What was found
NUMBER 2 ENG PYLON RT OB SKIN STRUCTURE PAN AFT AND ABOVE AFT ENG MOUNT CRACKED. TRIMMED OUT DAMAGE AND FABRICATED REPAIR PARTS. PYLON SIDEWALL PAN ASSEMBLY REPAIRED PER ENGINEERING AUTHORIZATION 1-5481-T0359918.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMBER 2 ENG PYLON RT OB SKIN STRUCTURE PAN AFT AND ABOVE AFT ENG MOUNT CRACKED. TRIMMED OUT DAMAGE AND FABRICATED REPAIR PARTS. PYLON SIDEWALL PAN ASSEMBLY REPAIRED PER ENGINEERING AUTHORIZATION 1-5481-T0359918.