What was found
INSPECTION FOUND A .75 INCH CRACK IN LEFT MAIN GEAR AFT SECTION OF WHEEL WELL RING ASSEMBLY CHORD. THE RING ASSEMBLY LOWER 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 .75 INCH CRACK IN LEFT MAIN GEAR AFT SECTION OF WHEEL WELL RING ASSEMBLY CHORD. THE RING ASSEMBLY LOWER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.