Chosen One said:
I was thinking it was due to fuel continuing to dump while the engine had stopped rotation (and noticing on the transcripts it took them quite a while to start the memory items (cont. ignition on), those thrust levers must have been up there the whole time). Did not realize it was due to vaporization.
Still not following what you are thinking, but remember that the engine fuel pump and fuel control unit are driven by the accessory gearbox, which is driven by the N2 compressor. It is alleged that the N2 stopped and froze into position due to differential cooling - hence there would not have been any rotation to the accessory gearbox.
I don't have the figures for the CF-34, but it would not surprise me if the fuel pressure on the outlet side of the engine fuel pump is in excess of 730 PSI to ensure atomization of the fuel at the nozzles and power the variable stators in the compressor section. The nozzles have a spring loaded valve that closes when there is insufficient fuel pressure ( to keep fuel from draining into the engine and potentially causing hot starts )
Differential cooling was also cited the 737 Rudder PCU investigations and the allegations were never proven to everyone's satisfaction. The conditions have to be very, very, extreeme for this to happen, or else these engines would be seizing at start and shutdown all the time. I would guess that the engine cools more rapidly at -40C at sea level than it does at ISA at FL410 due to air density.
What I strongly suspect is that air density had everything to do with this loss. Obviously the airplane can fly at FL410 all day, every day, if it is light enough and cool enough to get there
with sufficient speed.
Those big cowlings are there for a lot more reason than to shroud the fan. Those cowlings are huge turbochargers that are in effect the first stage of compression for the engine. The more air you shove in the engine, the more power it can produce ( and the higher the N1 carat )
And it is not so easy to accelerate up there. To go from 150 knots indicated to 250 KIAS is actually an increase of around 182 knots TAS. With no thrust, in the dark and the airplane depressurizing we are not talking cake.
I think ( and hope ) we will see the FAA be much more restrictive regarding green on green pairings. These guys did not know that this would get them in trouble. Putting Captains with less than 500 hours together with very experienced First Officers, or vice versa would procedurally stop anything like this from happening.
And even now, I fear som people are getting the wrong message on this. If you can stay on profile and go high in an RJ, fine. I've been to FL390 several times with weights over 47K and will do it again if the conditions make that the right place to be. But if you can't climb at at least 290KIAS or the greater of M.70/ 250 you have no business at that altitude.