Scott Flandermeyer - Experimental Aircraft Builder's Log

Flandy Rv-10


Date: 7-19-2008
Number of Hours: 2.50
Manual Reference: 9-14 and 9-17
Brief Description: Bonded elevator and trim tab ribs and edge

9-14 Step 8 Applied sealant to ribs and placed into position Step 9 Applied thin coat of sealant to trailing edge wedge and inserted into position Step 10 Clecoed trailing edge and weighted down to allow to cure 9-17 Step 8 Riveted trim tab horns and botton flange of rear spar to trim tab skins. Step9 Applied sealant to trim tab ribs and inserted. Clecoed skin to top sapr and set in clamp blocks to cure. Step 10 Riveted end flanges of trim tabs

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