What was found
CRACK ON AFT/UPPER CORNER BETWEEN BS 851 TO 870 AT LT RING PAN. PAN 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 AFT/UPPER CORNER BETWEEN BS 851 TO 870 AT LT RING PAN. PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.