RV-Archive.digest.vol-ry

May 13, 2006 - May 30, 2006



      > RV-6, and in excellent condition.
      >
      > $125 US OBO plus shipping. ($228 new from Van's)
      >
      > Curt
      > RV-6 C-GACR
      >
      >
      > 
      
      
________________________________________________________________________________
Date: May 13, 2006
From: sarg314 <sarg314(at)comcast.net>
Subject: panel installation - radio trays
I am getting down to the little details on panel design and am wondering about clearance between instruments and my radio stack. The "stack" is only an SL-30 radio and a KT-76C transponder. I have the trasponder in hand, but not the radio yet. (I guess it's about time I rodered it.) I gather these are normally mounted in a some sort of framework that attaches to the panel but I've never seen one of these. How close can I realistically place an instrument to this support frame? Does any one have any photos on their web site that I can look at? Thanks, -- Tom Sargent RV-6A ________________________________________________________________________________
Date: May 13, 2006
From: Walter Tondu <walter(at)tondu.com>
Subject: Re: panel installation - radio trays
On 05/13 7:26, sarg314 wrote: > I am getting down to the little details on panel design and am wondering > about clearance between instruments and my radio stack. The "stack" is > only an SL-30 radio and a KT-76C transponder. I have the trasponder in > hand, but not the radio yet. (I guess it's about time I rodered it.) > > I gather these are normally mounted in a some sort of framework that > attaches to the panel but I've never seen one of these. How close can I > realistically place an instrument to this support frame? Does any one > have any photos on their web site that I can look at? I used 3/4" al angle for the frame, behind and attached to the panel. I suppose you could use 1/2" al angle too. See pics and desc here. Look for entry dated 6/14/04 http://www.rv7-a.com/avionics.htm -- Walter Tondu http://www.rv7-a.com Flying! ________________________________________________________________________________
Subject: Re: panel installation - radio trays
From: "Rick Galati" <rick6a(at)yahoo.com>
Date: May 14, 2006
Tom, Installing a radio stack is fairly straightforward. I used .032 aluminum angle stock to tie the trays together and to the back of the panel. The two photographs (of my Garmin 430 stack) should give you a fairly good idea of a typical installation whether for 2 trays or 5 trays....the idea is about the same. http://img101.imageshack.us/img101/3903/radiostack029bh.jpg http://img101.imageshack.us/img101/527/radiostack031zh.jpg Rick Galati RV-6A "Darla" 124 hours .......I gather these are normally mounted in a some sort of framework that attaches to the panel but I've never seen one of these. How close can I realistically place an instrument to this support frame? Does any one have any photos.........I can look at?..........Tom Sargent ] Read this topic online here: http://forums.matronics.com/viewtopic.php?p=34519#34519 ________________________________________________________________________________
Date: May 14, 2006
From: Bobby Hester <bobbyhester(at)charter.net>
Subject: Re: panel installation - radio trays
Check near the bottom of this page: http://members.hopkinsville.net/bhester/FinishKitAssyPg2.htm Please update your address book with my new email address: bobbyhester(at)charter.net Surfing the Web, Highspeed now, from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse-XPO360 engine :-) sarg314 wrote: > >I am getting down to the little details on panel design and am wondering >about clearance between instruments and my radio stack. The "stack" is >only an SL-30 radio and a KT-76C transponder. I have the trasponder in >hand, but not the radio yet. (I guess it's about time I rodered it.) > >I gather these are normally mounted in a some sort of framework that >attaches to the panel but I've never seen one of these. How close can I >realistically place an instrument to this support frame? Does any one >have any photos on their web site that I can look at? > > >Thanks, >-- >Tom Sargent >RV-6A > > > > > > > > > ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: Painter Feedback Sought
Date: May 14, 2006
I'd like to hear from anyone who has had a paint job done by Alan Woodson at Brady Texas. I'm about to go down there to get my RV8A painted. Dave Reel ________________________________________________________________________________
Date: May 14, 2006
From: sarg314 <sarg314(at)comcast.net>
Subject: Re: panel installation - radio trays
Great photographs, guys. I think I get the idea. It looks like I'll have to give the radios a 1/2 to 3/4 margine around the edge. Thanks very much. -- Tom Sargent ________________________________________________________________________________
From: JEllis9847(at)aol.com
Date: May 14, 2006
Subject: Re: panel installation - radio trays
Go to www.rvwiki.org and look at "Avionics Rack" to see how I mounted the avionics in my 9-A. There are several pictures that might be helpful. Jim Ellis RV9-A, N155T taxi testing, ready for first flight ________________________________________________________________________________
Date: May 14, 2006
From: George Inman 204 287 8334 <ghinman(at)mts.net>
Subject: Looking for reviews on the Lowrance AirMap 2000C
Have you tried Lithium AA batteries in the 2000C ? They might last quite a bit longer in an emergancy power failure. >The
> >only squawks >are the batteries (4 aa) are For backup only >as they only last
> >about >an hour. -- George H. Inman ghinman(at)mts.net ________________________________________________________________________________
Date: May 14, 2006
From: "DEAN PSIROPOULOS" <dean.psiropoulos(at)verizon.net>
Subject: Inst panel hole cutting
Quick question folks: I'm finally to the point where I HAVE to cut the instrument and engine monitor display holes in my panel blanks. I thought I had some folks close by who could do that but in talking to them yesterday I discovered that they really don't have the capabilities that I need. I have a Dynon D-10 that I want to flush mount and that requires a nicely made SQUARE hole. That could probably be done with an old hand operated milling machine. The biggest problem though is the Vision Microsystems engine monitor display. Its outside edges are basically a square hole but at the corners, instead of making them 90 degrees, they transition into something like a 45 deg angle from the vertical lines to the horizontal lines. Those of you who have VM-1000 know what I'm talking about and needless to say, I'm convinced the only way to get a nice looking hole to put this display in is to have it CNC machined. Since there is no bezel that fits over the top of this funny looking hole, it has to be done right the first time or I'll be looking at the botched workmanship every time I check my engine parameters. Any suggestions about how I'm might achieve this. Is there anyone east of the Mississippi river that has machining templates to do this or can I do it in my shop with common tools somehow? Thanks. Dean Psiropoulos RV-6A N197DM Trying to get the wiring finished ________________________________________________________________________________
From: "J. R. Dial" <jrdial@hal-pc.org>
Subject: Painter Feedback Sought
Date: May 14, 2006
I had my plane done there and I am very satisfied. He has done several others as a result of mine. Mine is the yellow and red RV6 that is on his web-site and if you have any questions email me off list and I will give you my phone number or email off list. Dick Dial N89DD -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of DAVID REEL Sent: Sunday, May 14, 2006 9:02 AM Subject: RV-List: Painter Feedback Sought I'd like to hear from anyone who has had a paint job done by Alan Woodson at Brady Texas. I'm about to go down there to get my RV8A painted. Dave Reel ________________________________________________________________________________
Date: May 14, 2006
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Handheld GPS batteries
Find someone with >2300 mAh NiMH batteries to see how long they last. You can get 2500 mAh AAs at Walmart now and with a 15 minute charger (Energizer), you can recharge them quickly and often Ron Lee > >The
> >only squawks > >are the batteries (4 aa) are For backup only > >as they only last
> >about > >an hour. ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: Handheld GPS batteries
Date: May 14, 2006
In the current (June 2006) issue of Popular Science, pg. 22, they did a test of batteries in a digital camera. Since the requirements are not the same as for a GPS, these results may not translate well, but they are interesting. Conventional alkaline batteries: 533 shots Duracell Powerpix (Nickel Oxy Hydroxide): 920 shots Panasonic Oxyride (Nickel Oxy Hydroxide): 990 shots Energizer e2 Lithium: 3,107 shots Although the lithium batteries cost twice as much, they were obviously the best deal. Terry -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Ron Lee Sent: Sunday, May 14, 2006 11:49 AM Subject: RV-List: Handheld GPS batteries Find someone with >2300 mAh NiMH batteries to see how long they last. You can get 2500 mAh AAs at Walmart now and with a 15 minute charger (Energizer), you can recharge them quickly and often Ron Lee > >The
> >only squawks > >are the batteries (4 aa) are For backup only > >as they only last
> >about > >an hour. ________________________________________________________________________________
Date: May 14, 2006
From: Charles Reiche <charlieray(at)optonline.net>
Subject: Re: panel installation - radio trays
As an avionics installer by trade, I would recommend placing like .060" sheet between the trays when you design where the go, If you arent using a avionics cooling fan like one from troll avionics.... I recommend leaving that gap for some air flow.. you may think that a 1/8" gap between radios is unsightly but they will last longer if they are allowed to breath, especially in a non force-cooled installation. Position the trays with the .060 sheet and then take it out when doing final assembly of your racks. Never never never and never place forced cooling into a radio from something like a NACA duct on the side of the airframe. I recently pulled a 210 apart to install a Garmin GTX 330 and found that the 530 was being supplied cooling air from outside the airplane via a ram air vent on the sidewall. For S's and G's I took the cover off the 530 and looked inside, I found pieces of grass and corrosion all over the thing that will lead to its early demise. Cooling air has to be dry! And from inside the airplane. Charlie > Tom, > > Installing a radio stack is fairly straightforward. I used .032 aluminum > angle stock to tie the trays together and to the back of the panel. The > two photographs (of my Garmin 430 stack) should give you a fairly good > idea of a typical installation whether for 2 trays or 5 trays....the idea > is about the same. > http://img101.imageshack.us/img101/3903/radiostack029bh.jpg > http://img101.imageshack.us/img101/527/radiostack031zh.jpg > > Rick Galati RV-6A "Darla" 124 hours > > > .......I gather these are normally mounted in a some sort of framework > that attaches to the panel but I've never seen one of these. How close > can I realistically place an instrument to this support frame? Does any > one have any photos.........I can look at?..........Tom Sargent ________________________________________________________________________________
Date: May 13, 2006
Subject: Re: Lightspeed EI installation
From: Doug Weiler <dcw(at)mnwing.org>
> > You need to rotate the prop (or flywheel) somewhat quickly to get it to > fire. I suspect the issue you're seeing is that you're not moving it > quickly enough. My experience with my Plasma II was that if you don't > rotate the prop/flywheel quickly enough during the phase test, you won't see > the coils firing. > > Otherwise, Klaus should be able to help you. Give him a call on the > phone...contact info at the bottom of this page: > http://www.lightspeedengineering.com/ > > Where are you located? If you're anywhere near SoCal I could probably give > you a hand. Thanks for the offer Dan, except I am way out here in Minnesota. I think you are right and affirmed by Alex that rotating the ring gear by hand won't do it. I'll proceed and check everything as instructed and hopefully it will fire up when finished. Thanks Doug ________________________________________________________________________________
From: "JIM" <perfeng(at)3rivers.net>
Subject: Re: Inst panel hole cutting
Date: May 14, 2006
Dean, An easy way to do it using "common tools" is to measure and make your own template. Before you undertake several hours of measuring and layout you might try contacting the technical or production department and ask them if they have production drawings or 1:1 templates available. If not there are several ways in which to transfer your demensions to your template. You can either make the deminsions directly to a sheet of aluminum or draw it out on vellum and trace it using carbon paper backing. Either way using a piece of Al or very thin polycarbonate the same face size as your panel area will allow you to position and size the unit along with allowing you to make all your cuts and trial fit prior to actually cutting your panel. A good adjustable protactor saves lots of time laying out the off angles used. Just be sure you have the spacing in your sub. Oh BTW, a good machinist don't need no stinking CNC! :) Jim Duckett RV-7A N708JD ----- Original Message ----- From: "DEAN PSIROPOULOS" <dean.psiropoulos(at)verizon.net> Sent: Sunday, May 14, 2006 12:01 PM Subject: RV-List: Inst panel hole cutting > > > Quick question folks: > > I'm finally to the point where I HAVE to cut the instrument and engine > monitor display holes in my panel blanks. I thought I had some folks > close > by who could do that but in talking to them yesterday I discovered that > they > really don't have the capabilities that I need. I have a Dynon D-10 that > I > want to flush mount and that requires a nicely made SQUARE hole. That > could > probably be done with an old hand operated milling machine. The biggest > problem though is the Vision Microsystems engine monitor display. Its > outside edges are basically a square hole but at the corners, instead of > making them 90 degrees, they transition into something like a 45 deg angle > from the vertical lines to the horizontal lines. Those of you who have > VM-1000 know what I'm talking about and needless to say, I'm convinced the > only way to get a nice looking hole to put this display in is to have it > CNC > machined. Since there is no bezel that fits over the top of this funny > looking hole, it has to be done right the first time or I'll be looking at > the botched workmanship every time I check my engine parameters. Any > suggestions about how I'm might achieve this. Is there anyone east of the > Mississippi river that has machining templates to do this or can I do it > in > my shop with common tools somehow? Thanks. > > Dean Psiropoulos > RV-6A N197DM > Trying to get the wiring finished > > > ________________________________________________________________________________
Date: May 14, 2006
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Handheld GPS batteries
I would take this a step further and look at life cycle cost. Assume Alkaline battery = $1 each (533 shots) NiMH battery = $3.50 each (900 shots assumed) e2 Lithium battery = $3.50 each 3107 shots) Also assume only one battery is needed. Cost per shot then is: Alkaline = $1.00/533 = 0.187 cents/shot e2 Lithium = $3.50/3107 = 0.113 cents/shot Yes the Lithium is better than alkaline. But wait, we have examined the NiMh which is at first glance $3.50/900 = 0.389 cents/shot but since it can be recharged hundreds of times (let's be conservative and only use 300) then we are at 0.389/300 = 0.0013 cents/shot. Even adding in the charger cost makes the NiMh much better. Ron Lee >In the current (June 2006) issue of Popular Science, pg. 22, they did a test >of batteries in a digital camera. Since the requirements are not the same as >for a GPS, these results may not translate well, but they are interesting. > >Conventional alkaline batteries: 533 shots >Duracell Powerpix (Nickel Oxy Hydroxide): 920 shots >Panasonic Oxyride (Nickel Oxy Hydroxide): 990 shots >Energizer e2 Lithium: 3,107 shots > >Although the lithium batteries cost twice as much, they were obviously the >best deal. > >Terry ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Rotating the Tires
Date: May 14, 2006
I finished my condition inspection yesterday but deferred pulling the wheels. A visual inspection indicated that the brakes are in good shape, and the tires have plenty of tread left, but it soon will be time to rotate the tires left to right again, and when I do that, I'll re-pack the wheel bearings. Anyway, the point is that whenever I do this, it seems to take forever. You'd think it would be doable in a couple of hours, but for me it seems to take a half day. Pulling the wheelpants, extracting the cotter pins on the axle nuts, pulling loose the brake calipers, alternately jacking up one side of the plane, then the other, removing a wheel and putting the axle up on wood blocks. Then, it is time to let the air out of the tubes, split the wheels, clean and pack the bearings, and reverse the process. It takes forever... Which is why I deferred it yesterday. I wanted to be done with the condition inspection, which turned out fine, except for a broken Adel clamp on one of the exhaust hangars. Also, I had my AI replace the mixture control thingie in the carburetor, because it wasn't sealing well and it was getting difficult to stop the engine with the mixture control. Back to the reason for the post... Are there any masters of the tire rotation task? If so, what are your suggestions, other than having everything at hand when the time comes? Suggestions appreciated. KB ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Wing Leveler
Date: May 14, 2006
While I was doing my condition inspection, I did a little poking around and discovered that it might *just* be possible to get a couple more wires out into the right wing of N46KB to run the servo for a wing leveler. Which brings me back to the old issue of which of the two common wing levelers is "best", which is a heck of a subjective issue. I like the pseudo AH feature with the Tru-Track ADI, but then again, if I got into a situation where I needed that feature, maybe it would be best if I just turned on the wing leveler? On the other hand, the EZ pilot seems to give the pilot more navigation information, but it doesn't have provide any vertical navigation or the pseudo AH. I guess the bottom line is that I'm leaning towards the EZ pilot, but I'm easily swayed. Thanks for any input. KB ________________________________________________________________________________
Date: May 14, 2006
From: Bobby Hester <bobbyhester(at)charter.net>
Subject: Re: Inst panel hole cutting
You should be able to do it like I did. I used a jig saw at first I thought that idea was crazy, but it worked great! you cut it just a little shy and file to the finish line. You can read about it on this page: http://www.geocities.com/hester-hoptown/RVSite/FinishKitAssyPg3.html Please update your address book with my new email address: bobbyhester(at)charter.net Surfing the Web, Highspeed now, from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse-XPO360 engine :-) DEAN PSIROPOULOS wrote: > >Quick question folks: > >I'm finally to the point where I HAVE to cut the instrument and engine >monitor display holes in my panel blanks. I thought I had some folks close >by who could do that but in talking to them yesterday I discovered that they >really don't have the capabilities that I need. I have a Dynon D-10 that I >want to flush mount and that requires a nicely made SQUARE hole. That could >probably be done with an old hand operated milling machine. The biggest >problem though is the Vision Microsystems engine monitor display. Its >outside edges are basically a square hole but at the corners, instead of >making them 90 degrees, they transition into something like a 45 deg angle >from the vertical lines to the horizontal lines. Those of you who have >VM-1000 know what I'm talking about and needless to say, I'm convinced the >only way to get a nice looking hole to put this display in is to have it CNC >machined. Since there is no bezel that fits over the top of this funny >looking hole, it has to be done right the first time or I'll be looking at >the botched workmanship every time I check my engine parameters. Any >suggestions about how I'm might achieve this. Is there anyone east of the >Mississippi river that has machining templates to do this or can I do it in >my shop with common tools somehow? Thanks. > >Dean Psiropoulos >RV-6A N197DM >Trying to get the wiring finished > > > > > > > > > ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Inst panel hole cutting
Date: May 14, 2006
What you want to do is find a friend that has AutoCAD and have him layout your panel on the computer. Then send the autocad file to a laser cutter and volla, instant perfect cutout panel. Wayne at www.engravers.net can cut your panel for you from your autocad file. 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 Bobby Hester Sent: Sunday, May 14, 2006 9:45 PM Subject: Re: RV-List: Inst panel hole cutting You should be able to do it like I did. I used a jig saw at first I thought that idea was crazy, but it worked great! you cut it just a little shy and file to the finish line. You can read about it on this page: http://www.geocities.com/hester-hoptown/RVSite/FinishKitAssyPg3.html Please update your address book with my new email address: bobbyhester(at)charter.net Surfing the Web, Highspeed now, from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse-XPO360 engine :-) DEAN PSIROPOULOS wrote: > >Quick question folks: > >I'm finally to the point where I HAVE to cut the instrument and engine >monitor display holes in my panel blanks. I thought I had some folks close >by who could do that but in talking to them yesterday I discovered that they >really don't have the capabilities that I need. I have a Dynon D-10 that I >want to flush mount and that requires a nicely made SQUARE hole. That could >probably be done with an old hand operated milling machine. The biggest >problem though is the Vision Microsystems engine monitor display. Its >outside edges are basically a square hole but at the corners, instead of >making them 90 degrees, they transition into something like a 45 deg angle >from the vertical lines to the horizontal lines. Those of you who have >VM-1000 know what I'm talking about and needless to say, I'm convinced the >only way to get a nice looking hole to put this display in is to have it CNC >machined. Since there is no bezel that fits over the top of this funny >looking hole, it has to be done right the first time or I'll be looking at >the botched workmanship every time I check my engine parameters. Any >suggestions about how I'm might achieve this. Is there anyone east of the >Mississippi river that has machining templates to do this or can I do it in >my shop with common tools somehow? Thanks. > >Dean Psiropoulos >RV-6A N197DM >Trying to get the wiring finished > > > > > > > > > ________________________________________________________________________________
From: "randall" <rv6n6r(at)comcast.net>
Subject: Re: Inst panel hole cutting
Date: May 14, 2006
Jigsaw, files, hacksaw, drill -- worked fine for all of us "old-timers" who built before laser cutters were in vogue. Its a bit of work but I doubt it'd take less time than drawing on CAD. Randall Henderson > DEAN PSIROPOULOS wrote: > > > > > >Quick question folks: > > > >I'm finally to the point where I HAVE to cut the instrument and engine > >monitor display holes in my panel blanks. I thought I had some folks close > >by who could do that but in talking to them yesterday I discovered that > they > >really don't have the capabilities that I need. I have a Dynon D-10 that I > >want to flush mount and that requires a nicely made SQUARE hole. That could > >probably be done with an old hand operated milling machine. The biggest > >problem though is the Vision Microsystems engine monitor display. Its > >outside edges are basically a square hole but at the corners, instead of > >making them 90 degrees, they transition into something like a 45 deg angle > >from the vertical lines to the horizontal lines. Those of you who have > >VM-1000 know what I'm talking about and needless to say, I'm convinced the > >only way to get a nice looking hole to put this display in is to have it > CNC > >machined. Since there is no bezel that fits over the top of this funny > >looking hole, it has to be done right the first time or I'll be looking at > >the botched workmanship every time I check my engine parameters. Any > >suggestions about how I'm might achieve this. Is there anyone east of the > >Mississippi river that has machining templates to do this or can I do it in > >my shop with common tools somehow? Thanks. > > > >Dean Psiropoulos > >RV-6A N197DM > >Trying to get the wiring finished > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: Rotating the Tires
Date: May 14, 2006
Rotated mine today. It took about an hour and a half. Once you get the system down it goes more quickly. Here are my "tips": 1. I use 3/8" long screws on the wheel pants instead of the 1/2" screws called out on the plans. Shorter screws means fewer threads...means the screws are in/out faster. Also saves a tiny bit of weight (whatever). 2. I use a 7/16" "ratcheting dogbone" wrench on the bolts that attach the outsides of the wheel pants to the axle nut. This makes very quick work of getting those bolts out and back in. You might be able to get a small socket wrench on there, but I find the ratcheting dogbone is exactly what the doctor ordered. 3. Remove the valve stem completely when working with tubes. When you said "let the air out" in your email below, I wasn't sure how you were doing that...so if you're not removing the valve stem, do that. Air is let out very quickly (pretty much instantely...no need to hold the valve) and the tubes are much easier to work with when scrunching 'em up to fit into the tires. 4. This is general advice rather than a trick...DO NOT HANDLE A FULLY INFLATED TIRE/WHEEL that is not held captive by the axle nut. While it's extraordinarily unlikely, it HAS happened -- the wheel can "explode" by virtue of the halves separating, becoming projectiles. I *ALWAYS* remove the valve stem completely before loosening the axle nut. I re-inflate the tires only after the wheel is on the axle with the axle nut ON. In your email below it sounded like you removed the wheel from the axle and then let the air out. Ask around among A&Ps or shops and you'll hear some real horror stories. I met one guy personally who suffered a head injury when a wheel separated. Hope this helps... )_( Dan RV-7 N714D (904 hours) http://www.rvproject.com ----- Original Message ----- From: "Kyle Boatright" <kboatright1(at)comcast.net> Sent: Sunday, May 14, 2006 6:20 PM Subject: RV-List: Rotating the Tires > > > I finished my condition inspection yesterday but deferred pulling the > wheels. A visual inspection indicated that the brakes are in good shape, > and the tires have plenty of tread left, but it soon will be time to > rotate the tires left to right again, and when I do that, I'll re-pack > the wheel bearings. > > Anyway, the point is that whenever I do this, it seems to take forever. > You'd think it would be doable in a couple of hours, but for me it seems > to take a half day. Pulling the wheelpants, extracting the cotter pins > on the axle nuts, pulling loose the brake calipers, alternately jacking > up one side of the plane, then the other, removing a wheel and putting > the axle up on wood blocks. Then, it is time to let the air out of the > tubes, split the wheels, clean and pack the bearings, and reverse the > process. It takes forever... Which is why I deferred it yesterday. I > wanted to be done with the condition inspection, which turned out fine, > except for a broken Adel clamp on one of the exhaust hangars. Also, I > had my AI replace the mixture control thingie in the carburetor, because > it wasn't sealing well and it was getting difficult to stop the engine > with the mixture control. > > Back to the reason for the post... Are there any masters of the tire > rotation task? If so, what are your suggestions, other than having > everything at hand when the time comes? > > Suggestions appreciated. > > KB > > > ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Inst panel hole cutting
Date: May 14, 2006
It took me a couple of weeks with autocad and my learning curve to layout my very complex panel in my Glasair III. I can now do your average panel in about an hour. When you throw in all the 3/4 ATI square, 45 degree corners, VM 1000's and the other strange shaped stuff, it might take me 2 hours. When I'm done, every thing fits, all the mounting holes line up. You might be able to do it with a file, but you sure can tell when you look at the finished product. If you're going to make layout mistakes, it's much easier to fix the error on a computer screen than a sheet of aluminum. 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 randall Sent: Sunday, May 14, 2006 10:44 PM Subject: Re: RV-List: Inst panel hole cutting Jigsaw, files, hacksaw, drill -- worked fine for all of us "old-timers" who built before laser cutters were in vogue. Its a bit of work but I doubt it'd take less time than drawing on CAD. Randall Henderson > DEAN PSIROPOULOS wrote: > > > > > >Quick question folks: > > > >I'm finally to the point where I HAVE to cut the instrument and engine > >monitor display holes in my panel blanks. I thought I had some folks close > >by who could do that but in talking to them yesterday I discovered that > they > >really don't have the capabilities that I need. I have a Dynon D-10 that I > >want to flush mount and that requires a nicely made SQUARE hole. That could > >probably be done with an old hand operated milling machine. The biggest > >problem though is the Vision Microsystems engine monitor display. Its > >outside edges are basically a square hole but at the corners, instead of > >making them 90 degrees, they transition into something like a 45 deg angle > >from the vertical lines to the horizontal lines. Those of you who have > >VM-1000 know what I'm talking about and needless to say, I'm convinced the > >only way to get a nice looking hole to put this display in is to have it > CNC > >machined. Since there is no bezel that fits over the top of this funny > >looking hole, it has to be done right the first time or I'll be looking at > >the botched workmanship every time I check my engine parameters. Any > >suggestions about how I'm might achieve this. Is there anyone east of the > >Mississippi river that has machining templates to do this or can I do it in > >my shop with common tools somehow? Thanks. > > > >Dean Psiropoulos > >RV-6A N197DM > >Trying to get the wiring finished > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Subject: Re: Lightspeed EI installation
Date: May 15, 2006
From: "Stewart, Michael (ISS Atlanta)" <mstewart(at)iss.net>
Doug. Recommend you read this thread for gapping the direct crank pickup . http://www.vansairforce.com/community/showthread.php?t7688 Best, Mike Fellow Listers: I am into a major project installing a dual Lightspeed Ignition system in my flying RV-4. It will be using the direct crank sensor installation. This project is just about done and I am beginning to do some preliminary tests are stated in the LSI manual. I have run a magnetic across the sensors on both systems on the direct crank sensor circuit board and the coils fire fine across their terminals. Here is my question. I have carefully measured the calculated clearance between the sensors on the circuit board and the small magnets which are installed in the ring gear (I had LSI install them so I assume they are in the correct position). I have been trying to see if I can get the coils to fire my temporarily positioning the starter ring gear and moving the engine through TDC. No luck in getting them to fire. Now I don't know if this is a valid test. I assume I am moving the ring gear fast enough through the sensor positions but it is hard to say. For any of you that have installed the LSI system with the direct crank sensor, did you have any issues like this?. Or did you put it together and it just ran?? Doug Weiler N722DW, 290 hours ________________________________________________________________________________
From: "Dale Ensing" <densing(at)carolina.rr.com>
Subject: Re: Idle mixture screw on MA-4-5
Date: May 08, 2006
Mark, When you turn the idle mixture screw counter clockwise, you are turning it out. Be sure you do not turn it so far that there is no longer tension on the spring. A friend did this trying to get that RPM increase on shut down and had the engine quit on final because the idle mixture screw fill out during a flight. Probably came out because of engine vibration during the flight. Dale Ensing ________________________________________________________________________________
Date: Jun 15, 2006
From: Richard Seiders <seiders(at)bellsouth.net>
Subject: Re: Rotating the Tires
Sounds like what I do exactly, and it takes 4 hrs to do it right. I suppose you could work faster, but likely make mistakes and add to future woes. It's a pain. The last occasion for me I saved time by installing new tires at the change instead of switching as tires were worn on the outside a bit more than usual. Saving time = spending more. Relax and enjoy it. Dick At 09:20 PM 5/14/2006, you wrote: > > >I finished my condition inspection yesterday but deferred pulling the >wheels. A visual inspection indicated that the brakes are in good shape, >and the tires have plenty of tread left, but it soon will be time to >rotate the tires left to right again, and when I do that, I'll re-pack >the wheel bearings. > >Anyway, the point is that whenever I do this, it seems to take forever. >You'd think it would be doable in a couple of hours, but for me it seems >to take a half day. Pulling the wheelpants, extracting the cotter pins >on the axle nuts, pulling loose the brake calipers, alternately jacking >up one side of the plane, then the other, removing a wheel and putting >the axle up on wood blocks. Then, it is time to let the air out of the >tubes, split the wheels, clean and pack the bearings, and reverse the >process. It takes forever... Which is why I deferred it yesterday. I >wanted to be done with the condition inspection, which turned out fine, >except for a broken Adel clamp on one of the exhaust hangars. Also, I >had my AI replace the mixture control thingie in the carburetor, because >it wasn't sealing well and it was getting difficult to stop the engine >with the mixture control. > >Back to the reason for the post... Are there any masters of the tire >rotation task? If so, what are your suggestions, other than having >everything at hand when the time comes? > >Suggestions appreciated. > >KB > > ________________________________________________________________________________
Date: May 15, 2006
Subject: rotary engine firewall package for 6, 7, or 9 for sale
From: WALTER B KERR <jbker(at)juno.com>
Sorry about the commercial, but believe this is the best spot to get a plug in for my engine package! Have decided to part my 9A out and build a LSA since medicals or getting tougher as 70 is upon me. Will sell the rotary and install a lycoming in the 9A before selling it. Do not wish to have the double jeopardy of an alternative engine and homebuilt combination if I sell it with the rotary. The engine installation has had minimum problems once I got past a faulty DPDT switch that was apparently backfeeding 12 volts to electronic control and burning the chip which operates off of 5 volts. Flew the 40 hours off in minimum time and have about 10 hours on it since. Fuel burn is not bad if leaned which the flight report in Sport Aviation alludes to. That controller does not allow for leaning. I have over $12K invested and will sell it for $8K. The gear reduction and electronic controller are built by Tracy Crook at RWS inc, the engine is a street ported 13B built by Bruce Turrentine, the engine mount is by Fred Breese, and the prop is a Sensenich. You get the nose gear leg, dual electronic fuel pumps, intake and exhaust manifolds, muffler, radiator (Griffen custom aluminum), oil cooler, and many more items. I have not pulled the engine yet, so you can come to Ft Pierce Fl and see and hear it run until I start the conversion to the lycoming. Bernie Kerr, 6A 450 hours and sold, 9A rotary with 50 hours ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.edu>
Subject: OSH Notam
Date: May 15, 2006
I don't remember if this has been announced but the OSH 2006 Notam is now available. http://www.airventure.org/2006/flying/notam06.pdf W ________________________________________________________________________________
Date: May 15, 2006
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: AD compliance documentation questions
Folks, I just added the hard-line for my prop governor. There is also a Lycoming SB leading to an AD for this line. After I comply with the requirements, how do I document the compliance? I'm guessing that it should go in my engine Log-Book. Here are the questions: Am I authorized to make the entry? I am the builder - but I don't have my ltd A&P for the airframe as it isn't flying yet. Is there a specific text for the compliance? Thanks, Ralph Capen RV6AQB N822AR @ N06 Firewall Foreward Building an experimental is supposed to be a learning experience - that's an understatement! ________________________________________________________________________________
From: "Glen Matejcek" <aerobubba(at)earthlink.net>
Subject: Inst panel hole cutting
Date: May 15, 2006
HI Dean- RE: ...and needless to say, I'm convinced the only way to get a nice looking hole to put this display in is to have it CNC machined.... I have to agree here with the majority of the responses you've gotten so far. It's really not a big deal to do the panel well. There should be dimensional data for mounting your avionics available in your literature, or at least on a web site. Lay it out right on your panel blank, use common drills, unibits, and a saber saw with a metal cutting blade as necessary. File carefully to a nice fit. Test fit your avionics as you go. You will surprise yourself with how nice a job you can do. Virtually all the metal working skills I have I learned building this plane. All my avionics are face mounted, with only one bezel involved. The results are pretty gratifying. FWIW- Glen Matejcek aerobubba(at)earthlink.net ________________________________________________________________________________
From: "Steve Struyk" <rv8striker(at)hotmail.com>
Subject: Inst panel hole cutting
Date: May 15, 2006
I've read with interest this string and thought I'd add my two cents worth. I found making the panel one of the more rewarding parts of the project and did it with a few basic tools. At first I called a few local shops with CNC machines and was shocked at the price just to do the hole for my VM-1000. I decided to get creative with the metal template provided with the VM-1000 and my trusty Craftsman router. First I mounted the template and blank panel on a piece of 3/4" MDF. Then using a straight cutting bit with a roller guide, made a very nice opening for the VM-1000 indicator. After laying out the panel full scale on 1/4" graph paper I did the remaining holes with an instrument hole cutting punch. http://cleavelandtoolstore.com/prodinfo.asp?numberIHC318 Sure it cost 150 bucks but it's the right tool for the job, does both 3 1/8 and 2 1/4 holes. The only other tool needed was a mounting hole jig, 14 bucks. http://cleavelandtoolstore.com/prodinfo.asp?numberIHT250I (I'm a self admitted tool junkie so needing a couple of tools along the way is an excuse to buy one.) BTW I'm not partial to Cleaveland, Avery and others have them as well. A little file work to open holes for things like the Kollsman knob and VS adjustment screw and that was it. I've got pictures if anybody wants to see them off list. Again, just my two cents worth but it worked for me. Steve Struyk St. Charles MO RV-8, 45 Hours ________________________________________________________________________________
From: "Mike Robertson" <mrobert569(at)hotmail.com>
Subject: AD compliance documentation questions
Date: May 15, 2006
Ralph, If the plane isn't flying yet then nothing needs to be done. If the plane is flying then a logbook entry would be in line. Because its experimental you don't need any type of certificate. Simply enter that date, and brief description of what you did, then sign it off and print your name. AS you asked I will volunteer a brief description: " Complied with AD ??-??-?? by installing stainless steel oil line." Thats all that needed. Mike Robertson Das Fed >From: "Ralph E. Capen" <recapen(at)earthlink.net> >Reply-To: rv-list(at)matronics.com >To: lycomingengines-list(at)matronics.com, rv-list(at)matronics.com, >rv6-list(at)matronics.com, RV7A(at)yahoogroups.com >Subject: RV-List: AD compliance documentation questions >Date: Mon, 15 May 2006 10:11:34 -0400 (GMT-04:00) > > >Folks, > >I just added the hard-line for my prop governor. There is also a Lycoming >SB leading to an AD for this line. > >After I comply with the requirements, how do I document the compliance? >I'm guessing that it should go in my engine Log-Book. > >Here are the questions: Am I authorized to make the entry? I am the >builder - but I don't have my ltd A&P for the airframe as it isn't flying >yet. Is there a specific text for the compliance? > >Thanks, >Ralph Capen >RV6AQB N822AR @ N06 Firewall Foreward > >Building an experimental is supposed to be a learning experience - that's >an understatement! > > ________________________________________________________________________________
Date: May 15, 2006
From: George Inman 204 287 8334 <ghinman(at)mts.net>
Subject: Inst panel hole cutting
I managed to make decent looking square holes using an ordinary power jig saw with a mettle cutting blade. Drill holes at the corners,then use the jig saw to cut close to finished size.Then finish with a flat file. You can do the corners with a small file. > I have a Dynon D-10 that I >want to flush mount and that requires a nicely made SQUARE hole. That could >probably be done with an old hand operated milling machine. The biggest >problem though is the Vision Microsystems engine monitor display. Its >outside edges are basically a square hole but at the corners, instead of >making them 90 degrees, they transition into something like a 45 deg angle >from the vertical lines to the horizontal lines. Those of you who have >VM-1000 know what I'm talking about and needless to say, I'm convinced the >only way to get a nice looking hole to put this display in is to have it CNC >machined. Since there is no bezel that fits over the top of this funny >looking hole, it has to be done right the first time or I'll be looking at >the botched workmanship every time I check my engine parameters. Any >suggestions about how I'm might achieve this. Is there anyone east of the >Mississippi river that has machining templates to do this or can I do it in >my shop with common tools somehow? Thanks. > >Dean Psiropoulos >RV-6A N197DM -- George H. Inman ghinman(at)mts.net ________________________________________________________________________________
From: "Glen Matejcek" <aerobubba(at)earthlink.net>
Subject: glued canopy
Date: May 15, 2006
HI All- I have an update on my glued canopy saga. Life has conspired to keep me from working on my project, but the canopy is now glued on, cut, filleted, and the edges are dressed. Along the way I came up with a few data points I'd like to share. First though I'd like to thank those who've gone before, especially Billy and Mickey. Thanks guys! WRT the chemicals used, the cleaner does have a primer element to it. It is very easy to use and the minimum purchase quantity is several times what you will need. The primer itself is about double or more of what you need. The primer forms a very smooth surface for the adhesive to bond to. This is a fundamental requirement of the process. Somewhere out there in cyberworld is a recommendation to scuff the primer if you can't get the adhesive in place right away. This would be a large mistake, as would adding another coat of primer. Per the manufacturer, the adhesive is to be applied to the primer within 2 hours. Between 2 hours and about 3 days, you can simply wash the primer with the cleaner, and it will re-soften it adequately to apply the adhesive. Scuffing the primer will cause a significantly weaker bond, as the adhesive won't flow into the 'tooth'. If you were to scuff the primer, you should remove ALL the affected area and start the process over with the cleaner. Adding a second coat of primer would make an unacceptably thick, and therefore structurally weak, layer. When applying the adhesive, I used perhaps 2 dozen latex gloves. This helped me to keep the project (and myself!) pretty clean. My wife and I had no trouble doing the installation by ourselves. It's really pretty darn slick, and I just can't imagine drilling and using fasteners. I used Billy's idea of scoring the primer from the inside with a screw to locate the big cut, then re-marked it with masking tape on the outside. A die grinder and cutting disc made pretty quick and easy work of the cut. I did underestimate what the final kerf was going to be, but the gasket will take care of that just fine. Once the canopy was cut and removed from the plane, I prepped and finish glued it. This involved back filling the areas where the spacers had been and creating aesthetically pleasing fillets. In most places this is easily done with a gloved finger. For the windscreen base, I used a four inch diameter ceramic candy dish as a squeegee. It worked extremely well, was very convenient to grip, and cleaned up easily. The glue actually had to sit for 2 days before I was comfortable handling it. After 2 weeks, it is a whole lot tougher. To dress the 'big cut', I used 100 and then 220 grit self adhesive sandpaper on both sides of a 1/2 x 1-1/2 x 6" sanding block. I closed the canopy on the block and then sanded both sides of the cut at the same time. This ensured that the two cut edges stayed parallel as I cleaned them up. I final finished them with scotchbrite, and am quite pleased with the results. The way I did my installation, two tubes of adhesive was just about enough to do the canopy, but not the skirt. That will require part of a third tube. How to seal the leading edge of the skirt will take a little thought, but shouldn't be too arduous. As ever, FWIW! Glen Matejcek aerobubba(at)earthlink.net ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Inst panel hole cutting
Date: May 15, 2006
Of the 11 holes in my panel, only 6 are round. The rest are 3 inch ATI, (that's 3 inch square with 45 degree clipped corners), 1/3 ATI, rectulangar (AOA), and my VM1000. Now you might be able to do a passing job by hand on the big holes, but the real clincher is locating the instrument mounting holes. If you're mounting with pan head screws you have some fudge factor to oversize the hole if you're off a little bit. But all my instrument mounting screws are countersunk. Which means I had to be dead nuts on. My Glasair III has 5 metal sub panels that mount to a fiberglass frame. My cost to CNC all the panels and holes was under $300 total. The cutter worked from my autocad drawing, which I supplied. 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 Steve Struyk Sent: Monday, May 15, 2006 10:45 AM Subject: RV-List: Inst panel hole cutting I've read with interest this string and thought I'd add my two cents worth. I found making the panel one of the more rewarding parts of the project and did it with a few basic tools. At first I called a few local shops with CNC machines and was shocked at the price just to do the hole for my VM-1000. I decided to get creative with the metal template provided with the VM-1000 and my trusty Craftsman router. First I mounted the template and blank panel on a piece of 3/4" MDF. Then using a straight cutting bit with a roller guide, made a very nice opening for the VM-1000 indicator. After laying out the panel full scale on 1/4" graph paper I did the remaining holes with an instrument hole cutting punch. http://cleavelandtoolstore.com/prodinfo.asp?numberIHC318 Sure it cost 150 bucks but it's the right tool for the job, does both 3 1/8 and 2 1/4 holes. The only other tool needed was a mounting hole jig, 14 bucks. http://cleavelandtoolstore.com/prodinfo.asp?numberIHT250I (I'm a self admitted tool junkie so needing a couple of tools along the way is an excuse to buy one.) BTW I'm not partial to Cleaveland, Avery and others have them as well. A little file work to open holes for things like the Kollsman knob and VS adjustment screw and that was it. I've got pictures if anybody wants to see them off list. Again, just my two cents worth but it worked for me. Steve Struyk St. Charles MO RV-8, 45 Hours ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: AD compliance documentation questions
Date: May 15, 2006
Mike, Because we're not subject to AD's don't you think he should state he complied with the SB rather than the AD? 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 Mike Robertson Sent: Monday, May 15, 2006 10:54 AM Subject: RE: RV-List: AD compliance documentation questions Ralph, If the plane isn't flying yet then nothing needs to be done. If the plane is flying then a logbook entry would be in line. Because its experimental you don't need any type of certificate. Simply enter that date, and brief description of what you did, then sign it off and print your name. AS you asked I will volunteer a brief description: " Complied with AD ??-??-?? by installing stainless steel oil line." Thats all that needed. Mike Robertson Das Fed >From: "Ralph E. Capen" <recapen(at)earthlink.net> >Reply-To: rv-list(at)matronics.com >To: lycomingengines-list(at)matronics.com, rv-list(at)matronics.com, >rv6-list(at)matronics.com, RV7A(at)yahoogroups.com >Subject: RV-List: AD compliance documentation questions >Date: Mon, 15 May 2006 10:11:34 -0400 (GMT-04:00) > > >Folks, > >I just added the hard-line for my prop governor. There is also a Lycoming >SB leading to an AD for this line. > >After I comply with the requirements, how do I document the compliance? >I'm guessing that it should go in my engine Log-Book. > >Here are the questions: Am I authorized to make the entry? I am the >builder - but I don't have my ltd A&P for the airframe as it isn't flying >yet. Is there a specific text for the compliance? > >Thanks, >Ralph Capen >RV6AQB N822AR @ N06 Firewall Foreward > >Building an experimental is supposed to be a learning experience - that's >an understatement! > > ________________________________________________________________________________
Subject: Instrument screws/nuts
From: Gerry Filby <gerf(at)gerf.com>
Date: May 15, 2006
Folks, I'm assuming that brass screws are what to use anywhere on the panel (although all my instruments are "electronic" apart from 2 steam gauges - altimeter and ASI). I see various brass screws in Spruce's catalog - but no brass nuts and washers - do folks generally go with the cad plated steel locknuts (AN365) ? Or is there a source of brass nuts and washers ? __g__ ========================================================== Gerry Filby gerf(at)gerf.com Tel: 415 203 9177 ---------------------------------------------------------- ________________________________________________________________________________
Subject: Re: Inst panel hole cutting
From: Gerry Filby <gerf(at)gerf.com>
Date: May 15, 2006
That's the way I went - one tip - put masking tape 2 layers thick anywhere the base plate of your jigsaw is going to contact the panel - mine got scratched up a bit as the saw travelled across the surface. g > > > > > I managed to make decent looking square holes using an > ordinary power jig saw with a mettle cutting blade. > Drill holes at the corners,then use the jig saw to cut > close to finished size.Then finish with a flat file. > You can do the corners with a small file. > > > > > I have a Dynon D-10 that I > >want to flush mount and that requires a nicely made SQUARE hole. That could > >probably be done with an old hand operated milling machine. The biggest > >problem though is the Vision Microsystems engine monitor display. Its > >outside edges are basically a square hole but at the corners, instead of > >making them 90 degrees, they transition into something like a 45 deg angle > >from the vertical lines to the horizontal lines. Those of you who have > >VM-1000 know what I'm talking about and needless to say, I'm convinced the > >only way to get a nice looking hole to put this display in is to have it CNC > >machined. Since there is no bezel that fits over the top of this funny > >looking hole, it has to be done right the first time or I'll be looking at > >the botched workmanship every time I check my engine parameters. Any > >suggestions about how I'm might achieve this. Is there anyone east of the > >Mississippi river that has machining templates to do this or can I do it in > >my shop with common tools somehow? Thanks. > > > >Dean Psiropoulos > >RV-6A N197DM > -- __g__ ========================================================== Gerry Filby gerf(at)gerf.com Tel: 415 203 9177 ---------------------------------------------------------- ________________________________________________________________________________
Date: May 15, 2006
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: glued canopy
On 8:15:42 2006-05-15 "Glen Matejcek" wrote: > I have an update on my glued canopy saga. Life has conspired to keep > me from working on my project, but the canopy is now glued on, cut, > filleted, and the edges are dressed. Along the way I came up with a > few data points I'd like to share. First though I'd like to thank > those who've gone before, especially Billy and Mickey. Thanks guys! Glen, i've added your post to the Gluing Your Canopy page on the Matronics RV Wiki. You can find it here: <http://wiki.matronics.com/wiki/index.php/Gluing_Your_Canopy> Feel free to edit if you'd like to add more info. -Rob ________________________________________________________________________________
From: James Freeman <flyeyes(at)mac.com>
Subject: Re: Instrument screws/nuts
Date: May 15, 2006
On May 15, 2006, at 10:28 AM, Gerry Filby wrote: > > > Folks, > > I'm assuming that brass screws are what to use anywhere on the > panel (although all my instruments are "electronic" apart from > 2 steam gauges - altimeter and ASI). > > I see various brass screws in Spruce's catalog - but no brass > nuts and washers - do folks generally go with the cad plated > steel locknuts (AN365) ? Or is there a source of brass nuts > and washers ? > Gerry- The only reason to use the brass hardware is to avoid interference with your compass. If you don't have a compass on your panel, don't worry about it. Stainless nuts and washers are widely available and mostly (but not completely) non-magnetic. These are usually good enough for "gubmint" work. For items that won't be removed frequently, don't overlook soft aluminum pop rivets. They are quick and cheap to install, and can be drilled out more quickly than you can remove a typical threaded fastener. I used them to mount my magnetometer rather than fool around trying to find appropriate brass or nylon hardware. James Freeman ________________________________________________________________________________
From: Denis Walsh <denis.walsh(at)comcast.net>
Subject: Re: Instrument screws/nuts
Date: May 15, 2006
Grasshoppers or threaded instruments Denis Walsh On May 15, 2006, at 9:28 AM, Gerry Filby wrote: > > > Folks, > > I'm assuming that brass screws are what to use anywhere on the > panel (although all my instruments are "electronic" apart from > 2 steam gauges - altimeter and ASI). > > I see various brass screws in Spruce's catalog - but no brass > nuts and washers - do folks generally go with the cad plated > steel locknuts (AN365) ? Or is there a source of brass nuts > and washers ? > > __g__ > > ========================================================= > Gerry Filby gerf(at)gerf.com > Tel: 415 203 9177 > ---------------------------------------------------------- > > ________________________________________________________________________________
Subject: RV-4 for Sale
Date: May 15, 2006
From: "Rainey, Steven A CIV" <steven.rainey(at)navy.mil>
Jim, can I get some info on this RV-4?? Where is it located, etc?? contact email from the seller , etc?? thanks......... Steven at Steven.rainey(at)navy.mil ........... -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Jim Cimino Sent: Friday, May 12, 2006 13:51 Subject: RV-List: RV-4 for Sale I am listing this for a friend of mine who has an RV-4 for sale. It has an O-320-D1A with 310 TTAE bought new from Van's. It is VFR and is in great shape. This is a very nice RV-4 that was built by a close friend of mine who is a retired sheet metal fabricator. This was the 3rd RV that he built and the workmanship is flawless. It is yellow and red. My friend is asking $45,000 for it. If you are interested or have any other questions you can contact Richard at rblakesl(at)ptd.net . Or I will try to answer any questions I can for you. Thanks, Jim Jim Cimino N7TL RV-8 S/N 80039 200+ Hours http://www.geocities.com/jcimino.geo/ ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: Inst panel hole cutting
Date: May 15, 2006
Or maybe work from the back of the panel. But if you do, don't cut the notch for the altimeter setting on the wrong corner. I hear someone did that. Terry -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Gerry Filby Sent: Monday, May 15, 2006 8:30 AM Subject: Re: RV-List: Inst panel hole cutting That's the way I went - one tip - put masking tape 2 layers thick anywhere the base plate of your jigsaw is going to contact the panel - mine got scratched up a bit as the saw travelled across the surface. g > > > > > I managed to make decent looking square holes using an > ordinary power jig saw with a mettle cutting blade. > Drill holes at the corners,then use the jig saw to cut > close to finished size.Then finish with a flat file. > You can do the corners with a small file. > ________________________________________________________________________________
From: "John Fasching" <n1cxo320(at)salidaco.com>
Subject: Re: Rotating the Tires
Date: May 15, 2006
Kyle, I think rotating the tires is a lot of work for minimal returns. I decided some time ago to get the best tires out there and leave them in place. I found that the Goodyear Flight Custom II wear like iron. I have not rotated them and they seem to wear fairly evenly...I use 30PSI....I can't recall when I replaced them, must have been several years ago and many, many, landings, and they still have deep even threads. FWIW John at Salida, CO ----- Original Message ----- From: "Kyle Boatright" <kboatright1(at)comcast.net> Sent: Sunday, May 14, 2006 7:20 PM Subject: RV-List: Rotating the Tires > > > I finished my condition inspection yesterday but deferred pulling the > wheels. A visual inspection indicated that the brakes are in good shape, > and the tires have plenty of tread left, but it soon will be time to > rotate the tires left to right again, and when I do that, I'll re-pack > the wheel bearings. > > Anyway, the point is that whenever I do this, it seems to take forever. > You'd think it would be doable in a couple of hours, but for me it seems > to take a half day. Pulling the wheelpants, extracting the cotter pins > on the axle nuts, pulling loose the brake calipers, alternately jacking > up one side of the plane, then the other, removing a wheel and putting > the axle up on wood blocks. Then, it is time to let the air out of the > tubes, split the wheels, clean and pack the bearings, and reverse the > process. It takes forever... Which is why I deferred it yesterday. I > wanted to be done with the condition inspection, which turned out fine, > except for a broken Adel clamp on one of the exhaust hangars. Also, I > had my AI replace the mixture control thingie in the carburetor, because > it wasn't sealing well and it was getting difficult to stop the engine > with the mixture control. > > Back to the reason for the post... Are there any masters of the tire > rotation task? If so, what are your suggestions, other than having > everything at hand when the time comes? > > Suggestions appreciated. > > KB > > > ________________________________________________________________________________
From: Jerry2DT(at)aol.com
Date: May 15, 2006
Subject: Re: Inst panel hole cutting
Dean, I have successfully used a router table to cut very clean and straight lines on my panel. First, I cut with a hole saw, jig saw, or other means to get close to the edge. Then with a small, .125" cutter in the router, and a fence made from a piece of .063 alum angle one can progressively take small cuts out to the edge you want. If you need smaller than .125 radius at the corners, you can predrill those before routing. This method results in a finish comparable to professional machining if you are careful, and it is relatively fast compared to filing, etc... You will need to devise a method to keep the fence solidly in place while routing but easy to move. With mine, I simply use clamps. You will need a variable speed control. Harbor Freight. Cheap. It is important to practice on a similar piece and learn the technique first. Did I mention this is inexpensive? Provide you already have router access, of course. Disclaimer and warning: Routers can be dangerous cutting aluminum, so take small cuts, say .003, push work against cutter rotation, not with, or there could be an ugly surprise. Wear eye protection and leather gloves. FWIW, YMMV, etc. Hope this helps Jerry Cochran Wilsonville, OR In a message dated 5/15/2006 12:04:44 A.M. Pacific Daylight Time, rv-list(at)matronics.com writes: From: "DEAN PSIROPOULOS" <dean.psiropoulos(at)verizon.net> Subject: Quick question folks: I'm finally to the point where I HAVE to cut the instrument and engine monitor display holes in my panel blanks. I thought I had some folks close by who could do that but in talking to them yesterday I discovered that they really don't have the capabilities that I need. I have a Dynon D-10 that I want to flush mount and that requires a nicely made SQUARE hole. That could probably be done with an old hand operated milling machine. The biggest problem though is the Vision Microsystems engine monitor display. Its outside edges are basically a square hole but at the corners, instead of making them 90 degrees, they transition into something like a 45 deg angle from the vertical lines to the horizontal lines. Those of you who have VM-1000 know what I'm talking about and needless to say, I'm convinced the only way to get a nice looking hole to put this display in is to have it CNC machined. Since there is no bezel that fits over the top of this funny looking hole, it has to be done right the first time or I'll be looking at the botched workmanship every time I check my engine parameters. Any suggestions about how I'm might achieve this. Is there anyone east of the Mississippi river that has machining templates to do this or can I do it in my shop with common tools somehow? Thanks. Dean Psiropoulos RV-6A N197DM Trying to get the wiring finished ________________________________________________________________________________
Subject: Re: Inst panel hole cutting
From: "Rick Galati" <rick6a(at)yahoo.com>
Date: May 15, 2006
dean.psiropoulos(at)veriz wrote: > ......... The biggest > problem though is the Vision Microsystems engine monitor display...... Those of you who have VM-1000 know what I'm talking about and needless to say, I'm convinced the only way to get a nice looking hole to put this display in is to have it CNC machined. Dean, I did not find the VM-1000 hole to be particularily difficult to fashion at all. As my usual practice in approaching such things, I rough cut the hole open as large as possible with a fiber cutoff wheel...the same one used to separate the canopy bubble...then using various high speed rotary files in a standard die grinder and a combination of smaller files and stones in a pencil grinder, I think the VM-1000 opening came out just fine. http://img478.imageshack.us/img478/7321/00001139tx.jpg Rick Galati RV-6A "Darla" Read this topic online here: http://forums.matronics.com/viewtopic.php?p=34741#34741 ________________________________________________________________________________
From: "Wesley T Robinson" <wesleyt(at)stanfordfurniture.com>
Subject: EAA Chapter 731 Fly-in at Morganton-Lenoir, NC, May 20th
Date: May 15, 2006
Listers, EAA Chapter 731 is holding their Spring Fly-in at Morganton-Lenoir, NC (KMRN) on May 20th. Join us for food, fun, and flying! Should be a great day with quite a few aircraft attending. An award will be given to the best RV and to aircraft in other categories. Check the club website for full details. www.eaa731.org Wesley T Robinson WR Consulting EAA 731 Web/Newsletter Editor RV-9A N224WR 150Hrs ________________________________________________________________________________
From: "Mike Robertson" <mrobert569(at)hotmail.com>
Subject: AD compliance documentation questions
Date: May 15, 2006
You're choice, but as the AD calls out the SB I feel it would be better to call out the AD. That way if any question should come up down the line you are able to point right to the entry instead of having to explain that the SB is called out in the AD and therefore the same. Mike Robertson >From: "Bruce Gray" <Bruce(at)glasair.org> >Reply-To: rv-list(at)matronics.com >To: >Subject: RE: RV-List: AD compliance documentation questions >Date: Mon, 15 May 2006 11:19:15 -0400 > > >Mike, > >Because we're not subject to AD's don't you think he should state he >complied with the SB rather than the AD? > >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 Mike Robertson >Sent: Monday, May 15, 2006 10:54 AM >To: rv-list(at)matronics.com >Subject: RE: RV-List: AD compliance documentation questions > > >Ralph, > >If the plane isn't flying yet then nothing needs to be done. If the plane >is flying then a logbook entry would be in line. Because its experimental >you don't need any type of certificate. Simply enter that date, and brief >description of what you did, then sign it off and print your name. > >AS you asked I will volunteer a brief description: " Complied with AD >??-??-?? by installing stainless steel oil line." Thats all that needed. > >Mike Robertson >Das Fed > > > >From: "Ralph E. Capen" <recapen(at)earthlink.net> > >Reply-To: rv-list(at)matronics.com > >To: lycomingengines-list(at)matronics.com, rv-list(at)matronics.com, > >rv6-list(at)matronics.com, RV7A(at)yahoogroups.com > >Subject: RV-List: AD compliance documentation questions > >Date: Mon, 15 May 2006 10:11:34 -0400 (GMT-04:00) > > > > > >Folks, > > > >I just added the hard-line for my prop governor. There is also a >Lycoming > >SB leading to an AD for this line. > > > >After I comply with the requirements, how do I document the compliance? > >I'm guessing that it should go in my engine Log-Book. > > > >Here are the questions: Am I authorized to make the entry? I am the > >builder - but I don't have my ltd A&P for the airframe as it isn't flying > >yet. Is there a specific text for the compliance? > > > >Thanks, > >Ralph Capen > >RV6AQB N822AR @ N06 Firewall Foreward > > > >Building an experimental is supposed to be a learning experience - that's > >an understatement! > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "RV6 Flyer" <rv6_flyer(at)hotmail.com>
Subject: Ryton sumps
Date: May 16, 2006
There are several out there. ECI makes a metal one that I saw at Oshkosh and it was several pounds ligher than the one Lycoming sells. This is ECI's experimental one: http://www.eci2fly.com/exp/cis_flyer.pdf http://www.eci2fly.com/exp/cis_tds.pdf http://www.superflite.com/products.asp?p=115&SID=17&SN=Front%20Servo%20Sump I thought that Raven Aircraft also had a 4 cylinder parallel valve version but cannot find it anymore. Only the 540 version. http://www.ravenaircraft.com/raven_012.htm http://www.skydynamics.com/maxisump.html http://users.adelphia.net/~aeroengine/Barrett.html http://www.attawayair.com/eci_fi_system.htm http://www.performanceengines.com/images/LineCard.pdf I remember seeing a link to another one out there but cannot find it now. Lets put this one in the archives for next time when we go looking for cold air sumps. Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, 1,852 + Flying Hours So. CA, USA http://SoCAL_WVAF.rvproject.com ----Original Message Follows---- From: "Karen and Robert Brown" <bkbrown(at)ashcreekwireless.com> Subject: RV-List: Ryton sumps Date: Mon, 15 May 2006 06:38:12 -0700 Yesterday, I joined the ranks of people who have broken their ryton sumps during startup. 3 out of 4 ryton sumps on the field have now broken at least once. I am not comfortable with that record, so am now looking at alternatives for replacement. Does anyone have feedback on what options are out there for a forward facing sump? Bob Brown RV7A last few things...oh, and a NEW INDUCTION SYSTEM! ________________________________________________________________________________
Date: May 15, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Instrument screws/nuts
I just used some really cool stainless hex head screws from home depot. Works great. I think the brass screw thing is an old wives tale, personally...that is unless you are using them screw in a compass. Paul Besing --- James Freeman wrote: > > > > On May 15, 2006, at 10:28 AM, Gerry Filby wrote: > > > > > > > > Folks, > > > > I'm assuming that brass screws are what to use > anywhere on the > > panel (although all my instruments are > "electronic" apart from > > 2 steam gauges - altimeter and ASI). > > > > I see various brass screws in Spruce's catalog - > but no brass > > nuts and washers - do folks generally go with the > cad plated > > steel locknuts (AN365) ? Or is there a source of > brass nuts > > and washers ? > > > > Gerry- > > The only reason to use the brass hardware is to > avoid interference > with your compass. If you don't have a compass on > your panel, don't > worry about it. > > Stainless nuts and washers are widely available and > mostly (but not > completely) non-magnetic. These are usually good > enough for "gubmint" > work. > > For items that won't be removed frequently, don't > overlook soft > aluminum pop rivets. They are quick and cheap to > install, and can be > drilled out more quickly than you can remove a > typical threaded > fastener. I used them to mount my magnetometer > rather than fool > around trying to find appropriate brass or nylon > hardware. > > James Freeman > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
From: DOUGPFLYRV(at)aol.com
Date: May 15, 2006
Subject: Re: Ryton sumps
We also had a broken sump on the Superior XP-360. I don't even know if it is a Ryton. It has been replaced but I am very leery of it now. Seems we were running a bit lean at low power. It back fired on start up. Our servo was a repaired unit so we got a new one but not sure it is any different. Please give me some input if u are running the same engine. 1. What is the fuel flow at take off power....we show 16.3 GPH. 2. What are the EGT's at some altitude at full rich. 3. What are the EGT's at that altitude after leaning on the rich side Appreciate any and all info on this engine. We are not confident that things are as they should be and concerned with causing damage. Thanks, Doug Preston RV-7A N196VA ________________________________________________________________________________
Subject: Re: AD compliance documentation questions
From: "N395V" <n395v(at)hughes.net>
Date: May 16, 2006
> That's kinda like saying there's no harm in letting the cops do a > warrant-less search of your car for drugs if you don't use drugs Actually I liken more to painting my house in a traditional color as opposed to pink and purple to enhance curb appeal and resale value. Were I purchasing an RV 8 or a Rocket I would like to know if the fuel pump AD had been done or if any of the Crank SBs applied. Logbook notations to that effect would help. If the FAA checks your logbooks on a ramp check it's cuz you #1 had them with you and #2 told them to look at them. Don't want them looked at don't carry them in the plane. Now as for the Gumn't keeping records on our phone calls, yep we failed to connect the dots. Theyr'e probably also reading the e mail lists which those 9 black robed distinguished idiots would probably also say is ok. -------- Milt N395V F1 Rocket Read this topic online here: http://forums.matronics.com/viewtopic.php?p=34835#34835 ________________________________________________________________________________
Subject: Re: AD compliance documentation questions
From: "Jekyll" <rcitjh(at)aol.com>
Date: May 16, 2006
ceengland(at)bellsouth.ne wrote: > N395V wrote: > > That's kinda like saying there's no harm in letting the cops do a > warrant-less search of your car for drugs if you don't use drugs. Or > letting the Gummint have a record of all your phone calls & emails if > you aren't a terrorist. > > Oh, please! Missed the point. It is about taking the extra (and easy) step now to avoid future arguements that may crop up in pre-sale negotiations or post-accident legal or insurance coverage hassels. This is an "ounce of prevention" being better than a "pound of cure". Jekyll Read this topic online here: http://forums.matronics.com/viewtopic.php?p=34866#34866 ________________________________________________________________________________
From: Jerry2DT(at)aol.com
Date: May 16, 2006
Subject: Re:Ryton sumps
Guys, Please post your messages concerning these sumps also on _http://groups.yahoo.com/group/XP-360Forum/_ (http://groups.yahoo.com/group/XP-360Forum/) . I am sure the guys at Superior check that one so important they know what the sentiment is out here. Last time I talked to them about these failures, they assured me "It's never happened in flight." Cold comfort. They also said they're working on a replacement, but not free to present owners unless you "have a problem". These folks need to step up, communicate with their customers, and schedule free replacements when available. Mine is still in the garage, but 90/90, so I hope they get off their duff. My .10. Jerry Cochran Wilsonville, OR In a message dated 5/16/2006 12:06:17 A.M. Pacific Daylight Time, rv-list(at)matronics.com writes: From: DOUGPFLYRV(at)aol.com Subject: Re: RV-List: Ryton sumps We also had a broken sump on the Superior XP-360. I don't even know if it is a Ryton. It has been replaced but I am very leery of it now. Seems we were running a bit lean at low power. It back fired on start up. Our servo was a repaired unit so we got a new one but not sure it is any different. Please give me some input if u are running the same engine. 1. What is the fuel flow at take off power....we show 16.3 GPH. 2. What are the EGT's at some altitude at full rich. 3. What are the EGT's at that altitude after leaning on the rich side Appreciate any and all info on this engine. We are not confident that things are as they should be and concerned with causing damage. Thanks, Doug Preston RV-7A N196VA ________________________________________________________________________________
From: Jerry2DT(at)aol.com
Date: May 16, 2006
Subject: Re: Ryton sumps
Bob and Doug, Superior has told me these incidents have only happened with electronic ignitions. Is that what you guys have? Something about the "wasted spark"... Even though I have mags, still makes me nervous as hell... Jerry Cochran Wilsonville, OR In a message dated 5/16/2006 12:06:17 A.M. Pacific Daylight Time, rv-list(at)matronics.com writes: ----Original Message Follows---- From: "Karen and Robert Brown" <bkbrown(at)ashcreekwireless.com> Subject: RV-List: Ryton sumps Yesterday, I joined the ranks of people who have broken their ryton sumps during startup. 3 out of 4 ryton sumps on the field have now broken at least once. I am not comfortable with that record, so am now looking at alternatives for replacement. Does anyone have feedback on what options are out there for a forward facing sump? Bob Brown RV7A last few things...oh, and a NEW INDUCTION SYSTEM! ________________________________________________________________________________
Subject: Re: AD compliance documentation questions
From: "Jekyll" <rcitjh(at)aol.com>
Date: May 16, 2006
Milt: Quite right. My quoting ability was a mouse click or two from my desired results. Quotes inside quotes... something along the lines of riddles inside inigmas. My appologies. Jekyll Read this topic online here: http://forums.matronics.com/viewtopic.php?p=34872#34872 ________________________________________________________________________________
Date: May 16, 2006
From: "Jeff Linebaugh" <jefflinebaugh(at)earthlink.net>
Subject: Panel For Sale
-------Original Message------- From: Jeff Linebaugh Date: 05/16/06 15:25:37 rv-list(at)matonics.com; v8-list(at)matronics.com; rv4-list(at)matronics.com; RVSouthEast-list(at)matronics.com Subject: F1 Rocket Panel For Sale I have a new (never flown) F1 Rocket Panel for sale. The panel is comple te with all components installed, and pre-wired avionics harnesses. Please e-mail me for more photos/details if interested. Thanks Jeff Jeff Linebaugh jeff@rocket-boys.com F1 Rocket N240KT soon coming to... Memphis, TN. ________________________________________________________________________________
Date: May 16, 2006
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Re: Ryton sumps
I don't believe this. How much ignitable fuel/air mixture can be there? Plus the exhaust valve is likely open. And it does not explain Doug's case were he has two mags. Ron Lee >What happens in the wasted spark ignition is that >there are two sparks to a complete cycle. The first >is at the top of the compression stroke. The second >is at the top of the exhaust stroke and the opening of >the intake valve. If the spark hits the fuel/air >mixture at this point, a back fire occurs towards the >carb or throttlebody and the ryton sump cannot contain >the explosive condition, therefore, it disintegrates. > >Dave ________________________________________________________________________________
Date: May 16, 2006
From: sarg314 <sarg314(at)comcast.net>
Subject: use tax in arizona
Has any one registered their homebuilt in Arizona in the last 6 mo. or 12 months? I'd be interested in hearing your experience with the use tax and the AZ Dept. of Revenue. Apparently their response is not very consistent from one case to the next. -- Tom Sargent RV-6A ________________________________________________________________________________
Date: May 16, 2006
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: AD compliance documentation questions
Jekyll wrote: > > >ceengland(at)bellsouth.ne wrote: > > >>N395V wrote: >> >>That's kinda like saying there's no harm in letting the cops do a >>warrant-less search of your car for drugs if you don't use drugs. Or >>letting the Gummint have a record of all your phone calls & emails if >>you aren't a terrorist. >> >> >> >> > > >Oh, please! Missed the point. It is about taking the extra (and easy) step now to avoid future arguements that may crop up in pre-sale negotiations or post-accident legal or insurance coverage hassels. This is an "ounce of prevention" being better than a "pound of cure". > >Jekyll > The point is that AD's carry legal obligation. I believe that Das Fed will tell you that an AD has never been issued on a homebuilt. Yet. Remember the uproar just a few weeks ago over Van issuing a 'mandatory' service bulletin? Do you really want something like that issued by the Feds with the force of law? I'm not questioning the wisdom of carrying out some particular safety-related SB. I'm just saying that I don't want the Gummint treating my homebuilt like a factory plane. Making logbook entries that talk about complying with AD's are starting the slide down that slippery slope. (BTW, the dots were visible and connected; the people at the top just refused to listen, just like they refused to listen to the CIA & military prior to the current Iraq situation.) Charlie ________________________________________________________________________________
Date: May 16, 2006
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: Ryton sumps
In any case, I personally do not like the idea of a poly/plastic media containing my engines blood (oil). These engines are expensive! When I first saw the Ryton sump it looked like a problem just waiting to happen. Just my .02 cents... Darrell Ron Lee wrote: I don't believe this. How much ignitable fuel/air mixture can be there? Plus the exhaust valve is likely open. And it does not explain Doug's case were he has two mags. Ron Lee >What happens in the wasted spark ignition is that >there are two sparks to a complete cycle. The first >is at the top of the compression stroke. The second >is at the top of the exhaust stroke and the opening of >the intake valve. If the spark hits the fuel/air >mixture at this point, a back fire occurs towards the >carb or throttlebody and the ryton sump cannot contain >the explosive condition, therefore, it disintegrates. > >Dave --------------------------------- Blab-away for as little as 1/min. Make PC-to-Phone Calls using Yahoo! Messenger with Voice. --------------------------------- ________________________________________________________________________________
Date: May 16, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: use tax in arizona
No, it's not real consistent. I registered my RV-6A back in '98 or so. I got a bill about 6 months later. Told them it was just a pile of metal, and never heard from them again. Paul Besing --- sarg314 wrote: > > > Has any one registered their homebuilt in Arizona in > the last 6 mo. or > 12 months? I'd be interested in hearing your > experience with the use > tax and the AZ Dept. of Revenue. Apparently their > response is not very > consistent from one case to the next. > -- > Tom Sargent > RV-6A > > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
From: "Karen and Robert Brown" <bkbrown(at)ashcreekwireless.com>
Subject: Re: Ryton sumpsRyton sumps
Date: May 16, 2006
I've been on the phone all day researching this topic. Thanks for pointing me in the right direction Gary. Here's the deal: If you want a "cold air sump", there seems to be 3 choices- Ryton sump by Superior Magnesium sump by ECI Barrett Precision cold air sump All the other metal sumps out there- Aerosport Power Aero Engines Superflite Are all copies of the Lycoming cast aluminum sump (not cold air sumps) The Ryton sump (by Superior Engines) we've discussed before here, it costs 1000 to 1300 dollars and will break when used with a wasted spark electronic ignition system...if not sooner, then later. You might not know it's broken unless you inspect it closely like I did. Superior does not see the magnitude of the problem of the sumps it has in the field, but is currently in a "redesign" of the Ryton sump to address the wasted spark ignition issue. The new sump is expected out by October. Based on other new product announcements, I wouldn't look for it a day sooner. The magnesium sump by ECI is just now becoming available and costs about $2400 including the tubes. There are two of them out there on aircraft so far. If you want to be #3, they should be ready to ship on May 22. I was told I'd have to fab a support bracket for the Bendix or AFP servo because that was "too much weight" out there for the induction portion of the sump to hold unsupported. That bothered me. The flange for mounting the fuel servo is also forward from where the Ryton sump flange is, which will mean more extensive alteration of the air snorkel to get it to fit. I don't have the information on the Barrett Cold Sump system, but it is the most expensive of the three. I'll post that here when I find it. I guess that's it... My choice will be the Superflight sump, when it's available in a few weeks. It's a clone of the Lycoming forward facing sump, so it's not a "cold air sump". I have made peace with that and decided if I get a sump that WON'T BREAK, that will be more important than a few more horsepower. All these clones of the Lycoming forward facing sump are priced about the same at $2200. I sure think there's a market out there for a well made cold air induction system...but I don't think there's a good one at a reasonable price that's available yet. For those of you who are running Ryton sumps, I encourage you to inspect them very closely and very regularly. Like every time you fly. Two of these sumps that have broken here have actually broken into pieces that fell out onto the ground below the aircraft. The others have just cracked. In the case of my sump, the engine still ran fine with the cracked sump. Had we had the engine cowled, I would have had no reason to uncowl it to inspect it before going flying. Had the lower part of the sump (where the fuel servo mounts) broken off in flight, I am sure it would have ruined my day. bob rv7a last few things plus a new induction system ________________________________________________________________________________
Date: May 17, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Ryton sumps
Didn't Superior just sell the company off to a German company. My experience in the past when a company has a massive design problem with their product line, they end up selling it off to another company, who of course does not support the old line. Both times in the past it was with electronic items not engine parts. Is that an effort to avoid liability? I wounder it the German company knew about this before they bought it? Not saying this is Superior's reason for the buy out, but I see this time and time again, a company sell off ownership preceded by some massive design or QC screw up of a product or line of products. I guess there is something to be said for certified parts that have stood the test of time. George RV-7 __________________________________________________ ________________________________________________________________________________
Date: May 17, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: AD compliance documentation questions
We are experimental amateur built and don't have to meet any AD or is there any log book entry or maintenance regulation. All we have to do is have a condition inspection sign off in the last 12 months. Bottom line we have NO regulations and our aircraft are not certified or need to meet any particular regulation (unless noted in the operating limitations). However from a common sense stand point and what I do is comply with AD's on my engine. I was on the fence about changing the prop Gov oil line from aluminum to a stainless steel part. If the aluminum is properly supported, chance of failure is nil (by the fact for many decades, on many planes, flown many hours with no problem). I ended up changing it because the parts where fairly cheap. Ramp checks? Who has been ramped checked? I get checked about once a year, but that is airline flying. In private flying or as a corporate or CFI pilot instructor, never in 20 years of flying. The chance is your more likely to get ramped from a law officer because you just did a buzz job or wants to know if you paied the state sales / use tax on the plane. We have great freedom lets not goof it up by doing dumb things. Right now the FAA has a healthy we don't need to know and don't want to know, you are experimental, RIGHT wink wink nod nod. Fact is the FAA has a hard enough time doing their other jobs. This may be a hit on our collective ego's, but flying little planes that mostly seat two people is not a priority. However as HOMEBUILTS have progressed into 6 place pressurized turboprops that can fly in the flight levels (well above FL180). The FAA has a hard time ignoring this since they are mixing it up with the airline traffic. I predict (it already has happened) there will be two classes of amateur homebuilt experimental, small and large (turbine). I hope we can stay off the Fed's radar and continue to enjoy minimal government oversight so we can continue to exercise judgment and self imposed (common sense) practices. I think by and large most homebuilts are very airworthy and flown safely. However if this changes things will change. Just do the prudent thing, but don't be paranoid. No one really cares about your AD status (at this time). It is experimental RIGHT? George __________________________________________________ ________________________________________________________________________________
From: "Steve Glasgow" <willfly(at)carolina.rr.com>
Subject: MA-4 carbs
Date: May 17, 2006
While I was gone on Vacation I saw a question about the MA-4-5 carb idle mixture setting, but was unable to respond do to receive only status. In the August 2004 Light Plane Maintenance periodical, I found the following: "Some MA-4 series carbs have something of a strange glitch in that you can attempt to richen the mixture with the screw, but a 25 RPM rise at altitude is all you'll get. Often these engines will have no rise at all at sea level. Not to worry. The MA-4 series will operate well despite the strange behavior, and problems are few. No not, however, back the idle mixture knob out so far that holding-spring tension is lost. There have been reports of the valve falling out in flight." To bad I did not see this before I lost mine on my first flight. Oh well. If you do loose the screw in flight, all is well till you land and the engine idles slower than in flight. When this happens you are calling for full rich, and the engine quits due to flooding. The point is, for MA-4 series only, adjust the idle mixture screw till the engine idles well on the ground and forget trying to get a rise when shutting down. Mine has been trouble free for the last 300 hours. Sometimes I see a slight rise when shutting down, but it seems to be totally dependant on atmospheric pressure and temperature. Steve Glasgow - Cappy N123SG RV-8 Cappy's Toy ________________________________________________________________________________
Subject: Ryton sumps
Date: May 17, 2006
From: "Rhonda Bewley" <Rhonda(at)bpaengines.com>
Our Cold air system is available only on the IO-540. We designed and build them as an experimental replacement for the Lycoming certified cold air sump (which costs approx. $8500) for any model parallel or angle head IO/AEIO-540. We do not have a cold air sump for the 360 engines. We tested some many years ago and found that there was no performance enhancement, so we decided not to pursue. The IO-540 Cold Air System sells for $3995 as a stand alone unit, $3495 with an engine purchase. Rhonda Barrett-Bewley Barrett Precision Engines, Inc. 2870-B N. Sheridan Rd. Tulsa, OK 74115 (918) 835-1089 phone (918) 835-1754 fax www.barrettprecisionengines.com Here's the deal: If you want a "cold air sump", there seems to be 3 choices- Ryton sump by Superior Magnesium sump by ECI Barrett Precision cold air sump All the other metal sumps out there- Aerosport Power Aero Engines Superflite Are all copies of the Lycoming cast aluminum sump (not cold air sumps) I don't have the information on the Barrett Cold Sump system, but it is the most expensive of the three. I'll post that here when I find it. ________________________________________________________________________________
From: "Joe & Jan Connell" <jconnell(at)rconnect.com>
Subject: Ryton sumps
Date: May 17, 2006
Guys, Here is an item from E-Magair regarding composite sumps. He indicates back-firing can fracture composite sumps. I hope this info is of value. I have an Aerosport O-320 with a Slick and a P-Mag... Joe Connell Stewartville, MN RV-9A, baffle & cowling ----- Original Message ----- From: Brad Dement Sent: Monday, September 05, 2005 5:49 PM Subject: Service Update Service Update Run Mode Starting Delay: Starting September, 2005 new production units (as well as units getting firmware updates after this time) will have a Run Mode Starting Delay ("RMSD") feature that will prevent plug firing until the ignition sees two (2) passes of the TDC index. At start up, this will help ventilate the intake and exhaust chambers of accumulated vapor. Normal RMSD Operation - RMSD will engage when a "normal" start up sequence is followed. i.e. The ignition is powered ON WHILE the key (or other p-lead switch) is in the OFF position. (Note: This is the same sequence used for entering Set Up Mode). Pilots then turn ON (unground) the p-lead switch and start the engine. Bypassing the RMSD - The RMSD can be bypassed (fire on the first index pass) simply by powering the ignition ON WHILE the key (or other p-lead switch) is in the ON position. This will enable prop starting, if needed. Keep in mind that bypassing RMSD will increase the possibility of igniting fuel vapor (if present) on the "wasted" side of the spark - see below. At the time of this writing, this is felt to be problematic only for those customers using composite oil sumps. For them, bypassing RMSD will risk damaging the sump. Emulating RMSD - It is also possible to emulate the RMSD manually (without the update) if you use toggle (or similar) switches instead of a key type ignition switch. Keeping the ignition p-lead switches grounded (OFF) for a few revolutions during engine start, will accomplish the same thing. Those who elect to not get the RMSD update might use this technique when performing hot starts. See below. Background - Wasted spark systems avoid the weight, mechanical complexity, and high altitude operating issues associated with traditional ignition distributors. In a wasted spark system, plugs are fired in pairs at A) the charged cylinder that's ready to ignite, as well as B) the opposing cylinder during the exhaust stroke. This second spark is not intended to ignite, hence the name "wasted spark". However, when restarting an engine shortly after shut down (a hot start), it is possible for fuel vapor to accumulate in the intake manifold. This vapor can be ignited by what is normally the "wasted" side of the spark during valve overlap. [Valve overlap is when intake and exhaust valves are momentarily open at the same time.] Even so, in the one controlled (test cell) instance where this was observed, the event itself was rather unremarkable. It was heard only as a hard "puff" prior to engine start. However, in the test cell instance, the intake manifold channeled this "puff" to the sump, which was later measured as a 15 to 20 psi pulse. This pulse cracked the light weight composite sump installed on this particular engine. An identical replacement sump did the same thing during a second hot start. When replaced with a standard aluminum sump, the problem did not recur on any subsequent (hot or cold) starts. To date, we have no other reports of sump related issues. So it's tempting (and maybe appropriate) to narrowly define this as the only configuration (fuel injection with side entry composite sumps) at risk, but we don't know that with certainty. Either way, we'd rather engage such issues with solutions, rather than require customers avoid innovative and exciting new products. So the Run Mode Starting Delay will be incorporated as a standard feature. It is also available as an upgrade (free of charge) to all customers getting a firmware update after September 1, 2005. The RMSD update is not mandatory unless you are using, or plan to use a composite sump. NOTE: RMSD is a new feature, and we cannot guarantee it will, in all cases, prevent ignition on the wasted spark side if conditions are just right. In which case, a composite sump, if used, could be damaged. We hope this update is in keeping with your expectations of E-MAG customer service and support. As always, your questions and comments are welcome and very much appreciated. Brad Dement E-MAG Ignitions 649 Boling Ranch Road Azle, Texas 76020 (817) 448-0555 ________________________________________________________________________________
Date: May 17, 2006
From: sportav8r(at)aol.com
Subject: Re: Ryton sumps
I guess if one is wired per the AeroElectric schematic for dual P-mags, that the RMSD bypass can be accomplished by use of the Ignition Maintenance Mode switch in conjunction with the progressive transfer toggles that control normal ignition operation. I have the old firmware and the Nuckolls wiring, and love the way it starts my Lycoming on the first or second blade. I'd hate to give that up for a firmware upgrade (which I need for the stumble issue) and not having a Ryton sump to fret over. -Bill B -----Original Message----- From: Joe & Jan Connell <jconnell(at)rconnect.com> Subject: Fw: RV-List: Ryton sumps Guys, Here is an item from E-Magair regarding composite sumps. He indicates back-firing can fracture composite sumps. I hope this info is of value. I have an Aerosport O-320 with a Slick and a P-Mag... Joe Connell Stewartville, MN RV-9A, baffle & cowling ----- Original Message ----- From: Brad Dement Sent: Monday, September 05, 2005 5:49 PM Subject: Service Update Service Update Run Mode Starting Delay: Starting September, 2005 new production units (as well as units getting firmware updates after this time) will have a Run Mode Starting Delay ("RMSD") feature that will prevent plug firing until the ignition sees two (2) passes of the TDC index. At start up, this will help ventilate the intake and exhaust chambers of accumulated vapor. Normal RMSD Operation - RMSD will engage when a "normal" start up sequence is followed. i.e. The ignition is powered ON WHILE the key (or other p-lead switch) is in the OFF position. (Note: This is the same sequence used for entering Set Up Mode). Pilots then turn ON (unground) the p-lead switch and start the engine. Bypassing the RMSD - The RMSD can be bypassed (fire on the first index pass) simply by powering the ignition ON WHILE the key (or other p-lead switch) is in the ON position. This will enable prop starting, if needed. Keep in mind that bypassing RMSD will increase the possibility of igniting fuel vapor (if present) on the "wasted" side of the spark - see below. At the time of this writing, this is felt to be problematic only for those customers using composite oil sumps. For them, bypassing RMSD will risk damaging the sump. Emulating RMSD - It is also possible to emulate the RMSD manually (without the update) if you use toggle (or similar) switches instead of a key type ignition switch. Keeping the ignition p-lead switches grounded (OFF) for a few revolutions during engine start, will accomplish the same thing. Those who elect to not get the RMSD update might use this technique when performing hot starts. See below. Background - Wasted spark systems avoid the weight, mechanical complexity, and high altitude operating issues associated with traditional ignition distributors. In a wasted spark system, plugs are fired in pairs at A) the charged cylinder that's ready to ignite, as well as B) the opposing cylinder during the exhaust stroke. This second spark is not intended to ignite, hence the name "wasted spark". However, when restarting an engine shortly after shut down (a hot start), it is possible for fuel vapor to accumulate in the intake manifold. This vapor can be ignited by what is normally the "wasted" side of the spark during valve overlap. [Valve overlap is when intake and exhaust valves are momentarily open at the same time.] Even so, in the one controlled (test cell) instance where this was observed, the event itself was rather unremarkable. It was heard only as a hard "puff" prior to engine start. However, in the test cell instance, the intake manifold channeled this "puff" to the sump, which was later measured as a 15 to 20 psi pulse. This pulse cracked the light weight composite sump installed on this particular engine. An identical replacement sump did the same thing during a second hot start. When replaced with a standard aluminum sump, the problem did not recur on any subsequent (hot or cold) starts. To date, we have no other reports of sump related issues. So it's tempting (and maybe appropriate) to narrowly define this as the only configuration (fuel injection with side entry composite sumps) at risk, but we don't know that with certainty. Either way, we'd rather engage such issues with solutions, rather than require customers avoid innovative and exciting new products. So the Run Mode Starting Delay will be incorporated as a standard feature. It is also available as an upgrade (free of charge) to all customers getting a firmware update after September 1, 2005. The RMSD update is not mandatory unless you are using, or plan to use a composite sump. NOTE: RMSD is a new feature, and we cannot guarantee it will, in all cases, prevent ignition on the wasted spark side if conditions are just right. In which case, a composite sump, if used, could be damaged. We hope this update is in keeping with your expectations of E-MAG customer service and support. As always, your questions and comments are welcome and very much appreciated. Brad Dement E-MAG Ignitions 649 Boling Ranch Road Azle, Texas 76020 (817) 448-0555 ________________________________________________________________________________
Subject: Ryton sumps
Date: May 17, 2006
From: "RV Builder (Michael Sausen)" <rvbuilder(at)sausen.net>
Just as an FYI, I know many vendors don't like to come off as pushing their products on the lists so I thought I would forward this..... Michael Sausen RV-10 #352 Working on Fuselage -----Original Message----- From: Rhonda Bewley [mailto:Rhonda(at)BPAENGINES.com] Sent: Wednesday, May 17, 2006 11:23 AM Subject: RE: RV-List: Ryton sumps Sure Michael: Barrett's Cold Air system is a vacuum impregnated magnesium casting which is durable and lightweight. The castings used to be made of aluminum, but we switched them to magnesium for the weight savings. The plenum box removes intake charge from hot oil bath, resulting in approx 15 bolt on hp in a parallel head engine. Aerobatic bosses are integrally cast, resulting in no welds to crack. The system is complete with hardware, fittings and gaskets, no additional parts to buy and may be installed with the engine already mounted. The Van's standard cowl on the RV-10 doesn't fit with our cold air because the system has horizontal induction and the inlet air is in the wrong location on the cowl. -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Rhonda Bewley Sent: Wednesday, May 17, 2006 9:34 AM Subject: RE: RV-List: Ryton sumps Our Cold air system is available only on the IO-540. We designed and build them as an experimental replacement for the Lycoming certified cold air sump (which costs approx. $8500) for any model parallel or angle head IO/AEIO-540. We do not have a cold air sump for the 360 engines. We tested some many years ago and found that there was no performance enhancement, so we decided not to pursue. The IO-540 Cold Air System sells for $3995 as a stand alone unit, $3495 with an engine purchase. Rhonda Barrett-Bewley Barrett Precision Engines, Inc. 2870-B N. Sheridan Rd. Tulsa, OK 74115 (918) 835-1089 phone (918) 835-1754 fax www.barrettprecisionengines.com Here's the deal: If you want a "cold air sump", there seems to be 3 choices- Ryton sump by Superior Magnesium sump by ECI Barrett Precision cold air sump All the other metal sumps out there- Aerosport Power Aero Engines Superflite Are all copies of the Lycoming cast aluminum sump (not cold air sumps) I don't have the information on the Barrett Cold Sump system, but it is the most expensive of the three. I'll post that here when I find it. ________________________________________________________________________________
From: "Karen and Robert Brown" <bkbrown(at)ashcreekwireless.com>
Subject: Re: Ryton sumps
Date: May 17, 2006
we do have the Ryton composite sump. Superior tells us that ours was # 11 to break. We are running slick mags. This is huge news. Up to now everyone has been repeating the mantra that the problems with the Superior ryton sump have only occurred while coupled with electronic ignitions utilizing wasted spark technology. If one has failed with mags, then I would think all those people running Lasar ignitions are now also under the same shadow of risk. Doug, do you have additional details like when/how the failure occurred? A photo posted somewhere would be most enlightening. For those of us in the same situation, I believe we should all write to Tim Archer, president of Superior, as well as Frank Thielert, who just bought Superior, and express our concerns for a rapid solution to this issue. They should pull the sumps off the market now and inform all owners of the possibility of failure and the need to inspect the induction system at the end of each flight. At the same time they need to recognize the need/market for a reliable, lightweight cold air induction system. Come on guys, this isn't rocket science. Since I have totally lost confidence in the Ryton sump (as it's currently manufactured), the solution I have been forced into is to try (and I mean try...since there are none currently available anywhere) and purchase an aftermarket cast aluminum forward facing sump. I am told the shortest lead time is several weeks, with no firm delivery date. At the time I receive it, I'll then have to completely re-do the fiberglass snorkel, the fuel lines and linkages to compensate for the different geometry of the two sumps. Superior is apparently willing to cover $1000 for reimbursement of my old sump. The new one will cost about $2200, so besides the lost 100 hours or so of labor, I'll be out an additional $1500 dollars or so. bob brown rv7a last few things, and a new induction system. ________________________________________________________________________________
Date: May 17, 2006
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: Ryton sumps
A few letters to them might help.... A few other letters might help also......EAA, AOPA, FAA -----Original Message----- >From: Karen and Robert Brown <bkbrown(at)ashcreekwireless.com> >Sent: May 17, 2006 1:25 PM >To: rv-list(at)matronics.com >Subject: Re: RV-List: Ryton sumps > > >we do have the Ryton composite sump. Superior tells us that ours was # > 11 to break. We are running slick mags. > >This is huge news. > >Up to now everyone has been repeating the mantra that the problems with >the Superior ryton sump have only occurred while coupled with electronic >ignitions utilizing wasted spark technology. If one has failed with >mags, then I would think all those people running Lasar ignitions are >now also under the same shadow of risk. Doug, do you have additional >details like when/how the failure occurred? A photo posted somewhere >would be most enlightening. > >For those of us in the same situation, I believe we should all write to >Tim Archer, president of Superior, as well as Frank Thielert, who just >bought Superior, and express our concerns for a rapid solution to this >issue. They should pull the sumps off the market now and inform all >owners of the possibility of failure and the need to inspect the >induction system at the end of each flight. At the same time they need >to recognize the need/market for a reliable, lightweight cold air >induction system. Come on guys, this isn't rocket science. > >Since I have totally lost confidence in the Ryton sump (as it's >currently manufactured), the solution I have been forced into is to try >(and I mean try...since there are none currently available anywhere) and >purchase an aftermarket cast aluminum forward facing sump. I am told >the shortest lead time is several weeks, with no firm delivery date. At >the time I receive it, I'll then have to completely re-do the fiberglass >snorkel, the fuel lines and linkages to compensate for the different >geometry of the two sumps. Superior is apparently willing to cover >$1000 for reimbursement of my old sump. The new one will cost about >$2200, so besides the lost 100 hours or so of labor, I'll be out an >additional $1500 dollars or so. > >bob brown >rv7a >last few things, and a new induction system. > > > > > > > ________________________________________________________________________________
Subject: Ryton sumps Ryton sumps Another fix or Solution
Date: May 17, 2006
From: "Condon, Philip M." <pcondon(at)mitre.org>
Cc: , , "Condon, Philip M." I made a forward facing sump out of a Lycoming magnesium casting from a B1A sump. The Normal B1A sump has a rearward machined injector mount and also has a rough cast area in the front that can be machined flat and the studs mounted to mount a front injector. I spent 90 dollars at a machine shop in my little 'berg where I live to machine the front rough cast flat and thread the studs. I cut a plate from 1/4 inch aluminum stock to make a plate for the rear hole. Works fine and when you eye-ball the sump you can see where the cast areas are identical in the front or rear. This is not a TSO/FAA/PMA/STC'ed mod, but as experimental, works great. The magnesium is light too. Not the cold air thing, but at least not subject to breakage either. I have a spare, untouched sump (as described); When I looked into this a few years ago. One salvage yard sent me one a few months after I contacted them...... then they didn't have one initially. Wires got crossed and the sent me one (with a bill for 750$). So, I wound up with two, modified the one now on my airplane--hence the spare in the garage. Maybe this is a solution for the Ryton folks........ ::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: ::::::::::::::::::::::::::::::::::::::::::::: I've been on the phone all day researching this topic. Thanks for pointing me in the right direction Gary. Here's the deal: If you want a "cold air sump", there seems to be 3 choices- Ryton sump by Superior Magnesium sump by ECI Barrett Precision cold air sump All the other metal sumps out there- Aerosport Power Aero Engines Superflite Are all copies of the Lycoming cast aluminum sump (not cold air sumps) The Ryton sump (by Superior Engines) we've discussed before here, it costs 1000 to 1300 dollars and will break when used with a wasted spark electronic ignition system...if not sooner, then later. You might not know it's broken unless you inspect it closely like I did. Superior does not see the magnitude of the problem of the sumps it has in the field, but is currently in a "redesign" of the Ryton sump to address the wasted spark ignition issue. The new sump is expected out by October. Based on other new product announcements, I wouldn't look for it a day sooner. ....................................................................... .... The magnesium sump by ECI is just now becoming available and costs about $2400 including the tubes. There are two of them out there on aircraft so far. If you want to be #3, they should be ready to ship on May 22. I was told I'd have to fab a support bracket for the Bendix or AFP servo because that was "too much weight" out there for the induction portion of the sump to hold unsupported. That bothered me. The flange for mounting the fuel servo is also forward from where the Ryton sump flange is, which will mean more extensive alteration of the air snorkel to get it to fit. I don't have the information on the Barrett Cold Sump system, but it is the most expensive of the three. I'll post that here when I find it. I guess that's it... My choice will be the Superflight sump, when it's available in a few weeks. It's a clone of the Lycoming forward facing sump, so it's not a "cold air sump". I have made peace with that and decided if I get a sump that WON'T BREAK, that will be more important than a few more horsepower. All these clones of the Lycoming forward facing sump are priced about the same at $2200. I sure think there's a market out there for a well made cold air induction system...but I don't think there's a good one at a reasonable price that's available yet. For those of you who are running Ryton sumps, I encourage you to inspect them very closely and very regularly. Like every time you fly. Two of these sumps that have broken here have actually broken into pieces that fell out onto the ground below the aircraft. The others have just cracked. In the case of my sump, the engine still ran fine with the cracked sump. Had we had the engine cowled, I would have had no reason to uncowl it to inspect it before going flying. Had the lower part of the sump (where the fuel servo mounts) broken off in flight, I am sure it would have ruined my day. bob rv7a last few things plus a new induction system ________________________________________________________________________________
From: DOUGPFLYRV(at)aol.com
Date: May 17, 2006
Subject: Re: Ryton sumps
My partner (A&P) was starting the engine and it backfired and blew the bottom out of the induction plenum. He called Superior and they told him it was the 11th, but all the others were with electronic ignition. Supposed to be about 200 engines on service. Probably not likely to happen in flight but I don't feel good about it. Doug ________________________________________________________________________________
From: "Bob 1" <rv3a.1(at)comcast.net>
Subject: Re: Minimum altitude to return to airport
Date: May 17, 2006
Any one have some data points about real (not simulated) 180 deg turn to touchdown gliding performance? Jim Oke RV-6A Wpg., MB Sorta, Jim. The last guy I knew that survived a 180 emergency back to the airport did not make it. Although he survived, his aircraft was a near total and so was his passenger's face. Many surgeries needed before even a shadow of her good looks returned. No shoulder harnesses installed. FYI... Normally, a 180 turn will just put an aircraft PARALLEL with the departure runway. More than likely you will need additional turning [and time] to line up.... and then a turn [and time] in the opposite direction to utilize the departure runway. Add in downwind speed and things can get very interesting. I believe a decision to turn back to the airport is like the popularity of the lottery. There are always enough winners to keep the suckers coming. Bob - over a half century of flight ________________________________________________________________________________
Date: May 17, 2006
From: "Bob C. " <flyboy.bob(at)gmail.com>
Subject: Re: Minimum altitude to return to airport
Well I did the impossible turn and am here to tell about it . . . no dings on the aircraft either . . . it was in an old wood wing Mooney (Mk 20A) near gross, and of course it had the manual gear and flaps . . . I don't recall how high I was but I know I wasn't anywhere near 500 ft AGL (Probaly 200-350 AGL?). . . . I did have the gear up it was a cold winter day . . . the engine quit . . . I bent her around hard and got her turned back over the (7,000 ft) runway . . . popped the gear back out just before flare. I was young and brave and highly skilled (had just finished my commercial program) . . . I knew I shouldn't but thought I could and did! Don't take this as a recommendation . . . I wouldn't have made it in most aircraft . . . It scared the hell out of me and god knows whether my passengers ever flew again Good Luck! Bob in SE Iowa On 5/17/06, Bob 1 wrote: > > > Any one have some data points about real (not simulated) 180 deg turn > to touchdown gliding performance? > > Jim Oke > RV-6A > Wpg., MB > > > Sorta, Jim. > The last guy I knew that survived a 180 emergency back to the airport did > not make it. > Although he survived, his aircraft was a near total and so was his > passenger's face. > Many surgeries needed before even a shadow of her good looks returned. > No shoulder harnesses installed. > > FYI... > Normally, a 180 turn will just put an aircraft PARALLEL with the departure > runway. > More than likely you will need additional turning [and time] to line up.... > and then a turn [and time] in the opposite direction to utilize the > departure runway. > Add in downwind speed and things can get very interesting. > > I believe a decision to turn back to the airport is like the popularity of > the lottery. > There are always enough winners to keep the suckers coming. > > Bob - over a half century of flight > > ________________________________________________________________________________
Date: May 17, 2006
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: Ryton sumps
gmcjetpilot(at)yahoo.com wrote: > >Didn't Superior just sell the company off to a German company. > > My experience in the past when a company has a massive design problem with their product line, they end up selling it off to another company, who of course does not support the old line. Both times in the past it was with electronic items not engine parts. Is that an effort to avoid liability? I wounder it the German company knew about this before they bought it? > > Not saying this is Superior's reason for the buy out, but I see this time and time again, a company sell off ownership preceded by some massive design or QC screw up of a product or line of products. > > I guess there is something to be said for certified parts that have stood the test of time. > > George RV-7 > Hmmm......I seem to remember a certain certified tractor...uh...I mean a/c carb changing hands a few times over the last decade, followed shortly by an AD each time. Probably just a coincidence or 2. Or 3. :-> ________________________________________________________________________________
Date: May 17, 2006
From: "Tim Bryan" <flyrv6(at)bryantechnology.com>
Subject: Hangar question - Not RV related
Hi Listers, Like others, this is such a great resource even non RV rela ted I am drawing plans for a hangar on my own property. While the RV will fi t in a much smaller hangar, it isn't prudent (IMHO) to build a hangar that small. What is the basic size of a hangar such as the typical T-hangars at the local airport? Width, depth, and ceiling height Thanks Tim RV-6 N616TB ________________________________________________________________________________
Date: May 17, 2006
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: Hangar question - Not RV related
Hello Tim, IMHO, no smaller than 38x40 but a 40x40 would be perfect. A 12' ceiling would work just fine. Darrell Tim Bryan wrote: Hi Listers, Like others, this is such a great resource even non RV rela ted I am drawing plans for a hangar on my own property. While the RV will fi t in a much smaller hangar, it isn't prudent (IMHO) to build a hangar that small. What is the basic size of a hangar such as the typical T-hangars at the local airport? Width, depth, and ceiling height Thanks Tim RV-6 N616TB --------------------------------- ________________________________________________________________________________
Date: May 17, 2006
From: Steve Eberhart <steve(at)newtech.com>
Subject: Re: Hangar question - Not RV related
Tim Bryan wrote: > > Hi Listers, Like others, this is such a great resource even non RV rela >ted > > >I am drawing plans for a hangar on my own property. While the RV will fi >t >in a much smaller hangar, it isn't prudent (IMHO) to build a hangar that >small. What is the basic size of a hangar such as the typical T-hangars >at >the local airport? Width, depth, and ceiling height > > My friend and I are in the middle of building a new hangar to house our RV-7's. The hangar is 32' x 56' with a 40' x 10' door. Inside ceiling height is 13'. It works out pretty well with the RV's angled in. Each can get in and out without moving the other. Of course we have only had one in the hangar to check out how well it fits because the hangar isn't finished and my RV-7A isn't finished either. I will post pictures within the next couple of days. Hangar construction web page, now that is different. Steve Eberhart ________________________________________________________________________________
Date: May 17, 2006
From: "Tim Bryan" <flyrv6(at)bryantechnology.com>
Subject: Re: Hangar question - Not RV related
Thanks to all for the answers. This is about what I was thinking. My 1 70 was about 37' wingspan if I remember right. Tim -------Original Message------- From: Darrell Reiley Date: 05/17/06 15:38:53 Subject: Re: RV-List: Hangar question - Not RV related > Hello Tim, IMHO, no smaller than 38x40 but a 40x40 would be perfect. A 12' ceiling would work just fine. Darrell Tim Bryan wrote: Hi Listers, Like others, this is such a great resource even non RV rela ted I am drawing plans for a hangar on my own property. While the RV will fi t in a much smaller hangar, it isn't prudent (IMHO) to build a hangar that small. What is the basic size of a hangar such as the typical T-hangars at the local airport? Width, depth, and ceiling height Thanks Tim RV-6 N616TB --------------------------------- e big. ________________________________________________________________________________
Date: Jun 17, 2006
From: Richard Seiders <seiders(at)bellsouth.net>
Subject: Re: Hangar question - Not RV related
Tim ours is 3000sft. 50 wide 60 deep. Holds 3 rv's comfortably, but could do 4 with a little care. Dick At 07:23 PM 5/17/2006, you wrote: > > Thanks to all for the answers. This is about what I was thinking. My 1 >70 >was about 37' wingspan if I remember right. >Tim > >-------Original Message------- > >From: Darrell Reiley >Date: 05/17/06 15:38:53 >To: rv-list(at)matronics.com >Subject: Re: RV-List: Hangar question - Not RV related > > > > >Hello Tim, > > IMHO, no smaller than 38x40 but a 40x40 would be perfect. A 12' ceiling >would work just fine. > > Darrell > > >Tim Bryan wrote: > >Hi Listers, Like others, this is such a great resource even non RV rela > >ted > > >I am drawing plans for a hangar on my own property. While the RV will fi > >t >in a much smaller hangar, it isn't prudent (IMHO) to build a hangar that >small. What is the basic size of a hangar such as the typical T-hangars > >at >the local airport? Width, depth, and ceiling height > >Thanks >Tim >RV-6 N616TB > > >--------------------------------- >e >big. > > > > > > > > > > > ________________________________________________________________________________
Date: May 17, 2006
From: Craig <craigtxtx(at)yahoo.com>
Subject: Re: Hangar question - Not RV related
When it comes to hangers, no matter how big you make it, it will be "too small" in a year. Mine is 46' wide by 38' deep. I wanted a minimum 40' door to accomodate my C172 I owned when I built the hanger. That width is good for many single engine GA aircraft. The depth was a matter of how much hanger I could afford to build. After owning this hanger for three years, I wish it was larger. Craig Eastover Air Ranch, Fayetteville, NC RV8A ........ working on the canopy ________________________________________________________________________________
Date: May 17, 2006
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: Hangar question - Not RV related
Tim Bryan wrote: > > Hi Listers, Like others, this is such a great resource even non RV rela >ted > > >I am drawing plans for a hangar on my own property. While the RV will fi >t >in a much smaller hangar, it isn't prudent (IMHO) to build a hangar that >small. What is the basic size of a hangar such as the typical T-hangars >at >the local airport? Width, depth, and ceiling height > >Thanks >Tim >RV-6 N616TB > Most of the hangars on the airpark where I live are ~50x50 with 12' eaves & 12' tall x 45' bifold doors. I've seen 4 Globe Swifts & a Stinson 108 in a 50x52 hangar. (Careful fitting to do that.) If you are building on agricultural land & want to save money, find the chicken farmers in your area & ask them who builds their houses (chicken, that is). For us, the chicken house builder was waaay cheaper than any other option, except maybe do-it-yourself. Just about any desirable width; length from here to eternity. The guy we used erects the trusses on footing pads (no slab needed) so you can let the ground dry out & get well packed with vehicle traffic before pouring the slab. The interior & exterior can be as fancy as you desire after the roof is up & the slab is poured. I added a 30' wide 'lean-to' shop to my hangar, using metal purlins from a metal building supplier. 12' at the original eave, 8' at the new eave & I can taxi an RV into the shop. (~10' height at the prop location). Anything taller is pretty much wasted (for RV's) unless you go up to at least 14' eaves so you can add a mezzanine. A 12' tall bi-fold door is just barely tall enough to accept something like a Baron or big antique Biplane. Something like a Hydro-swing one-piece door will add almost 2' to the usable opening. My shop addition has 2" foam under the roof/in the walls & is at least 15 degrees cooler in the summer than the original hangar. I regret not insulating under the slab when I had it poured. I've probably told you more than you ever wanted to know; time to stop. Charlie ________________________________________________________________________________
Date: May 17, 2006
From: Dave Nellis <truflite(at)yahoo.com>
Subject: Re: MA-4 carbs
We had a club 172 quit on final due to the idle mixture needle departing the aircraft. Fortunately, the pilot was over the fence when he pulled the throttle to idle. That is when it quit. His landing was uneventful other than having to be pushed off the runway. Dave --- Steve Glasgow wrote: > > > While I was gone on Vacation I saw a question about > the MA-4-5 carb idle > mixture setting, but was unable to respond do to > receive only status. > > In the August 2004 Light Plane Maintenance > periodical, I found the > following: > > "Some MA-4 series carbs have something of a strange > glitch in that you > can attempt to richen the mixture with the screw, > but a 25 RPM rise at > altitude is all you'll get. Often these engines will > have no rise at all > at sea level. Not to worry. The MA-4 series will > operate well despite > the strange behavior, and problems are few. > > No not, however, back the idle mixture knob out so > far that > holding-spring tension is lost. There have been > reports of the valve > falling out in flight." > > To bad I did not see this before I lost mine on my > first flight. Oh > well. If you do loose the screw in flight, all is > well till you land > and the engine idles slower than in flight. When > this happens you are > calling for full rich, and the engine quits due to > flooding. > > The point is, for MA-4 series only, adjust the idle > mixture screw till > the engine idles well on the ground and forget > trying to get a rise when > shutting down. Mine has been trouble free for the > last 300 hours. > Sometimes I see a slight rise when shutting down, > but it seems to be > totally dependant on atmospheric pressure and > temperature. > > Steve Glasgow - Cappy > N123SG RV-8 > Cappy's Toy > > > > > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
From: "Dale Ensing" <densing(at)carolina.rr.com>
Subject: Re: Hangar question - Not RV related
Date: May 17, 2006
Start by checking the local building codes for hangars.Especially if you are in an airpark. Some places have limits on the foot print and the maximum height. Dale Ensing ________________________________________________________________________________
Subject: Re: not rv related
From: "Jekyll" <rcitjh(at)aol.com>
Date: May 17, 2006
That's Indian Springs air field, not Indian Hills. I saw Blue Man Group in Vegas. I've attended many concerts, shows plays and etc. in my life, all over the world but I'VE NEVER SEEN ANYTHING LIKE THIS ACT. It will blow your mind! It is clean, family fun. Well, it's not actually clean except that there's no vulgarity or not-ready-for-prime-time language. Lots of paint flying around but they don't get it on the audience. Jekyll Read this topic online here: http://forums.matronics.com/viewtopic.php?p=35154#35154 ________________________________________________________________________________
From: "RAS" <deruiteraircraftservices(at)btinternet.com>
Subject: Re: Ryton sumps
Date: May 18, 2006
----- Original Message ----- From: "BPA" <BPA(at)BPAENGINES.COM> Sent: Wednesday, May 17, 2006 8:34 PM Subject: RE: RV-List: Ryton sumps > > Regardless of what type of ignition source you have, or, which sump you snip Allen, so why then don't any other sumps give the same problem as the Ryton? regardless of make as you said in your post. The method of using the electric boost pump is described method by Lycoming to start their injected series of engines. I'm somewhat confused by your post. MJR ________________________________________________________________________________
Date: May 18, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Hangar question - Not RV related
>From: "Tim Bryan" <flyrv6(at)bryantechnology.com> > >I am drawing plans for a hangar on my own property. >While the RV will fit in a much smaller hangar, it isn't >prudent (IMHO) to build a hangar that small. What is >the basic size of a hangar such as the typical T-hangars >at the local airport? Width, depth, and ceiling height > >Thanks Tim RV-6 N616TB Tim build it as large as you can afford and have room for. Don't copy a T-hanger. I don't have dimensions but consider the largest plane you may ever put it to it. The tallest planes are Amphibian / Float planes. Consider a large twin like an Aerostar or Navajo. My plans (shelved for now) where for a hanger about 40 wide by 50 feet (dream hanger 100 feet deep). In the back was a shop and garage plus room for more than one plane. Don't forget about height. You want to may be leave room for an aircraft lift. http://www.armaerospace.com/ You forgot to mention MONEY. So build the biggest thing you can. You will not regreat having too much room. George __________________________________________________ ________________________________________________________________________________
Date: May 18, 2006
From: Bob <panamared3(at)brier.net>
Subject: Re: Hangar question - Not RV related
>Don't know what a T-Hanger size is, but built it a little bigger then >what you need whilst at it. You will never have to much room. Except when you are trying to heat or cool it. In July and August it is way too hot to work in, and then in Jan and Feb it is way to cold to work in. If you have never tried heating a 50' X 50' uninsulated metal building then you are in for a real surprise. A 250,000 BTU barn heater works great if you are standing next to it! Bob ________________________________________________________________________________
Date: May 18, 2006
From: Gary Childers <cowboy286(at)sbcglobal.net>
Subject: 0-320 E2D $10,500
0-320-E2D For Sale $10,500 removing from my 68 Cessna Cardinal for HP upgrade. 3,000 TT, 1056 SMOH, 560 STOH, new cam, main and rod bearings, and oil pump gears 130 hrs ago for oil pump repair. includes vacuume pump, starter and alternator, price is outright NO core. Contact cowboy286(at)sbcglobal.net ________________________________________________________________________________
Subject: Ryton sumps
Date: May 18, 2006
From: "BPA" <BPA(at)bpaengines.com>
Because the Ryton sump is the non metal. All others, at least that I know about, are either aluminum or magnesium mostly. When an engine backfires, there is a flame front. Continuing to crank the engine puts the flame out. Except of course with the Ryton sump. Allen -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of RAS Sent: Thursday, May 18, 2006 1:56 AM Subject: Re: RV-List: Ryton sumps ----- Original Message ----- From: "BPA" <BPA(at)BPAENGINES.COM> Sent: Wednesday, May 17, 2006 8:34 PM Subject: RE: RV-List: Ryton sumps > > Regardless of what type of ignition source you have, or, which sump you snip Allen, so why then don't any other sumps give the same problem as the Ryton? regardless of make as you said in your post. The method of using the electric boost pump is described method by Lycoming to start their injected series of engines. I'm somewhat confused by your post. MJR ________________________________________________________________________________
Date: May 18, 2006
From: sportav8r(at)aol.com
Subject: Re: Hangar question - Not RV related
Tell 'em about your parachute trick, Bob ;-) And be advised Stormy's fly-in is June 24th this year, and the LWB gang is all invited for lunch. -Bill B -----Original Message----- From: Bob <panamared3(at)brier.net> Subject: Re: RV-List: Hangar question - Not RV related >Don't know what a T-Hanger size is, but built it a little bigger then >what you need whilst at it. You will never have to much room. Except when you are trying to heat or cool it. In July and August it is way too hot to work in, and then in Jan and Feb it is way to cold to work in. If you have never tried heating a 50' X 50' uninsulated metal building then you are in for a real surprise. A 250,000 BTU barn heater works great if you are standing next to it! Bob ________________________________________________________________________________
From: Jerry2DT(at)aol.com
Date: May 18, 2006
Subject: Ryton:Sniffle Valve
... and be sure to test that sniffle valve before install. My first one from Superior leaked air in the "closed" position. Jerry Cochran In a message dated 5/18/2006 12:04:59 A.M. Pacific Daylight Time, rv-list(at)matronics.com writes: Subject: RE: RV-List: Ryton sumps From: "BPA" <BPA(at)bpaengines.com> Regardless of what type of ignition source you have, or, which sump you have be it a Ryton, ECI, Lycoming, or Happy Joes from Kokamoe, if the electric boost pump is used to prime the engine, you are getting fuel in the intake plenum, plane (only spelling I know :)and simple! That is the reason for the drain (sniffle valve). It is important that the sniffle valve be located in the LOWEST spot on the induction part of the system, with the plane at it's natural resting attitude. You have to realize that if the pump is turned on say for 5 seconds, you have to wait until you are confident that any excess fuel in the plenum has drained before you crank the engine. This is in my opinion the cause of the Ryton issue. Allen Barrett BPE, Inc -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Karen and Robert Brown Sent: Wednesday, May 17, 2006 12:43 PM Subject: Re: RV-List: Ryton sumps ________________________________________________________________________________
Date: May 18, 2006
From: Gary Childers <cowboy286(at)sbcglobal.net>
Subject: 0-320-E2D $10,500
0-320 E2D $10,500 Forgot to list mags and carb are also with it. Will be complete with mags, carb, starter, alternator, and Vac Pump cowboy286(at)sbcglobal.net ________________________________________________________________________________
Subject: Hangar question - Not RV related
Date: May 18, 2006
From: "Chuck Jensen" <cjensen(at)dts9000.com>
Bob, That's why they make radiant heaters. Heat only the object(s) you're aiming at, not the 'hole dern building. Chuck Jensen > -----Original Message----- > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > server(at)matronics.com] On Behalf Of Bob > Sent: Thursday, May 18, 2006 8:57 AM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Hangar question - Not RV related > > > > >Don't know what a T-Hanger size is, but built it a little bigger then > >what you need whilst at it. You will never have to much room. > > Except when you are trying to heat or cool it. In July and August it is > way too hot to work in, and then in Jan and Feb it is way to cold to work > in. If you have never tried heating a 50' X 50' uninsulated metal > building > then you are in for a real surprise. A 250,000 BTU barn heater works > great > if you are standing next to it! > > Bob ________________________________________________________________________________
From: PGLong(at)aol.com
Date: May 18, 2006
Subject: Canopy cover
I want to get a light weight canopy cover to travel with for my RV 4. Anyone have a favorite one that they would recommend? Pat Long PGLong(at)aol.com N120PL RV4 Bay City, Michigan 3CM Do Not Archive ________________________________________________________________________________
From: "Mike Kraus" <n223rv(at)wolflakeairport.net>
Subject: Canopy cover
Date: May 18, 2006
I don't know if this is considered light weight, but I have a Bruce's Custom Cover for my RV-4 and love it. -Mike Kraus RV-4 Flying RV-10 Fuselage -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of PGLong(at)aol.com Sent: Thursday, May 18, 2006 5:43 PM Subject: RV-List: Canopy cover I want to get a light weight canopy cover to travel with for my RV 4. Anyone have a favorite one that they would recommend? Pat Long PGLong(at)aol.com N120PL RV4 Bay City, Michigan 3CM Do Not Archive ________________________________________________________________________________
From: "Tony Marshall" <tony(at)lambros.com>
Subject: Re: Canopy cover
Date: May 18, 2006
http://kennoncovers.com These guys made a cover for my RV6 and it is great....and they were great to work with. tony marshall rv6 polson, mt ----- Original Message ----- From: <PGLong(at)aol.com> Sent: Thursday, May 18, 2006 3:43 PM Subject: RV-List: Canopy cover > > I want to get a light weight canopy cover to travel with for my RV 4. > Anyone have a favorite one that they would recommend? > > Pat Long > PGLong(at)aol.com > N120PL > RV4 > Bay City, Michigan > 3CM > > Do Not Archive > > > ________________________________________________________________________________
Date: May 18, 2006
From: Richard Dudley <rhdudley1(at)bellsouth.net>
Subject: Re: Canopy cover
Hi Pat, I have a canopy cover for my -6A that I bought from Van's. It is very light weight and is more suitable for occasional use such as traelling. I would want something heaver for continuous use if my plane were tied down all the time. I am very happy with mine for my limited outdoor use. Regards, Richard Dudley PGLong(at)aol.com wrote: > >I want to get a light weight canopy cover to travel with for my RV 4. >Anyone have a favorite one that they would recommend? > >Pat Long >PGLong(at)aol.com >N120PL >RV4 >Bay City, Michigan >3CM > >Do Not Archive > > > > > > > > > ________________________________________________________________________________
Date: May 18, 2006
Subject: Re: Hangar Question - More Info
From: Jack Haviland <jgh2(at)charter.net>
> I was kinda thinking of the T-hangar > sizes. Are they sized to accomodate most typical planes? Tim, A "typical" commercially built T-hangar intended for factory built single engine aircraft is on the order 35' deep with a clear door opening 42' wide and 12' high. Some or all of the major metal hangar building companies have charts listing the height, width and depth of a wide variety of aircraft. Check their websites e.g. FullFab and Erect-a-Tube. Jack ________________________________________________________________________________
From: "Heinrich Gerhardt" <hgerhardt(at)earthlink.net>
Subject: wing walk anti-slip
Date: May 18, 2006
Has anyone ever tried to use 3M rocker panel spray rock chip guard like this: http://multimedia.mmm.com/mws/mediawebserver.dyn?6666660Zjcf6lVs6EVs66STLKCO rrrrQ- for wing walk anti-slip? You'd have to use it between primer and top coat, so it isn't something you can add after the plane is painted. This is the same stuff that European cars have used for years on their rockers and lower fenders for rock chip protection. ________________________________________________________________________________
From: "Chopper 2" <mkellems(at)bellsouth.net>
Subject: Re: Canopy cover
Date: May 18, 2006
> I bought one from Van's for the -4 and then got one for the -3 as well -- > they are perfect for traveling. Grey in color - fit exact and lightweight > nylon (I think) with a carry bag total weight is about 3lbs. About $150 I > believe. Mike Kellems > > > I want to get a light weight canopy cover to travel with for my RV 4. > Anyone have a favorite one that they would recommend? > > Pat Long > PGLong(at)aol.com > N120PL > RV4 > Bay City, Michigan > 3CM > > Do Not Archive > > > -- > > -- ________________________________________________________________________________
From: "Steven DiNieri" <capsteve(at)adelphia.net>
Subject: wing walk anti-slip
Date: May 18, 2006
We used urethane bed liner material from the body shop that was tintable to any color. It can be color matched to any factory formula color. We actually removed the old paint on aggregate type and messed the paint up underneath. Then I masked off and scuffed the area, rolled on some bedliner and walahhh....Was tough as nails and wasn't topcoated with paint to chip off. Actually I used this stuff on the sillplates and on the canopy. Wherever ther was going to be a fair amount of wear and tear.... steve -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Heinrich Gerhardt Sent: Thursday, May 18, 2006 9:26 PM Subject: RV-List: wing walk anti-slip Has anyone ever tried to use 3M rocker panel spray rock chip guard like this: http://multimedia.mmm.com/mws/mediawebserver.dyn?6666660Zjcf6lVs6EVs66STLKCO rrrrQ- for wing walk anti-slip? You'd have to use it between primer and top coat, so it isn't something you can add after the plane is painted. This is the same stuff that European cars have used for years on their rockers and lower fenders for rock chip protection. -- -- ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Canopy cover
Date: May 18, 2006
I also have Van's cover on the RV-8. I consider it perfect for the occasional use during overnight trips. - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: Chopper 2 [mailto:mkellems(at)bellsouth.net] > Sent: Thursday, May 18, 2006 9:54 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Canopy cover > > > > I bought one from Van's for the -4 and then got one for the > -3 as well > > -- they are perfect for traveling. Grey in color - fit exact and > > lightweight nylon (I think) with a carry bag total weight is about > > 3lbs. About $150 I believe. Mike Kellems > > > > > > I want to get a light weight canopy cover to travel with > for my RV 4. > > Anyone have a favorite one that they would recommend? > > > > Pat Long > > PGLong(at)aol.com > > N120PL > > RV4 > > Bay City, Michigan > > 3CM ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: May 18, 2006
Subject: Re: wing walk anti-slip
In a message dated 05/18/2006 8:34:03 PM Central Daylight Time, hgerhardt(at)earthlink.net writes: wing walk anti-slip? Just as a suggestion, here's what I did on my plane and it has really worked out nicely- 1 year and 4 months since application and it still looks & works great- http://websites.expercraft.com/n51pw/index.php?q=log_entry&log_id=5276 Thanks, George- good tip! >From The PossumWorks in TN Mark ________________________________________________________________________________
Date: May 19, 2006
From: "Lapsley R & Sandra E. Caldwell" <caldwel(at)ictransnet.com>
Subject: Glueing Canopy
Has any one in central or South FL glued their canopy. I am about ready to start my RV-7 canopy and I would like to check out a glue job. Roger ________________________________________________________________________________
Date: May 19, 2006
From: sportav8r(at)aol.com
Subject: Re: Canopy cover
The cover from Bruce's Custom for the 6A weighs - are you ready - five pounds. It's nice, but a bit heavy for those max baggage weight camping trips to OSH. -Stormy -----Original Message----- From: Larry Bowen <Larry(at)bowenaero.com> Subject: RE: RV-List: Canopy cover I also have Van's cover on the RV-8. I consider it perfect for the occasional use during overnight trips. - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: Chopper 2 [mailto:mkellems(at)bellsouth.net] > Sent: Thursday, May 18, 2006 9:54 PM > To: rv-list(at)matronics.com > Subject: Re: RV-List: Canopy cover > > > > I bought one from Van's for the -4 and then got one for the > -3 as well > > -- they are perfect for traveling. Grey in color - fit exact and > > lightweight nylon (I think) with a carry bag total weight is about > > 3lbs. About $150 I believe. Mike Kellems > > > > > > I want to get a light weight canopy cover to travel with > for my RV 4. > > Anyone have a favorite one that they would recommend? > > > > Pat Long > > PGLong(at)aol.com > > N120PL > > RV4 > > Bay City, Michigan > > 3CM ________________________________________________________________________________
Date: May 19, 2006
Subject: Glueing Canopy
From: James H Nelson <rv9jim(at)juno.com>
Roger, I have glued my canopy on my RV9-A. I'm just finishing the slider with a fiberglass rear skirt. I'll be leaving the windshild untill I get my engine mounted and wired. You can come and see it any weekend. Let me know. Jim Nelson St. Petersburg ________________________________________________________________________________
From: "Heinrich Gerhardt" <hgerhardt(at)earthlink.net>
Subject: Re: wing walk anti-slip
Date: May 19, 2006
Thanks! That's just what I'm looking for. Heinrich Gerhardt RV-6 ready for paint >In a message dated 05/18/2006 8:34:03 PM Central Daylight Time, >hgerhardt(at)earthlink.net writes: >wing walk anti-slip? >Just as a suggestion, here's what I did on my plane and it has really >worked out nicely- 1 year and 4 months since application and it still looks & >works great- http://websites.expercraft.com/n51pw/index.php?q=log_entry&log_id=5276 Thanks, George- good tip! >From The PossumWorks in TN Mark ________________________________________________________________________________
From: "Dan Beadle" <dan.beadle(at)inclinesoftworks.com>
Subject: Sealing tank inspection covers
Date: May 19, 2006
Did you use light or medium weight Titeseal? Are there other areas that make sense to use this product? Thanks Dan -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Richard Dudley Sent: Saturday, March 11, 2006 3:04 PM Subject: RV-List: Sealing tank inspection covers FWIW If you haven't yet sealed your inspection plates onto your tanks or don't like using Pro Seal on your inspection plates, the following may be of interest to you. I originally sealed my tanks about four years ago. I've been flying for a year with about 75 hours on my RV-6A. I used the cork gaskets that were supplied with the wing kit. In the assembly process, I coated the seal area of inboard rib surface with Titeseal (that I purchased from ACS) and placed the cork gasket on the coated surface. I then coated inside mating surface of the inspection plate with the Titeseal and placed it on the gasket. I then inserted the screws and torqued them a moderate amount that resulted in a small compression of the gasket and extrusion of the Titeseal from the edges and around the screws. The original pressure test of the tanks showed no leaks around the inspection plate. After assembling the plane and filling the tanks, there were no fuel leaks around the plates. During the last few days, I removed the tanks to do the recent Service Bulletin. After removing the screws from the inspection plates, they lifted off without any effort. I then cleaned the old Tite-Seal from both the plate and the inboard rib with acetone. After doing the work for the SB, I then repeated the above procedures of Titeseal coating and assembly. The tanks are re-installed and filled with fuel with no leaks. Regards, Richard Dudley ________________________________________________________________________________
From: "Mike Robertson" <mrobert569(at)hotmail.com>
Subject: Re: AD compliance documentation questions
Date: May 19, 2006
George, While I certainly support your opinion you do have something slightly wrong in your opening statement where you say that nothing needs to be entered in your logbook except the yearly condition inspection. If you will look at your aircraft's Operating Limitations the very first paragraph should have something to the sound that you must obey the operating rules of FAR 91 and all additional limitations herein. FAR 91.407(a) states that "no person may opeate any aircraft that has undergone maintenance.....unless(1) approved for return to service by an authorized person (in this case the owner is acceptable); and (2) The maintenance record entry required by 43.9 or 43.11, as applicable, of this chapter has been made. Logbook entries for any maintenance are, therefore, required. Sorry. But compliance with AD are optional. Mike Robertson >From: <gmcjetpilot(at)yahoo.com> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: Re: AD compliance documentation questions >Date: Wed, 17 May 2006 03:51:02 -0700 (PDT) > > >We are experimental amateur built and don't have to meet any AD or is there >any log book entry or maintenance regulation. All we have to do is have a >condition inspection sign off in the last 12 months. Bottom line we have NO >regulations and our aircraft are not certified or need to meet any >particular regulation (unless noted in the operating limitations). > > However from a common sense stand point and what I do is comply with >AD's on my engine. I was on the fence about changing the prop Gov oil line >from aluminum to a stainless steel part. If the aluminum is properly >supported, chance of failure is nil (by the fact for many decades, on many >planes, flown many hours with no problem). I ended up changing it because >the parts where fairly cheap. > > Ramp checks? Who has been ramped checked? I get checked about once a >year, but that is airline flying. In private flying or as a corporate or >CFI pilot instructor, never in 20 years of flying. The chance is your more >likely to get ramped from a law officer because you just did a buzz job or >wants to know if you paied the state sales / use tax on the plane. > > We have great freedom lets not goof it up by doing dumb things. Right >now the FAA has a healthy we don't need to know and don't want to know, you >are experimental, RIGHT wink wink nod nod. Fact is the FAA has a hard >enough time doing their other jobs. This may be a hit on our collective >ego's, but flying little planes that mostly seat two people is not a >priority. However as HOMEBUILTS have progressed into 6 place pressurized >turboprops that can fly in the flight levels (well above FL180). The FAA >has a hard time ignoring this since they are mixing it up with the airline >traffic. I predict (it already has happened) there will be two classes of >amateur homebuilt experimental, small and large (turbine). > > I hope we can stay off the Fed's radar and continue to enjoy minimal >government oversight so we can continue to exercise judgment and self >imposed (common sense) practices. I think by and large most homebuilts are >very airworthy and flown safely. However if this changes things will >change. Just do the prudent thing, but don't be paranoid. No one really >cares about your AD status (at this time). It is experimental RIGHT? > > George > > __________________________________________________ > > ________________________________________________________________________________
From: "Charles Heathco" <cheathco(at)cox.net>
Subject: Lyc -320 E2A/E2d differences
Date: May 19, 2006
I have gotten conflickting info re differences, Mags being one, and Carb being the other so far. Can anyone say if I can for sure change my E2A for an E2D without a problem? Charlie Heathco Send email direct is good cheathco(at)cox.net ________________________________________________________________________________
Subject: Re: Sealing tank inspection covers
From: "Rick Galati" <rick6a(at)yahoo.com>
Date: May 19, 2006
dan.beadle(at)inclinesoft wrote: > Did you use light or medium weight Titeseal? Are there other areas that make sense to use this product? > Thanks Dan-- I too can echo Richard Dudley's experience and leak free success using Titeseal. In my case, I used MEDIUM WEIGHT Titeseal with the cork gaskets. At the time, I merely followed a suggestion offered in an Orndorff construction video. In the video, George cautioned about the potential consequences of using proseal on those fuel tank access covers. I was much inclined to agree since I worked with proseal daily for too many years and know well...even intimately...how tenacious its properties can be. Even in a highly skilled production environment there sometimes arises a need to rework an assembly after the proseal has set up and it is never fun to separate the parts, clean and prepare anew. I have not used Titeseal in any other application. A pity they don't sell the stuff in a much smaller container appropriately sized for the RV builder. Rick Galati RV-6A "Darla" 126 hours Read this topic online here: http://forums.matronics.com/viewtopic.php?p=35486#35486 ________________________________________________________________________________
Date: May 19, 2006
From: Richard Dudley <rhdudley1(at)bellsouth.net>
Subject: Re: Sealing tank inspection covers
Dan, To be sure of the answer to your question, I'll have to check my Tite Seal can at my hangar. I don't remember which I used. I plan to go to the hangar tomorrow and I'll check and let you know. I haven't used the Tite Seal anywhere else on the plane. For pipe threads I have used Seal Lube, another material that is immune to fuel and oil. Regards, Richard Dudley Dan Beadle wrote: > >Did you use light or medium weight Titeseal? > >Are there other areas that make sense to use this product? > >Thanks >Dan > >-----Original Message----- >From: owner-rv-list-server(at)matronics.com >[mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Richard Dudley >Sent: Saturday, March 11, 2006 3:04 PM >To: rv-list(at)matronics.com >Subject: RV-List: Sealing tank inspection covers > > >FWIW > >If you haven't yet sealed your inspection plates onto your tanks or >don't like using Pro Seal on your inspection plates, the following may >be of interest to you. > >I originally sealed my tanks about four years ago. I've been flying for >a year with about 75 hours on my RV-6A. >I used the cork gaskets that were supplied with the wing kit. In the >assembly process, I coated the seal area of inboard rib surface with >Titeseal (that I purchased from ACS) and placed the cork gasket on the >coated surface. I then coated inside mating surface of the inspection >plate with the Titeseal and placed it on the gasket. I then inserted the >screws and torqued them a moderate amount that resulted in a small >compression of the gasket and extrusion of the Titeseal from the edges >and around the screws. The original pressure test of the tanks showed no >leaks around the inspection plate. After assembling the plane and >filling the tanks, there were no fuel leaks around the plates. > >During the last few days, I removed the tanks to do the recent Service >Bulletin. After removing the screws from the inspection plates, they >lifted off without any effort. I then cleaned the old Tite-Seal from >both the plate and the inboard rib with acetone. After doing the work >for the SB, I then repeated the above procedures of Titeseal coating and >assembly. The tanks are re-installed and filled with fuel with no leaks. > >Regards, > >Richard Dudley > > > > > > > > > > > > > > ________________________________________________________________________________
From: "RaNDY Frost" <jamesrfrost(at)hotmail.com>
Subject: RV-4 for Sale
Date: May 19, 2006
Hey: I'm interested in both planes for different reasons. Randy Frost 678-859-1861 >From: "Jim Cimino" <jcimino(at)echoes.net> >Reply-To: rv-list(at)matronics.com >To: "RV-LIST" >Subject: RV-List: RV-4 for Sale >Date: Fri, 12 May 2006 16:51:08 -0400 > > >I am listing this for a friend of mine who has an RV-4 for sale. It has >an O-320-D1A with 310 TTAE bought new from Van's. It is VFR and is in >great shape. This is a very nice RV-4 that was built by a close friend >of mine who is a retired sheet metal fabricator. This was the 3rd RV >that he built and the workmanship is flawless. It is yellow and red. >My friend is asking $45,000 for it. If you are interested or have any >other questions you can contact Richard at rblakesl(at)ptd.net . Or I will >try to answer any questions I can for you. >Thanks, >Jim > >Jim Cimino >N7TL >RV-8 S/N 80039 >200+ Hours >http://www.geocities.com/jcimino.geo/ > > ________________________________________________________________________________
Date: May 19, 2006
From: Bobby Hester <bobbyhester(at)charter.net>
Subject: Re: wing walk anti-slip
Hey hot dog you goin to fly up tomarrow for our wings weekend? I got another toy for the panel :-) http://webpages.charter.net/bobbyhester/FWFfinishing.htm Please update your address book with my new email address: bobbyhester(at)charter.net Surfing the Web, Highspeed now, from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse-XPO360 engine :-) Fiveonepw(at)aol.com wrote: > > >>From The PossumWorks in TN >Mark > > ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Wheel Balancing
Date: May 19, 2006
After another couple of landings this week with noticable shimmy, I've decided I'm tired enough of this problem to actually do something about it. Here are the four issues I usally see when the subject of shimmy comes up: - Wheelpant balance. I balanced 'em before the first flight, so I have no idea if the balancing helped or hurt. - Gear leg stiffeners. Don't have 'em. - Wheel/tire balance. I have noticed that the gear seems more shimmy resistant on new tires. This may be a roundness or a balance issue. - Air pressure - I keep it at 22-24 lbs, so reducing it more isn't practical. My plan is to: 1) Balance the wheels and see if this helps. 2) If not...New tires (balanced). This should take roundness out of the equation. 3) If that doesn't work, I guess I'll pull off the gear leg fairings and add wood stiffeners. 4) If *that* doesn't work, I'll remove the wheel pants and related hardware. If that helps, I'll try a new set of wheel pants without balancing 'em. Anyone got a better plan? I'm all ears on this one. By the way, how do you balance aircraft wheels? I don't remember any suggestions on this. Thanks in advance, KB ________________________________________________________________________________
Date: May 19, 2006
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Re: Wheel Balancing
I already posted about this a few months ago. Check for tire roundness and then balance the wheel/tire assembly. Also applies to nosegear. My A&P has a balancing tool. Balance with motorcycle lead weights. Previous post may have been Nose wheel shimmy topic. Ron Lee ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: May 19, 2006
Subject: Wings w/e screw-up
Oh shit- is that tomorrow! Damn- I'm flying down to Orlando to talk to a guy about building a -7A for him (do ya hate me?). Will update address- hmmm- that's odd- I already got ya as bobbyhester(at)charter.net (?) I remember you going over your engine/prop decisions- what did ya wind up with & why? I also know another guy named Dan Garrett who is building a -7. He is agonizing over what to buy for his panel- wants "occasional" IFR capability. Looking at your panel you have the Dynon, Garmin audio panel, xpndr, SL30(?) and 296(?) Do you feel this is enough for his requirements- in other words, would you think just adding a 430 would make this good to go for his needs? Maybe even lose the SL30 if 430 was on board. Nice panel, by the way! so when ya gonna fire the puppy up? Brooks & I need more Middle TN formation flyers- HURRY! You heard Tommy Walker has is Phase I done? Saw him at MBT for b'fast Sat & his -6A REALLY came out nice!! Take 'er e-z & gitrdun! Mark ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: Wheel Balancing
Date: May 19, 2006
----- Original Message ----- From: "linn Walters" <pitts_pilot(at)bellsouth.net> Sent: Friday, May 19, 2006 10:23 PM Subject: Re: RV-List: Wheel Balancing > > Kyle, you need to define shimmy, and where it's from. I think that > technically, the nosewheel (or tailwheel) can have shimmy, but the mains > cannot. Shimmy is the rapid back/forth movement of a wheel located > behind a pivot point. Like a shopping cart. Another vibration can come > from the Whitman - style main gear, which I call 'walking' for lack of a > better term. My issue is the mains on a tailwheel -6. You can get several different movements on the mains. You can get a fore/aft walking thing going, but the gear can also get into a wiggle about the vertical axis where the wheel goes from toe-in to toe-out. Beyond that, the gear can also flex in and out. There are plenty of movement options to go around! The gear leg stiffeners probably best address the fore/aft movement, but that's a guess. The only times I get a shimmy (or whatever we want to define it as) is on landing or in seriously high speed taxi. Obviously, I don't know the exact speed where it begins, but I'd guess 30 mph +/-. Once it starts, the shimmy will continue down to almost walking speed. It is strange that I don't have this problem accelerating for takeoff, but I don't... > > OK, what to do about shimmy. The pivot axis needs to be as vertical as > possible. As the top of the pivot axis moves forward, the more prone to > shimmy the wheel becomes. The second thing is the drag on the nosewheel > fork. My Grumman has a castering nosewheel, and shimmy prevention is > due to the pressure on the belleville washers. Belleville washers are > cupped and you can nest and stack them for more drag as the spindle nut > is tightened. > > As for the 'walking' of the mains .... well, the only knowledge I have > is what's been on the list .... stiffeners on the gear legs. > Personally, I hate the Whitman gear. Watching the wheels lurch fore > and aft is just plain painful from an aesthetic point of view. Just my > opinion. I'd much rather have a spring gear on my -10. Blasphemy, I > know, but I'm going to consider it. Call it an experiment. But I > digress. I can see 'walking' occurring from bent discs and/or dragging > brakes or even bad bearings ...... but I don't think tire balance or > fairings contributes to either 'malfunction'. > > Here's what I'd do. Go fly. Just after liftoff, see if the vibration > goes away. If not, stomp on the brakes and see if it goes away. If it > goes away, then you have an unbalanced tire on the mains. That leaves > the nosewheel. Have someone watch you as you takeoff and land ..... > they'll be able to spot the shimmy or the walking. Work from there. > > As for balancing, jack the tire off the ground and loosen the axle nut a > little. Spin the tire a couple of times and see if one place > consistently ends up on the bottom. Aviation wheel weights are stick-on > ...... cut an inch or so and stick it on the inside of the rim on the > high side. Trim or add weight until the tire stops on a random spot. > That's all there is to it. > Linn Thanks for the response... KB ________________________________________________________________________________
Date: May 19, 2006
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Re: Wheel Balancing
Kyle, here was the first post: http://tinyurl.com/zqt2r And this: http://tinyurl.com/ku5uh To check for out of round just spin it with a stick or suitable object close to the tire (front or back). Look for even distance between the stick and the tire as it rotates. It is obvious if significantly out of round. Ron ________________________________________________________________________________
From: JEllis9847(at)aol.com
Date: May 20, 2006
Subject: Re: Glueing Canopy
Roger, You can see the glued tip-up canopy on my 9-A at the Sarasota-Bradenton airport (SRQ) in Sarasota, FL almost anytime. To see pictures go to: _http://wiki.matronics.com/wiki/index.php/Gluing_Your_Canopy_ (http://wiki.matronics.com/wiki/index.php/Gluing_Your_Canopy) Scroll down to my name. Jim Ellis RV9-A tip-up, ready for first flight ________________________________________________________________________________
From: "Ron Schreck" <ronschreck(at)alltel.net>
Subject: Sealing tank inspection covers
Date: May 20, 2006
Dan, I used the medium Teteseal to do my inspection covers originally and used it again to do the SB. It is easy to use, and easy to remove when access is required and no leaks. I have done the SB on covers which were installed with Proseal and cannot recommend that route. What a pain! Ron Schreck RV-8 "Miss Izzy" Gold Hill Airpark, NC > Did you use light or medium weight Titeseal? > Are there other areas that make sense to use this product? >Thanks >Dan ________________________________________________________________________________
Date: May 20, 2006
Subject: Re: wing walk anti-slip
From: James H Nelson <rv9jim(at)juno.com>
Mickey, Have you explored "expercraft.com". I use the web site and its free I got my build on their site. It fairly easy to use and pictures are easy to attach on each daily entry. Jim Nelson RV9-A (90599) ________________________________________________________________________________
Subject: Re: Sealing tank inspection covers
From: "Rick Galati" <rick6a(at)yahoo.com>
Date: May 20, 2006
Bob Collins wrote: > Since my tanks won't be filled for a couple of years (at least, at thisrate), is there any problem with using Titeseal now. Is there anyproblem,for example, with cork drying out and affcting it, etc. etc.?- The Titeseal is not likely to dry out. My tanks went empty for well over 2-1/2 years before the introduction of fuel. I found that over time, excess Titeseal would slowly run down the tank sides. I simply wiped the excess ooze away. The Titeseal that remains and oozes from the perimeter of the cork gaskets continues to be "gooey" to the touch and will probably remain so. My guess...and this is only a guess.....Titeseal applied to the cork gaskets now will keep them soft and flexible indefinitely and there exists much less chance of the cork drying out over time as opposed to shelving them exposed to the open air for several years. Of course, stowing the cork gaskets in an airtight ziplock bag over the long term would probably accomplish the same thing. Rick Galati RV-6A "Darla" 126 hours Read this topic online here: http://forums.matronics.com/viewtopic.php?p=35571#35571 ________________________________________________________________________________
Date: May 20, 2006
From: Dan <dan(at)rdan.com>
Subject: how mant rivet's are there ?
So, About how many rivet's are there in an RV ?? Dan -8 Elevators Snohomish WA ________________________________________________________________________________
From: "Dave Cordner" <davcor(at)comcast.net>
Subject: how mant rivet's are there ?
Date: May 20, 2006
the story I tell is 15 - 18,000 and you touch each hole about 10 times... Dave RV7 - N898DC (rsvd) Rear fuse (706-712) riveting today -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Dan Sent: Saturday, May 20, 2006 12:32 PM Subject: RV-List: how mant rivet's are there ? So, About how many rivet's are there in an RV ?? Dan -8 Elevators Snohomish WA ________________________________________________________________________________
Date: May 20, 2006
From: Richard Dudley <rhdudley1(at)bellsouth.net>
Subject: Re: Sealing tank inspection covers
Hi Dan, I used the light version of Titeseal. However, if I were to do it again, I would use the Medium. The light is low enough viscosity that any excess creeps down the root rib and across the bottom surface of the tank. I found the material had run into the sump valve. So, for several weeks, I had to remove the valve and clean a small amount Tite Seal material from it. I would expect that the viscoity of the medium would reduce that tendency. At this time, I am finding no sign of the material on the sump valves. Regards, Richard Dudley Dan Beadle wrote: > >Did you use light or medium weight Titeseal? > >Are there other areas that make sense to use this product? > >Thanks >Dan > >-----Original Message----- >From: owner-rv-list-server(at)matronics.com >[mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Richard Dudley >Sent: Saturday, March 11, 2006 3:04 PM >To: rv-list(at)matronics.com >Subject: RV-List: Sealing tank inspection covers > > >FWIW > >If you haven't yet sealed your inspection plates onto your tanks or >don't like using Pro Seal on your inspection plates, the following may >be of interest to you. > >I originally sealed my tanks about four years ago. I've been flying for >a year with about 75 hours on my RV-6A. >I used the cork gaskets that were supplied with the wing kit. In the >assembly process, I coated the seal area of inboard rib surface with >Titeseal (that I purchased from ACS) and placed the cork gasket on the >coated surface. I then coated inside mating surface of the inspection >plate with the Titeseal and placed it on the gasket. I then inserted the >screws and torqued them a moderate amount that resulted in a small >compression of the gasket and extrusion of the Titeseal from the edges >and around the screws. The original pressure test of the tanks showed no >leaks around the inspection plate. After assembling the plane and >filling the tanks, there were no fuel leaks around the plates. > >During the last few days, I removed the tanks to do the recent Service >Bulletin. After removing the screws from the inspection plates, they >lifted off without any effort. I then cleaned the old Tite-Seal from >both the plate and the inboard rib with acetone. After doing the work >for the SB, I then repeated the above procedures of Titeseal coating and >assembly. The tanks are re-installed and filled with fuel with no leaks. > >Regards, > >Richard Dudley > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Jim Cimino" <jcimino(at)echoes.net>
Subject: Re: RV-4 for Sale
Date: May 20, 2006
Here is the info for the Archer with a picture and below is contact info ro the RV-4, you can contact Rich for details and pictures of the -4. John's Archer and the equipment list: KX170B, KX175B, KT78 Transponder, KR86 ADF, KMA20 Audio, Apollo 604 Loran, 4 Place Intercom, DME, EGT/CHT. 2410 TT, 410 SMOH If you want to give him a call, here is his cell number: 570-350-4178 RV-4 Contact Rich at rblakes(at)ptd.net Let me know if you get the info. Jim ----- Original Message ----- From: "RaNDY Frost" <jamesrfrost(at)hotmail.com> Sent: Friday, May 19, 2006 9:22 PM Subject: RE: RV-List: RV-4 for Sale > > Hey: I'm interested in both planes for different reasons. > > Randy Frost > > 678-859-1861 > > >>From: "Jim Cimino" <jcimino(at)echoes.net> >>Reply-To: rv-list(at)matronics.com >>To: "RV-LIST" >>Subject: RV-List: RV-4 for Sale >>Date: Fri, 12 May 2006 16:51:08 -0400 >> >> >>I am listing this for a friend of mine who has an RV-4 for sale. It has >>an O-320-D1A with 310 TTAE bought new from Van's. It is VFR and is in >>great shape. This is a very nice RV-4 that was built by a close friend >>of mine who is a retired sheet metal fabricator. This was the 3rd RV >>that he built and the workmanship is flawless. It is yellow and red. >>My friend is asking $45,000 for it. If you are interested or have any >>other questions you can contact Richard at rblakesl(at)ptd.net . Or I will >>try to answer any questions I can for you. >>Thanks, >>Jim >> >>Jim Cimino >>N7TL >>RV-8 S/N 80039 >>200+ Hours >>http://www.geocities.com/jcimino.geo/ >> >> >> >> >> >> >> >> >> >> >> >> > > > ________________________________________________________________________________
From: "John Linman" <joplin1(at)charter.net>
Subject: HARMON ROCKET II FOR SALE
Date: May 20, 2006
I just placed this ad in Barnstormers. HARMON ROCKET II =95 PRICE SLASHED =95 I must sell this beautiful Harmon Rocket II because of my age and related health problems. Cruise with your Van RV buddies or climb at 3000 fpm and accelerate out to 230 MPH when you are in a hurry. Gets excellent MPG at economy cruise 210 to 220 miles per hour. Light fast, mini fighter with 290 HP IO-540 Lycoming, 525 hrs, 2-blade Hartzell 95 hrs SOH, King KLX135A Gps/Comm, KY97A Transceiver, KT76A Transponder, Rocky Mountain Instrument Monitor and Encoder, Full Gyros, Navaid auto pilot couples to GPS, Whelen Strobes, Dual Landing Lights, Oxygen for two people and more. Click this URL for photos and details: http://www.myplaneonline.com/N76HR.html Contact John P. Linman - located Grants Pass, OR USA =95 Telephone: 541-218-8393 =95 Posted May 20, 2006 =95 Recommend This Ad to a Friend =95 Send a Message ________________________________________________________________________________
Date: May 21, 2006
From: Charlie Kuss <chaztuna(at)adelphia.net>
Subject: Rotorway Exec 90 helicopter for sale
Listers, A friend has asked that I let you know about a Rotorway Exec 90 kit built helicopter for sale. The owner/builder of the helicopter died in a motorcycle accident 3 years ago. His widow has decided to sell off all his toys, including this helicopter. The kit was finished and flown about 3.5 to 4 years ago. It is currently partially disassembled. The tail boom and instrument panel are apart. For more information please contact Cindy at (954)648-6569 Charlie Kuss ________________________________________________________________________________
Date: May 21, 2006
From: Bobby Hester <bobbyhester(at)charter.net>
Subject: Garmin 296 features?
I have a Garmin 296 and a SL30 Nav/Com. I have read that the 296 can set the com freqs automatically on the SL30. If so can someone give me the direction for hooking this up and making it work? I also heard that it can be hooked up to the Garmin audio panel and give verbal terrain avoidance warning. How does that get hooked up? Anybody have links to these directions or any more info about these features? -- Please update your address book with my new email address: bobbyhester(at)charter.net Surfing the Web, Highspeed now, from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse-XPO360 engine :-) ________________________________________________________________________________
Date: May 21, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Garmin 296 features?
There is a serial output (two actually) that you need to hook up. You need a special garmin cable that plugs into the power port on the back and has loose wires coming out. That is for the connection to the SL30. The audio warning is done by a 1/8" stereo jack that is on the back lower corner of the unit. You can wire that to an unswitched audio on your audio panel, or if your audio panel has a 1/8" input jack, you can just get a 1/8" to 1/8" cable and plug that in. I found the terrain feature kind of annoying because it tells you to "pull up" even if you are landing at your destination airport! She get's quite frustrated and says "pull up, pull up!" in an ever increasing urgency in her voice! Paul Besing --- Bobby Hester wrote: > > > I have a Garmin 296 and a SL30 Nav/Com. > I have read that the 296 can set the com freqs > automatically on the > SL30. If so can someone give me the direction for > hooking this up and > making it work? > > I also heard that it can be hooked up to the Garmin > audio panel and give > verbal terrain avoidance warning. How does that get > hooked up? > > Anybody have links to these directions or any more > info about these > features? > > -- > Please update your address book with my new email > address: > bobbyhester(at)charter.net > Surfing the Web, Highspeed now, from Hopkinsville, > KY > Visit my web site at: > http://www.geocities.com/hester-hoptown/RVSite/ > RV7A Slowbuild wings-QB Fuse-XPO360 engine :-) > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
From: "Dale Ensing" <densing(at)carolina.rr.com>
Subject: Re: Garmin 296 features?
Date: May 22, 2006
Paul, I think you are describing the 396. Mr. Hester's question was regarding the 296 which does not have features. Dale Ensing There is a serial output (two actually) that you need to hook up. You need a special garmin cable that plugs into the power port on the back and has loose wires coming out. That is for the connection to the SL30. The audio warning is done by a 1/8" stereo jack that is on the back lower corner of the unit. You can wire that to an unswitched audio on your audio panel, or if your audio panel has a 1/8" input jack, you can just get a 1/8" to 1/8" cable and plug that in. Paul Besing --- Bobby Hester wrote: > > I have a Garmin 296 and a SL30 Nav/Com. > I have read that the 296 can set the com freqs > automatically on the > SL30. > __________________________________________________ ________________________________________________________________________________
From: "Dale Ensing" <densing(at)carolina.rr.com>
Subject: Garmin 296 features?
Date: May 22, 2006
----- Original Message ----- From: "Dale Ensing" <densing(at)carolina.rr.com> Sent: Monday, May 22, 2006 9:05 AM Subject: Re: RV-List: Garmin 296 features? > > Paul, > I think you are describing the 396. Mr. Hester's question was regarding the > 296 which does not have features. > Dale Ensing > > There is a serial output (two actually) that you need > to hook up. You need a special garmin cable that > plugs into the power port on the back and has loose > wires coming out. That is for the connection to the > SL30. The audio warning is done by a 1/8" stereo jack > that is on the back lower corner of the unit. You can > wire that to an unswitched audio on your audio panel, > or if your audio panel has a 1/8" input jack, you can > just get a 1/8" to 1/8" cable and plug that in. > > Paul Besing > > --- Bobby Hester wrote: > > > > I have a Garmin 296 and a SL30 Nav/Com. > > I have read that the 296 can set the com freqs > > automatically on the > > SL30. > > > > __________________________________________________ > > ________________________________________________________________________________
Date: May 22, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Garmin 296 features?
It's the same unit, except for the XM radio and weather. The cable is still required. Paul Besing --- Dale Ensing wrote: > > > > ----- Original Message ----- > From: "Dale Ensing" <densing(at)carolina.rr.com> > To: > Sent: Monday, May 22, 2006 9:05 AM > Subject: Re: RV-List: Garmin 296 features? > > > > > > > Paul, > > I think you are describing the 396. Mr. Hester's > question was regarding > the > > 296 which does not have features. > > Dale Ensing > > > > There is a serial output (two actually) that you > need > > to hook up. You need a special garmin cable that > > plugs into the power port on the back and has > loose > > wires coming out. That is for the connection to > the > > SL30. The audio warning is done by a 1/8" stereo > jack > > that is on the back lower corner of the unit. You > can > > wire that to an unswitched audio on your audio > panel, > > or if your audio panel has a 1/8" input jack, you > can > > just get a 1/8" to 1/8" cable and plug that in. > > > > Paul Besing > > > > --- Bobby Hester wrote: > > > > > > I have a Garmin 296 and a SL30 Nav/Com. > > > I have read that the 296 can set the com freqs > > > automatically on the > > > SL30. > > > > > > > __________________________________________________ > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
From: "Dale Ensing" <densing(at)carolina.rr.com>
Subject: Re: Garmin 296 features?
Date: May 22, 2006
Paul Besing said "It's the same unit, except for the XM radio and weather. The cable is still required." Yes, but the 296 does not have the 1/8" stereo out put. At least mine doesn't. Dale Ensing ________________________________________________________________________________
Subject: Re: Engine Problem
From: "bdjones1965" <rv_8pilot(at)hotmail.com>
Date: May 22, 2006
Flying a photo flight, your buddy was probably at a reduced power setting which could make the icing more probable. If the ice cleared up while decending through 4000' or so, then I would imagine he flew into warmer and/or dryer air. I used to have a link to a handy-dandy carb ice chart which plotted % power, RH and OAT. As I recall, the most severe icing occurred in the 70-75-F range (at high humidity and reduced power of course). But showed moderate icing could occur as low as 40-50 F and up to 90 F when near 100% RH. I'd bet your friend iced up the carburetor. 2 cents Bryan Jones -8 Houston, Texas Read this topic online here: http://forums.matronics.com/viewtopic.php?p=35774#35774 ________________________________________________________________________________
From: "John Fasching" <n1cxo320(at)salidaco.com>
Subject: Low RPM Harmful ?
Date: May 22, 2006
At our EAA Chapter meeting the gossip turned to cruise rpm settings. One pilot, who I had thought was fairly knowledgeable, said that low rpm settings (say 2000 or so) for an extended time would harm the valves. I can't see his logic and didn't have the opportunity at the meeting to question him further about his statement. My relatively uninformed view is that his idea isn't on track. Opinions from engine experts would be welcome. ________________________________________________________________________________
Date: May 22, 2006
From: Matt Dralle <dralle(at)matronics.com>
Subject: Matronics BBS Forums
Hello Listers, I just wanted to send out a reminder to all of the Listers regarding the new-ish BBS (Bulletin Board System) Forums that are available at Matronics for the Email Lists. The BBS Forums give you Web-based access into the same email content that is generated by the Email Lists. When an email message is posted to any of the email lists, a copy of the message is also copied to the respective List forum section on in the BBS Forums. By the same token, when a message is posted within the BBS Forum interface context, it will also be posted to the respective email list. Basically, the BBS Forums give you yet another method of accessing the Matronics Email List content. Some people prefer email, some prefer web forums; now you can have it either way or both with the Matronics Lists! You'll have to register for a login/password on the BBS Forum to _post_ from the BBS, but you can view message content without registering for an account. To Register for an account, look for the link at the top of the main BBS Forum page entitled "Register". Click on it and follow the instructions. Site Administrator approval will be required (to keep spammers out), but I will try to get these approved in less than 24 hours. If you haven't yet taken a look at the Matronics Email List content over on the BBS Forum, surf on over and take a peek. Its pretty cool. The URL is: http://forums.matronics.com I want to stress that the BBS Forums are simply an adjunct to the existing Matronics Email Lists; another way of viewing and interacting with the Matronics List content. If you like Email, great. If you like Web Forums, great. If you like both, great. Its up to you how you view and create your content. You will also find a URL link at the bottom of this email called Matronics List Features Navigator. You can click on this link at any time to find URL links to all of the other great features available on the Matronics site like the Archive Search Engine, List Browse, List Download, FAQs, Wiki, and lots more. There is a specific Navigator for each Email List and the link for this specific List is shown below. Thanks for all the great list participation and support; it is greatly appreciated! Matt Dralle Matronics Email List Administrator ________________________________________________________________________________
Subject: Re: Low RPM Harmful ?
From: "bdjones1965" <rv_8pilot(at)hotmail.com>
Date: May 22, 2006
n1cxo320(at)salidaco.com wrote: > At our EAA Chapter meeting the gossip turned to cruise rpm settings. One > pilot, who I had thought was fairly knowledgeable, said that low rpm > settings (say 2000 or so) for an extended time would harm the valves. > > I can't see his logic and didn't have the opportunity at the meeting to > question him further about his statement. My relatively uninformed view > is that his idea isn't on track. > > Opinions from engine experts would be welcome. I'm not an expert, but I would think he had it reversed. Higher RPM will cause greater dynamic loads on the valve train and other moving parts. Valves contact the seat when the cylinder is under compression, transferring very little load anywhere except the inside of the cylinder. Lower rpm would be easier on the moving parts, but the cumbustion chamber will see higher pressures longer. This results in higher cylinder pressure and greater blowby (if sealing is an issue). 2 cents Bryan Houston Read this topic online here: http://forums.matronics.com/viewtopic.php?p=35901#35901 ________________________________________________________________________________
Date: May 22, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Garmin 296 features?
Oh...my fault. I thought it did. Make sense, since the 296 doesn't have XM, there isn't a need for the 1/8" output. Paul Besing --- Dale Ensing wrote: > > > Paul Besing said > "It's the same unit, except for the XM radio and > weather. The cable is still required." > > Yes, but the 296 does not have the 1/8" stereo out > put. At least mine > doesn't. > Dale Ensing > > > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
Date: May 22, 2006
From: Charles Reiche <charlieray(at)optonline.net>
Subject: Re: Garmin 296 features?
The audio for the 296 for audio beeps and boops and warnings, if it has them should also live in the data cord that you would use to get "Aviation" position data or VHF freq data. Check on the tag that comes with the cable. ----- Original Message ----- From: "Paul Besing" <pbesing(at)yahoo.com> Sent: Monday, May 22, 2006 6:00 PM Subject: Re: Fw: RV-List: Garmin 296 features? > > Oh...my fault. I thought it did. Make sense, since > the 296 doesn't have XM, there isn't a need for the > 1/8" output. > > Paul Besing > > --- Dale Ensing wrote: > >> >> >> Paul Besing said >> "It's the same unit, except for the XM radio and >> weather. The cable is still required." >> >> Yes, but the 296 does not have the 1/8" stereo out >> put. At least mine >> doesn't. >> Dale Ensing >> >> >> >> >> >> >> browse >> Subscriptions page, >> FAQ, >> >> >> Admin. >> >> >> >> >> >> >> >> >> >> >> > > > __________________________________________________ > > > ________________________________________________________________________________
From: <dwhite17(at)columbus.rr.com>
Subject: New Lycoming Engine Installation
Date: May 22, 2006
Has anyone drained the Preservative Oil from their new Lycoming engine AFTER installion of the engine on the airframe? The Service Instruction No 1472 says to do it PRIOR to installing the engine, but it is not possible to install the engine and then run it within 6 months of installation. Any tips? ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: New Lycoming Engine Installation
Date: May 22, 2006
Yep, I drained my preservative oil right before my first engine run. The engine had long since been installed on the airplane. )_( Dan RV-7 N714D (912 hours) http://www.rvproject.com ----- Original Message ----- From: <dwhite17(at)columbus.rr.com> Sent: Monday, May 22, 2006 7:21 PM Subject: RV-List: New Lycoming Engine Installation > > Has anyone drained the Preservative Oil from their new Lycoming engine > AFTER installion of the engine on the airframe? The Service Instruction > No 1472 says to do it PRIOR to installing the engine, but it is not > possible to install the engine and then run it within 6 months of > installation. Any tips? > > > ________________________________________________________________________________
Date: May 22, 2006
From: Bobby Hester <bobbyhester(at)charter.net>
Subject: Re: [RV Builders] Garmin 296 features?
I'm thinking it should go somthing like this: Garmin cable on GPS: Garmin GMA340: Black = Ground Yellow = Port 1 In From my SL30 not sure what pin yet Brown = Voice + ADF In Pin #7 Connector J1 Green = Port 2 In From my autopilot (later) not sure what pin yet Red = DC Power Blue = Port 1 Out To my SL30 not sure what pin yet White = Alarm Not sure Orange = Voice - ADF Return Pin #8 Connector J1 Violete = Port 2 Out To my autopilot (later) not sure what pin yet This was just a quick look over I'll study it some more then varify with Garmin. My new email address: bobbyhester(at)charter.net Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A N857BH SB wings-QB Fuse-XPO360 engine :-) Bobby Hester wrote: > When I get time I'm going to sit down and figure out exaclly what pin > goes to what. > I looked at the Garmin cable that I have installed and here are the wires: > Black = Ground > Yellow = Port 1 In > Brown = Voice + > Green = Port 2 In > Red = DC Power > Blue = Port 1 Out > White = Alarm > Orange = Voice - > Violete = Port 2 Out > >My new email address: bobbyhester(at)charter.net >Surfing the Web from Hopkinsville, KY >Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ >RV7A N857BH SB wings-QB Fuse-XPO360 engine :-) > > > > Dave Figgins wrote: > >> I have the 396 hooked to my audio panel, I use the audio output on >> the back of the 396 with a short mini jack cable to the aux input of >> my PM2000 audio panel. Seems to work fine for terrain warnings but >> have not figured out how to get other warning tones through the >> intercom (fuel timer etc). According to Garmin all the audio outputs >> go through this jack. You can get a cable from Garmin that has the >> wires free to enable you to hard wire power audio and serial in/out. >> Dave >> >> ------------------------------------------------------------------------ >> From: RV7A(at)yahoogroups.com [mailto:RV7A(at)yahoogroups.com] On Behalf Of >> Bobby Hester >> Sent: Sunday, May 21, 2006 7:26 PM >> To: RV-List; RV7A >> Subject: [RV Builders] Garmin 296 features? >> >> I have a Garmin 296 and a SL30 Nav/Com. >> I have read that the 296 can set the com freqs automatically on the >> SL30. If so can someone give me the direction for hooking this up and >> making it work? >> >> I also heard that it can be hooked up to the Garmin audio panel and give >> verbal terrain avoidance warning. How does that get hooked up? >> >> Anybody have links to these directions or any more info about these >> features? >> >> -- >> Please update your address book with my new email address: >> bobbyhester(at)charter.net >> Surfing the Web, Highspeed now, from Hopkinsville, KY >> Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ >> RV7A Slowbuild wings-QB Fuse-XPO360 engine :-) > > > The RV Aircraft Builders Group > > > SPONSORED LINKS > Family reunion > <http://groups.yahoo.com/gads?t=ms&k=Family+reunion&w1=Family+reunion&w2=Aviation+school&w3=Plane+tickets&w4=Charter+plane&w5=Aviation+headset&c=5&s=101&.sig=saH-2YDdiNlrMxaQLxLrfQ> > Aviation school > <http://groups.yahoo.com/gads?t=ms&k=Aviation+school&w1=Family+reunion&w2=Aviation+school&w3=Plane+tickets&w4=Charter+plane&w5=Aviation+headset&c=5&s=101&.sig=cjWB8GRwKv5Uz5jKzlcPDw> > Plane tickets > <http://groups.yahoo.com/gads?t=ms&k=Plane+tickets&w1=Family+reunion&w2=Aviation+school&w3=Plane+tickets&w4=Charter+plane&w5=Aviation+headset&c=5&s=101&.sig=bI7w_J2BWUncI7wuOyb8iw> > > Charter plane > <http://groups.yahoo.com/gads?t=ms&k=Charter+plane&w1=Family+reunion&w2=Aviation+school&w3=Plane+tickets&w4=Charter+plane&w5=Aviation+headset&c=5&s=101&.sig=Vr2y7jdOh-aD-lYP1YW3Eg> > Aviation headset > <http://groups.yahoo.com/gads?t=ms&k=Aviation+headset&w1=Family+reunion&w2=Aviation+school&w3=Plane+tickets&w4=Charter+plane&w5=Aviation+headset&c=5&s=101&.sig=qfyQdo1ehHCPdcZQoKzEFQ> > > > ------------------------------------------------------------------------ > YAHOO! GROUPS LINKS > > * Visit your group "RV7A <http://groups.yahoo.com/group/RV7A>" on > the web. > > * To unsubscribe from this group, send an email to: > RV7A-unsubscribe(at)yahoogroups.com > > > * Your use of Yahoo! Groups is subject to the Yahoo! Terms of > Service <http://docs.yahoo.com/info/terms/>. > > > ------------------------------------------------------------------------ > ________________________________________________________________________________
Date: May 22, 2006
From: Walter Tondu <walter(at)tondu.com>
Subject: Re: New Lycoming Engine Installation
On 05/22 7:42, Dan Checkoway wrote: > Yep, I drained my preservative oil right before my first engine run. The > engine had long since been installed on the airplane. > > )_( Dan > RV-7 N714D (912 hours) > http://www.rvproject.com Ditto. Make sure to pull the plugs and get them good and clean. Lots of, uh, stuff in there. :) -- Walter Tondu http://www.rv7-a.com Flying! ________________________________________________________________________________
From: LessDragProd(at)aol.com
Date: May 23, 2006
Subject: Re: Low RPM Harmful ?
If all else fails, read the manual. For the engine side of the system: Figure 3-17 & 3-19 are similar for the IO-540-C & -D engines. Minimum RPM & Maximum MP continuous power settings are 1800 RPM @ 25" MP to 2200 RPM @ 29" MP. For the propeller side of the system: MT Propeller engineering says these engine power settings are acceptable with the RV-10 MT Propeller. Does anyone know what is acceptable for the RV-10 Hartzell propeller? Regards, Jim Ayers In a message dated 05/22/2006 9:24:59 AM Pacific Daylight Time, n1cxo320(at)salidaco.com writes: --> RV-List message posted by: "John Fasching" At our EAA Chapter meeting the gossip turned to cruise rpm settings. One pilot, who I had thought was fairly knowledgeable, said that low rpm settings (say 2000 or so) for an extended time would harm the valves. I can't see his logic and didn't have the opportunity at the meeting to question him further about his statement. My relatively uninformed view is that his idea isn't on track. Opinions from engine experts would be welcome. ________________________________________________________________________________
Subject: Who is this guy?
From: "Rick Galati" <rick6a(at)yahoo.com>
Date: May 22, 2006
Terrific low level flying. Does anybody know who the pilot is? http://www.youtube.com/watch?v=ij1qWr99qLE Rick Galati RV-6A "Darla" 128 hours Read this topic online here: http://forums.matronics.com/viewtopic.php?p=35956#35956 ________________________________________________________________________________
From: "JAMES BOWEN" <jabowenjr(at)hotmail.com>
Subject: Who is this guy?
Date: May 22, 2006
It was called treetop flyer when I saw it a few weeks back and put it out on the list for others to see. All I know is he's wearing a UW huskies cap. Probably someone out here in the west. jim bowen lake yapps, wa. >From: "Rick Galati" <rick6a(at)yahoo.com> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: Who is this guy? >Date: Mon, 22 May 2006 22:43:13 -0700 > > >Terrific low level flying. Does anybody know who the pilot is? > >http://www.youtube.com/watch?v=ij1qWr99qLE > >Rick Galati RV-6A "Darla" 128 hours > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=35956#35956 > > ________________________________________________________________________________
From: "Scott Brown" <cptbuzz(at)adelphia.net>
Subject: RV4 for sale
Date: May 23, 2006
Guys, I am selling my RV4. I have it listed on ebay now, item number 4643128671. If you or anyone you know is interested, please email me. Thanks! Scott ________________________________________________________________________________
Subject: Re: Low RPM Harmful ?
Date: May 23, 2006
From: "Chuck Jensen" <cjensen(at)dts9000.com>
Bryan, Intuition is a strong force....that's often wrong. While the argument of engine life v. operating will not be settled soon, primarily because there is no one single answer, Aviation Consumer did a 'study' of the issue and canvassed many of the engine builders and over haulers and looked at, in detail, peak cylinder pressures and other issues of running at high v. low rpm. In short, the consensus was running at higher rpm and higher hp output equated well with engine life for a variety of reasons, but upper most among them was stress on the engine. The worst power configuration was low rpm, high power output. As rpm went up, stress was reduced. The cylinder wear from more linear feet of piston travel was also counter-intuitive. The cylinder wear was more a function of peak pressures, which were lower at higher rpm; hence higher rpm operations reduced cylinder wear. We always need to remember, 'for every complex question, there is a simple answer---that's wrong.' Chuck Jensen I slept at a Holiday Inn last night. > -----Original Message----- > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > server(at)matronics.com] On Behalf Of bdjones1965 > Sent: Monday, May 22, 2006 5:44 PM > To: rv-list(at)matronics.com > Subject: RV-List: Re: Low RPM Harmful ? > > > > n1cxo320(at)salidaco.com wrote: > > At our EAA Chapter meeting the gossip turned to cruise rpm settings. One > > pilot, who I had thought was fairly knowledgeable, said that low rpm > > settings (say 2000 or so) for an extended time would harm the valves. > > > > I can't see his logic and didn't have the opportunity at the meeting to > > question him further about his statement. My relatively uninformed view > > is that his idea isn't on track. > > > > Opinions from engine experts would be welcome. > > I'm not an expert, but I would think he had it reversed. Higher RPM will > cause greater dynamic loads on the valve train and other moving parts. > Valves contact the seat when the cylinder is under compression, > transferring very little load anywhere except the inside of the cylinder. > > Lower rpm would be easier on the moving parts, but the cumbustion chamber > will see higher pressures longer. This results in higher cylinder > pressure and greater blowby (if sealing is an issue). > > 2 cents > > Bryan > Houston > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=35901#35901 > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Date: May 23, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: RV: Low RPM Harmful ?
Great question. With gas prices what they are flying at low power is a great idea. The idea of saving wear on the engine not so much. I am no expert but Lycoming is, and here is a key reprint (article) from Lycomings Flyer publication. http://www.lycoming.textron.com/main.jsp?bodyPage=support/publications/keyReprints/operation/lowPowerLowRPM.html Bottom line engine parameters should be within limits (for my O360A1A): CHT: 280-400F* Oil Temp: 185-210F* *(These are all personal limits, 190F OT is what I like to see; much lower than this you are not buring off the water from conbustion fully and it stays in your crank case. 300F CHT is as cold as I like to see. Below that you can get more lead deposits.) See your manual for proper limits. also http://www.lycoming.textron.com/main.jsp?bodyPage=support/publications/keyReprints/operation/leaningEngines.html http://www.lycoming.textron.com/main.jsp?bodyPage=support/publications/keyReprints/operation/properLeaning.html http://www.lycoming.textron.com/main.jsp?bodyPage=support/publications/keyReprints/operation/powerSettings.html You also have to watch prop limits. In my case I have a no 2000-2500rpm continuous ops stay out range. I could fly at 1950 rpm but that is not quite enough get up an go for me. However is I was circling and going for endurance I could go 1900 RPM. IT is all about percent power. For my RV-7 the best L/D is down in the 100mph range, so for a real slow flight of say 120-140 mph it does not take much power. The gas burn is very low. I think more in percent power and not RPM alone. Bottom line RPM is part of the power equation and thus ECON. I don't worry about wear. A Lyc can be flown at 2,700 rpm all day. The reason is GAS. Cheers George >From: "John Fasching" <n1cxo320(at)salidaco.com> > >At our EAA Chapter meeting the gossip turned to cruise rpm settings. >One pilot, who I had thought was fairly knowledgeable, said that low rpm >settings (say 2000 or so) for an extended time would harm the valves. > >I can't see his logic and didn't have the opportunity at the meeting to >question him further about his statement. My relatively uninformed view >is that his idea isn't on track. > >Opinions from engine experts would be welcome. __________________________________________________ ________________________________________________________________________________
Date: May 23, 2006
From: George Inman 204 287 8334 <ghinman(at)mts.net>
Subject: Engine Problem
Go to this site http://www.tc.gc.ca/CivilAviation/publications/tp14371/AIR/2-1.htm#2-3 scroll down to the carb ice chart and compare it to the temp and dew point on that day. >All, I have a friend who was recently flying a photo shoot at 9500' in a Cessna >when the engine began running rough. He quickly pulled carb heat and >the engine began running normally, but as soon as he pushed in the carb heat >control, the engine began running rough again. > >As he descended to around 4000' feet, the engine began running fine without >using carb heat. Disassembly of the carb has revealed no problem. Any ideas >about what could be the cause? Carb Ice, maybe? > >Walt Shipley -- George H. Inman ghinman(at)mts.net ________________________________________________________________________________
Date: May 23, 2006
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Crouch Strap
Can someone scan a copy of Van's Crotch Strap Instructions for an RV7A (pdf) to me to review? Darrell --------------------------------- with Voice. ________________________________________________________________________________
From: PSPRV6A(at)aol.com
Date: May 23, 2006
Subject: Re: RV-List Digest: 26 Msgs - 05/22/06 Carb ice
One of the best carb ice detectors is EGT. Carbureted Lycomings will develop small amounts of ice under surprisingly clear conditions. The first symptom if you are cruising fully leaned will be a small drop in EGT, no change in power. If EGT recovers to normal lean cruise temp after a SHORT application of carb heat, you had a trace of ice. This is common on those perfect clear mornings. 25 years of flying the same Cessna with the 0-320 E2D engine gave lots of familiarity with this. Paul S. Petersen, RV6A building, flying soon ________________________________________________________________________________
Date: May 23, 2006
From: "Vern W." <highflight1(at)gmail.com>
Subject: Re: Low RPM Harmful ?
All engines are engineered to operate at peak levels for their designed purpose. Operating at anything other than at those peak levels (over OR under) introduces various non-desireable effects on the engine. RPM, if operated within the engines limits (even at upper limits) is not a "stressor" to the engine. Operating at low RPMs and at high torque loads is . When I was a "kid" (20 years old), I rode with a couple of friends quite a bit and they typically "lugged" their Harleys along at 12 or 14 hundred RPM s while I always let my Sportster "sing" along at 2500 to 2800 RPM's and I never had any mechanical failures nor carbon build up like my friends did. In fact, that 1970 Sportster I bought new back then is still in my garage waiting to be taken for another ride :-) I think the best way to make a Lycoming last beyond it's 2000 hours is to run it at 2500 to 2700 all day long and change oil every 25 hours. But maybe that's just me. Vern RV7-A On 5/23/06, Chuck Jensen wrote: > > > Bryan, > > Intuition is a strong force....that's often wrong. While the argument > of engine life v. operating will not be settled soon, primarily because > there is no one single answer, Aviation Consumer did a 'study' of the > issue and canvassed many of the engine builders and over haulers and > looked at, in detail, peak cylinder pressures and other issues of > running at high v. low rpm. > > In short, the consensus was running at higher rpm and higher hp output > equated well with engine life for a variety of reasons, but upper most > among them was stress on the engine. The worst power configuration was > low rpm, high power output. As rpm went up, stress was reduced. The > cylinder wear from more linear feet of piston travel was also > counter-intuitive. The cylinder wear was more a function of peak > pressures, which were lower at higher rpm; hence higher rpm operations > reduced cylinder wear. > > We always need to remember, 'for every complex question, there is a > simple answer---that's wrong.' > > Chuck Jensen > I slept at a Holiday Inn last night. > > > -----Original Message----- > > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > > server(at)matronics.com] On Behalf Of bdjones1965 > > Sent: Monday, May 22, 2006 5:44 PM > > To: rv-list(at)matronics.com > > Subject: RV-List: Re: Low RPM Harmful ? > > > > > > > > n1cxo320(at)salidaco.com wrote: > > > At our EAA Chapter meeting the gossip turned to cruise rpm settings. > One > > > pilot, who I had thought was fairly knowledgeable, said that low rpm > > > settings (say 2000 or so) for an extended time would harm the > valves. > > > > > > I can't see his logic and didn't have the opportunity at the meeting > to > > > question him further about his statement. My relatively uninformed > view > > > is that his idea isn't on track. > > > > > > Opinions from engine experts would be welcome. > > > > I'm not an expert, but I would think he had it reversed. Higher RPM > will > > cause greater dynamic loads on the valve train and other moving parts. > > Valves contact the seat when the cylinder is under compression, > > transferring very little load anywhere except the inside of the > cylinder. > > > > Lower rpm would be easier on the moving parts, but the cumbustion > chamber > > will see higher pressures longer. This results in higher cylinder > > pressure and greater blowby (if sealing is an issue). > > > > 2 cents > > > > Bryan > > Houston > > > > > > > > > > Read this topic online here: > > > > http://forums.matronics.com/viewtopic.php?p=35901#35901 > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ======================= ========= ======================= ========= ======================= ========= ======================= ========= > > ________________________________________________________________________________
Subject: Re: Low RPM Harmful ?
From: "bdjones1965" <rv_8pilot(at)hotmail.com>
Date: May 23, 2006
highflight1(at)gmail.com wrote: > All engines are engineered to operate at peak levels for their > designed purpose. Operating at anything other than at those peak levels > (over OR under) introduces various non-desireable effects on the engine. > > RPM, if operated within the engines limits (even at upper limits) is not a > "stressor" to the engine. Operating at low RPMs and at high torque loads is Excellent discussion topic. But a couple of points to make: 1. RPM certainly is a factor to a mechanical device. That's why there's a red line. 2. The are many factors in recip engine life/wear. Some involve *driving* components (pistons, rods, crank...), and some involve *driven* components (valve train, accessory devices...). To say low rpm ops cause the most damage is not absolute, any more than saying high rpm ops will cause the most damage. Personally, these (Lycomings) have such short stroke already, I don't feel too comfortable with extended low rpm ops. Aside from OEM limits, I don't like operating below 2300 or oversquare in any instance. 95 % of my time is spent 2350 to 2400 rpm. General - yes. But it's just my thing. another 2 cents Bryan Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36046#36046 ________________________________________________________________________________
Subject: RV-9 Gear legs interfere with lower firewall
From: Gerry Filby <gerf(at)gerf.com>
Date: May 23, 2006
Apparently this is well documented in the community but not at all by Vans. Installing the eninge mount on my RV-9 (taildragger) I noticed that the gear mounting tybes interfere with the lower flange of the firewall. I trimmed the firewall back as others have, but even so I had to start eating into the lower firewall stiffener angle to get enough clearance for the gear leg. I have about 1/16" clearance between the aft side of the leg and the lower firewall angle - is that enough ? I can see that the legs have to flex, but I'm thinking the movement this close to the mounting tube should be minimal. Is 16th enough clearance ? __g__ ========================================================== Gerry Filby gerf(at)gerf.com Tel: 415 203 9177 ---------------------------------------------------------- ________________________________________________________________________________
Date: May 23, 2006
From: bertrv6(at)highstream.net
Subject: Re: New Lycoming Engine Installation
Quoting dwhite17(at)columbus.rr.com: > > Has anyone drained the Preservative Oil from their new Lycoming engine > AFTER installion of the engine on the airframe? The Service Instruction > No 1472 says to do it PRIOR to installing the engine, but it is not > possible to install the engine and then run it within 6 months of > installation. Any tips? > > I left it in, until engine was installed and connected.. bert rv6a flying> > > ________________________________________________________________________________
Date: May 23, 2006
From: bertrv6(at)highstream.net
Subject: Who is this guy?
Quoting JAMES BOWEN : > > It was called treetop flyer when I saw it a few weeks back and put it out on > the list for others to see. All I know is he's wearing a UW huskies cap. > Probably someone out here in the west. > > jim bowen > lake yapps, wa. > > JIm: I am trying to see the video, but starts for a second or so, and then stops.. What I do to see the complete video? what key to push? Thanks,\\ Bert > >From: "Rick Galati" <rick6a(at)yahoo.com> > >Reply-To: rv-list(at)matronics.com > >To: rv-list(at)matronics.com > >Subject: RV-List: Who is this guy? > >Date: Mon, 22 May 2006 22:43:13 -0700 > > > > > >Terrific low level flying. Does anybody know who the pilot is? > > > >http://www.youtube.com/watch?v=ij1qWr99qLE > > > >Rick Galati RV-6A "Darla" 128 hours > > > > > > > > > >Read this topic online here: > > > >http://forums.matronics.com/viewtopic.php?p=35956#35956 > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "RV6 Flyer" <rv6_flyer(at)hotmail.com>
Subject: Re: Low RPM Harmful ?
Date: May 24, 2006
So you are telling me that the way I have been operating my engine for the past 8.75 years is not good for it and it will not make it past 1,000 hours? I typically cruse at full throttle 2,300 RPM. If I can run over square, I do. One of my favorite power settings is 2,100 RPM 22 inches MAP with a 6 GPH fuel burn. My engine has over 5,000 hours since new and over 1,850 in the RV. Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, 1,850 + Flying Hours So. CA, USA http://SoCAL_WVAF.rvproject.com ----Original Message Follows---- highflight1(at)gmail.com wrote: > All engines are engineered to operate at peak levels for their > designed purpose. Operating at anything other than at those peak levels > (over OR under) introduces various non-desireable effects on the engine. > > RPM, if operated within the engines limits (even at upper limits) is not a > "stressor" to the engine. Operating at low RPMs and at high torque loads is ________________________________________________________________________________
From: "JAMES BOWEN" <jabowenjr(at)hotmail.com>
Subject: Who is this guy?
Date: May 23, 2006
Bert, here is the link that I had to the treetop flyer. Just klick on the link and it should play. http://www.experimentalpilots.com/anrr.wmv I hope this works for you. Jim Bowen >From: bertrv6(at)highstream.net >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RE: RV-List: Who is this guy? >Date: Tue, 23 May 2006 18:59:13 -0400 > > >Quoting JAMES BOWEN : > > > > > It was called treetop flyer when I saw it a few weeks back and put it >out on > > the list for others to see. All I know is he's wearing a UW huskies cap. > > Probably someone out here in the west. > > > > jim bowen > > lake yapps, wa. > > > > JIm: I am trying to see the video, but starts for a second or so, and >then >stops.. > > What I do to see the complete video? what key to push? > >Thanks,\\ > >Bert > > > > >From: "Rick Galati" <rick6a(at)yahoo.com> > > >Reply-To: rv-list(at)matronics.com > > >To: rv-list(at)matronics.com > > >Subject: RV-List: Who is this guy? > > >Date: Mon, 22 May 2006 22:43:13 -0700 > > > > > > > > >Terrific low level flying. Does anybody know who the pilot is? > > > > > >http://www.youtube.com/watch?v=ij1qWr99qLE > > > > > >Rick Galati RV-6A "Darla" 128 hours > > > > > > > > > > > > > > >Read this topic online here: > > > > > >http://forums.matronics.com/viewtopic.php?p=35956#35956 > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Donald Harker" <dpharker(at)worldnet.att.net>
Subject: AFP Booster Pump and Filter on Firewall
Date: May 24, 2006
Working on my 7A fuselage and have the AFP BP/Filter installed per plans. Seems like too much plumbing inside the cockpit to me. Thinking of placing the pump and filter on the front of the firewall. Anybody done this or have a suggested location? Thanks Don Harker Gurnee IL 7A fuselage ________________________________________________________________________________
Subject: Re: AFP Booster Pump and Filter on Firewall
From: Gerry Filby <gerf(at)gerf.com>
Date: May 24, 2006
All the instructions I've seen from AFP say DON'T put it on the hot side of the firewall. I think heat is the major issue. If you do put it on the firewall side you will need to install a shield around it and cool it with a blast tube. g > > > > > Working on my 7A fuselage and have the AFP BP/Filter installed > per plans. > Seems like too much plumbing inside the cockpit to me. > Thinking of placing > the pump and filter on the front of the firewall. Anybody done > this or have > a suggested location? Thanks > > Don Harker > Gurnee IL > 7A fuselage > > > > > > > > > > > > > > > > -- __g__ ========================================================== Gerry Filby gerf(at)gerf.com Tel: 415 203 9177 ---------------------------------------------------------- ________________________________________________________________________________
Date: May 24, 2006
From: "D.Bristol" <dbris200(at)sbcglobal.net>
Subject: Re: AFP Booster Pump and Filter on Firewall
Mine is in the lower right corner of the firewall. I put a cover over the top of it and installed a blast tube just in case. It fit very nicely behind the landing gear (-6). I've never had a problem with it and it's easy to service the filter. Dave Donald Harker wrote: > > >Working on my 7A fuselage and have the AFP BP/Filter installed per plans. >Seems like too much plumbing inside the cockpit to me. Thinking of placing >the pump and filter on the front of the firewall. Anybody done this or have >a suggested location? Thanks > >Don Harker >Gurnee IL >7A fuselage > > > > > > > > > ________________________________________________________________________________
Subject: AFP Booster Pump and Filter on Firewall
Date: May 24, 2006
From: "Wentz, Don" <don.wentz(at)intel.com>
I initially had my AFP boost pump and filter forward of the firewall and had nothing but problems with hot fuel. After the -7 came out with the pump and filter location near the fuel selector, I moved mine there and it has worked much better, no more dead-stick landings due to hot fuel. Kind of a nice thing ;-). A carefully constructed sealed box with plenty of cool air should work, assuming you're able to fit it in without restricting access to other areas under the cowl. Dw RV-6 925hrs -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Donald Harker Sent: Wednesday, May 24, 2006 6:20 AM Subject: RV-List: AFP Booster Pump and Filter on Firewall --> Working on my 7A fuselage and have the AFP BP/Filter installed per plans. Seems like too much plumbing inside the cockpit to me. Thinking of placing the pump and filter on the front of the firewall. Anybody done this or have a suggested location? Thanks Don Harker Gurnee IL 7A fuselage ________________________________________________________________________________
From: "Michael" <cubflyr(at)comcast.net>
Subject: Low-level river flying
Date: May 24, 2006
Oh, my. Just some observations from an "old salt": First of all: cool video. I may have had less head and more scenery going by, but that's just me. Who and where: probably Washington state somewhere; Husky hat and the area/weather. Doubt seriously Rio Grand. That's just the song, "Tree Top Flyer". Written and sung here by Stephen Stills of CSN/Y fame. About running drugs. Doesn't matter who the pilot is but he seems to know his skills and airplane. He is flying here near the edge of his envelope. The RV-4 looks older from what I can see. Flying points: low level flight is very cool but your situational awareness needs to be WAY up. At 160 kts things happen in a big hurry; there is not much room for error. High G turns low down can make for a difficult day if things don't go right. This pilot obviously has done this before and on this stretch of river before, I would imagine. Some of his turns were a bit more than 45 degrees; they had to be to get around stuff. You have to be familiar with low-level flight to begin with. Things change quickly when you're in the slot. A slight breeze coming off a ridge is not a bid deal if you have more than 50 feet to play with but can make you go where you hadn't planned if you are in the river bottom. I learned to fly from a pipeline patrol pilot so most of my early hours were 50 to 100 fee off the ground. In a Cub, not fast flying RV. Low level flying takes PRACTICE, as does everything else done in an airplane. This pilot seems to be familiar with low-level. His military hair cut may or may not be a give-away. Problems with low-level: there are rules against flying close to people or people-made objects; to practice, you have to fly low-level but you can get progressively lower as you get better. Things still happen quickly. Newbie's: don't try this at home. River running has several problems and most of them are power lines. Not to mention trees and ridges. And radio stations love to put antennas in river bottoms. You occasionally meet another airplane coming the other way. Ask me how I know. If you have a low-level route, you need to be familiar with it and know it from altitude FIRST before going down on the deck. Find a flat area way out somewhere with no obstructions or people. Fly it at altitude first. Did I mention that? And you won't see the power lines until it is just a little too late if you are down low and coming on them quickly. Or even slowly. And sometimes you have to go under them to get past them. Another story. The lines are difficult to see; you look for the power poles: they are much easier to see. The roll in the video for his turn around: low level aerobatics can end poorly. Don't split-S out of a roll: there isn't enough room to recover down low. Know your airplane. Know your area. Maintain HIGH situational awareness. (This pilot even gets momentarily distracted before making his return run.) Know your own limitations. Don't show off; it isn't necessary in an airplane. Don't do this the first time with someone in the back seat. (Hey: I saw this cool video: let's go fly the river!) Watch for power poles. You can go under a power line if there is no where else to be but you should have done that under controlled conditions the first time, too, and shouldn't be in the situation that calls for that in the first place. This reminds me of watching a snow boarding video and thinking how easy that looks, then trying it yourself. Ouch. Be careful out there. IMHO, YMMV Michael RV-4 N232 Suzie Q ________________________________________________________________________________
Date: May 24, 2006
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: AFP Booster Pump and Filter on Firewall
I ordered the -7 boost pump/filter mount for my -6A - I like the way it finishes up.....much better than finding a place myself...... Ralph -----Original Message----- >From: "Wentz, Don" <don.wentz(at)intel.com> >Sent: May 24, 2006 10:58 AM >To: rv-list(at)matronics.com >Subject: RE: RV-List: AFP Booster Pump and Filter on Firewall > > >I initially had my AFP boost pump and filter forward of the firewall and >had nothing but problems with hot fuel. > >After the -7 came out with the pump and filter location near the fuel >selector, I moved mine there and it has worked much better, no more >dead-stick landings due to hot fuel. Kind of a nice thing ;-). > >A carefully constructed sealed box with plenty of cool air should work, >assuming you're able to fit it in without restricting access to other >areas under the cowl. >Dw >RV-6 925hrs > >-----Original Message----- >From: owner-rv-list-server(at)matronics.com >[mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Donald Harker >Sent: Wednesday, May 24, 2006 6:20 AM >To: rv-list(at)matronics.com >Subject: RV-List: AFP Booster Pump and Filter on Firewall > >--> > > >Working on my 7A fuselage and have the AFP BP/Filter installed per >plans. >Seems like too much plumbing inside the cockpit to me. Thinking of >placing the pump and filter on the front of the firewall. Anybody done >this or have a suggested location? Thanks > >Don Harker >Gurnee IL >7A fuselage > > > > > > > ________________________________________________________________________________
From: "Jeff Dowling" <shempdowling2(at)earthlink.net>
Subject: Re: AFP Booster Pump and Filter on Firewall
Date: May 24, 2006
I modified my 6 to put this where the plans state and it really is no problem. Shemp/Jeff Dowling RV-6A, N915JD 265 hours Chicago/Louisville ----- Original Message ----- From: "Gerry Filby" <gerf(at)gerf.com> Sent: Wednesday, May 24, 2006 9:14 AM Subject: Re: RV-List: AFP Booster Pump and Filter on Firewall > > > All the instructions I've seen from AFP say DON'T put it on the > hot side of the firewall. I think heat is the major issue. If > you do put it on the firewall side you will need to install a > shield around it and cool it with a blast tube. > > g > >> >> >> >> >> Working on my 7A fuselage and have the AFP BP/Filter installed >> per plans. >> Seems like too much plumbing inside the cockpit to me. >> Thinking of placing >> the pump and filter on the front of the firewall. Anybody done >> this or have >> a suggested location? Thanks >> >> Don Harker >> Gurnee IL >> 7A fuselage >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> >> > > -- > __g__ > > ======================================================= > Gerry Filby gerf(at)gerf.com > Tel: 415 203 9177 > ---------------------------------------------------------- > > > ________________________________________________________________________________
Date: May 24, 2006
From: Walter Tondu <walter(at)tondu.com>
Subject: Re: Who is this guy?
On 05/24 11:14, Chris W wrote: > > JAMES BOWEN wrote: > > > > >Bert, here is the link that I had to the treetop flyer. Just klick on the > >link and it should play. > > > >http://www.experimentalpilots.com/anrr.wmv > > > > > > That link gives a file not found error, I saw the video from the other > link but you can't download the file and save it from that other page. > Does anyone have copy of the video I can put on my computer? You never > know when that other site will go down and the video will be gone for good. http://rv7-a.com/videos.htm -- Walter Tondu http://www.rv7-a.com Flying! ________________________________________________________________________________
From: RVer273sb(at)aol.com
Date: May 24, 2006
Subject: Re: AFP Booster Pump and Filter on Firewall
I have my AFP fuel pump on the front of the firewall on my RV-4. 6 years and 1450 hrs later I have not had a single problem. The filter is in the tunnel. Pump is mounted to a plate that is adel clamped to the engine mount lower tubes. I have a 1in scat tube to it for cooling. Stewart, RV-4 ________________________________________________________________________________
Subject: Re: Who is this guy?
From: "kitfoxmike" <kitfoxmike(at)yahoo.com>
Date: May 24, 2006
I'm going to try and do a post to everybody here. First, what's wrong with a 45 25ft off the ground, I've done them many of times in the Fox. Haven't done one in the rv because I ain't flying one, but I think that could be doable also with a lot of practice. Flying in this video is very doable without military training, u just need to fly over the area first at a higher altitude and get use to the terrain and then fly lower and lower until you know it like the back of your hand. As far as the computer, I've own so many that I finally have a nice high speed, the hook up, once you experience the dsl you will never know how you got along with dial up. The cell phone, I hate it, but I found out a long time ago, if you don't have one on a road test(auto repair) the vehicle that you have will break down on ya and you have to walk back to the shop. Most the time I turn mine off. After all if you do get a call it's generally a bad call and depressing, so I don't let that happen. It's mainly for calling out on. Lastely, in the northwest there is a river that is called the spokane river and runs up to lake roosevelt, fort spokane. This is a cool gorge with river, the flight at 20 ft. off the water is just breathtaking. -------- kitfoxmike kitfox4 1200 912ul speedster http://www.frappr.com/kitfoxmike Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36252#36252 ________________________________________________________________________________
Subject: Re: Low-level river flying
From: "kitfoxmike" <kitfoxmike(at)yahoo.com>
Date: May 24, 2006
very good info. To add just a bit, I would suggest doing a mountain flying seminar. Golden rule when doing this kind of flying is slow down, way down, your turn radius is shorted on slow flight and raised as you go faster, hence the statement low and slow. flying low opens up a new world. I myself call anything over 1000agl nose bleed altitude. One last note, I will not go down close to the ground if there is turbulance below 1000 ft agl and if the winds are up any. Also if you are the person that has to watch your guages when landing, think again, you don't know your airplane. When you can land without any help from the guages and rely on your own insticts than you can give it a try. Generally this is called flying out the window. -------- kitfoxmike kitfox4 1200 912ul speedster http://www.frappr.com/kitfoxmike Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36259#36259 ________________________________________________________________________________
Subject: Re: AFP Booster Pump and Filter on Firewall
From: Erich_Weaver(at)URSCorp.com
Date: May 24, 2006
I can relate to the desire to avoid all the plumbing. Rather than do all the aluminum tube bending, I used various AN fittings (Earls Performance or similar) for the AFP pump (on the cool side of the firewall) to make the turns along with an appropriate flexible hose. Ok, the cost of the fittings did add up. It was easy to put together after that though, and I avoided prolonged bouts of cussing that I am prone to. Something to consider anyway Erich Weaver ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: Re: AFP Booster Pump and Filter on Firewall
Date: May 24, 2006
About using AN fittings in the fuel system, I ran across this note in the Airflow Performance installation manual: Apendix A, page A-20, Rev. A. photo: "Care must be taken to avoid the use of 90 degree fittings on the suction side of the fuel pump on high horse power applications. The more correct way would be to use a straight bulkhead fitting and a full flow 90 degree hose end to eliminate flow pressure drop." A retired mechanical engineer friend told me that way back when he was in school, his hydraulics instructor told him that three elbows is equal to a plug. It was meant to be tongue-in-cheek, but the idea was that elbows reduce flow in a way that bent tubing does not. Of course it will all depend on tubing size, horsepower, and a few other considerations, but this is why I went through a lot of tubing to get the bends right for the fuel valve and boost pump. I also used a wing root mounted Andair gascolator with my AFP system, which probably wasn't a good idea in hindsight. I did talk to AFP about it and he thought it was a wasted effort, but acceptable. Terry RV-8A #80729 Baffles finished! I can relate to the desire to avoid all the plumbing. Rather than do all the aluminum tube bending, I used various AN fittings (Earls Performance or similar) for the AFP pump (on the cool side of the firewall) to make the turns along with an appropriate flexible hose. Ok, the cost of the fittings did add up. It was easy to put together after that though, and I avoided prolonged bouts of cussing that I am prone to. Something to consider anyway Erich Weaver ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.edu>
Subject: Engine life
Date: May 24, 2006
Excessive RPM or Pressure will catastrophically destroy any engine eventually. But if you had to choose one over the other I would go for RPM to get HP as that causes more cooling for the HP gained. That said most Lycs and Continentals are rated for continuous HP at what's listed in the TC. But there's no requirement or correlation to that power setting and the suggested TBO. Generally TBOs are based upon an average of 75% power with variations in RPM throughout the testing. That doesn't mean the engine can't operate continuously at max power, it just means that if you do this it probably won't make TBO. That said, changing the oil a lot and flying a lot are the two best things you can do for your engine life as both remove or prevent moisture. Moisture causes micro pits which does the most of anything to wear out your engine. And that is straight out of about nine different aviation engine manufacturer and aviation oil manufacturer reps mouths over the years. So, go fly further or more often at 75% power for the same cost as flying less at 100% power and have more fun making sure your engine doesn't wear out. It's kinda like a sale, spend money to save money.... ;{) ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: May 24, 2006
Subject: Re: Low-level river flying
One more point to consider about power lines. They are "Structures" so legally you have to be 500 feet from them. I love the low flying and as a Highway Patrol Pilot in the California pilot I have done a lot of it. As stated above - you can go under the power lines , BUT learn under the high part of the span . > I didn't say that !!! Bob Olds RV-4 , N1191X Charleston, Arkansas ________________________________________________________________________________
From: "JAMES BOWEN" <jabowenjr(at)hotmail.com>
Subject: Re: Who is this guy?
Date: May 24, 2006
Sorry about that. I tried the link right before I added it to the email I sent it with. It was ok at that time. Your right, now it's gone. Jim Bowen >From: Walter Tondu <walter(at)tondu.com> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: Re: RV-List: Who is this guy? >Date: Wed, 24 May 2006 12:49:19 -0400 > > >On 05/24 11:14, Chris W wrote: > > > > > JAMES BOWEN wrote: > > > > > > > >Bert, here is the link that I had to the treetop flyer. Just klick on >the > > >link and it should play. > > > > > >http://www.experimentalpilots.com/anrr.wmv > > > > > > > > > > That link gives a file not found error, I saw the video from the other > > link but you can't download the file and save it from that other page. > > Does anyone have copy of the video I can put on my computer? You never > > know when that other site will go down and the video will be gone for >good. > >http://rv7-a.com/videos.htm > >-- >Walter Tondu >http://www.rv7-a.com >Flying! > > ________________________________________________________________________________
Date: May 24, 2006
From: sarg314 <sarg314(at)comcast.net>
Subject: epanelbuilder
I have been using Panel Planner and have not been happy with it. It has a lot of trouble with drawing text strings correctly and in the right place. It probably reflects my particular experience with computer cad software, but I also don't much like the user interface either. epanelbuilder looks interesting since it claims to be cross paltform compatible: I could use it with my Linux system and could thus stop using the acursed Windows, as panel planner is the only thing I ever use Windows for anyway. So.... Can any one advise me if epanelplanner actually works? Is it quirky? Can I get a useful output form from it (like autocad or some such)? Can I get printouts of x-y coordinates of things? Does it mangle text? Thanks, -- Tom Sargent, RV-6A ________________________________________________________________________________
Subject: Looking For Airport Home - Columbia, SC
Date: May 25, 2006
From: "Snow, Daniel A." <Daniel.Snow(at)wancdf.com>
My wife and I are moving to the Columbia, SC area in July and would like to buy a house near an airport or grass strip. Does anyone have any suggestions or leads? We would prefer to live on the northwest side of town. We've already been looking at Whiteplains Plantation, but it looks like prices in that residential airpark have soared in the last few years. Thanks for any ideas. Daniel Snow ________________________________________________________________________________
Date: May 25, 2006
From: "James Clark" <jclarkmail(at)gmail.com>
Subject: Re: Looking For Airport Home - Columbia, SC
Yes prices have gone up over time at Whiteplains. Probably in part due to the fact that it is almost full now. There is no (known) airpark on the NW (Lake area) part of town. I live in that area an wish there was one. :-) Whiteplains is the closest airpark. There is one to the south called "Do-Little Field". It is a grass strip and is a bit farther away. Good luck in your move! Keep in touch with us at EAA242. James On 5/25/06, Snow, Daniel A. wrote: > > > My wife and I are moving to the Columbia, SC area in July and would like > to buy a house near an airport or grass strip. Does anyone have any > suggestions or leads? We would prefer to live on the northwest side of > town. We've already been looking at Whiteplains Plantation, but it looks > like prices in that residential airpark have soared in the last few years . > > Thanks for any ideas. > > Daniel Snow > > =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D > > -- This is an alternate email. Please continue to email me at james(at)nextupventures.com . ________________________________________________________________________________
From: "Mark & Lisa" <marknlisa(at)hometel.com>
Subject: Helicopter Pilots
Date: May 25, 2006
Shouldn't you have said, "Helicopters we don't have to worry about his though... whopwhopwhopwhopwhopwhop...?" Paul Besing said: > Helicopters we don't have to worry about this > though...nanananananana... Mark Sletten Legacy FG N828LM http://www.legacyfgbuilder.com ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: Heavy Wing Experiment
Date: May 25, 2006
I tried eliminating my heavy left wing by increasing the angle of incidence of the left wingtip. The theory was advanced by Scott Risan that a change out at the tip has lots of leverage to affect roll trim. This contradicted a theory advanced by Gus Funnel that wingtips contribute nothing to lift so changes will not affect roll trim. Anyway, I went ahead and split the trailing edge of the wingtip and drilled out the rivets holding the aft wingtip rib in place. Then I flexed the now limp trailing edge 1/2" further down. Happily thinking this would solve my problem, maybe even be way too much, I removed the aileron trim tab I had been using to avoid large roll corrections opposite to my original problem, secured everything with duct tape and a couple of rivets & went flying. Bottom line: No change. Gus wins. Dave Reel - RV8A now having it's aileron trailing edge squeezed. ________________________________________________________________________________
From: "Bill VonDane" <bill(at)vondane.com>
Subject: Re: epanelbuilder
Date: May 25, 2006
Tom... The ePanel Builder does not output CAD or coordinates at all... As you said, Panel Planner does not do this very well because in general it is a very hard thing to do automatically... The difference with the ePanel Builder is that once you have figured out the final design you really want, you work with one of our partners to get your CAD work done. This way there is a human involved in the final layout and CAD work and you can be absolutely sure it is right... The ePanel Builder has a collaboration tool that allows you and the CAD guy to work on the panel online...together...at the same time to ensure you both know exactly what the final product should be... Furthermore you can take it to the next level and have your panel build for using the same collaboration tools... The goal was to try to illuminate the errors and problems associated with the Panel Planner, and the only way I see to do that is put a human back into the mix... If you use ePanel Builder to design your panel and then one of our partners to either have your CAD work done, or your panel built for you, you can be sure it will be exactly what you want... By the way, I am working on getting all of the pricing updated on all the products in the next couple of weeks... -Bill VonDane www.epanelbuilder.com www.creativair.com ----- Original Message ----- From: "sarg314" <sarg314(at)comcast.net> Sent: Wednesday, May 24, 2006 11:06 PM Subject: RV-List: epanelbuilder I have been using Panel Planner and have not been happy with it. It has a lot of trouble with drawing text strings correctly and in the right place. It probably reflects my particular experience with computer cad software, but I also don't much like the user interface either. epanelbuilder looks interesting since it claims to be cross paltform compatible: I could use it with my Linux system and could thus stop using the acursed Windows, as panel planner is the only thing I ever use Windows for anyway. So.... Can any one advise me if epanelplanner actually works? Is it quirky? Can I get a useful output form from it (like autocad or some such)? Can I get printouts of x-y coordinates of things? Does it mangle text? Thanks, -- Tom Sargent, RV-6A ________________________________________________________________________________
Subject: Re: Low-level river flying
From: "kitfoxmike" <kitfoxmike(at)yahoo.com>
Date: May 25, 2006
Gummi, So true, I responded so fast that I left out the need to maintain va and above on turns. When I went through a mountain flying seminar and did the flight instruction I got the fella that had over 20,000 hrs. way cool, we did all kinds of stuff in the mountains, one of which was to try a high speed turn and a turn at va. Really inlightening, we were in a small area and it was very appearent that the high speed turn was not going to make it. -------- kitfoxmike kitfox4 1200 912ul speedster http://www.frappr.com/kitfoxmike Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36373#36373 ________________________________________________________________________________
Subject: Re: Low-level river flying
From: "bdjones1965" <rv_8pilot(at)hotmail.com>
Date: May 25, 2006
Now this is flying!! Quite a few bayous and a few rivers in my part of the country that work nicely for this type of flying. As for speed, slow is not what you want when flying like this. Too fast reduces reaction time. Too slow, the maneuverability is reduced and proximity to stall too close. 120-140 mph depending on the nature of the turns. Reminds me of an old Cub flying expression. Accidents experience while flying slow will only barely kill you. Please hold the warnings. I know the FARs, I know my plane and I know the geography. I also know power lines are strung across, sometimes not easily seen. I never fly down a river or bayou cold. I know the area and where the obstacles are. If boats or people are on present, I'll pull up well clear. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36378#36378 ________________________________________________________________________________
Date: May 25, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: epanelbuilder
Agreed, Bill. When I did both of my panels, Steve Davis cut them for me, and I had Panel Planner the first time around. He flat out told me to not send him the CAD files, because they would have to be re worked anyway. A screen shot or printout from epanelbuilder should be all that is needed for a competent panel cutter to do the job...they have most of the databases of the instrument demensions already, so it's just a matter of taking the instruments you selected out of their library of instruments and getting them placed correctly. (Ok, not that simple, but you get the idea) Anyway, I wouldn't trust any program to output a CAD file to cut a nice piece of metal without some sort of human interface...too many variables there. Just have them build it from the layout tool which epanelbuilder was designed to do. For those of you that would like to see my new panel cut by Steve Davis, go to www.mykitlog.com/pbesing and click on the panel cutting. Paul Besing --- Bill VonDane wrote: > > > Tom... > > The ePanel Builder does not output CAD or > coordinates at all... As you > said, Panel Planner does not do this very well > because in general it is a > very hard thing to do automatically... > > The difference with the ePanel Builder is that once > you have figured out the > final design you really want, you work with one of > our partners to get your > CAD work done. This way there is a human involved > in the final layout and > CAD work and you can be absolutely sure it is > right... The ePanel Builder > has a collaboration tool that allows you and the CAD > guy to work on the > panel online...together...at the same time to ensure > you both know exactly > what the final product should be... Furthermore you > can take it to the next > level and have your panel build for using the same > collaboration tools... > > The goal was to try to illuminate the errors and > problems associated with > the Panel Planner, and the only way I see to do that > is put a human back > into the mix... If you use ePanel Builder to design > your panel and then one > of our partners to either have your CAD work done, > or your panel built for > you, you can be sure it will be exactly what you > want... > > By the way, I am working on getting all of the > pricing updated on all the > products in the next couple of weeks... > > -Bill VonDane > www.epanelbuilder.com > www.creativair.com > > > ----- Original Message ----- > From: "sarg314" <sarg314(at)comcast.net> > To: > Sent: Wednesday, May 24, 2006 11:06 PM > Subject: RV-List: epanelbuilder > > > > > I have been using Panel Planner and have not been > happy with it. It has > a lot of trouble with drawing text strings correctly > and in the right > place. It probably reflects my particular > experience with computer cad > software, but I also don't much like the user > interface either. > > epanelbuilder looks interesting since it claims to > be cross paltform > compatible: I could use it with my Linux system and > could thus stop > using the acursed Windows, as panel planner is the > only thing I ever use > Windows for anyway. > > So.... Can any one advise me if epanelplanner > actually works? Is it > quirky? Can I get a useful output form from it > (like autocad or some > such)? Can I get printouts of x-y coordinates of > things? Does it mangle > text? > > Thanks, > -- > Tom Sargent, RV-6A > > > > > > > > > > > > > > > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
Date: May 25, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Wires
Ahh..thanks for mentioning power lines, Bob...a helo pilot's worst nightmare, literally. I've had dreams at night where I'm underneath a whole network of wires and can't get out! Wake up in a cold sweat realizing it was just a dream. Yes, wires, wires, wires. I didn't mention it because I take it for granted because I am ALWAYS looking for them. Heck, we call out wires when they are passing below us by 500 feet. If you don't look for them all the time, sometimes they are hard to spot, depending on the angle that you are to them. I have flown through some canyons that had wires stretched accrossed them. I knew they were there, but couldn't see them until I got just about on top of them. The more I think of this thread, I think that it would be a shame for someone to think, "Hey, this low level flight sounds cool". Yes, it is really cool. But very dangerous if you aren't completely situationally aware. I do it alot...in the day and at night, with a little green picture strapped to one eye. And let me tell you, I never get comfortable. As soon as I get 100% comfortable with that type of flying, that's when I quit because my confidence level has exceeded my abilities. To re post what others have said...be careful out there...this post could be a dangerous thing to some people if not taken seriously. And one other thing...the 500 foot thing...don't forget there is an FAA catch all that is mentioned just before the 500 foot thing..."Anywere that a power unit were to fail that you could make a safe landing without due hazard to persons or propety on the surface". That's a blanket statement, and could mean 5,000 feet. If your engine quits, and you land into a fence, the FAA can get you for this catch all, even if you were 500 feet from any structure. Paul Besing --- Oldsfolks(at)aol.com wrote: > > One more point to consider about power lines. They > are "Structures" so > legally you have to be 500 feet from them. > I love the low flying and as a Highway Patrol Pilot > in the California pilot > I have done a lot of it. As stated above - you can > go under the power lines > , BUT learn under the high part of the span . > I > didn't say that !!! > > Bob Olds > RV-4 , N1191X > Charleston, Arkansas > > > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
Subject: Re: Low-level river flying
From: "kitfoxmike" <kitfoxmike(at)yahoo.com>
Date: May 25, 2006
always keep a safe margine, all this has made me think and come to think about it, most of this flying and meneuvering is covered in private pilot training, at least it was for me. ground reference meneuvers and steep turns, etc. Most of the low flying is just the same but closer to the ground and next to trees. My advice is if you can't maintain exactly the altitude you are flying or can't do ground reference meneuvers than grab an instructor and go fly. If we are strickly talking rv's here and you have been not flying while building your machine, and your moving from a cessna to the rv, my advice is get some instruction in an rv before flying the rv at any altitude or circumstance. -------- kitfoxmike kitfox4 1200 912ul speedster http://www.frappr.com/kitfoxmike Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36386#36386 ________________________________________________________________________________
Subject: Re: Low-level river flying
From: "steveadams" <dr_steve_adams(at)yahoo.com>
Date: May 25, 2006
I have no desire for that type of flight. I'm sure it is a rush, but I equate it with the guys going down the freeway on their crotch rockets at 90 mph doing wheelies. It's a thrill until one mistake or something unexpected happens and you're pretty much dead. To each his own, but my life is worth more than a cheap thrill. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36387#36387 ________________________________________________________________________________
Date: May 25, 2006
Subject: Re: Helicopter Pilots
From: James H Nelson <rv9jim(at)juno.com>
Rotor heads always say nanananana! Much grins low leveling in a chopper, just takes a good visual recon all the way down to flight level 10'. Skids in the trees----- Jim Nelson (CW4 rotor head retired) ________________________________________________________________________________
From: "John" <joplin1(at)charter.net>
Subject: Re: Low-level river flying
Date: May 25, 2006
This has been a great review on Maximum Performance Flying. Top performers like Bob Hoover nibble at the edges of the envelope so often that if becomes second nature. But you need to be perfectly coordinated as you approach that critical AOA (i.e. no skid or slip), or the airplane will bite you in the butt and snap roll ... not a good outcome close to the ground. The rate at which you apply back pressure on the stick is just as important. Too quick and you will tend to overshoot that optimum AOA. Too slow and your turn radius will increase. Back to that terrific video. We all love to get down in the weeds, but it's a roll of the dice. You won't see wires and you won't see ducks coming around the bend in time to avoid them! The Koreans and Vietnamese put juicy targets down in narrow canyons. A friend of mine hit a cable dead center with an F-80 but was able to limp home. It ripped back through the gun bay and thankfully snapped before it reached his cockpit. If he had been turning, it would have grabbed a wing. If he had been a foot lower, it would have taken off his head and vertical stab. ----- Original Message ----- From: Tom Gummo To: rv-list(at)matronics.com Sent: Wednesday, May 24, 2006 9:13 PM Subject: Re: RV-List: Re: Low-level river flying I hate too but I have to disagree but slow is not the way to decrease your turn radius. As an Air to Air and Air to Ground Instructor (F-4G) in the military, there is a magic speed for turning your aircraft. We called it "corner velocity" or Va (I am not very good with V speeds in the military we used names for the various speeds). It is the min speed that you can pull the max G. Therefore, as you increase your speed from the stall speed toward the Va speed several things happen: your available G INCREASES, your rate of turn (degrees/sec) INCREASES, your stall margin INCREASES and your turn radius DECREASES. Now this only works if you use ALL the AVAILABLE G. Here is where AOA indicator helps alot. For my plane with a 60 Knot Indicated Stall speed (no flap at gross weight), my corner velocity is 147 knots indicated at 6 G's. (NOTE: all speeds are indicated, not true) I have equations and tables but my email program won't put them into a message for the RV-List. So email me directly and I will send you a word doc attachment with the info. Tom "GummiBear" Gummo Wild Weasel #1573 USAF, Major Retired F-4G Instructor Pilot Apple Valley, CA Harmon Rocket-II ________________________________________________________________________________
Subject: Andair Fuel Selector For Sale
From: "DanBish" <danbish(at)norwalktucson.com>
Date: May 25, 2006
Hi All, Sorry to butt in.... but I've got an Andair fuel selector up for auction on eBay for anyone that's interested - model #FS20x5-F. It's a 3-valve version for 3/8" tubing, with 1/4"npt female inputs. Brand new, never used. Details on site. I've got to order one that will fit in the smaller console of the Europa I'm building. I'm told this one is just right for an RV or similar build. They go for $220 and the current bid price is $96. Just put the auction number, 4643331420, in the search field and it'll take you right there. Thanks, Dan Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36394#36394 ________________________________________________________________________________
Date: May 25, 2006
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Low RPM Harmful Re: Engine Life
Engine life if based on DIS-USE. Engines flown everyday, hard, medium or soft will make TBO and have less maintenance issues. Engines that SIT collect dust and RUST will not make TBO no matter how much you BABY IT. Don't baby your engine. There are so so so many factors besides RPM that control the life of an engine. I recommend the book by sacramento sky ranch, Lyc engineering manual. I am not saying I fly at 2,700 rpm all day, in fact I throttle/prop back to 25 square for climb. I have been told by many to leave it WOT full high RPM from take off to climb and let the altitude take care of MAP. Its a habit to go 25" and than maintain that with the throttle as long as possible. RPM wise 2,700 is just more noise. HOWEVER if you are trying to get to altitude faster WOT & RPM makes sense. Obviously for cruise if you have a C/S prop lower RPM is just less noise and actually better efficiency from the props aerodynamic stand point (more efficency). Low RPM is NOT harmful if the Temps and Pressures are in the green, period. There is a practical limit on how low you can go RPM wise and still make headway. At altitude you may need the RPM to make power and airspeed. A side benifit is lower RPM increases prop efficency, which means more of the HP your engine makes gets turned into thrust. As far as low RPM and MAP that is a differnt topic......... Yes you can run OVER square. Just look at FAA APPROVED flight manuals for Lycoming powered planes. You see plenty of over square power settings. Over square is a throw back to some radial engines. http://www.lycoming.textron.com/main.jsp?bodyPage=support/publications/keyReprints/operation/powerSettings.html AND SECOND http://www.lycoming.textron.com/main.jsp?bodyPage=support/publications/keyReprints/operation/oldWivesTales.html (second old wives tail) One caveat is this chart is 65% POWER. Keep it simple get a manual for your engine and follow it. Using higher MAP and lower RPM has advantages. I usually fly at altitude so M.P. is usually lower anyway. However when given the opportunity of two combos of RPM/MAP which produce the same power, one being OVER SQUARE. I'll pick over square. Every time I take off I am over square, 2700/29". Just give lycoming a call and they can reassure you. They have run engines on test stands for 10's of thousands of hours like this. There is no need to get with all up with the urban legend, rumor, fear and prejudice about it. The data is out there. Cheers George __________________________________________________ ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.edu>
Subject: low speed low alt
Date: May 25, 2006
The other major factor with low speed is Murphy. That SOB will wait until you are flat out of energy before he turns your engine off. At all times you should be able to do a no engine pull up to 500 ft agl (or whatever min you like) so you can see a spot to crash into. If the turns are too tight to maintain this speed then don't go into the slot in that section. W ________________________________________________________________________________
From: MLWynn(at)aol.com
Date: May 25, 2006
Subject: Tank Plumbing
Hi folks, I am finishing up my fuel tanks and ran into a couple of questions. The vent line comes out of the inboard rib with a 90 degree turn. Which way should that angle face? I saw one picture on (Dan Checkaway's site?) that had it facing forward and slightly down, paralleling the curvature of the leading edge. I asked Van's and they were pretty vague. Thoughts? I am a little unclear as to where that eventually gets attached. Is anyone putting proseal along the course of the vent line where it passes through the ribs? I couldn't see any overwhelming reason to do so, unless it would reduce rattle or chaffing. When you put the fittings connecting the vent tube, fuel pickup, etc together, there are pictures of folks prosealing the outside. Do you also put the proseal in the threads as a thread lock? How tight does one make these connections. I am not sure if there is a torque spec. If so, how do you measure it? I would think just good and tight with proseal as a thread locker (and safety-wired on the fuel pickup). I am also finished with the leading edges and was thinking about riveting them on. Any reason that I need to have the tanks completely done before I do that? Thanks in advance for the usual good advice. Michael Wynn RV 8 Wings (tanks) San Ramon, CA ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: Tank Plumbing
Date: May 25, 2006
> I am finishing up my fuel tanks and ran into a couple of questions. The > vent line comes out of the inboard rib with a 90 degree turn. Which way > should > that angle face? I saw one picture on (Dan Checkaway's site?) that had > it > facing forward and slightly down, paralleling the curvature of the > leading > edge. I asked Van's and they were pretty vague. Thoughts? I am a > little > unclear as to where that eventually gets attached. Use an angle that won't make it difficult to connect the thing. It's vague because there's no hard and fast requirement for anything specific. Literally, don't sweat it! As long as it's not pointed up at the flange of the root rib & skin, you won't have an issue. > Is anyone putting proseal along the course of the vent line where it > passes > through the ribs? I couldn't see any overwhelming reason to do so, unless > it > would reduce rattle or chaffing. No, I didn't. If you ever needed to get the vent tube out for some reason, you'd be shooting yourself in the foot. That said, I don't see any reason why you'd need to get it out. > When you put the fittings connecting the vent tube, fuel pickup, etc > together, there are pictures of folks prosealing the outside. Do you also > put the > proseal in the threads as a thread lock? How tight does one make these > connections. I am not sure if there is a torque spec. If so, how do you > measure > it? I would think just good and tight with proseal as a thread locker > (and > safety-wired on the fuel pickup). I didn't use any proseal on any threads that I can recall. I did proseal all over the bulkhead nuts on bulkhead fittings, and did make a fillet around every pass-through where something passed through exterior surfaces. Put it this way...now that the fuel tank SB has reared its can-o-worms head, if you had completed a tank and had used proseal on the threads, you would be HATIN' it. Just my 2 cents. It's bad enough (good enough?) with proseal AROUND the fitting, let alone in the threads. Imho. > I am also finished with the leading edges and was thinking about riveting > them on. Any reason that I need to have the tanks completely done before > I do > that? Not that I'm aware of. )_( Dan RV-7 N714D (914 hours) http://www.rvproject.com ________________________________________________________________________________
From: "Michael" <cubflyr(at)comcast.net>
Subject: Bolt torque for prop extension
Date: May 25, 2006
I had to replace my alternator belt after almost 1000 hours (it was still good but how long do you trust a rubber tree?) and, of course, had to remove the starter ring. For the life of me I can't find the torque for the bolts that secure the prop extension spool to the engine. As I remember, it is 25ft/lb but would like to know for sure. Thanks!! Michael RV-4 N232 Suzie Q 967 hours; not enough...... ________________________________________________________________________________
Date: May 25, 2006
From: sarg314 <sarg314(at)comcast.net>
Subject: george goff
There was a notice in the latest RV-ator about George Goff's RV-6A first flight. He's in Missouri City, TX. Does any one know how I can contact George? I want to ask him about his prop. He's never posted to the list, apparently because I couldn't find him in the archives. Thanks, Tom Sargent, RV-6A ________________________________________________________________________________
From: PGLong(at)aol.com
Date: May 26, 2006
Subject: Landoll Balancer
Decided to put one of Mark Landoll's 12 pound weights on my RV-4 with an 0-320. Tried to contact him at _landollskydoll2001(at)yahoo.com_ (mailto:landollskydoll2001(at)yahoo.com) where I have in the past. No joy. Anyone have a different email address for him or have one of these critters for sale? Pat Long PGLong(at)aol.com N120PL RV4 Bay City, Michigan 3CM Do Not Archive ________________________________________________________________________________
Date: May 26, 2006
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: george goff
This was live on the internet so it can't be a secret... RV White Pages: ENTIRE LIST (100 Person Increments) ...(2040) listings ... Missouri City. Goff,George V. 281.499.8822. 6A. FL. N626DD ...www.vansairforce.net/db/RVWPcode/rvwp_100.asp?offset=1700 - 103k - Cached - More from this site - Save Untitled Document ... RV White Pages: Last Name A-G (100 Person Increments) ...(739) listings ... Missouri City. Goff,George V. 281.499.8822. 6A. FL. N626DD ... www.vansairforce.net/db/RVWPcode/rvwp_A-G.asp?offset=600 - 104k - Cached - More from this site - Save sarg314 wrote: There was a notice in the latest RV-ator about George Goff's RV-6A first flight. He's in Missouri City, TX. Does any one know how I can contact George? I want to ask him about his prop. He's never posted to the list, apparently because I couldn't find him in the archives. Thanks, Tom Sargent, RV-6A --------------------------------- with Voice. --------------------------------- ________________________________________________________________________________
Date: May 26, 2006
From: Bob <panamared3(at)brier.net>
Subject: Re: Cheap Thrills
>I have no desire for that type of flight. I'm sure it is a rush, but I >equate it with the guys going down the freeway on their crotch rockets at >90 mph doing wheelies. It's a thrill until one mistake or something >unexpected happens and you're pretty much dead. To each his own, but my >life is worth more than a cheap thrill. Yep, that is why my airshow specialty and trademark is a low speed high altitude pass. I don't even have to do it inverted, at 10,000 feet AGL spectators can't tell the difference! I have never flown in a canyon below the treetops at 160KTS, and I promise I won't do it again. On the other hand my American Idol, Patty Wagstaff, says she loves to fly low level aerobatics, and never misses an opportunity to do it. Regardless, I do not consider flying my RV a cheap thrill, on a Whitewater River Raft Guides salary, flying is not cheap!!!! As a professional guide, I get paid to perform what some may call a "Thrill". And based upon my salary, yep, it is cheap! Bob ________________________________________________________________________________
Subject: Re: Cheap Thrills
From: "bdjones1965" <rv_8pilot(at)hotmail.com>
Date: May 26, 2006
[quote="panamared3(at)brier.net"] > I have no desire for that type of flight. I'm sure it is a rush, but I > equate it with the guys going down the freeway on their crotch rockets at > 90 mph doing wheelies. It's a thrill until one mistake or something > unexpected happens and you're pretty much dead. To each his own, but my life is worth more than a cheap thrill. > I didn't want to respond, but since someone else already did, what the heck. Some would say those who fly "home-made airplanes" are seeking a cheap thrill! Each and every pilot has different comfort and ability levels. Please don't judge those of us who fly more aggresively, and I won't judge those of you who fly the way you do. Bryan Read this topic online here: http://forums.matronics.com/viewtopic.php?p=36663#36663 ________________________________________________________________________________
From: Oldsfolks(at)aol.com
Date: May 26, 2006
Subject: Re: > RE: Re: Low-level river flying
If something on your helicopter hasn't broken --- It's about to !!! There are no antique helicopter shows !! Bob Olds RV-4 , N1191X Charleston, Arkansas ________________________________________________________________________________
Date: May 27, 2006
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Cruise Prop O320
Anyone using a Sensenich 70CM()S9-0-81 Cruise Prop with an O320/160 hp on an RV 7 0r RV 9? Darrell --------------------------------- ________________________________________________________________________________
From: "james frierson" <tn3639(at)hotmail.com>
Subject: Cruise Prop O320
Date: May 27, 2006
Darrel, I asked the same qeustion and awhile back and this was the response I got from a guy that was running an 79" on a 160hp 6A. "I recently upgraded my 150hp motor to 160hp and have about 30 hours since the rebuild. I started out with the 150hp prop (77") as I was only turning 2150 on take off and 2470 cruise. However, that went up to 2350 on take off and well over 2650 cruise (could not use full throttle as the prop is limited to 2600 rpm). I now have about 10 hours on the 79" prop. I was measuring some numbers the other day - I can pull about 2630 at 5500' giving about 150 kt indicated (around 170 kt true), although that is 30 rpm over the limit. At 2470 I get 137 kt indicated (around 155 true). I am thinking about getting an extra inch of pitch added to the prop, but might stay where I am. On climb I'm getting over 1000 fpm at about 1000 ft on a hot Texas day (low 90s) at about 1500lbs - my CHTs get hot quickly so I can't sustain that for very long. On the runway I am now getting 2300 rpm, so am loathe to increase the pitch more as at 2150 the climb rate was really poor (sometimes less than 500 fpm). However I might go for an additional inch of pitch (to 80"), I would have thought 81" would really be a cruise prop and not yield very good climb performance. I think I am ready to sacrifice a couple of knots of cruise speed for better climb." I resently put the 80" on my 160HP 6A and this is the results I am experiencing as noted in an earlier posting.. "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" Hope this helps Scott RV6A 160hp >From: Darrell Reiley <lifeofreiley2003(at)yahoo.com> >Reply-To: rv-list(at)matronics.com >To: RV-List >Subject: RV-List: Cruise Prop O320 >Date: Sat, 27 May 2006 09:35:48 -0700 (PDT) > > >Anyone using a Sensenich 70CM()S9-0-81 Cruise Prop with an O320/160 hp >on an RV 7 0r RV 9? > >Darrell > > >--------------------------------- > > ________________________________________________________________________________
From: "lowell lemay" <llemay1(at)austin.rr.com>
Subject: BRAKES
Date: May 28, 2006
Problem: Have a nice RV-7 whose brakes heat up on landing with a no brake rollout and braking used only to stop at the hangar. Very hard to move by pulling on the prop on level ground for about 10 minutes. Then all is well and it rolls freely. Have 88 hours on the airplane and brake pads show no abnormal wear. Any suggestions?? llemay1(at)austin.rr.com ________________________________________________________________________________
Date: May 28, 2006
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: BRAKES
Sounds like you might have some air in the brake lines. Try and bleed them and you want to do this from the bottom up. Darrell lowell lemay wrote: Problem: Have a nice RV-7 whose brakes heat up on landing with a no brake rollout and braking used only to stop at the hangar. Very hard to move by pulling on the prop on level ground for about 10 minutes. Then all is well and it rolls freely. Have 88 hours on the airplane and brake pads show no abnormal wear. Any suggestions?? llemay1(at)austin.rr.com --------------------------------- better. ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: BRAKES
Date: May 28, 2006
Idea #1 -- may have to add a "return spring" on your master cylinders. Wonder if there's not enough springback built into the master cylinder. Heard of that in a few cases, solved with a return spring. Get down in there by the pedals, push 'em, and see if you need to pull them back for the master cylinder pushrod to come back out, or if they stay "stuck in." Both sides or just one side? If it's both sides, I'd be inclined to say it's gotta be the springback thing. Idea #2 -- could be gunk between the piston & caliper? If the pedals and master cylinder pushrods are springing back just fine, then I'd drain the fluid from the brakes and remove the pistons from the calipers. Could be that there's some crud in there causing the piston to stick. Probably not, but worth checking if nothing else pans out. Just a couple of guesses. Best of luck. See you up at SQI & OSH for formation? )_( Dan RV-7 N714D (920 hours) http://www.rvproject.com ----- Original Message ----- From: "lowell lemay" <llemay1(at)austin.rr.com> Sent: Sunday, May 28, 2006 4:05 PM Subject: RV-List: BRAKES > > Problem: Have a nice RV-7 whose brakes heat up on landing with a no > brake rollout and braking used only to stop at the hangar. Very hard to > move by pulling on the prop on level ground for about 10 minutes. Then > all is well and it rolls freely. Have 88 hours on the airplane and > brake pads show no abnormal wear. Any suggestions?? > > llemay1(at)austin.rr.com > > > ________________________________________________________________________________
From: RVer273sb(at)aol.com
Date: May 28, 2006
Subject: Re: BRAKES
They are supposed to run at 0 clearance. Perhaps the linings are a little thicker than usual. It's not uncommon to add shims between the anvil and the puck housing. As linings wear you can remove the shims. Stewart RV-4 ________________________________________________________________________________
From: "DonVS" <dsvs(at)comcast.net>
Subject: BRAKES
Date: May 28, 2006
One other possiblity. The bolts that the brake patals pivot on may be to tight. I know of at least one person who had this problem. They need to be rather loose, that is why they are locked with cotter pins. Don -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of lowell lemay Sent: Sunday, May 28, 2006 4:06 PM Subject: RV-List: BRAKES Problem: Have a nice RV-7 whose brakes heat up on landing with a no brake rollout and braking used only to stop at the hangar. Very hard to move by pulling on the prop on level ground for about 10 minutes. Then all is well and it rolls freely. Have 88 hours on the airplane and brake pads show no abnormal wear. Any suggestions?? llemay1(at)austin.rr.com ________________________________________________________________________________
From: "Michael" <cubflyr(at)comcast.net>
Subject: Brakes
Date: May 29, 2006
Is this airplane new to you? There is an ancient issue with "old" return springs on the master cylinders. The "old" ones were too short and new replacements were sent to you from Van's for free. Was this done? It may be in the log books but probably not. Search the archives. There are certain lengths the correct and incorrect springs are. This measurement can be done with the springs in place, as I recall. Having brakes that work is a nice thing. Michael ________________________________________________________________________________
Date: May 29, 2006
From: Charles Reiche <charlieray(at)optonline.net>
Subject: Re: BRAKES
Check a few things here. bleed the system up from the bottom. take brakes off the mount and see if the way your hose or line runs to the caliper causes it to jam sideways in the slide pins. (loosen line and tighten it so there is no sideload when you slide the caliper in the mounting holes.) polish slide pins with scotchbrite. These are parker brakes right? we havent even gotten to the fuselage yet, but im a mechanic. Charles ----- Original Message ----- From: "lowell lemay" <llemay1(at)austin.rr.com> Sent: Sunday, May 28, 2006 7:05 PM Subject: RV-List: BRAKES > > Problem: Have a nice RV-7 whose brakes heat up on landing with a no > brake rollout and braking used only to stop at the hangar. Very hard to > move by pulling on the prop on level ground for about 10 minutes. Then > all is well and it rolls freely. Have 88 hours on the airplane and > brake pads show no abnormal wear. Any suggestions?? > > llemay1(at)austin.rr.com > > > ________________________________________________________________________________
Date: May 29, 2006
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: BRAKES
Charles, I had forgotten about this issue of the caliper binding on the slide pins due to the brake fluid line side-load pressure. I had that happen on an RV7A about 9 months ago. The brakes did heat up a little from this condition while in taxi mode. I believe we were dealing with the left brake. A quick dis-assembly, cleanup and reassembly with a very light film of brake caliper pin grease and we were done. We did go ahead and bleed both brakes at the same time since we had a little grime on our hands. Darrell Charles Reiche wrote: Check a few things here. bleed the system up from the bottom. take brakes off the mount and see if the way your hose or line runs to the caliper causes it to jam sideways in the slide pins. (loosen line and tighten it so there is no side-load when you slide the caliper in the mounting holes.) polish slide pins with scotchbrite. These are parker brakes right? we havent even gotten to the fuselage yet, but im a mechanic. Charles ----- Original Message ----- From: "lowell lemay" Sent: Sunday, May 28, 2006 7:05 PM Subject: RV-List: BRAKES > > Problem: Have a nice RV-7 whose brakes heat up on landing with a no > brake rollout and braking used only to stop at the hangar. Very hard to > move by pulling on the prop on level ground for about 10 minutes. Then > all is well and it rolls freely. Have 88 hours on the airplane and > brake pads show no abnormal wear. Any suggestions?? > > llemay1(at)austin.rr.com > > > --------------------------------- better. ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.edu>
Subject: stiff brakes
Date: May 29, 2006
Most likely is the pedal rocker pivots are too stiff and the small compensating valve spring in the master cyl can't open, thereby pushing the pedal back that last bit. (These are NOT the pedal swing pivots which allow for rudder movement) After a bit they either bleed down, or the system cools and reduces fluid pressure. Check by getting the brakes to the stiff condition then pull back on the tops of the pedals to force them fully back and see if that loosens the brakes. (This also assumes the pedal rocker action has enough swing clearence to let the master cyls fully extend.) If this is the case the best fix is to loosen those pivots some as another spring is something that could break/jam/whatever at the wrong time. Air in the line would not cause this as the compensating port allows for air or fluid to return immediately. Is also not likely to be gunk in the caliper as that would probably not get better after a few minutes. The same would also be true for the too tight pins that retain the floating calipers. The one other option is the matco style parking brake valve could be not fully opening both poppets thereby acting like one way check valves, if one is installed. If the above test doesn't make it better remove the pants and get them stiff, then open the bleeder for a tad and see if they loosen. This will tell you if the P brake is holding the pressure on. (you could also try working the P-brake valve when they are stiff and see if that suddenly loosens them.) W ________________________________________________________________________________
Date: May 29, 2006
From: Matt Dralle <dralle(at)matronics.com>
Subject: Two New Email Lists at Matronics and Wiki Reminder!
Dear Listers, I have added two new email Lists to the Matronics Line up today. These include a Continental engine List and a Lightning aircraft List: ========== continental-list(at)matronics.com http://www.matronics.com/Navigator?Continental-List Everything related to the Continental aircraft engine. Sky's the limit on discussions here. ========== ========== lightning-list(at)matronics.com http://www.matronics.com/Navigator?Lightning-List This is an exciting new design from Arion Aircraft LLC in Shelbyville Tennessee. Pete Krotje has a very nice web site on the aircraft that can be found here: http://www.arionaircraft.com/ ========== Also, if you haven't checked out the new Matronics Aircraft Wiki, swing by and have a look. Remember, a Wiki is only as good as the content that the members put into it. Have a look over some of the sections, and if you've got some interesting or useful, please add it to the Wiki! Its all about YOU! :-) The URL for the Matronics Wiki is: http://wiki.matronics.com Best regards, Matt Dralle Matronics Email List Administrator ________________________________________________________________________________
From: "Kelly Patterson" <kbob(at)cox.net>
Subject: RE: 81" pitch on O-320
Date: May 29, 2006
I'll throw in my 2 cents, and some numbers, since I'm running a 6A with 81" pitch. Couple of specs: 9.2:1 CR, carb & Emag on a fresh O-320 rated 175HP @ 2700RPM. My performance is nearly identical to the 79" below on the O-320 160 HP, except slightly higher speeds in cruise (~160kts or 195 MPH). It runs about 2150 at WOT static runup, 2300 on takeoff, 2450-2500 at cruise over 8000', 2600 in WOT 200-300 FPM descents. In other words, it never exceeds the RPM limit except at lower altitude runs (<8000') or diving. Climb is 1000-1500 depending on wt. & density altitude. This is all done in Phoenix where D.A. is about 3000'+ & solo I'm at 1500 FPM climb. In return I get 7 GPH fuel burns, which is great economy, and even EGT's & CHT's when WOT. I prefer WOT operation. I would not change the prop unless I needed more climb rate, but have not used a short runway where it is critical. With this setup, a 3000' long runway is fine at 5000' DA & gross weight. This combo returns about 750 FPM climb. YMMV, Kelly Patterson N716K RV-6A PHX, AZ 61 hrs >From: "james frierson" <tn3639(at)hotmail.com> >Subject: RE: RV-List: Cruise Prop O320 > > >Darrel, >I asked the same qeustion and awhile back and this was the >response I got >from a guy that was running an 79" on a 160hp 6A. > > >"I recently upgraded my 150hp motor to 160hp and have about 30 >hours since the rebuild. I started out with the 150hp prop >(77") as I was only turning 2150 on take off and 2470 cruise. >However, that went up to 2350 on take off and well over 2650 >cruise (could not use full throttle as the prop is limited to >2600 rpm). I now have about 10 hours on the 79" prop. I was >measuring some numbers the other day - I can pull about 2630 >at 5500' giving about 150 kt indicated (around 170 kt true), >although that is 30 rpm over the limit. At 2470 I get 137 kt >indicated (around 155 true). I am thinking about getting an >extra inch of pitch added to the prop, but might stay where I am. > >On climb I'm getting over 1000 fpm at about 1000 ft on a hot >Texas day (low 90s) at about 1500lbs - my CHTs get hot quickly >so I can't sustain that for very long. On the runway I am now >getting 2300 rpm, so am loathe to increase the pitch more as >at 2150 the climb rate was really poor (sometimes less than >500 fpm). However I might go for an additional inch of pitch >(to 80"), I would have thought 81" would really be a cruise >prop and not yield very good climb performance. I think I am >ready to sacrifice a couple of knots of cruise speed for better climb." > >I resently put the 80" on my 160HP 6A and this is the results I am >experiencing as noted in an earlier posting.. > >"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" > >Hope this helps >Scott >RV6A >160hp > >> >>Anyone using a Sensenich 70CM()S9-0-81 Cruise Prop with an >O320/160 hp >>on an RV 7 0r RV 9? >> >>Darrell ________________________________________________________________________________
From: "Marc Jones" <mjflying(at)comcast.net>
Subject: New Aymar-Demuth prop for sale
Date: May 29, 2006
I have a new in the box Aymar-Demuth prop for sell. Also have the spinner kit and extension. Was to be mounted on a 0-320-D2J RV-6. If interested please contact me off the list at mjflying(at)comcast.net Marc RV-6 N589M ________________________________________________________________________________
Subject: Re: Fuel Line Firewall Penetration Location
From: "Jekyll" <rcitjh(at)aol.com>
Date: May 30, 2006
Dwight: IO-360 firewall penetration location IS DIFFERENT from the O-360 location. Drawing OP-32 shows the correct location and the parts list. The drawing comes with the FWF. Jekyll Read this topic online here: http://forums.matronics.com/viewtopic.php?p=37372#37372 ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Hangar For Sale at KCNO (Chino, CA)
Date: May 30, 2006
My hangarmate (RV-7A builder) Linas is selling one of his hangars at Chino, CA (KCNO). Here's the deal... Port-A-Port Executive II hangar large enough for a twin engine aircraft. Price $15,000. Contact number 949-436-1792. ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: How to add 15kt to cruise speed by adding weight
Date: May 30, 2006
I've been exploring the CG range in flight testing of my RV8A and have found an unanticipated cruise speed effect. At 85.9 inches, I was getting 155kias with 2300rpm, 23 in mp, 5,500 ft, and 42 degrees F outside. At 79.6 inches, I got 142kias with 2300rpm, 23 in mp, 4,500 ft, and 64 degrees F outside. My whiz wheel gives true airspeeds of roughly 169kt and 154kt. Quite an improvement just by adding some weight in back. Yes, the fast flight was with a little bit higher weight! There's lots of discussion of speed improvements in the archives, but nothing related to CG location that I could find and certainly nothing so easy to get and of this magnitude. So, my question to everyone is have you had similar experience? Do you know anywhere this has been quantified or further detailed? After all, I'm just comparing two test flights here, but theoretically, I'd guess the decrease in drag due to decreased pitch stability requirements as the CG moves aft would explain the speed increase. Excited! Dave Reel - RV8A ________________________________________________________________________________
Date: May 30, 2006
From: "Ralph E. Capen" <recapen(at)earthlink.net>
Subject: Re: How to add 15kt to cruise speed by adding weight
Have you tried simply altering the CG and not the weight? I think I remember reading somewhere that the shifted CG changes stabilized AOA thereby changing drag characteristics. Geek - not aerodynamicist...and I stayed at a Marriot this weekend instead of a Holiday Inn! -----Original Message----- >From: DAVID REEL <dreel(at)cox.net> >Sent: May 30, 2006 10:47 AM >To: rvlist >Subject: RV-List: How to add 15kt to cruise speed by adding weight > > >I've been exploring the CG range in flight testing of my RV8A and have found >an unanticipated cruise speed effect. At 85.9 inches, I was getting 155kias >with 2300rpm, 23 in mp, 5,500 ft, and 42 degrees F outside. At 79.6 inches, >I got 142kias with 2300rpm, 23 in mp, 4,500 ft, and 64 degrees F outside. >My whiz wheel gives true airspeeds of roughly 169kt and 154kt. Quite an >improvement just by adding some weight in back. Yes, the fast flight was >with a little bit higher weight! > >There's lots of discussion of speed improvements in the archives, but >nothing related to CG location that I could find and certainly nothing so >easy to get and of this magnitude. So, my question to everyone is have you >had similar experience? Do you know anywhere this has been quantified or >further detailed? After all, I'm just comparing two test flights here, but >theoretically, I'd guess the decrease in drag due to decreased pitch >stability requirements as the CG moves aft would explain the speed increase. > >Excited! > >Dave Reel - RV8A > > > > > > > ________________________________________________________________________________
Subject: Re: Fuel Line Firewall Penetration Location
From: "Jekyll" <rcitjh(at)aol.com>
Date: May 30, 2006
Dwight: If you are to the point of doing your fuel line passthrough, you are to the point of needing your FWF. It comes with the parts you install on the FW behind the engine such as the heater valve, the master and battery relays and the battery/battery box to name a few. The engine driven fuel pump is in the same location but you need a different fuel line to accommodate the location. You said you are using a vertical induction IO so, you will be getting O-360 finishing and FWF kits. Email or call Vans for the full list of the FWF parts to allow you to add and delete parts as necessary to adapt the O-360 for a vertical induction IO-360. You need to delete the gascolator, gascolator bracket. Substitute certain fule lines and throttle cable and throttle bracket. Jekyll Read this topic online here: http://forums.matronics.com/viewtopic.php?p=37390#37390 ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)earthlink.net>
Subject: How to add 15kt to cruise speed by adding weight
Date: May 30, 2006
> > I've been exploring the CG range in flight testing of my RV8A > and have found an unanticipated cruise speed effect. At 85.9 > inches, I was getting 155kias with 2300rpm, 23 in mp, 5,500 > ft, and 42 degrees F outside. At 79.6 inches, I got 142kias > with 2300rpm, 23 in mp, 4,500 ft, and 64 degrees F outside. > My whiz wheel gives true airspeeds of roughly 169kt and > 154kt. Quite an improvement just by adding some weight in > back. Yes, the fast flight was with a little bit higher weight! > > There's lots of discussion of speed improvements in the > archives, but nothing related to CG location that I could > find and certainly nothing so easy to get and of this > magnitude. So, my question to everyone is have you had > similar experience? Do you know anywhere this has been > quantified or further detailed? After all, I'm just > comparing two test flights here, but theoretically, I'd guess > the decrease in drag due to decreased pitch stability > requirements as the CG moves aft would explain the speed increase. > > Excited! > > Dave Reel - RV8A Dave, What were the fuel burns during those two runs? One cannot state that the power was the same, only that the MAP and RPM were the same. You can vary airspeed greatly with mixture. A more aft cg is more efficient, but not that much. (The tail doesn't have to generate as much downward lift.) Alex Peterson RV6-A N66AP 755 hours Maple Grove, MN ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: Re: Hangar For Sale at KCNO (Chino, CA)
Date: May 30, 2006
Sorry for the confusion, but the hangar has been taken off the market. ________________________________________________________________________________
Date: May 30, 2006
From: Sherman Butler <lsbrv7a(at)yahoo.com>
Subject: Re: How to add 15kt to cruise speed by adding weight
David, That is true in my Bonanza as well, although I have never tried to quantify it. Less drag from less elevator (ruddivator) down force. The Bonanza experts warn of CG change with fuel burn moving the CG aft and the possibility of elevator sensitivity during the landing flare resulting in over correction. Did you notice increased elevator sensitivity? DAVID REEL wrote: I've been exploring the CG range in flight testing of my RV8A and have found an unanticipated cruise speed effect. At 85.9 inches, I was getting 155kias with 2300rpm, 23 in mp, 5,500 ft, and 42 degrees F outside. At 79.6 inches, I got 142kias with 2300rpm, 23 in mp, 4,500 ft, and 64 degrees F outside. My whiz wheel gives true airspeeds of roughly 169kt and 154kt. Quite an improvement just by adding some weight in back. Yes, the fast flight was with a little bit higher weight! There's lots of discussion of speed improvements in the archives, but nothing related to CG location that I could find and certainly nothing so easy to get and of this magnitude. So, my question to everyone is have you had similar experience? Do you know anywhere this has been quantified or further detailed? After all, I'm just comparing two test flights here, but theoretically, I'd guess the decrease in drag due to decreased pitch stability requirements as the CG moves aft would explain the speed increase. Excited! Dave Reel - RV8A Sherman Butler RV-7a Wings Idaho Falls --------------------------------- ________________________________________________________________________________
From: "Charles Heathco" <cheathco(at)cox.net>
Subject: Sterio Icom
Date: May 30, 2006
I have a mono flightcom 403 that has alwqys had a slight echo, and it has a static discharge sound every so often. I want to upgrad and am thinking Sigtronics steri might be a good choice. Would like coments, and also will I have to change headst jacks? Charlie H ________________________________________________________________________________
From: "Dan Beadle" <dan.beadle(at)inclinesoftworks.com>
Subject: How to add 15kt to cruise speed by adding weight
Date: May 30, 2006
This is basic aerodynamics. To get stability (AKA, hard to flare), you move the CG forward. Think Lawn Dart. In this mode, the tail actually pulls down, not up. This results in the wing needing to produce more lift (weight + the tails negative lift so that total lift = weight). If you move the CG back, you have less and less down-lift on the tail, letting the wing work less, thus getting less induced drag. Faster. A heavier airplane, with the same CG, should fly slower than the same plane, same CG, when it is lighter. The reason is the heavier airplane must have a higher angle of attack to produce the needed additional lift. That means more induced drag. The CG limits are set to give reasonable handling. The forward CG is limited by the ability to flare. The Aft CG is limited by the need for positive stability. If we moved the CG back to where the tail was lifting, we would have no stability. In the normal range, as the plane slows from the trimmed AS, the wing and the tail both lose some lift. But the tail is now lifting less in the downward direction, letting the nose fall down a bit and resume the trimmed AS. If we move too far back, we lose the stability feature making the airplane difficult or impossible to fly. Rule of thumb: smooth air, load for aft CG (within limits). Rough air, keep a more forward CG. So your data does make sense. (But the faster/heavier combination is probably just due to aft CG.) Dan -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Sherman Butler Sent: Tuesday, May 30, 2006 8:38 AM Subject: Re: RV-List: How to add 15kt to cruise speed by adding weight David, That is true in my Bonanza as well, although I have never tried to quantify it. Less drag from less elevator (ruddivator) down force. The Bonanza experts warn of CG change with fuel burn moving the CG aft and the possibility of elevator sensitivity during the landing flare resulting in over correction. Did you notice increased elevator sensitivity? DAVID REEL wrote: I've been exploring the CG range in flight testing of my RV8A and have found an unanticipated cruise speed effect. At 85.9 inches, I was getting 155kias with 2300rpm, 23 in mp, 5,500 ft, and 42 degrees F outside. At 79.6 inches, I got 142kias with 2300rpm, 23 in mp, 4,500 ft, and 64 degrees F outside. My whiz wheel gives true airspeeds of roughly 169kt and 154kt. Quite an improvement just by adding some weight in back. Yes, the fast flight was with a little bit higher weight! There's lots of discussion of speed improvements in the archives, but nothing related to CG location that I could find and certainly nothing so easy to get and of this magnitude. So, my question to everyone is have you had similar experience? Do you know anywhere this has been quantified or further detailed? After all, I'm just comparing two test flights here, but theoretically, I'd guess the decrease in drag due to decreased pitch stability requirements as the CG moves aft would explain the speed increase. Excited! Dave Reel - RV8A Sherman Butler RV-7a Wings Idaho Falls --------------------------------- Voice. ________________________________________________________________________________
Subject: Hanging my IO-320 - lower mount spacer
From: Gerry Filby <gerf(at)gerf.com>
Date: May 30, 2006
Has anyone else had this experience ? I hung my engine this weekend - but I think it needs to come off again. Vans supplies 2 large diameter AN7 washers in the engine mount bolt kit that are to shim the forward faces of the lower engine mounts off the engine so that the mount clears a "step" in the engine casing. The "step" is the mounting flange for the oil sump. All's well on the right lower mount, but on the lower left its as if the shim isn't thick enough, or more to the point, the flange on the engine protrudes too much. Consequence is that mount doesn't sit flush on the engine - its slightly at an angle with the top part of the mount making contact and the lower part interfering with the oil sump flange. Is this a common problem or am I breaking new ground here :) I guess the obvious solution is to pull the engine and grind off the flange on the oil sump mount. I'm more than a little hesitant about doing surgery on my engine. __g__ ========================================================== Gerry Filby gerf(at)gerf.com Tel: 415 203 9177 ---------------------------------------------------------- ________________________________________________________________________________
Date: May 30, 2006
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: GPS Tracking...
> I am looking for some software that I can download GPS track info to > that will display it on a map to show where I have been... Anyone > know = of such a thing? I download the tracks from my Garmin GPS into the Garmin MapSource program. It requires that you have purchased some MapSource data from Garmin, of course, so you have a map to overlay it on, but I have most of North America so it works for me. I experimented with downloading the track and converting it to an XML file that I could read into a website and overlay on a Google map... It worked very well, but I found that the performance seriously bogged down beyond about 50 points in the GPS track. It works great for tracking yourself if you're jogging or hiking, but not so good when you fly across country. Here's a website showing how it works for runners. I wanted to do the same thing for pilots, but the API can't handle the large number of points in a typical flight track. <http://www.favoriterun.com/> -Rob ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: How to add 15kt to cruise speed by adding weight
Date: May 30, 2006
Hi Dave, I discovered the same effect in my RV-6A which is a bit nose heavy. Best top speed was when I had the baggage compartment load to the max with camping gear and full wing tanks. I suspect you are correct in that the aft CG results in less down component from the horizonal stabilizer resulting in less drag. The wing incident may also be a bit more optimum (less) also resulting in less drag. As best I could determine my speed increase was between 8-10 MPH. Ed Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC eanderson(at)carolina.rr.com ----- Original Message ----- From: "DAVID REEL" <dreel(at)cox.net> Sent: Tuesday, May 30, 2006 10:47 AM Subject: RV-List: How to add 15kt to cruise speed by adding weight > > I've been exploring the CG range in flight testing of my RV8A and have > found > an unanticipated cruise speed effect. At 85.9 inches, I was getting > 155kias > with 2300rpm, 23 in mp, 5,500 ft, and 42 degrees F outside. At 79.6 > inches, > I got 142kias with 2300rpm, 23 in mp, 4,500 ft, and 64 degrees F outside. > My whiz wheel gives true airspeeds of roughly 169kt and 154kt. Quite an > improvement just by adding some weight in back. Yes, the fast flight was > with a little bit higher weight! > > There's lots of discussion of speed improvements in the archives, but > nothing related to CG location that I could find and certainly nothing so > easy to get and of this magnitude. So, my question to everyone is have > you > had similar experience? Do you know anywhere this has been quantified or > further detailed? After all, I'm just comparing two test flights here, > but > theoretically, I'd guess the decrease in drag due to decreased pitch > stability requirements as the CG moves aft would explain the speed > increase. > > Excited! > > Dave Reel - RV8A > > > ________________________________________________________________________________
Date: May 30, 2006
From: Paul Besing <pbesing(at)yahoo.com>
Subject: Re: Sterio Icom
PS Engineering all the way...can't beat the quality or customer service...not too much more expensive, but the audio quality is far superior, IMHO...I've had both sigtronics and PS Engineering...there's a reason that sigtronics sells "budget quality" headsets and avionics. Spend the extra money on PS Engineering in my opinion. Paul Besing --- Charles Heathco wrote: > > > I have a mono flightcom 403 that has alwqys had a > slight echo, and it > has a static discharge sound every so often. I want > to upgrad and am > thinking Sigtronics steri might be a good choice. > Would like coments, > and also will I have to change headst jacks? Charlie > H > > > > > browse > Subscriptions page, > FAQ, > > > Admin. > > > > > > > > > > > __________________________________________________ ________________________________________________________________________________
Subject: mixture cable flexing
From: Erich_Weaver(at)URSCorp.com
Date: May 30, 2006
I have an io-360 with the AFP fuel controller mounted below the sump (vertical induction). AFP supplies nice, heavy duty brackets with the fuel controller for mounting the mixture and throttle cables. However, with the mixture cable in particular, the distance between the firewall pass-through point and the point where the cable attaches to the bracket is very short - maybe 4 inches. This short distance doesnt allow any room for curving the cable and allowing it to flex during engine shaking etc, especially since the eyeball socket at the firewall cable does not allow the cable to slip in and out at all. Do folks generally build-in a little flex in the mixture and throttle cables forward of the firewall, or is it pretty much a straight shot from the firewall to the rod-end bearing? Dont I have a legitimate concern with respect to the need for cable flexing? thanks for any insights Erich Weaver ________________________________________________________________________________
From: "Rick McCraw" <rick(at)n608ef.us>
Subject: How to add 15kt to cruise speed by adding weight
Date: May 30, 2006
I like Dan's explanation, but will add a bit more. Specifically, we require the CG to be forward of the center of lift (CL) in order to have a stable aircraft (and one whose nose drops when the wing is stalled). The closer the CG gets to the CL, the less induced drag, but the less stable the plane will be. If the CG should go aft of the CL, all bets are off in terms of controllability. Another e-mail commented on Bonanzas and how their CG moves with fuel burn. Whether the CG moves aft with fuel burn should depend on the CG of the tank and its fuel relative to the CG of the plane. I fly an A-36 Bonanza, and when weight is up (hence, realistically, with a CG farther aft than when lightly loaded), I have indeed noticed greater pitch sensitivity after a long flight. When I plan flights at higher weights, I check my loading by calculating CG for zero fuel, just to be on the safe side. For extra margin), I try to land with fuller tanks, too. Rick A-36, RV-7 in process -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Dan Beadle Sent: Tuesday, May 30, 2006 12:38 PM Subject: RE: RV-List: How to add 15kt to cruise speed by adding weight This is basic aerodynamics. To get stability (AKA, hard to flare), you move the CG forward. Think Lawn Dart. In this mode, the tail actually pulls down, not up. This results in the wing needing to produce more lift (weight + the tails negative lift so that total lift = weight). If you move the CG back, you have less and less down-lift on the tail, letting the wing work less, thus getting less induced drag. Faster. A heavier airplane, with the same CG, should fly slower than the same plane, same CG, when it is lighter. The reason is the heavier airplane must have a higher angle of attack to produce the needed additional lift. That means more induced drag. The CG limits are set to give reasonable handling. The forward CG is limited by the ability to flare. The Aft CG is limited by the need for positive stability. If we moved the CG back to where the tail was lifting, we would have no stability. In the normal range, as the plane slows from the trimmed AS, the wing and the tail both lose some lift. But the tail is now lifting less in the downward direction, letting the nose fall down a bit and resume the trimmed AS. If we move too far back, we lose the stability feature making the airplane difficult or impossible to fly. Rule of thumb: smooth air, load for aft CG (within limits). Rough air, keep a more forward CG. So your data does make sense. (But the faster/heavier combination is probably just due to aft CG.) Dan ________________________________________________________________________________
Subject: Re: How to add 15kt to cruise speed by adding weight
From: "bdjones1965" <rv_8pilot(at)hotmail.com>


May 13, 2006 - May 30, 2006

RV-Archive.digest.vol-ry