What was found
CRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927. ON FWD / LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927 WAS REPAIRED IAW SRM 50-20-02, REPAIR 1, FIG 202, CRACK LENGTH 0.198".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927. ON FWD / LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927 WAS REPAIRED IAW SRM 50-20-02, REPAIR 1, FIG 202, CRACK LENGTH 0.198".