As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE ACCOMPLISHING NON DESTRUCTIVE TEST HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, HOLE A AT TEE CAP (NCA6042-15) FOUND WITH CRACKED. CRACK AT TEE CAP (NCA6042-15) HOLE A REPAIRED AS PER EA # 1-5330-T0385040 PART 1 TITLE: FUSELAGE - PLATES & SKINS - ACA3354 FUSELAGE SKIN REPAIR AT FORWARD CORNER FOR NOSE LANDING GEAR DOOR CUTOUT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00569 FOR WORK DETAILS.