What was found
INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT BS 804.5, S15R. THE CRACKED AREA WAS REMOVED, A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT BS 804.5, S15R. THE CRACKED AREA WAS REMOVED, A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3.