What was found
INSPECTION FOUND A .5 INCH CRACK IN STIFFENER BETWEEN STRINGER 10L AND 11L AT FS 295. THE CRACKED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN STIFFENER BETWEEN STRINGER 10L AND 11L AT FS 295. THE CRACKED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-10-2.