Today's Message Index:
----------------------
 
     1. 01:17 AM - Was I bad? (Stephen!)
     2. 06:31 AM - Re: Landing gear setup (Rick Holland)
     3. 08:52 AM - Re: Was I bad? (Dick Navratil)
     4. 10:33 AM - Re: Was I bad? (Isablcorky@aol.com)
     5. 12:57 PM - Re: Landing gear setup (GCARDINAL@mn.rr.com)
     6. 04:25 PM - Spar Size analysis? (Jake Crause)
     7. 06:21 PM - Wire wheel info from Brodhead (Jim Markle)
     8. 10:40 PM - Re: Spar Size analysis? (Gene Hubbard)
 
 
 
Message 1
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      --> Pietenpol-List message posted by: "Stephen!" <pietenpol@imagesdesavions.com>
      
      
         Was I a bad boy and cut off from the list?
      
      
      -- 
      IBA# 11465
      http://imagesdesavions.com
      
      
Message 2
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| Subject:  | Re: Landing gear setup | 
      
      Greg
      
      Two questions: Is your firewall position to the plans? (12" forward of the
      front ash cross strut). How many inches did you have to move your wing back
      to make CG (if any)?
      
      Thanks
      
      Rick H
      
      On 7/24/05, gcardinal@mn.rr.com <gcardinal@mn.rr.com> wrote:
      >
      > Long fuselage (per Don P.'s supplemental plans), A-65 engine, axle located
      > 20" aft of the firewall has resulted in
      > very good ground handling.
      > With the plane level there is 15# on the skid.
      > With a 220+ lb pilot the plane is quite maneuverable on the ground (no
      > brakes, tailskid equipped)
      > 
      
      
      --
      Rick Holland
      
Message 3
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  | 
      
      
      
      --> Pietenpol-List message posted by: "Dick Navratil" <horzpool@goldengate.net>
      
      After Broadhead everybody may be going thru a period of quiet relection or 
      rapid gluing and sanding.
      Dick N.
      
      do not archive
      ----- Original Message ----- 
      From: "Stephen!" <pietenpol@imagesdesavions.com>
      Subject: Pietenpol-List: Was I bad?
      
      
      > --> Pietenpol-List message posted by: "Stephen!" 
      > <pietenpol@imagesdesavions.com>
      >
      >
      >   Was I a bad boy and cut off from the list?
      >
      >
      > -- 
      > IBA# 11465
      > http://imagesdesavions.com
      >
      >
      > 
      
      
Message 4
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  | 
      
      
      
      After reading all the glowing reports of Brodhead 05 I have been trying  hard 
      to work under an outside shed on my fuse but this La heat is tough on an  ole 
      man so have decided to cover the fuse with a tarp and go into the a/c  shop 
      and begin the wings. By the time they are completed it should be a bit  cooler.
      
      I want to be one of those who fly into Brodhead 06, God willing.  Promised 
      Chuck Gantzer he could have a portion of my stand-up tent since his is  too long
      
      for his Wal-Mart shelter
      CMC in La
      
Message 5
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  | 
      
      
| Subject:  | Re: Landing gear setup | 
      
      --> Pietenpol-List message posted by: GCARDINAL@mn.rr.com
      
      Rick,
      The fuselage is built to the supplemental (Corvair) plans. I will 
      verify the dimension this weekend.
      The wing is moved back 3 1/2 inches and we are flying close to the aft 
      cg limit. 
      
      Greg Cardinal
      
      ----- Original Message -----
      From: Rick Holland <at7000ft@gmail.com>
      Subject: Re: Pietenpol-List: Landing gear setup
      
      > Greg
      > 
      > Two questions: Is your firewall position to the plans? (12" 
      > forward of the 
      > front ash cross strut). How many inches did you have to move your 
      > wing back 
      > to make CG (if any)?
      > 
      > Thanks
      > 
      > Rick H
      > 
      > On 7/24/05, gcardinal@mn.rr.com <gcardinal@mn.rr.com> wrote:
      > > 
      > > Long fuselage (per Don P.'s supplemental plans), A-65 engine, 
      > axle located 
      > > 20" aft of the firewall has resulted in
      > > very good ground handling.
      > > With the plane level there is 15# on the skid.
      > > With a 220+ lb pilot the plane is quite maneuverable on the 
      > ground (no 
      > > brakes, tailskid equipped)
      > >  
      > 
      > 
      > 
      > -- 
      > Rick Holland
      > 
      
      
Message 6
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  | 
      
      
| Subject:  | Spar Size analysis? | 
      
      --> Pietenpol-List message posted by: "Jake Crause" <admin@homebuiltairplanes.com>
      
      Greetings,
      
      I've been able to find some references in the archives about the 3/4"
      spar being OK.  My question is how was that conclusion reached?  Can't
      seem to find that part in the archives.  I do not doubt that it is OK,
      but I was hoping to have some facts to back up my choice for the smaller
      spar.  Was there an analysis done?
      
      Does anyone have a weight comparison between the 1" routed spar and a
      solid 3/4". 
      
      Jake Crause
      www.homebuiltairplanes.com
      
      P.S.  Got my Table DONE - Working on the Rib Jig!!
      
      
Message 7
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  | 
      
      
| Subject:  | Wire wheel info from Brodhead | 
      
      --> Pietenpol-List message posted by: Jim Markle <jim_markle@mindspring.com>
      
      
      Several people asked about where to order the hub/rim/spokes/tires/tubes like the
      21" wheel I took to Brodhead.
      
      I scanned all the invoices and copied them to the files section of mykitplane.com...
      
      Keep in mind that the invoices are for 2 sets so watch the quantities......I think
      the tires/tubes were for one set but just watch the quantities closely....
      
      They can be found here:
      
      <http://www.mykitplane.com/Planes/filesList2.cfm?AlbumID=67>
      
      Jim
      
      
Message 8
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  | 
      
      
| Subject:  | Re: Spar Size analysis? | 
      
      --> Pietenpol-List message posted by: Gene Hubbard <enhubbard@sbcglobal.net>
      
      Jake,
      
      Page 64 of the manual (note 10) says that Pietenpol himself used spars 
      laminated out of 3/4" square material for his later aircraft.
      
      The engineering that would go into it would be to calculate the moment 
      of inertia for the two cross-sections.  Units come out as inches to the 
      fourth power.  The higher the moment of inertia, the better.
      
      I started covering my Piet this week--tail and one aileron have 
      Polyfiber on them now, and wings are off.
      
      Gene Hubbard
      San Diego
      
      Jake Crause wrote:
      
      >--> Pietenpol-List message posted by: "Jake Crause" <admin@homebuiltairplanes.com>
      >
      >Greetings,
      >
      >I've been able to find some references in the archives about the 3/4"
      >spar being OK.  My question is how was that conclusion reached?  Can't
      >seem to find that part in the archives.  I do not doubt that it is OK,
      >but I was hoping to have some facts to back up my choice for the smaller
      >spar.  Was there an analysis done?
      >
      >Does anyone have a weight comparison between the 1" routed spar and a
      >solid 3/4". 
      >
      >Jake Crause
      >www.homebuiltairplanes.com
      >
      >P.S.  Got my Table DONE - Working on the Rib Jig!!
      >
      >
      > 
      > 
      > 
      >
      >
      >  
      >
      
      
 
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