What was found
CHAFE DAMAGE ON RT ENGINE WIRE HARNESS, LOCATED FWD END OF F4 EMS STRUT. INSPECTED, CHAFE DAMAGE IS TO OUTER WIRE WRAP ONLY, NO DAMAGE TO INNER WIRE NOTED. WRAPPED WIRES WITH FIBERGLASS TAPE IAW WM CHAPTER 20-12-10-201, REV 39.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHAFE DAMAGE ON RT ENGINE WIRE HARNESS, LOCATED FWD END OF F4 EMS STRUT. INSPECTED, CHAFE DAMAGE IS TO OUTER WIRE WRAP ONLY, NO DAMAGE TO INNER WIRE NOTED. WRAPPED WIRES WITH FIBERGLASS TAPE IAW WM CHAPTER 20-12-10-201, REV 39.