As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION REQUIREMENTS OF DOCUMENT 18, TASK 54-51-00-210 REVEALED RT ENGINE PYLON FIREWALL BOX ASSEMBLY IS CRACKED ON THE FORWARD PART OF THE BOX FROM THE OUTBOARD EDGE TO THE INBOARD RADIUS OF THE FIREWALL BOX APPROX .750" IN LENGTH, P/N 6312204-65. SERVICE BULLETIN SB525A-54-01 HAS NOT BEEN INCORPORATED.