What was found
INSPECTION FOUND A .5 INCH CRACK AT FORWARD AND AFT CORNERS OF C-2 DOOR LOWER T-CHORD. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT FORWARD AND AFT CORNERS OF C-2 DOOR LOWER T-CHORD. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.