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 BS 500L HAS MULTIPLE SPOTS/AREAS OF CORR. GROUNDED - YES. REMOVED CORROSION ON TRANSITION PANEL IAW SRM 51-10-02. ORIGINAL THICKNESS IS .040 , AT MULTIPLE LOCATIONS REMAINING THICKNESS IS .030, LOSS OF .010 OF MATERIAL. OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED TRANSITION PANEL FROM STA 500A TO STA 500L AND REPLACED WITH REPAIRED/FABRICATED TRANSITION PANEL IAW SRM 53-00-53-2R-5 & BAC DWG 143A7500 REV A.