What was found
FOUND INDICATION OF CRACK DURING REAR PRESSURE BULKHEAD INSPECTION. CRACK INDICATION IS AT THE LINTEL FITTING REF: NDTM PART 6 53-61-153 PG 8 & 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND INDICATION OF CRACK DURING REAR PRESSURE BULKHEAD INSPECTION. CRACK INDICATION IS AT THE LINTEL FITTING REF: NDTM PART 6 53-61-153 PG 8 & 9.