As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE STATION 540 SKIN AT STRINGER 22L & 23L, TWO CRACKS AT CHORD HOLES & ONE AT SKIN HOLE. PERFORMED PART 1 INTERIM REPAIR, INSTALLED FREEZE PLUG HOLE A & OPENING HOLE TO .2455 IAW ECRA 5310-06438 REV A. INITIATE DIP TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 12 MONTHS. PLANNING TO CONTACT ENGINEERING AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR THE PERMANENT REPAIR.