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Scott's Aircraft Build Logs
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Date:  9-1-2014
Number of Hours:  3.00
Manual Reference:  
Brief Description:  Canopy frame

Removed the canopy frame for final installation of the locks. Primed, installed and torqued bolts on the locks.

Reinstalled canopy frame to check canopy fit ONE MORE TIME. The frame moved around during the riveting process. Canopy fit is right where I want it for the Sikaflex process. With the tonque depressors under the front edge and the aft rib clamped to the roll bar I have just under 1/8" at the roll bar and about 3/32" at the front edge. Marked the forward edge of the canopy on the skin as a reference for the Sikaflex process.

I worked on the forward edge of the of the canopy frame to get a more consistant distant from the forward skin across the entire fuselage.
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