What was found
EXTERNAL FUSELAGE STA 844 STR18R+5" SKIN PANEL WITH SCRATCH.(<P>PERFORMED BLEND OUT REPAIR AND FOUND STRUCTURALLY ACCEPTABLE TO BOEING IAW COOPESA EO N°: COO-EO-2024-20121-R00 DATED MAY/08/2024 AND BOEING MESSAGE COO-TLS-24-0107-0413 DATED MAY/08/24. DOCUMENTED AND APPROVED ON FAA FORM 8100-9 REF: ID: 202405060171-0002 DATED MAY/14/24. NOTE: THIS 8100-9 IS A FIRST STAGE APPROVAL FOR STATIC STRENGTH AND WILL REQUIRE A NEW 8100-9 TO BE FINDING COMPLIANCE WITH 14CFR26.43 (D) WITHIN 24 MONTHS FROM THE DATE ON THE ATTACHED 8100-9, BOEING WILL FORWARD THE NEW DTA 8100-9 WITHIN 18 MONTHS. TC:25645 / TT:52793:09 </P>)