Ken Cox - Experimental Aircraft Builder's Log

Ken & Susie's Web Site


Date: 3-29-2010
Number of Hours: 3.00
Manual Reference: 6-5
Brief Description: Dimple & Prime Vertical Stab

Disassembled the Vertical stabilizer. Deburred all holes, Dimpled the skin, ribs and spars. Countersunk rivet holes on Rear Spar for flush rivets at the bottom. Used Cortec system to prepare parts for priming and primed all ribs and spars.

Dimpled Skin

Using Cortec Corosion System

Cortec Primer

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