What was found
DURING EVALUATION OF CORROSION ON TCAS BONDING PLATE (WHICH IS ATTACHED TO PANEL 170AB) FOUND PLATE TO BE OUT OF ACCEPTABLE LIMITS. REMOVED TCAS PLATE PER SRM 51-40-03. MANUFACTURED NEW TCAS PLATE IAW DWG F2MA285033C01
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING EVALUATION OF CORROSION ON TCAS BONDING PLATE (WHICH IS ATTACHED TO PANEL 170AB) FOUND PLATE TO BE OUT OF ACCEPTABLE LIMITS. REMOVED TCAS PLATE PER SRM 51-40-03. MANUFACTURED NEW TCAS PLATE IAW DWG F2MA285033C01