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Explore Everyone Says This Engine Exploded. The NTSB Says It Worked. with 1,335 views, 16 likes, and 1 comments. Experience the impact of this video content that has captured audience attention.

On April 17, 2018, a fan blade broke off inside the left engine of Southwest 1380. Everyone remembers it as the engine that exploded. The NTSB found the opposite: the fan case never let a single fragment through. It "performed as designed." What hit the airplane came from outside the case — and one of those pieces struck the fuselage right next to a cabin window held in place by ten spring clips. ━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━ PRIMARY SOURCE NTSB/AAR-19/03 — "Left Engine Failure and Subsequent Depressurization, Southwest Airlines Flight 1380, Boeing 737-7H4, N772SW, Philadelphia, Pennsylvania, April 17, 2018" Adopted November 19, 2019. https://www.ntsb.gov/investigations/AccidentReports/Reports/AAR1903.pdf p. 90 — Probable cause: a low-cycle fatigue crack in the dovetail of fan blade No. 13 p. 74 — "the fan case and the inlet containment shield remained intact, exhibited no pass-through penetrations, and performed as designed" p. 60 — No through-hole penetrations. Maximum crack depth 0.695 in. 15,000 striation cycles p. ix — Impact damage and witness marks on the fuselage consistent with the inboard fan cowl aft latch keeper. 15 blade cracks found on separate engines as of August 2019 p. 40 — Seat 14A. Window 10 1/2 x 14 3/8 in. Ten spring clips around the window frame NTSB Board Meeting Synopsis, November 19, 2019 — recommendations to the FAA to redesign the 737NG fan cowl structure, fit it to new production aircraft, and retrofit the existing fleet. https://www.ntsb.gov/news/events/Documents/2019-DCA18MA142-BMG-abstract.pdf ━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━ NOTES - 144 passengers and 5 crew on board. One fatality, eight minor injuries. - The report does not say an inspection missed this crack. It states only that the fan blade set was processed according to the repair instructions and passed the final quality check at the October 2012 overhaul (p. 14). We do not claim more than that. - The cabin lost pressure by two paths: inlet fragments punctured the fuselage skin, and the departing window caused the rapid depressurization (p. 60, p. 90). - Safety recommendation numbers are not shown on screen. The synopsis we cite uses placeholders and we could not verify the final A-19 numbers. ━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━ HOW THIS WAS MADE Background footage: AI-generated. All figures, dimensions and citations: original work. Every number on screen comes from the pages listed above. Corrections go in the pinned comment within 48 hours. #aviation #engineering #ntsb

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