As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, FOUND APPROXIMATELY 3 INCH CRACK IN WEB BETWEEN RIGHT 940 AND 950 FITTINGS AT STRINGER 180 IN R/W/W. REMOVED EXISTING WEB AND TWO ANGLES PER S/B 727-53-140. ALODINED AND PRIMED AREA PER SRM 51-10-2. REPLACED WITH NEW 'T' CHORD PER S/B 727-53-140.