What was found
LEFT NACELLE FLAP, UPPER SURFACE, INTERNAL STRINGER CRACKED, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW EMB 120 SRM 51-25-00, 51-12-02, 51-30-01, 51-40-02, 57-50-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT NACELLE FLAP, UPPER SURFACE, INTERNAL STRINGER CRACKED, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW EMB 120 SRM 51-25-00, 51-12-02, 51-30-01, 51-40-02, 57-50-02.