What was found
CLT - Q1 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S22L. REPAIRED FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S22L IAW TYPICAL REPAIR 53-60-07.
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 380 BETWEEN S20L TO S22L. REPAIRED FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S22L IAW TYPICAL REPAIR 53-60-07.