RV-List Digest Archive

Sun 12/01/02


Total Messages Posted: 48



Today's Message Index:
----------------------
 
     1. 12:04 AM - All New List Digest Format!! (Matt Dralle)
     2. 12:58 AM - Runaway Trim (Vincent Welch)
     3. 03:45 AM - Re: Bench grinder vs Buffer (Dean Pichon)
     4. 05:42 AM - Re: 14 Hours Inspiration Report (Lenleg@aol.com)
     5. 06:27 AM - Re: How to torque a bolt? (Elsa & Henry)
     6. 06:34 AM - Re: Bench grinder vs Buffer (Rick Galati)
     7. 07:02 AM - Re: Runaway Trim (Carl Froehlich)
     8. 07:08 AM - Re: engine mount holes (Ed's Compuserve)
     9. 07:54 AM - Re: Runaway Trim (Vincent Welch)
    10. 08:30 AM - Re: Alternative Engine Questions (lm4@juno.com)
    11. 08:35 AM - Re: engine mount holes and installing it! (Elsa & Henry)
    12. 09:25 AM - Re: Runaway Trim (Jerry Springer)
    13. 09:48 AM - Re: Bench grinder vs Buffer (Elsa & Henry)
    14. 10:48 AM - Re: Bench grinder vs Buffer (Jerry Springer)
    15. 11:17 AM - Engines (Wheeler North)
    16. 11:40 AM - Data recording (Chris)
    17. 12:03 PM - Re: Working on a non-owner built RV (Mike Robertson)
    18. 12:27 PM - Re: Working on a non-owner built RV (Paul Besing)
    19. 01:44 PM - Re: Engines (Tedd McHenry)
    20. 01:44 PM - Re: Alternative Engine Questions (Kyle Boatright)
    21. 01:55 PM - rudder pedal assemblies - RV7QB (Karen and Robert Brown)
    22. 02:06 PM - baggage area floors, strobes & ELT's - RV7 (Karen and Robert Brown)
    23. 02:53 PM - Re: Data recording (Terry Watson)
    24. 03:04 PM - Re: Data recording (Kevin Horton)
    25. 03:12 PM - manifold pressure reads low on VM-1000 (Tom Barnes)
    26. 03:56 PM - Re: Data recording (Doug Rozendaal)
    27. 04:27 PM - Re: Data recording (James E. Clark)
    28. 04:32 PM - Re: Runaway Trim (Alex Peterson)
    29. 04:34 PM - Re: Data recording (Doug Rozendaal)
    30. 04:39 PM - Re: manifold pressure reads low on VM-1000 (Alex Peterson)
    31. 04:48 PM - Oil Cooler/Heat Muff (Jim Bean)
    32. 05:02 PM - Re: Engines (kempthornes)
    33. 05:12 PM - Re: Alternative Engine Questions (kempthornes)
    34. 05:33 PM - Re: Alternative Engine Questions (Dave Bristol)
    35. 05:57 PM - Re: Alternative Engine Questions (Finn Lassen)
    36. 06:10 PM - Re: Data recording (Bill VonDane)
    37. 07:50 PM - More Freebies!!!!  (KAKlewin@aol.com)
    38. 08:01 PM - RV's, BAD Wind! & Larry Vetterman (Long). (Stein Bruch)
    39. 08:07 PM - Re: Engines (Jim Oke)
    40. 08:21 PM - Paint and filling tips (Jerry)
    41. 08:30 PM - Freebies Gone!!! (KAKlewin@aol.com)
    42. 09:35 PM - Re: Prop (Reinback)
    43. 09:47 PM - Re: Paint and filling tips (Jim Oke)
    44. 09:50 PM - Re: Prop (Reinback)
    45. 10:27 PM - Re: Alternative Engine Questions (Tedd McHenry)
    46. 10:42 PM - Drill Sizes (Norman)
    47. 11:12 PM - New, NEW List Digest Format... (Matt Dralle)
    48. 11:42 PM - Re: Drill Sizes (BrownTool@aol.com)
 
 
 


Message 1


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    Time: 12:04:56 AM PST US
    From: Matt Dralle <dralle@matronics.com>
    Subject: All New List Digest Format!!
    --> RV-List message posted by: Matt Dralle <dralle@matronics.com> Dear Listers, I've just finished up some awesome code that will completely change your thinking about how email Digests should work and look! Yeah, I'm kind of proud of it, that is true... :-) What you'll be getting in the new List Digest message is the following: The main message will contain the new text-based index I introduced a few weeks back. But here's where things get different... Instead of simply including all of the day's posts in line within the message, there will now be included two enclosures - one with a HTML encoded version of the Digests, and another with the usual text-only version of the Digests. I think you're really going to like the new HTML enclosure of the Digests. All of the Indexes at the top are now hyperlinked to the actual posts and there are hyperlinks at the top of each post that will: o Take you back to the Index o Take you to the next post o Take you to the previous post o Allow you to respond to the LIST regarding the message o Allow you to respond directly to the POSTER regarding the message You'll have to check it out to appreciate the full goodness of the new format! :-) The text-only version is basically exactly the same data that has been normally sent in line within the message. You'll also note that the filenames of the enclosures are such that they can be conveniently placed in a personal "archive" directory for future reference. Hope you enjoy the new Digest format!!! Oh, and don't forget about the Fund Raiser! :-) Matt Dralle Email List Admin.


    Message 2


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    Time: 12:58:48 AM PST US
    From: "Vincent Welch" <welchvincent@hotmail.com>
    Subject: Runaway Trim
    --> RV-List message posted by: "Vincent Welch" <welchvincent@hotmail.com> Hey Guys, I am building my electrical distribution around the EXP Bus (before you start about Bob and his fuses, I already have the unit in hand and intend to use it). I was reading the most recent issue of Sport Aviation discussing cockpit layout. One of the items mentioned was being able to reach circuit breakers to disconnect in the event of runaway trim or flaps. I can accomplish this by putting switches in the power line (trim and flaps are actuated by switching the ground). Has anyone had a problem with runaway trim with the MAC units? Has anyone had uncommanded flap movement? In other words, do I really need to include the disconnect switches? Vince Welch RV-8A


    Message 3


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    Time: 03:45:11 AM PST US
    From: "Dean Pichon" <DeanPichon@msn.com>
    Subject: Re: Bench grinder vs Buffer
    --> RV-List message posted by: "Dean Pichon" <DeanPichon@msn.com> A buffer differs from a grinder in that the shaft that extends from either side of the motor is longer. This little extra difference (1-3") between the motor and the buffing/grinding wheel makes it much easier to buff large/irregular parts. This configuration makes the buffer better for buffing (than a grinder). However, if you are using files and sandpaper, the switch to a grinder with a buffing wheel be completely satisfactory. Mounting your bench grinder on a pedastal and/or putting buffing wheels on both sides helps to ensure you can easily reach all areas of your parts. Good luck, Dean Pichon RV-4 (flying) Morgantown, WV ----- Original Message ----- From: Will & Lynda Allen Subject: RV-List: Bench grinder vs Buffer --> RV-List message posted by: "Will & Lynda Allen" <linenwool@attbi.com> I'm needing to get something that's faster than using sand paper and files and am looking for some feedback on the less expensive Bench Grinder vs the Buffer. Is there anything that the Buffer will do that the grinder won't? The only difference I can see is that the grinder has the guards that might be in the way but I would think I could take those off if needed. And I'm assuming I can use all the same attachments for the grinder ie: scotch bright wheel, wire brush wheel, etc. Thanks, Will Allen North Bend, Wa. RV8 Emp


    Message 4


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    Time: 05:42:41 AM PST US
    From: Lenleg@aol.com
    Subject: RE: 14 Hours Inspiration Report
    --> RV-List message posted by: Lenleg@aol.com Fellow Builders: Just an update to hopefully inspire you to keep working hard on your projects. I now have 14 hours on my 8A. I have spent most of this time taking care of the minor problems and squawks that are common on most projects. I was lucky in that the DAR gave me a 50 miles fly-off area. I think I would go crazy if I only had 25 miles ... definitely beg for 50. I am flying almost every day the weather allows. I have not painted or put the wheel pants/fairings on yet. The EGT, CHT temps are great. CHT in the 380 range. I had to block off part of the oil cooler ... temps were too cool. I am still not getting the full 2700 rpm on takeoff. Right now getting 2600. When pulling back to 2500 rpm I am still showing around 1500-1600 FPM climbout at 110 knots. Pull it back to 90 - 95 knots and you get 1800 - 2000 FPM. The angle of climb will frighten you at first ... it is definitely not a Piper !!!!! Cruise at 4500' is around 140-145 kts at 2350 rpm. Yesterday I saw a ground speed of 210 mph. I like that !!! One of the most pleasant surprises is the ease of landing. According to my training with Mike Seager in the 6A ... I would say the 8A is easier to land. It is such a thrill to open that hanger to see a plane ready to fly sitting there. That alone is enough for me to encourage you to keep working hard. Don't give up. There are many times during the final six months you feel like selling it as scrap aluminum but just a few hours in the air will make you glad you didn't. Len Leggette RV-8A N901LL (res) Greensboro, N.C. 14 hours !!


    Message 5


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    Time: 06:27:19 AM PST US
    From: "Elsa & Henry" <elsa-henry@darlor-watch.com>
    Subject: Re: How to torque a bolt?
    --> RV-List message posted by: "Elsa & Henry" <elsa-henry@darlor-watch.com> As some have responded, you torque the nut. But there will be instances where this cannot be done, such as the bolts that hold the u/c weldments to the bulkhead and spar on the 6-A. In those cases, add a AN 960 washer under the bolt head (if its length allows), coat the shank, (NOT THE THREADS) with a little anti-seize compound and torque the bolt to near the top limit of ft-lbs as shown in in AC 43-13-XX Cheers!!-------Henry Hore


    Message 6


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    Time: 06:34:53 AM PST US
    From: "Rick Galati" <rick07x@earthlink.net>
    Subject: Re: Bench grinder vs Buffer
    --> RV-List message posted by: "Rick Galati" <rick07x@earthlink.net> Will Lynda, My bench grinder, like most is not really the best platform for buffing operations but as a construction tool a grinder will get used much more often. So if it were an either/or buying choice, I would go with a grinder. Faced with buffing out my aluminum spinner and not willing to spring for a new buffing machine, I used my Delta drill press and it worked out just fine. With 12 speeds to choose from, it was easy to select an optimum speed based upon the diameter of a given buffing wheel. I simply mounted the buffing wheel on a long 1/4" threaded bolt well away from the drill press's chuck. With a 16" throat, it was no problem to manipulate the spinner without any chance of it bumping up against anything. It took a little getting used to having the buffing wheel attached and spinning vertically rather than horizontally but was really no big deal. Rick Galati --- Rick Galati --- rick07x@earthlink.net


    Message 7


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    Time: 07:02:44 AM PST US
    From: "Carl Froehlich" <carlfro@erols.com>
    Subject: Runaway Trim
    --> RV-List message posted by: "Carl Froehlich" <carlfro@erols.com> In a word - no. Flaps don't get touched unless you are slow anyway. The elevator and/or aileron trim, even at extreme travel, are controllable with the stick. Carl Froehlich RV-8A (flying) Vienna, VA -----Original Message----- From: owner-rv-list-server@matronics.com [mailto:owner-rv-list-server@matronics.com]On Behalf Of Vincent Welch Subject: RV-List: Runaway Trim --> RV-List message posted by: "Vincent Welch" <welchvincent@hotmail.com> Hey Guys, I am building my electrical distribution around the EXP Bus (before you start about Bob and his fuses, I already have the unit in hand and intend to use it). I was reading the most recent issue of Sport Aviation discussing cockpit layout. One of the items mentioned was being able to reach circuit breakers to disconnect in the event of runaway trim or flaps. I can accomplish this by putting switches in the power line (trim and flaps are actuated by switching the ground). Has anyone had a problem with runaway trim with the MAC units? Has anyone had uncommanded flap movement? In other words, do I really need to include the disconnect switches? Vince Welch RV-8A


    Message 8


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    Time: 07:08:54 AM PST US
    From: "Ed's Compuserve" <edwardoconnor@compuserve.com>
    Subject: Re: engine mount holes
    --> RV-List message posted by: "Ed's Compuserve" <edwardoconnor@compuserve.com> Take a look at some pictures on my web site. I used an engine stand and 2x4s. I did not drill out the holes. I cut some threaded rod to length through the firewall and 2x4s and taps on each end. I fabricated an adjustable tail stand since you have to do some things to the fuselage with it level. Site <http://homepage.mac.com/edwardoconnor>


    Message 9


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    Time: 07:54:26 AM PST US
    From: "Vincent Welch" <welchvincent@hotmail.com>
    Subject: Runaway Trim
    --> RV-List message posted by: "Vincent Welch" <welchvincent@hotmail.com> Thanks Carl, just trying to see if there is any failure mode that could apply a ground to one of the control wires. It would make for a bad day if something chaffed and the flap down wire found a ground in cruise flight. Do Not Archive Vince >From: "Carl Froehlich" <carlfro@erols.com> >Reply-To: rv-list@matronics.com >To: <rv-list@matronics.com> >Subject: RE: RV-List: Runaway Trim >Date: Sun, 1 Dec 2002 10:00:57 -0500 > >--> RV-List message posted by: "Carl Froehlich" <carlfro@erols.com> > >In a word - no. Flaps don't get touched unless you are slow anyway. The >elevator and/or aileron trim, even at extreme travel, are controllable with >the stick. > >Carl Froehlich >RV-8A (flying) >Vienna, VA > > >-----Original Message----- >From: owner-rv-list-server@matronics.com >[mailto:owner-rv-list-server@matronics.com]On Behalf Of Vincent Welch >To: rv-list@matronics.com >Subject: RV-List: Runaway Trim > > >--> RV-List message posted by: "Vincent Welch" <welchvincent@hotmail.com> > > >Hey Guys, > >I am building my electrical distribution around the EXP Bus (before you >start about Bob and his fuses, I already have the unit in hand and intend >to >use it). I was reading the most recent issue of Sport Aviation discussing >cockpit layout. One of the items mentioned was being able to reach circuit >breakers to disconnect in the event of runaway trim or flaps. I can >accomplish this by putting switches in the power line (trim and flaps are >actuated by switching the ground). Has anyone had a problem with runaway >trim with the MAC units? Has anyone had uncommanded flap movement? In >other words, do I really need to include the disconnect switches? > >Vince Welch >RV-8A > >


    Message 10


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    Time: 08:30:30 AM PST US
    Subject: Re: Alternative Engine Questions
    From: lm4@juno.com
    --> RV-List message posted by: lm4@juno.com Chris, Subaru has a boxer engine (horizontally opposed) much like lync. or cont. It's 2.5 liter (2500 cc) will put out 160 to 220 HP depending on weather it's turbo'd or has a cam grind etc. It also happens to be liquid cooled, which means far better engine heat balancing as well as heat in the cabin. You could probably complete a project such as this for 7 thousand or so. Thats about where the prices start for a mid time linc., probably without accessories ($$$). I keep hearing that such a soob can run at cruise on about 8 gal. /Hr while the comparable lync would use about 10 to 13. Thats part of the answer. HTH Larry Mac Donald Rochester N.Y. On Sat, 30 Nov 2002 19:02:09 -0600 Chris <chrisw3@cox.net> writes: > --> RV-List message posted by: Chris <chrisw3@cox.net> > > Ok I know the basics about how engines work and what the difference > between 2 and 4 stroke, gas and diesel, Fuel injection and > Carburetors > but that is about it. Lately there is a lot of talk about > "alternative" > engines. One of the things everyone seems to hit on, is that > traditional aviation engines are an old design and that newer > engines in > cars are more "high tech". As I see it most of the high tech with > the > ECU and sensors is as much for pollution control as anything else. > I > personally couldn't care less about emissions and if those who are > in > power really cared, I would be able to fill my car with Propane, > Natural > Gas, Methanol, and or Hydrogen at the corner gas station, but back > to > the topic. Also there is a lot in car engines to allow them to run > efficiently at low power settings which we don't really care about > in > airplanes. My question is this. Other than Electronic Ignition > (which > is easy enough to put on a more traditional aircraft engine) what is > so > high tech about car engines that has any application in an airplane? > > -- > Chris Woodhouse > 3147 SW 127th St. > Oklahoma City, OK 73170 > 405-691-5206 (home) > chrisw@programmer.net > N35 20.492' > W97 34.342' > > > > _-> > > > > > > >


    Message 11


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    Time: 08:35:48 AM PST US
    From: "Elsa & Henry" <elsa-henry@darlor-watch.com>
    Subject: Re: engine mount holes and installing it!
    --> RV-List message posted by: "Elsa & Henry" <elsa-henry@darlor-watch.com> Living in Canada, I bought all the kits at one time to avoid the annual price-hikes and the pitfalls of several border crossings. Thus I had the engine mount available at the time I built-up the firewall. I simply laid it flat on a table, centered the mount on it, clamped it in place and then back-drilled the holes through the tubes using a 3/8" B&D Bullet drill. Worked great! With the fuselage out of the jig and up-right, I used two 2x4"s bolted to the firewall (through the mount holes) to act as front legs. Before mounting the engine, I turned the fuselage on it side resting it on two other 2x4"s bolted in place. I then primed the belly and painted it with the final finish colour. Sure beats crawling under the fuselage to do that later! Regarding mounting the engine: Van's instructions on how to install the bolts through the "Lord" mounts (at least in the manual that came with my kit in 1995) are a "bunch of garbage"! It says, with the engine suspended, "----it can be moved into position on the engine mount and the two upper Lord mounts and the bolts installed (*) and partially tightened. then by lifting the engine with the hoist, and actually lifting part of the airframe also, the upper lord mounts are flexed upward enough that the lower mounts are then brought nearly into position.---"--Nuts!! Think about it! If you do as suggested, all that will happen is that the engine will pivot upward on the top mounts and PULL AWAY from the bottom ones!! No way will you be "--- lifting part of the airframe also---"!! (*) That's the problem,-getting those first two bolts through! Here is what I did, working alone: I used two lengths of 1/4" threaded rod to clamp the top mounts. Being 1/8" smaller dia. than the bolts, they went in easily. Then I lowered the hoist to allow the weight of the engine to COMPRESS the front biscuit of the lower mounts. I could peer through from the rear and align the biscuit with the engine bolt hole and then insert the bolt and the rear biscuit easily. Once both bolts were in and tight, I lifted the engine to compress the top front biscuit of the top mounts and removing the 1/4" rods, inserted the bolts as was done on the bottom.---Simple and easy. Sure beats some articles I've seen in other publications that describe how other people did it with aides pushing and heaving to get the bolts in! Cheers!!--------Henry Hore


    Message 12


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    Time: 09:25:38 AM PST US
    From: Jerry Springer <jsflyrv@earthlink.net>
    Subject: Re: Runaway Trim
    --> RV-List message posted by: Jerry Springer <jsflyrv@earthlink.net> In an emergency situation like that you could turn the master switch off. I do not buy the Bob Nucholls approach to not be able to reach the breakers. In my airplane I use the breaker switch combination, So I can turn off any circuit I wish with a circuit breaker switch. Jerry Vincent Welch wrote: > --> RV-List message posted by: "Vincent Welch" <welchvincent@hotmail.com> > > Thanks Carl, just trying to see if there is any failure mode that could > apply a ground to one of the control wires. It would make for a bad day if > something chaffed and the flap down wire found a ground in cruise flight. > > Do Not Archive > > > Vince > > > >>From: "Carl Froehlich" <carlfro@erols.com> >>Reply-To: rv-list@matronics.com >>To: <rv-list@matronics.com> >>Subject: RE: RV-List: Runaway Trim >>Date: Sun, 1 Dec 2002 10:00:57 -0500 >> >>--> RV-List message posted by: "Carl Froehlich" <carlfro@erols.com> >> >>In a word - no. Flaps don't get touched unless you are slow anyway. The >>elevator and/or aileron trim, even at extreme travel, are controllable with >>the stick. >> >>Carl Froehlich >>RV-8A (flying) >>Vienna, VA >> >> >>-----Original Message----- >>From: owner-rv-list-server@matronics.com >>[mailto:owner-rv-list-server@matronics.com]On Behalf Of Vincent Welch >>To: rv-list@matronics.com >>Subject: RV-List: Runaway Trim >> >> >>--> RV-List message posted by: "Vincent Welch" <welchvincent@hotmail.com> >> >> >>Hey Guys, >> >>I am building my electrical distribution around the EXP Bus (before you >>start about Bob and his fuses, I already have the unit in hand and intend >>to >>use it). I was reading the most recent issue of Sport Aviation discussing >>cockpit layout. One of the items mentioned was being able to reach circuit >>breakers to disconnect in the event of runaway trim or flaps. I can >>accomplish this by putting switches in the power line (trim and flaps are >>actuated by switching the ground). Has anyone had a problem with runaway >>trim with the MAC units? Has anyone had uncommanded flap movement? In >>other words, do I really need to include the disconnect switches? >> >>Vince Welch >>RV-8A >> >> >


    Message 13


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    Time: 09:48:23 AM PST US
    From: "Elsa & Henry" <elsa-henry@darlor-watch.com>
    Subject: Re: Bench grinder vs Buffer
    --> RV-List message posted by: "Elsa & Henry" <elsa-henry@darlor-watch.com> The very, VERY, best tool to have in your shop is table-top 1'' belt sander! I have a Delta 31-050. It uses 30'' dia. belts which are easily available in several grit sizes. My wife also loves it because I use it to sharpen all her kitchen knives using the fine grit belt. Practically every piece of aluminum on my 6-A has had corners and slots cleaned, deburred, rounded, etc, and after 7 years of use (abuse?) it's still going strong! I don't know if Delta still make that model. The ones I see advertised also have a disc sander on the side of the belt drive. Maybe this is a better purchase. A bench grinder is not good for doing aluminum work. The wheels that come with them are too coarse for that and will clog-up. I am fortunate enough to have the original "ShopSmith" (now 50 years old) and I use it for all drill-press work and have the scotch-bright wheel mounted on one of its arbors. Another most useful tool is a Dremel hand grinder-polisher. Funnily enough the kit does not include the most useful accessory (not here in Canada anyway) which is a fiber reinforced cut-off wheel.The ones that come with the kit are not reinforced and shatter at the least excuse. "Craftsman" (#36959) makes a 1 1/4"dia x 1/32" thk wheel (5 in package) that is great to cut aluminum sheet and cut holes, for example the Naca vent-holes in the fuselage side. They wear pretty fast cutting aluminum, you'll find!


    Message 14


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    Time: 10:48:48 AM PST US
    From: Jerry Springer <jsflyrv@earthlink.net>
    Subject: Re: Bench grinder vs Buffer
    --> RV-List message posted by: Jerry Springer <jsflyrv@earthlink.net> I find that a double ended type bench grinder works great. Have a fine grinding wheel on one end and a Scotch type buffing wheel on the other end. Elsa & Henry wrote: > --> RV-List message posted by: "Elsa & Henry" <elsa-henry@darlor-watch.com> > > The very, VERY, best tool to have in your shop is table-top 1'' belt sander! > I have a Delta 31-050. It uses 30'' dia. belts which are easily available in > several grit sizes. My wife also loves it because I use it to sharpen all > her kitchen knives using the fine grit belt. Practically every piece of > aluminum on my 6-A has had corners and slots cleaned, deburred, rounded, > etc, and after 7 years of use (abuse?) it's still going strong! I don't know > if Delta still make that model. The ones I see advertised also have a disc > sander on the side of the belt drive. Maybe this is a better purchase. > > A bench grinder is not good for doing aluminum work. The wheels that come > with them are too coarse for that and will clog-up. I am fortunate enough to > have the original "ShopSmith" (now 50 years old) and I use it for all > drill-press work and have the scotch-bright wheel mounted on one of its > Yes, they well clog up, but just use a grinding wheel dressing tool to clean it once in a while. Jerry do not archive


    Message 15


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    Time: 11:17:16 AM PST US
    From: Wheeler North <wnorth@sdccd.cc.ca.us>
    Subject: Engines
    --> RV-List message posted by: Wheeler North <wnorth@sdccd.cc.ca.us> Well, The only real difference between auto vs. aviation engines is their respective missions. One is designed to accelerate and decelerate a lot, to not run at full power continously and to deliver reasonable power over its entire RPM range which can be from 600-6000 RPM commonly, the other is designed to stay at a constant power/RPM setting, to deliver most of its power between 2000-2700 RPM, and run at full power until it wears out. And finally one is designed to spin a nice round symetrical weight, where the other is designed to spin a god awful set of paddles that are trying to rip its face off in five different ways, at all times. ;{) So, trying to use one for the other, either way, is kinda silly, expensive and can be risky if not done correctly, not that there really is a correct way to do this. (I know I'm gonna get flammed here) Its just that it makes no sense to me to redesign something to an application that no part in it was ever designed for, when there is already something that is designed for this. (You will not save one dime doing this, but you might have some fun if you are into that much work.) I think we will get a lot further by using our efforts at improving the thing that was designed for this application, rather than redesigning something that wasn't meant for this application. Which, by the way, is what the engine manufacturers are doing via the IOF-360 lyc and the IOF-240 Cont. being produced or modified by TCM Aerosance. TexLyc is also working on their own version of this, but they both need to get a clue on costs. The TCM FADEC costs as much as the engine does. I am in the middle of installing one and its a nice product if it runs well, but damm, the cost is unbelieveable. The real issue about these powerplant costs are mass production.... So next time you order an aircraft engine, order twenty of them.... ;{)


    Message 16


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    Time: 11:40:13 AM PST US
    From: Chris <chrisw3@cox.net>
    <ExperimentalAvionics@yahoogroups.com>, RV-list <rv-list@matronics.com>, vansairforce <vansairforce@yahoogroups.com>
    Subject: Data recording
    --> RV-List message posted by: Chris <chrisw3@cox.net> I was thinking it would be nice to be able to record EGT CHT OAT Altitude, IAS and GPS data on a frequency of a few times a second. I think this would be a very valuable tool while in the test flight stage of a new home built plane. Is there a way to do this with say a lap top and no more than say $2000 for the data acquisition equipment. I know recording the GPS data wouldn't be that hard with a lap top but what about all the rest of it? -- Chris Woodhouse 3147 SW 127th St. Oklahoma City, OK 73170 405-691-5206 (home) chrisw@programmer.net N35 20.492' W97 34.342'


    Message 17


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    Time: 12:03:16 PM PST US
    From: "Mike Robertson" <mrobert569@hotmail.com>
    Subject: Re: Working on a non-owner built RV
    --> RV-List message posted by: "Mike Robertson" <mrobert569@hotmail.com> >From: "Paul Besing" <azpilot@extremezone.com> >Reply-To: rv-list@matronics.com >To: <rv-list@matronics.com> >Subject: Re: RV-List: Working on a non-owner built RV >Date: Sat, 30 Nov 2002 13:56:58 -0700 > >--> RV-List message posted by: "Paul Besing" <azpilot@extremezone.com> > >You got it. Since you don't hold the repairman certificate, treat it like >a >certified plane, as far as work is concerned. All your work (beyond >maintenance such as oil changes, tires, etc) needs to be signed off by an >A&P, or the the builder that holds the repairman certificate. For the >annual condition inspection, it needs to be an IA or the original builder. > >Paul Besing >RV-6A Sold (Waiting on the RV-10) >http://www.lacodeworks.com/besing >Kitlog Pro Builder's Log Software >http://www.kitlog.com > >----- Original Message ----- >From: "Henry Hochberg" <infodocta@pol.net> >To: <rv-list@matronics.com> >Subject: RV-List: Working on a non-owner built RV > > > > --> RV-List message posted by: Henry Hochberg <infodocta@pol.net> > > > > > > This question may have been addressed before, so excuse me if it has. > > When you buy a used RV and then want to do the work on it yourself, > > including major work (such as converting mechanical flaps to > > electrical), what do the regs say about your not being the builder? > > Can you just have an IA supervise?Thanks. > > > > Henry H. > > > > > > ------------------ Reply Separator -------------------- > > Originally From: RV-List Digest Server <rv-list-digest@matronics.com> > > Subject: RV-List Digest: 34 Msgs - 11/27/02 > > Date: 11/27/2002 11:57pm > > > > > > * > > > > > > Paul, I'm sorry but I have to jump in here. Anybody can work on an experimental aircraft and no certificate at all is required. The only time a certificate is required by regulations is during the annual condition inspection. Then, only the original builder with a Repairman's Certificate or an licensed A&P, not an IA, can conduct the inspection. As to major alterations you have to go by whatever tyhe Operating Linmitations state. The older ones say that any major change has to be coordinated with the local FSDO, and the new ones state that the owner can just make an entry in the maintenance logs, conduct a minimum 5 hour test flight, sign it off and go on your merry way. Just remember....ALL maintenance MUST be entered in the maintenance logs. Seeing as how anybody can do the maintenance, only those entries not entered could get one in trouble (maybe). Mike Robertson DAS FED RV-8A, 6A, 9A


    Message 18


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    Time: 12:27:59 PM PST US
    From: "Paul Besing" <azpilot@extremezone.com>
    Subject: Re: Working on a non-owner built RV
    --> RV-List message posted by: "Paul Besing" <azpilot@extremezone.com> Thanks, Mike. Yes, I was corrected many times. I was just going off of what my DAR told me. It seems that there is alot of mis information being dissimated by the different DAR's out there. They all have their own idea on what the regs say we must do. Paul Besing RV-6A Sold (Waiting on the RV-10) http://www.lacodeworks.com/besing Kitlog Pro Builder's Log Software http://www.kitlog.com ----- Original Message ----- From: "Mike Robertson" <mrobert569@hotmail.com> Subject: Re: RV-List: Working on a non-owner built RV > --> RV-List message posted by: "Mike Robertson" <mrobert569@hotmail.com> > > > >From: "Paul Besing" <azpilot@extremezone.com> > >Reply-To: rv-list@matronics.com > >To: <rv-list@matronics.com> > >Subject: Re: RV-List: Working on a non-owner built RV > >Date: Sat, 30 Nov 2002 13:56:58 -0700 > > > >--> RV-List message posted by: "Paul Besing" <azpilot@extremezone.com> > > > >You got it. Since you don't hold the repairman certificate, treat it like > >a > >certified plane, as far as work is concerned. All your work (beyond > >maintenance such as oil changes, tires, etc) needs to be signed off by an > >A&P, or the the builder that holds the repairman certificate. For the > >annual condition inspection, it needs to be an IA or the original builder. > > > >Paul Besing > >RV-6A Sold (Waiting on the RV-10) > >http://www.lacodeworks.com/besing > >Kitlog Pro Builder's Log Software > >http://www.kitlog.com > > > >----- Original Message ----- > >From: "Henry Hochberg" <infodocta@pol.net> > >To: <rv-list@matronics.com> > >Subject: RV-List: Working on a non-owner built RV > > > > > > > --> RV-List message posted by: Henry Hochberg <infodocta@pol.net> > > > > > > > > > This question may have been addressed before, so excuse me if it has. > > > When you buy a used RV and then want to do the work on it yourself, > > > including major work (such as converting mechanical flaps to > > > electrical), what do the regs say about your not being the builder? > > > Can you just have an IA supervise?Thanks. > > > > > > Henry H. > > > > > > > > > ------------------ Reply Separator -------------------- > > > Originally From: RV-List Digest Server <rv-list-digest@matronics.com> > > > Subject: RV-List Digest: 34 Msgs - 11/27/02 > > > Date: 11/27/2002 11:57pm > > > > > > > > > * > > > > > > > > > > > Paul, > > I'm sorry but I have to jump in here. Anybody can work on an experimental > aircraft and no certificate at all is required. The only time a certificate > is required by regulations is during the annual condition inspection. Then, > only the original builder with a Repairman's Certificate or an licensed A&P, > not an IA, can conduct the inspection. > As to major alterations you have to go by whatever tyhe Operating > Linmitations state. The older ones say that any major change has to be > coordinated with the local FSDO, and the new ones state that the owner can > just make an entry in the maintenance logs, conduct a minimum 5 hour test > flight, sign it off and go on your merry way. > Just remember....ALL maintenance MUST be entered in the maintenance logs. > Seeing as how anybody can do the maintenance, only those entries not entered > could get one in trouble (maybe). > > Mike Robertson > DAS FED > RV-8A, 6A, 9A > >


    Message 19


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    Time: 01:44:55 PM PST US
    From: Tedd McHenry <tedd@vansairforce.org>
    Subject: Re: Engines
    --> RV-List message posted by: Tedd McHenry <tedd@vansairforce.org> > Its just that it makes no sense to me to redesign something to an > application that no part in it was ever designed for, Many people say this, or something like it (including Van), but never, ever mention even one thing that would be done differently on an engine designed for automotive use as compared to aircraft use. I'm not suggesting that there are no differences, but I am suggesting that most of the people who say this have little idea what any of those differences are. Which makes me wonder what makes them think they're qualified to offer an opinion. Tedd McHenry Surrey, BC -6 wings


    Message 20


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    Time: 01:44:57 PM PST US
    From: "Kyle Boatright" <kyle.boatright@adelphia.net>
    Subject: Re: Alternative Engine Questions
    --> RV-List message posted by: "Kyle Boatright" <kyle.boatright@adelphia.net> I've got a buddy who has installed one of the 220 HP Subaru's in his Velocity. He's achieved 27 hours and 3 engine related emergency landings since his first flight last February. This is an individual who has gone the extra step to do things right, and he still doesn't have a satisfactory drivetrain. So far, his biggest problem is finding a reliable gearbox.He's on gearbox MK III now, and is dealing with people who advertise these things in the back of Sport Aviation. If you want to fly and not tinker, go with a proven package. Kyle Boatright ----- Original Message ----- From: <lm4@juno.com> Subject: Re: RV-List: Alternative Engine Questions > --> RV-List message posted by: lm4@juno.com > > Chris, > Subaru has a boxer engine (horizontally opposed) much like > lync. or cont. It's 2.5 liter (2500 cc) will put out 160 to 220 HP > depending on weather it's turbo'd or has a cam grind etc. It also > happens to be liquid cooled, which means far better engine heat > balancing as well as heat in the cabin. You could probably complete > a project such as this for 7 thousand or so. Thats about where the > prices start for a mid time linc., probably without accessories ($$$). > I keep hearing that such a soob can run at cruise on about 8 gal. /Hr > while the comparable lync would use about 10 to 13. Thats part of > the answer. HTH > Larry Mac Donald > Rochester N.Y. > > On Sat, 30 Nov 2002 19:02:09 -0600 Chris <chrisw3@cox.net> writes: > > --> RV-List message posted by: Chris <chrisw3@cox.net> > > > > Ok I know the basics about how engines work and what the difference > > between 2 and 4 stroke, gas and diesel, Fuel injection and > > Carburetors > > but that is about it. Lately there is a lot of talk about > > "alternative" > > engines. One of the things everyone seems to hit on, is that > > traditional aviation engines are an old design and that newer > > engines in > > cars are more "high tech". As I see it most of the high tech with > > the > > ECU and sensors is as much for pollution control as anything else. > > I > > personally couldn't care less about emissions and if those who are > > in > > power really cared, I would be able to fill my car with Propane, > > Natural > > Gas, Methanol, and or Hydrogen at the corner gas station, but back > > to > > the topic. Also there is a lot in car engines to allow them to run > > efficiently at low power settings which we don't really care about > > in > > airplanes. My question is this. Other than Electronic Ignition > > (which > > is easy enough to put on a more traditional aircraft engine) what is > > so > > high tech about car engines that has any application in an airplane? > > > > -- > > Chris Woodhouse > > 3147 SW 127th St. > > Oklahoma City, OK 73170 > > 405-691-5206 (home) > > chrisw@programmer.net > > N35 20.492' > > W97 34.342' > > > > > > > > _-> > > > > > > > > > > > > > > > >


    Message 21


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    Time: 01:55:46 PM PST US
    From: "Karen and Robert Brown" <bkbrown@wmca.net>
    Subject: rudder pedal assemblies - RV7QB
    --> RV-List message posted by: "Karen and Robert Brown" <bkbrown@wmca.net> I am bummed at my lack of foresight, but felt the need to warn other builders, especially QB's... The plans give exact dimensions to trim the (steel) rudder pedal weldments, in my case 40 1/8" for the right and 40 5/32" for the left. I dutifully trimmed to those exact dimensions. When I trial fitted the (trimmed) assembly to the fuselage at the 3" minimum distance (from the forward side of the firewall stiffener), I find that I have .16" of rudder pedal weldment end play. I don't know what that magic number should be, but if the side rudder pedal bearing blocks (the rudder assembly) are adjusted toward a more aft position, this rudder pedal weldment endplay becomes more like over 1/2", which really seems like a lot of lateral movement in the rudder pedals. I know I should have trial fitted the rudder pedal weldments before I trimmed...but at least my rudder pedals are cut to the length specified in the plans! I trimmed a total of .117" from these steel tubes, I think I would have been better off not trimming at all. I think I am going to install some 1" nylon washers inside the (nylon) side rudder pedal bearing blocks to reduce the endplay, any thoughts on this remedy?? Bob Brown RV7A - fuselage


    Message 22


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    Time: 02:06:04 PM PST US
    From: "Karen and Robert Brown" <bkbrown@wmca.net>
    Subject: baggage area floors, strobes & ELT's - RV7
    --> RV-List message posted by: "Karen and Robert Brown" <bkbrown@wmca.net> Thanks for the suggestions on the placement of strobe power supplies and ELT's. I will be placing mine between the ribs under the baggage floor similar to some of the examples sent to me offline. I have installed nutplates at various locations in the baggage area ribs to make the baggage area floor panels removable...I don't like having places in the airplane I can't LOOK at. This option will also allow easy installation and future inspection access for antennas and wiring. Again, thanks for the options...there's a lot of thoughtful builders out there. Bob Brown RV7A - fuselage


    Message 23


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    Time: 02:53:21 PM PST US
    From: "Terry Watson" <terry@tcwatson.com>
    Subject: Data recording
    --> RV-List message posted by: "Terry Watson" <terry@tcwatson.com> Bluemountain's EFIS-one has a built-in data recorder that records "each fixed sensor and every user configured sensor written every 5 seconds." Their example includes time, airspeed, true airspeed, altitude, outside air temperature, density altitude, heading, rpm, manifold pressure, fuel left, fuel right, volts, fuel pressure, oil pressure, and coolant pressure. The flash memory in it can hold 12 hours of flight data. Terry --> RV-List message posted by: Chris <chrisw3@cox.net> I was thinking it would be nice to be able to record EGT CHT OAT Altitude, IAS and GPS data on a frequency of a few times a second. I think this would be a very valuable tool while in the test flight stage of a new home built plane. Is there a way to do this with say a lap top and no more than say $2000 for the data acquisition equipment. I know recording the GPS data wouldn't be that hard with a lap top but what about all the rest of it?


    Message 24


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    Time: 03:04:32 PM PST US
    From: Kevin Horton <khorto1537@rogers.com>
    Subject: Re: Data recording
    --> RV-List message posted by: Kevin Horton <khorto1537@rogers.com> >--> RV-List message posted by: Chris <chrisw3@cox.net> > >I was thinking it would be nice to be able to record EGT CHT OAT >Altitude, IAS and GPS data on a frequency of a few times a second. I >think this would be a very valuable tool while in the test flight stage >of a new home built plane. Is there a way to do this with say a lap top >and no more than say $2000 for the data acquisition equipment. I know >recording the GPS data wouldn't be that hard with a lap top but what >about all the rest of it? > >-- >Chris Woodhouse >3147 SW 127th St. >Oklahoma City, OK 73170 >405-691-5206 (home) >chrisw@programmer.net >N35 20.492' >W97 34.342' > Some of the integrated engine instrument packages are designed to either record data, or to feed it to a laptop so it can record it. I know the Grand Rapids EIS systems can output data to a laptop, and I believe the Rocky Mountain microMonitor has some sort of functionality like this. -- Kevin Horton RV-8 (baffles, induction air, oil cooler) Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/


    Message 25


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    Time: 03:12:23 PM PST US
    From: "Tom Barnes" <skytop@megsinet.net>
    Subject: manifold pressure reads low on VM-1000
    --> RV-List message posted by: "Tom Barnes" <skytop@megsinet.net> Listers, With the engine off, the VM-1000 reports manifold pressure at 29.2 when it should be reporting 29.8 +/- (based on field elevation). I talked to the Vision "man" while at OSH and he said I have a unit that is at the limit of their tolerance. Looking through the archives, I can find no other references to this problem. He offered to allow me to try another unit, but before I do that, I would like to know if this is an issue that I should or should not be concerned with. Thanks in advance for any personal experience on this issue. Tom Barnes -6 in hangar, wings on.


    Message 26


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    Time: 03:56:22 PM PST US
    From: "Doug Rozendaal" <dougr@petroblend.com>
    Subject: Re: Data recording
    --> RV-List message posted by: "Doug Rozendaal" <dougr@petroblend.com> Go to this site and click Data Acquisition, you can collect all kinds of info and it is not that expensive. You need to be a whiz to get is all wired up and programed, but the equipment is not that expensive. BTW they have a GREAT set of catalogs that have loads of good info and ideas in them. Tailwinds Doug Rozendaal ----- Original Message ----- From: "Chris" <chrisw3@cox.net>


    Message 27


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    Time: 04:27:45 PM PST US
    From: "James E. Clark" <jclark@conterra.com>
    Subject: Data recording
    --> RV-List message posted by: "James E. Clark" <jclark@conterra.com> Take a visit to: http://flightperformance.com/default.htm The system does not do everything you want but many of the things you mention. I think it is about $2500. James > -----Original Message----- > From: owner-rv-list-server@matronics.com > [mailto:owner-rv-list-server@matronics.com]On Behalf Of Chris > Sent: Sunday, December 01, 2002 2:42 PM > To: ExperimentalAvionics@yahoogroups.com; RV-list; vansairforce > Subject: RV-List: Data recording > > > --> RV-List message posted by: Chris <chrisw3@cox.net> > > I was thinking it would be nice to be able to record EGT CHT OAT > Altitude, IAS and GPS data on a frequency of a few times a second. I > think this would be a very valuable tool while in the test flight stage > of a new home built plane. Is there a way to do this with say a lap top > and no more than say $2000 for the data acquisition equipment. I know > recording the GPS data wouldn't be that hard with a lap top but what > about all the rest of it? > > -- > Chris Woodhouse > 3147 SW 127th St. > Oklahoma City, OK 73170 > 405-691-5206 (home) > chrisw@programmer.net > N35 20.492' > W97 34.342' > >


    Message 28


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    Time: 04:32:07 PM PST US
    From: "Alex Peterson" <alexpeterson@usjet.net>
    Subject: Runaway Trim
    --> RV-List message posted by: "Alex Peterson" <alexpeterson@usjet.net> > apply a ground to one of the control wires. It would make > for a bad day if > something chafed and the flap down wire found a ground in > cruise flight. It should take more than this failure to cause uncommanded flap movement. The standard flap wiring should take a hot wire and ground wire to the center of a DPDT, three position spring centered switch. Everything "downstream" of this switch, when it is in the neutral position, is dead, meaning it is totally disconnected from the airplane. Two different things would have to spontaneously happen to cause an uncommanded flap movement. A more probable failure would be the switch sticking during a commanded movement. Alex Peterson Maple Grove, MN RV6-A N66AP 235 hours www.usfamily.net/web/alexpeterson


    Message 29


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    Time: 04:34:08 PM PST US
    From: "Doug Rozendaal" <dougr@petroblend.com>
    Subject: Re: Data recording
    --> RV-List message posted by: "Doug Rozendaal" <dougr@petroblend.com> DUH! www.omega.com then click Data Acquisition ----- Original Message ----- From: "Doug Rozendaal" <dougr@petroblend.com> Subject: Re: RV-List: Data recording > --> RV-List message posted by: "Doug Rozendaal" <dougr@petroblend.com> > > Go to this site and click Data Acquisition, > > you can collect all kinds of info and it is not that expensive. You need to > be a whiz to get is all wired up and programed, but the equipment is not > that expensive. BTW they have a GREAT set of catalogs that have loads of > good info and ideas in them. > > Tailwinds > Doug Rozendaal > > ----- Original Message ----- > From: "Chris" <chrisw3@cox.net> > To: <ExperimentalAvionics@yahoogroups.com>; " > >


    Message 30


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    Time: 04:39:19 PM PST US
    From: "Alex Peterson" <alexpeterson@usjet.net>
    Subject: manifold pressure reads low on VM-1000
    --> RV-List message posted by: "Alex Peterson" <alexpeterson@usjet.net> > With the engine off, the VM-1000 reports manifold > pressure at 29.2 when it should be reporting 29.8 +/- (based > on field elevation). You probably already have this figured correctly, but.... How are you getting the 29.8" in the above example? The ATIS or whatever will only give a barometer reading which will agree with a MAP gauge at a sea level airport. Alex Peterson Maple Grove, MN RV6-A N66AP 235 hours www.usfamily.net/web/alexpeterson


    Message 31


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    Time: 04:48:19 PM PST US
    From: Jim Bean <jim-bean@att.net>
    Subject: Oil Cooler/Heat Muff
    --> RV-List message posted by: Jim Bean <jim-bean@att.net> I have my oil cooler mounted on the baffle behind #3 cylinder, pretty much as Van's drawing shows. My heat muff is below on a cross tube. It would be rather convenient to run the heat muff scat tube off of the back of the oil cooler. I am picturing a 2" flange placed over the bottom of the back of the cooler. I am not looking to improve the heating effiency, it's just a mechanically convenient way to get the scat tube to the heat muff. The engine is an IO360 which seems to need all the cooling it can get. On the other hand there is constant air flow through the muff because the heat valve dumps it overboard when heat is not is use So what does the group think about the effect this might have on the oil cooler, IE might it raise the oil temp? Anybody tried this? Jim Bean RV-8 Cooling Baffles (3 months) Starting third year building


    Message 32


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    Time: 05:02:28 PM PST US
    From: kempthornes <kempthornes@earthlink.net>
    Subject: Re: Engines
    --> RV-List message posted by: kempthornes <kempthornes@earthlink.net> At 11:14 AM 12/1/2002 -0800, you wrote: >--> RV-List message posted by: Wheeler North <wnorth@sdccd.cc.ca.us> > >Its just that it makes no sense to me ................ Lots of things make no sense to me -- usually because I am ignorant about them. K. H. (Hal) Kempthorne RV6-a N7HK flying! PRB (El Paso de Robles, CA)


    Message 33


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    Time: 05:12:38 PM PST US
    From: kempthornes <kempthornes@earthlink.net>
    Subject: Re: Alternative Engine Questions
    --> RV-List message posted by: kempthornes <kempthornes@earthlink.net> At 04:40 PM 12/1/2002 -0500, you wrote: >--> RV-List message posted by: "Kyle Boatright" <kyle.boatright@adelphia.net> > >I've got a buddy who has installed one of the 220 HP Subaru's in his >Velocity. He's achieved 27 hours and 3 engine related emergency landings >since his first flight last February. This is an individual who has gone >the extra step to do things right, and he still doesn't have a satisfactory >drivetrain. Give him some encouragement, Kyle. You are a buddy. There is a story about an engineering manager, at Baldwin Locomotive Works I think. After a new locomotive was all designed he gathered his engineers together and said, "Okay, guys, let's build one and see what doesn't work". The development of new products involves many corrections along the way. Guys who do engine conversions right, like your buddy, are bold adventurers. They have the courage (and funds) the rest of us lack. Aren't there builders with a few engine related emergency landings who are flying Lycomings????? K. H. (Hal) Kempthorne RV6-a N7HK flying! PRB (El Paso de Robles, CA)


    Message 34


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    Time: 05:33:46 PM PST US
    From: Dave Bristol <bj034@lafn.org>
    Subject: Re: Alternative Engine Questions
    --> RV-List message posted by: Dave Bristol <bj034@lafn.org> 220 HP is a LOT of power to be asking of a 152 cu engine, and even 1 HP per cubic inch is pushing it. The normal aircraft engine is about 1/2 HP per cubic inch, which I admit is a little conservative but almost 1.5 per cu inch? Not on my airplane. Automotive engines are not designed to put out high HP for long periods of time as are aircraft engines. Dave lm4@juno.com wrote: > --> RV-List message posted by: lm4@juno.com > > Chris, > Subaru has a boxer engine (horizontally opposed) much like > lync. or cont. It's 2.5 liter (2500 cc) will put out 160 to 220 HP > depending on weather it's turbo'd or has a cam grind etc. It also > happens to be liquid cooled, which means far better engine heat > balancing as well as heat in the cabin. You could probably complete > a project such as this for 7 thousand or so. Thats about where the > prices start for a mid time linc., probably without accessories ($$$). > I keep hearing that such a soob can run at cruise on about 8 gal. /Hr > while the comparable lync would use about 10 to 13. Thats part of > the answer. HTH > Larry Mac Donald > Rochester N.Y. > > On Sat, 30 Nov 2002 19:02:09 -0600 Chris <chrisw3@cox.net> writes: > > --> RV-List message posted by: Chris <chrisw3@cox.net> > > > > Ok I know the basics about how engines work and what the difference > > between 2 and 4 stroke, gas and diesel, Fuel injection and > > Carburetors > > but that is about it. Lately there is a lot of talk about > > "alternative" > > engines. One of the things everyone seems to hit on, is that > > traditional aviation engines are an old design and that newer > > engines in > > cars are more "high tech". As I see it most of the high tech with > > the > > ECU and sensors is as much for pollution control as anything else. > > I > > personally couldn't care less about emissions and if those who are > > in > > power really cared, I would be able to fill my car with Propane, > > Natural > > Gas, Methanol, and or Hydrogen at the corner gas station, but back > > to > > the topic. Also there is a lot in car engines to allow them to run > > efficiently at low power settings which we don't really care about > > in > > airplanes. My question is this. Other than Electronic Ignition > > (which > > is easy enough to put on a more traditional aircraft engine) what is > > so > > high tech about car engines that has any application in an airplane? > > > > -- > > Chris Woodhouse > > 3147 SW 127th St. > > Oklahoma City, OK 73170 > > 405-691-5206 (home) > > chrisw@programmer.net > > N35 20.492' > > W97 34.342' > > > > > > > > _-> > > > > > > > > > > > > > > >


    Message 35


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    Time: 05:57:13 PM PST US
    From: Finn Lassen <finnlassen@netzero.net>
    Subject: Re: Alternative Engine Questions
    --> RV-List message posted by: Finn Lassen <finnlassen@netzero.net> I really need to take issue with the "funds" statement. The reason I chose to install a Mazda 13-B rotary in my RV-3 was lack of funds. Sure it took more time and there have been adventures along the way, but I've spent nowhere near what a Lycoming would have cost me. Not to mention what I've saved by running on the cheapest Mo gas available. The gearbox issue is well solved with Tracy's gearbox being available. He also sells a redundant Ignition and Fuel injection controller. There are even people selling engine mounts if you don't care to make/modify your own. Soon intake manifold and throttle body will be available too. This is no longer virgin territory. Finn 304 hours since August 2000. kempthornes wrote: >--> RV-List message posted by: kempthornes <kempthornes@earthlink.net> > >At 04:40 PM 12/1/2002 -0500, you wrote: > > >>--> RV-List message posted by: "Kyle Boatright" <kyle.boatright@adelphia.net> >> >>I've got a buddy who has installed one of the 220 HP Subaru's in his >>Velocity. He's achieved 27 hours and 3 engine related emergency landings >>since his first flight last February. This is an individual who has gone >>the extra step to do things right, and he still doesn't have a satisfactory >>drivetrain. >> >> > >Give him some encouragement, Kyle. You are a buddy. > >There is a story about an engineering manager, at Baldwin Locomotive Works >I think. After a new locomotive was all designed he gathered his engineers >together and said, "Okay, guys, let's build one and see what doesn't work". > >The development of new products involves many corrections along the >way. Guys who do engine conversions right, like your buddy, are bold >adventurers. They have the courage (and funds) the rest of us lack. > >Aren't there builders with a few engine related emergency landings who are >flying Lycomings????? > >K. H. (Hal) Kempthorne >RV6-a N7HK flying! >PRB (El Paso de Robles, CA) > > > >


    Message 36


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    Time: 06:10:57 PM PST US
    From: "Bill VonDane" <n8wv@vondane.com>
    Subject: Re: Data recording
    --> RV-List message posted by: "Bill VonDane" <n8wv@vondane.com> If you use the EIS 4000 for your engine monitoring you can do this... -Bill ----- Original Message ----- From: "Chris" <chrisw3@cox.net> <rv-list@matronics.com>; "vansairforce" <vansairforce@yahoogroups.com> Subject: RV-List: Data recording > --> RV-List message posted by: Chris <chrisw3@cox.net> > > I was thinking it would be nice to be able to record EGT CHT OAT > Altitude, IAS and GPS data on a frequency of a few times a second. I > think this would be a very valuable tool while in the test flight stage > of a new home built plane. Is there a way to do this with say a lap top > and no more than say $2000 for the data acquisition equipment. I know > recording the GPS data wouldn't be that hard with a lap top but what > about all the rest of it? > > -- > Chris Woodhouse > 3147 SW 127th St. > Oklahoma City, OK 73170 > 405-691-5206 (home) > chrisw@programmer.net > N35 20.492' > W97 34.342' > > > ________________________________________________________________________ >


    Message 37


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    Time: 07:50:40 PM PST US
    From: KAKlewin@aol.com
    Subject: More Freebies!!!!
    --> RV-List message posted by: KAKlewin@aol.com Well my wife made me clean the attic...again...doesn't she know that my plane will never get done with all my honey do's!!! uggg...anyway....I found two more Air Force Issue Flight Suits that were issued to me about 5 years ago. Looks to me that I worn them very little (there were a bit short..hence the early retirement) and are in excellent condition. Specifics below: AF Green Nomex Flight Suit Size 40S (40 Short) Should fit height of 5'4" to 5"8", 40in chest All patch velcro sewn on suit (my old Captain rank is still sewn on it, but easily removed) I have two of these...and judging from the last one I put on here you have to be fast to get your hands on one. Im not selling these, but there are yours FREE!! (few things in the RV world are free..and hell its christmas!!!) I am asking for about 10 bucks to cover shipping. To spread the wealth I would like to give to two separate individuals. SO....if your interested...please respond off list.... Kurt Klewin, OKC, OK RV6A Finishing DO NOT ARCHIVE


    Message 38


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    Time: 08:01:40 PM PST US
    From: "Stein Bruch" <stein@steinair.com>
    "Rv-List" <rv-list@matronics.com>
    Subject: RV's, BAD Wind! & Larry Vetterman (Long).
    --> RV-List message posted by: "Stein Bruch" <stein@steinair.com> Hi All, I just arrived home from my Thanksgiving flight to Sturgis-SD from Minneapolis. Instead of a lengthy trip report, I've just got one (OK, 2) interesting items to report on. I left for Sturgis Last Wed (11/27) from Minneapolis at 10:00 am. Weather forecast for Sturgis was partly cloudy with light winds NW@10-15. I headed out under the overcast in Minnesota, found a hole and climbed on top. Perfect sailing until Pierre-SD. I was cruising at 9500', and started to get banged around pretty good, so I slowed down from my 180mph to about 160. It didn't help much. At this point the weather was hazy, but no cloud layer so I headed on towards the Black Hills I now could see in the distance. As the turbulence got worse, I decided to see if I could find a better altitude, all to no avail. I was really getting the crap beat out of me, so the next step was to start trying to find out what the winds were like in Sturgis. I dialed up Rapid City tower and just caught a message from a NWA DC-9 as follows: "RAP Tower, NWAxxx is going around, we had some pretty bad wind shear on final...could you give us an current wind condition report when we turn base again". RAP Tower replied, and reported current winds a few minutes later. "NWAxxx, winds variable 270-330o @35Gusting-42". My heart skipped a beat and my jaw hit my lap! 35-42, could that be right???!?!?! I mean the forecast had said 10-15! I decided to have a short conversation with ATC in RAP to confirm my worst susupicions. They confirmed that winds were terribly gusty and gave me the same report as the NWA folks. I asked if they knew what Sturgis, Spearfish or any of the other Northern Hills were, and they said it's pretty much blowing bad everywhere. I decided to plow on (slowly) to Sturgis. Got to the airport flying sideways, and entered the pattern the best I could. The windsock was straight out stiff, and about 30o off the runway (29). I decided I had to try so I lined up, no flaps, and flew right down to the runway. It wasn't pretty, I've never moved a stick and rudder so violently from stop to stop in my life, but only one small bounce and I was down. Here's the funny thing. My heart was pounding so heard I just stopped as quickly as I could and sat there for a couple of seconds. When I looked outside, I was sitting smack on top of the numbers. I had to wipe the sweat off my palms, and started the 4600' taxi to the ramp. Needless to say, I could raise the tail just sitting still, and the turn off the runway was difficult but doable at crawling speed. I parked on the ramp and couldn't get out of the plane, because the plane wouldn't stay put (no parking-brake), so the line guy put some bricks under the tires to hold the plane still. The G-Meter had +4/-2 on it, and I hadn't done ANY aerobatics - just turbulence. Now, you may think I'm completely crazy, but I filled up with gas and decided to fly over to my dads place (2 minute flight) which was ultimately my final destination. My takeoff roll was only a couple of plane lengths! My dad's runway is the same direction as Sturgis, and actually a bit longer so I headed out. It took 2 tries to put it on the ground there and once again stop-to-stop on the stick/rudder, but all ended up OK with me COMPLETELY WORE OUT. Speaking of my dads place, he just finished the "modification" on the runway, which has resulted in 5,000'x75' of perfectly smooth grass/gravel. It's minutes from Mt.Rushmore and Devils Tower, and right against Bear Butte. We're planning on having a BBQ this summer so keep your eyes open for a good chance for an unofficial fly-in! The runway is so smooth, that during a calm day, even a greenhorn like me could consistently stick some beautiful wheel landings. Overall I'm now even more impressed with these planes than before. I came home today in 2:15 (225-235mph over the ground,) and it was smooth as glass at 10.5K', FYI the trip is 520 miles. I won't voluntarily EVER fly in 35mph winds, but at least I know the plane will do it if it has to. One more thing in this rambling note. While filling up with gas yesterday in Sturgis (I was giving rides like mad), I taxied up to the pump and behold-ANOTHER RV! It was a gorgeous RV4. Right away the guy walked up and started talking to me. He new who I was, but I didn't know him. It was Larry Vetterman, just out goofing around. After I filled up Larry wanted to go over and buzz my dads place again (he hadn't seen the new runway). We got to do some really good formation practice. Just an FYI---His plane is every bit as good looking as his exhausts, the only difference to most, is that he has Vortex Generators. More to come on that later. Well, sorry for the lengthy note. I'm usually one to keep 'em short. This was my first long flight in my newly minted RV6, so I had to brag! For those still building, KEEP IT UP. It's Soooooooo worth it! Happy Flying & Building, Stein Bruch RV6(My crosswind angel)60hrs, Minneapolis Flying like mad!


    Message 39


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    Time: 08:07:16 PM PST US
    From: Jim Oke <wjoke@shaw.ca>
    Subject: Re: Engines
    --> RV-List message posted by: Jim Oke <wjoke@shaw.ca> Cannot but agree that auto and aviation engines are generally designed for somewhat different missions. There are exceptions; consider the engine on a glider towplane compared to that of a long haul 18 wheeler truck and the load cycle that each is exposed to, for instance. However, I think the point could be made that the aviation engine world can perhaps learn a few things from the auto world. (I agree that maybe Lyc. and Cont. are trying and it's just aviation's rules and culture that's holding them back). I'm thinking of stuff like the carefully controlled combustion process that let's some of the smaller compacts wring a lot of power from a small size & weight package while dealing with all sorts of pollution control rules. Think also of the durability of the average auto engine in the face of often abusive handling (cold starts, no warm up, over-reving, etc.) and often casual, minimal, or even nonexistent maintenance. At $20k a pop there is an incentive to look after one's O-320 plus there are few convenient stopping places if it quits at 2,000 ft over a great big forest, but what would the failure rate of an O-320 be if it was treated the same as the stereotypical soccer mom's van? The reason to consider using automotive technology today is to take advantage of the great cost savings implicit in the mass production of the automotive world. There is no free lunch and a good reduction drive will cost some money, but the cost advantage both in initial purchase and later overhaul costs of an auto engine are considerable. There is, of course, a cost versus time tradeoff to make that will be different for different folks. Some missions, such as glider tow plane operators who are fed up with replacing Lyc. cylinders that have been shock cooled too often, can see an operational advantage in water cooling, etc. as well. Jim Oke Winnipeg, MB RV-6A (with a Lyc. - no time to deal with an auto conversion this time around) ----- Original Message ----- From: "Wheeler North" <wnorth@sdccd.cc.ca.us> Subject: RV-List: Engines > --> RV-List message posted by: Wheeler North <wnorth@sdccd.cc.ca.us> > > Well, > > The only real difference between auto vs. aviation engines is their > respective missions. One is designed to accelerate and decelerate a lot, to > not run at full power continously and to deliver reasonable power over its > entire RPM range which can be from 600-6000 RPM commonly, the other is > designed to stay at a constant power/RPM setting, to deliver most of its > power between 2000-2700 RPM, and run at full power until it wears out. > > And finally one is designed to spin a nice round symetrical weight, where > the other is designed to spin a god awful set of paddles that are trying to > rip its face off in five different ways, at all times. ;{) > > So, trying to use one for the other, either way, is kinda silly, expensive > and can be risky if not done correctly, not that there really is a correct > way to do this. (I know I'm gonna get flammed here) > > Its just that it makes no sense to me to redesign something to an > application that no part in it was ever designed for, when there is already > something that is designed for this. (You will not save one dime doing this, > but you might have some fun if you are into that much work.) > > I think we will get a lot further by using our efforts at improving the > thing that was designed for this application, rather than redesigning > something that wasn't meant for this application. > > Which, by the way, is what the engine manufacturers are doing via the > IOF-360 lyc and the IOF-240 Cont. being produced or modified by TCM > Aerosance. TexLyc is also working on their own version of this, but they > both need to get a clue on costs. The TCM FADEC costs as much as the engine > does. I am in the middle of installing one and its a nice product if it runs > well, but damm, the cost is unbelieveable. > > The real issue about these powerplant costs are mass production.... > > So next time you order an aircraft engine, order twenty of them.... ;{) > >


    Message 40


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    Time: 08:21:31 PM PST US
    From: "Jerry" <jdoyal@sport.rr.com>
    Subject: Paint and filling tips
    --> RV-List message posted by: "Jerry" <jdoyal@sport.rr.com> I am building an 8A and I have seen some nice paint jobs; and some not so nice. My question is about filling the tips on the ennpenage. What is a good filler to blend the fiberglass tips into the aluminum? A lot of planes have very obvious cracks in the paint after shrinkage. How do I avoid these? Some planes have very smooth transitions with no sign of these cracks. I can only guess that the preparation and quality of the filler is the reason for the best results. Any recomendations will be appreciated! Thanks, Jerry Doyal jdoyal@sport.rr.com


    Message 41


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    Time: 08:30:58 PM PST US
    From: KAKlewin@aol.com
    Subject: Freebies Gone!!!
    --> RV-List message posted by: KAKlewin@aol.com Thanks to the quick respondents to taking these flight suits off my hands.....if I come across anymore I'll post them to the list.... Cheers.... Kurt Klewin, OKC, OK DO NOT ARCHIVE


    Message 42


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    Time: 09:35:12 PM PST US
    21: 33:01 PST
    From: Reinback <reinback@yahoo.com>
    Subject: Re: Prop
    --> RV-List message posted by: Reinback <reinback@yahoo.com> Dave , Im in the same boat, Ive asked Aerocomposites several times same questions you have specifically weight of the entire propeller and also spinner kit details (is it just raw materials or a finished spinner?) and other detailed questions and have gotten had no response. And I asked for costumers I could speak to, preferably with RVs again no response. Ive asked this information of other propeller companies and I did get answers and customer referrals. I also wanted to ask Aerocomposites why the Lancair Legacy (that they use to quote performance numbers for their 3 blade prop) put the 3 blade Hartzell propeller back on to fly in the Reno race rather than going with the Aerocomposites prop. If the Aerocomposites prop really had the claimed performance increase, wouldnt they have kept it on for the race? Makes a guy wonder ? Roger RV-7 http://mailplus.yahoo.com


    Message 43


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    Time: 09:47:26 PM PST US
    From: Jim Oke <wjoke@shaw.ca>
    Subject: Re: Paint and filling tips
    --> RV-List message posted by: Jim Oke <wjoke@shaw.ca> There are lots of autobody fillers out there to suit different applications. I used some stuff called "Evercoat" in a purple tin that cured very quickly and sanded nicely however it is a bit brittle for some locations where some flex is needed. Epoxy with microballons works not badly in these locations. A visit to your local auto body supply place should fix you up with something suitable. Jim Oke YWG RV-6A ----- Original Message ----- From: "Jerry" <jdoyal@sport.rr.com> Subject: RV-List: Paint and filling tips > --> RV-List message posted by: "Jerry" <jdoyal@sport.rr.com> > > I am building an 8A and I have seen some nice paint jobs; and some not so nice. My question is about filling the tips on the ennpenage. What is a good filler to blend the fiberglass tips into the aluminum? A lot of planes have very obvious cracks in the paint after shrinkage. How do I avoid these? Some planes have very smooth transitions with no sign of these cracks. I can only guess that the preparation and quality of the filler is the reason for the best results. Any recomendations will be appreciated! > > > Thanks, > > Jerry Doyal > > jdoyal@sport.rr.com > >


    Message 44


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    Time: 09:50:11 PM PST US
    21: 48:40 PST
    From: Reinback <reinback@yahoo.com>
    Subject: Re: Prop
    --> RV-List message posted by: Reinback <reinback@yahoo.com> Randy Im interested in the AC prop. You mention several times the AC prop has the best performance. Please help me because I have not seen or heard of a AC prop on an RV as of yet. The only performance numbers I have seen is the 3 blade AC on the Lancair with a Continental 550. Another question I have is you mention AC is using the McCauly 220 hub. The last time a spoke with them they said they where making there own hub and not using the McCauly hub? I am still pondering about 2 vs 3blade props. I had a good buddy some 20yrs ago who had several Cessna 185s some with 2 blade and some with 3 blade props. I asked him what performance difference there was. He said the larger diameter 2-blade prop climbed slightly better but the 3-blade was slightly faster than the 2-blade prop. He also said it took someone with a lot of time in the airplane the really notice any of these differences at all. The only thing I can say for myself after riding in my friends 185s is that the three bladed prop was incredibly smooth and quiet compared to the 2-bladed 185 , it was like a completely different airplane with the 3 blade prop. Roger RV-7 http://mailplus.yahoo.com


    Message 45


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    Time: 10:27:15 PM PST US
    From: Tedd McHenry <tedd@vansairforce.org>
    Subject: Re: Alternative Engine Questions
    --> RV-List message posted by: Tedd McHenry <tedd@vansairforce.org> > Automotive engines are not designed to put out high HP for long periods of > time as are aircraft engines. You should have a look at the endurance tests the auto industry does and compare them to aircraft certification tests. The auto industry tests are much more rigorous. Tedd


    Message 46


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    Time: 10:42:43 PM PST US
    From: "Norman" <nhunger@sprint.ca>
    Subject: Drill Sizes
    --> RV-List message posted by: "Norman" <nhunger@sprint.ca> Can anyone tell me how many thou's a #16 drill is? #11? I'm putting the plastic knob on my canopy latching mechanism. Thanks, Norman Hunger RV6A Delta BC Do not archive


    Message 47


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    Time: 11:12:11 PM PST US
    From: Matt Dralle <dralle@matronics.com>
    Subject: New, NEW List Digest Format...
    --> RV-List message posted by: Matt Dralle <dralle@matronics.com> Dear Listers, Okay, so I woke up this morning to an email box full of hate-mail about the new List Digest format. I thought it was cool, but I guess not... Still, it seemed like too much code to just throw out, so I've modified things a little and I'm hoping everyone will be happy with the new, NEW arrangement. Here's how it works now: o The HTML and TXT enclosures aren't sent in the Digest any longer. o URL Links to the HTML and TEXT versions of the day's Digests will be found at the top of the digest email. o The new Digest Index will be found at the top of the digest email following the URL Links. o The full digest text will then be found in the email as before. o All of the previous Digests will now be available on line. The URL for the main digest page is: http://www.matronics.com/digest From here, you can drill into the specific List Digest of interest. o Both the HTML and TXT versions of the Digests can be found here. o The List Message Trailer will contain a Link directly to the given o Right now there's only one Digest shown, but each day there will be another. They will be sorted with the newest at the top. Left-hand column is the HTML version, right-hand column the TXT version. A couple people also complained that some messages in the HTML version were just one long line that went off to the right forever and they hated that. Come to think of it, this is also an issue in the Search Engine, List Browser, and Archive Browser. Some email programs don't included hard Returns at regular intervals and that's what causes this. I wrote a program tonight that will automatically chop these long lines into 78 characters or less and wrap the rest of the line. After tonight's Archive transfer, all of the Searching and Browsing tools shouldn't have the problem any longer either. Woo hoo! So, back to the new Digest format. What people are going to see in the new, NEW Digest is a bit of verbiage at the top of the email describing the URL links to the HTML and TXT on-line versions, followed by the Links, followed by the day's Index, followed by the day's messages just as before. Lines longer than 78 characters will also be automatically wrapped onto the next line. Hopefully this will be a more pleasing arrangement for everyone. Sorry to get everybody so stirred up over the format change! The List of Contributors is coming out tomorrow night... Still time to make that Contribution! http://www.matronics.com/contribution Best regards, Matt Dralle Email List Admin.


    Message 48


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    Time: 11:42:26 PM PST US
    From: BrownTool@aol.com
    Subject: Re: Drill Sizes
    --> RV-List message posted by: BrownTool@aol.com In a message dated 12/2/2002 12:43:59 AM Central Standard Time, nhunger@sprint.ca writes: > Can anyone tell me how many thou's a #16 drill is? > > #11? > > #16 - .1770 #11 - .1910 Michael Brown Brown Aviation Tool Supply Co.




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