What was found
DURING OVERNIGHT CHECK, IT WAS DETECTED THE LEFT ENGINE ACOUSTIC PANEL DAMAGED. MAINTENANCE PERSONNEL PERFORMED INSPECTION ON THE LEFT ENGINE ACOUSTIC PANEL, DETECTING A CRACK OF 0.500” LENGTH LOCATED AT 01:00 HOUR POSITION AND AT 13.00” FROM REAR EDGE ON INNER BARREL ACOUSTIC PANEL OUT OF LIMITS IAW SRM 54-10-01-1A-1, PARAGRAPH 4C(1)(B) AND THE TAP TEST AND DETAIL VISUAL INSPECTIONS WERE PERFORMED IAW B737 NDTM PART 1 51-05-01, THE DAMAGED AREA WAS DELIMITED AND THE LEFT ENGINE INNER BARREL ACOUSTIC PANEL WAS REPAIRED IAW SRM 54-10-01-2R, ALL CORRECT.