As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HFEC INSPECTION FOUND 01EA CRACK APPROX. 0.90 INCH IN LENGTH ON THE FUSELAGE SKIN BELOW THE 13TH STRINGER-ATTACH RIVET ALONG S-14R, FORWARD OF FRAME STA1654.5. THE CRACKED AREA OF SKIN TRIMMED OUT AND REPAIRED AS PER SRM 53- 80-01-2R-7 REPAIR 7 FIG201 RELEASE 119.00-06/01/22. 37500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR WITHIN 7500 FLIGHT CYCLES FROM THE REPAIR INSTALLATION. (2529715)