Author Topic: Cabin Eagle rear wing spar location versus fuse carry through dimensions  (Read 7742 times)

Offline pramer

  • Jr. Member
  • **
  • Posts: 14
  • Total likes: 3
  • New Member
  • OS:
  • Windows NT 10.0 Windows NT 10.0
  • Browser:
  • Chrome 52.0.2743.82 Chrome 52.0.2743.82
Hi I just received #19 of the cabin eagle plans.  I am in Winnipeg Canada.  I have been going through the plans in detail and came across a mistake I think.  On page 7 the top fuse carry throughs are dimensioned @ 29.8" on center.  On the rib drawing the spars are ~28.75 apart on center.  I beleive the rib drawing is wrong.  Can any one confirm.  I plan to build my wing first as I dont have a garage yet.
Thanks
Phil


Offline Kiwi55

  • Full Member
  • ***
  • Posts: 110
  • Total likes: 48
  • Cabin Eagle
  • OS:
  • Windows 7/Server 2008 R2 Windows 7/Server 2008 R2
  • Browser:
  • MS Internet Explorer 9.0 MS Internet Explorer 9.0
  • Eagle Type: Cabin Eagle
Phil,
I had the same issue. Having already built the wings I modifed cabin top to fit. Also page 32 the plans shows the bottom of the tank at 28 1/2 inches long. If the cabin top was at 29.8 the tank would not sit on the top tubes.
Oh and... The template for the wing ribs pretty much dictates where the spars go, leaving moving the fuselage the only place you can make a change...

This was just my interpretation, YMMV.
...Paul

Offline Leonard

  • The Boss
  • *
  • Posts: 80
  • Total likes: 27
  • Designer
  • OS:
  • Windows NT 10.0 Windows NT 10.0
  • Browser:
  • Chrome 46.0.2486.0 Chrome 46.0.2486.0
    • Better Half VW
Hi Build the wings and build the fuselage to fit.  Leonard