As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION IN AND AROUND NUTPLATE HOLES AT BS 987+6 ;RBL36<[01] REMOVED CORROSION ON SUPPORT (P/N 147A5710-2) BS 987+6; RBL 36. ORIGINAL MATERIAL THICKNESS IS .050? REMOVED .015? OF MATERIAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REMOVED AND REPLACED SUPPORT (P/N 147A5710-2) IAW SRM 51-40-02.;[02] C/W PART REPLACEMENT