What was found
FOUND CORROSION. PERFORMED A STRINGER REPAIR AT BUTT LINE 0.00, FUSELAGE FLIGHT STATION 320-333 FOR A FLANGE BELOW .063 LIMIT. THIS REPAIR WAS MADE IN ACCORDANCE WITH CESSNA'S 550 STRUCTURAL REPAIR MANUAL 53-12-04. THE "BEFORE" ULTRASONIC INSPECTION OF THE DAMAGED PIECES WAS PERFORMED BY APPLIED TECHNICAL SERVICES. AFTER THE DAMAGED PIECES WERE CLEANED OF CORROSION, THE "AFTER" ULTRASONIC INSPECTION OF THE DAMAGED PIECES WAS PERFORMED BY APPLIED TECHNICAL SERVICES.