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Flandy Rv-10
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Date:  5-25-2010
Number of Hours:  3.50
Manual Reference:  21-3,4,5 & 22-7,8
Brief Description:  Aileron and Flap work

Back riveted stiffeners to right top aileron skin. Clecoed in place and match drilled all skin to rib holes. Both ailerons now ready to disassemble and deburr.

Installed left flap in cradle and riveted top skin in place. Removed and back riveted last two rivets on each rib. Installed in reverse cradle and clecoed in bottom skin. Started riveting.

Installed right flap in forward cradle.

Finished Fuselage Inventory.
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