What was found
AT C CHECK, FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT LOWER LEG W/S 170. REMOVED WEB, INSTALLED ANGLE REPAIR PER SRM 51-40-4, 4 BY 6, N/R 2108.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT LOWER LEG W/S 170. REMOVED WEB, INSTALLED ANGLE REPAIR PER SRM 51-40-4, 4 BY 6, N/R 2108.