What was found
DURING ALLEGIANT ACCOMPLISHMENT OF TASK A32X-53-212-020 , UPPER FUSELAGE COCKPIT RH LATERAL WINDOW FRAME FR4 VERTICAL STIFFENER WITH CRACK WAS FOUND. AIRBUS WAS CONTACTED ASKING FROR FURTHER INSTRUCTIONS. THE STIFFENER WAS REPAIRED FOLLOW REPAIR INSTRUCTIONS AS PER COOPESA EO COO-EO-2025-21684-R00. AIRBUS PROVIDED APPROVED DOCUMENTED UNDER RDAF 81537258-004-2025#A AND ALLEGIANT ERO A32X-STR-53ERO-00204-R00. THIS IS A CATEGORY B REPAIR WITH INSPECTION REQUIRED.THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1Q010 ITEM 2-4