As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION DAMAGE HAS BEEN FOUND ON THE REAR SPAR LOWER CHORD OF THE INBOARD TRAILING EDGE FLAP ON THE RH WING. THE DAMAGE HAS BEEN CUT OUT TO REMOVE THE DAMAGED SECTION OF THE 2024-T3511 EXTRUDED TEE AND REPLACED WITH AN EQUIVALENT 2024-T3 EXTRUSION. THE REPAIR MEMBER IS SPLICED TO THE EXISTING LOWER CHORD USING 2024-T3 EXTRUDED ANGLES AT EACH END IN ACCORDANCE WITH SEMAN PERU SAC REPAIR DRAWING ED-2025-0005 (REF. 7).