What was found
(AUS) HYDRAULIC PIPE LOCATED IN THE LOWER FUSELAGE ADJACENT TO THE SPAR CONTAINED A CORROSION PIN HOLE IN THE AREA BELOW THE PIPE IDENTIFICATION TAG. PART TOTAL CYCLES: 19,729.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) HYDRAULIC PIPE LOCATED IN THE LOWER FUSELAGE ADJACENT TO THE SPAR CONTAINED A CORROSION PIN HOLE IN THE AREA BELOW THE PIPE IDENTIFICATION TAG. PART TOTAL CYCLES: 19,729.