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Printed page 1. PDF page 1.
deformation was observed, all features consistent with intragranular fatigue; however, the root cause of the fatigue cracking could not be determined. Page 1 of 11Open final report at PDF page 1CEN25FA006: UAS Transervices Inc.: N130GP
Printed page 48. PDF page 64.
Moissy-Cramayel, France, to identify any cracks on the concave and convex sides of the fan blade roots. 82 (Blade No. 20 was examined on scene and was excluded from these additional inspections because that blade had been sectioned for SEMOpen official document at PDF page 64Left Engine Failure and Subsequent Depressurization: Southwest Airlines Flight 1380, Boeing 737-7H4, N772SW, Philadelphia, Pennsylvania, April 17, 2018
Printed page 74. PDF page 90.
blade mid-span fragments traveled forward of the fan case into the inlet, and the blade root and other fan blade mid-span fragments traveled aft within the fan case. Also, the fan case and the inlet containment shield remained intact, exhibitedOpen official document at PDF page 90Left Engine Failure and Subsequent Depressurization: Southwest Airlines Flight 1380, Boeing 737-7H4, N772SW, Philadelphia, Pennsylvania, April 17, 2018