What was found
INSPECTION FOUND A .25 INCH CRACK IN LONGERON 4L AT STA 160. A LONGERON SPLICE REPAIR WAS 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 .25 INCH CRACK IN LONGERON 4L AT STA 160. A LONGERON SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18.