What was found
DURING C-CHECK/BRIDGING INSPECTION, FOUND TEE EXTRUSION WORN 0.025 THICKNESS AND GOUGED TO DEPTH OF 0.045 AT NR 4 ENGINE, LHS, FS 410, 11.0. WORN AREA BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK/BRIDGING INSPECTION, FOUND TEE EXTRUSION WORN 0.025 THICKNESS AND GOUGED TO DEPTH OF 0.045 AT NR 4 ENGINE, LHS, FS 410, 11.0. WORN AREA BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.