What was found
TWO STIFFENERS DAMAGED AT UPPER ATTACH POINTS COMMON TO I/B PYLON RIB & LEADING EDGE SKIN. REPLACED DAMAGED STIFFENERS PER SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO STIFFENERS DAMAGED AT UPPER ATTACH POINTS COMMON TO I/B PYLON RIB & LEADING EDGE SKIN. REPLACED DAMAGED STIFFENERS PER SRM 51-40-02.