As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON STIFFENER OVER FRAME WEB STA CANT 1531 AND 11HRS POSITION AT AFT ACCESSORY COMPARTMENT. DAMAGE OVER FRAME WEB STA CANT 1531 AND 11HRS POSITION WAS REMOVED PER SRM 51-30-05 VOL II. NEW STIFFENER WAS DRILLING AND ADJUSTED PER SRM 51-10-05 VOL II. NEW STIFFENER WAS TREATED AND PAINTED PER SRM 51-10-03 PAR 14 AND 21 VOL II. NEW STIFFENER WAS INSTALLED PER SRM 51-30-05 VOL II LONG CRACK IS .300".