What was found
C-CHECK, 2 INCH CRACK ON I/B UPPER ANGLE ON LEADING EDGE INT OF I/B FRAME AT WS 185.5 RT WING OF PYLON. REMOVED, FABRICATED, HEAT TREATED TO T3 COND, ALODINED AND REPLACED RIB IAW SRM 57-20-2 AND 57-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-CHECK, 2 INCH CRACK ON I/B UPPER ANGLE ON LEADING EDGE INT OF I/B FRAME AT WS 185.5 RT WING OF PYLON. REMOVED, FABRICATED, HEAT TREATED TO T3 COND, ALODINED AND REPLACED RIB IAW SRM 57-20-2 AND 57-30-2.