What was found
DURING A MAINTENANCE VISIT, FOUND A CRACK, EXTENDING FROM BOLT HOLE RT I/B FLAP I/B HINGE ATTACH FITTING AT XW 3.125. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. MACHINE REPAIRED FITTING AND INSTALLED IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO 99-024 AND DC8 SRM 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).