As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A-CHECK FUSELAGE SKIN DAMAGE, SIZE 10"L X 5.1"W, AND STRINGER DAMAGED SIZE 1.5" L X 0.3" W. REFER TO RAM FORM N453PA-21-01 AND N453PA-21-02. ACCOMPLISHED A PERMANENT REPAIR TO / THE DAMAGED SKIN (PN: 65B23900-1) BETWEEN STA 2577 TO BSTA 2598 AND STRINGER S-38R TO S-42R PER EO 4453B984 PART 1 AND DAMAGED TO STRINGER S-42R PER EO 4453B984 PART 2.