What was found
AFTER REMOVAL OF THE NR 1 PYLON, THE DIAGONAL BRACE AFT ATTACHMENT ON FRONT SPAR HAS PITTING AND FRETTING CORROSION'S ON THE BUSHINGS. ACCOMPLISHED SB 767-57-053 HIGH INTERFERENCE FIT METHOD OF BUSHINGS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF THE NR 1 PYLON, THE DIAGONAL BRACE AFT ATTACHMENT ON FRONT SPAR HAS PITTING AND FRETTING CORROSION'S ON THE BUSHINGS. ACCOMPLISHED SB 767-57-053 HIGH INTERFERENCE FIT METHOD OF BUSHINGS.