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Jeremy Balentines RV-8
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Date:  3-8-2014
Number of Hours:  6.00
Manual Reference:  
Brief Description:  Preparing the VS for riveting

all of the components of the VS were disassembled, de-burred, dimpled, and certain holes of the lower portion of the rear spar were countersunk so that when attaching the VS to the fuselage, it will lay flush against the support.
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