What was found
CRACK ON RING PAN, AFT UPPER CORNER, BS 1231 AND BS 1250. RING PAN REMOVED AND REPAIRED 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, AFT UPPER CORNER, BS 1231 AND BS 1250. RING PAN REMOVED AND REPAIRED IAW SRM 53-05, FIG 122.