What was found
THE RT FUSELAGE TO DORSAL FIN ATTACH ANGLE WAS CUT AT STA 1520, COMPLETELY SEVERED. OEM APPROVED REPAIR AS PERMANENT, ERA 518618-14. REQUIRES GVI AT 3000 CYCLES OR CHECK THRESHOLD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE RT FUSELAGE TO DORSAL FIN ATTACH ANGLE WAS CUT AT STA 1520, COMPLETELY SEVERED. OEM APPROVED REPAIR AS PERMANENT, ERA 518618-14. REQUIRES GVI AT 3000 CYCLES OR CHECK THRESHOLD.