What was found
CLT - FOUND CORROSION ON CLEVIS LUG .019 INCH BY 2 INCH, LEFT HORIZONTAL CENTER, UP REAR SPAR AFT LUG, AFT FACE. SPOT FACED AFFECTED AREA AND INSTALLED NEW BUSHINGS PER EA NR 85229. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - FOUND CORROSION ON CLEVIS LUG .019 INCH BY 2 INCH, LEFT HORIZONTAL CENTER, UP REAR SPAR AFT LUG, AFT FACE. SPOT FACED AFFECTED AREA AND INSTALLED NEW BUSHINGS PER EA NR 85229. (M)