As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS WERE REMOVED AND THE DISCREPANT AREAS REWORKED, HFEC WAS PERFORMED AT EACH AREA. FASTENERS INSTALLED. ALL WORK WAS ACCOMPLISHED IAW INSTRUCTIONS SR 1-1993034429.