As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER NOTING A HYDRAULIC LEAK BY THE RT MAIN GEAR WHEEL WELL, FOUND ALUMINUM HYDRAULIC LINE FOR THE FLAP RETURN SYSTEM WEEPING FROM A CORROSION PIN HOLE. THE PIN HOLE IS APPROXIMATELY 1 INCH FROM END OF LINE AND IN THE MIDDLE OF A 90 DEGREE BEND. THE LINE IS DATED 1-30-81, AND LOOKS TO BE ORIGINAL. THE LINE IS PAINTED WITH ZINC CHROMATE INCLUDING THE AREA WITH THE PIN HOLE. NEW LINE WAS INSTALLED.