What was found
LEFT WING LEADING EDGE, INBOARD ATTACH ANGLE, ON FRONT SPAR IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-41-02 AND 51-41-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING LEADING EDGE, INBOARD ATTACH ANGLE, ON FRONT SPAR IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-41-02 AND 51-41-04.