As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT MLG FITTING CORRODED ON UPPER SURFACE OF LWR RETRACT ACT ATTACHMENT. REMOVED CORROSION BY LOCAL BLEND, .020 DEEP. REMOVED CORROSION PER SRM 57-14-00, HFEC PER SRM 54-14-00 PG 809. ROTO PEENED PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED.