Matthew Lorenz - Experimental Aircraft Builder's Log

My RV-10


Date: 7-29-2010
Number of Hours: 3.00
Manual Reference: Sec. 7-9 DWG 13A
Brief Description: Epoxy Primed / Sealed Rear Spar

Epoxy primed / Sealed the outer rear spar and hinge points. My plan is epoxy seal any areas that will be exposed to the outer eliments. I am using a 3 part PPG Epoxy primer... thinned to specs which acts to seal the structure. Seems to work excellent... need a chisel to get it off.

Rear Spar Epoxy Sealed

Hinge Points Epoxy Sealed

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