Arthur Gibeaut - Experimental Aircraft Builder's Log

ARTHUR'S WEB SITE


Date: 1-11-2010
Number of Hours: 2.00
Manual Reference: N/A
Brief Description: Fuselage Stiffeners

I decided to install "L" angles on the inside fuselage skins to avoid the "oil-canning" that is described by the other builders. Took a little work to align the angles and holes.

Layout holes

Drill

Reverse and rivet.

< Previous Log Entry Next Log Entry >