What was found
DURING 'H' CHECK, FOUND CORROSION IN THE NR 2 ENGINE AFT MOUNT FITTING, AFT FLANGE. REPLACED FITTING PER SRM 54-40-1, PG.1-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 'H' CHECK, FOUND CORROSION IN THE NR 2 ENGINE AFT MOUNT FITTING, AFT FLANGE. REPLACED FITTING PER SRM 54-40-1, PG.1-2.