What was found
CRACK FIN 80VU IS IN CONTACT WITH STRUCTURE LOWER LATERAL FITTING RH SI DE. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. (REFER TO AMDS 2515-01014-02B AD RELATED). C/A: ER/A 623985-14AD REV A APPROVED DATE: 04/APR/25 WAS VERIFIED AGAINST ER/A 623985-14AD PRI REV 0 REPAIR INSTRUCTIONS AND WEREFOUND IN COMPLIANCE WITH THE SCOPE OF THE WORK ACCOMPLISHED, STEPS RELATED ON ER/A 623985-14AD REV A TO ITEM 144, 145 AND 146ARE DOCUMENTED IN THIS ORNRC 86/100 AND PERFORMED ACCORDINGLY , FOR TIME CONTROLLED ITEM SEE SECTION IV AND LOG PAGE # 0895434INITIAL INSPECTION WITHIN 19,500FC FROM ACCOMPLISHMENT OF SECTION III ( APR/2025) AS PER ER/A 623985-14AD REV A,