As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE MAIN FRAME BS 1000 BULKHEAD CHORD STR 37L-STR 39L AFTER INSPECTION FOUND CRACK APPROX 0.75". FUSELAGE MAIN FRAME BS 1000 BULKHEAD CHORD STR 37L- STR 39L CRACKED AREA REPAIRED IAW EO 4453A506 PART 3. THIS REPAIR IS A MAJOR REPAIR.