What was found
INNER CHORD ANGLE AT BOTTOM OF FRAME 616R AT S17R HAS CRACK. REMOVED & INSTALLED DOUBLER PER TR 53-62-01, DEFECT SIZE: .750 INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INNER CHORD ANGLE AT BOTTOM OF FRAME 616R AT S17R HAS CRACK. REMOVED & INSTALLED DOUBLER PER TR 53-62-01, DEFECT SIZE: .750 INCH.