What was found
DAMAGE TO THE LH STA5025 FRAME INNER SKIN PANEL (PN: B533K5606-211) IN THE FORM OF 2EA CRACKS ON THE UPPER END OF THE PART AND A CHAFE ON THE LOWER END OF THE PART. THE CRACKS WERE MEASURED TO BE APPROXIMATELY 0.19” AND 0.20” IN LENGTH EMANATING FROM A FASTENER HOLE. THE CHAFE WAS MEASURED TO BE APPROXIMATELY 0.66” X 0.55” AND 0.010” DEEP. THIS DAMAGE HAS BEEN REPAIRED AND DOCUMENTED ON FAA FORM 337 DATED 06/05/2021.