Today's Message Index:
----------------------
 
     1. 06:56 AM - Rib to spar attachment.  (Comcast)
     2. 07:10 AM - Re: Rib to spar attachment.  (Jack Textor)
     3. 07:12 AM - Re: Rib to spar attachment.  (Jack Philips)
     4. 07:18 AM - Re: Rib to spar attachment.  (Glen Schweizer)
     5. 07:20 AM - Re: Rib to spar attachment.  (Jack Textor)
     6. 07:22 AM - Re: Rib to spar attachment.  (Jack Philips)
     7. 08:12 AM - Re: Rib to spar attachment.  (John C Black)
     8. 08:59 AM - Re: Rib to spar attachment.  (Jack Philips)
     9. 09:02 AM - Re: Rib to spar attachment.  (Jack Textor)
    10. 09:20 AM - Re: Rib to spar attachment. (jarheadpilot82)
    11. 11:03 AM - Re: Rib to spar attachment.  (John C Black)
    12. 09:26 PM - Re: Rib to spar attachment. (taildrags)
 
 
 
Message 1
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  | 
      
      
| Subject:  | Rib to spar attachment.  | 
      
      In reviewing drawing 5 for steel materials needed, it shows 2 nails at top a
      nd bottom securing to the spar. 
      
      Is this what you guys do/did?
      
      This is just enough to hold general position. 
      
      
      - Rich
      
Message 2
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  | 
      
      
| Subject:  | Re: Rib to spar attachment.  | 
      
      
      Most dont do it this way. Many dont secure at all. I tacked through the vertical
      brace into the side of the spar 
      
      Jack Textor
      
      Sent from my iPad
      
      > On Jan 2, 2018, at 8:55 AM, Comcast <4rcsimmons@comcast.net> wrote:
      > 
      > In reviewing drawing 5 for steel materials needed, it shows 2 nails at top and
      bottom securing to the spar. 
      > 
      > Is this what you guys do/did?
      > 
      > This is just enough to hold general position. 
      > 
      > <image1.jpeg>
      > 
      > 
      > 
      > - Rich
      
      
Message 3
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  | 
      
      
| Subject:  | Rib to spar attachment.  | 
      
      
      That's all you will need, and I wouldn't do it until you have your wing
      trammeled and the drag and anti drag wires tight.  You might need to move a
      rib or two to clear the bracing wires on the rib diagonals.  Once the fabric
      is in place and the rib lacing is done, the ribs are very secure.
      
      Jack Phillips
      Pietenpol NX899JP "Icarus Plummet", flying for 13 years
      RV-10 N142KW, under construction, hopefully flying this year
      
      
      -----Original Message-----
      From: owner-pietenpol-list-server@matronics.com
      [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Comcast
      Sent: Tuesday, January 2, 2018 9:56 AM
      Subject: Pietenpol-List: Rib to spar attachment. 
      
      In reviewing drawing 5 for steel materials needed, it shows 2 nails at top
      and bottom securing to the spar. 
      
      Is this what you guys do/did?
      
      This is just enough to hold general position. 
      
      
Message 4
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  | 
      
      
| Subject:  | Re: Rib to spar attachment.  | 
      
      
      All the nails do is maintain position while glue cures
      > On Jan 2, 2018, at 6:55 AM, Comcast <4rcsimmons@comcast.net> wrote:
      > 
      > In reviewing drawing 5 for steel materials needed, it shows 2 nails at top and
      bottom securing to the spar. 
      > 
      > Is this what you guys do/did?
      > 
      > This is just enough to hold general position. 
      > 
      > <image1.jpeg>
      > 
      > 
      > 
      > - Rich
      
      
Message 5
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  | 
      
      
| Subject:  | Re: Rib to spar attachment.  | 
      
      
      Good point JP, I had to move or modify a couple of ribs to clear the cables...
      
      Jack Textor
      
      Sent from my iPad
      
      > On Jan 2, 2018, at 9:12 AM, Jack Philips <jack@bedfordlandings.com> wrote:
      > 
      > 
      > That's all you will need, and I wouldn't do it until you have your wing
      > trammeled and the drag and anti drag wires tight.  You might need to move a
      > rib or two to clear the bracing wires on the rib diagonals.  Once the fabric
      > is in place and the rib lacing is done, the ribs are very secure.
      > 
      > Jack Phillips
      > Pietenpol NX899JP "Icarus Plummet", flying for 13 years
      > RV-10 N142KW, under construction, hopefully flying this year
      > 
      > 
      > -----Original Message-----
      > From: owner-pietenpol-list-server@matronics.com
      > [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Comcast
      > Sent: Tuesday, January 2, 2018 9:56 AM
      > To: pietenpol-list@matronics.com
      > Subject: Pietenpol-List: Rib to spar attachment. 
      > 
      > In reviewing drawing 5 for steel materials needed, it shows 2 nails at top
      > and bottom securing to the spar. 
      > 
      > Is this what you guys do/did?
      > 
      > This is just enough to hold general position. 
      > 
      > 
      > 
      > 
      > 
      
      
Message 6
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  | 
      
      
| Subject:  | Rib to spar attachment.  | 
      
      
      Glue is not necessary, and might be detrimental if you ever need to replace
      a rib.  I did not glue my ribs in place.  
      
      Jack Phillips
      NX899JP "Icarus Plummet"
      Smith Mountain Lake, Virginia
      
      -----Original Message-----
      From: owner-pietenpol-list-server@matronics.com
      [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Glen
      Schweizer
      Sent: Tuesday, January 2, 2018 10:18 AM
      Subject: Re: Pietenpol-List: Rib to spar attachment. 
      
      --> <glenschweizer@yahoo.com>
      
      All the nails do is maintain position while glue cures
      > On Jan 2, 2018, at 6:55 AM, Comcast <4rcsimmons@comcast.net> wrote:
      > 
      > In reviewing drawing 5 for steel materials needed, it shows 2 nails at top
      and bottom securing to the spar. 
      > 
      > Is this what you guys do/did?
      > 
      > This is just enough to hold general position. 
      > 
      > <image1.jpeg>
      > 
      > 
      > 
      > - Rich
      
      
Message 7
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  | 
      
      
| Subject:  | Re: Rib to spar attachment.  | 
      
      I would appreciate any comments on my plan for assembling the ribs and 
      spars.   
      
      I am using Aluminum Spars from Carlson Aircraft.   My plan is to make a 
      filler for the side of the spar facing the rib. a 1/2=9D 
      wide (maybe 1=9D wide) x 3/8=9D thick piece of spruce to 
      fill the ~4.25=9D space between the bottom & top rails 
      relieved for the top channel and bulbs on the spar. (See picture) To 
      assemble I would slide the filler into place.  I want to make sure the 
      rib stays square to the spar.  I want to experiment to determine whether 
      to epoxy the rib to the filler.  If the rib stays square when epoxied to 
      the filler and the  rib/filler can be slid along the spar in case it 
      needs to move for diagonal wires then I=99d use a single 
      screw/nut in the center of the spar to hold the rib in location.  If 
      this approach had problems, then use no epoxy between rib and filler and 
      use 2 #8 screws with nuts to hold the filler and rib to the spar... 
      drilling 2 holes for screws 1.5=9D apart (1.5=9D from the 
      top & bottom of spar).
      
      I have some small concern about drilling the spar, but the center of the 
      web is doing little work so I think that would be acceptable.
      
      Since I=99ve never done this before, any help is appreciated.
      
      Thanks,
      
      John
      La Conner, WA
      
      On Jan 2, 2018, at 7:22 AM, Jack Philips <jack@bedfordlandings.com> 
      wrote:
      
      <jack@bedfordlandings.com>
      
      Glue is not necessary, and might be detrimental if you ever need to 
      replace
      a rib.  I did not glue my ribs in place.  
      
      Jack Phillips
      NX899JP "Icarus Plummet"
      Smith Mountain Lake, Virginia
      
      -----Original Message-----
      From: owner-pietenpol-list-server@matronics.com
      [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Glen
      Schweizer
      Sent: Tuesday, January 2, 2018 10:18 AM
      Subject: Re: Pietenpol-List: Rib to spar attachment. 
      
      --> <glenschweizer@yahoo.com>
      
      All the nails do is maintain position while glue cures
      > On Jan 2, 2018, at 6:55 AM, Comcast <4rcsimmons@comcast.net> wrote:
      > 
      > In reviewing drawing 5 for steel materials needed, it shows 2 nails at 
      top
      and bottom securing to the spar. 
      > 
      > Is this what you guys do/did?
      > 
      > This is just enough to hold general position. 
      > 
      > <image1.jpeg>
      > 
      > 
      > 
      > - Rich
      
      
Message 8
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  | 
      
      
| Subject:  | Rib to spar attachment.  | 
      
      I=99m just curious, not judgmental, but why do you want to use 
      aluminum spars?  It would seem that a great deal of extra work would be 
      involved, they would be heavier (by the time you add all the wood 
      fillers) and I=99m not sure without running a stress analysis that 
      they would be any stronger than wood spars.  Are they cheaper?
      
      
      Jack Phillips
      
      NX899JP =9CIcarus Plummet=9D
      
      Smith Mountain Lake, Virginia
      
      
      From: owner-pietenpol-list-server@matronics.com 
      [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of John C 
      Black
      Sent: Tuesday, January 2, 2018 11:12 AM
      Subject: Re: Pietenpol-List: Rib to spar attachment. 
      
      
      I would appreciate any comments on my plan for assembling the ribs and 
      spars.   
      
      
      I am using Aluminum Spars from Carlson Aircraft.   My plan is to make a 
      filler for the side of the spar facing the rib. a 1/2=9D 
      wide (maybe 1=9D wide) x 3/8=9D thick piece of spruce to 
      fill the ~4.25=9D space between the bottom & top rails 
      relieved for the top channel and bulbs on the spar. (See picture) To 
      assemble I would slide the filler into place.  I want to make sure the 
      rib stays square to the spar.  I want to experiment to determine whether 
      to epoxy the rib to the filler.  If the rib stays square when epoxied to 
      the filler and the  rib/filler can be slid along the spar in case it 
      needs to move for diagonal wires then I=99d use a single 
      screw/nut in the center of the spar to hold the rib in location.  If 
      this approach had problems, then use no epoxy between rib and filler and 
      use 2 #8 screws with nuts to hold the filler and rib to the spar... 
      drilling 2 holes for screws 1.5=9D apart (1.5=9D from the 
      top & bottom of spar).
      
      
      I have some small concern about drilling the spar, but the center of the 
      web is doing little work so I think that would be acceptable.
      
      
      Since I=99ve never done this before, any help is appreciated.
      
      
      Thanks,
      
      
      John
      
      La Conner, WA
      
      
      On Jan 2, 2018, at 7:22 AM, Jack Philips <jack@bedfordlandings.com 
      <mailto:jack@bedfordlandings.com> > wrote:
      
      
      <jack@bedfordlandings.com <mailto:jack@bedfordlandings.com> >
      
      Glue is not necessary, and might be detrimental if you ever need to 
      replace
      a rib.  I did not glue my ribs in place.  
      
      Jack Phillips
      NX899JP "Icarus Plummet"
      Smith Mountain Lake, Virginia
      
      -----Original Message-----
      From: owner-pietenpol-list-server@matronics.com 
      <mailto:owner-pietenpol-list-server@matronics.com> 
      [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Glen
      Schweizer
      Sent: Tuesday, January 2, 2018 10:18 AM
      Subject: Re: Pietenpol-List: Rib to spar attachment. 
      
      --> <glenschweizer@yahoo.com <mailto:glenschweizer@yahoo.com> >
      
      All the nails do is maintain position while glue cures
      
      
      On Jan 2, 2018, at 6:55 AM, Comcast <4rcsimmons@comcast.net 
      <mailto:4rcsimmons@comcast.net> > wrote:
      
      In reviewing drawing 5 for steel materials needed, it shows 2 nails at 
      top
      
      and bottom securing to the spar. 
      
      
      Is this what you guys do/did?
      
      This is just enough to hold general position. 
      
      <image1.jpeg>
      
      
      - Rich
      
      
      http://www.matronics.com/Navigator?Pietenpol-List
      http://wiki.matronics.com
      http://www.matronics.com/contribution
      
      
Message 9
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  | 
      
      
| Subject:  | Re: Rib to spar attachment.  | 
      
      Uncharted territory there John. Was your reason for aluminum weight savings?
       Do you know how it=99s strength compare to plans spar? Using it will m
      ean changes in many areas for things attached to the spar.
      
      Jack Textor
      
      Sent from my iPad
      
      > On Jan 2, 2018, at 10:11 AM, John C Black <john@jcblack.com> wrote:
      > 
      > I would appreciate any comments on my plan for assembling the ribs and spa
      rs.   
      > 
      > I am using Aluminum Spars from Carlson Aircraft.   My plan is to make a fi
      ller for the side of the spar facing the rib. a 1/2=9D wide (
      maybe 1=9D wide) x 3/8=9D thick piece of spruce to fill the ~4.2
      5=9D space between the bottom & top rails relieved for the to
      p channel and bulbs on the spar. (See picture) To assemble I would slide the
       filler into place.  I want to make sure the rib stays square to the spar.  I
       want to experiment to determine whether to epoxy the rib to the filler.  If
       the rib stays square when epoxied to the filler and the  rib/filler can be s
      lid along the spar in case it needs to move for diagonal wires then
       I=99d use a single screw/nut in the center of the spar to hold the ri
      b in location.  If this approach had problems, then use no epoxy between rib
       and filler and use 2 #8 screws with nuts to hold the filler and rib to the s
      par... drilling 2 holes for screws 1.5=9D apart (1.5=9D from the
       top & bottom of spar).
      > 
      > I have some small concern about drilling the spar, but the center of the w
      eb is doing little work so I think that would be acceptable.
      > 
      > Since I=99ve never done this before, any help is appreciated.
      > 
      > Thanks,
      > 
      > John
      > La Conner, WA
      > <000-Spar.JPG>
      > On Jan 2, 2018, at 7:22 AM, Jack Philips <jack@bedfordlandings.com> wrote:
      
      > 
      .com>
      > 
      > Glue is not necessary, and might be detrimental if you ever need to replac
      e
      > a rib.  I did not glue my ribs in place.  
      > 
      > Jack Phillips
      > NX899JP "Icarus Plummet"
      > Smith Mountain Lake, Virginia
      > 
      > -----Original Message-----
      > From: owner-pietenpol-list-server@matronics.com
      > [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of Glen
      > Schweizer
      > Sent: Tuesday, January 2, 2018 10:18 AM
      > To: pietenpol-list@matronics.com
      > Subject: Re: Pietenpol-List: Rib to spar attachment. 
      > 
      > --> <glenschweizer@yahoo.com>
      > 
      > All the nails do is maintain position while glue cures
      >> On Jan 2, 2018, at 6:55 AM, Comcast <4rcsimmons@comcast.net> wrote:
      >> 
      >> In reviewing drawing 5 for steel materials needed, it shows 2 nails at to
      p
      > and bottom securing to the spar. 
      >> 
      >> Is this what you guys do/did?
      >> 
      >> This is just enough to hold general position. 
      >> 
      >> <image1.jpeg>
      >> 
      >> 
      >> 
      >> - Rich
      > 
      > 
      > 
      > 
      > 
      > 
      > http://www.matronics.com/Navigator?Pietenpol-List
      > http://wiki.matronics.com
      > http://www.matronics.com/contribution
      > 
      > 
      > 
      > 
      
Message 10
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  | 
      
      
| Subject:  | Re: Rib to spar attachment. | 
      
      
      John,
      
      I am also using the aluminum extruded spars. I did the spacers pretty much as you
      described and epoxied them to the spar, clamping them until the epoxy dried.
      I trammeled my wings, then set the ribs where I wanted them. I  wanted the ribs
      to be equally spaced, and to do so, I had to dremel out a slot/space in one
      or two diagonals. After the diagonals were slotted, I added additional diagonals
      behind the slotted ones to reinforce them. I then epoxied them into place.
      I wanted to  ensure a transfer of the aerodynamic loads between the ribs and
      the spars and was advised to glue them in place. I used a pin nailer to nail
      the ribs in place until they dried.
      
      Two things I would suggest, First, ensure your spacers are wide enough (mine were
      about 1 and 1/2 inches wide) so you can move the ribs off the center of the
      spacer if you need to and choose to move the ribs to clear the drag/anti-drag
      wires. Second, if you choose to screw the ribs into place, I think that one screw
      in the center of the shear web would be best, the loads are lowest at the
      center of the shear web, and using the smallest screw possible should not affect
      the spar strength.
      
      My $.02. Keep us posted.
      
      --------
      Semper Fi,
      
      Terry Hand
      Athens, GA
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=477011#477011
      
      
Message 11
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  | 
      
      
| Subject:  | Re: Rib to spar attachment.  | 
      
      Using 14=99 lengths for comparison.
      
      Carlson Spars (4-A) are $103 per 14=99 length  My Spruce 
      is $10/bd ft so 7 bdft is $70 for 14=99, but there is waste wood 
      so I think costs are about equal.
      
      My research says Aluminum spars are significantly stronger than Spruce.
      
      My weight numbers =94 A 14=99 aluminum spar weighs 9lb 3oz 
      plus .5lb of fillers and fastenings 9lb 11oz total.
      A 4.5=9Dx1=9Dx14=99 Sitka Spruce (.4375 cu ft @ 28 
      lb/cuft) spar would weigh 12.25 lbs less routed out 10=99x2.5=9D
      x1/2=9D (.087 cu ft @ 28 lbs/cuft) = 2.43 lbs. So 12.25-2.43= 
      9.82lb (9lb 13oz).
      
      I concluded :
      Equal Cost
      Equal Weight
      Greater Strength
      
      What's not to like ?
      
      John
      
      
      On Jan 2, 2018, at 8:59 AM, Jack Philips <jack@bedfordlandings.com> 
      wrote:
      
      I=99m just curious, not judgmental, but why do you want to use 
      aluminum spars?  It would seem that a great deal of extra work would be 
      involved, they would be heavier (by the time you add all the wood 
      fillers) and I=99m not sure without running a stress analysis that 
      they would be any stronger than wood spars.  Are they cheaper?
      
      Jack Phillips
      NX899JP =9CIcarus Plummet=9D
      Smith Mountain Lake, Virginia
      
      From: owner-pietenpol-list-server@matronics.com 
      [mailto:owner-pietenpol-list-server@matronics.com] On Behalf Of John C 
      Black
      Sent: Tuesday, January 2, 2018 11:12 AM
      Subject: Re: Pietenpol-List: Rib to spar attachment.
      
      I would appreciate any comments on my plan for assembling the ribs and 
      spars.   
      
      I am using Aluminum Spars from Carlson Aircraft.   My plan is to make a 
      filler for the side of the spar facing the rib. a 1/2=9D 
      wide (maybe 1=9D wide) x 3/8=9D thick piece of spruce to 
      fill the ~4.25=9D space between the bottom & top rails 
      relieved for the top channel and bulbs on the spar. (See picture) To 
      assemble I would slide the filler into place.  I want to make sure the 
      rib stays square to the spar.  I want to experiment to determine whether 
      to epoxy the rib to the filler.  If the rib stays square when epoxied to 
      the filler and the  rib/filler can be slid along the spar in case it 
      needs to move for diagonal wires then I=99d use a single 
      screw/nut in the center of the spar to hold the rib in location.  If 
      this approach had problems, then use no epoxy between rib and filler and 
      use 2 #8 screws with nuts to hold the filler and rib to the spar... 
      drilling 2 holes for screws 1.5=9D apart (1.5=9D from the 
      top & bottom of spar).
      
      I have some small concern about drilling the spar, but the center of the 
      web is doing little work so I think that would be acceptable.
      
      Since I=99ve never done this before, any help is appreciated.
      
      Thanks,
      
      John
      La Conner, WA
      
      On Jan 2, 2018, at 7:22 AM, Jack Philips <jack@bedfordlandings.com 
      <mailto:jack@bedfordlandings.com>> wrote:
      
      <jack@bedfordlandings.com <mailto:jack@bedfordlandings.com>>
      
      Glue is not necessary, and might be detrimental if you ever need to 
      replace
      a rib.  I did not glue my ribs in place.  
      
      Jack Phillips
      NX899JP "Icarus Plummet"
      Smith Mountain Lake, Virginia
      
      -----Original Message-----
      From: owner-pietenpol-list-server@matronics.com 
      <mailto:owner-pietenpol-list-server@matronics.com>
      [mailto:owner-pietenpol-list-server@matronics.com 
      <mailto:owner-pietenpol-list-server@matronics.com>] On Behalf Of Glen
      Schweizer
      Sent: Tuesday, January 2, 2018 10:18 AM
      Subject: Re: Pietenpol-List: Rib to spar attachment. 
      
      --> <glenschweizer@yahoo.com <mailto:glenschweizer@yahoo.com>>
      
      All the nails do is maintain position while glue cures
      
      > On Jan 2, 2018, at 6:55 AM, Comcast <4rcsimmons@comcast.net 
      <mailto:4rcsimmons@comcast.net>> wrote:
      > 
      > In reviewing drawing 5 for steel materials needed, it shows 2 nails at 
      top
      and bottom securing to the spar. 
      
      > 
      > Is this what you guys do/did?
      > 
      > This is just enough to hold general position. 
      > 
      > <image1.jpeg>
      > 
      > 
      > 
      > - Rich
      
      
      http://www.matronics.com/Navigator?Pietenpol-List 
      <http://www.matronics.com/Navigator?Pietenpol-List>
      http://wiki.matronics.com <http://wiki.matronics.com/>
      http://www.matronics.com/contribution 
      <http://www.matronics.com/contribution>
      
      
Message 12
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  | 
      
      
| Subject:  | Re: Rib to spar attachment. | 
      
      
      OK, I am ready to duck into my foxhole after I hit  and the shooting starts, but
      I'm going to poke at the aluminum spar vs. wood spar topic.  First of all though,
      I'll say that the second installment of my upcoming series on Piet wing
      spars (BPA Newsletter) will dig deeply into the weight and strength comparison
      of almost a dozen different wing spar variations that are seen on the Sky Scout
      and Air Camper, so what I'll throw out right now are just a few numbers that
      I've come up with but I'll present no figgerin' to back up those numbers.  Get
      the newsletter to get the figgerin' ;o)
      
      Best I can tell and calculate from the drawings in the 1932 Flying & Glider Manual,
      there is about 0.715 cu. ft. of spruce in a routed 1" spar that measures
      29 ft from tip to tip.  That spruce will weigh 20.02 lb.  A built-up "I" spar
      of the same dimensions will probably weigh a little more due to the plywood in
      the web and the glue used in the buildup, but it will perform about the same
      and is a great option.  Some judicious lightening holes in the plywood webs can
      also improve the strength-to-weight ratio and are probably needed anyway to
      allow brace cables and stiffeners to pass through the web.
      
      Let's say that the routed 1" spruce spar is good for a maximum bending moment of
      2475 ft-lb (see my first installment, coming out soon in the Newsletter).  Now
      comparing the data published by Carlson for their 4-A extruded spar, I get
      a weight of right at 19 lb for a 29 ft spar length, and from my figgerin' I get
      a maximum bending moment of 2407 ft-lb.  From this I conclude that the routed
      1" spruce spar and the Carlson 4-A spar are almost identical in weight and strength.
      
      Now let's look at cost and ignore labor since experimental aircraft builders all
      work for free, right?  ;o)  Aircraft Spruce shows 1" x 4-3/4" spruce spar stock
      at $9.28/ft for a cost of $269.12 for 29 feet.  Carlson shows the 4-A aluminum
      spar material at $103 for a 14 ft length.  If we cheat a bit and say we can
      make the outer 6" of the wingtips out of something other than aluminum spar
      stock so we can use standard length Carlson spars, two 14-footers will cost a
      total of $206.
      
      Using the spruce spars there's work to do the routing and smoothing.  Using the
      aluminum spars there's work to do the fitting of blocks to get the ribs to attach
      to the spars neatly.  Either way, there's work to do.  Either way, the cost
      is roughly the same.  Either way, you should get just about the same outcome
      once it gets in the air.  So now we're down to pitting spruce vs. aluminum in
      the never-ending circular argument that won Miller Lite the ranking of 8th best
      advertising campaign in history: "tastes great, or less filling?" ;o)  The
      aluminum spars appear to be a very nice, very viable option, especially if you
      don't have good wood available or if you're better at metal-working than at
      wood-working.
      
      --------
      Oscar Zuniga
      Medford, OR
      Air Camper NX41CC "Scout"
      A75 power, 72x36 Culver prop
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=477032#477032
      
      
 
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