Re:NTSB Preliminary Report – UPS Boeing MD-11F Crash [pdf]
by shtzvhdx on Thursday November 20, 2025 @03:47PM
(#45997484)
Aluminum has limited loading cycles
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Re:NTSB Preliminary Report – UPS Boeing MD-11F Crash [pdf]
by dreamcompiler on Thursday November 20, 2025 @05:08PM
(#45998504)
I'd be very surprised to read that the aft lug that cracked (and the bearing it contained) were made of aluminum. They were almost certainly steel or Inconel.
Re:NTSB Preliminary Report – UPS Boeing MD-11F Crash [pdf]
by CoastalCoder on Thursday November 20, 2025 @08:10PM
(#46000073)
Wouldn't that be true of all cast metals objects?
Or are some metals impervious?
Re:NTSB Preliminary Report – UPS Boeing MD-11F Crash [pdf]
by harshreality on Thursday November 20, 2025 @11:09PM
(#46001141)
No; roughly, yes. Based on the crystal structure of the metal, fatigue works differently.
> The fatigue limit or endurance limit is the stress level below which an infinite number of loading cycles can be applied to a material without causing fatigue failure.[1] Some metals such as ferrous alloys and titanium alloys have a distinct limit,[2] whereas others such as aluminium and copper do not and will eventually fail even from small stress amplitudes.
Re:NTSB Preliminary Report – UPS Boeing MD-11F Crash [pdf]
by hnuser123456 on Friday November 21, 2025 @11:58AM
(#46006235)
I know Veritasium gets posted here a lot, but a few days ago he posted a deep-dive into the the engineering of jet engine turbine blades. Turns out they're made from a single crystal of a superalloy that entangles itself at a molecular level such that it actually gains strength as it's heated, only losing strength above 1200 degrees C / 2200 degrees F. Below that temperature, as long as the strain on the part is below the plastic deformation threshold, it's not really losing any strength at all over time.