What was found
INSPECTION FOUND A 2 INCH CRACK IN LONGERON 2L AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, SHEET 1, 51-30-2, AND 51-30-5.
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 2L AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, SHEET 1, 51-30-2, AND 51-30-5.