What was found
IN COMPLIANCE WITH AD 2018-26-01 AND SB CFM56-7B S/B 72-1033 REV 3. JAW PARA 3. F. (4)(C) - FAN BLADE #20 OF #1 ENGINE FOUND UNSERVICEABLE. REPEATABLE UT CRACK INDICATION AT CONVEX AREA OF DOVETAIL EXCEEDING 30%.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IN COMPLIANCE WITH AD 2018-26-01 AND SB CFM56-7B S/B 72-1033 REV 3. JAW PARA 3. F. (4)(C) - FAN BLADE #20 OF #1 ENGINE FOUND UNSERVICEABLE. REPEATABLE UT CRACK INDICATION AT CONVEX AREA OF DOVETAIL EXCEEDING 30%.