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.1.650" IN LENGTH ON THE FUSELAGE SKIN AROUND THE 8TH AND 9TH STRIGNER ATTACH RIVETS ALONG S-13AR AFT OF FRAME 1654 AS MARKED. C/W WITH ERA 566324-14 WHICH REFERS TO REPAIR CRACKS PER SRM 53-00-01. (LP 0898008)