As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
POSSIBLE CRACK ON RT WHEEL WELL FORWARD BULKHEAD, NEAR THE TOP, IT IS LOCATED JUST ABOVE THE SPOILER HYD CONTROL VALVE. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED REPAIR IAW SRM 57-10-10-2R-3, REPAIR 3. REPAIR IS A CATEGORY B REPAIR. THRESHOLD IS AT 56.000 FLIGHT CYCLES. REPEAT INSPECTIONS ARE DUE AT 36.000 FLIGHT CYCLES BY HFEC IAW NDT PART 6 51-00-00 PROCEDURE 4 OR NDT PART 6 51-00-00 PROCEDURE 23 IAW SRM 57-10-10-2R, REPAIR 3, TABLE 203.