As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AT STA 294 TO 312 RBL 22 ON PANEL BREAK (REF: AAR NR 99960033) EVALUATED DAMAGE CORROSION ORIGINAL THICK: 0.080" MATERIAL REM: (REF: WORK ACCOMPLISHED BY V940184 AND AAR QC A-82 V931568) 0.065",MATERIAL LOSS: 0.015", FOUND TO BE OUT OF LIMITS IAW B737 -800 SRM 53-10-51-1A-1 FIG 105 DET C AAR TOOL:46 DUE:08/05/2023& REMOVED & PLACED NEW PANEL BREAK SUPPOR IAW 51-40-02-0G-0