What was found
INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF STRINGER 17R INNER FLANGE AT B.S. 1342. THE STRINGER TIE WAS REMOVED AND THE CRACK WAS STOP DRILLED. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND MM 51-20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF STRINGER 17R INNER FLANGE AT B.S. 1342. THE STRINGER TIE WAS REMOVED AND THE CRACK WAS STOP DRILLED. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND MM 51-20.