As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD PIT R/H TRANSITION PANEL HAS SPOTS OF CORROSION FROM STA.500B TO 500L. GROUNDED - YES. REMOVED CORROSION IAW B737-900 SRM 53-00-53 ORIG. THICKNESS .040 REMOVED .020 REMAINING .020 FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53 T8224B 02/DEC/2025 LOCATED, DRILLED AND TREATED REPAIR PARTS IAW B737-900 SRM 53-00-53 ASSEMBLED AND INSTALLED REPAIR PARTS IAW B737-900 SRM 53-00-53 BAC DWG'S 143A7501 REV A, 143A7500 REV- AND 143A7505 REV-.