What was found
PERFORM CUTTING AND SPLICING OF STRINGER 14 L/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0062 DATED 08 MAY 25 AND BOEING DRAWING # 002A 0084 SHEET 24.(<P><SPAN LANG="EN-US">PERFORMED SPLICE REPAIR OF FUSELAGE STGR 14L BTWN B/S 663.75 AND B/S 685 I.A.W COO-EO-2025-22272-R00 REV 00 DATED 09-MAY-25, BOEING MESSAGE NUMBER COO-T25-25-0062-04B DATED 08-MAY-25. APPROVED AND DOCUMENTED ON FAA FORM 8100-9 REF ID 202505060081-0002 DATED 10-JUN-25. THIS HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAG (G) OF AD 2025-07-03.NO FURTHER DEFECTS NOTED.</SPAN></P>)