What was found
DURING ENGINE CHANGE FOUND GOUGE DAMAGE ON NR 1 THRUST REVERSER HINGE FITTING FWD WEB UPPER BIFURCATION. BLENDED GOUGE AREA IAW SRM 54-31-01, FIG 101 THICKNESS OF WEB .125" MINIMUM AFTER BLEND WAS MAINTAINED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ENGINE CHANGE FOUND GOUGE DAMAGE ON NR 1 THRUST REVERSER HINGE FITTING FWD WEB UPPER BIFURCATION. BLENDED GOUGE AREA IAW SRM 54-31-01, FIG 101 THICKNESS OF WEB .125" MINIMUM AFTER BLEND WAS MAINTAINED.