As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A CRACK WAS FOUND OF 0.156IN LENGTH APROX. ON BS 1640 RT FUSELAGE FRAME INNER CHORD FWD RETURN FLANGE RADIUS JUST BELOW STGR 14R. RH FUSELAGE FRAME STA. 1640 INNER CHORD FWD WAS REPAIRED PER ER/A 588298-14AD REV. C SECTION III: PERMANENT REPAIR #2 AND PRI REV 0 TO PRI REV 6. (1572703) AIRCRAFT WAS GROUNDED