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 STA 500C+15 TO 500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500C+15 -500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737- 800 SRM 53-30-53-1A-2. TABLE 2. REMOVED .020" REMAINING THICKNESS IS .020" AND IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2.4.A.(2). REPLACED FWD PIT R/H TRANSITION PANEL STA 500C+15 TO 500I IAW B737-800 SRM 53-00-53-2R-5.