As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH BEAM Y=+10.748" FRAME 86-89. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 RH BEAM Y=+10.748" FRAME 86-89 PER SRM 51-40-08. SEE EAMS W/O H6968 SN 136 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.