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AF447 final crew conversation - Thread No. 1

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AF447 final crew conversation - Thread No. 1

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Old 14th Dec 2011, 12:16
  #801 (permalink)  
 
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Originally Posted by Icepack
Recent Sim exercise (...) speed only got down to 120Kts with VS -6000'/min.
Based on the recorded groundspeed AF447 didn't get below 120 kCAS either. The IAS went below 60 kt due to distortion of the local pressure at the static source at extreme angles of attack which (AoA) also may have affected the pressure in the pitots.

Last edited by HazelNuts39; 14th Dec 2011 at 12:39. Reason: Rearranged for clarity
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Old 14th Dec 2011, 13:19
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With an AoA well in excess of 30 degrees, one does wonder why the LAW did not change to ABNORMAL ATTITUDES?

Yes, Zorin, Inertial triggers only, fine. Why is "g"<.5 not an UA trigger? And why were all three ADRs rejected? You still fancy ICE?

There is a glaring and obvious appearance that the Pilot had no reliable indications, including his own words; this somehow doesn't impinge on his recovery solution?
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Old 14th Dec 2011, 13:39
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AoA is measured through AoA sensor, which are part of the ADR. If ADR rejected then altitude/speed/AoA rejected.

g < .5 does not meet the definition of abnormal attitute, IMO.

All three ADRs were rejected due to discrepancies between the measured speed values. Ice or not ice is not the question. If speeds match = ADR valid. If speeds do not match = ADR rejected. Simple as that. No magic

Fancy trying finding more reasonnable explanations than those of the BEA? Feel free to do Scepticism is good
But please don't "just" ask rethorical questions
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Old 14th Dec 2011, 15:17
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Wasn't the crew of the West Caribbean MD80 pulling hard on the yokes all the way to the ground when they found themselves in a stall at cruising level? It's not about whether sticks move together or not, it's about remember flying 101.

Sometimes I think that maybe knowing less about the FBW control system would actually be better. It looks like a lot of people misunderstand what the system will and will not do, and rightfully so.

The reality is that FBW or not, it's the same - push and the aircraft goes down, pull and the aircraft goes up. Normal, Alternate, Abnormal, or Direct Laws - the subtleties change but the basics are all the same.

If you treat the Airbus just like any other aircraft, it works - you just get the table and auto trim. The protections exist as a last resort, and should never be relied upon. I think even getting a protection of any kind activated should be treated as an event.

What baffles me more is how little communication of any sort is going on (assuming the Popular Mechanics transcript is full). After the Captain enters the deck, there is a period of 1 minute 25 seconds when nothing is said at all. It is a long time, and I just can't believe the three of them would be sitting there completely silent.

Could be there is much more on the CVR that we read.

Last edited by Frankie_B; 14th Dec 2011 at 15:27.
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Old 14th Dec 2011, 15:28
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Thanks, clive, for being in violent agreement with me. I don't know how many courses currently teach "stalls in IMC" as a standard maneuver.

Back when I taught such things, in a non-FBW trainer, stalls and spins "under the bag" (to simulate IMC) were an advanced maneuver.

Our topic is a mishap in an FBW aircraft that is flown with a SideStick. I am very familiar, thanks, with control positions and developing feel in non-FBW aircraft.

If your aircraft is FBW, you have to fly it and deal with it as FBW, not as if it were not.

Let me put this in a different way: if you fly a fixed wing aircraft in to land the same way as you fly a helicopter in to land, and use that feel, you may put yourself in a bad situation. (High flare, bleeding off airspeed farther above ground than you should). I know, this since I've done it. I waved off the approach. You fly fixed wing aircraft by a different combination of scan and control movements than you do a helicopter.

The analogy is very rough, but it seems to fit the idea of applying techniques appropriate to the airframe you are flying.

Is there a 'stalls under the bag' / 'stalls in IMC' training module in Airbus qualification?

Would you consider that an advanced maneuver?

Would you, when analyzing the training system and the system to be trained on, consider making your learning objective the recognition and prevention of stall the core competency?
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Old 14th Dec 2011, 15:49
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Frankie_B wrote:
Wasn't the crew of the West Caribbean MD80 pulling hard on the yokes all the way to the ground when they found themselves in a stall at cruising level? It's not about whether sticks move together or not, it's about remember flying 101.
This whole discussion has already occurred, many pages ago, although I guess it is valuable to have new comments on it. (Something about a hamster wheel?)
The above fact doesn't prove that seeing the yoke back might not have helped in the case of AF447. It can't be proven one way or the other. And "it's about" BOTH; the two are not mutually exclusive.

What baffles me more is how little communication of any sort is going on (assuming the Popular Mechanics transcript is full). After the Captain enters the deck, there is a period of 1 minute 25 seconds when nothing is said at all. It is a long time, and I just can't believe the three of them would be sitting there completely silent.
Well sir, I'd counter that SEEING yokes back would constitute a heckuva lot more communication than they did have! And, I doubt that few of us can believe they were silent for that length of time.

Could be there is much more on the CVR that we read.
Yep! Something is being withheld here, so far. And, until and unless they share it with the world, we'll never fully know what happened. Mark my words, and as others have said, the final BEA report will be gamed. I hope I'm wrong.
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Old 14th Dec 2011, 19:46
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My understanding is that BEA have released so far only a CRV transcript extract. Its not the full transcript. We will need to wait for a more detailed report or 'Final' report for the full transcript.
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Old 14th Dec 2011, 22:20
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Originally Posted by ChrisJ800
My understanding is that BEA have released so far only a CRV transcript extract. Its not the full transcript. We will need to wait for a more detailed report or 'Final' report for the full transcript.
I think you're perfectly right....
The excerpts in 'that book' and the PM article are still that.... excerpts, evn if they seem slightly more complete than those published originally. More "leaks" ???
Most people here seem to have missed that.
I doubt we'll see a full transcript until the 'final' report, and as with CVR transcripts usually, I expect it to have been edited (simple matter of respect to those who can no longer explain why they were swearing....)
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Old 14th Dec 2011, 23:25
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Originally Posted by RunSick
Wouldn´t it have been better to have somewhere a Note that clearly stated "The stall warning synthetic voice will not activate below 60kts"?
It would. Just 2 lines for a nice to know item.
To the contrary the following was written and still is.
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Old 15th Dec 2011, 02:20
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Originally Posted by Zorin_75
Sigh. BEA Report:

Quote:
The flight control law switched from normal to alternate at about 2 h 10 min 05. The alternate law adopted was alternate 2B and it did not change again subsequently. Due to the rejection of the three ADR by the flight control computers (PRIM), the abnormal attitudes law could only have been triggered for criteria relating to inertial parameters, but these conditions were never met.

While the reference is appreciated, how does this information relate to the current discussion on training and stall warning indications? Is there a direct reference in the training materials you care to share or are you making this leap of faith on your own?

Or perhaps your helpful reference is aimed at an entirely different vein of thought within this thread, and not me. If this is the case, kindly disregard my blather and carry on.
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Old 15th Dec 2011, 04:09
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http://www.pprune.org/6545680-post595.html

If this no more documentation (available to pilots) about this item (aural stall warning) I think that lawyers of Airbus will have to find good arguments to defend their client on this item that has already been controversy in the BEA preliminary report N°3
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Old 15th Dec 2011, 04:37
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Print - What Really Happened Aboard Air France 447 - Popular Mechanics

At 1h 36m, the flight enters the outer extremities of a tropical storm system. Unlike other planes' crews flying through the region, AF447's flight crew has not changed the route to avoid the worst of the storms. The outside temperature is much warmer than forecast, preventing the still fuel-heavy aircraft from flying higher to avoid the effects of the weather. Instead, it ploughs into a layer of clouds.

At 1h51m, the cockpit becomes illuminated by a strange electrical phenomenon. The co-pilot in the right-hand seat, an inexperienced 32-year-old named Pierre-Cédric Bonin, asks, "What's that?" The captain, Marc Dubois, a veteran with more than 11,000 hours of flight time, tells him it is St. Elmo's fire, a phenomenon often found with thunderstorms at these latitudes.

At approximately 2 am, the other co-pilot, David Robert, returns to the cockpit after a rest break. At 37, Robert is both older and more experienced than Bonin, with more than double his colleague's total flight hours. The head pilot gets up and gives him the left-hand seat. Despite the gap in seniority and experience, the captain leaves Bonin in charge of the controls.

At 2:02 am, the captain leaves the flight deck to take a nap. Within 15 minutes, everyone aboard the plane will be dead.]

02:03:44 (Bonin) La convergence inter tropicale… voilà, là on est dedans, entre 'Salpu' et 'Tasil.' Et puis, voilà, on est en plein dedans…
The inter-tropical convergence... look, we're in it, between 'Salpu' and 'Tasil.' And then, look, we're right in it...

The intertropical convergence, or ITC, is an area of consistently severe weather near the equator. As is often the case, it has spawned a string of very large thunderstorms, some of which stretch into the stratosphere. Unlike some of the other planes's crews flying in the region this evening, the crew of AF447 has not studied the pattern of storms and requested a divergence around the area of most intense activity. (Salpu and Tasil are two air-traffic-position reporting points.)

02:05:55 (Robert) Oui, on va les appeler derrière... pour leur dire quand même parce que...
Yes, let's call them in the back, to let them know...

Robert pushes the call button.

02:05:59 (flight attendant, heard on the intercom) Oui? Marilyn.
Yes? Marilyn.

02:06:04 (Bonin) Oui, Marilyn, c'est Pierre devant... Dis-moi, dans deux minutes, on devrait attaquer une zone où ça devrait bouger un peu plus que maintenant. Il faudrait vous méfier là.
Yes, Marilyn, it's Pierre up front... Listen, in 2 minutes, we're going to be getting into an area where things are going to be moving around a little bit more than now. You'll want to take care.

02:06:13 (flight attendant) D'accord, on s'assoit alors?
Okay, we should sit down then?

02:06:15 (Bonin) Bon, je pense que ce serait pas mal… tu préviens les copains!
Well, I think that's not a bad idea. Give your friends a heads-up.

02:06:18 (flight attendant) Ouais, OK, j'appelle les autres derrière. Merci beaucoup.
Yeah, okay, I'll tell the others in the back. Thanks a lot.

02:06:19 (Bonin) Mais je te rappelle dès qu'on est sorti de là.
I'll call you back as soon as we're out of it.

02:06:20 (flight attendant) OK.
Okay.

The two copilots discuss the unusually elevated external temperature, which has prevented them from climbing to their desired altitude, and express happiness that they are flying an Airbus 330, which has better performance at altitude than an Airbus 340.

02:06:50 (Bonin) Va pour les anti-ice. C'est toujours ça de pris.
Let's go for the anti-icing system. It's better than nothing.

Because they are flying through clouds, the pilots turn on the anti-icing system to try to keep ice off the flight surfaces; ice reduces the plane's aerodynamic efficiency, weighs it down, and in extreme cases, can cause it to crash.

02:07:00 (Bonin) On est apparemment à la limite de la couche, ça devrait aller.
We seem to be at the end of the cloud layer, it might be okay.

In the meantime Robert has been examining the radar system and has found that it has not been set up in the correct mode. Changing the settings, he scrutinizes the radar map and realizes that they are headed directly toward an area of intense activity.

02:08:03 (Robert) Tu peux éventuellement le tirer un peu à gauche.
You can possibly pull it a little to the left.

02:08:05 (Bonin) Excuse-moi?
Sorry, what?

02:08:07 (Robert) Tu peux éventuellement prendre un peu à gauche. On est d'accord qu'on est en manuel, hein?
You can possibly pull it a little to the left. We're agreed that we're in manual, yeah?

Bonin wordlessly banks the plane to the left. Suddenly, a strange aroma, like an electrical transformer, floods the cockpit, and the temperature suddenly increases. At first, the younger pilot thinks that something is wrong with the air-conditioning system, but Robert assures him that the effect is from the severe weather in the vicinity. Bonin seems ill at ease. Then the sound of slipstream suddenly becomes louder. This, presumably, is due to the accumulation of ice crystals on the exterior of the fuselage. Bonin announces that he is going to reduce the speed of the aircraft, and asks Robert if he should turn on a feature that will prevent the jet engines from flaming out in the event of severe icing.

Just then an alarm sounds for 2.2 seconds, indicating that the autopilot is disconnecting. The cause is the fact that the plane's pitot tubes, externally mounted sensors that determine air speed, have iced over, so the human pilots will now have to fly the plane by hand.

Note, however, that the plane has suffered no mechanical malfunction. Aside from the loss of airspeed indication, everything is working fine. Otelli reports that many airline pilots (and, indeed, he himself) subsequently flew a simulation of the flight from this point and were able to do so without any trouble. But neither Bonin nor Roberts has ever received training in how to deal with an unreliable airspeed indicator at cruise altitude, or in flying the airplane by hand under such conditions.

02:10:06 (Bonin) J'ai les commandes.
I have the controls.

02:10:07 (Robert) D'accord.
Okay.

Perhaps spooked by everything that has unfolded over the past few minutes—the turbulence, the strange electrical phenomena, his colleague's failure to route around the potentially dangerous storm—Bonin reacts irrationally. He pulls back on the side stick to put the airplane into a steep climb, despite having recently discussed the fact that the plane could not safely ascend due to the unusually high external temperature.

Bonin's behavior is difficult for professional aviators to understand. "If he's going straight and level and he's got no airspeed, I don't know why he'd pull back," says Chris Nutter, an airline pilot and flight instructor. "The logical thing to do would be to cross-check"—that is, compare the pilot's airspeed indicator with the co-pilot's and with other instrument readings, such as groundspeed, altitude, engine settings, and rate of climb. In such a situation, "we go through an iterative assessment and evaluation process," Nutter explains, before engaging in any manipulation of the controls. "Apparently that didn't happen."

Almost as soon as Bonin pulls up into a climb, the plane's computer reacts. A warning chime alerts the cockpit to the fact that they are leaving their programmed altitude. Then the stall warning sounds. This is a synthesized human voice that repeatedly calls out, "Stall!" in English, followed by a loud and intentionally annoying sound called a "cricket." A stall is a potentially dangerous situation that can result from flying too slowly. At a critical speed, a wing suddenly becomes much less effective at generating lift, and a plane can plunge precipitously. All pilots are trained to push the controls forward when they're at risk of a stall so the plane will dive and gain speed.

The Airbus's stall alarm is designed to be impossible to ignore. Yet for the duration of the flight, none of the pilots will mention it, or acknowledge the possibility that the plane has indeed stalled—even though the word "Stall!" will blare through the cockpit 75 times. Throughout, Bonin will keep pulling back on the stick, the exact opposite of what he must do to recover from the stall.

02:10:07 (Robert) Qu'est-ce que c'est que ça?
What's this?

02:10:15 (Bonin) On n'a pas une bonne… On n'a pas une bonne annonce de vitesse.
There's no good... there's no good speed indication.

02:10:16 (Robert) On a perdu les, les, les vitesses alors?
We've lost the, the, the speeds, then?

The plane is soon climbing at a blistering rate of 7000 feet per minute. While it is gaining altitude, it is losing speed, until it is crawling along at only 93 knots, a speed more typical of a small Cessna than an airliner. Robert notices Bonin's error and tries to correct him.

02:10:27 (Robert) Faites attention à ta vitesse. Faites attention à ta vitesse.
Pay attention to your speed. Pay attention to your speed.

He is probably referring to the plane's vertical speed. They are still climbing.

02:10:28 (Bonin) OK, OK, je redescends.
Okay, okay, I'm descending.

02:10:30 (Robert) Tu stabilises...
Stabilize…

02:10:31 (Bonin) Ouais.
Yeah.

02:10:31 (Robert) Tu redescends... On est en train de monter selon lui… Selon lui, tu montes, donc tu redescends.
Descend... It says we're going up... It says we're going up, so descend.

02:10:35 (Bonin) D'accord.
Okay.

Thanks to the effects of the anti-icing system, one of the pitot tubes begins to work again. The cockpit displays once again show valid speed information.

02:10:36 (Robert) Redescends!
Descend!

02:10:37 (Bonin) C'est parti, on redescend.
Here we go, we're descending.

02:10:38 (Robert) Doucement!
Gently!

Bonin eases the back pressure on the stick, and the plane gains speed as its climb becomes more shallow. It accelerates to 223 knots. The stall warning falls silent. For a moment, the co-pilots are in control of the airplane.

02:10:41(Bonin) On est en… ouais, on est en "climb."
We're... yeah, we're in a climb.

Yet, still, Bonin does not lower the nose. Recognizing the urgency of the situation, Robert pushes a button to summon the captain.

02:10:49 (Robert) Putain, il est où... euh?
Damn it, where is he?

The plane has climbed to 2512 feet above its initial altitude, and though it is still ascending at a dangerously high rate, it is flying within its acceptable envelope. But for reasons unknown, Bonin once again increases his back pressure on the stick, raising the nose of the plane and bleeding off speed. Again, the stall alarm begins to sound.

Still, the pilots continue to ignore it, and the reason may be that they believe it is impossible for them to stall the airplane. It's not an entirely unreasonable idea: The Airbus is a fly-by-wire plane; the control inputs are not fed directly to the control surfaces, but to a computer, which then in turn commands actuators that move the ailerons, rudder, elevator, and flaps. The vast majority of the time, the computer operates within what's known as normal law, which means that the computer will not enact any control movements that would cause the plane to leave its flight envelope. "You can't stall the airplane in normal law," says Godfrey Camilleri, a flight instructor who teaches Airbus 330 systems to US Airways pilots.

But once the computer lost its airspeed data, it disconnected the autopilot and switched from normal law to "alternate law," a regime with far fewer restrictions on what a pilot can do. "Once you're in alternate law, you can stall the airplane," Camilleri says.

It's quite possible that Bonin had never flown an airplane in alternate law, or understood its lack of restrictions. According to Camilleri, not one of US Airway's 17 Airbus 330s has ever been in alternate law. Therefore, Bonin may have assumed that the stall warning was spurious because he didn't realize that the plane could remove its own restrictions against stalling and, indeed, had done so.

02:10:55 (Robert) Putain!
Damn it!

Another of the pitot tubes begins to function once more. The cockpit's avionics are now all functioning normally. The flight crew has all the information that they need to fly safely, and all the systems are fully functional. The problems that occur from this point forward are entirely due to human error.

02:11:03 (Bonin) Je suis en TOGA, hein?
I'm in TOGA, huh?

Bonin's statement here offers a crucial window onto his reasoning. TOGA is an acronym for Take Off, Go Around. When a plane is taking off or aborting a landing—"going around"—it must gain both speed and altitude as efficiently as possible. At this critical phase of flight, pilots are trained to increase engine speed to the TOGA level and raise the nose to a certain pitch angle.

Clearly, here Bonin is trying to achieve the same effect: He wants to increase speed and to climb away from danger. But he is not at sea level; he is in the far thinner air of 37,500 feet. The engines generate less thrust here, and the wings generate less lift. Raising the nose to a certain angle of pitch does not result in the same angle of climb, but far less. Indeed, it can—and will—result in a descent.

While Bonin's behavior is irrational, it is not inexplicable. Intense psychological stress tends to shut down the part of the brain responsible for innovative, creative thought. Instead, we tend to revert to the familiar and the well-rehearsed. Though pilots are required to practice hand-flying their aircraft during all phases of flight as part of recurrent training, in their daily routine they do most of their hand-flying at low altitude—while taking off, landing, and maneuvering. It's not surprising, then, that amid the frightening disorientation of the thunderstorm, Bonin reverted to flying the plane as if it had been close to the ground, even though this response was totally ill-suited to the situation.

02:11:06 (Robert) Putain, il vient ou il vient pas?
Damn it, is he coming or not?

The plane now reaches its maximum altitude. With engines at full power, the nose pitched upward at an angle of 18 degrees, it moves horizontally for an instant and then begins to sink back toward the ocean.

02:11:21 (Robert) On a pourtant les moteurs! Qu'est-ce qui se passe bordel? Je ne comprends pas ce que se passe.
We still have the engines! What the hell is happening? I don't understand what's happening.

Unlike the control yokes of a Boeing jetliner, the side sticks on an Airbus are "asynchronous"—that is, they move independently. "If the person in the right seat is pulling back on the joystick, the person in the left seat doesn't feel it," says Dr. David Esser, a professor of aeronautical science at Embry-Riddle Aeronautical University. "Their stick doesn't move just because the other one does, unlike the old-fashioned mechanical systems like you find in small planes, where if you turn one, the [other] one turns the same way." Robert has no idea that, despite their conversation about descending, Bonin has continued to pull back on the side stick.

The men are utterly failing to engage in an important process known as crew resource management, or CRM. They are failing, essentially, to cooperate. It is not clear to either one of them who is responsible for what, and who is doing what. This is a natural result of having two co-pilots flying the plane. "When you have a captain and a first officer in the cockpit, it's clear who's in charge," Nutter explains. "The captain has command authority. He's legally responsible for the safety of the flight. When you put two first officers up front, it changes things. You don't have the sort of traditional discipline imposed on the flight deck when you have a captain."

The vertical speed toward the ocean accelerates. If Bonin were to let go of the controls, the nose would fall and the plane would regain forward speed. But because he is holding the stick all the way back, the nose remains high and the plane has barely enough forward speed for the controls to be effective. As turbulence continues to buffet the plane, it is nearly impossible to keep the wings level.

02:11:32 (Bonin) Putain, j'ai plus le contrôle de l'avion, là! J'ai plus le contrôle de l'avion!
Damn it, I don't have control of the plane, I don't have control of the plane at all!

02:11:37 (Robert) Commandes à gauche!
Left seat taking control!

At last, the more senior of the pilots (and the one who seems to have a somewhat better grasp of the situation) now takes control of the airplane. Unfortunately, he, too, seems unaware of the fact that the plane is now stalled, and pulls back on the stick as well. Although the plane's nose is pitched up, it is descending at a 40-degree angle. The stall warning continues to sound. At any rate, Bonin soon after takes back the controls.

A minute and a half after the crisis began, the captain returns to the cockpit. The stall warning continues to blare.

02:11:43 (Captain) Eh… Qu'est-ce que vous foutez?
What the hell are you doing?

02:11:45 (Bonin) On perd le contrôle de l'avion, là!
We've lost control of the plane!

02:11:47 (Robert) On a totalement perdu le contrôle de l'avion... On comprend rien... On a tout tenté...
We've totally lost control of the plane. We don't understand at all... We've tried everything.

By now the plane has returned to its initial altitude but is falling fast. With its nose pitched 15 degrees up, and a forward speed of 100 knots, it is descending at a rate of 10,000 feet per minute, at an angle of 41.5 degrees. It will maintain this attitude with little variation all the way to the sea. Though the pitot tubes are now fully functional, the forward airspeed is so low—below 60 knots—that the angle-of-attack inputs are no longer accepted as valid, and the stall-warning horn temporarily stops. This may give the pilots the impression that their situation is improving, when in fact it signals just the reverse.

Another of the revelations of Otelli's transcript is that the captain of the flight makes no attempt to physically take control of the airplane. Had Dubois done so, he almost certainly would have understood, as a pilot with many hours flying light airplanes, the insanity of pulling back on the controls while stalled. But instead, he takes a seat behind the other two pilots.

This, experts say, is not so hard to understand. "They were probably experiencing some pretty wild gyrations," Esser says. "In a condition like that, he might not necessarily want to make the situation worse by having one of the crew members actually disengage and stand up. He was probably in a better position to observe and give his commands from the seat behind."

But from his seat, Dubois is unable to infer from the instrument displays in front of him why the plane is behaving as it is. The critical missing piece of information: the fact that someone has been holding the controls all the way back for virtually the entire time. No one has told Dubois, and he hasn't thought to ask.

02:12:14 (Robert) Qu'est-ce que tu en penses? Qu'est-ce que tu en penses? Qu'est-ce qu'il faut faire?
What do you think? What do you think? What should we do?

02:12:15 (Captain) Alors, là, je ne sais pas!
Well, I don't know!

As the stall warning continues to blare, the three pilots discuss the situation with no hint of understanding the nature of their problem. No one mentions the word "stall." As the plane is buffeted by turbulence, the captain urges Bonin to level the wings—advice that does nothing to address their main problem. The men briefly discuss, incredibly, whether they are in fact climbing or descending, before agreeing that they are indeed descending. As the plane approaches 10,000 feet, Robert tries to take back the controls, and pushes forward on the stick, but the plane is in "dual input" mode, and so the system averages his inputs with those of Bonin, who continues to pull back. The nose remains high.

02:13:40 (Robert) Remonte... remonte... remonte... remonte...
Climb... climb... climb... climb...

02:13:40 (Bonin) Mais je suis à fond à cabrer depuis tout à l'heure!
But I've had the stick back the whole time!

At last, Bonin tells the others the crucial fact whose import he has so grievously failed to understand himself.

02:13:42 (Captain) Non, non, non... Ne remonte pas... non, non.
No, no, no... Don't climb... no, no.

02:13:43 (Robert) Alors descends... Alors, donne-moi les commandes... À moi les commandes!
Descend, then... Give me the controls... Give me the controls!

Bonin yields the controls, and Robert finally puts the nose down. The plane begins to regain speed. But it is still descending at a precipitous angle. As they near 2000 feet, the aircraft's sensors detect the fast-approaching surface and trigger a new alarm. There is no time left to build up speed by pushing the plane's nose forward into a dive. At any rate, without warning his colleagues, Bonin once again takes back the controls and pulls his side stick all the way back.

02:14:23 (Robert) Putain, on va taper... C'est pas vrai!
Damn it, we're going to crash... This can't be happening!

02:14:25 (Bonin) Mais qu'est-ce que se passe?
But what's happening?

02:14:27 (Captain) 10 degrès d'assiette...
Ten degrees of pitch...

Exactly 1.4 seconds later, the cockpit voice recorder stops.

___

Today the Air France 447 transcripts yield information that may ensure that no airline pilot will ever again make the same mistakes. From now on, every airline pilot will no doubt think immediately of AF447 the instant a stall-warning alarm sounds at cruise altitude. Airlines around the world will change their training programs to enforce habits that might have saved the doomed airliner: paying closer attention to the weather and to what the planes around you are doing; explicitly clarifying who's in charge when two co-pilots are alone in the cockpit; understanding the parameters of alternate law; and practicing hand-flying the airplane during all phases of flight.

But the crash raises the disturbing possibility that aviation may well long be plagued by a subtler menace, one that ironically springs from the never-ending quest to make flying safer. Over the decades, airliners have been built with increasingly automated flight-control functions. These have the potential to remove a great deal of uncertainty and danger from aviation. But they also remove important information from the attention of the flight crew. While the airplane's avionics track crucial parameters such as location, speed, and heading, the human beings can pay attention to something else. But when trouble suddenly springs up and the computer decides that it can no longer cope—on a dark night, perhaps, in turbulence, far from land—the humans might find themselves with a very incomplete notion of what's going on. They'll wonder: What instruments are reliable, and which can't be trusted? What's the most pressing threat? What's going on? Unfortunately, the vast majority of pilots will have little experience in finding the answers.
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Old 15th Dec 2011, 06:34
  #813 (permalink)  
 
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Very helpful that glueball, very helpful.
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Old 15th Dec 2011, 08:41
  #814 (permalink)  
 
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Just a couple of things;
Suddenly, a strange aroma, like an electrical transformer, floods the cockpit, and the temperature suddenly increases. At first, the younger pilot thinks that something is wrong with the air-conditioning system, but Robert assures him that the effect is from the severe weather in the vicinity. Bonin seems ill at ease. Then the sound of slipstream suddenly becomes louder. This, presumably, is due to the accumulation of ice crystals on the exterior of the fuselage. Bonin announces that he is going to reduce the speed of the aircraft, and asks Robert if he should turn on a feature that will prevent the jet engines from flaming out in the event of severe icing.
That smell was from St Elmos fire and that noise was from flying in very heavy rain. Those two usually go hand in hand. That "feature" was probably auto ignition.

A stall is a potentially dangerous situation that can result from flying too slowly. At a critical speed, a wing suddenly becomes much less effective at generating lift, and a plane can plunge precipitously. All pilots are trained to push the controls forward when they're at risk of a stall so the plane will dive and gain speed.
This is typical rhetoric from someone without a very good understanding of basic aerodynamics. A airplane can stall at any attitude and airspeed (within structural limits of course) by not so much as flying slowly but exceeding the critical angle of attack Think about your accelerated stalls. The rule you learn in a basic acro course is to point the nose in the direction the aircraft is going to get it to fly again. Case in point:
By now the plane has returned to its initial altitude but is falling fast. With its nose pitched 15 degrees up, and a forward speed of 100 knots, it is descending at a rate of 10,000 feet per minute, at an angle of 41.5 degrees.
The nose would have had to be pointed in this case down to very close to 41 degrees since it does not have the power to fly out of that condition. Then letting the aircraft accelerate then retarding the power while pulling out of the dive. Pointing the nose down that much would seem very alien to most people however that is what was needed to survive at that point. The 1st problem was putting the aircraft assume that stalled condition, the second was not recognizing it and implementing correct recovery procedures.

Last edited by before landing check list; 15th Dec 2011 at 12:13.
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Old 15th Dec 2011, 09:23
  #815 (permalink)  
 
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CONF iture,
STALL WARNING: When the threshold is reached, a permanent aural stall warning is triggered "STALL + CRICKET" as long as a correct angle-of-attack is not recovered.
It could be argued that that description is correct provided the stall warning is respected as called for in FCOM 3.04.27 p.6:
Alternate law, pitch
(...)
An aural "STALL, STALL, STALL" warning sounds at low speeds. Upon hearing it, the pilot must return to the normal operating speeds by taking conventional action with the controls:
- Thrust levers .... TOGA
At the same time:
- Pitch attitude .... REDUCE
(...)
I strongly suspect that AB system designers never realized that airspeed could become as low as 60 kt in flight. As I explained in post #812, the true CAS didn't get as low and probably never will. It is the INDICATED airspeed that is mis-reading when AoA exceeds 25 degrees. That indicating error was unknown, since the airspeed indicating system was never calibrated in those conditions. Could the indicating error have been expected? Perhaps.
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Old 15th Dec 2011, 13:52
  #816 (permalink)  
 
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Originally Posted by HN39
I strongly suspect that AB system designers never realized that airspeed could become as low as 60 kt in flight.
But why include such speed condition ?
Isn't a weight on wheel restriction not good enough ?
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Old 15th Dec 2011, 14:42
  #817 (permalink)  
 
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Exactly. Why include a lane that has no benefit, only potential though remote, dangers. Just because Johnny keeps crying "WOLF", a good cop still investigates each time, yes?

Is there a CB for the STALLSTALLCRICKET? My guess is no, and good on that, at least. "The STALL warning is meant to be annoying and unavoidable" (FlightGlobal).
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Old 15th Dec 2011, 15:21
  #818 (permalink)  
 
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But why include such a speed condition?
Because there is a minimum speed below which the required accuracy of the AoA sensors cannot be guaranteed. Even if a lower value had been chosen, the IAS would probably have gone below it.
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Old 15th Dec 2011, 15:40
  #819 (permalink)  
 
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Originally Posted by HN39
But why include such a speed condition?
Because there is a minimum speed below which the required accuracy of the AoA sensors cannot be guaranteed. Even if a lower value had been chosen, the IAS would probably have gone below it.
But that is actually a fouled up design decision. AF447 always had adequate airspeed to properly deflect the AOA sensors on its way down. It was just that the speed sensing system didn't know how to compute for substantially off axis airflow.

Removing the airspeed calculation out of the AOA data is the proper fix. There is no valid reason for mixing the two. They are each independent sources of flight data.
I've flown down to 0 airspeed and observed my AOA data. No surprises.No big deal.

Once airborne, you will never get a jet transport below 60 knots in real life. A weight on wheels type validity is sufficient.

Last edited by Machinbird; 15th Dec 2011 at 15:46. Reason: Expand AOA comment
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Old 15th Dec 2011, 15:51
  #820 (permalink)  
 
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@Machinbird

"the speed sensing system did not know how to compute for substantially off axis flow."

That is what caused the crash in the first place. "Wind Shear". And a climb that had been experienced before. Sometimes, an aircraft "THINKS" too much. The INITIAL STALLSTALL is what spills the beans, among other things, and similarities with the other "uncommanded climbs".

Sorry, Machinbird, you are absolutely on target.
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