What was found
CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 351-370 RT AT PASSENGER CABIN. FASTENERS AND DAMAGE WERE REMOVED REPAIR PARTS WERE FABRICATED. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 351-370 RT AT PASSENGER CABIN. FASTENERS AND DAMAGE WERE REMOVED REPAIR PARTS WERE FABRICATED. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.