What was found
AT D CHECK, RT SIDE OF NR 2 ENGINE PYLON LOOK THROUGH ACCESS PANEL 35201 ANGLE IS CORRODED AND CRACKED. REMOVED ANGLE, INSTALLED NEW ANGLE PER SRM 54-10-2, 12 LONG, N/R 6778.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D CHECK, RT SIDE OF NR 2 ENGINE PYLON LOOK THROUGH ACCESS PANEL 35201 ANGLE IS CORRODED AND CRACKED. REMOVED ANGLE, INSTALLED NEW ANGLE PER SRM 54-10-2, 12 LONG, N/R 6778.