What was found
CRACKED INNER PAN BELOW STOP FITTING NR 2 AT MID CARGO COMPARTMENT DOOR. DAMAGE INNER PAN BELOW STOP FITTING WAS REWORKED AND MEASURED TRIM TO REMOVE DAMAGE: 0.236" LONG, IT IS WITHIN LIMITS IAW SRM 52-03D, FIG 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED INNER PAN BELOW STOP FITTING NR 2 AT MID CARGO COMPARTMENT DOOR. DAMAGE INNER PAN BELOW STOP FITTING WAS REWORKED AND MEASURED TRIM TO REMOVE DAMAGE: 0.236" LONG, IT IS WITHIN LIMITS IAW SRM 52-03D, FIG 10.