As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHEN PERFORMING EA 5310-05878 REV D, INSPECTION FOUNDS CRACK INDICATIONS AT 2 FASTENER HOLES IN SKIN AT STA 540 BETWEEN STR 22R T AND 23RT. CRACK INDICATIONS ARE IN FASTENER HOLES IN AFT ROW 1 .9" AND 3.0" BELOW CENTERLINE OF STR 22RT. VERIFIED BY HFEC. REMOVED DAMAGE AND INSTALLED REPAIR PER EC/RA 5310-07067 REVA PART 1 AND REF EA 5310-05878 REV D OP5.