What was found
CLT - Q4 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L IAW US AIRWAYS TYPICAL REPAIR 53-60-07A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q4 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 380 BETWEEN S20L TO S21L IAW US AIRWAYS TYPICAL REPAIR 53-60-07A.