What was found
AFTER REMOVAL OF Z-ANGLE ON UPPER RH TRANSCOWL (FOR REPAIR OF DAMAGED FASTENERS) FOUND 1.159" CRACK IN INNER PERFORATED SKIN. REPAIRED RH UPPER TRANSCOWL SKIN PER EA CRJ954-13905 REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF Z-ANGLE ON UPPER RH TRANSCOWL (FOR REPAIR OF DAMAGED FASTENERS) FOUND 1.159" CRACK IN INNER PERFORATED SKIN. REPAIRED RH UPPER TRANSCOWL SKIN PER EA CRJ954-13905 REV B.