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Printed page 28. PDF page 44.
inlet damage, a redesign of the inlet was not necessary and additional inlet testing was not required because (1) the inlet remained attached to the engine; (2) the inlet withstood the initial FBO impact, the surge pressure loads, and theOpen official document at PDF page 44Left Engine Failure and Subsequent Depressurization: Southwest Airlines Flight 1380, Boeing 737-7H4, N772SW, Philadelphia, Pennsylvania, April 17, 2018
Printed page 73. PDF page 89.
the SB. As a result, an ultrasonic inspection of the fan blades on the accident engine was not required to be performed. In addition, at the time of the PHL accident, the fan blades had accumulated 10,712 cycles since theirOpen official document at PDF page 89Left Engine Failure and Subsequent Depressurization: Southwest Airlines Flight 1380, Boeing 737-7H4, N772SW, Philadelphia, Pennsylvania, April 17, 2018