As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT BS 360 BETWEEN STR 4 AND 5 LT. REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 8 AND APPROVED 8110-3 REPAIR. ALL ACTIVE CRACK TIPS WERE ELIMINATED BY STOP DRILLING. A REINFORCING DOUBLER WAS INSTALLED.