As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE TO THE AFT LANDING GEAR FITTING (P/N: 350A21-4674.20) IN THE FORM OF A GOUGE / CHAFE. THE DAMAGE IS AT THE TWO HOLES OF THE TWIN CLEVIS, AND WAS MEASURED TO BE APPROXIMATELY 10.381MM (0.409”). THE BOLT HOLE IS ORIGINALLY 10JS13 MM (10.0MM (+/- 0.11)) DIAMETER (0.394” (+/-0.004”)).