What was found
PERFORM CUTTING AND SPLICING OF STRINGER 14 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0064 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 24. PERFORMED SPLICE REPAIR OF FUSELAGE STGR 14R BETWEEN B/S 663.75 AND B/S 685 I.A.W COO-EO-2025-22274-R00 REV00 DATED 09-MAY-25, BOEING MESSAGE COO-TLS-25-0064-04B DATED 08-MAY-25. APPROVED AND DOCUMENTED ON FAA FORM 8100-9 REF ID: 202505060093-0003 DATED JUN-10-25. THIS HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAG (G) OF AD 2025-07-03. NO FURTHER DEFECTS NOTED.