What was found
CRACK ON FWD, UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775. ON FWD/UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FWD, UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775. ON FWD/UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.