Scott Flandermeyer - Experimental Aircraft Builder's Log

Flandy Rv-10


Date: 6-26-2008
Number of Hours: 2.75
Manual Reference: 9-8 and 9-9
Brief Description: Dimpling and C'sinking

9-7 Step 9 Completed dimpling on skins and tip rib skins 9-8 Step 1 Dimpled both spar flanges 3/32 for skin dimples. Step 2 Machine C'sink first 29 holes on upper inboard surface of rear spar. Dimpled all remaining flange holes. Step 3 Dimpled front and rear spar root rib attach points. Step 4 Dimpled root rib flanges for skin dimples and attach points for spar dimples. 9-9 Step 2 Dimpled inboard shear clip for 1/8 rivet. Step 3 Dimpled flanges for both rib halves 3/32 for skin dimples. Step 4 Dimpled forward two dimples on E-903 and corresponding holes on E-904 for 1/8 flush rivets. Step 5 Dimples flanges on E-903 and E-904 for skin dimples.

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