airplane repairs shall be undertaken in areas not designated for such repairs, except for routine maintenance". Need some advice here... don't want to set a precedence for this airport that may spread. jim Tampa Vandenberg Airport VDF (near Sun-N-Fun, so don't come here on your way to Sun-n-Fun). ________________________________________________________________________________
From: "Elsa & Henry" <elsa-henry@darlor-watch.com>
Subject: Re: RV6A Wing attachment question
Date: Nov 02, 2002
To Pete Bodie: I put my wings on this spring and found it to be a ?#&~#*!* of a job! In answer to your questions, you can't have any bolts going through the F104 bulkhead, otherwise you can't slide the wings in. I built a very strong saw-horse out of two layers of 3/4" ply-wood with a 10" wide cross-member to support the fuselage right under the firewall, slotted to clear the exhaust pipes. The legs and cross-member were biscuit-glued together. It has to be strong, because when your assistants (at least 2) are pushing the wing in and you are trying to get that first bolt installed, considerable side pressure will be exerted to the fuselage. You don't want your saw-horse to collapse!! The tail is supported by a stand, (adjustable height) I built earlier during the fuselage building process and is on a platform with casters. Hopefully you made your spar spacers blocks a few thou wider than your wing spars!!! Smear some anti-seize compound on the spar stubs to help their sliding-in. The first bolt to install is one of the 3/8" ones that go through the splice-plates. Then install the two " ones at the out-board end.Then your assistants can relax while you install the rest of them!! (With the occasional jiggle to help the job) Installing the nuts and torquing them is a BIG job! Especially the ones under the weldment top flange that supports the leg-tube. Be prepared to "modify" some of your wrenches for this. I found that a double-offset (3/8") ring-wrench was OK to reach that pesky bolt right in the corner near the leg-tube, but it was too long to clear the side of the fuselage, so I put a torch to it and put a 90 bend it half way down. I also suggest that you fashion an aluminum strip with a releasable clip arrangement on the end to hold a nut while starting the thread by rotating the bolt. It took me 10 very long days to bolt and torque the 72 of them and working in a confined space at 75 years of age was no joke! Cheers!-- Henry ________________________________________________________________________________
From: "George McNutt" <gmcnutt(at)intergate.ca>
Subject: Airport Problems
Date: Nov 02, 2002
-----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Jim Norman Subject: RV-List: Airport Problems OK Listers, here's a new problem... I'm putting my wings on my plane in a hanger that I rent. I have been based at this airport for almost 8 years (I have an Archer). The airport manager (without ANY warnings) shows up yesterday with eviction papers giving me 5 days to clean out the hangar. Why? Because we are "building an airplane" at the airport and this is not allowed. Of course, my plane was "built" at home, painted in a shop, and transported to the airport ready to bolt together. Its done except for wings, ailerons, and flaps. Also, of course, there are a dozen or more experimentals at this airport. Some, being built from scratch at the airport. Bottom line, after begging (and other distasteful measures) I was allowed to keep the hangar, but only for a "completed" airplane. They gave me 24 hours to get rid of the plane "parts". I have complied with this (what a pain in the butt). They even demanded that a work bench and all tools be removed. Their issue "insurance". "What happens if your plane falls on you and you get crushed and hold us liable?" Of course, of the $419 a month I pay for a hangar, $23.00 goes to "insurance" (its a line item). My plane is insured with builder's insurance (John Helms, are you reading this?). (I think there may be some more underlying issues, but I can't put my finger on them yet). Questions: 1) Has anybody heard of this before? 2) When is the plane a plane? When it has wings but not flaps? Wings and flaps but not ailerons? Fuselage and wings, but no avionics? They are quoting a clause that says "no airplane repairs shall be undertaken in areas not designated for such repairs, except for routine maintenance". Need some advice here... don't want to set a precedence for this airport that may spread. jim Tampa Vandenberg Airport VDF (near Sun-N-Fun, so don't come here on your way to Sun-n-Fun). --------------------------------- Hi Jim Read your rental/lease agreement very carefully, what does it say? Are all aircraft in hangars required to have a current CofA? Are there commercial maintenance operations on the airport, do they take parts off and put them back on, do they have the same rental/lease agreements as you?? If there are commercial operations are they paying the same (proportional) lease rates as you? Do the commercial operations pay the same (proportional) insurance fees? Our airport CYNJ has different (double) rates for commercial leases. What does the lease/rental agreement say about termination? And is the workbench permanently attached to the building (illegal modification to building ) or on wheels (temporary aircraft related acessory). It should all be there in the lease fine print. Depending on these and other questions do you have grounds to sue (or at least threaten) for breach of contract?? Did I say read the rental/lease agreement very very carefully?? One option might be to rent space in a commercial hangar to get the wings and tail on, then surely it would be ok to have a assembled aircraft without a current CofA in your hangar. George McNutt Langley BC Beautiful sunney day, going flying! ________________________________________________________________________________
Date: Nov 02, 2002
From: Gert <gert(at)execpc.com>
rv-list
Subject: engine storage
Hi Folks I just bought a used io-360-a1b and want to store it for a while, I have it sitting on a engine stand, flange down. I expect to be at least a year away from starting it. I took the fuel injector part off of the sump and capped the sump air inlet, I also took off the magneto's, starter, alternator and fuel pump and made aluminum plates to cover those holes. would it be advisable to plug the open end of the crank shaft?? will oil seep out past the collar into the crank cavety?? should I take out the valve push rods so as to aliviate having at least one valve half open and the tappet pushing on the cam lobe ?? I am thinking of pouring the engine full of oil to prevent rust from forming as I am not sure I can control the humidety in my detached garage and would like to preserve the camshaft. for storage only, can I fill the engine with just cheap car oil, got gallons of that stuff so would be convienent. how much oil goes in approximately?? anybody found unexpected leakage points....I found one so far, the nose seal leaks a bit :-( and am planning to replace this before I pour the storage oil in. ah, questions, questions, questions .............. Thanks Gert -- is subject to a download and archival fee in the amount of $500 ________________________________________________________________________________
From: "Elsa & Henry" <elsa-henry@darlor-watch.com>
Subject: Re: RV6A Wing attachment question
Date: Nov 02, 2002
Looking at my posting as displayed in the RV listing, apparently a couple of "ALT" characters I used were not recognized by the e-mail processing down stream: The out-board bolts referred to are the 1/4" ones and the bend in the ring-wrench is 90 degrees. Pressing and holding "ALT" then typing "172" (on the numeric key-pad) produces a nice compact 1/4 when the keys are released. Similarly, "ALT 167" produces the nice small "o" degree sign. Try it! Henry ________________________________________________________________________________
Date: Nov 03, 2002
From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)mcleodusa.net>
Subject: Re: Airport Problems
Cy Galley wrote: > > Phil, > I don't think you comments about the Illinois Aeronautical Department are > true. I am based at Moline, Illinois and have no problems and neither do > any of the other many experimentals based as our class C airport. We have > built, assembled, and test flown several in just this last year. Everything > from a RV-4 to an L-29 Jet. No insurance requirement either. It all > depends on the airport commissioner or board. > > Cy Galley > Editor, EAA Safety Programs > cgalley(at)qcbc.org or experimenter(at)eaa.org > > ----- Original Message ----- > From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)mcleodusa.net> > To: > Subject: Re: RV-List: Airport Problems > > > > > > Jim Norman wrote: > > > > > > > > > OK Listers, here's a new problem... > > > > > > I'm putting my wings on my plane in a hanger that I rent. I have been > based > > > at this airport for almost 8 years (I have an Archer). > > > > > > The airport manager (without ANY warnings) shows up yesterday with > eviction > > > papers giving me 5 days to clean out the hangar. Why? Because we are > > > "building an airplane" at the airport and this is not allowed. Of > course, > > > my plane was "built" at home, painted in a shop, and transported to the > > > airport ready to bolt together. Its done except for wings, ailerons, > and > > > flaps. > > > > > > Also, of course, there are a dozen or more experimentals at this > airport. > > > Some, being built from scratch at the airport. > > > > > > Bottom line, after begging (and other distasteful measures) I was > allowed to > > > keep the hangar, but only for a "completed" airplane. They gave me 24 > hours > > > to get rid of the plane "parts". I have complied with this (what a pain > in > > > the butt). They even demanded that a work bench and all tools be > removed. > > > > > > Their issue "insurance". "What happens if your plane falls on you and > you > > > get crushed and hold us liable?" Of course, of the $419 a month I pay > for a > > > hangar, $23.00 goes to "insurance" (its a line item). My plane is > insured > > > with builder's insurance (John Helms, are you reading this?). (I think > > > there may be some more underlying issues, but I can't put my finger on > them > > > yet). > > > > > > Questions: 1) Has anybody heard of this before? 2) When is the plane a > > > plane? When it has wings but not flaps? Wings and flaps but not > ailerons? > > > Fuselage and wings, but no avionics? They are quoting a clause that > says > > > "no airplane repairs shall be undertaken in areas not designated for > such > > > repairs, except for routine maintenance". > > > > > > Need some advice here... don't want to set a precedence for this airport > > > that may spread. > > > > > > jim > > > Tampa > > > Vandenberg Airport VDF (near Sun-N-Fun, so don't come here on your way > to > > > Sun-n-Fun). > > > > > > > I thought for a minute you were going to say you were in Illinois. The > small > > city owned airprts around here pull the same stuff. Usually it is dictated > to > > them from Illinois Deptartment of Transportation, Aeronautics.. > > The State wants to have the final say so in small airport management, I > guess so > > they can justify their Fat State Paychecks....... > > > > Phil, Litchfield, IL building RV-6, flying Pitt's S1S > > > > > I think I am referring more to the small town airports. The larger towns like yours seem to have a hold on their property, I can cite many instances of little town airports letting IDOT aeronautics dictate to them. ... Phil ________________________________________________________________________________
Date: Nov 02, 2002
From: Ken Balch <kbalch1(at)attbi.com>
Subject: Re: Technical education
Hi Dan, I'm currently attending a Part 147 AMT school in pursuit of my A&P. Please contact me off-list with specific questions and I'll be happy to address them directly. Regards, Ken Balch RV-8 N118KB Dan Ahearn wrote: > >Listers .... > >Were can I learn more about the A&P rating? > >I've been curious what goes into the A&P rating. While I recognize it's not necessary for what I'm about to embark upon, it seems to me that all this effort I intend to put into my airplane might allow me to apply work towards an A&P. > >Any advise or links greatly appreciated > >Dan >Highland Village, TX > > > > ________________________________________________________________________________
From: Knicholas2(at)aol.com
Date: Nov 02, 2002
Subject: 0-320 E2D ad's?
Would any of you guys out there with access to such information look up and tell me of any AD's or service bulletins on a Lycoming 0-320E2D please. Thank you! Kim Nicholas ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Airport Problems
Date: Nov 02, 2002
Then get some help from the FAA and EAA. I hope you saw the FAA orders list in Carl Froehlich's message. He lists Randy Hansen is the contact man at EAA govt(at)eaa.org. I know Randy and he will provide great help. Just one more membership benefit of belonging to the EAA. Cy Galley Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org P.S. I think if I moved to Lacon, Illinois Marshal County Airport, I would not have your perceived State interference. Neil Pobanz does not behave in that manner. He is the FBO at that airport, the American Bonanza Tech, and works for us at EAA AirVenture. ----- Original Message ----- From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)mcleodusa.net> Subject: Re: RV-List: Airport Problems > > Cy Galley wrote: > > > > > Phil, > > I don't think you comments about the Illinois Aeronautical Department are > > true. I am based at Moline, Illinois and have no problems and neither do > > any of the other many experimentals based as our class C airport. We have > > built, assembled, and test flown several in just this last year. Everything > > from a RV-4 to an L-29 Jet. No insurance requirement either. It all > > depends on the airport commissioner or board. > > > > Cy Galley > > Editor, EAA Safety Programs > > cgalley(at)qcbc.org or experimenter(at)eaa.org > > > > ----- Original Message ----- > > From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)mcleodusa.net> > > To: > > Subject: Re: RV-List: Airport Problems > > Club" > > > > > > > > Jim Norman wrote: > > > > > > > > > > > > > OK Listers, here's a new problem... > > > > > > > > I'm putting my wings on my plane in a hanger that I rent. I have been > > based > > > > at this airport for almost 8 years (I have an Archer). > > > > > > > > The airport manager (without ANY warnings) shows up yesterday with > > eviction > > > > papers giving me 5 days to clean out the hangar. Why? Because we are > > > > "building an airplane" at the airport and this is not allowed. Of > > course, > > > > my plane was "built" at home, painted in a shop, and transported to the > > > > airport ready to bolt together. Its done except for wings, ailerons, > > and > > > > flaps. > > > > > > > > Also, of course, there are a dozen or more experimentals at this > > airport. > > > > Some, being built from scratch at the airport. > > > > > > > > Bottom line, after begging (and other distasteful measures) I was > > allowed to > > > > keep the hangar, but only for a "completed" airplane. They gave me 24 > > hours > > > > to get rid of the plane "parts". I have complied with this (what a pain > > in > > > > the butt). They even demanded that a work bench and all tools be > > removed. > > > > > > > > Their issue "insurance". "What happens if your plane falls on you and > > you > > > > get crushed and hold us liable?" Of course, of the $419 a month I pay > > for a > > > > hangar, $23.00 goes to "insurance" (its a line item). My plane is > > insured > > > > with builder's insurance (John Helms, are you reading this?). (I think > > > > there may be some more underlying issues, but I can't put my finger on > > them > > > > yet). > > > > > > > > Questions: 1) Has anybody heard of this before? 2) When is the plane a > > > > plane? When it has wings but not flaps? Wings and flaps but not > > ailerons? > > > > Fuselage and wings, but no avionics? They are quoting a clause that > > says > > > > "no airplane repairs shall be undertaken in areas not designated for > > such > > > > repairs, except for routine maintenance". > > > > > > > > Need some advice here... don't want to set a precedence for this airport > > > > that may spread. > > > > > > > > jim > > > > Tampa > > > > Vandenberg Airport VDF (near Sun-N-Fun, so don't come here on your way > > to > > > > Sun-n-Fun). > > > > > > > > > > I thought for a minute you were going to say you were in Illinois. The > > small > > > city owned airprts around here pull the same stuff. Usually it is dictated > > to > > > them from Illinois Deptartment of Transportation, Aeronautics.. > > > The State wants to have the final say so in small airport management, I > > guess so > > > they can justify their Fat State Paychecks....... > > > > > > Phil, Litchfield, IL building RV-6, flying Pitt's S1S > > > > > > > > > > I think I am referring more to the small town airports. The larger towns like > yours seem to have a hold on their property, I can cite many instances of little > town airports letting IDOT aeronautics dictate to them. ... Phil > > ________________________________________________________________________________
From: "Will & Lynda Allen" <linenwool(at)attbi.com>
Subject: Builders Bench plans
Date: Nov 02, 2002
I heard there are some plans for a re-configurable building bench out there somewhere. Can someone point me in the right direction? I need more work bench space in my garage already. (sorry wife, you'll have to park outside now, must build airplane!) :) Thanks, Will Allen RV8 emp. North Bend, WA ________________________________________________________________________________
From: "Ed Bundy" <ebundy(at)velocitus.net>
Subject: Re: engine storage
Date: Nov 02, 2002
Filling the engine with oil is a great way to keep things in good shape. The cheapest car oil you can find is fine (clean of course) and I seem to remember putting in most of 3 cases (!) before that sucker finally filled up. Put a pan or something underneath it because oil will find it's way out during storage. Ed Bundy RIVA 500+ hours Boise, ID > for storage only, can I fill the engine with just cheap car oil, got > gallons of that stuff so would be convienent. > > how much oil goes in approximately?? > ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: 0-320 E2D ad's?
Date: Nov 02, 2002
Go to: http://www2.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/MainFram e?OpenFrameSet If the URL wraps in email and you can't click on it, use this one instead: http://checkoway.com/url/?s=c051945 Click on "ADs by Make" on the left side, then click "T". Click the blue triangle next to "Textron Lycoming, AVCO Corporation". Click "More Data..." at the end of the page a couple of times, then click the blue triangle next to "O-320-E2D". Here's the heading list, for what it's worth: 98-17-11 10/19/98 Crankshafts 98-02-08 03/30/98 Crankshaft 96-09-10 07/15/96 Oil pump 95-26-02 01/24/96 Aviation Gasoline 87-10-06 R1 09/01/89 Rocker Arm Assembly 75-08-09 R3 08/18/77 Oil Pump Drive Shaft 73-23-01 R4 01/13/77 Piston Pin Assembly 66-20-04 08/27/66 Oil Filter Adapter Gasket 64-16-05 07/10/64 AC Pumps 63-23-02 R1 08/06/68 Exhaust Valves 59-10-07 Upon Receipt Cylinder Baffle Clamps 55-02-02 Upon Receipt Gasket )_( Dan RV-7 N714D (fuselage) http://www.rvproject.com ----- Original Message ----- From: <Knicholas2(at)aol.com> Subject: RV-List: 0-320 E2D ad's? > > Would any of you guys out there with access to such information look up and > tell me of any AD's or service bulletins on a Lycoming 0-320E2D please. > > Thank you! > > Kim Nicholas > > ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Airport Problems
Date: Nov 02, 2002
Who owns the hangars - the airport or the FBO? To whom do you pay your rent? Bruce Glasair III -----Original Message-----


October 28, 2002 - November 02, 2002

RV-Archive.digest.vol-ns