As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE TRAILING LINK ASSEMBLY ON LEFT AND RIGHT MAIN LANDING GEAR HAD CORROSION AND PITTING PRESENT IN THE LIGHTENING BORE AT THE FORWARD OR UPPER END. PITTING IN AREAS WAS APPROXIMATELY .025. AFTER BLENDING AND REMAINING THICKNESS DETERMINED WITH UT THE PART WAS DETERMINED TO BE WITHIN LIMITS BY MFG. THE BORES WERE REQUIRED TO BE SHOT PEENED BEFORE RETURN TO SERVICE, (AND PAINTED).