What was found
DURING ROUTINE C-CHECK, FOUND REINFORCING ANGLE WITH 1 INCH CRACK AT FS 804.5, ADJACENT TO STRINGER 14R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-03. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK, FOUND REINFORCING ANGLE WITH 1 INCH CRACK AT FS 804.5, ADJACENT TO STRINGER 14R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-03. (M)