Douglas C. Weiler - Experimental Aircraft Builder's Log

Douglass Web Site


Date: 2-11-2008
Number of Hours: 2.50
Manual Reference:
Brief Description: Rudder

Riveted bottom rib in place. Silicon applied at forward end of stiffeners to prevent cracks (I hope). Drilled angle to keep TE straight. Applied JB weld to TE and clecoed into postion. Will let set up for 4 days.

< Previous Log Entry Next Log Entry >