As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION LOCATED AROUND FASTENER HOLE ON FUSELAGE SKIN IN THE AREA UNDER THE DRAG LINK ASSEMBLY; COMMON TO THE BS540 BULKHEAD CHORD; BETWEEN S-21L AND S-22L. LOWER FUSELAGE. ; 2021-269663 / [01] ACCOMPLISHED EA 5331-E-14519-NG ON TTG8Q001PKAQ; [02] ACCOMPLISHED EA 5331-E-14519-NG ON TTG8Q001PKAQ.. RII ITEM