What was found
RT ENGINE STRUT INBOARD SKIN CRACKED FROM UPPER AFT RADIUS OF 442AL ACCESS PANEL CUTOUT THROUGH RIVET HOLE. CRACK IS LOCATED IN INTERNAL DOUBLER AS WELL. CRACK WAS CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 63.5MM (2.5IN).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT ENGINE STRUT INBOARD SKIN CRACKED FROM UPPER AFT RADIUS OF 442AL ACCESS PANEL CUTOUT THROUGH RIVET HOLE. CRACK IS LOCATED IN INTERNAL DOUBLER AS WELL. CRACK WAS CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 63.5MM (2.5IN).