What was found
UPON PYLON REMOVAL FOUND CORROSION DAMAGE IN THE BUSHING COMMON TO LT WING FRONT SPAR OUTBD AND INBD PITCH LOAD FITTING, BOTH FITTINGS BORE DIAMETER EXCEED PRODUCTION LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON PYLON REMOVAL FOUND CORROSION DAMAGE IN THE BUSHING COMMON TO LT WING FRONT SPAR OUTBD AND INBD PITCH LOAD FITTING, BOTH FITTINGS BORE DIAMETER EXCEED PRODUCTION LIMITS.