I've done a little research to refresh my memory of this phenomenon. As I recall, the BAC One Eleven was being tested at a rearward CoG. Once it had entered the "deep stall" condition it seems obvious that a highly skilled & experienced test pilot like Mike Lithgow & crew would have tried everything in their power to recover from it, including a wide variety of power settings & control inputs plus deploying the anti-spin parachute carried during this sort of testing. It seems likely that the aircraft ended up in a 'flat spin' from which recovery turned out to be impossible.
It's also worth considering that AoA is measured from the relative wind OTTOL mentioned & not necessarily from the horizontal as is shown in most textbooks
Welp...let me rephrase that with a little more emphasis on some key words.Fatal TU154 crash August 2006[/url]
Three previous fatal accidents with the same type of aircraft have been attributed to the "deep stall".
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You are correct. This is a recent "deep stall", jet accident. I think that a forty year old design that was "a bad knock-off of a mediocre design" (even back in 68', when it was new) is a weak example though...... very few, if any modern jets fall victim to stall related accidents during normal operations and day-to-day flying........
Welp...let me rephrase that with a little more emphasis on some key words.Fatal TU154 crash August 2006[/url]
Three previous fatal accidents with the same type of aircraft have been attributed to the "deep stall".
.You are correct. This is a recent "deep stall", jet accident. I think that a forty year old design that was "a bad knock-off of a mediocre design" (even back in 68', when it was new) is a weak example though...... very few, if any modern jets fall victim to stall related accidents during normal operations and day-to-day flying........
Although I sympathize with and respect your personal experience regarding the early designs, these examples are dated and IMO don't have a real bearing on the bulk of the current airline fleet today.
Oddly enough, the best example that I could find of this was this one that chornedsnorkack eluded to. http://www.airdisaster.com/news/0106/22/news.shtml Quote:The interim report contained a wealth of details from the plane's flight data recorder and cockpit voice recorder, showing that the crew was incorrect in saying that the plane had experienced a "dual engine flameout," and that the crew took the opposite action to recover from an aircraft stall than action that is taught to every beginner pilot. That suggests that the crew did not recognize that the plane was, in effect, stalling.
They still manufacture the Ural motorcycle (a bad rip-off of a late 30's BMW design) over there. Sure, the Ural may still get you to work (most of the time) but it's far from a good example of a motorcycle by which current bikes can be measured. This is just another example of the previously mentioned point. Economics drives the production of the Ural (zero development, tooling and employee training costs) in the same manner that it drove the production of the Tupolev.Although it's an old design, production of the Tu 154 ended in 2006 according to Wikipedia so that makes it a current type in my book. The Tu 134 is still very popular & many are still in regular service. http://www.tupolev.ru/English/Show.asp?SectionID=144
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The latest data from the MAK (Interstate Aviation Committee) reports that Flight 612 had step-climbed to 12,400 m (41,000ft). Maximum allowed weight at 12,100 m is 85t for the TU154. Take-off weight must have been around 93.5t, given the distance from Anapa to St. Petersburg and with 160 passengers. This would mean a weight of about 88t at the time of the crash .
The thunderstorm was reported as having been a heavy one, reaching up to 12-15 km. It looked like the aircraft had stalled and entered a flat spin when it encountered turbulence at a low indicated airspeed (IAS), because it was way too high up for its weight. This was confirmed two weeks later in a statement by the Ukrainian Attorney General.
A plane with zero forward airspeed still cannot drop out of the sky at any high speed.
What would you define as "any high speed"?
Look, I'm not looking for an argument here. And although I appreciate the Kudos, I don't need my ego padded either. The reason I argue my point so vehemently is that I hate to see a false idea or rumor perpetuated. Airplanes don't just fall out of the sky. The crew usually has to do something terribly wrong to create these circumstances. And any modern, high-performance airplane can fall victim to crew complacency. The fact of the matter is; all too often an aircraft is given an undeserved "bad rap."
I agree that a lot of these accidents are due to pilot error & most likely caused either by complacency or inadequate training.
I have no wish to appear patronising or to cause offence. I happen to find this subject interesting & I'm simply expressing my opinion. If you call that argument so be it. I call it discussion.
What worries me is that the stall doesn't seem to be fully understood by a large number of pilots flying regularly today. I think this is demonstrated by some of the comments in this thread & other similar topics. I'm not convinced that some instructors understand it themselves. This brings into question the basic training methods used by flying schools.
Being that, as far as I know, I'm the only CFI posting in this (and other) threads... and for my learning's sake, as well as the sake of challenging specifics ... I'm compelled to ask, "What exactly do you mean ?"
If you want to get into a real mental wrestling mach; let's start a new thread about lift. You would be surprised (maybe not) at how misunderstood that one is. ....by the majority of the aviation community!!
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