What was found
CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 655-674, RT AT CABIN PASSENGER DAMAGE AND FASTENER WERE REMOVED IAW SRM 53-05, FIG 122 AND 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 655-674, RT AT CABIN PASSENGER DAMAGE AND FASTENER WERE REMOVED IAW SRM 53-05, FIG 122 AND 51-30-2.