As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING OTBD FLAP INBD HINGE SIDE LOAD FITTING LOWER FASTENER HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER = 0.641 INCH, FINAL HOLE DIAMETER = 0.6455 INCH. MAXIMUM HOLE DIAMETER = 0.621 INCH. REPAIR ACCOMPLISHED AS PER EA 1-5750-162383 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.