What was found
CORROSION ON AFT VENTRAL DOOR LOWER FRAME X=9. DUE TO EXCESSIVE DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 34.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON AFT VENTRAL DOOR LOWER FRAME X=9. DUE TO EXCESSIVE DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 34.