What was found
CRACK IN AFT SIDE OF AFT PRESSURE BULKHEAD SKIN ON RT SIDE OF VENTRAL DOOR JAMB. REMOVED AND REPLACED REPAIR IAW SRM 53-05 FIG 76.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN AFT SIDE OF AFT PRESSURE BULKHEAD SKIN ON RT SIDE OF VENTRAL DOOR JAMB. REMOVED AND REPLACED REPAIR IAW SRM 53-05 FIG 76.