What was found
NR 1 ENGINE PYLON FWD ENGINE MOUNT FITTING HAS CORROSION ON MOUNTING FACE AND AROUND MOUNTING HOLES UPPER SIDE. REMOVED CORROSION FROM MOUNT FACE IAW A310-200 SRM 51-74-10, FOUND TO BE WITHIN LIMITS A310-200 SRM 54-51-81 FIG 104. SPOT-FACED UPPER AFT I/B & O/B HOLES IAW A310-200 SRM 51-11-80. FOUND AFT O/B HOLE TO BE WITHIN LIMITS IAW A310-200 SRM 54-51-81 FIG 104 SHT 1. FOUND AFT I/B HOLE BEYOND LIMITS A310-200 SRM 54-51-81 FIG 104 SHT 1. AFT I/B HOLE IS ACCEPTABLE IAW FEDEX EA 6-5450-85609 AND AIRBUS INTERIM RAS 034934/010/2005. PERFORMED DYE PENETRANT INSPECTION IAW A310-200 NDT 51-91-00. NO CRACKS NOTED. APPLIED CADMIUM PLATING AND HI-TEMP PLATING IAW A310-200 SRM 51-75-10.