As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD PIT RT TRANSITION PANEL FROM BS 500A TO 500G+4 CORRODED SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION ON FWD PIT RT TRANSITION PANEL FROM BS 500A TO 522G+4 IAW SRM 51-10-02, ORIGINAL THICKNESS IS .40 IAW SRM 53-30-53. REMOVED .010 REMAINING THICKNESS IS .030 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. R & R TRANSITION ANGLE FROM BS 500A TO 500G+4 IAW SRM 53-00-53-2R-6 ALODINED IAW SRM 51-20-01 AND PRIMED IAW SOPM 20-41-02. REMOVED DOT AND OR STREAMER .