Martin Lindsey - Experimental Aircraft Builder's Log

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Date: 6-15-2005
Number of Hours: 2.00
Manual Reference: 7-8
Brief Description: CS Front spar for skin dimples

Used microstop CS and a 0.032" test patch dimple to CS holes in front spar flange to accept skin dimples. Masked off area and spot primed CS holes with SEM self-etch primer. Completed both top and bottom sides of spar.

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