What was found
FUSELAGE UPPER AFT SKIN CRACKED AT FR 75 AT THE FIRST FASTENER BELOW STGR 2L 1 CRACK .25" IN LENGTH. C/A-ACCOMPLISHED A PERMANENT REPAIR OF FUSELAGE SKIN CRACK AT FR 75 BETWEEN STGR 2L-3L IAW ERS-EM-53MR-4269.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE UPPER AFT SKIN CRACKED AT FR 75 AT THE FIRST FASTENER BELOW STGR 2L 1 CRACK .25" IN LENGTH. C/A-ACCOMPLISHED A PERMANENT REPAIR OF FUSELAGE SKIN CRACK AT FR 75 BETWEEN STGR 2L-3L IAW ERS-EM-53MR-4269.