What was found
A CRACK WAS FOUND ON AFT VENTRAL DOOR UNDER UPPER HINGE FITTING. REPAIRED IAW SRM 51-30-2 AND 51-30-1, 51-10-3, PAR 14/21, 51-01, PAR 4 CAP 21 AND 52-05D, FIG 34.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A CRACK WAS FOUND ON AFT VENTRAL DOOR UNDER UPPER HINGE FITTING. REPAIRED IAW SRM 51-30-2 AND 51-30-1, 51-10-3, PAR 14/21, 51-01, PAR 4 CAP 21 AND 52-05D, FIG 34.