What was found
INSPECTION FOUND A .75 INCH CRACK IN LONGERON 17L AT STA 256 BELTFRAME ATTACHMENT. A LONGERON AND LONGERON SPLICE 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 .75 INCH CRACK IN LONGERON 17L AT STA 256 BELTFRAME ATTACHMENT. A LONGERON AND LONGERON SPLICE WERE INSTALLED IAW SRM 53-02, FIGURE 18.