Louis Ott - Experimental Aircraft Builder's Log

Louies Web Site


Date: 2-3-2010
Number of Hours: 4.00
Manual Reference: 6-ZU-1 & 4
Brief Description: Top skin reinforcment

Installed top skin rear reinforcing L angles between ribs 4, 5, 6. Fastened the reinforcing L angles to the rib flanges using a 0.025" cap strip over the top of the flange to join the L angle on each side of the flange.

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