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It's hard to directly compare properties. (It appears that different methods are used for different types of materials.) The tensile strength of gray resin appears to be better than "plywood" (although I'm not sure what kind).https://formlabs.com/materials/engineering/
It was printed in the "rigid" resin. They are not very forthcoming with details of what is in the resin, but there is a datasheet that has the material properties on that web page.
https://www.matweb.com/search/datasheet_print.aspx?matguid=bd6620450973496ea2578c283e9fb807
The high end for "plywood" is 35MPa compared to 61MPa.
"Aircraft plywood" appears to be "MIL-P-6070 B". Unfortunately it's a scanned document so hard to search, but the only thing I saw on quick perusal is a shear strength of 250PSI. (No shear strength is listed on the FormLabs data sheet.)
file:///Users/john/Downloads/MIL-P-6070.PDF
This is great stuff! Now I'm getting excited about SLA printing. Only big reservation is build volume.