What was found
RT ENGINE STRUT INBOARD SKIN CRACKED FROM UPPER AFT RADIUS OF 442AL ACCESS PANEL CUTOUT AND THROUGH RIVET HOLE. CRACK CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 58.4MM (2.3IN). CRACK ALSO EXISTS IN INTERNAL DOUBLER AS WELL.
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 AND THROUGH RIVET HOLE. CRACK CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 58.4MM (2.3IN). CRACK ALSO EXISTS IN INTERNAL DOUBLER AS WELL.