Pietenpol-List Digest Archive

Sat 08/29/09


Total Messages Posted: 17



Today's Message Index:
----------------------
 
     1. 06:24 AM - Re: Almost time to start covering this thing (Michael Perez)
     2. 06:27 AM - Re: Almost time to start covering this thing (Michael Perez)
     3. 06:40 AM - Re: Re: Almost time to start covering this thing (Michael Perez)
     4. 08:41 AM - A special Pietenpol (Jim Markle)
     5. 08:56 AM - Re: A special Pietenpol (Gary Boothe)
     6. 09:40 AM - Re: Okoume and fuselage gussets (Billy McCaskill)
     7. 12:06 PM - Brodhead Photos (Bill Church)
     8. 01:12 PM - Re: Brodhead Photos (Jack)
     9. 01:38 PM - Re: Brodhead Photos (Cuy, Michael D. (GRC-RXD0)[ASRC Aerospace Corporation])
    10. 02:04 PM - Re: Brodhead Photos (Ross Alexander)
    11. 02:20 PM - Re: Brodhead Photos (Jim)
    12. 06:33 PM - wood struts-test sample (Lawrence Williams)
    13. 07:44 PM - Re: Nicopress tools (shad bell)
    14. 08:20 PM - go/ no go tool--- a must when using Nicopress tools (Cuy, Michael D. (GRC-RXD0)[ASRC Aerospace Corporation])
    15. 08:57 PM - Re: Brodhead Photos (AMsafetyC@aol.com)
    16. 09:09 PM - Re: A special Pietenpol (AMsafetyC@aol.com)
    17. 09:52 PM - Re: wood struts-test sample (Bill Church)
 
 
 


Message 1


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    Time: 06:24:42 AM PST US
    From: Michael Perez <speedbrake@sbcglobal.net>
    Subject: Re: Almost time to start covering this thing
    I can't help you Dan with your fabric question, but what you described is exactly how I plan on doing my covering...same fabric, same brand adhesives, same type paint. I will be very curious to hear how it works out for you. PLEASE keep either the list or me directly posted regularly. Thank you.


    Message 2


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    Time: 06:27:01 AM PST US
    From: Michael Perez <speedbrake@sbcglobal.net>
    Subject: Re: Almost time to start covering this thing
    My apologies, I got my emails all in a bunch it was Rick's email I was referring to about the fabric, paint, etc. (not Dan.)


    Message 3


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    Time: 06:40:51 AM PST US
    From: Michael Perez <speedbrake@sbcglobal.net>
    Subject: Re: Almost time to start covering this thing
    If we are talking off the shelf home type latex, doesn't most places color match? I wonder if you could take a color sample to the store and they run it through the machine...presto! (?)


    Message 4


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    Time: 08:41:40 AM PST US
    From: Jim Markle <jim_markle@mindspring.com>
    Subject: A special Pietenpol
    Occasionally a really special Pietenpol shows up at Brodhead. Actually, I think this year there were several. Well, next year when Dan Helsper shows up with his...take close look. WOW. That will be one of the special ones! Anyway, I got to check it out on my recent visit to his hangar. It was a humbling experience. Dan is what we in the South call "just good people". Thanks for the visit Dan. JM


    Message 5


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    Time: 08:56:22 AM PST US
    From: "Gary Boothe" <gboothe5@comcast.net>
    Subject: A special Pietenpol
    Better check your tool chest, Dan! But that's one beautiful engine... Gary Boothe Cool, Ca. Pietenpol WW Corvair Conversion Tail done, Fuselage on gear (13 ribs down.) -----Original Message----- From: owner-pietenpol-list-server@matronics.com [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Jim Markle Sent: Saturday, August 29, 2009 7:46 AM Subject: Pietenpol-List: A special Pietenpol Occasionally a really special Pietenpol shows up at Brodhead. Actually, I think this year there were several. Well, next year when Dan Helsper shows up with his...take close look. WOW. That will be one of the special ones! Anyway, I got to check it out on my recent visit to his hangar. It was a humbling experience. Dan is what we in the South call "just good people". Thanks for the visit Dan. JM


    Message 6


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    Time: 09:40:23 AM PST US
    Subject: Re: Okoume and fuselage gussets
    From: "Billy McCaskill" <billmz@cox.net>
    The thickness of the gussets in the Flitzer's wings are not what makes it more capable of handling aerobatic stresses, nor is it a comparison of gross weight to wing area. If we were to double the thickness of the gussets in the Piet's wing to 1/8", I still wouldn't be inclined to do any snap maneuvers in a Piet. The shorter wingspan, stiffer spars, and extra bracing in the Flitzer's airframe is what gives it the strength to survive aerobatics. The Flitzer was engineered for a bit more aggressive type of flying. Bernard Pietenpol didn't design his airplane for aerobatics, but for simple flying pleasure out of his small pasture airport. This isn't really a comparison of apples to oranges but more like a comparison of apples to eggs... Billy McCaskill Urbana, IL Baker, LA tail feathers nearly done Read this topic online here: http://forums.matronics.com/viewtopic.php?p=260374#260374


    Message 7


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    Time: 12:06:41 PM PST US
    Subject: Brodhead Photos
    From: "Bill Church" <billspiet@sympatico.ca>
    Well, I finally got around to downloading some of the pictures I took at Brodhead this year! They can be found here: http://www.mykitplane.com/Planes/photoGalleryList2.cfm?AlbumID=344 Bill C. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=260384#260384


    Message 8


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    Time: 01:12:23 PM PST US
    From: "Jack" <jack@textors.com>
    Subject: Brodhead Photos
    Great pics, thanks Bill! Jack www.textors.com do not archive


    Message 9


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    Time: 01:38:28 PM PST US
    From: "Cuy, Michael D. (GRC-RXD0)[ASRC Aerospace Corporation]" <michael.d.cuy@nasa.gov>
    Subject: Brodhead Photos
    EXCELLENT photos Bill ! Thank you for sharing them. Mike C. do not archive


    Message 10


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    Time: 02:04:29 PM PST US
    From: Ross Alexander <karbath1@yahoo.ca>
    Subject: Re: Brodhead Photos
    Hey Bill! Those were great pic's of the Piet gathering in Brodhead. What a variety! I am getting time on mine everyday the sun shines! How sweet it is! Ross Alexander=0A=0A=0A=0A=0A________________________________=0AFrom : Bill Church <billspiet@sympatico.ca>=0ATo: pietenpol-list@matronics.com =0ASent: Saturday, August 29, 2009 3:05:53 PM=0ASubject: Pietenpol-List: Br lspiet@sympatico.ca>=0A=0AWell, I finally got around to downloading some of the pictures I took at Brodhead this year!=0AThey can be found here:=0A=0A http://www.mykitplane.com/Planes/photoGalleryList2.cfm?AlbumID=344=0A=0AB ill C.=0A=0A=0A=0A=0ARead this topic online here:=0A=0Ahttp://forums.matron ===============0A=0A=0A __________________ ________________________________________________=0AThe new Internet Explore r=AE 8 - Faster, safer, easier. Optimized for Yahoo! Get it Now for Free! at http://downloads.yahoo.com/ca/internetexplorer/


    Message 11


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    Time: 02:20:27 PM PST US
    From: Jim <jimboyer@hughes.net>
    Subject: Re: Brodhead Photos
    Jim Boyer Santa Rosa, CA Pietenpol builder with Corvair Bill, Very good pictures of the Brodhead flyin. Thanks for posting them, I looked forward to your pictures after seeing how good they were last year. Jim On Aug 29, 2009, Bill Church <billspiet@sympatico.ca> wrote: Well, I finally got around to downloading some of the pictures I took at Brodhead this year! They can be found here: http://www.mykitplane.com/Planes/photoGalleryList2.cfm?AlbumID=344 Bill C. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=260384#260384


    Message 12


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    Time: 06:33:29 PM PST US
    From: Lawrence Williams <lnawms@yahoo.com>
    Subject: wood struts-test sample
    Remember that the struts take the compression loads when landing or at rest and the cables take the lifting loads while flying. Big Jim Vandervoort il lustrated it by saying that you could saw the struts off in flight and noth ing would change. So, instead of a "pull" test for your laminated struts, y ou should probably be more concerned with the compression loading. - Larry=0A=0A=0A


    Message 13


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    Time: 07:44:11 PM PST US
    From: shad bell <aviatorbell@yahoo.com>
    Subject: Re: Nicopress tools
    I believe the nicopress tool dad bought is from cleveland telephone Co.- As long as the tool has a go/no go gauge use it.- The nicco press was des igned 1st for the pole line industry.- If you have any questions about th e integrity I will happily do some destructive testing, tractor pull style. - I think I have some shrubs to pull out any how, and the old Allis Chalm ers needs a work out. - Shad=0A=0A=0A


    Message 14


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    Time: 08:20:36 PM PST US
    From: "Cuy, Michael D. (GRC-RXD0)[ASRC Aerospace Corporation]" <michael.d.cuy@nasa.gov>
    Subject: go/ no go tool--- a must when using Nicopress tools
    Shad is right-- there is a slotted flat plate of steel with 'stepped' U chaped spaces machined into it where you slip the appropriate U slot over your completed nicopress sleeve to see if it slips in with no problems--if it doesn't slip in you have not gotten a good tight nicopress and the assembly should be trashed and made over. There are adjustments on the nicopress pliers so you can tighten the jaws a bit to make good, sound, nicopress presses if you're not getting 'passing' nico squeezes. Mike C. PS-- my tool from whomever I bought it from came with the go/ no go gauge and I use it on every single nicopress junction I make--take all of 2 seconds to see if you've got a good press or not.


    Message 15


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    Time: 08:57:27 PM PST US
    From: AMsafetyC@aol.com
    Subject: Re: Brodhead Photos
    Nice job Bill thanks for the pics John In a message dated 8/29/2009 3:06:59 P.M. Eastern Daylight Time, billspiet@sympatico.ca writes: --> Pietenpol-List message posted by: "Bill Church" <billspiet@sympatico.ca> Well, I finally got around to downloading some of the pictures I took at Brodhead this year! They can be found here: http://www.mykitplane.com/Planes/photoGalleryList2.cfm?AlbumID=344 Bill C. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=260384#260384


    Message 16


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    Time: 09:09:13 PM PST US
    From: AMsafetyC@aol.com
    Subject: Re: A special Pietenpol
    Did I notice some parts missing for that beautiful Model A engine? Markle strikes again Jim nice pic. Dan great looking work John In a message dated 8/29/2009 11:42:28 A.M. Eastern Daylight Time, jim_markle@mindspring.com writes: Occasionally a really special Pietenpol shows up at Brodhead. Actually, I think this year there were several. Well, next year when Dan Helsper shows up with his...take close look. WOW. That will be one of the special ones! Anyway, I got to check it out on my recent visit to his hangar. It was a humbling experience. Dan is what we in the South call "just good people". Thanks for the visit Dan. JM


    Message 17


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    Time: 09:52:29 PM PST US
    Subject: wood struts-test sample
    From: "Bill Church" <eng@canadianrogers.com>
    Well, that's not completely true Larry. The first part is correct. When the Piet is at rest (on it's wheels) the weight of the wings is supported entirely by the lift struts - in compression. Same goes for when touching down on landing. Cables are useless in compression - you can't push a rope. Now, when flying, all (at least 90%, anyway) of the lifting load is being borne by the lift strut attachment fittings on the bottom of the wings. Attached to those fittings are the lift struts. And attached to the lift struts are the flying wires. The primary purpose of the flying wires is to brace the lift struts - to prevent them from swaying fore or aft. If they were intended to carry the lifting load, they would be in-line with the lift struts, not arranged diagonally as they are. The lift struts are designed to carry the lifting loads. Having said that ... doubtlessly, some of the lifting load does get transferred to these cables when in flight. And if, for some odd reason, one ended up having one's lift struts sawed off in flight, the plane could probably manage to keep flying (as long as no sudden movements were made, or turbulence was encountered. Upon landing, the wings would of course, collapse, since someone sawed off the struts. So, I think the most important function that the lift struts serve is carrying the lifting load - in tension. And the second-most important function they serve is holding the wings up on the ground (in compression). The tension loads are considerably higher than the compression loads. In the archives, maybe a year or so ago, Jack Phillips did a quick calculation of the design loads for the lift struts (which if I remember correctly was about 4000 pounds for the front struts). 1/8" Aircraft cable is rated for around 2000 pounds. So, if a fabricated strut assembly can withstand a 4000 pound tension test, it's probably up for the task. Bill C. -----Original Message----- From: owner-pietenpol-list-server@matronics.com on behalf of Lawrence Williams Sent: Sat 29/08/2009 9:26 PM Subject: Pietenpol-List: wood struts-test sample Remember that the struts take the compression loads when landing or at rest and the cables take the lifting loads while flying. Big Jim Vandervoort illustrated it by saying that you could saw the struts off in flight and nothing would change. So, instead of a "pull" test for your laminated struts, you should probably be more concerned with the compression loading. - Larry




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