RV-Archive.digest.vol-rw

April 18, 2006 - April 27, 2006



      
      >
      > First question, where's a good place to put this in
      > the stream of fuel?  I'm not too savvy on injected
      > engines.
      >
      > While talking with Electronics International today, I
      > was told that since there is a return of unused fuel,
      > I'll need TWO transducers and a little box that
      > computes the unused fuel.  This adds about $300 to the
      > price of my fuel flow, and am wondering if it's worth
      > it now.  Thoughts?
      >
      > Paul Besing
      > RV-4
      > N73DD
      > Arizona (For Now)
      >
      >
      > 
      
      
________________________________________________________________________________
From: "DonVS" <dsvs(at)comcast.net>
Subject: Fuel Flow Transducer-Injected
Date: Apr 18, 2006
Paul, The AFP has no return. The purge valve is not used during noemal operations and this is the only source of returned fuel. Between the servo and the flow divider is the best spot and I like Alex's idea of bringing thewe lines to the firewall. Don -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Paul Besing Sent: Tuesday, April 18, 2006 6:53 PM To: rv-list(at)matronics.com.1.12.SUBJ_HAS_UNIQ_ID.Subject.contains.a.unique.ID Subject: RV-List: Fuel Flow Transducer-Injected First question, where's a good place to put this in the stream of fuel? I'm not too savvy on injected engines. While talking with Electronics International today, I was told that since there is a return of unused fuel, I'll need TWO transducers and a little box that computes the unused fuel. This adds about $300 to the price of my fuel flow, and am wondering if it's worth it now. Thoughts? Paul Besing RV-4 N73DD Arizona (For Now) ________________________________________________________________________________
From: "Jerry Calvert" <rv6(at)cox.net>
Subject: Re: Dakotas
Date: Apr 18, 2006
My wife and I are planning a trip to South Dakota in July. Will be staying over at Custer County Airport http://www.airnav.com/airport/KCUT which is southwest of Rapid City. Plenty of places to stay, state parks with wild life, Mount Rushmore nearby, Black hills country, should be places to camp. Rental cars are available. Jerry Calvert RV 6 N296JC Edmond Ok ----- Original Message ----- From: "Jimmy Hill" <jimmy(at)jhill.biz> Sent: Tuesday, April 18, 2006 7:07 PM Subject: RV-List: Dakotas > > Fellow RV'ers: > > My son and I plan a flight in our 8A this weekend from Okla. up to the Dakotas, and surrounding areas. > Would appreciate knowing of any RV friendly locations--good sightseeing, possibly airport camping spots, etc. > > Thanks. > Jimmy > > ________________________________________________________________________________
From: Dwight Frye <dwight(at)openweave.org>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 18, 2006
On Tue Apr 18 22:10:46 2006, Alex Peterson wrote : >> First question, where's a good place to put this in the >> stream of fuel? I'm not too savvy on injected engines. >> >> While talking with Electronics International today, I was >> told that since there is a return of unused fuel, I'll need >> TWO transducers and a little box that computes the unused >> fuel. This adds about $300 to the price of my fuel flow, and >> am wondering if it's worth it now. Thoughts? >> >> Paul Besing >> RV-4 >> N73DD >> Arizona (For Now) > >Paul, put it in the line between the servo and flow divider. You'll have to >add a hose, and you may need to bring those lines back to the firewall. > >For others paying attention, not all fuel injection systems have this return >line (Airflow Performance, for one), making the installation as simple as a >carb with respect to fuel lines. According to the folks at Airflow Performance, Alex is right on the money regarding where to install the transducer. I don't know what FI system you are using, but with the API system there is no return line for _normal_ operation. There is a return line for the purge valve but that is only used pre-start to purge vapor from the lines, and at shutdown to _positively_ terminate fuel flow to the flow divider (and thus insure a clean shutdown of the engine). The API opinion on the amount of fuel returned is that it is so little (startup and shutdown) that putting a Flowscan on the return line would be of little benefit. I learned all these little tidbits at the FI-101 class I took at the API facility. If you really want to know about fuel injection basics and are within striking distance of Spartanburg, SC ... I'd recommend it highly. I'm not affiliated, but am a satisfied customer. :) Hope this helps. -- Dwight ________________________________________________________________________________
Date: Apr 18, 2006
Subject: Helmet & Headset ponderings
From: Mark E Navratil <czechsix(at)juno.com>
Guys, I've been enjoying my trusty helmet but as the wx turns warmer I'm thinking I'll probably break down and get a good ANR headset. The head bucket is just too hot to wear when it gets into the upper 80's and beyond. The other thing I've noticed is that the Oregon Aero earseals in my helmet get extremely soft with higher temps and don't seem to seal as well as they do in wintertime....they're very comfortable (as advertised) but the ANR has a hard time keeping up with the noise level and I find it bothersome after several hours in the air. FWIW I have the Headsets Inc ANR in my helmet earcups and I imagine there are better systems available from the likes of Bose and Lightspeed. So...I've been looking at ANR headsets and figure if I'm gonna spend some dough, might as well get a good one and only cry once. I'm sure Bose is the best but I can't quite believe the cost/benefit tradeoff is worth the $1K price tag. So I'm looking at Lightspeed's top-of-the-line Thirty 3G instead. It is cheap by comparison at about half the price of the Bose X (iPilot.com has the Thirty 3G for $559 with free shipping). Couple questions: does anybody know if Lightspeed might have a better deal available at Oshkosh? If they have really good show specials it might be worth waiting... Also, any pireps on the Thirty 3G series or similar high-end Lightspeed model would be appreciated. In general I've heard that Lightspeed headsets are comfortable and work well, sometimes break but have good factory support to replace parts. One of my hangarmates has a pair of well-used Lightspeeds that have the thin covering pealing away from the foam earseals and head cushions. Still works but looks like crap... Thanks as always for the input, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D flying 25.0 hours now, first oil change just completed... ________________________________________________________________________________
Date: Apr 18, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Fuel Flow Transducer-Injected
Contrary to the fuel return on my airplane. Not sure what type of injection it is, but the fuel return is substantial in flight. I've run 30 mins on the left tank, and after 30 mins on the right tank, the left tank is full again. Paul Besing > The API opinion on the amount of fuel returned is > that it is so little > (startup and shutdown) that putting a Flowscan on > the return line would > be of little benefit. ________________________________________________________________________________
Date: Apr 18, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Helmet & Headset ponderings
Having worn helmets in hot helicopters in the Alabama humidity in the summer time, I know what you mean. At least what I fly now is air conditioned, but wearning helmets does get old. I know you were not thinking of Bose because of price, but in 4 years and 1000 hours of flying, no problems, so I haven't needed the support. I flight instructed with them in the hot AZ heat in the summer time, they took a beating and don't even show the slightest wear in the ear seals or anything. I know lightspeed has great customer service, but personally, I'd rather not have to use customer service and never have a problem. I've seen threads like this and I find it very humerous when people write, "I've shipped them back 4 times and their customer service is great..new ear seals and all!" Sorry, but I don't care if your customer service is great if you make a product that breaks. I don't get the whole lightspeed craze. Sure, they make a good quality ANR, but I find them bulky, and the plastic just seems chincy and delicate to me, which seems to be substantiated with all the claims of their customer service and repair history. Plus, with the Bose, you can't beat the music or comfort quality. So much that when I bought my RV-4, I splurged and bought a second pair. No interest payments from Bose...I know, payments on a headset? Worth every stinkin penny, IMHO. Paul Besing --- Mark E Navratil wrote: > > > Guys, > > I've been enjoying my trusty helmet but as the wx > turns warmer I'm > thinking I'll probably break down and get a good ANR > headset. The head > bucket is just too hot to wear when it gets into the > upper 80's and > beyond. The other thing I've noticed is that the > Oregon Aero earseals in > my helmet get extremely soft with higher temps and > don't seem to seal as > well as they do in wintertime....they're very > comfortable (as advertised) > but the ANR has a hard time keeping up with the > noise level and I find it > bothersome after several hours in the air. FWIW I > have the Headsets Inc > ANR in my helmet earcups and I imagine there are > better systems available > from the likes of Bose and Lightspeed. > > So...I've been looking at ANR headsets and figure if > I'm gonna spend some > dough, might as well get a good one and only cry > once. I'm sure Bose is > the best but I can't quite believe the cost/benefit > tradeoff is worth the > $1K price tag. So I'm looking at Lightspeed's > top-of-the-line Thirty 3G > instead. It is cheap by comparison at about half > the price of the Bose X > (iPilot.com has the Thirty 3G for $559 with free > shipping). > > Couple questions: does anybody know if Lightspeed > might have a better > deal available at Oshkosh? If they have really good > show specials it > might be worth waiting... > > Also, any pireps on the Thirty 3G series or similar > high-end Lightspeed > model would be appreciated. In general I've heard > that Lightspeed > headsets are comfortable and work well, sometimes > break but have good > factory support to replace parts. One of my > hangarmates has a pair of > well-used Lightspeeds that have the thin covering > pealing away from the > foam earseals and head cushions. Still works but > looks like crap... > > Thanks as always for the input, > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D flying 25.0 hours now, first oil change > just completed... > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Apr 19, 2006
Subject: Re: Helmet & Headset ponderings
In a message dated 4/18/2006 9:17:16 P.M. Pacific Daylight Time, czechsix(at)juno.com writes: I've been looking at ANR headsets and figure if I'm gonna spend some dough, might as well get a good one and only cry once. I'm sure Bose is the best but I can't quite believe the cost/benefit tradeoff is worth the $1K price tag. So I'm looking at Lightspeed's top-of-the-line Thirty 3G instead. It is cheap by comparison at about half the price of the Bose X (iPilot.com has the Thirty 3G for $559 with free shipping). ============================================ I have two Thirty 3Gs and they are okay although I hate the plastic and would encourage you to evaluate the ear seals (I didn't get good results from the new style ear seals, so I swapped them out for the older style). I would agree with others that the Bose X headsets are probably a superior product overall and if my stocks returned better numbers I would have splurged (invested) in Bose Xs as well, and with gas prices as high as they are we're not flying quite as much as we used to. GV (RV-6A N1GV O-360-A1A, C/S, Flying 780hrs, Silicon Valley, CA) ________________________________________________________________________________
From: "Bob Barrow" <bobbarrow10(at)hotmail.com>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
Dan, I thought you put your fuel transducer just after the AFP boost pump on the cabin floor. Are you now unhappy with the results from that position. >From: "Dan Checkoway" <dan(at)rvproject.com> >Reply-To: rv-list(at)matronics.com >To: >Subject: Re: RV-List: Fuel Flow Transducer-Injected Date: Tue, 18 Apr 2006 > > >In the metered fuel line between the servo and flow divider is about as >ideal a spot as any imho. > >)_( Dan >RV-7 N714D >http://www.rvproject.com > >----- Original Message ----- >From: "Paul Besing" <pbesing(at)yahoo.com> >To: > >Sent: Tuesday, April 18, 2006 6:53 PM >Subject: RV-List: Fuel Flow Transducer-Injected > > > > > > First question, where's a good place to put this in > > the stream of fuel? I'm not too savvy on injected > > engines. > > > > While talking with Electronics International today, I > > was told that since there is a return of unused fuel, > > I'll need TWO transducers and a little box that > > computes the unused fuel. This adds about $300 to the > > price of my fuel flow, and am wondering if it's worth > > it now. Thoughts? > > > > Paul Besing > > RV-4 > > N73DD > > Arizona (For Now) > > > > > > > > > > > > > > > > > > > > > > > > > > > > http://mobilecentral.ninemsn.com.au/mcmobileHotmail/home.aspx ________________________________________________________________________________
Date: Apr 19, 2006
Subject: Re: Helmet & Headset ponderings
From: "Larry Bowen" <Larry(at)bowenaero.com>
Another option priced in between the two you are considering: http://www.telex.com/aircraft/products.nsf/pages/Stratus50Digital -- Larry Bowen Larry(at)BowenAero.com http://BowenAero.com Vanremog(at)aol.com said: > > > In a message dated 4/18/2006 9:17:16 P.M. Pacific Daylight Time, > czechsix(at)juno.com writes: > > I've been looking at ANR headsets and figure if I'm gonna spend some > dough, might as well get a good one and only cry once. I'm sure Bose is > the best but I can't quite believe the cost/benefit tradeoff is worth the > $1K price tag. So I'm looking at Lightspeed's top-of-the-line Thirty 3G > instead. It is cheap by comparison at about half the price of the Bose X > (iPilot.com has the Thirty 3G for $559 with free shipping). > > > ============================================ > > I have two Thirty 3Gs and they are okay although I hate the plastic and > would encourage you to evaluate the ear seals (I didn't get good results > from the > new style ear seals, so I swapped them out for the older style). I would > agree with others that the Bose X headsets are probably a superior > product > overall and if my stocks returned better numbers I would have splurged > (invested) > in Bose Xs as well, and with gas prices as high as they are we're not > flying > quite as much as we used to. > > > GV (RV-6A N1GV O-360-A1A, C/S, Flying 780hrs, Silicon Valley, CA) > > ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
> Dan, I thought you put your fuel transducer just after the AFP boost pump > on > the cabin floor. Are you now unhappy with the results from that position. I did, and I don't have any problems. But it's not the best location from a "scientific" standpoint. ;-) Pressure drop across the transducer when it's on the suction side means more chances of vapor lock. And why not put it where it "matters" most for accuracy? In the metered fuel line is ideal from what I understand, since it's under positive pressure (as opposed to suction), and it's measuring the ACTUAL flow of fuel to the cylinders. Just my 2 cents. )_( Dan RV-7 N714D http://www.rvproject.com ________________________________________________________________________________
From: "Glen Matejcek" <aerobubba(at)earthlink.net>
Subject: Helmet & Headset ponderings, Oshkosh deals
Date: Apr 19, 2006
Hi Mark, et al- RE: does anybody know if Lightspeed might have a better deal available at Oshkosh? FWIW, I bought a pair of Sennheisers ANR's at just under $400 each at OSH. I'm not airborne yet so I can't speak definitively on their performance, but I believe it to be quite good. Also, as a general rule, I make sure the vendors know I'm seriously comparison shopping. I'll grid out my wish list with my shopping list down the edge of the paper, and vendors across the top. I fill in the squares as I talk to them. At least one, usually Pacific Coast Avionics, will cut to the chase and make me an offer I can't refuse. It may sound silly or trite, but I've saved a whoooole lot of money that way. As ever, FWIW- Glen Matejcek aerobubba(at)earthlink.net ________________________________________________________________________________
From: "Dean Van Winkle" <dvanwinkle(at)royell.net>
Subject: Re: OT - AOPA donation-solicitation phone calls
Date: Apr 19, 2006
Matt and Dale I believe that this is the third year in a row that I have had a solicitation call from AOPA Air Safety Foundation. Each time I have told them to send a notice to me and I will respond with a check, just to ensure that it is a legitimate call. They respond promptly. I plan to attend one of their Safety Seminars in Springfield, Illinois next week. I agree that AOPA is a good cause. Dean Van Winkle RV-9A Fuselage/Finish ----- Original Message ----- From: "Matt Dralle" <dralle(at)matronics.com> Sent: Tuesday, April 18, 2006 12:03 PM Subject: Re: RV-List: OT - AOPA donation-solicitation phone calls > > At 04:18 AM 4/18/2006 Tuesday, you wrote: >> >> >>Have been a member of AOPA for 20 years and do not remember ever getting a >>phone solicitation from them. Is this a scam? >>Dale Ensing >>do not achieve > > No, I don't think it is. I got a "reminder call" last year too and it was > legit. They are pretty persistent, that's for sure. Its a good cause, > though, if you value your right to fly in the US. > > Matt > > > 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 > > > ________________________________________________________________________________
Date: Apr 19, 2006
From: Phil Birkelbach <phil(at)petrasoft.net>
Subject: Re: Fuel Flow Transducer-Injected
I mounted mine in basically the same position that Dan did except that mine is further forward and attached to the floor. I plan to move it this weekend to where Dan put his. I think that the vibration on the floor is causing it to be WAY off. It shows about 10% higher rate than what I am actually flowing and turning the boost pump on will give it another 10% on top of that. With the airplane sitting in the hangar it's right on the money. Dan, How did you attach yours? Is it bolted to something or is the tubing holding it? Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB http://www.myrv7.com Dan Checkoway wrote: > > > >>Dan, I thought you put your fuel transducer just after the AFP boost pump >>on >>the cabin floor. Are you now unhappy with the results from that position. >> >> > >I did, and I don't have any problems. But it's not the best location from a >"scientific" standpoint. ;-) Pressure drop across the transducer when it's >on the suction side means more chances of vapor lock. And why not put it >where it "matters" most for accuracy? In the metered fuel line is ideal >from what I understand, since it's under positive pressure (as opposed to >suction), and it's measuring the ACTUAL flow of fuel to the cylinders. > >Just my 2 cents. > >)_( Dan >RV-7 N714D >http://www.rvproject.com > > > > > > > > > ________________________________________________________________________________
Date: Apr 19, 2006
From: Matt Jurotich <mjurotich(at)hst.nasa.gov>
Subject: 6 A is flight level when?
I am near to getting my RV 6A back in the air after a complete electrical and panel rebuild. I plan on redoing weight and balance. With a slider is the top rail of the slider parallel to the top longeron? The top longeron is Van's reference for on the ground level. I presume the top longeron is "level" when in straight and level flight. Thanks Matthew M. Jurotich e-mail mail to: phone : 301-286-5919 ________________________________________________________________________________
Date: Apr 19, 2006
From: Sherman Butler <lsbrv7a(at)yahoo.com>
Subject: Re: Helmet & Headset ponderings
Headset pirep I started with a Sigtronics standard headset, and would miss calls. I bought a Light speed 20X and was really impressed with the difference, and eventually bought a 25X. Both headsets plastic parts broke on occasion, and when both were broken at the same time I decided to buy the new earpiece Lightspeeds. The delivery date was pushed back a couple of times so I canceled the order. I bought the Boise. The size difference is similar to the difference between a volleyball and a softball. They are the best. My radio problems essentially disappeared. Good communication with the tower. I feel much safer using the Boise headset, and highly recommend them. Sherman Butler RV-7a Empennage Idaho Falls --------------------------------- ________________________________________________________________________________
From: <erichweaver(at)cox.net>
Subject: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
SUBJ_HAS_UNIQ_ID Subject contains a unique ID My io-360B1B (vertical induction) from Aerosport Power came with the purge valve installed adjacent to the flow divider. I am tempted to remove it to avoid another fuel line and hole through the firewall, but havent yet. I was a little surprised to see that everyone had installed the fuel flow transducer in front of the firewall. Not that its bad mind you, just not where I installed mine. Mine is aft of the firewall, between the boost pump and the firewall, where it seems to fit nicely under the cover plate. Now you are all messing with my head making me feel uncomfortable! Anything wrong with my location? With the exception of the purge line, all the firewall forward fuel lines were pre-made, and supplied with my engine, so I didnt want to waste one of those by adding in the fuel transducer. Since I had to fabricate the fuel lines aft of the firewall anyway, it was an easy decision to put the transducer back there. Whats really throwing me is that Dan Checkoway's web site shows the transducer back by the fuel booster pump as well (see http://www.rvproject.com/20030520.html). But I see Dan is now recommending the firewall forward location as well? What gives? Somebody is messin' wit my head. ________________________________________________________________________________
From: Dwight Frye <dwight(at)openweave.org>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
The one down-side to installing the transducer where Dan his his (and as you noted he is now suggesting a new location too) is that it puts the transducer on the suction-side of the engine driven fuel pump. The transducer acts as a restriction in the line, and my understanding is that if you pull a fluid through a restriction you will have a pressure drop across the restriction. Given the rather low vapor pressure of avgas (or, gasoline in general) this reduces your margin of protection against vapor lock in the feed lines. It is possible (again, I am not an expert but am simply passing along some of the things I learned in a fuel injection class) that on a really hot day vapor could form on the engine-side of the transducer as the engine driven pump tries to pull fuel. This would be a "Bad Thing (tm)". :) Is this guaranteed to happen? No. Clearly many have flown with their fuel flow transducers on the suction side of the fuel pump without incident. But once the logic was outlined (and once some vapor pressure graphs were examined in detail) I have made the decision to install my transducer in the line between the throttle-body and the flow divider. YMMV. -- Dwight On Wed Apr 19 12:16:08 2006, erichweaver(at)cox.net wrote : >My io-360B1B (vertical induction) from Aerosport Power came with the purge valve installed adjacent to the flow divider. I am tempted to remove it to avoid another fuel line and hole through the firewall, but havent yet. > >I was a little surprised to see that everyone had installed the fuel flow transducer in front of the firewall. Not that its bad mind you, just not where I installed mine. Mine is aft of the firewall, between the boost pump and the firewall, where it seems to fit nicely under the cover plate. Now you are all messing with my head making me feel uncomfortable! Anything wrong with my location? > >With the exception of the purge line, all the firewall forward fuel lines were pre-made, and supplied with my engine, so I didnt want to waste one of those by adding in the fuel transducer. Since I had to fabricate the fuel lines aft of the firewall anyway, it was an easy decision to put the transducer back there. > >Whats really throwing me is that Dan Checkoway's web site shows the transducer back by the fuel booster pump as well (see http://www.rvproject.com/20030520.html). But I see Dan is now recommending the firewall forward location as well? What gives? Somebody is messin' wit my head. ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
Eric, I too have an IO-360-B1B with Airflow Performance fuel injection. (You didn't say who made the fuel injection, but I am assuming it is Airflow Performance). There was some discussion on this list awhile back about this, but the purge valve is apparently necessary to shut the engine down. The engine shutdown checklist says to leave the mixture at full-rich and put the purge valve control to off position. Page 21 of my Airflow Performance manual says that when the mixture is at idle cut-off, there is "approximately 1.0 to 3.0 pph leakage in this position" which is apparently enough to keep the engine running. Terry RV-8A #80729 Baffles Seattle -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of erichweaver(at)cox.net Sent: Wednesday, April 19, 2006 9:16 AM Subject: RV-List: Fuel Flow Transducer-Injected My io-360B1B (vertical induction) from Aerosport Power came with the purge valve installed adjacent to the flow divider. I am tempted to remove it to avoid another fuel line and hole through the firewall, but havent yet. I was a little surprised to see that everyone had installed the fuel flow transducer in front of the firewall. Not that its bad mind you, just not where I installed mine. Mine is aft of the firewall, between the boost pump and the firewall, where it seems to fit nicely under the cover plate. Now you are all messing with my head making me feel uncomfortable! Anything wrong with my location? With the exception of the purge line, all the firewall forward fuel lines were pre-made, and supplied with my engine, so I didnt want to waste one of those by adding in the fuel transducer. Since I had to fabricate the fuel lines aft of the firewall anyway, it was an easy decision to put the transducer back there. Whats really throwing me is that Dan Checkoway's web site shows the transducer back by the fuel booster pump as well (see http://www.rvproject.com/20030520.html). But I see Dan is now recommending the firewall forward location as well? What gives? Somebody is messin' wit my head. ________________________________________________________________________________
Date: Apr 19, 2006
From: Phil Birkelbach <phil(at)petrasoft.net>
Subject: Re: Fuel Flow Transducer-Injected
I think that all Dan is saying is that the "Theoretically Perfect" solution is between the servo and the flow divider, but there are more practical choices like putting it where you describe. Mine is smack in the middle of the floor between the boost pump and the firewall. It doesn't work very well and I'm gonna move it back to where Dan has his and see if that improves it any. It think it's picking up vibration and it's causing high readings. That floor shakes pretty good. BTW you will love that purge valve. I can start mine in two blades when it's heat soaked, and I like the idea of killing the engine with the purge valve instead of the mixture. It will completely bleed off the fuel pressure, so that there is no way fuel can get into the cylinders while sitting on the ramp. Seems much safer to me. I'd suggest installing a spring to pull the purge valve closed in case the control cable breaks. Also make sure that the control cable is of the locking variety and don't put it next to the cabin heat knob lest ye grab the wrong one whilst flying, and ruineth thy day. Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB http://www.myrv7.com erichweaver(at)cox.net wrote: > >My io-360B1B (vertical induction) from Aerosport Power came with the purge valve installed adjacent to the flow divider. I am tempted to remove it to avoid another fuel line and hole through the firewall, but havent yet. > >I was a little surprised to see that everyone had installed the fuel flow transducer in front of the firewall. Not that its bad mind you, just not where I installed mine. Mine is aft of the firewall, between the boost pump and the firewall, where it seems to fit nicely under the cover plate. Now you are all messing with my head making me feel uncomfortable! Anything wrong with my location? > >With the exception of the purge line, all the firewall forward fuel lines were pre-made, and supplied with my engine, so I didnt want to waste one of those by adding in the fuel transducer. Since I had to fabricate the fuel lines aft of the firewall anyway, it was an easy decision to put the transducer back there. > >Whats really throwing me is that Dan Checkoway's web site shows the transducer back by the fuel booster pump as well (see http://www.rvproject.com/20030520.html). But I see Dan is now recommending the firewall forward location as well? What gives? Somebody is messin' wit my head. > > > > > > > > > ________________________________________________________________________________
Date: Apr 19, 2006
From: Phil Birkelbach <phil(at)petrasoft.net>
Subject: Re: Throttle, Prop, and Mixture cable slack
I have quite a bit of slack in mine aft of the firewall and they work fine. I didn't measure it but it's probably close to what you describe. Just route it somewhere out of the way and keep the bend radius as large as possible. Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB http://www.myrv7.com Ralph E. Capen wrote: > >Fellow listers, > >I'm working on my firewall foreward and since I had already made some decisions before the firewall foreward kit was available, I can't use the stock locations for my throttle and mixture cables. The prop cable went in to the stock location nicely with the one hole eyeball fitting. > >There seems to be just a little slack in that cable - just enough to allow flexibility to keep it out of the way. > >How much should I have? Upon measuring the cables that I got for the throttle and mixture after putting them in where I could, I have 6" too much throttle cable and 7" too much mixture cable. These are straight shot from the panel/console to the eyeball passthrough the firewall. on the firewall side, I have sufficient 'Lycoming wet dog shake room'. I'm thinking on the aft side of the firewall, I don't need much wiggle room other than to avoid stuff that could get in the way and wear the cable. > >Your thoughts please, >Ralph >RV6AQB N822AR @ N06 - fun firewall foreward! > > > > > > > > > ________________________________________________________________________________
From: dsvs(at)comcast.net
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
-------------- Original message ---------------------- From: Phil Birkelbach <phil(at)petrasoft.net> I just talked to the techs at Air Flow Performance. They told me that the best place is between the servo and the purge valve. They also said that the transducer will work fine if you mount it vertically in that line. They claim that they do it all the time. I am going to try it that way and see how it works. They also said to not mount it on the engine. Don > I think that all Dan is saying is that the "Theoretically Perfect" > solution is between the servo and the flow divider, but there are more > practical choices like putting it where you describe. Mine is smack in > the middle of the floor between the boost pump and the firewall. It > doesn't work very well and I'm gonna move it back to where Dan has his > and see if that improves it any. It think it's picking up vibration and > it's causing high readings. That floor shakes pretty good. > > BTW you will love that purge valve. I can start mine in two blades when > it's heat soaked, and I like the idea of killing the engine with the > purge valve instead of the mixture. It will completely bleed off the > fuel pressure, so that there is no way fuel can get into the cylinders > while sitting on the ramp. Seems much safer to me. I'd suggest > installing a spring to pull the purge valve closed in case the control > cable breaks. Also make sure that the control cable is of the locking > variety and don't put it next to the cabin heat knob lest ye grab the > wrong one whilst flying, and ruineth thy day. > > Godspeed, > > Phil Birkelbach - Houston Texas > RV-7 N727WB > http//www.myrv7.com > > > > erichweaver(at)cox.net wrote: > > > > >My io-360B1B (vertical induction) from Aerosport Power came with the purge > valve installed adjacent to the flow divider. I am tempted to remove it to > avoid another fuel line and hole through the firewall, but havent yet. > > > >I was a little surprised to see that everyone had installed the fuel flow > transducer in front of the firewall. Not that its bad mind you, just not where > I installed mine. Mine is aft of the firewall, between the boost pump and the > firewall, where it seems to fit nicely under the cover plate. Now you are all > messing with my head making me feel uncomfortable! Anything wrong with my > location? > > > >With the exception of the purge line, all the firewall forward fuel lines were > pre-made, and supplied with my engine, so I didnt want to waste one of those by > adding in the fuel transducer. Since I had to fabricate the fuel lines aft of > the firewall anyway, it was an easy decision to put the transducer back there. > > > >Whats really throwing me is that Dan Checkoway's web site shows the transducer > back by the fuel booster pump as well (see > http://www.rvproject.com/20030520.html). But I see Dan is now recommending the > firewall forward location as well? What gives? Somebody is messin' wit my > head. > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Date: Apr 19, 2006
From: sportav8r(at)aol.com
Subject: Re: 6 A is flight level when?
That's (presumed to be) correct. Someday, I want to see numbers where someone has done their w&b with wheels level and with top longeron level, to see if the difference is truly worth worrying about. It's a lot of work to jack these planes into that configuration and chock the wheels and scales to correct heights (or dig a hole under the nosewheel ;-). I may do it myself if I get bored... -Stormy -----Original Message----- From: Matt Jurotich <mjurotich(at)hst.nasa.gov> Subject: RV-List: 6 A is flight level when? I am near to getting my RV 6A back in the air after a complete electrical and panel rebuild. I plan on redoing weight and balance. With a slider is the top rail of the slider parallel to the top longeron? The top longeron is Van's reference for on the ground level. I presume the top longeron is "level" when in straight and level flight. Thanks Matthew M. Jurotich e-mail mail to: phone : 301-286-5919 ________________________________________________________________________________
Date: Apr 19, 2006
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: Throttle, Prop, and Mixture cable slack
Phil, Thanks for your 'been there - done that' answer. I'll try it before I swap cables. Ralph -----Original Message----- >From: Phil Birkelbach <phil(at)petrasoft.net> >Sent: Apr 19, 2006 1:16 PM >To: rv-list(at)matronics.com >Subject: Re: RV-List: Throttle, Prop, and Mixture cable slack > > >I have quite a bit of slack in mine aft of the firewall and they work >fine. I didn't measure it but it's probably close to what you >describe. Just route it somewhere out of the way and keep the bend >radius as large as possible. > >Godspeed, > >Phil Birkelbach - Houston Texas >RV-7 N727WB >http://www.myrv7.com > > >Ralph E. Capen wrote: > >> >>Fellow listers, >> >>I'm working on my firewall foreward and since I had already made some decisions before the firewall foreward kit was available, I can't use the stock locations for my throttle and mixture cables. The prop cable went in to the stock location nicely with the one hole eyeball fitting. >> >>There seems to be just a little slack in that cable - just enough to allow flexibility to keep it out of the way. >> >>How much should I have? Upon measuring the cables that I got for the throttle and mixture after putting them in where I could, I have 6" too much throttle cable and 7" too much mixture cable. These are straight shot from the panel/console to the eyeball passthrough the firewall. on the firewall side, I have sufficient 'Lycoming wet dog shake room'. I'm thinking on the aft side of the firewall, I don't need much wiggle room other than to avoid stuff that could get in the way and wear the cable. >> >>Your thoughts please, >>Ralph >>RV6AQB N822AR @ N06 - fun firewall foreward! >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> > > > > > > > ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
> How did you attach yours? Is it bolted to something or is the tubing > holding it? It's resting on a silicone pad. The tubing is somewhat rigid. Mine is very accurate with the exception of when the boost pump is running. )_( Dan ________________________________________________________________________________
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 19, 2006
On 19 Apr 2006, at 11:52, Paul Besing wrote: > > Dont' really know...I've got the cowl off right now > and it's kind of confusing...which is why I asked the > question in the first place...I know that some Cessnas > have this feature (it goes into a 3rd small storage > tank in the cowl) and bonanzas do as well. > > So is it my understanding that I do not need this fuel > return? Seems like an aweful lot of fuel to not > return (maybe 1 gallon per hour). The plane was built > 17 years ago, and has been that way ever since, with 5 > owners, and no problems. Where is that fuel return line coming from? If it is coming from the fuel injection servo, which make and model servo is it? It may be coming from a pressure regulating valve that is part of the high pressure fuel pump. If that is the case, most people run the fuel return into a T in the fuel line from the fuel selector valve. A small number of people use an expensive fuel selector from Andair that has two valves controlled by one knob. That allows you to send the return fuel to whatever tank is currently providing fuel, which avoids the problem of over filling a tank with the return fuel. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: 6 A is flight level when?
Date: Apr 19, 2006
On 19 Apr 2006, at 10:19, Matt Jurotich wrote: > > I presume the top longeron is "level" when in straight and > level flight. The pitch attitude in straight and level flight will depend on the airspeed, weight and flap angle, and to a less extent, on CG. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
Date: Apr 19, 2006
From: Charlie Brame <chasb(at)satx.rr.com>
Subject: RE: Helmet & Headset ponderings
I have a pair of Lightspeed 20XLs that I have had about four years. The noise abatement capabilities are great and the headsets are super comfortable, if a bit bulky. After about three years I had to replace the ear pads because the thin leather deteriorated. Lightspeed sent me two new sets of ear pads at no cost, including shipping. I had the opportunity to compare my 20XLs with a Bose set. Up against my very noisy air compressor, one was slightly quieter with ANR turned off, and the other was slightly better using ANR. Unfortunately, I can't remember which did what. In both cases, the difference was minimal. The upshot is, the Lightspeeds were at least the equal of the much more expensive Bose. I will admit to never using a Bose set in the aircraft. Charlie Brame RV-6A N11CB San Antonio --------------------------------- > Subject: RV-List: Helmet & Headset ponderings > From: Mark E Navratil <czechsix(at)juno.com> > > > Guys, > > I've been enjoying my trusty helmet but as the wx turns warmer I'm > thinking I'll probably break down and get a good ANR headset. The head > bucket is just too hot to wear when it gets into the upper 80's and > beyond. The other thing I've noticed is that the Oregon Aero earseals in > my helmet get extremely soft with higher temps and don't seem to seal as > well as they do in wintertime....they're very comfortable (as advertised) > but the ANR has a hard time keeping up with the noise level and I find it > bothersome after several hours in the air. FWIW I have the Headsets Inc > ANR in my helmet earcups and I imagine there are better systems available > from the likes of Bose and Lightspeed. > > So...I've been looking at ANR headsets and figure if I'm gonna spend some > dough, might as well get a good one and only cry once. I'm sure Bose is > the best but I can't quite believe the cost/benefit tradeoff is worth the > $1K price tag. So I'm looking at Lightspeed's top-of-the-line Thirty 3G > instead. It is cheap by comparison at about half the price of the Bose X > (iPilot.com has the Thirty 3G for $559 with free shipping). > > Couple questions: does anybody know if Lightspeed might have a better > deal available at Oshkosh? If they have really good show specials it > might be worth waiting... > > Also, any pireps on the Thirty 3G series or similar high-end Lightspeed > model would be appreciated. In general I've heard that Lightspeed > headsets are comfortable and work well, sometimes break but have good > factory support to replace parts. One of my hangarmates has a pair of > well-used Lightspeeds that have the thin covering pealing away from the > foam earseals and head cushions. Still works but looks like crap... > > Thanks as always for the input, > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D flying 25.0 hours now, first oil change just completed... > > ________________________________________________________________________________
From: luckymacy(at)comcast.net (lucky)
Subject: Re: RE: Helmet & Headset ponderings
Date: Apr 19, 2006
Well, I can say I have compared both in the back of an RV8, in flight, side by side and my ears couldn't tell the difference as far as noise attenuation goes. However, the Bose was a much better fit for the back of an RV8. The canopy tapers and since they don't stick out in any direction much I never hit the canopy with them. Can't say that for the Lightspeeds. The Bose are also noticeably lighter and fold up and out of the way easier when not in use. I didn't fly long enough to appreciate that but I'm sure on a long CC the Bose would be easier on the ears and jaw. Was I impressed enough to buy the Bose for myself? Nope but they did make me appreciate a design that differs physically than the Lightspeeds. I instead bought the ANR version QFRXCc. Really good all around product and has the basic same slim profile of the Bose as compared to the Lightspeeds for the back seat. Plus they stay on your head better for aerobatics. They have a full range of features regardless of price. http://www.anrheadsets.com/productsqfrx2.asp Nothing drives an engineer up the wall like having options and making choices ;-) -------------- Original message -------------- From: Charlie Brame <chasb(at)satx.rr.com> > > I have a pair of Lightspeed 20XLs that I have had about four years. The > noise abatement capabilities are great and the headsets are super > comfortable, if a bit bulky. After about three years I had to replace > the ear pads because the thin leather deteriorated. Lightspeed sent me > two new sets of ear pads at no cost, including shipping. > > I had the opportunity to compare my 20XLs with a Bose set. Up against my > very noisy air compressor, one was slightly quieter with ANR turned off, > and the other was slightly better using ANR. Unfortunately, I can't > remember which did what. In both cases, the difference was minimal. The > upshot is, the Lightspeeds were at least the equal of the much more > expensive Bose. I will admit to never using a Bose set in the aircraft. > > Charlie Brame > RV-6A N11CB > San Antonio > > --------------------------------- > > > Subject: RV-List: Helmet & Headset ponderings > > From: Mark E Navratil > > > > > > Guys, > > > > I've been enjoying my trusty helmet but as the wx turns warmer I'm > > thinking I'll probably break down and get a good ANR headset. The head > > bucket is just too hot to wear when it gets into the upper 80's and > > beyond. The other thing I've noticed is that the Oregon Aero earseals in > > my helmet get extremely soft with higher temps and don't seem to seal as > > well as they do in wintertime....they're very comfortable (as advertised) > > but the ANR has a hard time keeping up with the noise level and I find it > > bothersome after several hours in the air. FWIW I have the Headsets Inc > > ANR in my helmet earcups and I imagine there are better systems available > > from the likes of Bose and Lightspeed. > > > > So...I've been looking at ANR headsets and figure if I'm gonna spend some > > dough, might as well get a good one and only cry once. I'm sure Bose is > > the best but I can't quite believe the cost/benefit tradeoff is worth the > > $1K price tag. So I'm looking at Lightspeed's top-of-the-line Thirty 3G > > instead. It is cheap by comparison at about half the price of the Bose X > > (iPilot.com has the Thirty 3G for $559 with free shipping). > > > > Couple questions: does anybody know if Lightspeed might have a better > > deal available at Oshkosh? If they have really good show specials it > > might be worth waiting... > > > > Also, any pireps on the Thirty 3G series or similar high-end Lightspeed > > model would be appreciated. In general I've heard that Lightspeed > > headsets are comfortable and work well, sometimes break but have good > > factory support to replace parts. One of my hangarmates has a pair of > > well-used Lightspeeds that have the thin covering pealing away from the > > foam earseals and head cushions. Still works but looks like crap... > > > > Thanks as always for the input, > > > > --Mark Navratil > > Cedar Rapids, Iowa > > RV-8A N2D flying 25.0 hours now, first oil change just completed... > > > > > > > > > > > > > > > > Well, I can say I have compared both in the back of an RV8, in flight, side by side and my ears couldn't tell the difference as far as noise attenuation goes. However, the Bose was a much better fit for the back of an RV8. The canopy tapers and since they don't stick out in any direction much I never hit the canopy with them. Can't say that for the Lightspeeds. The Bose are also noticeably lighter and fold up and out of the way easier when not in use. I didn't fly long enough to appreciate that but I'm sure on a long CC the Bose would be easier on the ears and jaw. Was I impressed enough to buy the Bose for myself? Nope but they did make me appreciate a design that differs physically than the Lightspeeds. I instead boughtthe ANR version QFRXCc. Really good all around product and has the basic same slim profile of the Bose as compared to the Lightspeeds for the back seat. Plus they stay on your head better for aerobatics. They have a full range of features regardless of price. http://www.anrheadsets.com/productsqfrx2.asp Nothing drives an engineer up the wall like having options and making choices ;-) -------------- Original message -------------- From: Charlie Brame chasb(at)satx.rr.com -- RV-List message posted by: Charlie Brame I have a pair of Lightspeed 20XLs that I have had about four years. The noise abatement capabilities are great and the headsets are super comfortable, if a bit bulky. After about three years I had to replace the ear pads because the thin leather deteriorated. Lightspeed sent me two new sets of ear pads at no cost, including shipping. I had the opportunity to compare my 20XLs with a Bose set. Up against my very noisy air compressor, one was slightly quieter with ANR turned off, and the other was slightly better using ANR. Unfortunately, I can't remember which did what. In both cases, the difference was minimal. The u pshot is, the Lightspeeds were at least the equal of the much more expensive Bose. I will admit to never using a Bose set in the aircraft. Charlie Brame RV-6A N11CB San Antonio --------------------------------- Subject: RV-List: Helmet Headset ponderings From: Mark E Navratil <CZECHSIX(at)JUNO.COM> -- RV-List message posted by: Mark E Navratil Guys, I've been enjoying my trusty helmet but as the wx turns warmer I'm thinking I'll probably break down and get a good ANR headset. The head bucket is just too hot to wear when it gets into the upper 80's and beyond. The other thing I've noticed is that the Oregon Aero earseals in my helmet get extremely soft with higher temps and don' t seem to seal as well as they do in wintertime....they're very comfortable (as advertised) but the ANR has a hard time keeping up with the noise level and I find it bothersome after several hours in the air. FWIW I have the Headsets Inc ANR in my helmet earcups and I imagine there are better systems available from the likes of Bose and Lightspeed. So...I've been looking at ANR headsets and figure if I'm gonna spend some dough, might as well get a good one and only cry once. I'm sure Bose is the best but I can't quite believe the cost/benefit tradeoff is worth the $1K price tag. So I'm looking at Lightspeed's top-of-the-line Thirty 3G instead. It is cheap by comparison at about half the price of the Bose X (iPilot.com has the Thirty 3G for $559 with free shipping). Couple questions: does a nybody know if Lightspeed might have a better deal available at Oshkosh? If they have really good show specials it might be worth waiting... Also, any pireps on the Thirty 3G series or similar high-end Lightspeed model would be appreciated. In general I've heard that Lightspeed headsets are comfortable and work well, sometimes break but have good factory support to replace parts. One of my hangarmates has a pair of well-used Lightspeeds that have the thin covering pealing away from the foam earseals and head cushions. Still works but looks like crap... Thanks as always for the input, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D flying 25.0 hours now, first oil change just completed... ===== ============================ &g t; ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)earthlink.net>
Subject: RE: Helmet & Headset ponderings
Date: Apr 19, 2006
As another data point, this was from a post I made to this list a couple years back comparing the high end Telex to the Bose: "Telex was a generous sponsor of our Twin Cities RV Forum last year. I already had been flying with a set of Bose X headsets for a couple years in my RV, so the Telex rep and I hopped in my plane for some real time comparisons. My honest assessment was this: The Telex utterly stopped all pulsatile engine noise, so much so that it was unnerving, to me at least. The Bose allow a low level of the engine noise to come through, such that I have really gotten used to "hearing" the plane as subtle changes in airspeed/power occur. My perception, and it may not be real, is that there was more hissing (from airflow around the plane) allowed through the Telex, but that would require instrumentation to determine. I felt that the Bose were more comfortable, but that is something that would take hours of comparison to really establish. I believe that the Telex model we had was about $100 less than the Bose X, but don't recall exactly. We talked about bringing some of their instrumentation aboard to really nail it, but we haven't done so as yet." Alex Peterson RV6-A N66AP 751 hours Maple Grove, MN ________________________________________________________________________________
From: "Tracy Crook" <lors01(at)msn.com>
Subject: Re: 6 A is flight level when?
Date: Apr 19, 2006
True, which brings up a related subject. Anyone know what the AOA of the 230xx airfoil on the RV is at any typical cruise speed? I need to make a decision on whether to change from stock RV incidence on my "long wing" RV-8. Span is 3 feet longer than stock which should result in a lower AOA for any given condition. I have a program to predict the appropriate change but don't know what it is to start with and haven't seen it in the plans book. Tracy Crook > > I presume the top longeron is "level" when in straight and > level flight. The pitch attitude in straight and level flight will depend on the airspeed, weight and flap angle, and to a less extent, on CG. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8> ________________________________________________________________________________
Date: Apr 19, 2006
From: Charlie Kuss <chaztuna(at)adelphia.net>
Subject: Re: Fuel Flow Transducer-Injected
Paul This has been discussed on the Yahoo RV8 List several times before. JPI has an Acrobat file installation manual. In it, they recommend installing the transducer between the servo and the fuel distributor. It gets installed in the middle of a flex hose, so it isn't subjected to all the vibration of the engine. Check out the document on the web link below. Look at page 8
http://www.jpinstruments.com/700-800_FF_install.PDF Charlie Kuss > >First question, where's a good place to put this in >the stream of fuel? I'm not too savvy on injected >engines. > >While talking with Electronics International today, I >was told that since there is a return of unused fuel, >I'll need TWO transducers and a little box that >computes the unused fuel. This adds about $300 to the >price of my fuel flow, and am wondering if it's worth >it now. Thoughts? > >Paul Besing >RV-4 >N73DD >Arizona (For Now) > > ________________________________________________________________________________
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: 6 A is flight level when?
Date: Apr 19, 2006
The AOA will be quite low. If the airfoil was a true 23013.5 series, and this was a 2D wing (i.e. there were no effects from the fuselage or wing tip, the AOA at 1600 lb, 212 mph at 8,000 ft would be about 0.3 degrees (value calculated by XFOIL). If we drop the cruise speed to 189 mph, the AOA would be about 0.6 degrees. I understand that the leading edge of the RV airfoil differs slightly from the NACA profile. And, the local AOA is not constant along the span, due to the effect of the fuselage and wing tip. So the above values must be considered as approximate. Kevin Horton On 19 Apr 2006, at 19:55, Tracy Crook wrote: > > True, which brings up a related subject. > > Anyone know what the AOA of the 230xx airfoil on the RV is at any > typical cruise speed? I need to make a decision on whether to > change from stock RV incidence on my "long wing" RV-8. Span is 3 > feet longer than stock which should result in a lower AOA for any > given condition. I have a program to predict the appropriate > change but don't know what it is to start with and haven't seen it > in the plans book. > > Tracy Crook > > >> > >> >> I presume the top longeron is "level" when in straight and >> level flight. > > The pitch attitude in straight and level flight will depend on the > airspeed, weight and flap angle, and to a less extent, on CG. > > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada > http://www.kilohotel.com/rv8> > > ________________________________________________________________________________
From: "Bob Barrow" <bobbarrow10(at)hotmail.com>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 20, 2006
I can understand that any restriction upstream of the engine fuel pump might tend to increase the possibility of vapour lock. However you would think that the AFP electric fuel boost pump itself would cause some sort of restriction....surely the filter would. And then there's the people who also use gascolators...or additional filters in the wing roots etc. Wouldn't all of these things create some degree of resistance to flow. Why is the fuel flow transducer being singled out...does it present an exceptional resistance to flow. Have there been any reported cases of vapour lock associated with locating the transducer upstream of the engine fuel pump....or is this just more "worry bucket" stuff. Does anybody have any pix of their fuel transducer mounted between the servo and the divider (and off the engine as has been recommended). Have the people who have done this had universally good metering results...despite the fact that they "may" not have the prerequisite 5" of straight line before and after the transducer and may not have it mounted vertically as recommended by the manufacturer. Decisions, decisions...phew. New year, new job there's more than 100,00 jobs at SEEK ________________________________________________________________________________
Subject: Re: 6 A is flight level when?
From: "bdjones1965" <rv_8pilot(at)hotmail.com>
Date: Apr 19, 2006
Tracy - Regarding the 3' longer wings, did you consider the change in flutter characteristics of the new wings? How about longitudinal stability? Not trying to be a downer on new ideas, but I would be very concerned about the change in resonance characteristics of the wing. And to a lesser degree the stability. Just curious Bryan Jones, PE, -8 Houston, Texas Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=29551#29551 ________________________________________________________________________________
From: "Jerry Isler" <jlisler(at)alltel.net>
Subject: Scott Crossfield
Date: Apr 19, 2006
Off topic post! DO NOT ARCHIEVE. Has anyone heard anything about Scott Crossfield going down around Rome, Georgia this morning? I caught the tail end of a news cast about this and have no other details. Jerry Isler Donalsonville, GA RV-4 N455J Cessna C140A N9641A ________________________________________________________________________________
From: "Randy Lervold" <randy(at)romeolima.com>
Subject: Re: 6 A is flight level when?
Date: Apr 19, 2006
The standard angle of incidence on the RV-4 and RV-8 is .5 degrees. The guppy planes (side-by-side) are 1.0 degrees. Curiously the RV-3 is also 1.0 degrees. Randy Lervold ----- Original Message ----- From: "Tracy Crook" <lors01(at)msn.com> Sent: Wednesday, April 19, 2006 4:55 PM Subject: Re: RV-List: 6 A is flight level when? > > True, which brings up a related subject. > > Anyone know what the AOA of the 230xx airfoil on the RV is at any typical > cruise speed? I need to make a decision on whether to change from stock > RV incidence on my "long wing" RV-8. Span is 3 feet longer than stock > which should result in a lower AOA for any given condition. I have a > program to predict the appropriate change but don't know what it is to > start with and haven't seen it in the plans book. > > Tracy Crook > > >> > >> >> I presume the top longeron is "level" when in straight and >> level flight. > > The pitch attitude in straight and level flight will depend on the > airspeed, weight and flap angle, and to a less extent, on CG. > > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada > http://www.kilohotel.com/rv8> > > > ________________________________________________________________________________
Subject: Re: Scott Crossfield
From: "N395V" <n395v(at)hughes.net>
Date: Apr 20, 2006
Home > News > Georgia > WXIA-TV Atlanta 4/20/2006 7:52:03 AM Legendary Pilot's Plane Missing Scott Crossfield The Federal Aviation Administration confirmed for 11Alive News Thursday that a plane missing in North Georgia belongs to a legendary test pilot. The missing plane is owned by 85-year-old Scott Crossfield, but officials are not certain that Crossfield was piloting the plane when it disappeared Wednesday. The Cessna was last seen on radar near Ellijah, Ga.. It left Prattville, Ala. on a flight to Virginia. The Civil Air Patrol's Georgia wing is conducting air and ground searches along the flight path, a spokesperson said. On Nov. 20, 1953, Crossfield became the first man to fly at twice the speed of sound as he piloted the Douglas D-558-II Skyrocket to a speed of 1,291 mph. He was inducted into the National Aviation Hall of Fame in 1983, the International Space Hall of Fame in 1988, and the Aerospace Walk of Honor in 1990. -------- Milt N395V F1 Rocket Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=29603#29603 ________________________________________________________________________________
From: <ceengland(at)bellsouth.net>
Subject: 6 A is flight level:thread shift: wing AOA
Date: Apr 20, 2006
Related to the nose varying from 'true': My -7 leading edges, both tank skins & outboard leading edges, actually have a 'dip' both above & below the nose. I've also seen this on other current kits. I called Van's tech guys & they basically didn't care. They just said it's an artifact of the LE forming process & refused to discuss any detrimental aerodynamic effects. Have any others noticed this? Has anyone actually tried to do something to correct it? Is it worth trying to correct (meaning is there a speed penalty for ignoring it)? If you want to check yours, run your fingers from the leading edge toward the trailing edge & if it's there, you'll feel a significant dip just back of the rolled leading edge. Charlie > > From: Kevin Horton <khorton01(at)rogers.com> > Date: 2006/04/19 Wed PM 08:24:27 CDT > To: rv-list(at)matronics.com > Subject: Re: RV-List: 6 A is flight level when? > > > The AOA will be quite low. If the airfoil was a true 23013.5 series, > and this was a 2D wing (i.e. there were no effects from the fuselage > or wing tip, the AOA at 1600 lb, 212 mph at 8,000 ft would be about > 0.3 degrees (value calculated by XFOIL). If we drop the cruise speed > to 189 mph, the AOA would be about 0.6 degrees. > > I understand that the leading edge of the RV airfoil differs slightly > from the NACA profile. And, the local AOA is not constant along the > span, due to the effect of the fuselage and wing tip. So the above > values must be considered as approximate. > > Kevin Horton > > On 19 Apr 2006, at 19:55, Tracy Crook wrote: > > > > > True, which brings up a related subject. > > > > Anyone know what the AOA of the 230xx airfoil on the RV is at any > > typical cruise speed? I need to make a decision on whether to > > change from stock RV incidence on my "long wing" RV-8. Span is 3 > > feet longer than stock which should result in a lower AOA for any > > given condition. I have a program to predict the appropriate > > change but don't know what it is to start with and haven't seen it > > in the plans book. > > > > Tracy Crook > > > > > >> > > >> > >> I presume the top longeron is "level" when in straight and > >> level flight. > > > > The pitch attitude in straight and level flight will depend on the > > airspeed, weight and flap angle, and to a less extent, on CG. > > > > Kevin Horton RV-8 (finishing kit) > > Ottawa, Canada > > http://www.kilohotel.com/rv8> > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Bob Collins" <bcollinsrv7a(at)comcast.net>
Subject: Fuel Flow Transducer-Injected
Date: Apr 20, 2006
> > I can understand that any restriction upstream of the engine > fuel pump might > tend to increase the possibility of vapour lock. However you > would think > that the AFP electric fuel boost pump itself would cause some sort of > restriction....surely the filter would. I believe there's an automatic bypass on the AFP in the event of a blockage in the filter. On question though, the terms people are using here remind me of when I'm in a pattern and somebody says "NXXXX, on the GPS approach to Runway XYZ. Of course, that does absolutely no good to anybody who doesn't know the GPS approach." So when you give these places of where the thing should e installed, for those of us who haven't yet really tackled this task, could you provide a little more information regarding its exactly location in relation to the fuselage and firewall? It'd be a big help. Thanks Bob Collins RV Builder's Hotline
http://home.comcast.net/~rvnewsletter/ ________________________________________________________________________________
From: Dwight Frye <dwight(at)openweave.org>
Subject: Re: Fuel Flow Transducer-Injected
Date: Apr 20, 2006
Again ... I'm just passing on information I learned from others, and have not performed this installation myself. But this is how I intend to do it. The place that I have been instructed to install my flowscan is between the throttlebody and the flow divider. In fact, the suggestion is to install it very near the flow divider on the line that runs between the cylinders. There will be a straight run out from the throttle body up to the Flowscan, then out of the Flowscan will be a short straight run and then from the transducer a line runs to the purge valve, and with the purge valve plumbed into the flow divider inlet. The whole transducer assembly should be wrapped in firesleeve to protect it from heat. The impression I have been left with is that this makes for a simple install with good results. It measures only that fuel that metered out of the servo, is not affected (therefore) by pressure changes from turning on/off the boost pump, and does not create a restriction on the suction side of the engine driven pump. It -does- mean that when you purge the line at start up and shut down a small amount of fuel will be counted as "consumed" even though it is returned to the supply lines .. but that is going to be only a small amount of fuel compared to the total consumed during a flight, and thus results in only a small percentage error. And .. most importantly .. that error will be on the conservative side meaning you will have -slightly- more fuel than your equipment thinks it has rather than less. That is the "right kind" of error to have, if you are going to have any error. :) If someone has better information ... please feel free to correct any mistakes I might have made. But this is my memory of what was shared at the Airflow class. -- Dwight On Thu Apr 20 08:19:55 2006, Bob Collins wrote : >I believe there's an automatic bypass on the AFP in the event of a blockage >in the filter. > >On question though, the terms people are using here remind me of when I'm in >a pattern and somebody says "NXXXX, on the GPS approach to Runway XYZ. Of >course, that does absolutely no good to anybody who doesn't know the GPS >approach." So when you give these places of where the thing should e >installed, for those of us who haven't yet really tackled this task, could >you provide a little more information regarding its exactly location in >relation to the fuselage and firewall? It'd be a big help. > >Thanks ________________________________________________________________________________
Date: Apr 20, 2006
Subject: Slider canopy rear fit
From: sjhdcl(at)kingston.net
After a fight and a half my slider frame (RV7A) fits fairly nicely. The only spot I'm not happy with is the rear horizontal part near the secure pins. The canopy frame is too wide at this point and does not conform to the bend of the fuse or the suggestion of 1/16" clearance all around. This area is box framed steel and presents a challenge when it comes to bending the frame in that area. I'm planning on using fiberglass fairings all around since I've had good results with this in the past. Any others have problems in this area of the canopy frame? Steve RV7A #2 ________________________________________________________________________________
Date: Apr 20, 2006
From: Charlie Kuss <chaztuna(at)adelphia.net>
Subject: Re: Fuel Flow Transducer-Injected
Bob, Check out JPI's installation instructions. They use the same FlowScan transducer. Check out pages 8-10 on the web document below http://www.jpinstruments.com/700-800_FF_install.PDF FYI, folks use gascolators on carbureted engines. They are a relatively low pressure system (5 psi) versus 25 psi for the Bendix and AFP fuel injection systems. That's an apples to oranges comparison. Yes, installing the fuel filter before the aux fuel pump will create a slight restriction. However, these filters use a SS mesh screen, not a paper element like cars do, so the restriction is slight. The transducer is small and contains a close tolerance trubine. There is a greater possibility of cavitation (air bubbles) if this is installed before either of the pumps. I spoke to an engineer at FlowScan, he said that the 5" rule is not critical, so long as you aren't installing a 90 degree fitting at either end of the transducer. As you have noted, others have installed the transducer behind the firewall with success. If it's installed behind the firewall but after the electric aux pump, any cavitation issues can be resolved by engaging the electric pump. The transducer then goes from being on the suction side of the system, to the pressure side. The engineer I spoke with stated that the orientation issue is to prevent debris from jamming the transducer. Charlie Kuss > > >I can understand that any restriction upstream of the engine fuel pump might >tend to increase the possibility of vapour lock. However you would think >that the AFP electric fuel boost pump itself would cause some sort of >restriction....surely the filter would. And then there's the people who also >use gascolators...or additional filters in the wing roots etc. Wouldn't all >of these things create some degree of resistance to flow. Why is the fuel >flow transducer being singled out...does it present an exceptional >resistance to flow. Have there been any reported cases of vapour lock >associated with locating the transducer upstream of the engine fuel >pump....or is this just more "worry bucket" stuff. > >Does anybody have any pix of their fuel transducer mounted between the servo >and the divider (and off the engine as has been recommended). Have the >people who have done this had universally good metering results...despite >the fact that they "may" not have the prerequisite 5" of straight line >before and after the transducer and may not have it mounted vertically as >recommended by the manufacturer. > >Decisions, decisions...phew. > >New year, new job there's more than 100,00 jobs at SEEK > > ________________________________________________________________________________
From: HCRV6(at)comcast.net
Subject: Re: Helmet & Headset ponderings
Date: Apr 20, 2006
I've been following this thread with interest and now I'll toss in my $0.02. I was using a Lightspeed QFR XC (ANR) headset for the first fifty hours or so in my RV-6. I really thought the Lightspeed was more than adequate. Unfortunately for me, the Bose offer of no interest for 12 twelve months and 30 day no questions asked return policy intriqued me so I bit just to try it. I had no intention of keeping it since obviously no head set is worth $1000.00. Wrong! Long story short I now have two Bose and you'd have to pry them out of my cold dead fingers to get me to part with them. -- Harry Crosby RV-6 N16CX, 203 hours -------------- Original message ---------------------- > > Mickey Coggins wrote: > > > >> So...I've been looking at ANR headsets and figure if I'm gonna spend some > >> dough, might as well get a good one and only cry once. I'm sure Bose is > >> the best but I can't quite believe the cost/benefit tradeoff is worth the > >> $1K price tag. ... > > > > It is a lot of money, that's for sure. Before I had bought my Bose X > > headsets a few years ago, I had only used David Clark. I didn't have > > the chance to try many other headsets, since there are no pilot shops > > around here. All the various ones I had tried seemed fine, but I > > decided to order the Bose anyway, even though I had never tried a > > set. They claim you can send them back. I'm happy with them, and > > if I had invested the extra $500 in the stock market, it would be > > worth about $300! :-) > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "RV6 Flyer" <rv6_flyer(at)hotmail.com>
Subject: Scott Crossfield
Date: Apr 20, 2006
http://www.cnn.com/2006/US/04/20/georgia.plane.ap/index.html Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, 1,842 + Flying Hours So. CA, USA http://SoCAL_WVAF.rvproject.com ----Original Message Follows---- From: "Jerry Isler" <jlisler(at)alltel.net> Subject: RV-List: Scott Crossfield Date: Wed, 19 Apr 2006 22:20:22 -0400 Off topic post! DO NOT ARCHIEVE. Has anyone heard anything about Scott Crossfield going down around Rome, Georgia this morning? I caught the tail end of a news cast about this and have no other details. Jerry Isler Donalsonville, GA RV-4 N455J Cessna C140A N9641A ________________________________________________________________________________
From: Grenwis(at)aol.com
Date: Apr 20, 2006
Subject: We lost Scott Crossfield today
I just read with sadness the news that Scott Crossfield died as the lone occupant of his airplane in a crash in GA. My RV indirectly led me to the pleasure of meeting this great man. When I first started my project in 2001 I visited a flying RV-6A at Manassas airport in Virginia. While there, a Cessna taxied up and an old guy climbed out. The other pilot I was visiting took me over and introduced me to the first man to fly faster than Mach 2 and live. As Scott told me, someone else got to Mach 2 first, but didn't live long enough to land his plane afterwards. Within minutes Scott was telling a dirty joke about a time in the decompression chamber 50-some years ago. What an impact on me to meet this living legend of flight. My thoughts go out to his family and friends. Rick Grenwis ________________________________________________________________________________
From: "John Jessen" <jjessen(at)rcn.com>
Subject: Helmet & Headset ponderings
Date: Apr 20, 2006
I actually did the same with the Bose. I bit on the no interest, 30 day marketing ploy. Current my ANRs are converted David Clarks. The Bose certainly are better than what I have now, but I returned them all the same. While building I'm not flying as much, and therefore decided not to spend the $$ at this time. But, yes, when I get the RV-10 completed, actually while completing the panel, there will be a spot to plug in the Bose that I'm hoping someone close to me might spring for, given how poverty stricken I'll be by then. I plan to save the DC's for the back seaters. John Jessen RV-10 (Tailcone) -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of HCRV6(at)comcast.net Sent: Thursday, April 20, 2006 1:44 PM Subject: Re: RV-List: Helmet & Headset ponderings I've been following this thread with interest and now I'll toss in my $0.02. I was using a Lightspeed QFR XC (ANR) headset for the first fifty hours or so in my RV-6. I really thought the Lightspeed was more than adequate. Unfortunately for me, the Bose offer of no interest for 12 twelve months and 30 day no questions asked return policy intriqued me so I bit just to try it. I had no intention of keeping it since obviously no head set is worth $1000.00. Wrong! Long story short I now have two Bose and you'd have to pry them out of my cold dead fingers to get me to part with them. -- Harry Crosby RV-6 N16CX, 203 hours -------------- Original message ---------------------- > > Mickey Coggins wrote: > > --> > > > >> So...I've been looking at ANR headsets and figure if I'm gonna > >> spend some dough, might as well get a good one and only cry once. > >> I'm sure Bose is the best but I can't quite believe the > >> cost/benefit tradeoff is worth the $1K price tag. ... > > > > It is a lot of money, that's for sure. Before I had bought my Bose > > X headsets a few years ago, I had only used David Clark. I didn't > > have the chance to try many other headsets, since there are no pilot > > shops around here. All the various ones I had tried seemed fine, > > but I decided to order the Bose anyway, even though I had never > > tried a set. They claim you can send them back. I'm happy with > > them, and if I had invested the extra $500 in the stock market, it > > would be worth about $300! :-) > > > > > > > > > > > > > > > > ________________________________________________________________________________
Date: Apr 20, 2006
From: Kysh <vans-dragon(at)lapdragon.org>
Subject: Re: We lost Scott Crossfield today
He had a great run, and died flying. How can anyone beat that? -Kysh -- ST1300 - Areion - > 4k mi -- STOC #5943 CBR-F4 - Foxy - > 56k mi ~~ To fly is to truly live ________________________________________________________________________________
Date: Apr 20, 2006
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: "Dual" take-off fuel pump fitting for pressure sender
Folks, I'm looking for a dual fitting that allows the fuel to flow and allows me to either attach my sender or attach another hose to the firewall mounted manifold...I've seen these - where do they come from and what's the part number. Anyone have any pictures? Thanks, Ralph ________________________________________________________________________________
From: "Andy Gold" <winterland(at)rkymtnhi.com>
Subject: Re: We lost Scott Crossfield today
Date: Apr 20, 2006
To have a great run and NOT die flying Andy > > He had a great run, and died flying. > > How can anyone beat that? > > -Kysh ________________________________________________________________________________
From: UFOBUCK(at)aol.com
Date: Apr 20, 2006
Subject: Re: We lost Scott Crossfield today
In a message dated 04/20/2006 3:25:56 P.M. Central Daylight Time, winterland(at)rkymtnhi.com writes: To have a great run and NOT die flying HEAR, HEAR !!! ________________________________________________________________________________
Date: Apr 20, 2006
From: Kysh <vans-dragon(at)lapdragon.org>
Subject: Re: We lost Scott Crossfield today
As Andy Gold was saying: > > > He had a great run, and died flying. > > > > How can anyone beat that? > > > > -Kysh > > To have a great run and NOT die flying Gotta die sometime, somehow. I'd sure rather die flying than have it creep up to me while I'm laying in bed. 84 is a long time to be around, and me I'd hope to die before I lost my ability to do that which I loved. We all die, some sooner and more ignominiously than others. If I had the choice, I'd go out with a stick in one hand, throttle in the other. -Kysh -- ST1300 - Areion - > 4k mi -- STOC #5943 CBR-F4 - Foxy - > 56k mi ~~ To fly is to truly live ________________________________________________________________________________
Subject: We lost Scott Crossfield today
Date: Apr 20, 2006
From: "Folbrecht, Paul" <PFolbrecht(at)starkinvestments.com>
He was 84. If I make it to 84 and pass without ever being a resident at a group home, and with a valid FAA medical in my wallet, I'll consider that quite a good run. -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Andy Gold Sent: Thursday, April 20, 2006 3:20 PM Subject: Re: RV-List: We lost Scott Crossfield today To have a great run and NOT die flying Andy > > He had a great run, and died flying. > > How can anyone beat that? > > -Kysh ________________________________________________________________________________
From: "Curt Reimer" <cgreimer(at)mts.net>
Subject: Re: Helmet & Headset ponderings
Date: Apr 20, 2006
> Also, any pireps on the Thirty 3G series or similar high-end Lightspeed > model would be appreciated. In general I've heard that Lightspeed > headsets are comfortable and work well, sometimes break but have good > factory support to replace parts. One of my hangarmates has a pair of > well-used Lightspeeds that have the thin covering pealing away from the > foam earseals and head cushions. Still works but looks like crap... Mark, my experience with the Thirty 3G is pretty much as you describe. It's made almost entirely of plastic and it's a bit flimsy but the sound quality is great and it has features that I wouldn't live without, like the music and cellphone inputs. It also has the most earcup room of any of the ANR headsets I've tried. For me, that makes it the most comfortable because the cups seals don't press against my ears. The Thirty 3G has leatherette covered earcups and the peeling foam isn't an issue anymore. I've broken my headband once (it was -20F at the time) and I shipped it off to Lightspeed and repairs were prompt and free (two days plus shipping time). I have also taken my headset in for servicing at Airventure a couple of times. The Lightspeed people bring a stock of parts with them and you can walk up and get your headset serviced at their booth. Their policy seems to be to just replace everything, even if from normal wear and tear, forever, just for the asking. I found my earcups getting a bit stiff after a couple of years of wear and when I asked them at Osh how to care for them, they just handed my a new pair of cups, which snapped right in. If Lightspeed built their headsets with David Clark ruggedness, they would be unbeatable. For my money the Thirty 3G is still the best, but if I were flying professionally I might not put up with their fragility. Curt RV-6 C-GACR ________________________________________________________________________________
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: "Dual" take-off fuel pump fitting for pressure sender
Date: Apr 20, 2006
On 20 Apr 2006, at 15:58, Ralph E. Capen wrote: > > > Folks, > > I'm looking for a dual fitting that allows the fuel to flow and > allows me to either attach my sender or attach another hose to the > firewall mounted manifold...I've seen these - where do they come > from and what's the part number. > > Anyone have any pictures? I used an Earl's 100192ERL, purchased from a local speed shop: http://www.holley.com/100192ERL.asp It takes the -6 fuel line fittings, and you can screw in an elbow or straight fitting as required to attach the fuel line hose. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
From: "Gordon or Marge Comfort" <gcomfo(at)tc3net.com>
Subject: We lost Scott Crossfield today
Date: Apr 20, 2006
He had a great run, and died flying. How can anyone beat that? ~~ To fly is to truly live There are many people in this world for whom I have great respect, but few whom I truly admire. Of the latter, Scott Crossfield is at the top of the list. I will join many others in mourning his passing. Gordon Comfort N3363GC ________________________________________________________________________________
From: "Belue, Kevin" <KBelue@drs-tem.com>
Subject: Re: "Dual" take-off fuel pump fitting for pressure sende r
Date: Apr 20, 2006
I used the Tee fitting w/1/8" pipe thread tapping for fuel pressure, part # 07-00783 from Aircraft Spruce. It screws into the engine fuel pump outlet and has one port for the hose to the carb and another, smaller port for a hose to the fuel pressure sender. Kevin D. Belue RV-6A RV-10 > -----Original Message----- > From: Kevin Horton [mailto:khorton01(at)rogers.com] > Sent: Thursday, April 20, 2006 4:46 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: "Dual" take-off fuel pump fitting for > pressure sender > > > > On 20 Apr 2006, at 15:58, Ralph E. Capen wrote: > > > > > > > Folks, > > > > I'm looking for a dual fitting that allows the fuel to flow > and > > allows me to either attach my sender or attach another hose > to the > > firewall mounted manifold...I've seen these - where do they > come > > from and what's the part number. > > > > Anyone have any pictures? > > I used an Earl's 100192ERL, purchased from a local speed shop: > > http://www.holley.com/100192ERL.asp > > It takes the -6 fuel line fittings, and you can screw in an > elbow or > straight fitting as required to attach the fuel line hose. > > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada > http://www.kilohotel.com/rv8 > > > > > > > > > > > INFORMATION CONTAINED IN THIS EMAIL MAY BE DRS PROPRIETARY/COMPETITION SENSITIVE AND IS ONLY INTENDED FOR THE ADDRESSEE OF THIS EMAIL THIS DOCUMENT AND/OR SHIPMENT MAY CONTAIN COMMODITY ITEMS, SOFTWARE OR TECHNICAL DATA THAT IS CONTROLLED BY U.S. EXPORT LAW, AND MAY NOT BE EXPORTED OUTSIDE THE UNITED STATES OR TO NON U.S. PERSONS WITHOUT THE APPROPRIATE EXPORT LICENSE FROM EITHER THE U.S. DEPARTMENT OF STATE OR DEPARTMENT OF COMMERCE. ________________________________________________________________________________
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: "Dual" take-off fuel pump fitting for pressure sender
Date: Apr 20, 2006
This might work - depending on what I dream up.... Thanks ----- Original Message ----- From: "Kevin Horton" <khorton01(at)rogers.com> Sent: Thursday, April 20, 2006 5:46 PM Subject: Re: RV-List: "Dual" take-off fuel pump fitting for pressure sender > > On 20 Apr 2006, at 15:58, Ralph E. Capen wrote: > >> >> >> Folks, >> >> I'm looking for a dual fitting that allows the fuel to flow and >> allows me to either attach my sender or attach another hose to the >> firewall mounted manifold...I've seen these - where do they come >> from and what's the part number. >> >> Anyone have any pictures? > > I used an Earl's 100192ERL, purchased from a local speed shop: > > http://www.holley.com/100192ERL.asp > > It takes the -6 fuel line fittings, and you can screw in an elbow or > straight fitting as required to attach the fuel line hose. > > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada > http://www.kilohotel.com/rv8 > > > > > > > > > > > > > ________________________________________________________________________________
From: "Belue, Kevin" <KBelue@drs-tem.com>
Subject: "Dual" take-off fuel pump fitting for pressure s ender
Date: Apr 20, 2006
Belue, Kevin would like to recall the message, "RV-List: "Dual" take-off fuel pump fitting for pressure sender". INFORMATION CONTAINED IN THIS EMAIL MAY BE DRS PROPRIETARY/COMPETITION SENSITIVE AND IS ONLY INTENDED FOR THE ADDRESSEE OF THIS EMAIL THIS DOCUMENT AND/OR SHIPMENT MAY CONTAIN COMMODITY ITEMS, SOFTWARE OR TECHNICAL DATA THAT IS CONTROLLED BY U.S. EXPORT LAW, AND MAY NOT BE EXPORTED OUTSIDE THE UNITED STATES OR TO NON U.S. PERSONS WITHOUT THE APPROPRIATE EXPORT LICENSE FROM EITHER THE U.S. DEPARTMENT OF STATE OR DEPARTMENT OF COMMERCE. ________________________________________________________________________________
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: "Dual" take-off fuel pump fitting for pressure sende r
Date: Apr 20, 2006
Thanks - these are identical to the parts that Vans has in their catalog. Ralph ----- Original Message ----- From: "Belue, Kevin" <KBelue@DRS-TEM.com> Sent: Thursday, April 20, 2006 6:06 PM Subject: Re: RV-List: "Dual" take-off fuel pump fitting for pressure sende r > > I used the Tee fitting w/1/8" pipe thread tapping for fuel pressure, part > # > 07-00783 from Aircraft Spruce. It screws into the engine fuel pump outlet > and has one port for the hose to the carb and another, smaller port for a > hose to the fuel pressure sender. > > Kevin D. Belue > RV-6A > RV-10 > >> -----Original Message----- >> From: Kevin Horton [mailto:khorton01(at)rogers.com] >> Sent: Thursday, April 20, 2006 4:46 PM >> To: rv-list(at)matronics.com >> Subject: Re: RV-List: "Dual" take-off fuel pump fitting for >> pressure sender >> >> >> >> On 20 Apr 2006, at 15:58, Ralph E. Capen wrote: >> >> > >> > >> > Folks, >> > >> > I'm looking for a dual fitting that allows the fuel to flow >> and >> > allows me to either attach my sender or attach another hose >> to the >> > firewall mounted manifold...I've seen these - where do they >> come >> > from and what's the part number. >> > >> > Anyone have any pictures? >> >> I used an Earl's 100192ERL, purchased from a local speed shop: >> >> http://www.holley.com/100192ERL.asp >> >> It takes the -6 fuel line fittings, and you can screw in an >> elbow or >> straight fitting as required to attach the fuel line hose. >> >> Kevin Horton RV-8 (finishing kit) >> Ottawa, Canada >> http://www.kilohotel.com/rv8 >> >> >> >> >> >> >> >> >> >> >> > > > INFORMATION CONTAINED IN THIS EMAIL MAY BE DRS PROPRIETARY/COMPETITION > SENSITIVE AND IS ONLY INTENDED FOR THE ADDRESSEE OF THIS EMAIL > > THIS DOCUMENT AND/OR SHIPMENT MAY CONTAIN COMMODITY ITEMS, SOFTWARE OR > TECHNICAL DATA THAT IS CONTROLLED BY U.S. EXPORT LAW, AND MAY NOT BE > EXPORTED OUTSIDE THE UNITED STATES OR TO NON U.S. PERSONS WITHOUT THE > APPROPRIATE EXPORT LICENSE FROM EITHER THE U.S. DEPARTMENT OF STATE OR > DEPARTMENT OF COMMERCE. > > > ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: Blended Airfoil 72" vs. 74"
Date: Apr 17, 2006
Dear Jim et al, 3 years ago I wanted to try to find the best propeller for my RV8. I have a 76" Hartzell that I have had since new, and it worked well, however, I wanted more speed as well as climb. I also wanted lighter weight ----- Original Message ----- From: "Jim Thorne" <rv7a(at)cox.net> Sent: Wednesday, March 15, 2006 2:06 PM Subject: RV-List: Blended Airfoil 72" vs. 74" > > Does anyone have any information on pros and cons on choosing a 72" vs. > 74" Hartzell blended airfoil prop? Have searched archives and was unable > to find any specific information relative to propeller diameter. > > Jim Thorne > 7A-QB CHD > > > ________________________________________________________________________________
From: JVanLaak(at)aol.com
Date: Apr 20, 2006
Subject: ADI Impressions - Long
Listers, I have been flying a Tru Track ADI for about 10 hours now and thought I would share my early impressions with folks. The flying has all been VFR although I am an experienced IFR pilot (Ex-AF) but not current. I should also note that I bought the ADI in part because I was not comfortable relying on the Dynon that I had installed 2 years ago. The reliability issues I had with the Dynon were dealt with by the company but I just never really felt like I was getting the right data from the instrument. It just did not "feel" right, and having had a failure of the main ADI in bad weather in a fighter years ago I wanted to address that before trying to get IFR current again. So right after Christmas I bought the ADI and waited expectantly for it to show up. I say bought because my credit card was charged right away despite the fact that it took over 2 months for it to be delivered. High demand they said, but it will be coming " next week." It finally did come in mid March and I excitedly took it out of the box and hooked it up to power. The pitch system worked but made a rubbing sound. The roll function was completely inop. Then I noticed that the case had a bulge on the left side. Not a happy camper I sent an email to Tru Trak immediately telling them they had a quality problem. I got a note back from the service manager asking me to send it right back and they would fix it. About 5 days later I got an email indicating that one of the cards had come out of its mount and was jammed in the case, binding the pitch mechanism. Their speculation was that it was jarred out by shipment, but that seems unlikely to me. Regardless, they repaired the unit and sent it back express so I got it into the plane and working the next weekend. It is definitely different from a regular attitude indicator. As many of you know, both the pitch and roll signals come from rate sensors not a normal gyro platform. So a pitch input is indicated in the normal way but the amplitude of the movement soon reverts to a rate of climb indication. It is hard to describe but works pretty intuitively in practice. Likewise the roll indication initially comes from a roll sensor but then if you held knife-edge flight it would revert to show wings level. But in normal coordinated turns the roll sensor hands off to a yaw sensor in a nearly seamless way and it operates very much like a normal attitude indicator. A few of the funny things I have noticed so far. 1. The pitch indication looks extreme on departure with an RV's rate of climb. Even my timid 160 hp with fixed pitch prop does 1000 fpm and that is a BIG pitch indication on the scale. It would be easy for them to tone that down some and that will be a recommendation when I get more time on it. The down-indication is less of a problem. Normal under the hood flying works just fine. In fact level turns are extremely easy with the vertical velocity what you are actually flying. And the instantaneous pitch sensor addresses most of the lag of the traditional VS indicator. The roll sensor maxes out at 30 degrees and a red arrow flashes to tell you to roll out if you exceed that angle. You obviously cannot do steep turns that way which is something of a problem. Likewise it is unclear what happens in a truly serious unusual attitude. I will experiment at some point but have not done so yet. Finally, if you fly level and slow down until you approach the stall the pitch indicator stays level and then starts to go down as the sink rate increases even though the nose is way up. The only indication on the screen is a flashing "AS" for airspeed. Bottom line is I think I like it and am looking forward to some serious hood work to check it out. BUT I have decided to move the Dynon to the right side of the panel as a full performance back up instrument as well as an all-in-one instrument for guest pilots. But it addresses the extreme attitude situation and will offer a nice back up to this EXPERIMENTAL instrument. It seems to be a good addition to the homebuilt suite. BTW, I have no interest in investing in the AOA function they are adding. I am not a big AOA fan (despite hundreds of hours with them) and I really don't care for this implementation. Jim Van Laak RV-6 N79RL ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: We lost Scott Crossfield today
Date: Apr 20, 2006
OK, I should know better by now, but I must disagree. I am with you right up to "PLEASE - do not taint this mans character with Monday morning BS." There is no way we can "taint this man's character," but we might be able to save someone else's butt by discussing what MIGHT have happened. If you were a USAF pilot you must know how much effort goes into investigating and discussing accidents for the express purpose of trying to prevent others from falling into the same trap. Slamming the door on any discussion of an accident that cost the life of such a competent pilot does a great disservice to the cause of safe flying and doesn't help anyone's reputation. "Nuff said"?? No way. Lets honor the man by learning from what cost him his life. Terry -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of David Fenstermacher Sent: Thursday, April 20, 2006 6:04 PM Subject: Re: RV-List: We lost Scott Crossfield today I agree w/goodwin. It is simply our (the survivors) way of justifying it/dealing with it. Death while doing what a person loved is still death. I've been to many funerals (I was a USAF pilot). A 34 year old who left a wife and three kids dying while doing acro is still dead and the kids/wife are still alone. An F-16 pilot who left a wife and 4 kids is still dead. We are mourning - plain and simple. A pilot is dead. He obviously thought conditions were acceptable. Weather changes fast - especially when there is significant vertical development. Seen it - been there. PLEASE - do not taint this mans character with Monday morning BS. Nuff said. ________________________________________________________________________________
Date: Apr 20, 2006
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: We lost Scott Crossfield today
Kysh wrote: > > As Andy Gold was saying: >> >>> He had a great run, and died flying. >>> >>> How can anyone beat that? >>> >>> -Kysh >> To have a great run and NOT die flying > > Gotta die sometime, somehow. I'd sure rather die flying than have it > creep up to me while I'm laying in bed. 84 is a long time to be around, > and me I'd hope to die before I lost my ability to do that which I > loved. Kysh, I certainly hope you do not lose your medical at a fairly young age....... Someday, when you are surrounded by a loving extended family with a bunch of grandkids, you may realize the folly of your comments. Best regards, Sam Buchanan ________________________________________________________________________________
Date: Apr 20, 2006
From: David Fenstermacher <davidfenster(at)comcast.net>
Subject: Re: We lost Scott Crossfield today
OK. We SHOULD learn (that's understood). But that is not what this list does. It tends to crucify. Pilot error and all. Here is a guy who had the experience to "know better" and still died. That was my point. Start the "discussion" you are talking about, but do not question his abilities as a pilot. Normally, I would just walk away from this discussion. This list tends to "jump" at the easy answer. I met this man, and I DID NOT want anyone to mess with HIS LEGACY. So, the easy answer for you, Terry, is go get his experience and then post. Or even mine..... And, yes, you can taint his character with BS comments from inexperienced pilots who have never been in harms way. Terry Watson wrote: > > OK, I should know better by now, but I must disagree. I am with you right up > to "PLEASE - do not taint this mans character with Monday morning BS." There > is no way we can "taint this man's character," but we might be able to save > someone else's butt by discussing what MIGHT have happened. If you were a > USAF pilot you must know how much effort goes into investigating and > discussing accidents for the express purpose of trying to prevent others > from falling into the same trap. Slamming the door on any discussion of an > accident that cost the life of such a competent pilot does a great > disservice to the cause of safe flying and doesn't help anyone's reputation. > > "Nuff said"?? No way. Lets honor the man by learning from what cost him his > life. > > Terry > > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of David Fenstermacher > Sent: Thursday, April 20, 2006 6:04 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: We lost Scott Crossfield today > > > > I agree w/goodwin. > It is simply our (the survivors) way of justifying it/dealing with it. > Death while doing what a person loved is still death. > I've been to many funerals (I was a USAF pilot). A 34 year old who left > a wife and three kids dying while doing acro is still dead and the > kids/wife are still alone. An F-16 pilot who left a wife and 4 kids is > still dead. We are mourning - plain and simple. A pilot is dead. He > obviously thought conditions were acceptable. Weather changes fast - > especially when there is significant vertical development. Seen it - > been there. PLEASE - do not taint this mans character with Monday > morning BS. > > Nuff said. > > > > > > > > ________________________________________________________________________________
Date: Apr 20, 2006
From: linn Walters <pitts_pilot(at)bellsouth.net>
Subject: Re: We lost Scott Crossfield today
Kyle Boatright wrote: > snip >It wasn't a good time or place to fly a light single, and I'm surprised >someone with Mr. Crossfield's credentials got caught in it. > >KB > Everytime one of the 'greats' passes in an accident that appears preventable, I'm also surprised, and amazed. Thousands of hours in many varied types of aircraft don't appear enough to overcome an error in judgement. I'm saddened every time it happens. I have twisted the 'old-bold pilot' phrase to "An old pilot is one that survives all his (or her) stupid mistakes". Linn ________________________________________________________________________________
From: "Bob Collins" <bcollinsrv7a(at)comcast.net>
Subject: We lost Scott Crossfield today
Date: Apr 20, 2006
I would like to interrupt the developing flame war just long enough to say how much I admire the Greatest Generation. That includes, of course, Mr. Crossfield. When they came up with the phrase "he's got balls," it was for guys like him and, frankly, thousands of men and women of his generation who are passing from our lives every day. I am always saddened, of course, when one passes. I look at my generation (the Baby Boomers) and the one following it and I know we have not been or acted worthy of what they handed over to us. And we could, never, ever sacrifice in this day and age the way that one did. And that makes me sadder still. On the day of his death, I won't pollute his memory by thinking of anything other than remembering him and his generation for what they gave me and this country. Will the circumstances of his death somehow help make me a better pilot. I could not possibly care less. On this day, it's more important for me, personally, to reflect on whether his life will help make me a better person. On this day, I'd also like to remember another member of the Greatest Generation who passed today. Eustace Bohay. Resume. Bob Collins St. Paul ________________________________________________________________________________
Date: Apr 20, 2006
From: "kelby alexander" <n41va(at)blazemail.com>
Subject: Re: We lost Scott Crossfield today
Thank you David! I didnt know Scott Crossfield but I can only imagine what his family is going thru. I lost my dad in an -8 (Von ALexander)and I know that my whole family monitored this exact RV list the day of the accident. We were very comforted by the concerns of every other RVer. Even though some questioned a few of my dads choices, just keep in mind that his family very well might might be reading all of these posts. In that case my heart goes out to his family. I didnt know Scott, but it sounds like he is doing what I am working towrds... a test pilot. I am sure he will be missed in the aviation community. Kelby L Alexander --- davidfenster(at)comcast.net wrote: From: David Fenstermacher <davidfenster(at)comcast.net> Subject: Re: RV-List: We lost Scott Crossfield today Date: Thu, 20 Apr 2006 23:11:31 -0400 OK. We SHOULD learn (that's understood). But that is not what this list does. It tends to crucify. Pilot error and all. Here is a guy who had the experience to "know better" and still died. That was my point. Start the "discussion" you are talking about, but do not question his abilities as a pilot. Normally, I would just walk away from this discussion. This list tends to "jump" at the easy answer. I met this man, and I DID NOT want anyone to mess with HIS LEGACY. So, the easy answer for you, Terry, is go get his experience and then post. Or even mine..... And, yes, you can taint his character with BS comments from inexperienced pilots who have never been in harms way. Terry Watson wrote: > > OK, I should know better by now, but I must disagree. I am with you right up > to "PLEASE - do not taint this mans character with Monday morning BS." There > is no way we can "taint this man's character," but we might be able to save > someone else's butt by discussing what MIGHT have happened. If you were a > USAF pilot you must know how much effort goes into investigating and > discussing accidents for the express purpose of trying to prevent others > from falling into the same trap. Slamming the door on any discussion of an > accident that cost the life of such a competent pilot does a great > disservice to the cause of safe flying and doesn't help anyone's reputation. > > "Nuff said"?? No way. Lets honor the man by learning from what cost him his > life. > > Terry > > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of David Fenstermacher > Sent: Thursday, April 20, 2006 6:04 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: We lost Scott Crossfield today > > > > I agree w/goodwin. > It is simply our (the survivors) way of justifying it/dealing with it. > Death while doing what a person loved is still death. > I've been to many funerals (I was a USAF pilot). A 34 year old who left > a wife and three kids dying while doing acro is still dead and the > kids/wife are still alone. An F-16 pilot who left a wife and 4 kids is > still dead. We are mourning - plain and simple. A pilot is dead. He > obviously thought conditions were acceptable. Weather changes fast - > especially when there is significant vertical development. Seen it - > been there. PLEASE - do not taint this mans character with Monday > morning BS. > > Nuff said. > > > > > > > > Fight the power! BlazeMail.com ________________________________________________________________________________
Date: Apr 20, 2006
From: "kelby alexander" <n41va(at)blazemail.com>
Subject: Re: We lost Scott Crossfield today
Thank you David! I didnt know Scott Crossfield but I can only imagine what his family is going thru. I lost my dad in an -8 (Von ALexander)and I know that my whole family monitored this exact RV list the day of the accident. We were very comforted by the concerns of every other RVer. Even though some questioned a few of my dads choices, just keep in mind that his family very well might might be reading all of these posts. In that case my heart goes out to his family. I didnt know Scott, but it sounds like he is doing what I am working towrds... a test pilot. I am sure he will be missed in the aviation community. Kelby L Alexander --- davidfenster(at)comcast.net wrote: From: David Fenstermacher <davidfenster(at)comcast.net> Subject: Re: RV-List: We lost Scott Crossfield today Date: Thu, 20 Apr 2006 23:11:31 -0400 OK. We SHOULD learn (that's understood). But that is not what this list does. It tends to crucify. Pilot error and all. Here is a guy who had the experience to "know better" and still died. That was my point. Start the "discussion" you are talking about, but do not question his abilities as a pilot. Normally, I would just walk away from this discussion. This list tends to "jump" at the easy answer. I met this man, and I DID NOT want anyone to mess with HIS LEGACY. So, the easy answer for you, Terry, is go get his experience and then post. Or even mine..... And, yes, you can taint his character with BS comments from inexperienced pilots who have never been in harms way. Terry Watson wrote: > > OK, I should know better by now, but I must disagree. I am with you right up > to "PLEASE - do not taint this mans character with Monday morning BS." There > is no way we can "taint this man's character," but we might be able to save > someone else's butt by discussing what MIGHT have happened. If you were a > USAF pilot you must know how much effort goes into investigating and > discussing accidents for the express purpose of trying to prevent others > from falling into the same trap. Slamming the door on any discussion of an > accident that cost the life of such a competent pilot does a great > disservice to the cause of safe flying and doesn't help anyone's reputation. > > "Nuff said"?? No way. Lets honor the man by learning from what cost him his > life. > > Terry > > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of David Fenstermacher > Sent: Thursday, April 20, 2006 6:04 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: We lost Scott Crossfield today > > > > I agree w/goodwin. > It is simply our (the survivors) way of justifying it/dealing with it. > Death while doing what a person loved is still death. > I've been to many funerals (I was a USAF pilot). A 34 year old who left > a wife and three kids dying while doing acro is still dead and the > kids/wife are still alone. An F-16 pilot who left a wife and 4 kids is > still dead. We are mourning - plain and simple. A pilot is dead. He > obviously thought conditions were acceptable. Weather changes fast - > especially when there is significant vertical development. Seen it - > been there. PLEASE - do not taint this mans character with Monday > morning BS. > > Nuff said. > > > > > > > > Fight the power! BlazeMail.com ________________________________________________________________________________
From: aeroncadoc(at)comcast.net
Subject: Re: We lost Scott Crossfield today
Date: Apr 21, 2006
The scary thing about flying to me, is that while I know about many of the risks and dangers, I don't even know what I don't know. If flying ever does me in, it will come from something in this category. I can certainly limit my risk by some conscious and prudent decision making, but who hasn't violated his or her own rules once or twice? I guess most of us are willing to just accept the risks because there is something about flying that we are attracted (addicted?) to. Henry H. -------------- Original message -------------- From: linn Walters <pitts_pilot(at)bellsouth.net> > > Kyle Boatright wrote: > > > > snip > > >It wasn't a good time or place to fly a light single, and I'm surprised > >someone with Mr. Crossfield's credentials got caught in it. > > > >KB > > > Everytime one of the 'greats' passes in an accident that appears > preventable, I'm also surprised, and amazed. Thousands of hours in > many varied types of aircraft don't appear enough to overcome an error > in judgement. I'm saddened every time it happens. I have twisted the > 'old-bold pilot' phrase to "An old pilot is one that survives all his > (or her) stupid mistakes". > Linn > > > > > > > > > > > > > The scary thing about flying to me, is that while I know about many of the risks and dangers, I don't even know what I don't know. If flying ever does me in, it will come from something in this category. I can certainly limit my risk by some conscious and prudent decision making, but who hasn't violated his or her own rules once or twice? I guess most of us are willing to just accept the risks because there is something about flying that we are attracted (addicted?) to. Henry H. -------------- Original message -------------- From: linn Walters pitts_pilot(at)bellsouth.net -- RV-List message posted by: linn Walters Kyle Boatright wrote: -- RV-List message posted by: "Kyle Boatright" snip It wasn't a good time or place to fly a light single, and I'm surprised someone with Mr. Crossfield's credentials got caught in it. KB Everytime one of the 'greats' passes in an accident that appears preventable, I'm also surprised, and amazed. Thousands of hours in many varied types of aircraft don't appear enough to overcome an error in judgement. I'm saddened every time it happens. I have twisted the 'old-bold pilot' phrase to "An old pilot is one that survives all his (or her) stupid mistakes". Linn ralle, List Admin. ________________________________________________________________________________
Date: Apr 20, 2006
From: Dave Nellis <truflite(at)yahoo.com>
Subject: Re: We lost Scott Crossfield today
The day after JFK Jr. died, I had a flying lesson. My wife was having a Tupperware party and my mother was there. She implored me not to go flying. I told her the best thing to do would be to get in that plane and fly. All the while keeping in mind that accidents happen and knowledge gained from it could help save me or someone else. Keep flying and always have your eyes and mind open. Dave --- kelby alexander wrote: > > > Thank you David! I didnt know Scott Crossfield but I > can only imagine what his family is going thru. I > lost my dad in an -8 (Von ALexander)and I know that > my whole family monitored this exact RV list the day > of the accident. We were very comforted by the > concerns of every other RVer. Even though some > questioned a few of my dads choices, just keep in > mind that his family very well might might be > reading all of these posts. In that case my heart > goes out to his family. I didnt know Scott, but it > sounds like he is doing what I am working towrds... > a test pilot. I am sure he will be missed in the > aviation community. > > Kelby L Alexander > > --- davidfenster(at)comcast.net wrote: > > From: David Fenstermacher <davidfenster(at)comcast.net> > To: rv-list(at)matronics.com > Subject: Re: RV-List: We lost Scott Crossfield today > Date: Thu, 20 Apr 2006 23:11:31 -0400 > > > > OK. We SHOULD learn (that's understood). But that > is not what this > list does. It tends to crucify. Pilot error and > all. > Here is a guy who had the experience to "know > better" and still died. > That was my point. Start the "discussion" you are > talking about, but do > not question his abilities as a pilot. > > Normally, I would just walk away from this > discussion. This list tends > to "jump" at the easy answer. I met this man, and I > DID NOT want anyone > to mess with HIS LEGACY. > > So, the easy answer for you, Terry, is go get his > experience and then post. > Or even mine..... > > And, yes, you can taint his character with BS > comments from > inexperienced pilots who have never been in harms > way. > > > Terry Watson wrote: > > > > > OK, I should know better by now, but I must > disagree. I am with you right up > > to "PLEASE - do not taint this mans character with > Monday morning BS." There > > is no way we can "taint this man's character," but > we might be able to save > > someone else's butt by discussing what MIGHT have > happened. If you were a > > USAF pilot you must know how much effort goes into > investigating and > > discussing accidents for the express purpose of > trying to prevent others > > from falling into the same trap. Slamming the door > on any discussion of an > > accident that cost the life of such a competent > pilot does a great > > disservice to the cause of safe flying and doesn't > help anyone's reputation. > > > > "Nuff said"?? No way. Lets honor the man by > learning from what cost him his > > life. > > > > Terry > > > > > > > > > > > > -----Original Message----- > > From: owner-rv-list-server(at)matronics.com > > [mailto:owner-rv-list-server(at)matronics.com] On > Behalf Of David Fenstermacher > > Sent: Thursday, April 20, 2006 6:04 PM > > To: rv-list(at)matronics.com > > Subject: Re: RV-List: We lost Scott Crossfield > today > > > > > > > > I agree w/goodwin. > > It is simply our (the survivors) way of justifying > it/dealing with it. > > Death while doing what a person loved is still > death. > > I've been to many funerals (I was a USAF pilot). > A 34 year old who left > > a wife and three kids dying while doing acro is > still dead and the > > kids/wife are still alone. An F-16 pilot who left > a wife and 4 kids is > > still dead. We are mourning - plain and simple. > A pilot is dead. He > > obviously thought conditions were acceptable. > Weather changes fast - > > especially when there is significant vertical > development. Seen it - > > been there. PLEASE - do not taint this mans > character with Monday > > morning BS. > > > > Nuff said. > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > Fight the power! BlazeMail.com > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > ________________________________________________________________________________
Date: Apr 20, 2006
From: "kelby alexander" <n41va(at)blazemail.com>
Subject: Re: We lost Scott Crossfield today
1 year after my Dad dies in our RV I asked my Mom to start flying lessons. I got a HUGE "NOT IN A MILLION YEARS!!!!!" Now, almost 7 years after the accident, she is more than willing to pay for all of my ratings, Private, insturment, commercial, multi. cfi, cfii and mei. There is always dangers in flying, but I can look back and say my dad died doing something that he loved. Kelby --- truflite(at)yahoo.com wrote: From: Dave Nellis <truflite(at)yahoo.com> Subject: Re: RV-List: We lost Scott Crossfield today Date: Thu, 20 Apr 2006 21:14:23 -0700 (PDT) The day after JFK Jr. died, I had a flying lesson. My wife was having a Tupperware party and my mother was there. She implored me not to go flying. I told her the best thing to do would be to get in that plane and fly. All the while keeping in mind that accidents happen and knowledge gained from it could help save me or someone else. Keep flying and always have your eyes and mind open. Dave --- kelby alexander wrote: > > > Thank you David! I didnt know Scott Crossfield but I > can only imagine what his family is going thru. I > lost my dad in an -8 (Von ALexander)and I know that > my whole family monitored this exact RV list the day > of the accident. We were very comforted by the > concerns of every other RVer. Even though some > questioned a few of my dads choices, just keep in > mind that his family very well might might be > reading all of these posts. In that case my heart > goes out to his family. I didnt know Scott, but it > sounds like he is doing what I am working towrds... > a test pilot. I am sure he will be missed in the > aviation community. > > Kelby L Alexander > > --- davidfenster(at)comcast.net wrote: > > From: David Fenstermacher <davidfenster(at)comcast.net> > To: rv-list(at)matronics.com > Subject: Re: RV-List: We lost Scott Crossfield today > Date: Thu, 20 Apr 2006 23:11:31 -0400 > > > > OK. We SHOULD learn (that's understood). But that > is not what this > list does. It tends to crucify. Pilot error and > all. > Here is a guy who had the experience to "know > better" and still died. > That was my point. Start the "discussion" you are > talking about, but do > not question his abilities as a pilot. > > Normally, I would just walk away from this > discussion. This list tends > to "jump" at the easy answer. I met this man, and I > DID NOT want anyone > to mess with HIS LEGACY. > > So, the easy answer for you, Terry, is go get his > experience and then post. > Or even mine..... > > And, yes, you can taint his character with BS > comments from > inexperienced pilots who have never been in harms > way. > > > Terry Watson wrote: > > > > > OK, I should know better by now, but I must > disagree. I am with you right up > > to "PLEASE - do not taint this mans character with > Monday morning BS." There > > is no way we can "taint this man's character," but > we might be able to save > > someone else's butt by discussing what MIGHT have > happened. If you were a > > USAF pilot you must know how much effort goes into > investigating and > > discussing accidents for the express purpose of > trying to prevent others > > from falling into the same trap. Slamming the door > on any discussion of an > > accident that cost the life of such a competent > pilot does a great > > disservice to the cause of safe flying and doesn't > help anyone's reputation. > > > > "Nuff said"?? No way. Lets honor the man by > learning from what cost him his > > life. > > > > Terry > > > > > > > > > > > > -----Original Message----- > > From: owner-rv-list-server(at)matronics.com > > [mailto:owner-rv-list-server(at)matronics.com] On > Behalf Of David Fenstermacher > > Sent: Thursday, April 20, 2006 6:04 PM > > To: rv-list(at)matronics.com > > Subject: Re: RV-List: We lost Scott Crossfield > today > > > > > > > > I agree w/goodwin. > > It is simply our (the survivors) way of justifying > it/dealing with it. > > Death while doing what a person loved is still > death. > > I've been to many funerals (I was a USAF pilot). > A 34 year old who left > > a wife and three kids dying while doing acro is > still dead and the > > kids/wife are still alone. An F-16 pilot who left > a wife and 4 kids is > > still dead. We are mourning - plain and simple. > A pilot is dead. He > > obviously thought conditions were acceptable. > Weather changes fast - > > especially when there is significant vertical > development. Seen it - > > been there. PLEASE - do not taint this mans > character with Monday > > morning BS. > > > > Nuff said. > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > Fight the power! BlazeMail.com > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > Fight the power! BlazeMail.com ________________________________________________________________________________
Date: Apr 20, 2006
From: Dan <dan(at)rdan.com>
Subject: We lost Scott Crossfield today
Brovo Bob ! rest in peace Scott and Eustace, Dan -8 Bob Collins wrote: I would like to interrupt the developing flame war just long enough to say how much I admire the Greatest Generation. That includes, of course, Mr. Crossfield. When they came up with the phrase "he's got balls," it was for guys like him and, frankly, thousands of men and women of his generation who are passing from our lives every day. I am always saddened, of course, when one passes. I look at my generation (the Baby Boomers) and the one following it and I know we have not been or acted worthy of what they handed over to us. And we could, never, ever sacrifice in this day and age the way that one did. And that makes me sadder still. On the day of his death, I won't pollute his memory by thinking of anything other than remembering him and his generation for what they gave me and this country. Will the circumstances of his death somehow help make me a better pilot. I could not possibly care less. On this day, it's more important for me, personally, to reflect on whether his life will help make me a better person. On this day, I'd also like to remember another member of the Greatest Generation who passed today. Eustace Bohay. Resume. Bob Collins St. Paul ________________________________________________________________________________
Date: Apr 21, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
calls) >Matt Dralle wrote: >Its a good cause, though, if >you value your right to fly in the US. >Matt I was once a AOPA guy 20 years ago but quit for several reasons. However I did recently hear that the "AOPA adviser" was claiming homebuilts are such a liability that if you sell one you should part it out. I just want to say there has NEVER been a lawsuit against any builder. Absolutly NO legal precedence. Sure we are liable for everything. Your dog bites someone you can go to jail. However if you get a lawyer to draw up a liability release, sometimes called a "hold harmless waiver", chance of lawsuit is slim. If you knowingly did not put the spar bolts in, or some other nonsense, yes you might have negligence problem. A safe RV, built to plans, not likely to be a problem. Again NEVER happened, no lawsuits and AOPA is WRONG if this is their claim. I would love someone else to write or ask the AOPA adviser the same question. Any way I don't think AOPA supports Kit planes or homebuilts because it is counter to there main customers aircraft manufactures and corporate operators. Just read their magazine. It is like a corporate aviation magazine. Not saying they don't do good for all of us, I am just saying that they are somewhat impotent or ineffective, but it is better than nothing I guess. After 10 years I dropped them about 10 years ago. They sent me crap for years trying to get me back. George --------------------------------- ________________________________________________________________________________
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone call
From: "N395V" <n395v(at)hughes.net>
Date: Apr 21, 2006
There are many things I do not like about the aopa. 1. Every publication, web page etc is filled with 50% content of "Phil Boyer says" Phil Boyer does" etc. I think there is a rule that every simple sentence must mention Phil Boyer 7 times. 2. Unsolicited phone calls during the evening as mentioned some peskier than others. 3. Their seeming lack of support for experimentals. Having said all that they will continue to recieve my support as they do a good service for all of us. An entities 1st responsability is to survive and a good way to do this is cater to your sponsors. -------- Milt N395V F1 Rocket Read this topic online here: http://forums.matronics.com/viewtopic.php?p=29829#29829 ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
call
Date: Apr 21, 2006
I once offered to write an article for AOPA on the use of alternative engines in aircraft - absolutely no interest, said their readership was not interested - which clearly pointed out that I for one did not belong in an organization that had no interest in my interest. EAA has certainly slipped far down the Commercial slope and should really changed its name from the EAA or at least take the "E" out. Having said that, I support it simply because I do believe that without the EAA and AOPA our freedom to fly would have been even more seriously curtailed ( than has occurred). I do feel we must all be vigilant against the FAA's attempt to levy "users fees". We paid taxes to support the government and its agencies, we should not be taxed again simply to compensate for bureaucratic inefficiency and mismanagement. Look at Canada and take heed. my 0.02 worth Ed Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC eanderson(at)carolina.rr.com ----- Original Message ----- From: "N395V" <n395v(at)hughes.net> Sent: Friday, April 21, 2006 8:17 AM Subject: RV-List: Re: AOPA hates homebuilts? (was donation-solicitation phone call > > There are many things I do not like about the aopa. > > 1. Every publication, web page etc is filled with 50% content of "Phil > Boyer says" Phil Boyer does" etc. I think there is a rule that every > simple sentence must mention Phil Boyer 7 times. > > 2. Unsolicited phone calls during the evening as mentioned some peskier > than others. > > 3. Their seeming lack of support for experimentals. > > Having said all that they will continue to recieve my support as they do a > good service for all of us. > > An entities 1st responsability is to survive and a good way to do this is > cater to your sponsors. > > -------- > Milt > N395V > F1 Rocket > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=29829#29829 > > > ________________________________________________________________________________
From: "Oliver Washburn" <ollie6a(at)earthlink.net>
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
calls)
Date: Apr 21, 2006
----- Original Message ----- From: <gmcjetpilot(at)yahoo.com> Sent: Friday, April 21, 2006 4:05 AM Subject: RV-List: Re: AOPA hates homebuilts? (was donation-solicitation phone calls) > >>Matt Dralle wrote: >>Its a good cause, though, if >>you value your right to fly in the US. > >Matt > > I was once a AOPA guy 20 years ago but quit for several reasons. > > All I can say is if it wasn't for AOPA and EAA you would not be enjoying > as much freedom for flying as you have today, and anyone who dosen't > support them in my estimation dosen't care about freedom of flight. It > seems like everyday the TSA or some other organisation trys to grabe a > little more of our freedom. Ollie 6a Central Fl > > > ________________________________________________________________________________
Date: Apr 21, 2006
From: bertrv6(at)highstream.net
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
calls) Quoting gmcjetpilot(at)yahoo.com: > > >Matt Dralle wrote: > >Its a good cause, though, if > >you value your right to fly in the US. > >Matt > > I was once a AOPA guy 20 years ago but quit for several reasons. > > However I did recently hear that the "AOPA adviser" was claiming > homebuilts are such a liability that if you sell one you should part > it out. I just want to say there has NEVER been a lawsuit against > any builder. Absolutly NO legal precedence. > > Sure we are liable for everything. Your dog bites someone you can > go to jail. However if you get a lawyer to draw up a liability release, > sometimes called a "hold harmless waiver", chance of lawsuit is > slim. If you knowingly did not put the spar bolts in, or some other > nonsense, yes you might have negligence problem. A safe RV, > built to plans, not likely to be a problem. > > Again NEVER happened, no lawsuits and AOPA is WRONG > if this is their claim. > > I would love someone else to write or ask the AOPA adviser the > same question. > > Any way I don't think AOPA supports Kit planes or homebuilts > because it is counter to there main customers aircraft manufactures > and corporate operators. Just read their magazine. It is like a > corporate aviation magazine. Not saying they don't do good for all of > us, I am just saying that they are somewhat impotent or ineffective, > but it is better than nothing I guess. After 10 years I dropped them > about 10 years ago. They sent me crap for years trying to get me back. > > George > > George: whoever you are; I have been a member of AOPA for ever , at least 40 years.. There is not any one that admits, AOPA,is the only organization that do so much for General Aviation, No one, and we Experimental, are part of that.. Aopa has the clout in Washington, do change things. I do not have to tell you the number of things they accomplish, for us.... The magazine, yes, it is not "Experimental" per se....why, because, the market is saturated with dozens, or such magazines... what would be the purpose of adding to the already fillled segment...? I am subscribed, to three of this,, Custom Planes, Kit Planes, and Pilot magazine, in addition to EAA, which I am also member since I started flying. I wish you have named the person, that told you, about experimental no good... I have talked thru the years, with many of them...no once they ever even suggested, Experimental aircraft was unsafe, only the builders are unsafe... OH< by th way George,,,just this alone, makes my case...I recently got my medical Certificate back,,,,and only because AOPA.... ENOUGH SAID.. Bert rv6a Do nopt archive > > --------------------------------- > > ________________________________________________________________________________
Date: Apr 21, 2006
From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)consolidated.net>
Subject: Re: Sensitive reading of posts
> > >>I finally came to the conclusion that this list really doesn't tolerate >>differing points of view, and indeed those on this list act as if threatened >>by them. >> >>Thus after many years, I am unsubscribing. If I build an RV in the >>future, I will strictly make use of the archives. >> Kysh.... There are different points of view, but that doesnt mean "the List" won't tolerate them. The "list" is just a bunch of faceless, unknown typwriters somewhere off in the distance. Each of these typewriters (ok I'll say computers) has a personality (person) connected to it.. Keep in mind that for each posting, there may be 200 or 300 readers (lurkers) who read the post, agreed with it, and did not replay. We as pilots quite often don't agree with each other, but we should still stick together. We need to get as connected as firemen and COP's for our own survival. Those two groups have real fraternity. I'm sure they have disagreements, but they stick together. We as pilots tend to have "high" ego's. Whatever we have, we need to stick together, stop snitching on one another and become a Fraternity...... Flame me, I got skin that is 66 years old and tough as sandpaper... Phil in Illinois Oh, I met Linn Walters at the Curtis Pitts memorial in Sun and Fun. Now, he is not a faceless computer any more.......... Real fine person... Helpful and full of good answers... "Pitts" driver too....... that make him "special"........ ________________________________________________________________________________
From: "John Helms" <jhelms(at)nationair.com>
Subject: Parting out your homebuilt (was AOPA hates homebuilts?)
Date: Apr 21, 2006
In my professional opinion, parting it out doesn't get you what you're after. It merely spreads the risk around. If you sell the wings to one individual, he/she puts them on their plane and they fail, you might be sued over that. They may not win, but they can always sue. Same for the engine, fuselage, etc, etc. Hold harmless agreements might be useful. I'll allow attorney's to discuss that. In my humble opinion, the very best thing that a seller can do to alleviate the amount of liability any type of airplane owner has when selling a plane is to is have a third party do an annual on the plane as the pre-buy inspection. That way, a third party has signed his name to attest that the plane is airworthy. Lawsuits after an airplane has been sold happen. There just has not yet been one for what you all are discussing (poor building). If a person buys a plane (production or experimental) and the engine quits shortly after the purchase, whether someone is hurt in the subsequent landing/crash there will very likely be a lawsuit against the former owner for poorly maintaining the plane. As the builder of an experimental aircraft, one is always likely to have some risk of being sued, but the longer that the plane has been successfully flown (by both you when you owned it, and after it was sold) the harder that is going to be to win for someone claiming it was "built poorly" because "if it was built so poorly then why did it successfully fly XXXX hours?" John "JT" Helms Branch Manager, NationAir Insurance Agency, Light Aircraft Office. In response to: I was once a AOPA guy 20 years ago but quit for several reasons. However I did recently hear that the "AOPA adviser" was claiming homebuilts are such a liability that if you sell one you should part it out. I just want to say there has NEVER been a lawsuit against any builder. Absolutly NO legal precedence. Sure we are liable for everything. Your dog bites someone you can go to jail. However if you get a lawyer to draw up a liability release, sometimes called a "hold harmless waiver", chance of lawsuit is slim. If you knowingly did not put the spar bolts in, or some other nonsense, yes you might have negligence problem. A safe RV, built to plans, not likely to be a problem. Again NEVER happened, no lawsuits and AOPA is WRONG if this is their claim. I would love someone else to write or ask the AOPA adviser the same question. Any way I don't think AOPA supports Kit planes or homebuilts because it is counter to there main customers aircraft manufactures and corporate operators. Just read their magazine. It is like a corporate aviation magazine. Not saying they don't do good for all of us, I am just saying that they are somewhat impotent or ineffective, but it is better than nothing I guess. After 10 years I dropped them about 10 years ago. They sent me crap for years trying to get me back. George ________________________________________________________________________________
From: "Konrad L. Werner" <klwerner(at)comcast.net>
Subject: RV legend Eustace Bowhay dies
Date: Apr 21, 2006
Dear RV'ers, We lost another legendary Aviator this week, Mr. Eustace Bowhay. RV legend Eustace Bowhay dies. Eustace died Tuesday of apparent complications from a stroke. "He joined the RV ranks in the 1990s by building C-HAY, a 180 hp RV-6 which he flew on wheels, floats and amphibious floats. In the RV community he found many low time pilots venturing into the world of relatively high performance and became their mentor. At the factory, Van=92s people learned to listen carefully to the tall, white haired, slightly deaf Canadian fellow with the suspenders. There was a little =93eh?=94 and a little =93oot=94 in his speech, as well as a whole lot of humanity, wisdom and humor," wrote Doug Reeves in a recent tribute (More) My hat is off to the Giant. Have a grand journey! ________________________________________________________________________________
From: "Dan Morrow" <DanFM01(at)butter.toast.net>
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
calls)
Date: Apr 21, 2006
"Never" is a big word. I can think of two lawsuits against builders just from casual reading of the news in the last few years. Lawsuit 1: In the John Denver crash, the newspapers reported that Denver's relatives sued several people including the builder. I don't know the outcome however. Lawsuit 2: This one was somewhat complicated involving several sales and owners. Step 1: Individual A builds aircraft and flies for several years. Sells aircraft to individual B. Step 2: B flies aircraft for several years and then sells aircraft to individual C. Step 3: C flies aircraft for several years. Then one day he takes a friend's wife for a ride and performs low level aerobatics in view of the husband. Crashes killing himself and friend's wife. Step 4: Husband sues individual A. Step 5: Individual A sues B. I don't know the outcome of the lawsuits. Homebuilders can be sued and are sued on liability issues. Three factors seem to limit the number of lawsuits however. One is that juries tend to be sceptical of claims from anyone who knowingly flies in a homebuilt aircraft. The second is that most builders don't have the big bucks to attract big name tort lawyers. The third is that the builder often dies in the accident and his family has no reason to sue. Lawsuits are a something to worry about. Even if you win the lawsuit the legal fees can be devastating. Avemco at one point offered converage for a year or two after the sale of a homebuilt, but I don't know if they still do. ----- Original Message ----- From: <gmcjetpilot(at)yahoo.com> Sent: Friday, April 21, 2006 1:05 AM Subject: RV-List: Re: AOPA hates homebuilts? (was donation-solicitation phone calls) > >>Matt Dralle wrote: >>Its a good cause, though, if >>you value your right to fly in the US. > >Matt > > I was once a AOPA guy 20 years ago but quit for several reasons. > > However I did recently hear that the "AOPA adviser" was claiming > homebuilts are such a liability that if you sell one you should part > it out. I just want to say there has NEVER been a lawsuit against > any builder. Absolutly NO legal precedence. > > Sure we are liable for everything. Your dog bites someone you can > go to jail. However if you get a lawyer to draw up a liability release, > sometimes called a "hold harmless waiver", chance of lawsuit is > slim. If you knowingly did not put the spar bolts in, or some other > nonsense, yes you might have negligence problem. A safe RV, > built to plans, not likely to be a problem. > > Again NEVER happened, no lawsuits and AOPA is WRONG > if this is their claim. > > I would love someone else to write or ask the AOPA adviser the > same question. > > Any way I don't think AOPA supports Kit planes or homebuilts > because it is counter to there main customers aircraft manufactures > and corporate operators. Just read their magazine. It is like a > corporate aviation magazine. Not saying they don't do good for all of > us, I am just saying that they are somewhat impotent or ineffective, > but it is better than nothing I guess. After 10 years I dropped them > about 10 years ago. They sent me crap for years trying to get me back. > > George > > > --------------------------------- > > > -- > > ________________________________________________________________________________
Date: Apr 21, 2006
From: Chris W <3edcft6(at)cox.net>
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
call Ed Anderson wrote: > >I once offered to write an article for AOPA on the use of alternative >engines in aircraft - absolutely no interest, said their readership was not >interested - which clearly pointed out that I for one did not belong in an >organization that had no interest in my interest. > > So I guess you have no interest in being a private pilot and actually having the right to fly in the USA. -- Chris W KE5GIX ________________________________________________________________________________
Date: Apr 21, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Update: Fuel Flow Transducer-Injected
Pardon my ignorance on fuel injections, but here's how the routing goes: Fuel out of the firewall to servo. (I'm assuming the servo is where the mixture cable plugs into) There are two lines that go from the servo the to the divider (the thing on the sump where a carb would go, and where the spider is..the spider is on the bottom of my engine, not on the top like most). One fuel line to the left side, and one to the right (or from one side, as a return) Then there is a third line out of the servo back to the fuel selector or tee that fills the left tank. Not sure of the make..there is a data tag on it that I briefly read the other day but it wasn't anything familiar. There is a fuel pressure transducer from the original installation on one of the lines from the servo to the divider, so I'm assuming that's where I'll put my fuel flow. ________________________________________________________________________________
Date: Apr 21, 2006
From: "Bob J." <rocketbob(at)gmail.com>
Subject: Re: Update: Fuel Flow Transducer-Injected
Yep...this is not a bendix system, and the name eludes me right now. I have seen it before and and the spider and lines are on the bottom side as you describe. I have service instructions for this type of system, if I look it up in my foot thick stack of Lycoming service instructions I should be able to tell you what it is tonight.... Regards, Bob Japundza RV-6 flying, F1 under const. On 4/21/06, Paul Besing wrote: > > > Pardon my ignorance on fuel injections, but here's how > the routing goes: > > Fuel out of the firewall to servo. (I'm assuming the > servo is where the mixture cable plugs into) > > There are two lines that go from the servo the to the > divider (the thing on the sump where a carb would go, > and where the spider is..the spider is on the bottom > of my engine, not on the top like most). One fuel > line to the left side, and one to the right (or from > one side, as a return) > > Then there is a third line out of the servo back to > the fuel selector or tee that fills the left tank. > Not sure of the make..there is a data tag on it that I > briefly read the other day but it wasn't anything > familiar. > > There is a fuel pressure transducer from the original > installation on one of the lines from the servo to the > divider, so I'm assuming that's where I'll put my fuel flow. > > ________________________________________________________________________________
Date: Apr 21, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Update: Fuel Flow Transducer-Injected
Thanks, Bob. Yeah, it's definately not a bendix system, but it works very well...never any vapor lock and starts on the first blade every time, after 16 years of service and 800 hours. Can't find anyting in the logbook regarding maintenance issues. Paul Besing --- "Bob J." wrote: > > > Yep...this is not a bendix system, and the name > eludes me right now. I have > seen it before and and the spider and lines are on > the bottom side as you > describe. I have service instructions for this type > of system, if I look it > up in my foot thick stack of Lycoming service > instructions I should be able > to tell you what it is tonight.... > > Regards, > Bob Japundza > RV-6 flying, F1 under const. > > > On 4/21/06, Paul Besing wrote: > > > > > > > Pardon my ignorance on fuel injections, but here's > how > > the routing goes: > > > > Fuel out of the firewall to servo. (I'm assuming > the > > servo is where the mixture cable plugs into) > > > > There are two lines that go from the servo the to > the > > divider (the thing on the sump where a carb would > go, > > and where the spider is..the spider is on the > bottom > > of my engine, not on the top like most). One fuel > > line to the left side, and one to the right (or > from > > one side, as a return) > > > > Then there is a third line out of the servo back > to > > the fuel selector or tee that fills the left tank. > > Not sure of the make..there is a data tag on it > that I > > briefly read the other day but it wasn't anything > > familiar. > > > > There is a fuel pressure transducer from the > original > > installation on one of the lines from the servo to > the > > divider, so I'm assuming that's where I'll put my > fuel flow. > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
call
Date: Apr 21, 2006
----- Original Message ----- From: "Chris W" <3edcft6(at)cox.net> Sent: Friday, April 21, 2006 2:34 PM Subject: Re: RV-List: Re: AOPA hates homebuilts? (was donation-solicitation phone call > > Ed Anderson wrote: > >> >>I once offered to write an article for AOPA on the use of alternative >>engines in aircraft - absolutely no interest, said their readership was >>not >>interested - which clearly pointed out that I for one did not belong in an >>organization that had no interest in my interest. >> >> > > So I guess you have no interest in being a private pilot and actually > having the right to fly in the USA. > > -- > Chris W Actually, Chris, you apparently failed to read my complete message in which I also stated " ..... Having said that, I support it simply because I do believe that without the EAA and AOPA our freedom to fly would have been even more seriously curtailed ( than has occurred)...." Ed A ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: AOPA hates homebuilts? (was donation-solicitation phone
call
Date: Apr 21, 2006
----- Original Message ----- From: "Chris W" <3edcft6(at)cox.net> Sent: Friday, April 21, 2006 2:34 PM Subject: Re: RV-List: Re: AOPA hates homebuilts? (was donation-solicitation phone call > > Ed Anderson wrote: > >> >>I once offered to write an article for AOPA on the use of alternative >>engines in aircraft - absolutely no interest, said their readership was >>not >>interested - which clearly pointed out that I for one did not belong in an >>organization that had no interest in my interest. >> >> > > So I guess you have no interest in being a private pilot and actually > having the right to fly in the USA. > > -- > Chris W > KE5GIX > > > > ________________________________________________________________________________
From: "Gordon or Marge Comfort" <gcomfo(at)tc3net.com>
Subject: AOA
Date: Apr 21, 2006
. I am not a big AOA fan (despite hundreds of hours with them) Jim Van Laak RV-6 N79RL Jim: I am interested in your comment about AOA's. Some have suggested I invest in one but I'm doubtful. Would you amplify on the subject, please? Reply off list if you like. Gordon Comfort N363GC ________________________________________________________________________________
From: "Konrad L. Werner" <klwerner(at)comcast.net>
Subject: Re: Eustace Bowhay
Date: Apr 21, 2006
To Eustace: May you rest in Peace and fly on forever [Ed. This news hurts. The text below appears in this site's Safety section and was written several months back. Eustace was kind enough to host RVTalk #17. He passed away on Tuesday, apparently of complications from a stroke. The RV community has lost one of its giants and our hearts go out to the Bowhay family and friends. By Doug Reeves of www.vansairforce.com] This is for those of you that have never met him, but it is also for the one's that did have the priviledge . . . . "For RV pilots and builders who have never had the opportunity to meet Eustace Bowhay, here=92s a little background. Eustace is one of the few people around who=92ve accumulated over 20,000 hours of flying time without ever having a military or airline career. He spans aviation from before WW2 to the present day. His first flight, as a boy of 10 or 11, was in a Gypsy Moth over his native Saskatchewan. It=92s a great story...Eustace and his mother lived on a farm outside of town, and every weekend the weather permitted they=92d go into the city for supplies and a bit of recreation. He would spend part of his Saturday morning at piano lessons. Nothing in this world was going to make a pianist out of Eustace, but he went to please his mother and because she gave him a quarter so he could go to the movies after his lesson. Eustace soon discovered that the airport on the edge of town was far more interesting to him than any movie, so after his lesson he=92d go down and hang on the fence until it was time to go, just hoping to see an airplane fly. He=92d time it carefully so he could run back to town and meet his mother at the theatre...he knew she=92d never approve of something so dangerous as flying! After a few weeks of this, one of the local pilots on the other side of the fence motioned him over to a hangar and opened the back door. Completely awestruck, Eustace stepped through the door and into what was to become his world for a lifetime. In the hangar was a brand new Staggerwing, painted royal blue. Out in front, a pilot who needed to warm the oil in his Moth invited Eustace to occupy the front cockpit. Stricken to silence by his good fortune, Eustace pulled on a leather helmet and goggles and held on as the upright Gypsy engine rattled the Moth into the air. They flew out over the prairie and over Eustace=92s home. When they returned, Eustace realized he was late meeting his mother and dashed into town, maintaining a minimum altitude of about six inches the whole way. Without comment, he climbed into the car and home they went. At the dinner table that evening, his uncle casually mentioned that an airplane had circled the farm several times earlier in the day. Did Eustace know anything about that? Oh, no, Eustace said. He=92d been at piano lessons and the movies the whole day. Everyone at the table broke into laughter. When his mother handed him a mirror he saw why: the Gypsy had been spraying a fine mist back over the fuselage for the entire flight and the oily outline of the helmet and goggles was clearly printed on his face. He looked like a surprised raccoon. When Eustace tells this story, the memories of that day - more than seventy years ago now - are printed on his face as plainly as the outline of those goggles. He still remembers the smell of the paint and dope on the Staggerwing and the exhilaration of banking and seeing his home between the flying wires of the Moth. After that came flying and more flying. Eustace instructed thousands of students in the RCAF, some of whom died in combat just weeks later - he=92s never fully accepted that waste and a bit of grief is with him still. After the war he instructed thousands more, as well as flying Navions and Aeronca Champs and God knows what else away from the factories and back to Canada. Supported by his wife Nora, he formed his own company, providing charter air service all over the Canada and the Northern Territories. He flew and flew; in Aztec, in Cessnas, in Beavers and Otters. He acquired a P-51 from the Canadian government and flew it all over the country keeping an eye on his operations. He owned and flew a DC-3 for many years. He=92s got 9000+ hours of water operation...1000 hours of it in a Grumman Goose. He=92s landed parts of a bulldozer on the edge of the Arctic Ocean in a Beech 18, helped weld the machine back together and build a landing strip and watched the bulldozer leave, intact, in the hold of a Hercules that flew into the strip to retrieve it. And all the while, one of his primary concerns was keeping other pilots safe. He preached, cajoled, and extolled safe flying at every opportunity, bringing his vast experience to bear and distilling it to benefit the newest of pilots. We will never know just how many pilots are alive (and airplanes unbroken) because Eustace had a word with them, planting some seed of care and awareness that allowed them to avoid danger. He joined the RV ranks in the 1990s by building C-HAY, a 180 hp RV-6 which he flew on wheels, floats and amphibious floats. In the RV community he found many low time pilots venturing into the world of relatively high performance and became their mentor. At the factory, Van=92s people learned to listen carefully to the tall, white haired, slightly deaf Canadian fellow with the suspenders. There was a little "eh?" and a little "oot" in his speech, as well as a whole lot of humanity, wisdom and humor. Eustace and Nora have been to many of Van=92s Homecomings and many RV pilots have met and talked with them. If you=92ve ever had a chance to sit and talk with them, you=92ll have realized that you were in the presence of truly fine people Now recovering from a stroke in his hometown of Salmon Arm, British Columbia, Eustace is still pursuing his passion for helping pilots fly safely and skillfully. It is our incredibly good fortune that he's part of the RV world and that modern technology allows us to essentially sit around the campfire and listen to him pass on knowledge gained over a career that has spanned 70% of powered aviation. Don=92t miss the chance - there aren=92t many like him. Heck, there aren=92t any like him. Eustace is one of a kind." Arrangements (from a Ken Hoshowski email fwd'd to me) Just to let you know that the service gathering for Eustace will be this Saturday at 1:30 at Fischer's Funeral Services, 4060 1st. Ave S.W. Salmon Arm. Toll free phone 1-888-816-1117 This is going to be a tea only, a celebration of life service will be held at a later date in Eustace's home town in Alberta. Eustace's wife's name is Nora and the home address is #6-350 Hudson St. N.W, Salmon Arm B.C., V1E1P4, phone 250 832-3273. That is about all I can tell (you) for now. Ken Hoshowski RV6 C-FKEH Salmon Arm B.C. ________________________________________________________________________________
Date: Apr 21, 2006
From: "kelby alexander" <n41va(at)blazemail.com>
Subject: Flying A Transporting is ready to take your order
Here it is! "Flying A Transporting" will be taking reservations for May and the months to follow to deliver your QB or Standard Kits. The trailer has arrived, the truck is days from being here. Insurance, permits and all liscences are all in order finally. I will be advertising on this site in a month or so, so keep your eyes open for that as well and I will post a link for my new web site soon. Email me at rvshipper(at)blazemail.com for a price quote. The first 5 customers will receive a FREE headset or a Gift Certificate to Sportys Pilot Shop for the value of the headset. I am a Liscenced, Bonded and Insured Tranporting Company. And I am personally going to be driving the truck and trailer with your kit in it. So I can do it at a better price than ANYBODY else because I dont have to pay any drivers, Guaranteed! Kelby L. Alexander "Flying A Transporting" 541.550.0689 Fight the power! BlazeMail.com ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: MT Props delay
Date: Apr 21, 2006
Steve, Suggest you consider a Aero Composites carbon fiber prop. It we be on average 10 knots faster, same weight, has lightning protection, is considerably stronger etc. ad infinitum. Also more expensive, but worth it. Delivery is usually 70 to 90 days. Dick Martin RV8 N233M the fast one ----- Original Message ----- From: "Steve & Denise" <sjhdcl(at)kingston.net> Sent: Monday, April 03, 2006 2:29 PM Subject: RV-List: MT Props delay > > Anybody know a faster way to get a MT Prop? > > Van's (MTs) wait time is currently 16 weeks. > > Looking for 2 blade, hydraulic. MTV15B/183-109 > > Steve > RV7A > > > ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: Performance Problem Analysis
Date: Apr 21, 2006
Dave, I have an RV8 with a James Cowl and plenum and a IO-390 engine. I believe that it contributes and average speed increase of 10 knots over a standard Vans cowl. I have over 1300 hours with this set up. I have also talked to as many others with this set up as possible, and the general consensus is the same as mine. Also, cooling problems are usually not a problem with this cowl. Dick Martin RV8 N233M the fast one ----- Original Message ----- From: "David Burden" <hootsnik(at)sbcglobal.net> Sent: Friday, March 24, 2006 8:42 AM Subject: RV-List: Performance Problem Analysis > > Hello Listers, > > I am working through a performance issue and need some help. I need to > find some folks who have flying aircraft with the following combination of > features: > > Flying RV7a or 9a > Carburated 180 hp 0360 (Superior/ECI/Lyc) > Sam James Cowl/plenum/induction system > Fixed pitch propellor > > The intent is to compare some data and discuss any install challenges you > may have had to overcome with this, apparently rare combination. > > Please respond off list to: > > hootsnik(at)sbcglobal.net > > Thanks in advance for the help. > > Dave > > > ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: MT Props delay
Date: Apr 21, 2006
Steve, Suggest you consider a Aero Composites carbon fiber prop. It we be on average 10 knots faster, same weight, has lightning protection, is considerably stronger etc. ad infinitum. Also more expensive, but worth it. Delivery is usually 70 to 90 days. Dick Martin RV8 N233M the fast one ----- Original Message ----- From: "Steve & Denise" <sjhdcl(at)kingston.net> Sent: Monday, April 03, 2006 2:29 PM Subject: RV-List: MT Props delay > > Anybody know a faster way to get a MT Prop? > > Van's (MTs) wait time is currently 16 weeks. > > Looking for 2 blade, hydraulic. MTV15B/183-109 > > Steve > RV7A > > > ________________________________________________________________________________
From: "RV6 Flyer" <rv6_flyer(at)hotmail.com>
Subject: Re: MT Props delay
Date: Apr 22, 2006
Try another vendor. http://www.lessdrag.com/lycomingpropeller.html Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, 1,842 + Flying Hours So. CA, USA http://SoCAL_WVAF.rvproject.com ----Original Message Follows---- From: "dick martin" <martin(at)gbonline.com> Subject: Re: RV-List: MT Props delay Date: Fri, 21 Apr 2006 20:34:26 -0500 Steve, Suggest you consider a Aero Composites carbon fiber prop. It we be on average 10 knots faster, same weight, has lightning protection, is considerably stronger etc. ad infinitum. Also more expensive, but worth it. Delivery is usually 70 to 90 days. Dick Martin RV8 N233M the fast one ----- Original Message ----- From: "Steve & Denise" <sjhdcl(at)kingston.net> Sent: Monday, April 03, 2006 2:29 PM Subject: RV-List: MT Props delay > > Anybody know a faster way to get a MT Prop? > > Van's (MTs) wait time is currently 16 weeks. > > Looking for 2 blade, hydraulic. MTV15B/183-109 > > Steve > RV7A > > > > > > > > > > > > > > > ________________________________________________________________________________
From: luckymacy(at)comcast.net (lucky)
Subject: Re: Performance Problem Analysis
Date: Apr 22, 2006
WRT James cowl, is it basically just the differently shaped air inlets and their inlet area that make the difference? What's the diameter of the openings? In other words, if one took Van's cowl and redid the openings would that theoretically lower drag?? Or is there a fundamental difference in the air outlet area on the bottom too? Anyone ever take a side by side photos and otherwise do a meaningful compare? Just curious and looking for rainy day projects.... -------------- Original message -------------- From: "dick martin" <martin(at)gbonline.com> > > Dave, > I have an RV8 with a James Cowl and plenum and a IO-390 engine. I believe > that it contributes and average speed increase of 10 knots over a standard > Vans cowl. I have over 1300 hours with this set up. I have also talked to > as many others with this set up as possible, and the general consensus is > the same as mine. Also, cooling problems are usually not a problem with > this cowl. > Dick Martin > RV8 N233M > the fast one > ----- Original Message ----- > From: "David Burden" > To: > Sent: Friday, March 24, 2006 8:42 AM > Subject: RV-List: Performance Problem Analysis > > > > > > Hello Listers, > > > > I am working through a performance issue and need some help. I need to > > find some folks who have flying aircraft with the following combination of > > features: > > > > Flying RV7a or 9a > > Carburated 180 hp 0360 (Superior/ECI/Lyc) > > Sam James Cowl/plenum/induction system > > Fixed pitch propellor > > > > The intent is to compare some data and discuss any install challenges you > > may have had to overcome with this, apparently rare combination. > > > > Please respond off list to: > > > > hootsnik(at)sbcglobal.net > > > > Thanks in advance for the help. > > > > Dave > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > WRT James cowl, is it basically just the differently shaped air inlets and their inlet areathat make the difference? What's the diameter of the openings? In other words, if one took Van's cowl and redid the openings would that theoretically lower drag?? Or is there a fundamental difference in the air outlet area on the bottom too? Anyone ever take a side by side photos and otherwise do a meaningful compare? Just curious and looking for rainy day projects.... -------------- Original message -------------- From: "dick martin" martin(at)gbonline.com -- RV-List message posted by: "dick martin" Dave, I have an RV8 with a James Cowl and plenum and a IO-390 engine. I believe that it contributes and average speed increase of 10 knots over a standard Vans cowl. I have over 1300 hours with this set up. I have also talked to as many others with this set up as possible, and the general consensus is the same as mine. Also, cooling problems are usually not a problem with this cowl. Dick Martin RV8 N233M the fast one ----- Original Message ----- From: "David Burden" <HOOTSNIK(at)SBCGLOBAL.NET> To: Sent: Friday, March 24, 2006 8:42 AM Subject: RV-List: Perfor mance Problem Analysis -- RV-List message posted by: David Burden Hello Listers, I am working through a performance issue and need some help. I need to find some folks who have flying aircraft with the following combination of features: Flying RV7a or 9a Carburated 180 hp 0360 (Superior/ECI/Lyc) Sam James Cowl/plenum/induction system Fixed pitch propellor The intent is to compare some data and discuss any install challenges you may have had to overcome with this, apparently rare combination. Please respond off list to: hootsnik(at)sbcglobal.net Thanks in advance for the help. Dave < BR> hank y ou for your generous support! ________________________________________________________________________________
Date: Apr 22, 2006
From: "Bob J." <rocketbob(at)gmail.com>
Subject: Re: Update: Fuel Flow Transducer-Injected
Paul, I'm guessing its a Simmonds fuel injection system, in the picture the fuel distributor (spider) is part of the servo. SI1040A is titled "Maintenance procedures applicable to Simmonds #530 fuel injection system." Its a two pager with not much useful info. Regards, Bob Japundza RV-6 flying F1 under const. On 4/21/06, Paul Besing wrote: > > > Thanks, Bob. Yeah, it's definately not a bendix > system, but it works very well...never any vapor lock > and starts on the first blade every time, after 16 > years of service and 800 hours. Can't find anyting in > the logbook regarding maintenance issues. > > Paul Besing > > --- "Bob J." wrote: > > > > > > > Yep...this is not a bendix system, and the name > > eludes me right now. I have > > seen it before and and the spider and lines are on > > the bottom side as you > > describe. I have service instructions for this type > > of system, if I look it > > up in my foot thick stack of Lycoming service > > instructions I should be able > > to tell you what it is tonight.... > > > > Regards, > > Bob Japundza > > RV-6 flying, F1 under const. > > > > > > On 4/21/06, Paul Besing wrote: > > > > > > > > > > > Pardon my ignorance on fuel injections, but here's > > how > > > the routing goes: > > > > > > Fuel out of the firewall to servo. (I'm assuming > > the > > > servo is where the mixture cable plugs into) > > > > > > There are two lines that go from the servo the to > > the > > > divider (the thing on the sump where a carb would > > go, > > > and where the spider is..the spider is on the > > bottom > > > of my engine, not on the top like most). One fuel > > > line to the left side, and one to the right (or > > from > > > one side, as a return) > > > > > > Then there is a third line out of the servo back > > to > > > the fuel selector or tee that fills the left tank. > > > Not sure of the make..there is a data tag on it > > that I > > > briefly read the other day but it wasn't anything > > > familiar. > > > > > > There is a fuel pressure transducer from the > > original > > > installation on one of the lines from the servo to > > the > > > divider, so I'm assuming that's where I'll put my > > fuel flow. > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > browse > > Subscriptions page, > > FAQ, > > > > > > Admin. > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Performance Problem Analysis
Date: Apr 22, 2006
On 22 Apr 2006, at 10:41, lucky wrote: > > WRT James cowl, is it basically just the differently shaped air > inlets and their inlet area that make the difference? What's the > diameter of the openings? In other words, if one took Van's cowl > and redid the openings would that theoretically lower drag?? > > Or is there a fundamental difference in the air outlet area on the > bottom too? > > Anyone ever take a side by side photos and otherwise do a > meaningful compare? > > Just curious and looking for rainy day projects.... Lucky, As I understand it, the performance increase comes from three places: 1. The cowl comes with a plenum chamber, which means more of the air that comes in the inlets actually cools the engine. Baffles leak, so you need to bring in extra air to allow for that leakage. The fact that the plenum chamber has less leakage means less air is needed, so the inlets are smaller. The less air you bring in the inlets, the less cooling drag there is. 2. The contour of the inlet is designed to try to have laminar flow as the air expands, which results in the least amount of drag, and the greatest amount of pressure once the air has expanded. 3. The inlet shape is round. Round inlets have the smallest circumference for a given area, so there is less frictional drag along the walls of the inlet. Any frictional drag results in some pressure loss in the cooling air, which reduces the cooling effectiveness, and means you probably need a bit more air to get the same amount of cooling. This is probably a very minor effect. I believe you could achieve most of the performance increase by having a plenum chamber that has a good seal at the inlet, and reducing the size of the inlets. Many people add plenum chambers, but I believe most of them don't have a good seal at the inlet, so there is quite a bit of leakage there. I also believe that most people don't reduce the size of the inlets. If you don't reduce the size of the inlets, you won't realize any performance increase. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: Performance Problem Analysis
Date: Apr 22, 2006
Sam James used to sell (and may still sell) round inlets that you can retrofit into your stock cowl. I looked into it when I was building my plane and decided that 1) It would be a lot of work. 2) Even worse, the work would be *serious* fiberglass work. 3) It would be a shame to mess up the nice factory cowling. If I recall correctly, Sam's recommendation was that without a plenum (which he sold), the cowl mod probably wasn't worth the effort. KB ----- Original Message ----- From: "lucky" <luckymacy(at)comcast.net> Sent: Saturday, April 22, 2006 10:41 AM Subject: Re: RV-List: Performance Problem Analysis > > WRT James cowl, is it basically just the differently shaped air inlets and > their inlet area that make the difference? What's the diameter of the > openings? In other words, if one took Van's cowl and redid the openings > would that theoretically lower drag?? > > Or is there a fundamental difference in the air outlet area on the bottom > too? > > Anyone ever take a side by side photos and otherwise do a meaningful > compare? > > Just curious and looking for rainy day projects.... > -------------- Original message -------------- > From: "dick martin" <martin(at)gbonline.com> > >> >> Dave, >> I have an RV8 with a James Cowl and plenum and a IO-390 engine. I believe >> that it contributes and average speed increase of 10 knots over a >> standard >> Vans cowl. I have over 1300 hours with this set up. I have also talked to >> as many others with this set up as possible, and the general consensus is >> the same as mine. Also, cooling problems are usually not a problem with >> this cowl. >> Dick Martin >> RV8 N233M >> the fast one >> ----- Original Message ----- >> From: "David Burden" >> To: >> Sent: Friday, March 24, 2006 8:42 AM >> Subject: RV-List: Performance Problem Analysis >> >> >> > >> > Hello Listers, >> > >> > I am working through a performance issue and need some help. I need to >> > find some folks who have flying aircraft with the following combination >> > of >> > features: >> > >> > Flying RV7a or 9a >> > Carburated 180 hp 0360 (Superior/ECI/Lyc) >> > Sam James Cowl/plenum/induction system >> > Fixed pitch propellor >> > >> > The intent is to compare some data and discuss any install challenges >> > you >> > may have had to overcome with this, apparently rare combination. >> > >> > Please respond off list to: >> > >> > hootsnik(at)sbcglobal.net >> > >> > Thanks in advance for the help. >> > >> > Dave >> > >> > >> > >> > >> > >> > >> > >> > >> > >> > >> > >> > >> > >> > >> >> >> >> >> >> >> >> >> >> >> >> >> > > WRT James cowl, is it basically just the differently shaped air inlets and > their inlet areathat make the difference? What's the diameter of the > openings? In other words, if one took Van's cowl and redid the openings > would that theoretically lower drag?? > > Or is there a fundamental difference in the air outlet area on the bottom > too? > > Anyone ever take a side by side photos and otherwise do a meaningful > compare? > > Just curious and looking for rainy day projects.... > -------------- Original message -------------- > From: "dick martin" martin(at)gbonline.com > > -- RV-List message posted by: "dick martin" > > Dave, > I have an RV8 with a James Cowl and plenum and a IO-390 engine. I believe > that it contributes and average speed increase of 10 knots over a standard > Vans cowl. I have over 1300 hours with this set up. I have also talked to > as many others with this set up as possible, and the general consensus is > the same as mine. Also, cooling problems are usually not a problem with > this cowl. > Dick Martin > RV8 N233M > the fast one > ----- Original Message ----- > From: "David Burden" <HOOTSNIK(at)SBCGLOBAL.NET> > To: > Sent: Friday, March 24, 2006 8:42 AM > Subject: RV-List: > Perfor > mance Problem Analysis > > > -- RV-List message posted by: David Burden > > Hello Listers, > > I am working through a performance issue and need some help. I need to > find some folks who have flying aircraft with the following combination > of > features: > > Flying RV7a or 9a > Carburated 180 hp 0360 (Superior/ECI/Lyc) > Sam James Cowl/plenum/induction system > Fixed pitch propellor > > The intent is to compare some data and discuss any install challenges you > may have had to overcome with this, apparently rare combination. > > Please respond off list to: > > hootsnik(at)sbcglobal.net > > Thanks in advance for the help. > > Dave > > > < > BR> > > > hank y > ou for your generous support! > > > ________________________________________________________________________________
From: luckymacy(at)comcast.net (lucky)
Subject: Re: Performance Problem Analysis
Date: Apr 22, 2006
Any engineers out there care to hazard a guess what the percentage of gain is for each of the 3 referenced sources? ie, for the 10 knot gain in using the Sam James setup, 70% from the combo of the smaller area openings and use of a integrated/sealed plenum and 30 percent from exterior cowl shape? If it was the other way around, I wouldn't even consider it a worthwhile project.... -------------- Original message -------------- From: Kevin Horton <khorton01(at)rogers.com> > > On 22 Apr 2006, at 10:41, lucky wrote: > > > > > WRT James cowl, is it basically just the differently shaped air > > inlets and their inlet area that make the difference? What's the > > diameter of the openings? In other words, if one took Van's cowl > > and redid the openings would that theoretically lower drag?? > > > > Or is there a fundamental difference in the air outlet area on the > > bottom too? > > > > Anyone ever take a side by side photos and otherwise do a > > meaningful compare? > > > > Just curious and looking for rainy day projects.... > > > Lucky, > > As I understand it, the performance increase comes from three places: > > 1. The cowl comes with a plenum chamber, which means more of the air > that comes in the inlets actually cools the engine. Baffles leak, so > you need to bring in extra air to allow for that leakage. The fact > that the plenum chamber has less leakage means less air is needed, so > the inlets are smaller. The less air you bring in the inlets, the > less cooling drag there is. > > 2. The contour of the inlet is designed to try to have laminar flow > as the air expands, which results in the least amount of drag, and > the greatest amount of pressure once the air has expanded. > > 3. The inlet shape is round. Round inlets have the smallest > circumference for a given area, so there is less frictional drag > along the walls of the inlet. Any frictional drag results in some > pressure loss in the cooling air, which reduces the cooling > effectiveness, and means you probably need a bit more air to get the > same amount of cooling. This is probably a very minor effect. > > I believe you could achieve most of the performance increase by > having a plenum chamber that has a good seal at the inlet, and > reducing the size of the inlets. Many people add plenum chambers, > but I believe most of them don't have a good seal at the inlet, so > there is quite a bit of leakage there. I also believe that most > people don't reduce the size of the inlets. If you don't reduce the > size of the inlets, you won't realize any performance increase. > > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada > http://www.kilohotel.com/rv8 > > > > > > > > > > > > > Any engineers out there care to hazard a guess what the percentage of gain is for each of the 3 referenced sources? ie, for the 10 knot gain in using the Sam James setup, 70% from the combo of the smaller area openings and use of a integrated/sealed plenum and 30 percent from exterior cowl shape? If it was the other way around, I wouldn't even consider it a worthwhile project.... -------------- Original message -------------- From: Kevin Horton khorton01(at)rogers.com -- RV-List message posted by: Kevin Horton On 22 Apr 2006, at 10:41, lucky wrote: -- RV-List message posted by: luckymacy(at)comcast.net (lucky) WRT James cowl, is it basically just the differently shaped air inlets and their inlet area that make the difference? What's the diameter of the openings? In other words, if one took Van's cowl and redid the openings would that theoretically lower drag?? Or is there a fundamental difference in the air outlet area on the bottom too? Anyone ever take a side by side photos and otherwise do a meaningful compare? &g t;
Just curious and looking for rainy day projects.... Lucky, As I understand it, the performance increase comes from three places: 1. The cowl comes with a plenum chamber, which means more of the air that comes in the inlets actually cools the engine. Baffles leak, so you need to bring in extra air to allow for that leakage. The fact that the plenum chamber has less leakage means less air is needed, so the inlets are smaller. The less air you bring in the inlets, the less cooling drag there is. 2. The contour of the inlet is designed to try to have laminar flow as the air expands, which results in the least amount of drag, and the greatest amount of pressure once the air has expanded. 3. The inlet shape is round. Round inlets have the smallest circumference for a given area, so there is less frictio nal dr ag along the walls of the inlet. Any frictional drag results in some pressure loss in the cooling air, which reduces the cooling effectiveness, and means you probably need a bit more air to get the same amount of cooling. This is probably a very minor effect. I believe you could achieve most of the performance increase by having a plenum chamber that has a good seal at the inlet, and reducing the size of the inlets. Many people add plenum chambers, but I believe most of them don't have a good seal at the inlet, so there is quite a bit of leakage there. I also believe that most people don't reduce the size of the inlets. If you don't reduce the size of the inlets, you won't realize any performance increase. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ===== ================================================= &g t;
________________________________________________________________________________
Subject: Performance Problem Analysis
Date: Apr 22, 2006
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Kevin pretty much hit it on the head. You are looking for a couple of things in a cowl. One is to have easy bends for the inlet and outlet air to pass through so you are not imparting much of the airflow's energy into the airframe (more drag). Also you want the best pressure recovery ratio you can get. Essentially whatever the pressure is of the air entering the cowl you want to try and make it the same number as it exits. Any deviation from 1 to 1 will cause drag and/or cooling problems. You then use the venturi effect to either slow or speed up the airflow inside the cowling to increase or decrease the amount of heat transfer from the engine. These two areas are where the James cowl makes the difference. Michael Sausen -10 #352 Fuselage -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Kevin Horton Sent: Saturday, April 22, 2006 10:57 AM Subject: Re: RV-List: Performance Problem Analysis On 22 Apr 2006, at 10:41, lucky wrote: > > WRT James cowl, is it basically just the differently shaped air inlets > and their inlet area that make the difference? What's the diameter of > the openings? In other words, if one took Van's cowl and redid the > openings would that theoretically lower drag?? > > Or is there a fundamental difference in the air outlet area on the > bottom too? > > Anyone ever take a side by side photos and otherwise do a meaningful > compare? > > Just curious and looking for rainy day projects.... Lucky, As I understand it, the performance increase comes from three places: 1. The cowl comes with a plenum chamber, which means more of the air that comes in the inlets actually cools the engine. Baffles leak, so you need to bring in extra air to allow for that leakage. The fact that the plenum chamber has less leakage means less air is needed, so the inlets are smaller. The less air you bring in the inlets, the less cooling drag there is. 2. The contour of the inlet is designed to try to have laminar flow as the air expands, which results in the least amount of drag, and the greatest amount of pressure once the air has expanded. 3. The inlet shape is round. Round inlets have the smallest circumference for a given area, so there is less frictional drag along the walls of the inlet. Any frictional drag results in some pressure loss in the cooling air, which reduces the cooling effectiveness, and means you probably need a bit more air to get the same amount of cooling. This is probably a very minor effect. I believe you could achieve most of the performance increase by having a plenum chamber that has a good seal at the inlet, and reducing the size of the inlets. Many people add plenum chambers, but I believe most of them don't have a good seal at the inlet, so there is quite a bit of leakage there. I also believe that most people don't reduce the size of the inlets. If you don't reduce the size of the inlets, you won't realize any performance increase. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
Date: Apr 22, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Dan: I talked to my aviation lawyer less than a year ago and my info, John Denver's estate did not sue the builder. It would be ridiculous a multimillionaire (estate) suing a guy with $2 in the bank. Please send your source/ refrence. God rest his soul, Dear John was flying real low on altitude and gas, and had no license after a few DWI's. I think you are wrong. (John Denver flew into the water. The fuel selector was in a non-standard place and was thought that he accidentally flew into the water when reaching for it. However he was very low and was out or almost out of fuel. Lesson learned BUILD YOU RV PER PLANS and DON'T DO WEIRD ONE OFF SYSTEM DESIGNS YOU DREAM UP, at least if you don't want to be suied.) Your case TWO. Again no offense but facts, case number, names, not rumor, hearsay and urban legend. This is what I am talking about. You throw out a scenario that is hard to believe, no offense. I would not be surprised if someone at AOPA made this up. There have been people's estates who sue the pilot or pilot estate for killing the passenger, their family member, but that has NOTHING to do with selling a plane and being sued as the builder or manufacture. (BY THE WAY, waiver and hold harmless waivers work for passengers. Whether the hold up how know it would no hurt. ALSO have a LAWYER write these up. It is worth the few $100 bucks to have it written verses a generic boiler-plate form you found or dreamed up.) If you have examples: Names, places, state, city where the lawsuit is filed I'll look into it. I still stand by NEVER. Your other points and conjecture is correct and interesting. Yes lawsuits are expensive even if you win. However put that into the agreement. The agreement says if you buy and fly this home-built you can DIE, you accept all risk and waive all legal rights to sue, you the builder. If you do get sued from some 3rd party (a passenger) the buyer will pay all your legal fees. That is the way it should be anyway. That would cut down the stupid frivolous lawsuits. As I said these agreements should work but there is no legal precedence, since no builder has been sued for building (that I or my aviation lawyer knows of). It is better than nothing. CAN YOU BE SUED. you bet your sweat rudder you can. However as I said your dog bites someone you can get suied. Build a good plane, don't sell to an idiot, get a waiver drawn up by a Lawyer and allow or insist that the buyers faimly and their lawyer read and approve it. If for some reason you got sued the defense should not break the bank. Slam dunk, the buyer killed them self for say, doing low level acro. Cheers George >From: "Dan Morrow" <DanFM01(at)butter.toast.net> >Subject: Re: RV-List: Re: AOPA hates homebuilts? > >posted by: "Dan Morrow" > >"Never" is a big word. I can think of two lawsuits against builders >just from casual reading of the news in the last few years. >Lawsuit 1: In the John Denver crash, the newspapers reported that >Denver's relatives sued several people including the builder. I don't >know the outcome however. > >Lawsuit 2: This one was somewhat complicated involving several sales >and owners. Step 1: Individual A builds aircraft and flies for several >years. Sells aircraft to individual B. >Step 2: B flies aircraft for several years and then sells aircraft >to individual C. Step 3: C flies aircraft for several years. Then one >day he takes a friend's wife for a ride and performs low level aerobatics >in view of the husband. Crashes killing himself and friend's wife. >Step 4: Husband sues individual A. >Step 5: Individual A sues B. I don't know the outcome of the >lawsuits. --------------------------------- ________________________________________________________________________________
From: <erichweaver(at)cox.net>
Subject: AFP purge valve
Date: Apr 23, 2006
Howdy Thought I would share with the list the folowing question I e-mailed to Airflow Performance and their reply: "I have one of your fuel injection units on my new IO-360 B1B engine and RV-7A aircraft. It would seem prudent to have a spring or other similar device on the purge valve control arm to insure that if the cable controlling the pure valve were to fail, the control arm would remain in the normal run position. Do you agree, and if so, do you offer a product for this purpose? If not, perhaps you have some suggestions for obtaining or fabricating such a device?" Here is the replay that I received: "We typically recommend that the system is installed with good quality cables with rod ends. This should eliminate any need for return springs. I always ask; "Did you put a return spring on the mixture control or throttle?" But of course the choice is yours. If you feel a return spring on the purge valve will give you piece of mind, by all means do it. I have seen some installations use a simple extension spring connected to the purge valve lever to a adel clamp on a push rod tube to pull the lever to the run position." Don Rivera Airflow Performance ________________________________________________________________________________
From: "Jimmy Hill" <jimmy(at)jhill.biz>
Subject: Re: Dakotas
Date: Apr 23, 2006
Jerry: Thanks for the reply re. Black Hills. My son and I returned from Custer Airport yesterday. It is a real pretty area, with a lot to see. Jimmy Stillwater RV8A ----- Original Message ----- From: "Jerry Calvert" <rv6(at)cox.net> Sent: Tuesday, April 18, 2006 10:05 PM Subject: Re: RV-List: Dakotas > > My wife and I are planning a trip to South Dakota in July. Will be > staying > over at Custer County Airport http://www.airnav.com/airport/KCUT which is > southwest of Rapid City. > > Plenty of places to stay, state parks with wild life, Mount Rushmore > nearby, > Black hills country, should be places to camp. Rental cars are available. > > Jerry Calvert > RV 6 N296JC > Edmond Ok > ----- Original Message ----- > From: "Jimmy Hill" <jimmy(at)jhill.biz> > To: "rv-list" > Sent: Tuesday, April 18, 2006 7:07 PM > Subject: RV-List: Dakotas > > >> >> Fellow RV'ers: >> >> My son and I plan a flight in our 8A this weekend from Okla. up to the > Dakotas, and surrounding areas. >> Would appreciate knowing of any RV friendly locations--good sightseeing, > possibly airport camping spots, etc. >> >> Thanks. >> Jimmy >> >> >> >> >> >> >> >> >> >> >> >> >> > > > ________________________________________________________________________________
From: LessDragProd(at)aol.com
Date: Apr 23, 2006
Subject: Re: Blended Airfoil 72" vs. 74"
Hi Jim, I don't have any cruise performance flight test data yet. By my calculation (with some very rough assumptions): The 74" diameter requires 3% more power to turn at cruise than the 72" dia. (Or about a 3 mph reduction in cruise speed.) The 74" diameter could provide a slight increase in initial climb rate. The advantage of the 74" dia. Hartzell propeller would be when the blade tips are damaged. >From what I understand from Hartzell, if the blades can be trimmed and reformed to at least a 72" dia., they are still serviceable. >From what I understand from Hartzell, if the 72" dia. Hartzell blade tips are damaged, the complete propeller is scrap. Regards, Jim Ayers > > Does anyone have any information on pros and cons on choosing a 72" vs. > 74" Hartzell blended airfoil prop? Have searched archives and was unable > to find any specific information relative to propeller diameter. > > Jim Thorne > 7A-QB CHD ________________________________________________________________________________
From: "james frierson" <tn3639(at)hotmail.com>
Subject: Sensenich prop data
Date: Apr 23, 2006
I recently put a new 80 pitch Sensenich propeller on my 160HP RV6A. I made a cross country trip and here are my initial results. At 8500 at approximately 60 degrees F, I was indicating 158 mph, 2530 rpms at WOT and 1680 lbs. After doing the math that wound up being 185 mph TAS and the ground speed according to my GPS was 195 mph which would be about right as there should have been a slight 5-8 knot tail wind component according to Dans web sites wind calculator. After climbing to 9500 the results were still 158 mph indicated, 58deg F, 2500 rpm at WOT which works out to 188 mph TAS, 197 mph GPS ground speed. Again with the expected tail winds this was right on. This is the first time I have been able to fly at WOT and the CHTs and the EGTs were much more uniform. All in all the new prop is doing exactly as advertised. Note: These are not super picky test pilot figures, just what was noted during a flight from a fly-in with my lovely bride taking notes __________________ Scott Frierson N162RV RV6A 160HP ________________________________________________________________________________
From: pcowper(at)webtv.net (Pete Cowper)
Date: Apr 23, 2006
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
A builder of a kit plane becomes a manufacturer of that aircraft. If the builder is found to be negligent in the design or manufacture which causes harm to another, they can be held liable for that victim's damages. A waiver of liability can be prepared and signed by the buyer and spouse, however that is only an agreement between those individuals. The agreement must not be found unconscionable and signed by both parties after an arms-length negotiation with each party having an equal bargaining position. The new owner's minor children who lose their parent cannot legally enter into a contract, nor can a parent enter into a contract on their behalf, therefore the risk remains. The builder's negligent product has taken away the minor children's parental love, support and college tuition payments and someone gets to take over with their checkbook. Likewise, if the negligently designed or manufactured airplane harms someone or property on the ground the waiver between the buyer and seller will not apply to their claims against the negligent builder. The victims will all come after the negligent builder who must then file a lawsuit against the buyer for indemnity and hope the buyer has enough money to pay any judgments rendered against the builder. Lots of up front legal expenses even with an an attorney's fee provision. A few years ago AVEMCO announced that they were offering continuing products liability for up to three years after sale for insured builders who had been covered by an AVEMCO policy the previous three years. Each year of insurance extended the after sale coverage for one year up to a maximum of three years coverage after sale. This was a wonderful program for we homebuilders who decided to sell our aircraft. Regardless of the builder's ultimate liability or lack thereof, AVEMCO is paying for an attorney to defend the builder. AVEMCO's policy was the only economical products liability coverage available . . . without getting in line with Detroit automakers, passenger jet aircraft manufactures, cigarette manufacturers, makers of Vioxx, etc. to try to purchase a major manufacturer's product liability policy for your one single manufactured product. Hopefully after three years the new owner would learn to fly it safely or as a true EAA member make enough changes that none of your original work remains untampered with. John Denver's estate went after the manufacturer of the fuel valve that failed leaving about 45 minutes of fuel in the tank the valve had been switched to when the plane was pulled from the water. In expert testimony it became apparent that the manufacturer knew of the corrosion problem and failed to issue proper lubricants specifications for periodic maintenance. Hundreds of the valves had failed from the same problem that caused John Denver's to corrode. The maker of the fuel valve was forced to finally issue proper lubrication maintenance guidelines to prevent the continuing problem as part of the settlement. The fuel valve had been mounted on the bulkhead over the pilot's shoulder by the builder as a safety modification to eliminate having fuel lines running in the front near the pilot's feet and crotch in the plastic rear-engined aircraft. John Denver was observed switching the tank valve by a line person at the Monterey airport when he started his plane to takeoff to do some touch and go practices. With the larger engine on his particular aircraft he intentionally did not want full tanks for practice flights remaining within the local pattern. Please get the facts before throwing the term "frivolous litigation" around. Pete Cowper RV8 #81139 ________________________________________________________________________________
Date: Apr 23, 2006
From: Paul Trotter <ptrotter(at)acm.org>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Pete, Do you think that there is any advantage from a liability perspective to define the manufacturer of a homebuilt as a corporate entity of some kind, such as an LLC? Theoretically the purpose of an LLC is to limit the liability of the stockholders, although I don't know how it actually works out in reality, if a lawsuit were to occur. Paul ----- Original Message ----- From: "Pete Cowper" <pcowper(at)webtv.net> Sent: Sunday, April 23, 2006 6:21 PM Subject: RV-List: Re: Lawsuits against builders (Was AOPA hates homebuilts?) > > A builder of a kit plane becomes a manufacturer of that aircraft. If the > builder is found to be negligent in the design or manufacture which > causes harm to another, they can be held liable for that victim's > damages. > > ........... ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Date: Apr 23, 2006
Good idea, but you can't. You no longer can even define the "mfgr" as multiple people like you used to. Has to be a single person now. Cheers, Stein. -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Paul Trotter Sent: Sunday, April 23, 2006 5:54 PM Subject: Re: RV-List: Re: Lawsuits against builders (Was AOPA hates homebuilts?) Pete, Do you think that there is any advantage from a liability perspective to define the manufacturer of a homebuilt as a corporate entity of some kind, such as an LLC? Theoretically the purpose of an LLC is to limit the liability of the stockholders, although I don't know how it actually works out in reality, if a lawsuit were to occur. Paul ----- Original Message ----- From: "Pete Cowper" <pcowper(at)webtv.net> Sent: Sunday, April 23, 2006 6:21 PM Subject: RV-List: Re: Lawsuits against builders (Was AOPA hates homebuilts?) > > A builder of a kit plane becomes a manufacturer of that aircraft. If the > builder is found to be negligent in the design or manufacture which > causes harm to another, they can be held liable for that victim's > damages. > > ........... ________________________________________________________________________________
Date: Apr 23, 2006
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
On 15:21:44 2006-04-23 pcowper(at)webtv.net (Pete Cowper) wrote: > A builder of a kit plane becomes a manufacturer of that aircraft. If > the builder is found to be negligent in the design or manufacture > which causes harm to another, they can be held liable for that > victim's damages. > [stuff deleted] > > Please get the facts before throwing the term "frivolous litigation" > around. That's all well and good, but it doesn't do anything to contradict the claim in the previous post, which was that no builders, themselves, had ever been sued. Manufacturers of parts, yes. But no builders. I'm not saying that the claim was valid, just that it hasn't been done yet. Or does someone have some citations of cases where it's happened? -Rob ________________________________________________________________________________
Date: Apr 24, 2006
From: "Phil Sisson, Litchfield Aerobatic Club" <sisson(at)consolidated.net>
Subject: Re: Sensenich prop data
james frierson wrote: > >I recently put a new 80 pitch Sensenich propeller on my 160HP RV6A. I made >a cross country trip and here are my initial results. At 8500 at >approximately 60 degrees F, I was indicating 158 mph, 2530 rpms at WOT and >1680 lbs. After doing the math that wound up being 185 mph TAS and the >ground speed according to my GPS was 195 mph which would be about right as >there should have been a slight 5-8 knot tail wind component according to >Dans web sites wind calculator. After climbing to 9500 the results were >still 158 mph indicated, 58deg F, 2500 rpm at WOT which works out to 188 mph >TAS, 197 mph GPS ground speed. Again with the expected tail winds this was >right on. This is the first time I have been able to fly at WOT and the CHTs >and the EGTs were much more uniform. >All in all the new prop is doing exactly as advertised. Note: These are not >super picky test pilot figures, just what was noted during a flight from a >fly-in with my lovely bride taking notes >__________________ >Scott Frierson >N162RV >RV6A 160HP > > > > > sounds pretty good.......... Phil ________________________________________________________________________________
From: "Mark & Lisa" <marknlisa(at)hometel.com>
Subject: Builder's Liability
Date: Apr 24, 2006
Guys, guys, guys, It's not about providing for the orphaned children. Most lawyers could care less about the orphans; SHOW ME THE MONEY! You may find a lawyer that cares about the orphans, but they gotta earn a living too. Here's how it works (usually). A poor, destitute, (hopefully) taken-advantage of individual is injured or killed while using a defective product foisted on an unsuspecting public by a big, fat juicy manufacturer -- with mucho dinero and product liability insurance. The altruistic lawyer comes to the rescue offering to "help" the poor, destitute plaintiff(s) by taking the case without a retainer (usually because the plaintiff has no money); they'll only take a third (sometimes even more) of any court awarded damages or pre-trial settlement. Our altruistic friend has researched the situation and knows the evil manufacturer has cash, otherwise why waste the time? Now let's consider the case of the "manufacturer" of an experimental aircraft. A lawyer must be willing to bring a product liability suit against an individual with no real liquid assets (you spent all your money on your kitplane, right!?!) and (probably) no product liability insurance. Assuming the plaintiff wins, a big assumption considering the plaintiff was injured or killed flying an EXPERIMENTAL aircraft built in someone's garage (do ya think they assumed some risk?), the plaintiff still has to collect a judgement. If the jury awards my house, plane and cars -- my only real assets -- the plaintiff has to hassle with selling them. If they're in a hurry then those items won't sell at market value. And after all that hassle, they only get a third of the total proceeds -- a few year's work for maybe 30 or 40 grand (for the lawyer). No matter how much the lawyer cares about the orphans, they're not gonna take a case like this. A lawyer stupid enough to take a case like this won't make much of a legal attack. I'll even suggest that if you carry a tail (liability insurance held beyond ownership) you are MORE likely to get slapped with a suit since you (or your insurance company) have MONEY! On the other hand, if you've got millions in the bank, you might just consider buying a plane instead of building one. Come to think of, that's what I'd do! Regards, Mark & Lisa Sletten Legacy FG N828LM http://www.legacyfgbuilder.com ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: McCauley Governor Repair
Date: Apr 24, 2006
I'd like to hear about price or quality experiences from people who have had a governor repaired. My new McCauley governor is seeping oil out the back so I guess it needs new seals/gaskets and I need to find a good shop to do this work as I am advised one can't do it without special tools. Letting it sit for 5 years before using it probably wasn't real good for it. Dave Reel - RV8A ________________________________________________________________________________
Subject: stuff for sale
Date: Apr 24, 2006
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
> Guys, > I apologize for the spam to those who aren't interested in this type > of thing. > There was an auction last Saturday in Vincennes, IN and in a moment of > weakness... I bought a Piper Tomahawk. Complete, no damage... minus > the engine and prop and a few instruments. > I plan to part it out. Please let me know if you know anyone who wants > a wing, tail, small parts, fuselage.... or the whole darn thing. > Geez..... a Tomahawk..... what will my friends say? > I also bought a boatload of other stuff including (4) Beech 18 > rudders, a Beech 18 elevator, a Champ rudder, Stinson 108 aileron, > misc. steel tubing rudders (Cub type.. not sure exactly what planes > they came from), 7 Cessna wings, an Ercoupe wing, Cessna 150 lift > struts, Stinson 108 leading edge wingtip metal. All of this stuff > appears in useable condition, not new, and with the usual storage > scuffs and scrapes. Some stuff is in perfect shape... some not so > good. You'd have to be the judge. > I also picked up old Piper cowl sides with the Piper emblems, Cessna > 150 center console plastic covers and sun visors, a couple doors that > look like old Piper or T-craft, an elevator from a Rockwell Commander, > a couple Piper type hor. stab. pieces, a couple props.. unairworthy > decorative types,10 Simpson voltmeters, several instrument panels with > instrument cutouts, lots more, etc.... all this stuff is for sale. > Email me OFFLIST if interested in any of this stuff. It will all go > to Ebay if nobody is interested. > Thanks, > Vince Frazier > 3965 Caborn Road > Mount Vernon, IN 47620 > 812-464-1839 work > 812-985-7309 home > F-1H Rocket, N540VF > http://vincesrocket.com/ > > ________________________________________________________________________________
From: "Richard Suffoletto" <suffy(at)starstream.net>
Subject: Wing tip paint prep
Date: Apr 24, 2006
The wing tips on my 7A came with some minor gel coat voids in the area of the cut out for position lights. Other than that the gel coat is in good shape. Is there something I should be doing to prep them for paint other than roughing them up ? -- ________________________________________________________________________________
Date: Apr 24, 2006
From: "Tim Bryan" <flyrv6(at)bryantechnology.com>
Subject: Re: Builder's Liability
I have known of cases where the lawyer took the case because of friendship. But, the best protection if for you personally NOT to own anything of value. Your assests could be in a trust of other protected entity. Don't loose control, just ownership. You could sue me if you want, but I don't own a darn thing. The cost to defend a lawsuit could in itself be more than one can afford to loose. Prevent it! Tim -------Original Message------- From: Mark & Lisa Date: 04/24/06 06:46:23 Subject: RV-List: Builder's Liability Guys, guys, guys, It's not about providing for the orphaned children. Most lawyers could care less about the orphans; SHOW ME THE MONEY! You may find a lawyer that cares about the orphans, but they gotta earn a living too. Here's how it works (usually). A poor, destitute, (hopefully) taken-advantage of individual is injured or killed while using a defective product foisted on an unsuspecting public by a big, fat juicy manufacturer -- with mucho dinero and product liability insurance. The altruistic lawyer comes to the rescue offering to "help" the poor, destitute plaintiff(s) by taking the case without a retainer (usually because the plaintiff has no money); they'll only take a third (sometimes even more) of any court awarded damages or pre-trial settlement. Our altruistic friend has researched the situation and knows the evil manufacturer has cash, otherwise why waste the time? Now let's consider the case of the "manufacturer" of an experimental aircraft. A lawyer must be willing to bring a product liability suit against an individual with no real liquid assets (you spent all your money on your kitplane, right!?!) and (probably) no product liability insurance Assuming the plaintiff wins, a big assumption considering the plaintiff was injured or killed flying an EXPERIMENTAL aircraft built in someone's garage (do ya think they assumed some risk?), the plaintiff still has to collect a judgement. If the jury awards my house, plane and cars -- my only real assets -- the plaintiff has to hassle with selling them. If they're in a hurry then those items won't sell at market value. And after all that hassle, they only get a third of the total proceeds -- a few year's work for maybe 30 or 40 grand (for the lawyer). No matter how much the lawyer cares about the orphans, they're not gonna take a case like this. A lawyer stupid enough to take a case like this won't make much of a legal attack. I'll even suggest that if you carry a tail (liability insurance held beyond ownership) you are MORE likely to get slapped with a suit since you (or your insurance company) have MONEY! On the other hand, if you've got millions in the bank, you might just consider buying a plane instead of building one. Come to think of, that's what I'd do! Regards, Mark & Lisa Sletten Legacy FG N828LM http://www.legacyfgbuilder.com ________________________________________________________________________________
Subject: Oshkosh (Airventure) camping
From: "Bob Collins" <bcollinsrv7a(at)comcast.net>
Date: Apr 24, 2006
Darwin Barrie and I have been working on setting up an area in Camp Scholler for RVers of all stripes to camp. We're at the point where we need to know how many people -- if anyone -- would be interested in having us reserve spots starting on Friday July 21. If you're interested, more information is available here (http://home.comcast.net/~bcollinsrv7a/eaa/index.htm), but we'll probably need to make a firm decision within the next 3 weeks. Also, we're still looking for a few volunteers to help out with the RV Family Reunion BBQ on Wednesday July 26th. Information is available at: . And in the next month or so, we'll start take a head count to see if there's enough interest to pull it off. One more, unrelated thing, in Hotline this week, there was a survey that I'm conducting to try to get a general picture of the insurance situation for RVers. If you're interested, there's a blue box on the right side of the Hotline. Please fill out the form. Everything's confidential and all that. Bob Collins St. Paul -------- Bob Collins St. Paul, Minn. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=30348#30348 ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Builder's Liability
Date: Apr 24, 2006
Yep, it's called 'judgment proofing' yourself. Ironically, a lot of lawyers use this to protect themselves from judgments. If you live in a non-community property state, it can be as simple as putting all your assets except your airplane in your wife's name. Of course, you REALLY have to trust your wife. Bruce www.glasair.org -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Tim Bryan Sent: Monday, April 24, 2006 11:14 AM Subject: Re: RV-List: Builder's Liability I have known of cases where the lawyer took the case because of friendship. But, the best protection if for you personally NOT to own anything of value. Your assests could be in a trust of other protected entity. Don't loose control, just ownership. You could sue me if you want, but I don't own a darn thing. The cost to defend a lawsuit could in itself be more than one can afford to loose. Prevent it! Tim ________________________________________________________________________________
Date: Apr 24, 2006
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: Builder's Liability
On 9:14:27 2006-04-24 UFOBUCK(at)aol.com wrote: >> In a message dated 04/24/2006 10:54:48 A.M. Central Daylight Time, >> Bruce(at)glasair.org writes: >> >> If you live in a >> non-community property state, it can be as simple as putting all >> your assets except your airplane in your wife's name. > > What happens if your wife gets sued ?? Nothing. She doesn't own the plane, she didn't build the plane, and she wasn't (presumably) flying the plane. She's an unrelated third party. Hence the "non-community property" statement above. I believe Canada falls into this category. -Rob ________________________________________________________________________________
Date: Apr 24, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
>posted by: pcowper(at)webtv.net (Pete Cowper) > >A builder of a kit plane becomes a manufacturer of >that aircraft. If the builder is found to be >negligent in the design or manufacture which causes >harm to another, they can be held liable for that >victim's damages. FIRST KIT PLANE BUILDERS DONT DESIGN THEIR PLANE. We all know that as the builder we are the SO CALLED manufacture, SO what. However its not a product held out by a company for the general public in mass. No one is arguing there is liability, but it has to be related to the building of the aircraft. There is NO legal precedence of a builder being sued or loosing a product liability case TO DATE. (deal with facts please.) >A waiver of liability can be prepared and signed by >the buyer and spouse, however that is only an >agreement between those individuals. The agreement >must not be found unconscionable and signed by both >parties after an arms-length negotiation with each >party having an equal bargaining position. Are you a lawyer or legal expert. As I mentioned on a previous post hold harmless agreements should work, but then no one has needed to prove it in a law suits against a BUILDER, since there has been ZERO to date. >The new owner's minor children who lose their parent >cannot legally enter into a contract, nor can a >parent enter into a contract on their behalf, >therefore the risk remains. The builder's negligent >product has taken away the minor children's parental >love, support and college tuition payments and >someone gets to take over with their checkbook. You are getting into the minutia of legalities and WHAT IFS. My dog can sue you but he is not going to win. Your FICTITIOUS scenarios prove nothing but you have an imagination. Fiction does not make law, legal precedence does. THE adult parent in your scenario assumes all responsibility flying a homebuilt amateur built plane the DOES NOT MEET Federal regulations. If anyone is going to get sued it is the CHILD and his parents estate for being an idiot and killing himself and who ever else they killed or damaged. I have a question, ARE YOU A Liberal? Do you think gun and ammo makers should be sued when someone gets shot? You are the kind of person I would NOT want to sell my plane to, someone who looks to blame and not take responsibility for their actions and choices. >Likewise, if the negligently designed or manufactured >airplane harms someone or property on the ground the >waiver between the buyer and seller will not apply to >their claims against the negligent builder. Again SO WHAT. You are a chicken little sky falling kind of guy and worry way to much. I mean that is cool and works for you, however life has risks and liabilities. I am surprised you fly at all. Flying little planes is VERY risky. You can crash into an elementary school. You are going to get an ulcer. If a guy flies into a house with an amateur built plane you or I built and sold because of HIS stupidity, than OUR liability is nil, small. If sued the defense should be straight forward. AGAIN THERE IS NO Legal Precedence. THAT COUNTS A LOT. If you are going to give case history or examples give real ones not made up scenarios that have no REAL meaning. >The victims will all come after the negligent builder >who must then file a lawsuit against the buyer for >indemnity and hope the buyer has enough money to pay >any judgments rendered against the builder. Lots of >up front legal expenses even with an attorney's fee >provision. LOOK you keep saying the victims WILL all come after the negligent builder. WHY IS THE BUILDER NEGLIGENT? YOU MAKE ASSUMPTIONS, Like WILL come after. Chance is they will NOT sue at all. Why not sue the kit manufacture of the plane parts? How about Lycoming? Hartzell? I mean the list is long and your point is full of conjecture, assumptions and over wrought paranoia. Again your statements are sensational and emotional from your overactive paranoid mind. Go on FACTS and REAL risk, not what you can dream up can happen. S#@t happens. All you can do is protect yourself with documentation and agreements. TO be clear however, if you build and sell a plane and don't put the bolts in the rear spar you should get sued, bankrupted and thrown in jail. >A few years ago AVEMCO announced that they were >offering continuing products liability for up to three >years after sale for insured builders who had been >covered by an AVEMCO policy the previous three years. >Each year of insurance extended the after sale >coverage for one year up to a maximum of three years >coverage after sale. This was a wonderful >Program for we homebuilders who decided to sell our >aircraft. Regardless of the builder's ultimate >liability or lack thereof, AVEMCO is paying for an >attorney to defend the builder. WOW good old AVEMCO wants to take your money. Gee what great guys. Look they OFFER IT because they know the liability is low and they can defend against it easily. They dont offer it out of the goodness of their heart. THEY ARE MAKING MONEY, Bottom line. AVEMCO is all about MAKING MONEY. That is why AVEMCO, for all intensive purposes has priced homebuilts out of the (their) insurance market. They have dropped first flight and under construction insurance for most people. There premium of course is the highest and they will viciously sue YOU, their customer to NOT pay if they smell any breach in the conditions of the insurance. WOW gee what great guys. >AVEMCO's policy was the only economical products >liability coverage available . . . without getting >in line with Detroit automakers, passenger jet >aircraft manufactures, cigarette manufacturers, >makers of Vioxx, etc. to try to purchase a major >manufacturer's product liability policy for your one >single manufactured product. Hopefully after three >years the new owner would learn to fly it safely or >as a true EAA member make enough changes that none >of your original work remains untampered with. First of all jet manufactures like Boeing dont have product liability insurance. They defend themselves vigorously in court (and usually win) and are self covered if you will. Now you are just stretching and rambling about Vioxx. KEEP IT SIMPLE. Homebuilt plane, well built, per planes, with a PLACARD THIS IS A Amateur built plane and may not MEET federal standards. If you sell your plane, KEEP DETAILED records, pictures, logs and so on. AGAIN there is SOME liability but its not likely the worst case scenarios you dream up will happen. Also despite the cost of defending yourself, it is a long shot they will win. Look if you want to scrap your RV-8 when you loose your medical (soon with your blood pressure) that's your business. >John Denver's estate went after the manufacturer of >the FUEL VALVE that failed leaving about 45 minutes >of fuel in the tank the valve had been switched to >when the plane was pulled from the water. In expert >testimony it became apparent that the manufacturer >knew of the corrosion problem and failed to issue >proper lubricants specifications for periodic >maintenance. Hundreds of the valves had failed from >the same problem that caused John Denver's to >corrode. The maker of the fuel valve was forced to >finally issue proper lubrication maintenance >guidelines to prevent the continuing problem as part >of the settlement. SO? They sued the valve maker NOT the builder. They not only sued the valve maker Gould Electronics Inc., they sued Aircraft Spruce & Specialty Co. who sold it. I stand by my previous statement NO **BUILDER** HAS BEEN SUED TO DATE THAT I OR MY LAWYER KNOW OF. >The fuel valve had been mounted on the bulkhead over >the pilot's shoulder by the builder as a safety >modification to eliminate having fuel lines running >in the front near the pilot's feet and crotch in the >plastic rear-engined aircraft. SO WHAT, What is your POINT? >John Denver was observed switching the tank valve by >a line person at the Monterey airport when he started >his plane to takeoff to do some touch and go >practices. With the larger engine on his particular >aircraft he intentionally did not want full tanks for >practice flights remaining within the local pattern. Again SO WHAT? What is your point? AGAIN THE BUILDER DID NOT GET SUED! (Even though he did a weird thing.) You state the KNOWN facts of the accident as if you are going some where with it. SO WHAT! HE KILLED HIMSELF. >Please get the facts before throwing the term >"frivolous litigation" around. YOU HAVE NO FACTS. Everything I stated is correct. There has NEVER been any lawsuits TO DATE against a builder. Get YOUR facts straight. Also please have a beer or calm down before writing. You are scaring people for no reason. I hope you dont act like this in the cockpit if you have an emergency. I think you are going to have a massive heart attack and sue me. You make ZERO points, made up a few fictitious examples you dreamed up and prove nothing. AGAIN LEAGAL precedence against BUILDERS is (zero) so that your REAL liability risk is SMALL. Lawyers and judges go by previous case history and precedence. That does not mean your exposure is ZERO. I does NOT mean you cant be sued, but it does mean that the chance is small, and there are things to limit your exposure and help defend yourself if the worse happens, as I suggested. HOWEVER I am not going to give legal advice, because I dont want to be sued for giving out advice. My advice is get a lawyer when you sell your plane. When I sell my plane I will have independant inspections, agreements written up. I will put a placard across the panel saying USE AT YOUR OWN RISK (documented in the agreement, log book and photos). Of course they will take it off but that is not my problem since its documented in the agreement it will not be removed (like pillow tags). I will make log book entries, have excellent documentation. Could I still get sued, sure, but for what? Bad design? I did not design it. The case will be thrown out with my evidence. >Pete Cowper >RV8 #81139 Pete I suggest you never sell your plane I dont think your heart will take it. :-) lol. Take care and fly safe. We agree to disagree. Please stop making stuff up like it has happened. It than gets spread around that it did, than there is an issue where none exist. All the liability issue is trumped up but AOPA or Cessna because they want people the buy a $200,000 C172 that has the performance of a C-172. They would love to spread this urban legend. HOMEBUILTS RULE! George RV-7 --------------------------------- ________________________________________________________________________________
Date: Apr 24, 2006
From: chaztuna(at)adelphia.net
Subject: Nose Wheel Questions
Listers, I recently aquired a spare set of Cleveland 5:00 X 5" main wheels. I recently spoke to the owner of Matco Engineering, the current supplier of Vans Nose wheel. I asked him what differed between the product listed for our nose wheel and his standard 5:00 X 5" wheel offering. He stated that the only difference was the location of the hole in the wheel for the inner tube. It seems that the Lamb tire and tube supplied by Vans locates the exit of the valve stem in a different location, as compared to the main tires. I have three questions #1 When did Vans switch from Cleveland to Matco for the nose wheel? #2 Is there any weight difference between the Magnesium Cleveland wheel and the aluminum Matco wheel? #2a Has anyone used a 5:00 X 5" tire on their nose wheel? #2b Did this require modification of the fork or wheel pant? Charlie Kuss ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: McCauley Governor Repair
Date: Apr 24, 2006
Try John at SouthWest Aero (Seattle, WA, 206-575-8732). He was helpful a couple years ago when I got a Woodward governor from him. - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: DAVID REEL [mailto:dreel(at)cox.net] > Sent: Monday, April 24, 2006 10:05 AM > To: rvlist > Subject: RV-List: McCauley Governor Repair > > > I'd like to hear about price or quality experiences from > people who have had a governor repaired. My new McCauley > governor is seeping oil out the back so I guess it needs new > seals/gaskets and I need to find a good shop to do this work > as I am advised one can't do it without special tools. > Letting it sit for 5 years before using it probably wasn't > real good for it. > > Dave Reel - RV8A ________________________________________________________________________________
From: "Steve & Denise" <sjhdcl(at)kingston.net>
Subject: Re: MT Props delay
Date: Apr 23, 2006
Aerocomposites quotes a 20 week delivery. I have only seen 1 performance comparison between MT, Aerocomposites, and Hartzel. All props were within 6 mph top speed of each other. I have ordered the MT anyways despite the 16 week wait. Steve RV7A > Steve, > Suggest you consider a Aero Composites carbon fiber prop. It we be on > average 10 knots faster, same weight, has lightning protection, is > considerably stronger etc. ad infinitum. Also more expensive, but worth it. > Delivery is usually 70 to 90 days. > Dick Martin > RV8 N233M > the fast one ________________________________________________________________________________
From: "Denny M. Dennison" <Denny(at)DennisonSoftware.com>
Subject: RV-8 Tail Kit For Sale --- Save 25%
Date: Apr 24, 2006
Complete, unassembled RV-8/8A empennage kit with plans and assembly manual from Van's Aircraft. Electric Elevator Trim. Van's price is $1775.00 for the same items. My price $1331. Located near Yosemite, California. Call (209) 878-0810. Pictures at http://www.dennisonmountain.com/pages/2/index.htm Regards, Denny ________________________________________________________________________________
From: RVer273sb(at)aol.com
Date: Apr 24, 2006
Subject: (no subject)
Listers, I have a never been touched RV-8 tail kit for sale. Complete with electric elevator trim kit. Will sell for $1300 plus freight costs. Located in Denver Colorado. Stewart Bergner ________________________________________________________________________________
Subject: Re: MT Props delay
From: "N395V" <n395v(at)hughes.net>
Date: Apr 24, 2006
Is there a delay or is it just a quoted long lead time. From the above post it looks like the MT will arrive 1 month sooner than the aerocomposite. -------- Milt N395V F1 Rocket Read this topic online here: http://forums.matronics.com/viewtopic.php?p=30434#30434 ________________________________________________________________________________
Subject: RV-6A Tail Tie Down
From: "Paul Richardson" <prichar(at)mail.win.org>
Date: Apr 24, 2006
One of my fellow aviators was taking off from a grass strip in our RV-6A when the tail tie down contacted a clump of grass and was bent backward, cracking the bottom rudder fairing. Anyone experience that, and do you have any good or bad news as far as expected damage? Specifically, I'm wonder about how much is really bent back where you can't see anything. He said there were no flight problems. He didn't know it happened until postflight cleaning. -------- Paul Richardson RV-6A 106RV Read this topic online here: http://forums.matronics.com/viewtopic.php?p=30440#30440 ________________________________________________________________________________
From: "czechsix(at)juno.com" <czechsix(at)juno.com>
Date: Apr 25, 2006
Subject: Datapoint for Fairings Speed Improvement
Guys, I know others have commented on how much speed an RV picks up when fairings are installed. Just for kicks though I took some data in my RV-8A without any fairings and then again with wheel pants, gear leg and intersection fairings installed. My data was taken with four-way GPS runs using one of the calculators on Kevin Horton's website (the advantage of the four-way run vs. three-way is that the spreadsheet gives you a sanity check to show how good/bad your data is). Anyway, at 4000' density altitude, power set to 24 squared and mixture 50 ROP, I saw an 18 kt gain in TAS when when fairings were put on. I would imagine that the speed increase would be less in a taildragger since there are only two big gear legs/wheels to clean up. I wish now I'd taken some numbers at full power and lower altitude...I bet the speed increase would have been at least 20 kts. Even so I've told several of my spam-can buddies and they can't believe that fairings would make that much difference. Cool! --Mark Navratil Cedar Rapids, Iowa RV-8A N2D with O-360-A1A and blended Hartzell Flying 29.2 hours now.... Guys, I know others have commented on how much speed an RV picks up when fairings are installed. Just for kicks though I took some data in my RV-8A without any fairings and then again with wheel pants, gear leg and intersection fairings installed. My data was taken with four-way GPS runs using one of the calculators on Kevin Horton's website (the advantage of the four-way run vs. three-way is that the spreadsheet gives you a sanity check to show how good/bad your data is). Anyway, at 4000' density altitude, power set to 24 squared and mixture 50 ROP, I saw an 18 kt gain in TAS when when fairings were put on. I would imagine that the speed increase would be less in a taildragger since there are only two big gear legs/wheels to clean up. I wish now I'd taken some numbers at full power and lower altitude...I bet the speed increase would have been at least 20 kts. Even so I've told several of my spam-can buddies and they can't believe that fairings would make that much difference. Cool! --Mark Navratil Cedar Rapids, Iowa RV-8A N2D with O-360-A1A and blended Hartzell Flying 29.2 hours now.... ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: MT Props delay
Date: Apr 24, 2006
Milt, Aero Composites will usually quote a longer lead time because most customers are happier when the prop is available sooner than expected, rather than later. Dick Martin RV8 N233M the fast one Ps: I now have over 300 hours on my RV8, IO390 and Aero Composite 74" Propeller. It is lighter and faster than my Hartzell ----- Original Message ----- From: "N395V" <n395v(at)hughes.net> Sent: Monday, April 24, 2006 7:16 PM Subject: RV-List: Re: MT Props delay > > Is there a delay or is it just a quoted long lead time. From the above > post it looks like the MT will arrive 1 month sooner than the > aerocomposite. > > -------- > Milt > N395V > F1 Rocket > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=30434#30434 > > > ________________________________________________________________________________
From: "czechsix(at)juno.com" <czechsix(at)juno.com>
Date: Apr 25, 2006
Subject: Vx, Vy, Best Glide for O-360/Hartzell
Guys, I'm getting ready to do performance testing for Vx, Vy, and best glide speeds in my RV-8A with O-360/Hartzell setup. I know there are some POH's floating around out there with these numbers in them but I'm curious how many people have measured this data carefully themselves? In particular to get good glide data one would have to pull the mixture and ideally test with the prop stopped, prop rotating with oil pressure & lever aft, and prop rotating without oil pressure (fine pitch). This could take quite a few engine-off glide tests and the numbers should be pretty close from one RV to the next... Which brings me to my point: if there's any "consensus" on these speeds amongst those of you who've taken good data it would be nice to have those numbers as a starting point for my testing. For example if Vy is typically 80-90 kts I would narrow the range of my test from 75 to 95 instead of a much broader span of numbers. It would be cool if someone made a spreadsheet collecting this kind of data from different airplanes. Checkoway are you listening? Thanks, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D flying 29.2 hours now... Guys, I'm getting ready to do performance testing for Vx, Vy, and best glide speeds in my RV-8A with O-360/Hartzell setup. I know there are some POH's floating around out there with these numbers in them but I'm curious how many people have measured this data carefully themselves? In particular to get good glide data one would have to pull the mixture and ideally test with the prop stopped, prop rotating with oil pressure lever aft, and prop rotating without oil pressure (fine pitch). This could take quite a few engine-off glide tests and the numbers should be pretty close from one RV to the next... Which brings me to my point: if there's any "consensus" on these speeds amongst those of you who've taken good data it would be nice to have those numbers as a starting point for my testing. For example if Vy is typically 80-90 kts I would narrow the range of my test from 75 to 95 instead of a much broader span of numbers. It would be cool if someone made a spreadsheet collecting this kind of data from different airplanes. Checkoway are you listening? Thanks, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D flying 29.2 hours now... ________________________________________________________________________________
From: "c.ennis" <c.ennis(at)insightbb.com>
Subject: Re: RV-6A Tail Tie Down
Date: Apr 24, 2006
Paul, Shortly after my first few flights, while I was still trying to land my 6A like a Cessna, I bent the tie down ring in the same way...grass strip, drop on from 2 feet trying to flare. Anyway, I took the tiedown ring off and straightened it, checked the rear bulkhead for damage,(found none) and built a 2" diameter cupped recess into the rudder fairing for clearance for when it happened again. When it happened again, I was pondering the newly bent ring and fresh cracks in the fairing when an IA who I have trusted with my life on more than one occasion, commented that it was entirely possible that the next time it could cause rudder travel problems when I needed it the most. I worked at fabricating some sort of skid/guard to protect the tiedown ring but finally removed it altogether. I have since learned to land without abusing my gear and have not missed the tie down ring. The stainless weldment which was on my 6A bent above the ring stem...saving the bulkhead. Foolishly, I reinforced it before it was reinstalled. The second time it bent in the same place in spite of the reinforcement, still no bulkhead damage. Van designs them hell bent for stout. I am sure one could come up with a ring and mount which would tear the tail off before it bent...but I would rather spare the tail and lose the ring, and I don't have to worry about the ring jambing the rudder if I slam it during takeoff. Charlie Ennis ________________________________________________________________________________
From: Denis Walsh <denis.walsh(at)comcast.net>
Subject: Re: RV-6A Tail Tie Down
Date: Apr 24, 2006
Can't speak for the later models and or the removable ones; however the old original tail tie down was welded to mild steel and would usually bend without causing any damage to the bulkhead on such strikes. Simply remove three bolts, pound it straight, and re install. If it were jamming the rudder, it could be realigned by lying behind plane and using foot to shove it forward. This to get it home to do above precision fix. Voice of experience. Denis Walsh On Apr 24, 2006, at 6:35 PM, Paul Richardson wrote: > > > One of my fellow aviators was taking off from a grass strip in our > RV-6A when the tail tie down contacted a clump of grass and was > bent backward, cracking the bottom rudder fairing. Anyone > experience that, and do you have any good or bad news as far as > expected damage? Specifically, I'm wonder about how much is really > bent back where you can't see anything. He said there were no > flight problems. He didn't know it happened until postflight cleaning. > > -------- > Paul Richardson > RV-6A 106RV > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=30440#30440 > > ________________________________________________________________________________
From: "Steve Glasgow" <willfly(at)carolina.rr.com>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Date: Apr 25, 2006
Just because something has never happened before doesn't mean that it can't happen tomorrow. Witness 9/11. Steve Glasgow ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: RV-6A Tail Tie Down
Date: Apr 25, 2006
Hi Paul, I made a spectacularly hard landing (cause was failure to fully check out the effect of a propeller change on my rate of descent - it turned out it was considerable {:>)) in my RV-6A. It was HARD and I ended up having to eventually replace both main gear rods). When the bottom unexpectedly fell out, I did managed to yank the stick back just before impact getting the nose gear elevated to avoid tucking it under the belly. As a result, the tail tie down and bottom rudder fairing contacted the runway. The tie-down was bent back into the fiberglass rudder fairing, the fairing was abraded where it contacted the runway. On initial inspection that appeared to be the extent of the damage. After getting the aircraft into the hangar and upon further inspection I discovered that the rudder was slightly harder to turn than normal (even after removing the bent tie down from its embedded position in the rudder fairing). Upon closer examination, it was clear that the bearing races for the rudder hinge fittings had been distorted by the impact. The hinge fitting attached to the vertical stab being of thin 4130 had apparently flexed under the landing impact but the stiffer end rod fittings attached to rudder had not. As a result the bearing races had been distorted. The hinge bolts were now rotating rather than staying fixed I had to replace all three rudder hinge fittings. Given that this happened to your friend on a grass strip, the impact was undoubtedly less severe than mine - but have him check the rudder hinge bolts to make certain they are not rotating when the rudder is moved. Ed Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC eanderson(at)carolina.rr.com ----- Original Message ----- From: "Paul Richardson" <prichar(at)mail.win.org> Sent: Monday, April 24, 2006 8:35 PM Subject: RV-List: RV-6A Tail Tie Down > > One of my fellow aviators was taking off from a grass strip in our RV-6A > when the tail tie down contacted a clump of grass and was bent backward, > cracking the bottom rudder fairing. Anyone experience that, and do you > have any good or bad news as far as expected damage? Specifically, I'm > wonder about how much is really bent back where you can't see anything. He > said there were no flight problems. He didn't know it happened until > postflight cleaning. > > -------- > Paul Richardson > RV-6A 106RV > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=30440#30440 > > > ________________________________________________________________________________
Date: Apr 25, 2006
Subject: Re: MT Props delay
From: marknlisa(at)hometel.com
Last year at S-n-F I spent about 20 mins at the Aerocomposites booth. The gentleman manning the booth spent the majority of the time showing me why the Aerocomposites prop is better than MT's prop. No wood, no screws, more carbon fiber, etc. Then I went to MT's booth and asked the gentleman there to respond to the comments from the Aerocomposites guy. The MT guy paused for a moment, then said it wasn't his company's policy to bash competitor's products. He suggested if I was concerned about the quality of MT props I should take a walk around the ramp. He said I'd find that about 90% of the aircraft used by the aerobatic performers during the show are equipped with MT props. Things that make you go hmmmm..... Mark Sletten Legacy FG N828LM http://www.legacyfgbuilder.com Aerocomposites quotes a 20 week delivery. I have only seen 1 performance comparison between MT, Aerocomposites, and Hartzel. All props were within 6 mph top speed of each other. I have ordered the MT anyways despite the 16 week wait. Steve RV7A ________________________________________________________________________________
Date: Apr 25, 2006
From: Gary Childers <cowboy286(at)sbcglobal.net>
Subject: Lycoming 0320 E2D For Sale
Lycoming 0320 E2D For Sale. Currently running in my 68 C177 Cardinal. $12,500 OBO outright 1100 SMOH 500 STOH 130 Since Bottom overhault. 3,000 TT. Complete Logs. Previous owners did top then did bottom later as part of oil pump replacement. This engine is strong and will be sold complete with mags, vaccume pump, starter, alternator, and carb. Removing engine for 180hp conversion. Call 517-449-8142 or email cowboy286(at)sbcglobal.net ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: Apr 25, 2006
Subject: Re: RV-6A Tail Tie Down
In a message dated 4/24/06 9:02:45 PM Central Daylight Time, c.ennis(at)insightbb.com writes: > but I would rather spare the tail and lose the ring, and I don't have > to worry about the ring jambing the rudder if I slam it during takeoff. >>>> I welded a piece of 5/16" or 3/8" stainless steel rod (not sure which size) about 12" long to a stainless plate that is located in the same location as the ring mount. The rod is bent aft just below the plate and extends rearward at a slight downward angle, maybe 20-25 degrees from the rudder bottom. Originally, I had bent the rear end of it into a loop that I used to tie-down the rear for the climb test before first flight. After about 20 hours I cut the loop off with about 5" of the rod remaining aft of the plate, then fabricated a small clamp out of stainless. It is simply a rectangular block with a hole near one end that slips over the end of the "tail skid". A slot is cut from the opposite end of the block to the hole, then another hole is drilled through ninety degrees from the first- this passes through the slot. On one side of the slot, the hole is tapped for the same size tie down ring used for the wings, and the other side of the slot is bored out to clear the threads. Slip the block over the rod, insert the tie-down ring on the un-threaded side and screw it in until it clamps down on the rod. Easily removed and stored in the plane. You have tail protection without risk of damaging the ring and without the ring hanging in the breeze, I'm sure it gets me at least .0005 additional knots due to less drag... I've got some fotoz of this gizmo somewhere, but not on this machine- if the above description is really confusing I could dig one up and forward... >From The PossumWorks in TN Mark Phillips - N51PW, almost 300 hours ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: Interpreting Aileron Position
Date: Apr 25, 2006
I have a feeling my ailerons are trying to tell me something significant about my heavy left wing condition but I'm having trouble getting it. So, here goes. In level flight, I'm applying full right manual aileron trim to stay level with the left tank empty. On the ground, I've established a visual picture of the neutral trail position of the ailerons relative to the wingtips by measurement with a digital level. So, when I look in the air, I expect to see the left aileron displaced down from neutral and the right aileron displaced up. What I actually see is the reverse situation. The left aileron is displaced up and the right down. What does this mean? I've checked wing incidence, trimmed up the yaw, set the flaps to neutral trail, and found no vertical displacement errors in the ailerons themselves where they attach to the wing spar using the wing template. So, according to Van's instructions posted on their web site, I'm at the trailing edge squeezing stage. Could there be some other factor that would account for the unexpectedly reversed in-flight position? Something that should be corrected before squeezing? Or should I just follow Van's advice and squeeze til it flys level? Dave Reel - RV8A ________________________________________________________________________________
Date: Apr 25, 2006
From: "D.Bristol" <dbris200(at)sbcglobal.net>
Subject: Re: Interpreting Aileron Position
Don't do anything until you try it without the manual trim connected (assuming the spring system). The trim system can mask the symptoms and could actually be causing the problem. Dave -6 SoCal EAA Technical Counselor DAVID REEL wrote: > >I have a feeling my ailerons are trying to tell me something significant about my heavy left wing condition but I'm having trouble getting it. So, here goes. In level flight, I'm applying full right manual aileron trim to stay level with the left tank empty. On the ground, I've established a visual picture of the neutral trail position of the ailerons relative to the wingtips by measurement with a digital level. So, when I look in the air, I expect to see the left aileron displaced down from neutral and the right aileron displaced up. What I actually see is the reverse situation. The left aileron is displaced up and the right down. What does this mean? > >I've checked wing incidence, trimmed up the yaw, set the flaps to neutral trail, and found no vertical displacement errors in the ailerons themselves where they attach to the wing spar using the wing template. So, according to Van's instructions posted on their web site, I'm at the trailing edge squeezing stage. Could there be some other factor that would account for the unexpectedly reversed in-flight position? Something that should be corrected before squeezing? Or should I just follow Van's advice and squeeze til it flys level? > >Dave Reel - RV8A > > > > > > > > > ________________________________________________________________________________
From: "SteinAir, Inc." <stein(at)steinair.com>
Subject: Interpreting Aileron Position
Date: Apr 25, 2006
Is the ball centered or are you flying with the ball off center somewhat? This is the 1st thing to look at with heavy wings. If you are skidding through the air somewhat, that can cause a surprisingly heavy wing. This can and is caused by either the Vertical Stab needing adjustment, or more commonly the gear legs fairings being mis-aligned. If that isn't the cause, then you need to get to "squeezing" the light wing down and start fixin. If that doesn't work, then the only solution left is to remount the ailierons with a new hinge and place them up or down as needed. Cheers, Stein. >-----Original Message----- >From: owner-rv-list-server(at)matronics.com >[mailto:owner-rv-list-server(at)matronics.com]On Behalf Of DAVID REEL >Sent: Tuesday, April 25, 2006 9:51 AM >To: rvlist >Subject: RV-List: Interpreting Aileron Position > > >I have a feeling my ailerons are trying to tell me something >significant about my heavy left wing condition but I'm having >trouble getting it. So, here goes. In level flight, I'm applying >full right manual aileron trim to stay level with the left tank >empty. On the ground, I've established a visual picture of the >neutral trail position of the ailerons relative to the wingtips by >measurement with a digital level. So, when I look in the air, I >expect to see the left aileron displaced down from neutral and the >right aileron displaced up. What I actually see is the reverse >situation. The left aileron is displaced up and the right down. >What does this mean? > >I've checked wing incidence, trimmed up the yaw, set the flaps to >neutral trail, and found no vertical displacement errors in the >ailerons themselves where they attach to the wing spar using the >wing template. So, according to Van's instructions posted on >their web site, I'm at the trailing edge squeezing stage. Could >there be some other factor that would account for the unexpectedly >reversed in-flight position? Something that should be corrected >before squeezing? Or should I just follow Van's advice and >squeeze til it flys level? > >Dave Reel - RV8A > > ________________________________________________________________________________
Subject: Re: Interpreting Aileron Position
Date: Apr 25, 2006
From: "Glaeser, Dennis A" <dennis.glaeser(at)eds.com>
If the left tank is empty, then to compensate, the left aileron would be UP to compensate. In essence, the left wing needs less lift - up aileron - (less weight) and the right wing more lift - down aileron - (more weight with the fuller tank). So what you are seeing is what I would expect. I'm not clear about what you mean by 'full right aileron trim' - which way are you moving the trim lever? I agree with Dave Bristol - disconnect the manual trim and fly before doing anything. Dennis Glaeser RV7A I have a feeling my ailerons are trying to tell me something significant about my heavy left wing condition but I'm having trouble getting it. So, here goes. In level flight, I'm applying full right manual aileron trim to stay level with the left tank empty. On the ground, I've established a visual picture of the neutral trail position of the ailerons relative to the wingtips by measurement with a digital level. So, when I look in the air, I expect to see the left aileron displaced down from neutral and the right aileron displaced up. What I actually see is the reverse situation. The left aileron is displaced up and the right down. What does this mean? I've checked wing incidence, trimmed up the yaw, set the flaps to neutral trail, and found no vertical displacement errors in the ailerons themselves where they attach to the wing spar using the wing template. So, according to Van's instructions posted on their web site, I'm at the trailing edge squeezing stage. Could there be some other factor that would account for the unexpectedly reversed in-flight position? Something that should be corrected before squeezing? Or should I just follow Van's advice and squeeze til it flys level? Dave Reel - RV8A ________________________________________________________________________________
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Interpreting Aileron Position
Date: Apr 25, 2006
On 25 Apr 2006, at 10:51, DAVID REEL wrote: > > I have a feeling my ailerons are trying to tell me something > significant about my heavy left wing condition but I'm having > trouble getting it. So, here goes. In level flight, I'm applying > full right manual aileron trim to stay level with the left tank > empty. On the ground, I've established a visual picture of the > neutral trail position of the ailerons relative to the wingtips by > measurement with a digital level. So, when I look in the air, I > expect to see the left aileron displaced down from neutral and the > right aileron displaced up. What I actually see is the reverse > situation. The left aileron is displaced up and the right down. > What does this mean? > > I've checked wing incidence, trimmed up the yaw, set the flaps to > neutral trail, and found no vertical displacement errors in the > ailerons themselves where they attach to the wing spar using the > wing template. So, according to Van's instructions posted on their > web site, I'm at the trailing edge squeezing stage. Could there be > some other factor that would account for the unexpectedly reversed > in-flight position? Something that should be corrected before > squeezing? Or should I just follow Van's advice and squeeze til it > flys level? 1. Disconnect the trim springs and try it. 2. Remove the gear leg fairings and fly it, to confirm they are not causing the problem. 3. Level the aircraft side-to-side on the ground, and be sure your ball is centered. If not, slot the holes on the TC (or EFIS, or where ever the ball is), and rotate it to center the ball. Then, in flight, use rudder as required to center the ball. Add a rudder trim tab if required. 4. Carefully inspect the aileron trailing edges. Are the trailing edge radii and contours the same on each side? 5. How is the upper wing skin contour ahead of the ailerons? If you lay a straight edge on the wing skin, is there a difference in contour from one side to the other? If so, this could affect the air pressure on top of the aileron, and cause an aileron deflection. Keep us posted. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
Date: Apr 25, 2006
From: Phil Birkelbach <phil(at)petrasoft.net>
Subject: Re: Interpreting Aileron Position
My heavy left wing seems to be caused by a little twist in the flap, so you might want to check that I also don't have much faith in either digital levels or the wing template. Make sure the tooling holes in the wing ribs and aileron ribs are lined up. That's the way we do it on the -7's and since the wing is the same it should work on your -8 too. And just in case nobody mentioned this... try it without the trim hooked up. :-) If I had to guess I think the aileron is trying to tell you that your airplane is straight and the aileron trim is off. Godspeed, Phil Birkelbach - Houston Texas RV-7 N727WB http://www.myrv7.com DAVID REEL wrote: > >I have a feeling my ailerons are trying to tell me something significant about my heavy left wing condition but I'm having trouble getting it. So, here goes. In level flight, I'm applying full right manual aileron trim to stay level with the left tank empty. On the ground, I've established a visual picture of the neutral trail position of the ailerons relative to the wingtips by measurement with a digital level. So, when I look in the air, I expect to see the left aileron displaced down from neutral and the right aileron displaced up. What I actually see is the reverse situation. The left aileron is displaced up and the right down. What does this mean? > >I've checked wing incidence, trimmed up the yaw, set the flaps to neutral trail, and found no vertical displacement errors in the ailerons themselves where they attach to the wing spar using the wing template. So, according to Van's instructions posted on their web site, I'm at the trailing edge squeezing stage. Could there be some other factor that would account for the unexpectedly reversed in-flight position? Something that should be corrected before squeezing? Or should I just follow Van's advice and squeeze til it flys level? > >Dave Reel - RV8A > > > > > > > > > ________________________________________________________________________________
From: "Szantho B. Szantho" <jszantho(at)gmail.com>
Subject: Re: Medical in trouble
Date: Apr 25, 2006
Recently I was prescribed a medication that will prevent me from acting as PIC. Unfortunately this will have to be a lifetime commitment. I am building a RV9-A and I am approximately 8-10 month from finishing the project. You probably understand the total devastation this development created in my life (close to depression). I loved the building process and was looking forward to flying my airplane. Now all these dreams are wiped out. Perhaps light sport plane is still an option. I was not an active contributor to the list since I am a first time builder and my philosophy is to keep silent if you can't add better advice than already offered. All I can say is that this list and other RV lists were invaluable aid to me. A big hart felt thank to all of you. I am writing this to see if any of you guys know someone who might be interested in taking over the project. I would like to get as much of my basic cost back as possible. Any advice would be greatly appreciated. My kit had the quick build wing and fuselage, have the firewall forward kit and a new Lycoming O-320 engine. 90% of the riveting and 100% of the priming is done, the canopy is assembled. Essentially from here on it is an assembly project. I have full documentation on everything including cost. Thanks for any help. John RV9-A jszantho(at)gmail.com ________________________________________________________________________________
From: "Oliver Washburn" <ollie6a(at)earthlink.net>
Subject: Re: Medical in trouble
Date: Apr 25, 2006
John Sorry to hear of your problem, but if you enjoy building why don't you finish the plane. I think you would recoup more money from a finished plane than the kit and you will have the enjoyment of seeing it take shape. I also have had medical problems but I am lucky in that my wife also has a license so I take her along and keep right on a flyin, I also have a Rans S7S kit on order that is to be shipped May 8th so I can fly alone under the LSA rules. Hang in there. Ollie 6A Central Fl. ----- Original Message ----- From: "Szantho B. Szantho" <jszantho(at)gmail.com> Sent: Tuesday, April 25, 2006 3:10 PM Subject: RV-List: Re: Medical in trouble > > Recently I was prescribed a medication that will prevent me from acting as > PIC. Unfortunately this will have to be a lifetime commitment. I am > building > a RV9-A and I am approximately 8-10 month from finishing the project. You > probably understand the total devastation this development created in my > life (close to depression). I loved the building process and was looking > forward to flying my airplane. Now all these dreams are wiped out. Perhaps > light sport plane is still an option. I was not an active contributor to > the > list since I am a first time builder and my philosophy is to keep silent > if > you can't add better advice than already offered. All I can say is that > this > list and other RV lists were invaluable aid to me. A big hart felt thank > to > all of you. I am writing this to see if any of you guys know someone who > might be interested in taking over the project. I would like to get as > much > of my basic cost back as possible. Any advice would be greatly > appreciated. > My kit had the quick build wing and fuselage, have the firewall forward > kit > and a new Lycoming O-320 engine. 90% of the riveting and 100% of the > priming > is done, the canopy is assembled. Essentially from here on it is an > assembly > project. I have full documentation on everything including cost. Thanks > for > any help. > > > John > > RV9-A > > jszantho(at)gmail.com > > > ________________________________________________________________________________
From: "John Jessen" <jjessen(at)rcn.com>
Subject: Re: Medical in trouble
Date: Apr 25, 2006
I agree. Stay with the project! Finish it, see it fly, then move over to the LSA if you can. We all are behind you! -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Oliver Washburn Sent: Tuesday, April 25, 2006 2:26 PM Subject: Re: RV-List: Re: Medical in trouble John Sorry to hear of your problem, but if you enjoy building why don't you finish the plane. I think you would recoup more money from a finished plane than the kit and you will have the enjoyment of seeing it take shape. I also have had medical problems but I am lucky in that my wife also has a license so I take her along and keep right on a flyin, I also have a Rans S7S kit on order that is to be shipped May 8th so I can fly alone under the LSA rules. Hang in there. Ollie 6A Central Fl. ----- Original Message ----- From: "Szantho B. Szantho" <jszantho(at)gmail.com> Sent: Tuesday, April 25, 2006 3:10 PM Subject: RV-List: Re: Medical in trouble > > Recently I was prescribed a medication that will prevent me from acting as > PIC. Unfortunately this will have to be a lifetime commitment. I am > building > a RV9-A and I am approximately 8-10 month from finishing the project. You > probably understand the total devastation this development created in my > life (close to depression). I loved the building process and was looking > forward to flying my airplane. Now all these dreams are wiped out. Perhaps > light sport plane is still an option. I was not an active contributor to > the > list since I am a first time builder and my philosophy is to keep silent > if > you can't add better advice than already offered. All I can say is that > this > list and other RV lists were invaluable aid to me. A big hart felt thank > to > all of you. I am writing this to see if any of you guys know someone who > might be interested in taking over the project. I would like to get as > much > of my basic cost back as possible. Any advice would be greatly > appreciated. > My kit had the quick build wing and fuselage, have the firewall forward > kit > and a new Lycoming O-320 engine. 90% of the riveting and 100% of the > priming > is done, the canopy is assembled. Essentially from here on it is an > assembly > project. I have full documentation on everything including cost. Thanks > for > any help. > > > John > > RV9-A > > jszantho(at)gmail.com > > > ________________________________________________________________________________
From: "Randy Lervold" <randy(at)romeolima.com>
Subject: Re: Vx, Vy, Best Glide for O-360/Hartzell
Date: Apr 25, 2006
> I'm getting ready to do performance testing for Vx, Vy, and best glide > speeds in my RV-8A with O-360/Hartzell setup. I know there are some POH's > floating around out there with these numbers in them but I'm curious how > many people have measured this data carefully themselves? In particular > to get good glide data one would have to pull the mixture and ideally test > with the prop stopped, prop rotating with oil pressure & lever aft, and > prop rotating without oil pressure (fine pitch). This could take quite a > few engine-off glide tests and the numbers should be pretty close from one > RV to the next... > Which brings me to my point: if there's any "consensus" on these speeds > amongst those of you who've taken good data it would be nice to have those > numbers as a starting point for my testing. For example if Vy is > typically 80-90 kts I would narrow the range of my test from 75 to 95 > instead of a much broader span of numbers. > It would be cool if someone made a spreadsheet collecting this kind of > data from different airplanes. Checkoway are you listening? > Thanks, > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D flying 29.2 hours now... Mark, I did quite a bit of testing for Vy in my RV-8 in the course of doing prop climb rate testing. Interestingly I found a slightly different Vy for each prop, but if you stay within the 115-125 mph (99-107 kts) range you will find your number. 120-122 mph (103-105 kts) was the sweet spot so be sure and check there. I always meant to check my glide with the prop turning and with it not, but never did. Randy Lervold www.rv-3.com www.rv-8.com ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Re: Medical in trouble
Date: Apr 25, 2006
Why don't you talk to the AOPA and your physician to see if there is an alternative drug you can take and still keep your medical. If that fails, petition the FAA for a waiver, or just keep your mouth shut, the AME only knows what you tell him. In any case, you'll get more for your collection of parts if you turn it into an airplane. Bruce www.glasair.org -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Oliver Washburn Sent: Tuesday, April 25, 2006 5:26 PM Subject: Re: RV-List: Re: Medical in trouble John Sorry to hear of your problem, but if you enjoy building why don't you finish the plane. I think you would recoup more money from a finished plane than the kit and you will have the enjoyment of seeing it take shape. I also have had medical problems but I am lucky in that my wife also has a license so I take her along and keep right on a flyin, I also have a Rans S7S kit on order that is to be shipped May 8th so I can fly alone under the LSA rules. Hang in there. Ollie 6A Central Fl. ----- Original Message ----- From: "Szantho B. Szantho" <jszantho(at)gmail.com> Sent: Tuesday, April 25, 2006 3:10 PM Subject: RV-List: Re: Medical in trouble > > Recently I was prescribed a medication that will prevent me from acting as > PIC. Unfortunately this will have to be a lifetime commitment. I am > building > a RV9-A and I am approximately 8-10 month from finishing the project. You > probably understand the total devastation this development created in my > life (close to depression). I loved the building process and was looking > forward to flying my airplane. Now all these dreams are wiped out. Perhaps > light sport plane is still an option. I was not an active contributor to > the > list since I am a first time builder and my philosophy is to keep silent > if > you can't add better advice than already offered. All I can say is that > this > list and other RV lists were invaluable aid to me. A big hart felt thank > to > all of you. I am writing this to see if any of you guys know someone who > might be interested in taking over the project. I would like to get as > much > of my basic cost back as possible. Any advice would be greatly > appreciated. > My kit had the quick build wing and fuselage, have the firewall forward > kit > and a new Lycoming O-320 engine. 90% of the riveting and 100% of the > priming > is done, the canopy is assembled. Essentially from here on it is an > assembly > project. I have full documentation on everything including cost. Thanks > for > any help. > > > John > > RV9-A > > jszantho(at)gmail.com > > > ________________________________________________________________________________
Date: Apr 25, 2006
From: <erichweaver(at)cox.net>
Subject: identification of fuel level sender type
Cc: RV-List Digest Server My rv-7A kit came to me half finished from a builder who passed away before he could finish. I now need some help identifying the type of fuel level sender that was installed in my tanks. From memory, there is a small circular metal plate at the wing root rib, with five bolt heads around the perimeter of the plate. Cant quite picture it, but there is some sort of additional connector and/or wiring point in the center of the plate. Can anyone tell from this poor description whether this is a float or capacitive type sender, or is more info needed? A bonus would be any info on where to find associated info for wiring the sender to my GRT EFIS. regards Erich Weaver ________________________________________________________________________________
Date: Apr 25, 2006
From: Richard Tasker <retasker(at)optonline.net>
Subject: Re: identification of fuel level sender type
That is the float sender. The capacitance has no external parts except a BNC connector the internal plates. What GRT EIS do you have? (2000, 4000, 6000) Dick erichweaver(at)cox.net wrote: > >My rv-7A kit came to me half finished from a builder who passed away before he could finish. I now need some help identifying the type of fuel level sender that was installed in my tanks. From memory, there is a small circular metal plate at the wing root rib, with five bolt heads around the perimeter of the plate. Cant quite picture it, but there is some sort of additional connector and/or wiring point in the center of the plate. Can anyone tell from this poor description whether this is a float or capacitive type sender, or is more info needed? A bonus would be any info on where to find associated info for wiring the sender to my GRT EFIS. > >regards > >Erich Weaver > > ________________________________________________________________________________
From: "William Gill" <wgill10(at)comcast.net>
Subject: identification of fuel level sender type
Date: Apr 25, 2006
Yep, it's a float...should be a Stewart Warner 385B-F. Sorry, can't help with the GRT EFIS. Bill -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of erichweaver(at)cox.net Sent: Tuesday, April 25, 2006 5:58 PM Cc: RV-List Digest Server Subject: RV-List: identification of fuel level sender type My rv-7A kit came to me half finished from a builder who passed away before he could finish. I now need some help identifying the type of fuel level sender that was installed in my tanks. From memory, there is a small circular metal plate at the wing root rib, with five bolt heads around the perimeter of the plate. Cant quite picture it, but there is some sort of additional connector and/or wiring point in the center of the plate. Can anyone tell from this poor description whether this is a float or capacitive type sender, or is more info needed? A bonus would be any info on where to find associated info for wiring the sender to my GRT EFIS. regards Erich Weaver ________________________________________________________________________________
From: "Konrad L. Werner" <klwerner(at)comcast.net>
Subject: Re: identification of fuel level sender type
Date: Apr 25, 2006
If I understand you correctly, then it is highly likely a float type sender. The capacitance senders are flat plates -inside- the tank, and an unobstructed coverplate with no provision for a sender poking out. ----- Original Message ----- From: erichweaver(at)cox.net To: rv-list(at)matronics.com Cc: RV-List Digest Server Sent: Tuesday, April 25, 2006 4:58 PM Subject: RV-List: identification of fuel level sender type My rv-7A kit came to me half finished from a builder who passed away before he could finish. I now need some help identifying the type of fuel level sender that was installed in my tanks. From memory, there is a small circular metal plate at the wing root rib, with five bolt heads around the perimeter of the plate. Cant quite picture it, but there is some sort of additional connector and/or wiring point in the center of the plate. Can anyone tell from this poor description whether this is a float or capacitive type sender, or is more info needed? A bonus would be any info on where to find associated info for wiring the sender to my GRT EFIS. regards Erich Weaver -- ________________________________________________________________________________
From: RVer273sb(at)aol.com
Date: Apr 25, 2006
Subject: rv8 tail kit for sale
I have an untouched RV-8 tail kit for sale. With electric trim option. $1300 plus freight. Located in the Denver Co. area. Stewart ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Apr 25, 2006
Subject: Re: Medical in trouble
I agree with the others , go ahead and finish the plane. DON'T ask the FAA for anything !!!!!!!! Once they get a hint of any problem, you're duck soup !! As the other guy said , check the AOPA website and you can get a list of approved medicines. Work with you own doctor to switch to an approved one. Use it for awhile before you go to an AME for your medical. Try to get an AME recommended by other pilots. I had a problem with a partially clogged small artery and sent letters from my internal medicine specialist and cardiologist saying I was OK. I sent 2 pounds of paper to the FAA about 3 weeks before the LSA was approved , with the medical change sneaked in. They denied my medical and now I have a 62 hour RV-4 sitting in my hangar. NO LSA for me either. Don't trust the FAA for anything !! Bob Olds RV-4 , N1191X A&P , EAA Tech. Counselor Charleston,Arkansas Real Aviators Fly Taildraggers ________________________________________________________________________________
From: Joe Larson <jpl(at)showpage.org>
Subject: Re: Medical in trouble
Date: Apr 25, 2006
Write your congressmen. They can update the laws the FAA works under. -Joe On Apr 25, 2006, at 8:47 PM, Oldsfolks(at)aol.com wrote: > DON'T ask the FAA for anything !!!!!!!! ..... > They denied my medical and now I have a 62 > hour RV-4 sitting in my hangar. NO LSA for me either. > Don't trust the FAA for anything !! ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: Interpreting Aileron Position
Date: Apr 25, 2006
Dave, Six years ago when I first flew my RV8 I experienced a similar problem. After trying every remedy under the sun, I finally noticed that the outer aeleron hinge positioned the aeleron about 1/8 inch lower than the inboard hinge next to the flap. I had tried all of the other remedies to no avail. After many discussions with everybody who had an opinion, it was decided that I was experiencing "flow separation" on that aeleron. I got a new hinge from Vans and very carefully fitted it so that the top aeleron surface was perfectly even with the wing trailing edge. this corrected the problem and I have flown hands off ever since. I now have 1300 hours and still enjoy every minute. Good luck, Dick Martin RV8 N233M the fast one ----- Original Message ----- From: "DAVID REEL" <dreel(at)cox.net> Sent: Tuesday, April 25, 2006 9:51 AM Subject: RV-List: Interpreting Aileron Position > > I have a feeling my ailerons are trying to tell me something significant > about my heavy left wing condition but I'm having trouble getting it. So, > here goes. In level flight, I'm applying full right manual aileron trim > to stay level with the left tank empty. On the ground, I've established a > visual picture of the neutral trail position of the ailerons relative to > the wingtips by measurement with a digital level. So, when I look in the > air, I expect to see the left aileron displaced down from neutral and the > right aileron displaced up. What I actually see is the reverse situation. > The left aileron is displaced up and the right down. What does this mean? > > I've checked wing incidence, trimmed up the yaw, set the flaps to neutral > trail, and found no vertical displacement errors in the ailerons > themselves where they attach to the wing spar using the wing template. > So, according to Van's instructions posted on their web site, I'm at the > trailing edge squeezing stage. Could there be some other factor that > would account for the unexpectedly reversed in-flight position? Something > that should be corrected before squeezing? Or should I just follow Van's > advice and squeeze til it flys level? > > Dave Reel - RV8A > > > ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: Datapoint for Fairings Speed Improvement
Date: Apr 25, 2006
Mark, Welcome to the world of faster airplanes. A giant engine helps, but a CLEAN, LIGHT airplane always wins the speed contests. I have an RV8 and during my initial testing, I experimented with various gear leg to fuselage fairings and found that a considerable speed increase is available at this junction. An easy way to test the efficiency of the fairing is to spray some waste oil on the fuselage in the area where the landing gear attachs, and then go up an fly the airplane. If the fairing is efficient, you will see perfectly shaped oil lines on the side of the fuselage depicting the airflow (just like the pictures in the technical magazines). If the flow lines are erattic, you know you need to try some variations in shape of the fairing. As a general statement, the upper gear to fuse fairing will be more efficient when it has a lead is between 1 and 2 inchs long with a long ,narrow taper to the gear leg. A side note: some RV8s experience a sliight tail shudder when stall landing. If the above fairing is correct, the tail shudder disappears. Good luck with your project and hope to see you and others in the Air Venture Races. Dick Martin RV8 N233M the fast one ----- Original Message ----- From: <czechsix(at)juno.com> Sent: Monday, April 24, 2006 8:15 PM Subject: RV-List: Datapoint for Fairings Speed Improvement > > Guys, > I know others have commented on how much speed an RV picks up when > fairings are installed. Just for kicks though I took some data in my > RV-8A without any fairings and then again with wheel pants, gear leg and > intersection fairings installed. My data was taken with four-way GPS runs > using one of the calculators on Kevin Horton's website (the advantage of > the four-way run vs. three-way is that the spreadsheet gives you a sanity > check to show how good/bad your data is). > Anyway, at 4000' density altitude, power set to 24 squared and mixture 50 > ROP, I saw an 18 kt gain in TAS when when fairings were put on. I would > imagine that the speed increase would be less in a taildragger since there > are only two big gear legs/wheels to clean up. I wish now I'd taken some > numbers at full power and lower altitude...I bet the speed increase would > have been at least 20 kts. Even so I've told several of my spam-can > buddies and they can't believe that fairings would make that much > difference. > Cool! > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D with O-360-A1A and blended Hartzell > Flying 29.2 hours now.... > > > Guys, > > > I know others have commented on how much speed an RV picks up when > fairings are installed. Just for kicks though I took some data in my RV-8A > without any fairings and then again with wheel pants, gear leg and > intersection fairings installed. My data was taken with four-way GPS runs > using one of the calculators on Kevin Horton's website (the advantage of > the four-way run vs. three-way is that the spreadsheet gives you a sanity > check to show how good/bad your data is). > > > Anyway, at 4000' density altitude, power set to 24 squared and mixture 50 > ROP, I saw an 18 kt gain in TAS when when fairings were put on. I would > imagine that the speed increase would be less in a taildragger since there > are only two big gear legs/wheels to clean up. I wish now I'd taken some > numbers at full power and lower altitude...I bet the speed increase would > have been at least 20 kts. Even so I've told several of my spam-can > buddies and they can't believe that fairings would make that much > difference. > > > Cool! > > > --Mark Navratil > Cedar Rapids, Iowa > RV-8A N2D with O-360-A1A and blended Hartzell > Flying 29.2 hours now.... > > > ________________________________________________________________________________
Date: Apr 25, 2006
From: vft(at)aol.com
Subject: Stuff for sale
I've started to clean out some of the stuff accumulated in my shop. Falcon vertical card compass, mounted in panel but never used. --$100 F1 MK1 engine mount-- free to anyone who will pay shipping Lancair 4P engine mount (TSIO-550)-- same as above Danny Melnik F1 #25 Melbourne (FL) Rocket Factory ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Re: Medical in trouble
Date: Apr 25, 2006
Sorry to hear that Bob, did you have an angioplasty to clear the problem? Bruce www.glasair.org -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Oldsfolks(at)aol.com Sent: Tuesday, April 25, 2006 9:47 PM Subject: RV-List: Re: Medical in trouble I agree with the others , go ahead and finish the plane. DON'T ask the FAA for anything !!!!!!!! Once they get a hint of any problem, you're duck soup !! As the other guy said , check the AOPA website and you can get a list of approved medicines. Work with you own doctor to switch to an approved one. Use it for awhile before you go to an AME for your medical. Try to get an AME recommended by other pilots. I had a problem with a partially clogged small artery and sent letters from my internal medicine specialist and cardiologist saying I was OK. I sent 2 pounds of paper to the FAA about 3 weeks before the LSA was approved , with the medical change sneaked in. They denied my medical and now I have a 62 hour RV-4 sitting in my hangar. NO LSA for me either. Don't trust the FAA for anything !! Bob Olds RV-4 , N1191X A&P , EAA Tech. Counselor Charleston,Arkansas Real Aviators Fly Taildraggers ________________________________________________________________________________
Date: Apr 25, 2006
From: William Scaringe <bscaringe(at)sbcglobal.net>
Subject: For Sale: ENR Headset, 3X Rivet Gun, Misc. Tools
Please see the following items that I posted on Ebay: Noise Reduction Headset, DRE-6000 http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&item=4635038942 Tony Bingelis Book Set (4 books) http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=8060162187 3X Rivet Gun, U.S. Industrial Tool http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=7613777680 3.5" Rivet Sets, Cupped AN470 http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=7613778633 AN470 solid aluminum aircraft rivets, 1lb 3-3, .5lb 3-4 http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&item=4635043751 7 Bucking Bars http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=7613765837 New Fluting Pliers with Nylon Jaws (flute aluminum parts without marking them) http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=7613772961 3.5" Offset Hand Seamer http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=7613774520 Pop Air Rivet Gun Pneumatic Riveter with 1000 rivets http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=7613776848 15 Warbird Videos http://cgi.ebay.com/ws/eBayISAPI.dll?ViewItem&rd=1,1&item=9130185151 ________________________________________________________________________________
Date: Apr 26, 2006
From: David Fenstermacher <davidfenster(at)comcast.net>
Subject: Re: Medical in trouble
I may get flamed for this, but............... Don't tell the FAA squat. Do you feel safe? Oldsfolks(at)aol.com wrote: > > I agree with the others , go ahead and finish the plane. > DON'T ask the FAA for anything !!!!!!!! Once they get a hint of any > problem, you're duck soup !! As the other guy said , check the AOPA website and > you can get a list of approved medicines. Work with you own doctor to switch > to an approved one. Use it for awhile before you go to an AME for your > medical. > Try to get an AME recommended by other pilots. > I had a problem with a partially clogged small artery and sent letters from > my internal medicine specialist and cardiologist saying I was OK. I sent 2 > pounds of paper to the FAA about 3 weeks before the LSA was approved , with > the medical change sneaked in. They denied my medical and now I have a 62 > hour RV-4 sitting in my hangar. NO LSA for me either. > Don't trust the FAA for anything !! > > Bob Olds RV-4 , N1191X > A&P , EAA Tech. Counselor > Charleston,Arkansas > Real Aviators Fly Taildraggers > > > > > > > > ________________________________________________________________________________
From: "JAMES BOWEN" <jabowenjr(at)hotmail.com>
Subject: Stuff for sale
Date: Apr 25, 2006
Hello. If it's a 2.25 inch compass I'll take it. Thanks, Jim Bowen RV-8 Lake Tapps, Wa. jabowenjr(at)hotmail.com >From: vft(at)aol.com >Reply-To: rv-list(at)matronics.com >To: rocket-list(at)matronics.com, rv-list(at)matronics.com, >f1rocketbuilder(at)hotmail.com >Subject: RV-List: Stuff for sale >Date: Tue, 25 Apr 2006 23:27:23 -0400 > > >I've started to clean out some of the stuff accumulated in my shop. > >Falcon vertical card compass, mounted in panel but never used. --$100 >F1 MK1 engine mount-- free to anyone who will pay shipping >Lancair 4P engine mount (TSIO-550)-- same as above > > >Danny Melnik >F1 #25 >Melbourne (FL) Rocket Factory > > ________________________________________________________________________________
Date: Apr 26, 2006
From: Sherman Butler <lsbrv7a(at)yahoo.com>
Subject: Re: Medical in trouble
Who would support a candidate that wants the FAA to be removed from 3rd class medicals. So much is clincal evaluation that the FAA will second guess. Sherman Butler RV-7a Wings Idaho Falls --------------------------------- Love cheap thrills? Enjoy PC-to-Phone calls to 30+ countries for just 2/min with ________________________________________________________________________________
From: "Garrett Bray" <braygarrett(at)hotmail.com>
Subject: Re: Medical in trouble
Date: Apr 26, 2006
Make sure you don't try to get your medical renewed and are denied. You then can not fly sport pilot rules until you get the reason for the denial resolved with the FAA. I am taking meds that would preclude me from passing a medical, but I haven't gone to renew mine. If I decide to fly certified aircraft in the future I will be able to at least fly sport pilot rules. Good luck. ________________________________________________________________________________
From: "Jerry Grimmonpre" <jerry(at)mc.net>
Subject: Re: Datapoint for Fairings Speed Improvement
Date: Apr 26, 2006
Dick ... Can you expand on the description starting with: As a general statement, the upper gear to fuse fairing will be > more efficient when it has a lead is between 1 and 2 inchs long with a > long > ,narrow taper to the gear leg. Pictures would be good if you have them. Thanks ... Jerry Grimmonpre' RV8A Electrical > > Mark, > Welcome to the world of faster airplanes. A giant engine helps, but a > CLEAN, LIGHT airplane always wins the speed contests. I have an RV8 and > during my initial testing, I experimented with various gear leg to > fuselage > fairings and found that a considerable speed increase is available at this > junction. An easy way to test the efficiency of the fairing is to spray > some waste oil on the fuselage in the area where the landing gear attachs, > and then go up an fly the airplane. If the fairing is efficient, you will > see perfectly shaped oil lines on the side of the fuselage depicting the > airflow (just like the pictures in the technical magazines). If the flow > lines are erattic, you know you need to try some variations in shape of > the > fairing. As a general statement, the upper gear to fuse fairing will be > more efficient when it has a lead is between 1 and 2 inchs long with a > long > ,narrow taper to the gear leg. A side note: some RV8s experience a > sliight > tail shudder when stall landing. If the above fairing is correct, the > tail > shudder disappears. > Good luck with your project and hope to see you and others in the Air > Venture Races. > Dick Martin > RV8 N233M > the fast one ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: Apr 26, 2006
Subject: Re: Medical in trouble
I had a small artery with 'estimated' 60% blockage - FAA allows 50%. The cardiologist's letter stated that I wasn't likely to be incapicitated. FAA didn't even consider that ?? I have been driving my class 8 diesel tractor,riding our Goldwing motorcycle and anything else I would normally do. I had done the 40 hours testing(Including +4 & -3.5 aerobatic tests) on the RV-4 and was flying just fine until my medical was expiring. I appealed the decision and was denied again. The RV-4 will be sold and more time will be spent motorcycling - I'll see if I can wear out a Goldwing !! Keep flying guys - while you can and Good luck. Bob Olds RV-4 , N1191X A&P , EAA Tech. Counselor Charleston,Arkansas Real Aviators Fly Taildraggers ________________________________________________________________________________
Subject: Re: Medical in trouble
From: "Bob Collins" <bcollinsrv7a(at)comcast.net>
Date: Apr 26, 2006
This is a touchy subject for me as I am going through much the same thing. A lot of folks have suggested to me that I lie to the FAA and try to squeeze through a medical.... but let me ask you this. I have bouts of vertigo (Meniere's Disease). Do you really want me flying formation with you? Look, I get the whole "big bad federal government" thing, but the first step any pilot should consider when getting this news isn't "how can I fool the federal government and keep flying, " it's : am I safe to fly? Would I put my kids in the back seat and my wife in the front and launch? If you're not sure, then you already know the answer. Alternately, this is a long discussion you can and should have with your doctor (but definintely not your AME). Not telling the FAA is a silly suggestion -- imho -- because you've already told the person responsible for making the decision. You. Your medical records are on file, your prescriptions can be traced. and your insurance isn't going to pay for your careening into a schoolyard if it's determined you flew with a known disqualifying condition. And LSA was never meant to allow you to either. Can you get away with it? Maybe. Lots of folks will tell you you can. And you might even be able to rationalize it by telling yourself you're just striking a blow for pilot's freedom; that's it's really not about flying safely. But let's dig a little deeper. Where do you draw the line? An epileptic seizure? A debilitating bout of vertigo? Narcolepsy? Would you get into a plane as a passenger with one control stick and a pilot with no license and no training? Why not? They're just exercising their freedom. I'm with you. I probably will never fly again and there's nothing right now more depressing than that. I'm searching for ways to do so, but lying and breaking the law isn't an option for me. Why? Because if I do, I can never again look in the mirror and say I'm a responsible pilot. I can never advocate for us to fly safer and fly smarter and lead by example. And those are important to me. I can try to kid myself and say it's just me striking a blow against the bureacracy. Except for one thing. I know that it's not safe for me to fly. And I know it's not safe for YOU for me to fly. I can read the FAR as well as anyone and I can see I have a disqualifying condition. I KNOW that I'm required to ground myself and I KNOW I'm required to tell the FAA...not at my next medical. Right now. Do I like it? Hell no. It changes the entire rest of my life, including big plans for how my wife and I were to spend our retirement. But that's what being an adult is about in this world. Making sound decisions. So what do I recommend? I can't tell you what to do. I can only tell you what I'm doing. I'm going to keep building, and I may accelerate my building, basically for the same reason someone else posted: I finished plane is worth more than an unfinished one. If I'm never going to fly it but sell it when it's done...I can load more goodies into it, because I won't have to pay for it. Someone else will. In the meantime, I'm not giving up. I'm still going to investigate what alternatives are out there -- medically speaking -- that might allow me to one day fly again. But I'm not going to count on it. And I'm not going to risk anyone's life -- including my own -- or leave my estate stuck with a $1 million dollar payout because I wanted to fly illegally. One of the reasons I started the RV Builder's Hotline, is it's one way to still be a part of the RV community, even though I probably won't have an RV. That's why I'll probably build another RV when this one is done. Maybe folks will stop when they're flying via Minnesota and give me a ride in THEIR RV sometime. Hey, it's not the way I thought things were going to work out, but that's still a hell of a lot better than 99% of the people on this planet. We homebulders build becaue we love challenges. Well...now I've got one. And you've got one too. Meet it the same way you approach meeting the building challenge -- like a professional. YMMV. -------- Bob Collins St. Paul, Minn. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=30824#30824 ________________________________________________________________________________
Date: Apr 26, 2006
Subject:
From: marknlisa(at)hometel.com
Cc: jszantho(at)gmail.com John, Please, please, please listen to the good advice from the group and finish your project. You'll never forgive yourself if you don't build that -9 and see it fly, especially after all the hard work you've invested. The worst-case is you can't renew your FAA medical and someone has to fly with you. There are two individuals in my area in that situation and they fly regularly -- all they need is a qualified pilot to ride along and log the time. Somehow they never seem to have trouble finding a volunteer, even on short notice! Definitely contact AOPA for help with your medical issue vis-a-vis the FAA. You might be surprised what you can get waived if you follow the right procedure. AOPA has been helping folks with these problems for a long time and they have a staff of experts for just that purpose. If it turns out that you and AOPA feel that your medical condition will never pass FAA muster, then DON'T APPLY, REPEAT, DON'T APPLY! Once medically disqualified for a Private Certificate you can't get a Sport Pilot Certificate either. Proceed cautiously! Again, please reconsider your decision to sell your unfinished kit. One of the first major symptoms of depression is cessation of activities that one loves and brings one pleasure -- YOU CAN BEAT THIS! Nothing will help you feel better than seeing that -9 flying, and knowing that YOU finished it! Hoping you stick it out, Mark Sletten Legacy FG N828LM http://www.legacyfgbuilder.com Recently I was prescribed a medication that will prevent me from acting as PIC. Unfortunately this will have to be a lifetime commitment. I am building a RV9-A and I am approximately 8-10 month from finishing the project. You probably understand the total devastation this development created in my life (close to depression). I loved the building process and was looking forward to flying my airplane. Now all these dreams are wiped out. Perhaps light sport plane is still an option. I was not an active contributor to the list since I am a first time builder and my philosophy is to keep silent if you can't add better advice than already offered. All I can say is that this list and other RV lists were invaluable aid to me. A big hart felt thank to all of you. I am writing this to see if any of you guys know someone who might be interested in taking over the project. I would like to get as much of my basic cost back as possible. Any advice would be greatly appreciated. My kit had the quick build wing and fuselage, have the firewall forward kit and a new Lycoming O-320 engine. 90% of the riveting and 100% of the priming is done, the canopy is assembled. Essentially from here on it is an assembly project. I have full documentation on everything including cost. Thanks for any help. John RV9-A ________________________________________________________________________________
Subject: Re: Medical in trouble
Date: Apr 26, 2006
From: "Chuck Jensen" <cjensen(at)dts9000.com>
Bob, You raise a good point about responsibility resting with the pilot. This is particularly so if one starts taking liberties with the rules. While not suggesting that one ignores rules, limits, requirements, I would suggest that anyone contemplating doing so take a long hard look at the medical circumstances. Certainly, in your case, Meniere's disease, with an acute attack which may be fully unpredictable, can render a person absolutely unable to fly an aircraft. On the other hand, a poster that has 60% blockage when the FAA may allow 50%, and with the 'best-guess' from his cardiologist that it is not a problem, and he's exercising, eating right to lower the overall risk, may well reach a different conclusion about being a miscreant. In the end, it's all about risk management--with your health and with the FAA...both are important. Regarding the poster with the 60% blockage, I'd suggest that he redo the test and quiz his Cardiologist about the '60% rating'...is he sure it's 60%? It feels like 50% and sure looks like 50% to you? There is a high degree of subjectivity in many of these measurements and diagnosis. The Cardiologist may have 10% to give. Then again, it was maybe closer to 70% and he already 'gave' as much as he can. It's worth asking. Chuck Jensen > -----Original Message----- > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > server(at)matronics.com] On Behalf Of Bob Collins > Sent: Wednesday, April 26, 2006 9:35 AM > To: rv-list(at)matronics.com > Subject: RV-List: Re: Medical in trouble > > > This is a touchy subject for me as I am going through much the same thing. > A lot of folks have suggested to me that I lie to the FAA and try to > squeeze through a medical.... but let me ask you this. I have bouts of > vertigo (Meniere's Disease). Do you really want me flying formation with > you? > > Look, I get the whole "big bad federal government" thing, but the first > step any pilot should consider when getting this news isn't "how can I > fool the federal government and keep flying, " it's : am I safe to fly? > Would I put my kids in the back seat and my wife in the front and launch? > > If you're not sure, then you already know the answer. Alternately, this > is a long discussion you can and should have with your doctor (but > definintely not your AME). > > Not telling the FAA is a silly suggestion -- imho -- because you've > already told the person responsible for making the decision. You. Your > medical records are on file, your prescriptions can be traced. and your > insurance isn't going to pay for your careening into a schoolyard if it's > determined you flew with a known disqualifying condition. And LSA was > never meant to allow you to either. > > Can you get away with it? Maybe. Lots of folks will tell you you can. And > you might even be able to rationalize it by telling yourself you're just > striking a blow for pilot's freedom; that's it's really not about flying > safely. But let's dig a little deeper. Where do you draw the line? An > epileptic seizure? A debilitating bout of vertigo? Narcolepsy? > > Would you get into a plane as a passenger with one control stick and a > pilot with no license and no training? Why not? They're just exercising > their freedom. > > I'm with you. I probably will never fly again and there's nothing right > now more depressing than that. I'm searching for ways to do so, but lying > and breaking the law isn't an option for me. Why? Because if I do, I can > never again look in the mirror and say I'm a responsible pilot. I can > never advocate for us to fly safer and fly smarter and lead by example. > And those are important to me. > > I can try to kid myself and say it's just me striking a blow against the > bureacracy. Except for one thing. I know that it's not safe for me to fly. > And I know it's not safe for YOU for me to fly. > > I can read the FAR as well as anyone and I can see I have a disqualifying > condition. I KNOW that I'm required to ground myself and I KNOW I'm > required to tell the FAA...not at my next medical. Right now. > > Do I like it? Hell no. It changes the entire rest of my life, including > big plans for how my wife and I were to spend our retirement. But that's > what being an adult is about in this world. Making sound decisions. > > So what do I recommend? I can't tell you what to do. I can only tell you > what I'm doing. I'm going to keep building, and I may accelerate my > building, basically for the same reason someone else posted: I finished > plane is worth more than an unfinished one. If I'm never going to fly it > but sell it when it's done...I can load more goodies into it, because I > won't have to pay for it. Someone else will. > > In the meantime, I'm not giving up. I'm still going to investigate what > alternatives are out there -- medically speaking -- that might allow me to > one day fly again. But I'm not going to count on it. And I'm not going to > risk anyone's life -- including my own -- or leave my estate stuck with a > $1 million dollar payout because I wanted to fly illegally. > > One of the reasons I started the RV Builder's Hotline, is it's one way to > still be a part of the RV community, even though I probably won't have an > RV. That's why I'll probably build another RV when this one is done. > Maybe folks will stop when they're flying via Minnesota and give me a ride > in THEIR RV sometime. Hey, it's not the way I thought things were going to > work out, but that's still a hell of a lot better than 99% of the people > on this planet. > > We homebulders build becaue we love challenges. Well...now I've got one. > And you've got one too. Meet it the same way you approach meeting the > building challenge -- like a professional. > > YMMV. > > -------- > Bob Collins > St. Paul, Minn. > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=30824#30824 > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Szantho B. Szantho" <jszantho(at)gmail.com>
Subject: Re: Medical in trouble
Date: Apr 26, 2006
The flying community is truly unique. You realize you have friends you never knew existed. Thank you guys, but expressing this in words will never be enough. Your words of encouragement mean everything for me. I put into this project heart and sole and you are right it would be a shame to quit something I enjoyed so much. As you suggested I will try to go on. I am still in the dumper, but maybe just working on my RV project will help. I have talked to AOPA and EAA but they could not come up with any suggestions. The sad part of this is that I feel I am not a danger to anyone on the ground or in the air. Except for the medication I have to take I could fly. Obviously I do not know if my condition will become more serious in the future. If that would happen I would ground myself without FAA's help. According to two doctors I will have to stay on the pills for life and these are the mildest of the bunch. I wish the FAA would be less bureaucratic (even the word is a mouthful). Many of your suggestions were really helpful and I will try to follow up on them. I hope these discussions will be helpful for others now or in the future, they sure helped me. Thanks again!!! John RV9-A Firewall Forward ________________________________________________________________________________
Subject: Re: Medical in trouble
From: "Bob Collins" <bcollinsrv7a(at)comcast.net>
Date: Apr 26, 2006
jszantho(at)gmail.com wrote: > The flying community is truly unique. You realize you have friends you never > knew existed. John, Best of luck to you and working on the RV will, at times, be tough... or bittersweet is perhaps a better word. The minute you sell it, you lose touch with the RV community. Losing flying privileges is bad....losing a community is worse. What you and I -- and others -- are going to have to figure out...is how to build an RV and get it flight tested and hangared etc., when it isn't going to be hours. Doesn't make sense buying or renting a hangar.... so we'll need that RV FLYING community to really help us out. -------- Bob Collins St. Paul, Minn. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=30857#30857 ________________________________________________________________________________
Date: Apr 26, 2006
From: "Tim Bryan" <flyrv6(at)bryantechnology.com>
Subject: Re: Medical in trouble
John, do you mind sharing what the medication is? Only so we know if it is ever mentioned to any of us. thanks Tim ________________________________________________________________________________
Subject: The Fourth Annual Rebel's Bluff Fly-In
Date: Apr 26, 2006
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
Posted on behalf of Les Featherston. I can vouch that he puts on a real nice fly-in. Be there or be square. Vince ************************************************************************* *********************************************************************** The Fourth Annual Rebel's Bluff Fly-In Les Featherston will host the Fourth Annual Rebel's Bluff Fly-In on Saturday, May 6th at 10:00 A.M. until 5:00 P.M. Come on over for a great day of flying and visiting pilots from all over the Midwest. All aircraft are welcome and we should see some very nice homebuilt RV's, lovely antiques, Cessna, Beech, Piper, etc. And I wouldn't by surprised by a few "surprise" ships. Rebels Bluff Airstrip is located 2 miles NNE of Mt. Vernon Municipal Airport (2MO) and 2 =BD miles west of the town of Mt. Vernon, Missouri. The lat/longs are N37 06.1 W93 52.2. The runways 14/32 are 2,200'of very nice sod. Right traffic is preferred to RW14. Use UNICOM 122.9, and announce "Mt. Vernon Traffic, landing at Rebel's Bluff". AvGas is available. The best news is food. "The ladies at FBC will be serving lunch as a fund raiser" and promise some scrumptious items on the menu. Your R.S.V.P. really helps with the planning and is greatly appreciated. Last but not least, the Rain Date is Saturday, May 13th. See Ya'll at the 'Bluff. Les Featherston #17-4666-4663 (home), #-425-3595 (cell) ________________________________________________________________________________
Date: Apr 26, 2006
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: RV-List:
Good advice. If it is something that might take a special issuance, there are folks such as Virtual Flight Surgeons that supposedly facilitate getting all the right data to the FAA and through their system. I've been grounded with kidney stone in the past and AOPA was very helpful in getting my medical restored once the condition had passed. Quoting marknlisa(at)hometel.com: > > John, > > Please, please, please listen to the good advice from the group and finish > your project. You'll never forgive yourself if you don't build that -9 > and see it fly, especially after all the hard work you've invested. The > worst-case is you can't renew your FAA medical and someone has to fly with > you. There are two individuals in my area in that situation and they fly > regularly -- all they need is a qualified pilot to ride along and log the > time. Somehow they never seem to have trouble finding a volunteer, even > on short notice! > > Definitely contact AOPA for help with your medical issue vis-a-vis the > FAA. You might be surprised what you can get waived if you follow the > right procedure. AOPA has been helping folks with these problems for a > long time and they have a staff of experts for just that purpose. ________________________________________________________________________________
From: "Szantho B. Szantho" <jszantho(at)gmail.com>
Subject: Re: Medical in trouble
Date: Apr 26, 2006
Tim Bryan asked me about the medication I take. If any of you guys want to know, send me an e-mail and I will send it to your mailbox. John ________________________________________________________________________________
From: "Cleaveland Aircraft Tool" <mail(at)cleavelandtool.com>
Subject: New fuel valve handle
Date: Apr 26, 2006
We have designed a new fuel handle for those using Van's stock fuel valve. They will be available in a few weeks for $47. See our website for more info or to pre-order at: http://www.cleavelandtoolstore.com/prodinfo.asp?number=3DRVFS1 Mike Mike Lauritsen Cleaveland Aircraft Tool 2225 First St. Boone, Iowa 50036 515-432-6794 mike(at)cleavelandtool.com ________________________________________________________________________________
Date: Apr 26, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
>posted by: "Steve Glasgow" > >Just because something has never happened before doesn't mean that >it can't happen tomorrow. Witness 9/11. No KIDDING! Daaaaa, AND you invoke 9/11 somehow to make a point. Shame on you! Not only is that distastefully its ridiculous. Look your chance of flying your RV into the ground and killing yourself is way way way greater than being sued, so my suggestion is dont sell your plane or even fly at all, it is safer. No one said that you could NOT be sued but the risk is small with some common sense precautions. When talking legal issues you have to be rational and think in terms of RULE OF LAW. Get a Lawyer, specifically an aviation lawyer who understands product liability; ask them to get a perspective. Just get educated and cover your A, that's all. Let me repeat for you, legal precedence indicates the sensational fear of lawsuit is OVER hyped, although it is possible. Any thing is possible. Heck, Piper got sued for a 65 year old Piper Cub because the plane did not have shoulder harness. Of course the idiot pilot took off on a closed runway and hit a truck. So sure someone could sue you, but their chance of winning is small if you take some precautions, that others and myself have spoke to which I will not repeat. Get smart not concerned and anxious. If someone does a low level loop in a plane you built, that has changed hands three times, crashes, dies, your liability is small. Yes you may need to defend yourself, but unless they can prove you contributed to it, than the case is weak. You could counter sue them for a frivolous lawsuit. Now if the wing folded because you did not put the rivets in, than yes you are liable and should be. Van was sued for a factory RV-8 in-flight wing failure. Van prevaliled. This was a factory plane with an employee and the employees friend. A professional waiver could have all kinds of legal stipulations to cover your A. I am not going to give advice here. GET A GOOD LAWYER. Spend the time, money and effort to cover yourself per your legal council, and you can sell a RV or whatever with confidence and reduced risk of lawsuit, which statistically from legal precedence is already small (small but not non-existent). You have to weigh the risk with good counsel. I don't recommend a homemade waiver. Nuff Said. George --------------------------------- at 1¢/min. ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: Re: Interpreting Aileron Position
Date: Apr 26, 2006
After digesting all the replies, for which I thank you all, I got this idea from Phil Birkelbachs. I have adjusted the ailerons so that they are both at the same angle of attack on the assumption that they would be equally balanced in flight. Right now, when one is lined up with it's flap, the other lines up with the other flap. Seeing that they are indicating a roll to the left by their in-flight position even though I'm applying considerable roll right stick input to stay level tells me they're not balanced in this position. What I should be doing is decreasing the angle of attack on the powerful aileron, the left one, and increasing the angle of attack of the right one to get an in-flight balance position with the ailerons closer to the known neutral in-trail position. This will look funny on the ground because they won't line up with the flaps but something I can't see or measure is changing the airflow each sees & I should adjust to that. Is this reasonable? I think I'll just adjust one aileron or the other a little 'out of line' to see how this works. Dave Reel - RV8A ________________________________________________________________________________
Date: Apr 26, 2006
From: "Tim Bryan" <flyrv6(at)bryantechnology.com>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Why don't we all pitch in a dollar and get a good waiver written that we could all use. Why should we each spend the money to have these things drawn up. Tim ________________________________________________________________________________
From: "charles heathco" <cheathco(at)junct.com>
Subject: Re: Medical in trouble
Date: Apr 26, 2006
As for me, if I dont feel right, I dont fly, and if Im feeling ok, but not up to snuff, i will fly, but wont tack anyone else up with me. I think this is a paoint that Faa is missing. I would assume this is the way most of us think. If I dont feel right, I dont fly, Yes?? Charlie Heathco ________________________________________________________________________________
From: "dick martin" <martin(at)gbonline.com>
Subject: Re: Datapoint for Fairings Speed Improvement
Date: Apr 26, 2006
Jerry, Call me at 920 619 6968 and I will explain in detail. It would take a week to type out an explanation on email. Dick Martin RV8 N233M the fast one ----- Original Message ----- From: "Jerry Grimmonpre" <jerry(at)mc.net> Sent: Wednesday, April 26, 2006 7:43 AM Subject: Re: RV-List: Datapoint for Fairings Speed Improvement > > Dick ... > Can you expand on the description starting with: > > As a general statement, the upper gear to fuse fairing will be >> more efficient when it has a lead is between 1 and 2 inchs long with a >> long >> ,narrow taper to the gear leg. > > Pictures would be good if you have them. > > Thanks ... > Jerry Grimmonpre' > RV8A Electrical > > >> >> Mark, >> Welcome to the world of faster airplanes. A giant engine helps, but a >> CLEAN, LIGHT airplane always wins the speed contests. I have an RV8 and >> during my initial testing, I experimented with various gear leg to >> fuselage >> fairings and found that a considerable speed increase is available at >> this >> junction. An easy way to test the efficiency of the fairing is to spray >> some waste oil on the fuselage in the area where the landing gear >> attachs, >> and then go up an fly the airplane. If the fairing is efficient, you >> will >> see perfectly shaped oil lines on the side of the fuselage depicting the >> airflow (just like the pictures in the technical magazines). If the flow >> lines are erattic, you know you need to try some variations in shape of >> the >> fairing. As a general statement, the upper gear to fuse fairing will be >> more efficient when it has a lead is between 1 and 2 inchs long with a >> long >> ,narrow taper to the gear leg. A side note: some RV8s experience a >> sliight >> tail shudder when stall landing. If the above fairing is correct, the >> tail >> shudder disappears. >> Good luck with your project and hope to see you and others in the Air >> Venture Races. >> Dick Martin >> RV8 N233M >> the fast one > > > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Apr 26, 2006
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
In a message dated 4/26/2006 4:50:21 P.M. Pacific Daylight Time, flyrv6(at)bryantechnology.com writes: Why don't we all pitch in a dollar and get a good waiver written that we could all use. Why should we each spend the money to have these things drawn up. ================================ They're readily available. Would you like one? GV (RV-6A N1GV O-360-A1A, C/S, Flying 780hrs, Silicon Valley, CA) ________________________________________________________________________________
Subject: Re: Medical in trouble
From: "Bob Collins" <bcollinsrv7a(at)comcast.net>
Date: Apr 26, 2006
When dealing with medication, a lot of times what the FAA is looking is side effects. We all know, of course, how important it is to "stay ahead of" our machines. That's not easy sometimes with a clear head. Some of these meds are aimed directly at the brain and are intended to slow or change the signals it gets. It's very hard to stay ahead of a machine at that point. Even though we might feel "fine." The perfect solution? Meds with no side effects. But then they probably wouldn't work. -------- Bob Collins St. Paul, Minn. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=31003#31003 ________________________________________________________________________________
From: "Steve Glasgow" <willfly(at)carolina.rr.com>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Date: Apr 27, 2006
Don't you dare shame me. The idea of this forum is to make helpful suggestions about various topics, not to shame people because they post a message you personally do not agree with. Steve Glasgow ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: Mysterious Oil Leak
Date: Apr 27, 2006
Whenever I remove the nosewheel fairing cap to check the security of my RV8A nose gear leg fairing, I notice a ring of oil collected atop the nosewheel rotation limit stop. I can't think of any possible source for oil down here. Grease yes, but not oil. Has anyone observed a similar mystery? Has anyone got a clue? Dave Reel - RV8A 10 hrs ________________________________________________________________________________
From: "Belue, Kevin" <KBelue@drs-tem.com>
Subject: Mysterious Oil Leak
Date: Apr 27, 2006
I've noticed when I change oil, if I get any oil in the nose gear mount (the boxed section where the nose gear goes into the engine mount) oil will appear at the bottom of the gear leg for a long time. I spray engine cleaner in this boxed area and spray it with a high pressure hose to clean it out. Kevin D. Belue ________________________________________________________________________________
Date: Apr 27, 2006
From: "James Clark" <jclarkmail(at)gmail.com>
Subject: Re: Mysterious Oil Leak
I have seen something similar on a friends RV9A. I suspect there is some low pressure/suction in the area that is pulling a drop or two from the engine compartment down the faring. Have not investigated further. James ________________________________________________________________________________
Date: Apr 27, 2006
From: sportav8r(at)aol.com
Subject: Re: Mysterious Oil Leak
Ditto. The spilled engine oil weeps out of the rivet holes all along the fairing as well as out the bottom, onto the pant. Disgusting looking, but really cool how it shows the air streamlines ;-) I try to avoid spilling any oil into the gear/engine mount for this reason, but when cleaning the high pressure screen, it's hard not to drop some down there. -Stormy ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Apr 27, 2006
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Here is the text of the one I have used. Now let's all parse the language and argue about how to make it better and impenetrable by clever lawyers. As Former President Clinton said, define "is". ;o) EXPERIMENTAL-AMATEUR BUILT AIRCRAFT SALES AGREEMENT THIS FORM SUPPLEMENTS, BUT DOES NOT REPLACE, FAA AC FORM 8050-2. THE FAA REGISTRATION-NUMBER OF THIS AIRCRAFT IS NXXXX. THIS AIRCRAFT WAS CONSTRUCTE D IN ACCORDANCE WITH PLANS SERIAL NUMBER XXXXX, AND IS A FACSIMILE OF AN AIRCRAF T KNOWN AS AN XX-XX. THE AIRCRAFT IS DESCRIBED IN GREATER DETAIL ON SHEET 2 OF THIS AGREEMENT. The experimental-amateur built aircraft being sold is not designed and/or built to meet any defined standards of airworthiness as are =E2=80=9CStanda rd Aircraft=E2=80=9D . This aircraft does not have an FAA Form 317 Statement of Conformity on file, as there are no FAA approved data with which to conform. In the case of experimental-amateur built aircraft, the registered owner(s) is/are the experimenter(s). Most parts of this aircraft were not built in permanent j igs and, as such, may not be directly interchangeable with like parts on other aircraft of the same facsimile. The original builder of this experimental aircraft may possess a repairman=E2=80=99s certificate for purposes of main taining and performing condition inspections on this aircraft only, although he/she may not be a professional mechanic nor possess an FAA A&P license. FAA records lis t the registered owner(s) as the manufacturer of an experimental-amateur buil t aircraft as the manufacturer and, as manufacturer, the registered owner(s) is/are free to make any modifications or changes to the design as they see f it, although notification of major alterations have and must be made to the FAA . This aircraft is an example of the builder/owner=E2=80=99s creative abilit y and was built for their education and recreation. Upon sale, the newly registered owner of this experimental-amateur built aircraft in fact will be considere d its new manufacturer. As of the date of sale, the new owner becomes responsible for its aerodynamic and structural function and/or concept. Th e new owner is responsible for the performance, fit and/or purpose of every part/ piece on the aircraft. No warranty of any kind, either expressed or implied, is made to the Purchaser or anyone else as to the merchantability or airworthiness of NXXX X. This experimental-amateur built aircraft is sold on an =E2=80=9CAS IS, WHERE-IS a nd WITH ALL FAULTS PRESENTLY INCORPORATED=E2=80=9D basis. Flying poses certain inherent risks that can result in serious injury or death. Any person who pilots or acts as passenger in this experimental air craft does so at his/her own risk. Because of the sale hereof and in receipt of other good and valuable consideration, the Purchaser/new Owner hereby Waive s and Releases the seller(s) from any and all Demands, Claims of every kind, including but not limited to, Liability, Breach of Warranty or Negligence, which the Purchaser, owner , pilot, and/or passenger in this experimental aircraft may have. This Release and Waiver is binding on all Heirs, Persona l Representatives and Assigns of the Purchaser, Subsequent Owners, Pilots and /or Passengers. As Purchaser/new Owner, I accept the terms of this Sales Agreement for the experimental-amateur built aircraft identified above and agree to be bound by the above stipulations. I agree that any subsequent sale of this aircraft will be made with the same disclosures, agreements and assurances listed ab ove as a minimum. Name of Purchaser/new Owner: Name of Purchaser/new Co-Owner: Purchaser=E2=80=99s Address: Co-Owner=E2=80=99s Address: Signature of Purchaser: Signature of Co-Owner: As Seller(s), on this XXth day of Month, XXXX in the County of XXXX, State of XX, I/We do hereby sell, grant, transfer, release and deliver all rights , title, interest, possession and responsibility for/to such experimental aircraft to the above Purchaser and acknowledge the receipt of a Cashier =E2=80=99s Check in the amount of $XXXX.00, payable to the Seller. No sales tax was collected pursuant to State Law and this becomes the responsibility of the Purchaser. Total Hours Engine and Airframe at time of sale XXX.X Name of Seller/Owner: Name of Seller/Co-Owner: Seller/Owner=E2=80=99s Address: Seller/Co-Owner=E2=80=99s Address: Signature of Seller/Owner: Signature of Co-Owner: Witness: Signature of Witness: This Bill of Sale is to be signed by all parties. The FAA dropped the requirement for notarizing in 1972. Seller retains the original and a cop y is given to the Purchaser/new Owner. Seller sends a copy of the original docu ment to the FAA along with Cancellation of Registration FAA AC FORM 8050-73. ________________________________________________________________________________
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Interpreting Aileron Position
Date: Apr 27, 2006
On 26 Apr 2006, at 18:33, DAVID REEL wrote: > > After digesting all the replies, for which I thank you all, I got > this > idea from Phil Birkelbachs. I have adjusted the ailerons so that > they > are both at the same angle of attack on the assumption that they > would > be equally balanced in flight. Right now, when one is lined up with > it's flap, the other lines up with the other flap. Seeing that > they are > indicating a roll to the left by their in-flight position even > though > I'm applying considerable roll right stick input to stay level > tells me > they're not balanced in this position. What I should be doing is > decreasing the angle of attack on the powerful aileron, the left > one, > and increasing the angle of attack of the right one to get an in- > flight > balance position with the ailerons closer to the known neutral in- > trail > position. This will look funny on the ground because they won't > line up > with the flaps but something I can't see or measure is changing the > airflow each sees & I should adjust to that. > > Is this reasonable? I think I'll just adjust one aileron or the > other a > little 'out of line' to see how this works. If you are talking about adjusting the length of the various aileron pushrods, as a way to fix your roll trim problem, I believe you are wasting your time. If you have the aileron trim in neutral, and you let go of the stick, the ailerons will move to the position that balances the forces on the left and right ailerons. If you screw around with the pushrods, you might move both ailerons up a bit, or down a bit, but I don't believe you will make any significant difference the relative positions between the two ailerona. Go ahead, try it if you want. But don't be surprised if it doesn't fix your problem. The aileron positions are a symptom of the real problem. They are not the problem. You need to find the underlying problem, rather than trying to treat the symptoms. Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
From: "Dan Morrow" <DanFM01(at)butter.toast.net>
Subject: Re: RE: Lawsuits against builders (Was AOPA hates homebuilts?)
Date: Apr 27, 2006
In my earlier e-mail on this topic I stated that I had read that the builder was named as a defendant in the John Denver case. Mr. gmcjetpilot expressed doubt and asked for references. After searching around I found one on the EAA website. The following two paragraphs are copied from the website. "In today's litigious society, there is, perhaps, some justification for the anxiety homebuilders express about theoretical financial loss arising out of their efforts. Experience, to date, does not support these fears. I checked carefully with other aviation attorneys and insurers, and the number of lawsuits that have actually been litigated against homebuilders is minuscule. "Moreover, at the time of this writing there doesn't appear to be any instance in which an actual case was filed, tried, reduced to judgment, and collected against a homebuilder. There is one pending arising out of the John Denver crash, but that case is focused against the fuel valve manufacturer and its retailer, who appears to have coverage, although the builder is also being sued." The lawsuit was later settled out of court. News reports I have read don't give a complete list of the parties to the settlement, so I cann't say how the builder, Adrian Davis, fared. Details of the settlement were apparently not released, as is common in such cases. You can reach the source for the above quotation as follows: Navigate to members.eaa.org. Login--you must be an EAA member to do this. Follow the following links: building,homebuiders HQ->Selling/Buying,Articles->Part 5. Or for a short cut navigate to members.eaa.org. Login and enter "john denver" in the search box with the quotes. Click on the link to Part 5 Liability etc. Scroll down near the bottom to find the quoted text. The EAA web site has some extensive articles on legal issues for homebuilders. In particular if you follow the first method of navigation above, you get to page with links to 8 or 9 legal topics related to the homebuilder. One of them, Part 3, discusses waivers and releases. The author is sceptical of their value. The long and short of all this seems to me to be like this: 1. There is no legal impediment to prevent lawsuits against a homebuilder before or after he sells the aircraft. 2. Lawsuits after the sale are rare. The lawyers don't have a way of counting the number of lawsuits, however, so it's impossible to quantify the risk. 3. If you are Daddy Warbucks with lots of dough and own a homebuilt, you might consult a lawyer. 4. For the rest of us the risks are low compared with the ordinary risks of aviation. ________________________________________________________________________________
From: "Jim Pleasants" <jpleasants(at)bellsouth.net>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Date: Apr 27, 2006
Fellow listers: I hate to get involved in this, but I can't hold off any longer. Waiver forms are, in my opinion, just as good as Yogi Berra allegedly said of oral contracts: "Not worth the paper they're written on." I say this after 40+ years of law. I am unaware of any lawyer whose acumen I respect using any of these, or if they are using them because their client insists, opining that they have any immunizing effect at all. Having said that, if you want to prepare one, and insist the buyer sign it, have at it. It may make you feel better, but don't delude yourself into thinking that it adds any protection from suit or recovery. Indeed, it may have the opposite effect -- can't you just see that mean ol' plaintiff's lawyer asking the jury why the builder was so worried about the safety of his aircraft that he felt it necessary to get a signature on such a paper? It might be more efficient to wave a cross at any lawyer who shows up, or bury a silver bullet in the structure. Somewhere in this thread, the subject of asset protection came up. I urge each one of you to talk to a knowledgeable lawyer before you take any steps in that direction, and be sure to get him to explain the fraudulent transfer laws in your state. Judges and juries get very upset if they smell anything of that kind. And before you flame me, please take a few deep breaths and make sure you are taking your medicine. Jim Pleasants ----- Original Message ----- From: <Vanremog(at)aol.com> Sent: Thursday, April 27, 2006 11:52 AM Subject: Re: RV-List: Re: Lawsuits against builders (Was AOPA hates homebuilts?) -- ________________________________________________________________________________
From: "John Helms" <jhelms(at)nationair.com>
Subject: Chopping up your plane for sale doesn't help.
Date: Apr 27, 2006
I've posted this information before, but understand that a customer called one of my agents about this issue again today. So, I think it must not be too soon to post this again. For purposes of this discussion I refer to Van's Aircraft as the manufacturer, and the builder as the assembler. I'm not trying to step on any toes. only trying to help everyone understand better. When selling your plane, the liability that you would have as the assembler of the airplane would not be lessened by "parting it out" and selling the various parts to different people. Actually, it could, in essence, increase the liability exposure. Selling the wings to one person, the engine to another, etc. could potentially increase your exposure to liability. If any of the planes which your former parts go into crash, then you could be sued. Your part which is now in that plane wouldn't even necessarily have had to fail. Families often sue despite the cause of the crash or facts of the case. Their loved one couldn't have been at fault. In my opinion, the cost of defending the lawsuit could be as bad or worse than the eventual judgement. So, having 4 or 5 aircraft out there with your former parts and the potential to crash broadens the risk of a lawsuit being brought against you. A very few aviation insurance policies cover "liability for the sale of the aircraft" (AIG provides that but only for production aircraft, and AVEMCO offers it on all their policies) but that is designed to cover any aircraft owner from lawsuits arising out of poor maintenance and the like. It was not designed to cover your liabilities as the assembler of a kit aircraft. In fact, AVEMCO's coverage for sale of the aircraft even states that it is intended to provide coverage arising out of your "ownership, maintenance, and use" of the aircraft. It specifically does not state it covers liability arising out of "assembly of" or "manufacture of" the aircraft. As previously mentioned today on this forum, verbal and even written agreements to waive liability are pretty much worthless. The very best things which you as the assembler of the plane can do to lessen your exposure are: 1. Follow the plans exactly, don't substitute parts, or change anything. Any modification or substitution could be increasing your liability by crossing over into the manufacturer or engineering type liability areas. Obviously, there are differences amongst all your planes, and places in the plans where it calls for you to make a choice (i.e. tip up/slider) or whether or not to install an autopilot. In any event, if they exist I'd suggest following the plans or recommendations as closely as possible. 2. Have a third party A+P do an annual as the pre-buy. Don't do it yourself as the builder or if you're an A+P or allow an A+P who might be buying it from you do it. This applies to any airplane (production or homebuilt) that you might sell. The annual is a declaration by that A+P attesting to the airworthiness of the plane for another year. Having it be a third party will support your position if you are sued, and you might be able to even sue them if there was a problem which you were sued for successfully. Or, the buyer might sue the A+P and not you (although they'd likely sue both of you.) 3. Maintain the airplane well. 4. Don't own anything (and all the other legal things you can do to make yourself less of a target to go after). A lawyer once told me that the 2nd best thing you can do is have a ton of coverage, the best thing is to have none (and no assets). While product liability coverage exists, it exists for manufacturers. It is not realistic to believe it'd be affordable for any of you for having built one plane. It'd cost more than the value of your plane. Anything is insurable, but the starting price for special stuff like that thru Lloyd's would be in the multiple tens of thousands of $'s if not $50,000. One might as well make their plane into paperclips. Just please don't think that parting your plane out for sale achieves a lessening of liability exposure. John "JT" Helms Branch Manager NationAir Insurance Agencies, Inc. ***Notice to All Recipients*** Please be advised that we cannot bind, modify, or cancel coverage via the Internet, email or voicemail. Please call our office at (877) 475-5860 to speak with a NationAir Representative. Thank you for your cooperation. ***Confidentiality Notice*** The Information in this email and any attachments therein is intended for the addressee(s) only and may contain confidential information. If you are not the intended recipient of this email, you are hereby notified that any dissemination, distribution or copying of this email and/or any attachments thereto is strictly prohibited. If you receive this email in error, please notify us immediately by email, attaching the original message, and delete the original message from your system. ________________________________________________________________________________
From: "John Jessen" <jjessen(at)rcn.com>
Subject: RE: RV10-List: New fuel valve handle
Date: Apr 27, 2006
See if the picture below gets through... _____ From: owner-rv10-list-server(at)matronics.com [mailto:owner-rv10-list-server(at)matronics.com] On Behalf Of Mike Lauritsen - Work Sent: Wednesday, April 26, 2006 1:24 PM Subject: RV10-List: New fuel valve handle We have designed a new fuel handle for those using Van's stock fuel valve. They will be available in a few weeks for $47. See our website for more info or to pre-order at: http://www.cleavelandtoolstore.com/prodinfo.asp?number=RVFS1 RV Fuel Selector Handle Mike Mike Lauritsen Cleaveland Aircraft Tool 2225 First St. Boone, Iowa 50036 515-432-6794 mike(at)cleavelandtool.com ________________________________________________________________________________
From: MLWynn(at)aol.com
Date: Apr 27, 2006
Subject: Platenut Life
Hi all, Do I need to worry about platenuts loosing their locking ability from running screws in and out too frequently? Anyone know what the life expectancy is in terms of this? I am working on the tanks and was scratching my head about when to rivet on the platenuts. Regards, Michael Wynn RV 8 Wings (tanks) San Ramon, CA ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Re: Lawsuits against builders (Was AOPA hates homebuilts?)
Date: Apr 27, 2006
I'm not a lawyer but I thought that 'fraudulent transfer laws' only applied after the tort was commited. Bruce www.glasair.org -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Jim Pleasants Sent: Thursday, April 27, 2006 2:13 PM Subject: Re: RV-List: Re: Lawsuits against builders (Was AOPA hates homebuilts?) Fellow listers: I hate to get involved in this, but I can't hold off any longer. Waiver forms are, in my opinion, just as good as Yogi Berra allegedly said of oral contracts: "Not worth the paper they're written on." I say this after 40+ years of law. I am unaware of any lawyer whose acumen I respect using any of these, or if they are using them because their client insists, opining that they have any immunizing effect at all. Having said that, if you want to prepare one, and insist the buyer sign it, have at it. It may make you feel better, but don't delude yourself into thinking that it adds any protection from suit or recovery. Indeed, it may have the opposite effect -- can't you just see that mean ol' plaintiff's lawyer asking the jury why the builder was so worried about the safety of his aircraft that he felt it necessary to get a signature on such a paper? It might be more efficient to wave a cross at any lawyer who shows up, or bury a silver bullet in the structure. Somewhere in this thread, the subject of asset protection came up. I urge each one of you to talk to a knowledgeable lawyer before you take any steps in that direction, and be sure to get him to explain the fraudulent transfer laws in your state. Judges and juries get very upset if they smell anything of that kind. And before you flame me, please take a few deep breaths and make sure you are taking your medicine.


April 18, 2006 - April 27, 2006

RV-Archive.digest.vol-rw