What was found
INSPECTION FOUND A 2 INCH CRACK IN LONGERON 27L AT FS 256. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SPLICE AND LONGERON WERE INSTALLED IAW SRM 53-14-02, FIGURE 3, 53-02, FIGURE 18, 51-30-02, AND 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN LONGERON 27L AT FS 256. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SPLICE AND LONGERON WERE INSTALLED IAW SRM 53-14-02, FIGURE 3, 53-02, FIGURE 18, 51-30-02, AND 51-30-05.