As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ONE CRACK FOUND ON LEFT FUSELAGE INTERNAL STRUCTURE FROM FRAME 2 TO 4 WINDSHIELD FRAME LOWER SECTION AT FASTENER HOLE NR 10 AFT SIDE DURING EDDY CURRENT ROTATING PROBE TEST PER NTM53-11-01. LEFT FUSELAGE INTERNAL STRUCTURE FROM FRAME 2 TO 4 WINDSHIELD FRAME LOWER SECTION AT FASTENER HOLE NR 10 REPAIRED AS PER E.A. 6-5310-150316 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.