What was found
INSPECTION FOUND A .375 INCH CRACK WITH CORROSION IN FRAME 560 TO SKIN ATTACH FLANGE, BBL 0 TO LBL 6. THE CORRODED AREA OF FLANGE WAS CUT OFF IAW SRM 53-10-4. A NEW FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .375 INCH CRACK WITH CORROSION IN FRAME 560 TO SKIN ATTACH FLANGE, BBL 0 TO LBL 6. THE CORRODED AREA OF FLANGE WAS CUT OFF IAW SRM 53-10-4. A NEW FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.