As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENG LEFT TOP PANEL OF PYLON ANGLE SUPPORT IS CORRODED AND CRACK AT STA 1380. REMOVED CORRODED ANGLE AT TOP OF PYLON NR 2 ENG LEFT SIDE BS 1381.5 TO 1455 PER SRM 51-30-2. FABRICATED NEW ANGLE PER SRM 54-10-2 FIG 3. INSTALLED ANGLE PER SRM 51-30-2.