What was found
CRACK ON ACOUSTIC PANEL AFTER REMOVAL OF ZEE STIFFENER AT LH UPPER TRANSCOWL ACOUSTIC PANEL AT LT UPPER TRANSCOWL WAS REPAIRED PER EA NO CRJ954-22246 REV IR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ACOUSTIC PANEL AFTER REMOVAL OF ZEE STIFFENER AT LH UPPER TRANSCOWL ACOUSTIC PANEL AT LT UPPER TRANSCOWL WAS REPAIRED PER EA NO CRJ954-22246 REV IR.