As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 21 TO FRAME 22 BETWEEN STRINGER 22L TO STRINGER 23L, REMOVED AND REINSTALLED EXISTING REPAIR LOC. ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 21 TO FRAME 22 BETWEEN STRINGER 22L/H TO STRINGER 23L/H AS PER A 320 SRM 53-00-11 FIGURE 238 AND ER/A 549159 14 REV A