What was found
CRACKED RING PAN BETWEEN BS 237 - 256 AT UPPER, FWD CORNER AREA. RING PAN BETWEEN BS 237-256 WAS REPAIRED IAW SRM 56-20-02, FIG 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED RING PAN BETWEEN BS 237 - 256 AT UPPER, FWD CORNER AREA. RING PAN BETWEEN BS 237-256 WAS REPAIRED IAW SRM 56-20-02, FIG 202.