Raymond Sievers - Experimental Aircraft Builder's Log

Raymonds Web Site


Date: 2-24-2010
Number of Hours: 3.00
Manual Reference: DRAWING 14
Brief Description: Manual section 7 Lines 136 thru 139

Fitted top flap skin, FL-901C, to flap skeleton assembly. Matched drilled to ribs. Installed both inboard and outboard leading edge assemblies.

Flap assembly weighed flat

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