What was found
DURING ACCOMPLISHMENT OF THE ALLEGIANT A32X-53-210-003-WINDSHIELD, UPPER FUSELAGE COCKPIT LH WINDSHIELD CENTER POST LOWER HORIZONTAL FLANGE OPEN FASTENER HOLE WITH CRACK DETECTED DURING ROTOTEST INSPECTION OF THE CONTINUITY FITTINGS REPLACE PROCEDURE AS PER AIRBUS R53112919 FLAG NOTE 3.PERFORMED PERMANENT BUSH HOLE # D REPAIR ON COCKPIT WINDSHIELD LH FRAMING IAW COOPESA EO # COO-EO-2025-23038-R00 APPROVED AND DOCUMENTED ON AIRBUS RDAF 81638703/014/2025 # A AND ALLEGIANT ERO # A32X-STR-53ERO-00376-R00. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q171 ITEM 2-27.