As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TRANSITION PANEL AT STA 727D+4 TO STA 767 HAS CORROSION ON RH OUTTER EDGES IN SEVERAL PLACES. GROUNDED - YES. REPAIRED THE R/H TRANSITION PANEL AT STA 727D+4 TO 767 USING MAT BAC1496-377 PER B737-800 SRM 53-00-53-2R-5. REMOVED CORROSION FROM THE R/H TRANSITION PANEL FROM STA 727D+4 TO 767 PER B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040 PER B737-800 SRM 53-60-53-0I-2 TABLE 2. 100% MAT LOSS IN 3 LOCATIONS AND IS FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-00-53-1A-2.