Originally Posted by Capn Bloggs
(Post 6770877)
The purpose of washout (look at the outboard 1/4 of a 747 wing from the rear) is to prevent this entire-wing-stall-at-the-same-time. The entire wing won't stall "at the same time", surely?
My 'entire wing' thing was just an example of that. A deep stall can be induced on any aircraft with enough elevator authority or as a result of design. Recovery from a deep stall can be harder to achieve if the elevator then becomes less effective as per T-Tail aircraft or some other configuration. Considering that AF447 AoA was somewhere between 35 and 60 degrees you can surmise that the horizontal stabiliser also had a similar AoA, effectively the HS was also stalled. If they had made a large nose down input to attempt recovery that would have the effect of increasing the AoA of the HS past 60 degrees. Coupled with TOGA power I suspect the effect of the ND input would have been negligible. |
If they had made a large nose down input to attempt recovery that would have the effect of increasing the AoA of the HS past 60 degrees. Coupled with TOGA power I suspect the effect of the ND input would have been negligible. |
:eek:
The "then recover to flying speed..." part, though sounding good, appears to have at least the potential to be a bit problematical. |
Originally Posted by OK465
appears to have at least the potential to be a bit problematical.
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You are all ignoring the nose down pitch change that occurred each time nose down elevator was applied?
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BOAC indeed +1
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Was there a significant trend of AOA reduction with the pitch changes?
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Have you actually looked at the FDR trace? Tell me what you think.
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Nose drop with back stick is a classic stall indication taught at the PPL stage.
I don't think Flap 1 is used for stall recovery. It is, I believe, in the QRH POST stall recovery. However, if nothing else is working, most pilots would (I hope) try lots of things including gear down. |
And at no time did the AOA get below 35, but this of course may be a matter of magnitude & duration of ND inputs. I wish I knew. |
Very true, and as AZR stated, we don't 'ACTUALLY' know the effect of a positive ND SS input, because they never got there.
It is one possibility that a stall recovery could have been achieved, but not a certainty. I would prefer to see the final report rather than make assumptions, regardless of how well founded they seem to be from experience with previous or other aircraft flown. |
Clandestno.....fantastic post:
Well, we're out of prejudices here as it happened to long established western flag carrier. Most of the posters feel that it struck close to home and they can not write it off easily as something-that-can't-happen-to-me. Mental gymnastic they perform to deal with their shock and horror is very interesting thing to behold but its results are not particularly informative. I have been reading the AF447 threads since day one and have absorbed every conceivable scenario pointing towards some sort of aircraft malfunction. This obviously would have been an easier way for people to digest and understand what had happened. But from what we know so far...it seems two qualified pilots became disorientated, didn't correctly address the situation, and foundered without fully understanding they were in a stall.... That is hard to deal with, and adds to the depth of the dilemma of trying to comprehend this disaster. This is everybody's nightmare: pilots, passengers, manufacturers, airline companies....and it isn't going away... |
This is everybody's nightmare: pilots...
Originally Posted by OK465
seems preferable to a spin
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Yet again we are seeing a thread that is out-performing the Oozlum bird.
Here we are, over two years of time to digest, argue, prove that (supposedly) type-qualified pilots don't understand it, look at FDR traces, see CVR transcripts - and we still don't really understand what happened. We have two fairly inexperienced lads, and an experienced Captain, who presumably have been told that this a/c will protect you from cradle to grave (!!) and cannot be stalled and that one 'OK' thing to do when in difficulty is to put on full power and pull back the Sidestick - and she will sort it out. 'She' didn't. To make matters worse, when they relax the back pressure, it tells them it is stalling again. Is it any wonder they were confused? What is apparent is that auto-trim contributed to this accident as it also did in PGF when it trimmed in manual flight and the 737 at SPL. when it trimmed in A/P. If, apart from training issues, nothing else comes out of this I would hope that as I said after each of these three crashes - there HAS to be a point at which the trim system stops at some pre-determined value and ASKS for confirmation that what it is doing is what is wanted, particularly in the AB types and the newer Boeings where trim operation is 'un-noticed' - 'silent - but deadly'? |
Doesn't auto trim stop when you go below Vls? The worry for me isn't that they couldn't get out of the stall but that they got it there in the first place!
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Oozlum Bird. Good one BOAC. :D
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Originally Posted by OK465
Does the Velocity stall description bring anything to mind?
I don't mind stressing for the third time: we're discussing the deep stall as related to transport category aeroplanes and as is described by DP Davies, certainly an authority in the field of transport aeroplanes behaviour. Reference is "Handling the big jets", pages 115-119 in the third edition. Velocity is four seater aeroplane. A330 is not. Velocity is piston powered aeroplane. A330 is not Velocity is single engine pusher aeroplane. A330 is not Velocity is canard aeroplane. A330 is not. There are also some differences between Velocity and A330 regarding the mass and wing loading. To just wink-wink-nudge-nudge-you-know-what-I-mean in order to somehow make an impression that something that Velocity's test pilot has encountered during test flight and was labeled by NTSB as deep stall has anything to do with transport aeroplane's deep stall and therefore further imply that Velocity incident somehow proves that A330 is susceptible to the phenomenon is beyond my ability to comprehend. Why would anyone mix handful of facts with bag of suspect notions and expect to get something meaningful out of it is enigma to me. If we'd call every extremely high AoA situation deep stall, there would be no end of it.
Originally Posted by Lord Spandex Masher
I can't, I have paper copies of several flight test documents on controls and stability.
References contrary to your claim can be found in "Handling the big jets". third edition, page 119. Or any decent basic aerodynamics textbook, e.g. Atlantic Flight Training ltd JAA ATPL training handbook, Principles of flight, pages 8-14 to 8-16 in 2006. edition. Those were first that I dug out of my bookshelf and I can't publish excerpts due to copyright issues but if you really want to know what's written in them, i don't think you'll have problem finding out.
Originally Posted by Lord Spandex Masher
It is not the tendancy of a T-Tail to deep stall it is the recovery that can be a problem
Originally Posted by Lord Spandex Masher
Even if the entire length of a wing, swept or straight, stalls at the same time the separation of the airflow occurs towards the rear of the wing causing the centre of lift to move forward. Unchecked that may cause pitch up.
(...) But if any part of the wing stalls it still has the effect of moving the centre of lift forward purely because of the separation of the airflow from the rear of the wing section.
Originally Posted by Lord Spandex Masher
Did you not spot the part about several roll excursions, some up to 40 odd degrees and the 270 heading change?!
As for 270° turn, I find it quite astonishing for diametrically oposite reason to you: that it was so mild. 270° over three minutes gives astonishing average of 1.5° per second or four minutes to complete single turn. Now I'm only waiting for the next ignoramus in line to state that it was Airbus fault that aeroplane which was never intended to have good post-stall characteristics had so benign stall and if it spun (as B752 at Puerto Plata did) the pilots would have at least an idea what was wrong.
Originally Posted by Retired F4
I raised that question (how would the FCPC´s behave during manual trim when not in direct law) some moons ago. Nobody followed my lead there.
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OK.....here I am.....again. Why can't we all just admit that if this had been a "conventional" airplane [cable-operated, not computer/electric-operated] that we would not even have a thread on this? #378 Narrows, Virginia; ABX Air (Airborne Express) DC-8; December 22, 1996 "probable causes of this accident were the inappropriate control inputs applied by the flying pilot during a stall recovery attempt, [and] the failure of the nonflying pilot-in-command to recognize, address, and correct these inappropriate control inputs . (Summary)" "... the airplane remained in an aerodynamic stall condition because the PF held significant back pressure on the control column all the way to impact.(2.2.1)" |
BOAC writes
You are all ignoring the nose down pitch change that occurred each time nose down elevator was applied? Had they wound in nose down trim it might initially have caused some nose down pitch but would it have been enough to keep the THS from stalling as the up trim came off? |
CLANDY: Thank you for sparing us the pictures this time.
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"Again, somewhere on the Tech Log threads at least one Airbus FBW pilot stated that F/Os train on both sides of the flight deck, so left/right-hand orientation should not have been a problem. " "Sorry. Once again : prior to june 1st 2009 Air France F/Os did NOT get any, on purpose, left-seat flight training. Some sim sessions ("true" captain not compulsory) just happenned to be with a two F/O crew but the purpose was not to train F/Os in the left seat." I believe the PF was in the right seat in which case left/right hand orientation should not have been an issue for him. |
Oozlum's coming around again........................
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Razoray. ..what also doesn't sit well is the fact that the plane just fell out of the sky in a deep stall. The tail didn't tear off, the engines didn't fail, there was no "act of God"... There was no b*oody deep stall, man. The pilot held the stick hard back. THAT is what kept the aeroplane stalled. Whenever he got tired and released the back-pressure, the poor aeroplane started to recover. Then, he pulled it back again! Can people read the definition of 'deep stall' or 'super-stall' before using those phrases? |
Sorry, Sorry...I went back and edited my post....it must be contagious!:mad:
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Sorry, Razoray. My fault - getting frustrated.
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BOAC,
You are all ignoring the nose down pitch change that occurred each time nose down elevator was applied? Clandestino, References contrary to your claim can be found in "Handling the big jets". third edition, page 119. Or any decent basic aerodynamics textbook, e.g. Atlantic Flight Training ltd JAA ATPL training handbook, Principles of flight, pages 8-14 to 8-16 in 2006. edition. Those were first that I dug out of my bookshelf and I can't publish excerpts due to copyright issues but if you really want to know what's written in them, i don't think you'll have problem finding out. A deep stall is NOT irrecoverable. A deep stall maybe harder to recover in a T-Tail aircraft because of reduced elevator effectiveness. It is the combination of both swept wings AND T-Tail configurations in aircraft such as the 727 that makes a deep stall more of a problem. Elevator/pitch rocking and induced roll are two ways to recover but these may take a lot of time and height. Swept wing aircraft can all be made to deep stall if you have enough elevator authority. But it doesn't follow that moving the Cp in stall forward results in pitch-up! If it were so in the real world, we would be in deep trouble and I certainly would not be writing this post but pushing daisies at certain quiet village graveyard. Aileron Drag, There was no bloody locked in deep stall. If adequate control authority is not available to recover you are in a deep stall. Usually because of vortex buffeting on T-Tails or, on other types, anything else that reduces elevator control margins. |
Lord Spandex Masher
I was taught aerodynamics here - on Planet Earth. I really am not sure where you were taught. Which is why I have been hinting that this was a manually induced and prolonged deep stall. There.....was......no......DEEP.......stall.....in.....this. ...case. I suggest that you ferret a bit deeper into advanced aerodynamics. A deep stall is NOT irrecoverable. Swept wing aircraft can all be made to deep stall if you have enough elevator authority. There was no bloody locked in deep stall. The PILOT held the aircraft in a stalled condition until it hit the sea. Let me summarize.... 1. AF 447 DID NOT DEEP-STALL. 2. AF 447 was held in a stalled condition by the PF, for reasons known only to him. |
Which is presumably why there is no evidence of persistent ND inputs with a voice commentary along the lines of 'I am trying to reduce pitch but the aircraft isn't responding', or did I miss that bit ?
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No, Mr Optimistic, you didn't miss that bit.
This guy sat there with the stick held fully back, presumably wondering why the pitch attitude was so high, the airspeed so low, and the RoD so high. It's so sad. You wish you could have been there, as though in a simulator session, and say to them, "What are you doing? Why are you holding the nose up like this? |
"A deep stall is NOT irrecoverable."
Oh YES IT IS, mate; and I have one dead friend to prove it. AF447 was put into and held in a stable deep stall. If they had recognised this fact they may have had enough time to recover. The sad thing is they did not recognise it and held it in a deep stall for over three minutes. You understand the difference between a deep stall and locked in deep stall? |
AF447 was put into and held in a stable deep stall. |
"I don't really want to be dragged in to the SS/yoke battle except to say that if I had been dragged out of my pit in my silk pyjamas and arrived in a cockpit at 35,000' with 15 degrees nose up, 10,000fpm+ and a co-pilot with the yoke back in his groin, I might have had a clue as to why the nose was up that high - I hope so."
Very interesting point. There has been a lot mentioned about the lack of SS feedback to the pilot but very little about the lack of feedback to the rest of the crew compared to the old fashioned yoke, feedback that in this case may have been vital. I also wonder about the constant noises bells and whistles going off. There has been a lot of research showing that constant loud noises are an accelerant to panic (as anyone having to deal with a runaway smoke alarm at 2 in the morning can attest) which appears to have been a factor in this accident. By all means aural messages are good but constant repetitive noises will simply dramatically increase stress and degrade performance. The pilots knew there was a problem, and the constant alarms did not help them find a solution. |
They stalled.
Failed to recognise their situation and responded incorrectly. Occam's razor. |
No pilots who hold back pressure on the yoke or SS in a stall live very long if they ever stall. I thought it was instinctive to release any back pressure if it ever occured. I know, for some reason they didn't know they were in a stall even with their attitude and descent rate. Strange.
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They knew their descent rate, in the end. Originally "I have no Vertical Speed". You think they knew Attitude? Betcha a buck they did not."
The Captain came in...."What are you doing?" "I don't know, but we are descending". How do we know? Because with an attitude cue, one of these worthies would suggest Nose Down. Occam, again. Slightly less likely is that the two NF pilots were unaware PF was holding back stick, and assumed he was pushing the stick forward. Poor display, poor cockpit design, poor training, poor CRM, shortsighted SW design, inexplicable Autotrim...... all down to Occam? Hardworking fella, this Occam..... Repeating the same rhetorical "How could three pilots...bla, bla, bla......." does not suggest, let alone confirm, there was a reliable attitude display. How many times did PF correct the ship's Nose Down proclivity? Sufficient to climb to Stall? What attitude was he reading? What was the exact source of the disagreement between the PNF/PF re: altitude? CVR please....... |
I wish to ameliorate my previous post by saying that I do not accuse anyone.
However, with the info we all have, one draws certain conclusions, obvious or not. |
BEA have replaced what was an unimaginably dynamic cockpit with parsed and misleading bits of data. Drawing conclusions from these is premature. Not even BEA have made conclusions. And they get paid for them.
I know you do not accuse, and that is the sad part, for condemnation prior to investigation is absurd. |
No pilots who hold back pressure on the yoke or SS in a stall live very long if they ever stall. I thought it was instinctive to release any back pressure if it ever occured. I know, for some reason they didn't know they were in a stall even with their attitude and descent rate. Strange. |
What would 1g vertical acceleration have felt like in the cockpit during the descent?
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What would 1g vertical acceleration have felt like in the cockpit during the descent? It's as though a total lack of instinct prevailed. As bubbers said, "strange." |
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