Corvair Cores 
I won a 1965 164 CI 110 HP Corvair engine off Ebay for about $40. I've also purchased a 95 HP engine of the same year from a guy in Milwaukee for $150. By the time these two engines have had the necessary changes to convert them to aircraft usage, they will be essentially the same - producing 110 HP on takeoff, and 90 HP continuous.

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Rib #13 on Relined Jig 
I re-lined the jig to replace the wax paper with plastic wrap, then made another rib.

1 hr

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Unofficial Inspection 
I took a couple of ribs to the EAA 509 meeting. Several members looked them over and pronounced them good.

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Rib #12 
1 hr

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Rib #11 
1 hr

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Rib #10 
1 hr

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Rib #9 
1 hr

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Rib #8 
1 hr

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Rib #7 
1 hr

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Breaking a Test Piece 
I tried breaking the extra "T". Those joints are TOUGH! Supporting the top of the "T" about 1/2" on each side of the gusset, I tried pulling on the stem of the "T". I was expecting a bending or shear failure in the top of the "T", but I couldn't grip the stem hard enough to apply the force needed to break it. I was able to pull with maybe 100-150 lbs of force. In the process, I crushed the end of the stem with the grips.

I cut off the crushed part and tried pushing on the stem in a vise with the top supported similarly to above. The top broke just outside the glue joint. Bending failure in the tension fibers. Just for kicks I pushed sideways on the T until it broke. Same result.

With the next test piece, I intend to devise a better way to apply tension to the stem - perhaps by gusseting another crosspiece to the bottom to form an "I". I also want to try the compression test again by supporting the top closer to the gusset to induce shear failure in the top or compression failure in the stem. If I can get a test that consistently fails the stem in compression or tension (not bending), then I can be reasonably sure that I am testing the joint to its fullest capacity.

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