As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-212-020, UPPER FUSELAGE COCKPIT LATERAL WINDOW FRAME AT FR4 RH VERTICAL STIFFENER WITH CRACK WAS FOUND.STIFFENER WAS REPAIRED FOLLOW REPAIR INSTRUCTIONS PER ALLEGIANT ENGINEERING ENGINEERING ORDER A32X-STR-53ERO-00426-R00. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q242 ITEM 2-7.