What was found
BLENDED 10 AREAS OF CORROSION ON THE LT UPPER WING SKIN, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTION, PREPPED AND TREATED AREAS IAW SRM 51-10-03, AND MM 51-10-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BLENDED 10 AREAS OF CORROSION ON THE LT UPPER WING SKIN, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTION, PREPPED AND TREATED AREAS IAW SRM 51-10-03, AND MM 51-10-00.