As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FUSELAGE EXTERNAL SKIN AT BS727D S21R+4" REMOVED CORROSION LEVEL 2 AT FUSELAGE EXTERNAL SKIN AT BS727DS21R+4'' FROM P/N 65C38588 ORIGINAL THICKNESS 0.063'' REMOVED 0.063'' AND REMAINING THICKNESS IS 0'' AND IS OVER LIMITS PERFORM REPAIR PER SRM 53-00-01 REPAIR 35 I.A.W B737-300 SRM 51-10-02 PAGE 12~14 (REV130) PME:004692 DATE CAL OCT.18.2022 DAYE DUE : OCT .18.2023 MECH 360769 INSP 361733