Scott Flandermeyer - Experimental Aircraft Builder's Log

Flandy Rv-10


Date: 2-11-2010
Number of Hours: 3.00
Manual Reference: 22-5
Brief Description: Flap match drilled

Steps 2,3,4 Match drilled all skin holes #40. Drilled trailing edge perpendicular to wedge chord line. Match drilled flap hinge bracket joggled sections. Marked and disassembled flaps.

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