What was found
PERFORM CUTTING AND SPLICING OF STRINGER 10 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0063 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 14.<BR>(<P>PERFORMED SPLICE REPAIR OF FUSELAGE STINGER 10 RH, BETWEEN STA 663.75 AND STA 685 I.A.W COO-EO-2025-22273-R00 REV 00 DATED 09-MAY-25. APPROVED AND DOCUMENTED ON FAA FORM 8100-9 REF. ID 202505060091-0004 DATED 11-JUN-25. NOTE: THIS HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (G) OF AD 2025-07-03. NO FURTHER DEFECTS NOTED.</P>)