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Date:  10-4-2018
Number of Hours:  4.50
Manual Reference:  
Brief Description:  23iS/U-06

1. The wing spar penetration holes were cut out.
2. A large hole was drilled.
3. A mark was made on the F-01270-L-1 & -R-1 both sides.
4. The screw was dimpled and then riveted F-01270-L-1 & R-1
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