Scott Flandermeyer - Experimental Aircraft Builder's Log

Flandy Rv-10


Date: 3-6-2008
Number of Hours: 3.00
Manual Reference: 6-3
Brief Description: VS skeleton preparation

Dimpled ribs. Machine countersinked spar flanges that overlapped VS-1014. Disassembled skeleton and deburred rear spar. Dimpled flange above machine countersinking. #12 Final drilled 3/16 in. hole in each rudder hinge.

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