Damon Farnsley - Experimental Aircraft Builder's Log

Todd's Web site


Date: 7-22-2009
Number of Hours: 0.75
Manual Reference:
Brief Description: Cooling Ramp #1

-Trimmed the flanges of the cooling ramp skin according the plans -Clecoed and drilled the stiffeners to size -Drilled the #30 holes to size on the ramp -Match drilled the rear stiffener to the forward LG crossmember on the forward fuselage floor assembly -Deburred the holes on everything. Edge deburred the stiffeners. Still need to edge debur the cooling ramp skin

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