What was found
A .75 INCH CRACK IN REPAIR ANGLE UPPER ATTACH ANGLE ON NR 1 ENG PYLON AT AFT END. CRACK WAS FOUND AT F-2 LTR CK. REPLACED ANGLE PER SRM 54-04A PG 17 FIG 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .75 INCH CRACK IN REPAIR ANGLE UPPER ATTACH ANGLE ON NR 1 ENG PYLON AT AFT END. CRACK WAS FOUND AT F-2 LTR CK. REPLACED ANGLE PER SRM 54-04A PG 17 FIG 4.