What was found
DURING INSP, RT PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN 2 PLACES FWD EDGE OF LEADING EDGE. INSTALLED A REPAIR IAW SRM 54-04, FIG 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSP, RT PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN 2 PLACES FWD EDGE OF LEADING EDGE. INSTALLED A REPAIR IAW SRM 54-04, FIG 10.