As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME OUTER CHORD DAMAGED AT BS 188-LBL 14-15 MOD. REPAIRED CHORD AT BS 188 LBL 14-15, PER SRM 51-70-11-2R-0. THIS IS A TLD REPAIR; WITHIN 30 DAYS AFTER THE AIRPLANE RETURNS TO SERVICE. CONTACT THE BOEING COMPANY FOR INSPECTION THRESHOLD. PERMANENT ACTON REQUIRED. WITHIN 30 DAYS AFTER THE AIRCRAFT RETURNS TO SERVICE, CONTACT THE BOEING COMPANY FOR INSPECTION THRESHOLD: TLD REF SRM 51-70-11-2R-0.