As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 T/R RT UPPER ACT ATTACH POINT STRUCTURE CRACKED. DEFERRED NR 367364. REMOVED AND REPLACED 3 AND 4 O'CLOCK POSITION STIFFENERS PER ASSY DRAWING 491B1330033. ACCOMPLISHED PERMANENT REPAIR ON STIFFENERS AT 1 AND 2 O'CLOCK POSITIONS PER MRA CMM 78-33332-02 REPAIR 6. THIS CLEARS D367364.