As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE PERFORMING THE VISUAL INSPECTION OF THE RT PYLON IAW MM, TASK 000-54-420-500. A CRACK WAS DETECTED ON THE FORWARD ENGINE MOUNT SPAR. THE CRACK WAS FOUND ON THE AFT FACE OF THE SPAR AT FUSELAGE BS FS 625.30 APPROXIMATELY 2" INBD OF THE FUSELAGE SKIN. THE CRACK MEASURES APPROXIMATELY 0.375" AND WAS CONFIRMED WITH LIQUID PENETRANT INSPECTION.