What was found
DAMAGE WAS IDENTIFIED ON THE ATTACHMENT ANGLE (PN 350A21-4064-21), AS ILLUSTRATED IN FIGURE 1 OF DOCUMENT 17-5300-EA-5339, REV. –. THE DAMAGED COMPONENT, LOCATED BENEATH THE MAIN CABIN FLOOR AT BS 845 AND SHOWN IN THE SAME FIGURE, COULD NOT BE OBTAINED IN TIME TO SUPPORT RTS, AND REPAIR BY REINFORCEMENT WAS NOT PRACTICAL. AS A RESULT, A REPLACEMENT ANGLE WAS FABRICATED IN ACCORDANCE WITH AIR METHODS ENGINEERING AUTHORIZATION 17-5300-EA-5339, INITIAL REVISION DATED 11/11/2025 AND WAS APPROVED BY FAA FORM 8110-3.