What was found
PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LEFT SIDE UPPER FWD FUSELAGE SKIN BETWEEN FRAMES 0 TO 1 AND JUST FORWARD OF THE CAPTAINS WINDSHIELD MEASURES 9.5 INCHES BY 11.6 INCHES WITH A SKIN CUTOUT MEASURING 6.7 INCH BY 5.6 INCH REPAIR NOT IAW SRM REQUIREMENTS DUE TO LEVEL 1 SURFACE CORROSION FOUND ON REPAIR. REMOVED LEVEL 1 CORROSION BY HAND WITH NEGLIGIBLE MATERIAL LOSS AND RESTORED PROTECTIVE COATING IAW A310-200 SRM 53-12-12 FIG 201 SHEET 1, SRM 51-74-10, AND SRM 51-72-10. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION.