What was found
CLT - Q1 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 601, S17L, LBL 65.5. REPAIRED FUSELAGE FRAME AT BS 601, S17L, LBL 65.5 IAW TYPICAL REPAIR 53-62-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q1 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 601, S17L, LBL 65.5. REPAIRED FUSELAGE FRAME AT BS 601, S17L, LBL 65.5 IAW TYPICAL REPAIR 53-62-01.