What was found
(AUS) LEFT WING FORWARD MAIN SPAR CAP CONTAINED INTERGRANULAR CORROSION IN AREA ADJACENT TO THE INBOARD AND OUTBOARD EDGES OF THE ENGINE NACELLES. PART TOTAL CYCLES: 2,011.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) LEFT WING FORWARD MAIN SPAR CAP CONTAINED INTERGRANULAR CORROSION IN AREA ADJACENT TO THE INBOARD AND OUTBOARD EDGES OF THE ENGINE NACELLES. PART TOTAL CYCLES: 2,011.