What was found
FOUND CORROSION L6 CLEVIS AFT FACE. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CORROSION L6 CLEVIS AFT FACE. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION.