What was found
TPA - DURING EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK AT AFT ENTRY DOOR, UPPER HINGE CUTOUT FUSELAGE SKIN. REPAIRED PER SRM 53-30-03 FIG 21A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TPA - DURING EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK AT AFT ENTRY DOOR, UPPER HINGE CUTOUT FUSELAGE SKIN. REPAIRED PER SRM 53-30-03 FIG 21A. (M)