What was found
CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 769-788 RT AT CABIN PAX. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5, 51-30-2.
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 769-788 RT AT CABIN PAX. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5, 51-30-2.