What was found
INSPECTION FOUND A 2 INCH CRACK AT UPPER POSITION OF NR 4 PYLON AFT BULKHEAD INBOARD CHORD. THE CHORD AND AFT BULKHEAD ASSEMBLY WERE REPLACED IAW SRM 57-10-01 AND SB 747-54A2159.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK AT UPPER POSITION OF NR 4 PYLON AFT BULKHEAD INBOARD CHORD. THE CHORD AND AFT BULKHEAD ASSEMBLY WERE REPLACED IAW SRM 57-10-01 AND SB 747-54A2159.