What was found
CRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 617 TO 636. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR, FIG 202.
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 617 TO 636. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR, FIG 202.