What was found
DURING C-CHECK, FOUND CRACK IN ATTACH ANGLE COMMON TO CLOSE-OUT WEB IN FORWARD ENTRY DOORWAY, AFT END OF FUSELAGE CUT-OUT. REMOVED AND REPLACED DAMAGED ANGLE IAW SRM 51-20-02. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND CRACK IN ATTACH ANGLE COMMON TO CLOSE-OUT WEB IN FORWARD ENTRY DOORWAY, AFT END OF FUSELAGE CUT-OUT. REMOVED AND REPLACED DAMAGED ANGLE IAW SRM 51-20-02. (X)