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Couple of quick TW-5 questions

It's been a few years now, but wasn't that part of the prop sleeve impact fix?
 
Interesting. I wonder what causes the stress (different aerodynamics from the airframe, bigger prop/more blades, etc).

Something to do with stress on the prop blade with the prop's AOA during a stall/spin and air density below 10,000ft coupled with the prop tip breaking the sound barrier results in stress and vibration that might break the blade.
 
Doubt it. We spin with the PCL at idle. The PMU actually speeds up the blades to maintain the 80% Np (its usually around 48% at idle).
 
Interesting. I wonder what causes the stress (different aerodynamics from the airframe, bigger prop/more blades, etc).

Additionally, while not prop related...the book says 2-3 turns per second at 4-500' lost per turn. In a full spin, that's 10k/min descent rate. Never heard it mentioned, but staying above 10k keeps you in the "minute to live" window.
 
Additionally, while not prop related...the book says 2-3 turns per second at 4-500' lost per turn. In a full spin, that's 10k/min descent rate. Never heard it mentioned, but staying above 10k keeps you in the "minute to live" window.

I don't remember what the foot/rev was in the T-34, but it had a 7K-9K FPM spin rate, so you were always inside the minute to live envelope during Fams. High spins/spirals (which the studs didn't do) I was more concerned with, especially with multiple cases of guys not getting out of a progressive spin right away and getting read to blow the canopy (or worse, in Corpus).
 
I didn't figure it was that big of a concern and that the T-34 was probably pretty similar.
 
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