As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 1000 HOUR INSPECTION, CORROSION DAMAGE WAS NOTED TO THE T-CAP (PN: L533M1028203) OF FRAME 3 AT APPROXIMATELY FUSELAGE STATION 3,150MM. THE DAMAGE REQUIRES PART REPLACEMENT AND DUE TO PART AVAILABILITY, THE PART WAS FABRICATED PER AIR METHODS ENGINEERING AUTHORIZATION # 23-5300-EA-4303, INITIAL REVISION DATED 07 MAR 2023 AND APPROVED FOR STRUCTURAL ASPECTS ON FAA FORM 8110-3 BY RYAN LEE (DER-Y #905240204) DATED 09 MAR 2023 WITH DER SPECIFIC SEQUENCE # 23RL006AM.