As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ENGINE BOX BEAM INSPECTION FOUND A 2" CRACK ON L/H LOWER SKIN ACCESS PANEL OUTBD OF LBL36.20 AND A 1.75" CRACK ON THE R/H LOWER SKIN ACCESS PANEL OUTBD OF RBL 36.20.PERFORMED A MAJOR REPAIR BETWEEN FS 625.30 AND 640.00 TO L/H AND R/H LOWER ENGINE SUPPORT BEAM AT LBL 36.20 AND RBL 36.20 BY REMOVING DAMAGED AREAS AND INSTALLING REPAIR PARTS I/A/W CANADAIR REO 601R-53-61-366 REV C.