As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF RT INBD FLAP ASSEMBLY, NOTICED DAMAGE TO INBD HINGE ARM & BOX ATTACHMENT POINT. REPLACED RT INBD FLAP HINGE FITTING YOKE, IAW STEPS 1 - 5 FOR WORK PERFORMED IAW REO 601R-57-52-2105, REF PWI D538479 FOR DTA REQUIREMENTS.