What was found
INSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R AND 2L AT STA 1418. THE CRACKED SECTIONS OF LONGERON WERE REMOVED AND NEW SECTIONS WERE INSTALLED USING SPLICES IAW SRM 53-02, FIGURE 18 AND 51-10-3.
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 2R AND 2L AT STA 1418. THE CRACKED SECTIONS OF LONGERON WERE REMOVED AND NEW SECTIONS WERE INSTALLED USING SPLICES IAW SRM 53-02, FIGURE 18 AND 51-10-3.