As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING HFEC HOLE INSPECTION FOR EA 5310-05878 OP 2 STEP 6 & 7 FOUND CRACK INDICATION IN SKIN LOCATED AT STATION 540 BETWEEN STRINGER 22L & 23L, AFT HOLE SECOND ONE DOWN FROM TOP. FUSELAGE SKIN AT STATION 540 BETWEEN STRINGER 22L & 23L HAS BEEN REPAIRED IAW EA 5310-05878 REV A OP 4.