What was found
NR 2 ENG PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED 1 INCH. FOUND DURING D-1 LTR CK TPAMM. REPAIRED PER SRM 54-04A FIG 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENG PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED 1 INCH. FOUND DURING D-1 LTR CK TPAMM. REPAIRED PER SRM 54-04A FIG 4.