What was found
DURING WALKAROUND INSP, MX FOUND DAMAGE TO THE NR 2 ENG INLET COWL OUTER BARREL SKIN CRACK/DAMAGE (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEAT INSPECTIONS AT EVERY 25 FC AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 FH (FLIGHT HOURS) AFTER PART 1. ACCOMPLISH REPAIR TO THE NR 2 ENGINE INLET COWL OUTER BARREL SKIN CRACK/DAMAGE (REF FIG 1) AS FOLLOWS: 1 . STOP DRILL CRACK IAW SRM 51-10-01. 2 . APPLY 3 LAYERS OF ALUMINUM FOIL TAPE (SPEED TAPE) COVERING THE DAMAGED AREA ENSURING THAT EVERY LAYER OVERLAPS A MINIMUM OF 1.5 INCHES IAW LAYER 3.