What was found
INSPECTION FOUND A .5 INCH CRACK IN LONGERON 16L AND A .5 INCH CRACK IN LONGERON 13R AT STA 965. THE CRACKED AREAS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-02, FIGURE 18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN LONGERON 16L AND A .5 INCH CRACK IN LONGERON 13R AT STA 965. THE CRACKED AREAS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-02, FIGURE 18.