Today's Message Index:
----------------------
 
     1. 09:04 AM - Re: Pietenpol-List Digest: 4 Msgs - 10/07/14 (Bruce Kirk)
     2. 12:12 PM - tossing and turning (Cuy, Michael D. (GRC-LME0)[Vantage Partners, LLC])
     3. 12:32 PM - Re: tossing and turning (curtdm(at)gmail.com)
     4. 02:48 PM - Re: tossing and turning (AircamperN11MS)
 
 
 
Message 1
| 					INDEX |  Back to Main INDEX |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: Pietenpol-List Digest: 4 Msgs - 10/07/14 | 
      
      In response to Bill R about Carlson struts.You mentioned in your post about
       the strength in "SHEAR", should the value used be in tension which is prob
      ably different than shear.Bruce 
      
           On Wednesday, October 8, 2014 12:02 AM, Pietenpol-List Digest Server <
      pietenpol-list@matronics.com> wrote:
         
      
       *
      
       ========================
      
      =C2- Online Versions of Today's List Digest Archive
       ========================
      
      
      Today's complete Pietenpol-List Digest can also be found in either of the
      
      two Web Links listed below.=C2- The .html file includes the Digest format
      ted 
      in HTML for viewing with a web browser and features Hyperlinked Indexes 
      and Message Navigation.=C2- The .txt file includes the plain ASCII versio
      n 
      of the Pietenpol-List Digest and can be viewed with a generic text editor
      
      such as Notepad or with a web browser. 
      
      HTML Version:
      
      =C2- =C2- http://www.matronics.com/digest/digestview.php?Style=82701&
      View=html&Chapter 14-10-07&Archive=Pietenpol
      
      Text Version:
      
      =C2- =C2- http://www.matronics.com/digest/digestview.php?Style=82701&
      View=txt&Chapter 14-10-07&Archive=Pietenpol
      
      
       ========================
      =======================
      =C2- EMail Version of Today's List Digest Archive
       ========================
      =======================
      
      
      =C2- =C2- =C2- =C2- =C2- ----------------------------------------
      ------------------
      =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2
      - =C2- =C2- Pietenpol-List Digest Archive
      =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2
      - =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- ---
      =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- Total
       Messages Posted Tue 10/07/14: 4
      =C2- =C2- =C2- =C2- =C2- ----------------------------------------
      ------------------
      
      
      Today's Message Index:
      ----------------------
      
      =C2- =C2- 1. 04:09 PM - lift struts 2=C2- (Bill R)
      =C2- =C2- 2. 04:51 PM - Re: lift struts 2=C2- (Gary Boothe)
      =C2- =C2- 3. 07:55 PM - Re: Pietenpol-List Digest: 2 Msgs - 10/05/14=C2
      - (Temp623j)
      =C2- =C2- 4. 08:18 PM - Re: lift struts 2=C2- (Clif Dawson)
      
      
      ________________________________=C2- Message 1=C2- ____________________
      _________________
      
      
      Time: 04:09:54 PM PST US
      Subject: Pietenpol-List: lift struts 2
      From: "Bill R" <brcapper@gmail.com>
      
      
      ok, lets go down this road a little further.
      I am still trying to determine if the aluminum lift struts from Carlson A/C
       are
      adequate for a Pietenpol. I know there are=C2- Piets out there flying wit
      h these
      struts,Dan Helspers being one of them. (thanks Dan for your previous=C2- 
      response
      and detailed photos). But I am still looking at the numbers and have come u
      p
      with a very unscientific conclusion. If I built in a big fudge factor by us
      ing
      a gross weight of 1320 lbs. and stressed the airframe to 6 G's. that comes 
      out
      to 7920 lbs. The small lift struts from Carlson has a shear load capacity o
      f
      11,600 lbs. If the load is then divided by 4 (4 struts), it would appear th
      at
      these aluminum struts are easily capable of of handling the job.
      But alas, this is just to simple,I have to be missing something.
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=431626#431626
      
      
      ________________________________=C2- Message 2=C2- ____________________
      _________________
      
      
      Time: 04:51:03 PM PST US
      From: "Gary Boothe" <gboothe5@comcast.net>
      Subject: RE: Pietenpol-List: lift struts 2
      
      
      You are. Cabanes share that load. The picture is even better than you
      compute.
      
      Gary Boothe
      NX308MB
      
      -----Original Message-----
      From: owner-pietenpol-list-server@matronics.com
      [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Bill R
      Sent: Tuesday, October 07, 2014 4:09 PM
      Subject: Pietenpol-List: lift struts 2
      
      
      ok, lets go down this road a little further.
      I am still trying to determine if the aluminum lift struts from Carlson A/C
      are adequate for a Pietenpol. I know there are=C2- Piets out there flying
       with
      these struts,Dan Helspers being one of them. (thanks Dan for your previous
      response and detailed photos). But I am still looking at the numbers and
      have come up with a very unscientific conclusion. If I built in a big fudge
      factor by using a gross weight of 1320 lbs. and stressed the airframe to 6
      G's. that comes out to 7920 lbs. The small lift struts from Carlson has a
      shear load capacity of 11,600 lbs. If the load is then divided by 4 (4
      struts), it would appear that these aluminum struts are easily capable of o
      f
      handling the job.
      But alas, this is just to simple,I have to be missing something.
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=431626#431626
      
      
      ________________________________=C2- Message 3=C2- ____________________
      _________________
      
      
      Time: 07:55:56 PM PST US
      Subject: Pietenpol-List: Re: Pietenpol-List Digest: 2 Msgs - 10/05/14
      From: Temp623j <temp623j@embarqmail.com>
      
      
      > On Oct 6, 2014, at 3:02 AM, Pietenpol-List Digest Server <pietenpol-list@
      matronics.com>
      wrote:
      > 
      > *
      > 
      > ========================
      ========================
      >=C2- Online Versions of Today's List Digest Archive
      > ========================
      ========================
      > 
      > Today's complete Pietenpol-List Digest can also be found in either of the
      
      > two Web Links listed below.=C2- The .html file includes the Digest form
      atted 
      > in HTML for viewing with a web browser and features Hyperlinked Indexes
      
      > and Message Navigation.=C2- The .txt file includes the plain ASCII vers
      ion 
      > of the Pietenpol-List Digest and can be viewed with a generic text editor
      
      > such as Notepad or with a web browser. 
      > 
      > HTML Version:
      > 
      >=C2- =C2- http://www.matronics.com/digest/digestview.php?Style=82701
      &View=html&Chapter 14-10-05&Archive=Pietenpol
      > 
      > Text Version:
      > 
      >=C2- =C2- http://www.matronics.com/digest/digestview.php?Style=82701
      &View=txt&Chapter 14-10-05&Archive=Pietenpol
      > 
      > 
      > ========================
      ======================
      >=C2- EMail Version of Today's List Digest Archive
      > ========================
      ======================
      > 
      > 
      >=C2- =C2- =C2- =C2- =C2- ---------------------------------------
      -------------------
      >=C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2
      - =C2- =C2- Pietenpol-List Digest Archive
      >=C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2
      - =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- ---
      >=C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- Tota
      l Messages Posted Sun 10/05/14: 2
      >=C2- =C2- =C2- =C2- =C2- ---------------------------------------
      -------------------
      > 
      > 
      > Today's Message Index:
      > ----------------------
      > 
      >=C2- =C2- 1. 10:34 AM - Re: riblett 612=C2- (nightmare)
      >=C2- =C2- 2. 06:48 PM - Fw: Nose stand=C2- (Steven Dortch)
      > 
      > 
      > 
      > ________________________________=C2- Message 1=C2- __________________
      ___________________
      > 
      > 
      > Time: 10:34:49 AM PST US
      > Subject: Pietenpol-List: Re: riblett 612
      > From: "nightmare" <pauldonahuepilot@yahoo.com>
      > 
      > 
      > Great info Robert. im building with the 613.5 and making my educated gues
      s on
      equal
      > cabane lengths as well. we'll see...
      > 
      > --------
      > Paul Donahue
      > Started 8-3-12
      > do not archive
      > 
      > 
      > Read this topic online here:
      > 
      > http://forums.matronics.com/viewtopic.php?p=431538#431538
      > 
      > 
      > ________________________________=C2- Message 2=C2- __________________
      ___________________
      > 
      > 
      > Time: 06:48:35 PM PST US
      > Subject: Pietenpol-List: Fwd: Nose stand
      > From: Steven Dortch <steven.d.dortch@gmail.com>
      > 
      > Gentlemen, Here is version 2.0 of my nose cradle. Version 1.0 was just a 
      8
      > inch bench with an old Beech Bonanza seatback and a blanket.
      > 
      > Putting it on wheels makes it mobile and gives me at least a foot more ro
      om
      > for my other plane. Also this clears my cowling and carb.
      > 
      > Made from am $8 (with a coupon) Harbor Freight dolly, scrap 2x6, and scra
      p
      > plywood. the 2X6 is notched to match the prop shape and padded with one
      > layer of sleeping pad (the type you camp out with) and a layer of Pipe
      > insulation, covered with carpet.=C2- The hole in the front is so that I
       can
      > hang it on the prop while I bungee it in. I bungee the cradle onto the pr
      op
      > so that when I lower the nose I don't have to aim for the cradle, It is a
      ll
      > one piece.
      > 
      > When the piet is flying the planes will switch so that I can get the Piet
      > out without having to move the Beech Bonanza in and out, I intend on flyi
      ng
      > the piet a lot more than the Vtail.
      > 
      > Blue Skies,
      > Steve D.
      > 
      > 
      > 
      > 
      > 
      > 
      > 
      > 
      
      
      ________________________________=C2- Message 4=C2- ____________________
      _________________
      
      
      Time: 08:18:36 PM PST US
      From: "Clif Dawson" <cdawson5854@shaw.ca>
      Subject: Re: Pietenpol-List: lift struts 2
      
      
      First off you can't just divide by four. The front strut takes
      the larger part of the load and the rear less of it. I'm not
      sure what the ratio is on the Piet airfoil though. Most
      likely somewhere around a third more.
      Second, the load on the wing is vertical but the tensile stress
      on the strut is not.=C2- The length of the strut is in the
      neighbourhood of double the vertical component. So
      your strut sees double the value of the lift supported
      by that strut. 600lb lifted puts 1200lb tension on the strut.
      third, the cabanes carry a portion of the load but not a lot.
      I figured all this stuff out some time ago and put it in
      some quite intelligent location. Now that my intelligence
      has eroded I can't find it!!
      
      Clif
      When I was younger, I could remember anything,
      whether it happened or not.
      =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2
      - =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- =C2- Mark Twa
      in
      
      ----- Original Message ----- 
      From: "Bill R" <brcapper@gmail.com>
      Sent: Tuesday, October 07, 2014 4:09 PM
      Subject: Pietenpol-List: lift struts 2
      
      
      >
      > ok, lets go down this road a little further.
      > I am still trying to determine if the aluminum lift struts from Carlson
      
      > A/C are adequate for a Pietenpol. I know there are=C2- Piets out there 
      flying 
      > with these struts,Dan Helspers being one of them. (thanks Dan for your 
      > previous=C2- response and detailed photos). But I am still looking at t
      he 
      > numbers and have come up with a very unscientific conclusion. If I built
      
      > in a big fudge factor by using a gross weight of 1320 lbs. and stressed
      
      > the airframe to 6 G's. that comes out to 7920 lbs. The small lift struts
      
      > from Carlson has a shear load capacity of 11,600 lbs. If the load is then
      
      > divided by 4 (4 struts), it would appear that these aluminum struts are
      
      > easily capable of of handling the job.
      > But alas, this is just to simple,I have to be missing something.
      >
      >
      > Read this topic online here:
      >
      > http://forums.matronics.com/viewtopic.php?p=431626#431626
      >
      >
      > -----
      > No virus found in this message.
      > Checked by AVG - www.avg.com
      > 
      
      
      S -
       -
      =C2- =C2- =C2- =C2- =C2- -Matt Dralle, List Admin.
      
      
         
      
Message 2
| 					INDEX |  Back to Main INDEX |  
| 				PREVIOUS |  Skip to PREVIOUS Message |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | tossing and turning | 
      
      Piet group,
      
      Just a few thoughts after a few sleepless nights over decisions I'm making 
      during the early stages of overhauling a spare A-65 that I purchased with n
      o-logs
      in Michigan last month.
      
      Let me begin by saying that I'm not an engine authority of any kind but I d
      id overhaul my own A-65 18 years ago when building my Piet.  (That engine d
      idn't have logs
      either and was sitting in a basement for the 20 years prior to me obtaining
       it but that is superfluous information.)
      
      This is just my story to share with you---I'm not asking for your approval,
       disapproval, applause, or lectures but just sharing.
      
      Back in the early 90's when I overhauled my 1st A-65 Continental I got advi
      ce from two very close friends who were IA's and A&P's who specifically had
       been overhauling
      small Continental engines since the end of WWII.    I sent out the componen
      ts of my engine to the engine overhaul shops that these guys knew well and 
      that they had
      held in high regard.     I didn't skimp on sending these parts out for mach
      ining, inspection, and reconditioning.    I overhauled my A-65 early on in 
      my build so I had the money
      and wasn't pinching pennies yet and did that intentionally since I knew tha
      t engine would be used every summer for many years to come giving rides and
       going on trips to
      Wisconsin.
      
      Whatever parts came back rejected/red tagged I threw in the metal dumpsters
       at work and replaced with new parts from Fresno Air Parts.
      
      By God's grace and doing my homework I was able to fly that old engine for 
      16 years giving lots of rides and having lots of fun flying over lots of fa
      rmland and flying to lots
      of little and big fly-in's around the Midwest and not once did that faithfu
      l engine ever miss a beat.   (okay.....minus the time it quit cold when I t
      axied out with the fuel valve
      in the off position but if you haven't done that then you're my hero.)  At 
      the risk of getting a lecture (or not)  I'll also add that the mags and car
      b were rebuilt by these two seasoned
      IA's for me so I can't take any credit for the reliability that those two q
      uality jobs alone provided in good engine running over the years but certai
      nly a 1st class engine rebuild isn't
      worth a dime if the mags or carb screws up on your first few flights becaus
      e they were not properly overhauled.
      
      I digress.
      
      Some 18 years later I'm rebuilding this little gem and after taking all of 
      my measurements I realize that I can  (if I wanted to) get away with just h
      aving all of the parts magnafluxed
      and if they pass,  put the thing back together again and fly it but somethi
      ng inside won't let me do that.   Why?    Well okay---all the main bearings
       just barely measure up to the Standard
      diameter book values after polishing but not any more than that.    That on
      e up front polished out nicely but I can still see fine lines in the finish
      .   It's only a homebuilt---nothing requires me
      to send this crankshaft out for rework.    I go home thinking of how much m
      oney I'll save by just putting these parts back together again with new sea
      ls, bearing sets, and gaskets.
      
      A little tossing and turning later I thing about it more.     I look over m
      y numbers for my inside diameters where the crankshaft and the camshaft wil
      l ride for the next what, 5, 10, 15, 20 years?
      Nice.....they are standard too but only if I wipe all the gasket sealer fro
      m the engine halves and don't put any string in there.   Hmmm......well alm
      ost standard.  They aren't perfect but heck....this
      is just a homebuilt, you know?
      
      Okay....those cylinders will just clean up well and after lapping in those 
      valve and honing them out I can use them just like I got them once I get th
      em magnafluxed and Zyglo tested and they pass
      right?    Yes sir....I'm going to save a lot of money on this 'just on the 
      edge' overhaul.   This could be a $400 or less major overhaul!   My gosh...
      ..this is too good to be true!    Wow...did I luck out
      with this engine.
      
      Hmmmm........2am, bathroom break.    Can't do it.    Nope.    Can't do it. 
         "that is going to be a LOT of money Mike!!!"     Yep.....I don't like it
       much either.    "you have to crate and box all those
      heavy parts up and ship them to Texas---that is a pain!    Don't waste your
       time doing that......after all, this is only a homebuilt.   You don't have
       to have the parts all yellow tag pretty!  What are you
      thinking?    These are reliable little engines......even guys who put them 
      together half-fast usually get a good little running engine that doesn't mu
      ch know the difference right away or for the first
      year or so, so why fuss over all this?
      
      Tuesday comes and I call Aircraft Engine & Accessory in Dallas.....the plac
      e who reconditioned many of my major parts back in 1994 when I majored the 
      first engine.   "Hello this is Greg speaking."
      "wow.....Greg?    Greg, the same Greg who  I spoke with over the phone a fe
      w times back in the mid 90's who helped process my original A-65 overhaul t
      here in Dallas.....that Greg?     "yes sir.....I've
      been here nearly 30 years now."     I immediately felt a sense of calm and 
      peace run thru my bones talking with Greg and explaining to him what I had 
      to ship down to him.    Last time they took about
      10 days to turn my parts around and they came back like crown jewels out of
       airplane engine wonderland and they purred silky smooth for 16 straight se
      asons of summer fun flying.   "yes sir Greg,
      you can expect my parts down by you sometime late next week via FedEx groun
      d."     "okay Mike,  we'll keep an eye out for them."
      
      "by the way Greg.....do you have anyone you recommend for doing small Conti
      nental crankcase half overhauls??   Divco??"     "well yes sir.....yes sir 
      I do....we like to use Crankcase Services, Inc......here's
      their number, ask for Kevin."     "Excellent----thank you so much.   I'll g
      ive Kevin a call."
      
      "say Greg,  do you have anyone you'd recommend to do cylinder reconditionin
      g??"    "yes sir....we like to use...."     Thanks Greg........
      
      Zzzzzzzz.........zzzzzzzzzz.............zzzzzzzzzz.
      
      Finally I'm going to sleep good again tonight.
      
      Mike C.
      
      
Message 3
| 					INDEX |  Back to Main INDEX |  
| 				PREVIOUS |  Skip to PREVIOUS Message |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: tossing and turning | 
      
      
      Well...could you pass along those numbers for Greg, Kevin, etc...
      
      Thanks Mike!
      
      --------
      Curt Merdan
      Flower Mound, TX
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=431664#431664
      
      
Message 4
| 					INDEX |  Back to Main INDEX |  
| 				PREVIOUS |  Skip to PREVIOUS Message |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: tossing and turning | 
      
      
      Great post Mike,
      
      I haven't slept well this week too.  My problem is only slightly different.  I
      have a friend who has offered me his 4 place 170 MPH home built airplane for a
      very reasonable price. Do I want it? YES. Do I need it?  No. Hmm, That would
      mean two airplanes.  One slow and one to go places in. Guess I'll try to sleep
      on it.  Did I say it was a great buy? Oh yes, I did.  Now what do I do?  
      
      I can't sleep either,
      
      --------
      Scott Liefeld
      Flying N11MS since March 1972
      Steel Tube
      C-85-12
      Wire Wheels
      Brodhead in 1996
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=431667#431667
      
      
 
Other Matronics Email List Services
 
 
These Email List Services are sponsored solely by Matronics and through the generous Contributions of its members.
 
 
-- Please support this service by making your Contribution today! --
  
 |