What was found
CRACK ON RING PAN, FWD UPPER CORNER, BS 351 AND BS 88. RING PAN WERE REMOVED AND REPAIRED IAW IAW SRM 53-05, FIG 122.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RING PAN, FWD UPPER CORNER, BS 351 AND BS 88. RING PAN WERE REMOVED AND REPAIRED IAW IAW SRM 53-05, FIG 122.