As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INTERIOR FUSELAGE, RT WING PRESSURE DECK RE-ENFORCEMENT ANGLE AT STRINGER 4R IS CRACKED AFT OF FRAME 27. NO REPAIR ACTION IS REQUIRED OTHER THAN THE APPLICATION OF PR 1436GB. APPLIED BEAD ALONG THE CRACK WITH PR 1436GB PER DO/TS-3855/10-13855 E-MAIL INSTRUCTIONS. FINAL APPROVAL RECEIVED SRAS DO/TS-3673/05...3303 ISSUE C FOR RT UPDATED AFTER CRACK PROPAGATION.