What was found
DURING 4C+12A CHECK, EGAT MECHANIC FOUND CRACK ON NR 2 ENGINE INLET COWL INNER SKIN AT 6 O'CLOCK POSITION 1EA, 7 O'CLOCK POSITION 4EA, 8 O'CLOCK POSITION 3EA, 10 O'CLOCK POSITION 1EA, 11 O'CLOCK POSITION 2EA AND 12 O'CLOCK POSITION 1EA. [SUP 05-02-07] REPAIRED NR 2 ENGINE INLET COWL LIP INNER SURFACE CRACK AREA PER EGAT ENGINEERING INSTRUCTION NR 2007P20A-016 REV 00 & W2007A54B-207 REV.00 & HEAT TREATMENT 22/9-0 TO 22/9-T6 PER IE ATTACHMENT SHEET NR 0028588.