As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 PYLON OTBD SIDE AT RIB 8 FWD SCEW HOLE HAS A 0.250 CRACK GOING UPWARDS. TRIMMED OUT CRACK AND REPAIRED PYLON NR 2 SIDE PANEL IAW SRM 54-51-31 FO\IG 201 PAGE 203 TO 207. THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVALS . THE INSP INSTRUCTION REF IS SRI54-51-31-2-001-00.