What was found
#2 ENGINE, NICK FOUND ON LEADING EDGE OF FAN BLADE. GROUNDED - YES. PERFORMED FAN BLADE INSPECTION ON THE ENG #2, BLADE #3 DEPTH MEASUREMENT 0.0225 IN. PERMITTED UP TO 0.0137 IN PER B737-9 AMM 72-22-02-200-801-G00. THE NICK IS OUT OF LIMIT. STEP F(H). PERFORM FAN BLADE METAL LEADING EDGE BLENDING UP TO STEP G(6), PER AMM 72-22-02-900-805-G00. ACCOMPLISH FLO PEN ALTERNATE INSP PER STEP (7)(B)2 NO DISCONTINUITIES NOTED. THIS COMPLETES AMM 72-22-02-900-805-G00. TAP TEST STEP (9) WAS ACCOMP PER ASA PWRPL-72EA-24488. NO DISCONTINUITIES NOTED. NOTE: COMPLETED BLEND DEPTH MEASURED @ .077" MAX ALLOWED 0.120". COMPLETED ENGINE F.O.D. AND BIRDSTRIKE INSPECTION REF AMM 71-00-00-200-802-F00. IDLE LEAK CHECK COMPLETED, NO LEAKS DETECTED.