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Date:  11-9-2018
Number of Hours:  3.00
Manual Reference:  6.5
Brief Description:  Completed V-stab Skeleton Assembly

Radius'ed edges of VS-1205, VS-1206, and VS-1202. Smoothed and deburred edges. Fluted Flanges to straighten VS-1202, VS-1205, VS-1206, VS-1207. and VS-1208. Cleaned metal and primed with Zinc Phosphate Aviation Primer. Rivets VS1212A L&R to VS-1203 and attached VS-1208, VS-1207 to VS-1202 and then to VS-1203 Spar. Completed V-stab skeleton by attaching VS-1205 and VS-1206 to VS-1203 spar.
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