What was found
DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, LT OVERWING SKIN AT WBL 128.45 HAS A 4 X 4 AREA OF CORROSION 2 FT FWD OF MID SPAR. REMOVED CORROSION IAW B747 SRM 51-10-1. ULTRASONIC THICKNESS CHECK, MINIMUM NOMINAL THICKNESS AT WING SKIN EDGE .195 TO .230 IN 2.5 BY 3 AREA APPROX. REMOVED AND REPLACED BOLTS IAW B747 51-30-02 AND 51-30-04. REWORKED IAW EA B4-57-021. CORROSION TASK CARD NUMBER C53-190-01 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 12599.