What was found
INSPECTION C-CHECK, RT VERTICAL FIN SPAR CHORD IS CORRODED BEYOND LIMITS AT FIN STA 22.5. CUT OUT DAMAGE ON CHORD AND REPAIRED IAW BOEING DWG 65-68408 AND SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION C-CHECK, RT VERTICAL FIN SPAR CHORD IS CORRODED BEYOND LIMITS AT FIN STA 22.5. CUT OUT DAMAGE ON CHORD AND REPAIRED IAW BOEING DWG 65-68408 AND SRM 51-30-2.