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Zenith CruZer & Sonex Logs
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Date:  1-29-2019
Number of Hours:  1.40
Manual Reference:  C75-FA-5
Brief Description:  Forward skin L angles, miscellany

Finished up-drilling holes on the left side of the fuselage in the area of the forward side skin and other longeron-related holes.

Began the process of adding L-angle stiffeners to the inner surfaces of the forward skins. Each side has 3 longitudinal angles, with differring degrees of curvature to fit the skin. Had to use my fluting pliers to gradually insert a curve to the surfaces. Finished the 3 angles on the right side and the top one on the left. Cut the second left angle, but have not begun fluting.

There will be wider, and heavier-stock angles which mount to the TOP of these L angles to provide a more finished appearance as well as adding strength and eliminating an edge that might cut a shin in flight.
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