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MIKE'S WEB SITE
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Date:  2-11-2004
Number of Hours:  10.00
Manual Reference:  40
Brief Description:  Installing the cabin frame

Clamped and drilled F631C&D angle brackets to outside and inside of frame, Filed outside edge of F631C flush with outside contour of frame/fuselage skins Clecoed skin to fuselage Clamped cabin frmae to braclets and fuselage> Temp clecoed F632A Chaneel as brace Located and drilled screw holes in (#40 for now) with using holes in skin a guide. Drilled to #30 and correct size for screws/tap and bolts Made/fit/drilled F732B&C brackets to end of F632A Channel, F706 BH, and F631 Subassy. Removed and stored
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