What was found
CLT - Q4 - MAJOR REPAIR - CRACKS EMANATING FROM FASTENER HOLES ON FUSELAGE FRAME BS 380, BETWEEN S20L TO S22L. REPAIRED FUSELAGE FRAME AT BS 380, BETWEEN S20L TO S22L 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 - CRACKS EMANATING FROM FASTENER HOLES ON FUSELAGE FRAME BS 380, BETWEEN S20L TO S22L. REPAIRED FUSELAGE FRAME AT BS 380, BETWEEN S20L TO S22L IAW US AIRWAYS TYPICAL REPAIR 53-60-07A.