Fit F23-05L/R mount assemblies to aft fuselage section and pilot drilled/clecoed into place along upper longerons and upper cross tie #3. Leveled workbench and fuselage tail cone box for push rod support assembly installation. Measured out pushrod assembly hole centers from longerons and set center marking on laser level. Verified dimensions and pilot drilled into upper and lower cross ties. Repeated process for both forward and aft pushrod support assemblies.
Hours Worked: 1.98
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