What was found
CRACK ON RT RING PAN AFT UPPER CORNER STA Y=484-503 FUSELAGE STRUCTURE. RING PAN AFT UPPER CORNER ON STA Y=484 TO 503 WAS 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 RT RING PAN AFT UPPER CORNER STA Y=484-503 FUSELAGE STRUCTURE. RING PAN AFT UPPER CORNER ON STA Y=484 TO 503 WAS REPAIRED IAW SRM 53-05, FIG 122.