As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#2 TANK UPPER SKIN (INTERNAL) BETWEEN RIB 21 AND RIB 22; AFT UPPER STRINGER END IS CRACKED.<[01] CRACK ON #2 FUEL TANK (INTERNAL). AFT UPPER STRINGER; BETWEEN RIBS 21 AND 22 WAS REPAIRED IAW EA 25-157-00566-WIP1 AND EA 25-157-00566;[02] C/W