What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT CIRCUMFERENTIAL FRAME AT BS 480 BETWEEN STRINGER 25R AND 26R. A FRAME SPLICE WAS INSTALLED AND FLOOR SUPPORT SPLICE WERE INSTALLED IAW SRM 53-10-4 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT CIRCUMFERENTIAL FRAME AT BS 480 BETWEEN STRINGER 25R AND 26R. A FRAME SPLICE WAS INSTALLED AND FLOOR SUPPORT SPLICE WERE INSTALLED IAW SRM 53-10-4 AND 51-30-2.