What was found
INSPECTION FOUND A 2 INCH CRACK IN CIRCUMFERENTIAL BY INNER FLANGE ABOVE S25L AT BS 970. AN L-ANGLE AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN CIRCUMFERENTIAL BY INNER FLANGE ABOVE S25L AT BS 970. AN L-ANGLE AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)