What was found
CRACKED FWD LOWER CORNER OF RT RING PAN STA Y=1117-1136 AT INTERNAL FUSELAGE STRUCTURE. RING PAN FWD LOWER CORNER DAMAGE WAS REPAIRED WITH SRM 53-05, FIG 112 AND ERA 493648-14MA, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED FWD LOWER CORNER OF RT RING PAN STA Y=1117-1136 AT INTERNAL FUSELAGE STRUCTURE. RING PAN FWD LOWER CORNER DAMAGE WAS REPAIRED WITH SRM 53-05, FIG 112 AND ERA 493648-14MA, REV ORIGINAL.