As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) FOUND CRACK ON ENGINE SUPPORT BEAM WHILE PERFORMING SB A601R-53-059. FOUND CRACKS ON UPPER WEB AT LBL 8 FROM THE FASTENER TO THE AFT EDGE. RBL 8 (1.5 INCHES LONG) AND LOWER WEB EXTENDING FROM EACH ACCESS PANELS CUTOUTS R/H INBOARD FORWARD RADIUS 0.25 INCHES LONG. LT INBOARD FORWARD RADIUS 1.75 INCHES LONG.