What was found
INSPECTION FOUND A 0.7 CRACK IN LONGERON 3L AT STA 160 AND A 0.6 CRACK IN LONGERON 4L AT STA 160. THE LONGERONS WERE REPLACED IAW SRM 53-02, FIGURE 18, 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 0.7 CRACK IN LONGERON 3L AT STA 160 AND A 0.6 CRACK IN LONGERON 4L AT STA 160. THE LONGERONS WERE REPLACED IAW SRM 53-02, FIGURE 18, 51-30-2 AND 51-30-5.