AF 447 Thread No. 8
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The first page of the first thread seems to be largely taken up with discussion of finding the flight recorders using their pingers - are you talking about a different thread?
Last edited by DozyWannabe; 22nd May 2012 at 18:37.
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y PNF
Hi Doze,
But in this case there was no apparent "confusion" over laws. The drop to Alternate was called by the PNF, but the PF either didn't notice or disregarded the call. At no point does the PF question why the aircraft is respnsing the way it is and at no point does he quesiton the fact that the aircraft is clearly not in a protected mode.
What a wild statement to make!
The drop to ALTERNATE was called by PNF seventeen seconds after loss of AUTOPILOT. You claim there was no "confusion"? It is more likely PF thought he remained[/I] IN NORMAL than that he thought the LAWS had changed. Evidence would be his ham handed handling of the a/c in manual. One could say he was merely rusty in ALT, but one could also say he thought NORMAL LAW still obtained for flight, and the ship still responsible for smooth.
If PNF was seriously asking "What was that?" re: STALLSTALL, and PF did not even mention it, why would you say he saw amber "ALT LAW" on the screen? One can make no suppositions in the absence of even basic conversation re: CRM.
As to why he did not question why the a/c was "handling different", are you serious? He didn't know it was "handling" at ALL and I suggest he was unable to discern the simple matter of LAW differentiation on the "fly".....
But in this case there was no apparent "confusion" over laws. The drop to Alternate was called by the PNF, but the PF either didn't notice or disregarded the call. At no point does the PF question why the aircraft is respnsing the way it is and at no point does he quesiton the fact that the aircraft is clearly not in a protected mode.
What a wild statement to make!
The drop to ALTERNATE was called by PNF seventeen seconds after loss of AUTOPILOT. You claim there was no "confusion"? It is more likely PF thought he remained[/I] IN NORMAL than that he thought the LAWS had changed. Evidence would be his ham handed handling of the a/c in manual. One could say he was merely rusty in ALT, but one could also say he thought NORMAL LAW still obtained for flight, and the ship still responsible for smooth.
If PNF was seriously asking "What was that?" re: STALLSTALL, and PF did not even mention it, why would you say he saw amber "ALT LAW" on the screen? One can make no suppositions in the absence of even basic conversation re: CRM.
As to why he did not question why the a/c was "handling different", are you serious? He didn't know it was "handling" at ALL and I suggest he was unable to discern the simple matter of LAW differentiation on the "fly".....
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Evidence would be his ham handed handling of the a/c in manual.
One could say he was merely rusty in ALT, but one could also say he thought NORMAL LAW still obtained for flight, and the ship still responsible for smooth.
If PNF was seriously asking "What was that?" re: STALLSTALL, and PF did not even mention it, why would you say he saw amber "ALT LAW" on the screen? One can make no suppositions in the absence of even basic conversation re: CRM.
As to why he did not question why the a/c was "handling different", are you serious? He didn't know it was "handling" at ALL and I suggest he was unable to discern the simple matter of LAW differentiation on the "fly".....
First and foremost - even if he was in Normal Law, the attitude he was trying to command was completely inappropriate at cruise level.
Laws
Quote:
Originally Posted by CONF iture
No, my suggestion is simply the result of many years of observation. If you reduce the laws and the complexity, you end up with something more straight forward and simple for the pilot thinking.
Originally Posted by CONF iture
No, my suggestion is simply the result of many years of observation. If you reduce the laws and the complexity, you end up with something more straight forward and simple for the pilot thinking.
DW
But in this case there was no apparent "confusion" over laws. The drop to Alternate was called by the PNF, but the PF either didn't notice or disregarded the call. At no point does the PF question why the aircraft is respnsing the way it is and at no point does he quesiton the fact that the aircraft is clearly not in a protected mode.
But in this case there was no apparent "confusion" over laws. The drop to Alternate was called by the PNF, but the PF either didn't notice or disregarded the call. At no point does the PF question why the aircraft is respnsing the way it is and at no point does he quesiton the fact that the aircraft is clearly not in a protected mode.
Laws Reconfiguration - General
The reconfiguration of control laws is different in pitch axis and in lateral axis.
Control law reconfigurations are divided into two families :
- ALTERNATE
- DIRECT
There is no loss of normal law after a single failure. The transfer from normal
laws to alternate laws is automatic and depends on the number and nature of
failures.
In the event of loss of the normal control laws:
When the conditions required for keeping the normal control laws are no longer fulfilled, the control laws are reconfigured. The various degraded law states possible are (in flight or upon flare):
Roll and yaw:
- Yaw alternate law
Pitch:
- Nz law (with limited pitch rate and gains)
- Vc PROT law
- VMO2 law
- Pitch direct law
The laws called Alternate are engaged when the protections related to the
normal laws (ALPHA 1, VM01) are lost. The laws called Direct are engaged
when the Nz law is lost.
The other functions available are :
speedbrake function
ground spoiler function
MLA (except in direct laws)
rudder travel limitation
sideslip estimation (except in alternate 2 or direct laws)
computation of characteristic speeds (except in direct laws)
The computer in charge of these laws and functions is selected according to
the priority logic upon law engagement (Ref. Para. Priority Logics).
In abnormal conditions:
When certain aircraft parameters exceed pre-determined values, the laws
called abnormal attitude laws are engaged.
In the event of temporary loss of all electrical control:
Under these conditions, only the mechanical controls are available:
- Rudder mechanical control from the pedals.
- THS mechanical control from the trim control wheel.
The elevator servo controls are centered.
Actuator servoing
In the event of a failure affecting the aileron, rudder and elevator actuators, the
servoings are reconfigured in accordance with the servoing engagement priority
logic (Ref. Para. Priority Logics).
In the event of a failure affecting a spoiler servo control, the corresponding servoing
is de-activated together with the servoingof the symmetrical spoiler servo
control on the other wing.
The reconfiguration of control laws is different in pitch axis and in lateral axis.
Control law reconfigurations are divided into two families :
- ALTERNATE
- DIRECT
There is no loss of normal law after a single failure. The transfer from normal
laws to alternate laws is automatic and depends on the number and nature of
failures.
In the event of loss of the normal control laws:
When the conditions required for keeping the normal control laws are no longer fulfilled, the control laws are reconfigured. The various degraded law states possible are (in flight or upon flare):
Roll and yaw:
- Yaw alternate law
Pitch:
- Nz law (with limited pitch rate and gains)
- Vc PROT law
- VMO2 law
- Pitch direct law
The laws called Alternate are engaged when the protections related to the
normal laws (ALPHA 1, VM01) are lost. The laws called Direct are engaged
when the Nz law is lost.
The other functions available are :
speedbrake function
ground spoiler function
MLA (except in direct laws)
rudder travel limitation
sideslip estimation (except in alternate 2 or direct laws)
computation of characteristic speeds (except in direct laws)
The computer in charge of these laws and functions is selected according to
the priority logic upon law engagement (Ref. Para. Priority Logics).
In abnormal conditions:
When certain aircraft parameters exceed pre-determined values, the laws
called abnormal attitude laws are engaged.
In the event of temporary loss of all electrical control:
Under these conditions, only the mechanical controls are available:
- Rudder mechanical control from the pedals.
- THS mechanical control from the trim control wheel.
The elevator servo controls are centered.
Actuator servoing
In the event of a failure affecting the aileron, rudder and elevator actuators, the
servoings are reconfigured in accordance with the servoing engagement priority
logic (Ref. Para. Priority Logics).
In the event of a failure affecting a spoiler servo control, the corresponding servoing
is de-activated together with the servoingof the symmetrical spoiler servo
control on the other wing.
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@Franzl :
The point I was making was that you don't need to know the specifics as far as Alternate Law is concerned - fly the thing as you would normally fly it, just don't expect the protections to be there.
Is there anything in what you've posted that contradicts the above summary?
The point I was making was that you don't need to know the specifics as far as Alternate Law is concerned - fly the thing as you would normally fly it, just don't expect the protections to be there.
Is there anything in what you've posted that contradicts the above summary?
Last edited by DozyWannabe; 22nd May 2012 at 22:24.
DW
The point I was making was that you don't need to know the specifics as far as Alternate Law is concerned - fly the thing as you would normally fly it, just don't expect the protections to be there.
Is there anything in what you've posted that contradicts the above summary?
The point I was making was that you don't need to know the specifics as far as Alternate Law is concerned - fly the thing as you would normally fly it, just don't expect the protections to be there.
Is there anything in what you've posted that contradicts the above summary?
And the main problem is, that you normally donīt fly that thing, but you are being flown while monitoring. Except when the sh*t hits the fan.
Last edited by RetiredF4; 22nd May 2012 at 22:40.
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Doze.
Even in Normal Law this would have brought the aircraft to the edge of stall - those inputs were not only in excess of what was required, but also in excess of what was sensible. Discussion of control laws is a red herring, because it has absolutely no bearing on why those inputs were so inappropriately excessive in the first place.
Early on, we were treated to closeup video of short finals/touchdown, the pilots handling were stirring mayonnaise, yet the camera outside showed the a/c virtually on rails, very impressive, to see such stickwork. Now that means they were: Johnny Ace, able to fly through anything on a rail, or a forgiving a/c, smoothing stck to find a stable path.
All due respect, the stick was excessive, and the a/c shone brightly as a sweetie.
So I am calling mayonnaise on Bonin, him thinking the ship would smooth his "whatever" stickwork into grease....e thought he was in NORMAL, and made no effort to modify his stick inputs to a LAW of which he was unaware?
LAW has everything to do with everything, in those first twenty seconds. it took the a/c some seconds to load up, and go up, and once committed, no one would be able to suss her attitude. So think DIRECT in roll, and ask: Would this pilot, aware of his AL DIRECT ROLL, act as if he was low, and the a/c made him look good? I say no, and so I conclude his handling bespoke NORMAL, with protections. At 2:10:22, when PNF says "....ALTERNATE LAW", I think he was preoccupied, no, I KNOW he was preoccupied. Why? A pilot who does not know whether he is climbing, at Mach .80, or descending, has not thought of which LAW obtains. So my case is based on: STARTLE (agree?), loss of scan, loss of orientation, and loss of the plot.....This in the first twenty seconds, max. The only save was for the PNF to take over. He didn't. The rest is merely interesting, but the game was over quickly. The PNF and later the Captain, failed, for whatever combination of reasons, to call off the jam, send the RightSeat to jump seat, and fly the plane.
Even in Normal Law this would have brought the aircraft to the edge of stall - those inputs were not only in excess of what was required, but also in excess of what was sensible. Discussion of control laws is a red herring, because it has absolutely no bearing on why those inputs were so inappropriately excessive in the first place.
Early on, we were treated to closeup video of short finals/touchdown, the pilots handling were stirring mayonnaise, yet the camera outside showed the a/c virtually on rails, very impressive, to see such stickwork. Now that means they were: Johnny Ace, able to fly through anything on a rail, or a forgiving a/c, smoothing stck to find a stable path.
All due respect, the stick was excessive, and the a/c shone brightly as a sweetie.
So I am calling mayonnaise on Bonin, him thinking the ship would smooth his "whatever" stickwork into grease....e thought he was in NORMAL, and made no effort to modify his stick inputs to a LAW of which he was unaware?
LAW has everything to do with everything, in those first twenty seconds. it took the a/c some seconds to load up, and go up, and once committed, no one would be able to suss her attitude. So think DIRECT in roll, and ask: Would this pilot, aware of his AL DIRECT ROLL, act as if he was low, and the a/c made him look good? I say no, and so I conclude his handling bespoke NORMAL, with protections. At 2:10:22, when PNF says "....ALTERNATE LAW", I think he was preoccupied, no, I KNOW he was preoccupied. Why? A pilot who does not know whether he is climbing, at Mach .80, or descending, has not thought of which LAW obtains. So my case is based on: STARTLE (agree?), loss of scan, loss of orientation, and loss of the plot.....This in the first twenty seconds, max. The only save was for the PNF to take over. He didn't. The rest is merely interesting, but the game was over quickly. The PNF and later the Captain, failed, for whatever combination of reasons, to call off the jam, send the RightSeat to jump seat, and fly the plane.
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And you're not answering my question. You've got five failure modes there (you didn't bold "In the event of temporary loss of all electrical control:"), only one of which is relevant to the case we're discussing and two or three of which have never actually cropped up on the line. From a piloting perspective the only significant failure mode that requires a different approach entirely is mechanical reversion (i.e USE MAN PITCH TRIM ONLY).
Knowing what those modes mean is helpful, but not crucial. The only thing that *is* crucial is that outside Normal Law there are no protections and as such, more care must be taken.
And the main problem is, that you normally donīt fly that thing, but you are being flown while monitoring. Except when the sh*t hits the fan.
So I am calling mayonnaise on Bonin, him thinking the ship would smooth his "whatever" stickwork into grease....e thought he was in NORMAL, and made no effort to modify his stick inputs to a LAW of which he was unaware?
it took the a/c some seconds to load up, and go up, and once committed, no one would be able to suss her attitude.
... so I conclude his handling bespoke NORMAL, with protections.
A pilot who does not know whether he is climbing, at Mach .80, or descending, has not thought of which LAW obtains.
So my case is based on: STARTLE (agree?), loss of scan, loss of orientation, and loss of the plot.....
This in the first twenty seconds, max. The only save was for the PNF to take over. He didn't.
...
The PNF and later the Captain, failed, for whatever combination of reasons, to ... fly the plane.
...
The PNF and later the Captain, failed, for whatever combination of reasons, to ... fly the plane.
I suspect that even after the final report is published, the HF and psychology experts are going to be poring over this one for decades - in terms of complexity it is every bit as morbidly fascinating as KLM4805.
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Hi,
The final report will be certainly interesting (more than about thirty days to wait if the schedule of the BEA is respected)
It certainly will conclude with recommendations to avoid such accidents in the future
The trial has come (when ?) will be equally interesting .. but will concentrate more on what could possibly be done before the accident to prevent such a tragedy
The BEA will say what to do .. the trial will probably tell what it should have been done before and why
The final report will be certainly interesting (more than about thirty days to wait if the schedule of the BEA is respected)
It certainly will conclude with recommendations to avoid such accidents in the future
The trial has come (when ?) will be equally interesting .. but will concentrate more on what could possibly be done before the accident to prevent such a tragedy
The BEA will say what to do .. the trial will probably tell what it should have been done before and why
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Machinbird,
I agree with your general comment made on post #850
But it is still interesting to note that on both events you refer to, each time a pilot by his initial action on the sidestick probably tried to correct an attitude that was at least 3 degrees below what the attitude in cruise usually is.
Also, in the AF447 case, a level bust could be understandable and considered as normal as the memory item for UAS states to initially adopt 5 degrees of positive attitude.
I think the disconnection with the altitude became flagrant just later on, when the FD bars reappeared. The crew just didnt process the altitude when the PF instinctively decided to follow that unrealistic vertical command.
So I agree, if a guy, on a regular base, was manually leveling off at 350, he would deeply assimilate what is the necessary scanning and which level of inputs on the controls are acceptable.
I agree with your general comment made on post #850
But it is still interesting to note that on both events you refer to, each time a pilot by his initial action on the sidestick probably tried to correct an attitude that was at least 3 degrees below what the attitude in cruise usually is.
Also, in the AF447 case, a level bust could be understandable and considered as normal as the memory item for UAS states to initially adopt 5 degrees of positive attitude.
I think the disconnection with the altitude became flagrant just later on, when the FD bars reappeared. The crew just didnt process the altitude when the PF instinctively decided to follow that unrealistic vertical command.
So I agree, if a guy, on a regular base, was manually leveling off at 350, he would deeply assimilate what is the necessary scanning and which level of inputs on the controls are acceptable.
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@CONF iture
"So I agree, if a guy, on a regular base, was manually leveling off at 350, he would deeply assimilate what is the necessary scanning and which level of inputs on the controls are acceptable.
Absolutely. One cannot discourage manual control at altitude, and then, after something happens, blame the airman for less than sharp high altitude skills.
"So I agree, if a guy, on a regular base, was manually leveling off at 350, he would deeply assimilate what is the necessary scanning and which level of inputs on the controls are acceptable.
Absolutely. One cannot discourage manual control at altitude, and then, after something happens, blame the airman for less than sharp high altitude skills.
Last edited by Lyman; 23rd May 2012 at 04:23.
DW
Quote:
Originally Posted by RetiredF4
Yes, if you are a pilot and understand, how flying itself and management of abnormal situations is functioning in a human brain in opposition to an electronic gadget designed by engineers you will find some points to think over.
Quote:
Originally Posted by RetiredF4
Yes, if you are a pilot and understand, how flying itself and management of abnormal situations is functioning in a human brain in opposition to an electronic gadget designed by engineers you will find some points to think over.
DW
How many times can I say this before it sinks in? The Airbus FBW system was designed by a group that included pilots.
How many times can I say this before it sinks in? The Airbus FBW system was designed by a group that included pilots.
We human pilots have the tendency to grasp all available information at once and in a sum and draw the nearest conclusion out of the available information, the knowledge and our personal expierience. We start problem solving with the nearest probable cause, which might be wrong. The more possibilities there are, the greater the danger to start with the wrong conclusion.
Back to the different laws, if those are not displayed in detail by the system, the degradation of subsystems is not clearly recognizable in such a human thinking process. Itīs not only normal and alternate and direct as you say, its complicated as the excerpt of the manual in my previous post clearly points out.
DW
And you're not answering my question. You've got five failure modes there (you didn't bold "In the event of temporary loss of all electrical control:"), only one of which is relevant to the case we're discussing and two or three of which have never actually cropped up on the line. From a piloting perspective the only significant failure mode that requires a different approach entirely is mechanical reversion (i.e USE MAN PITCH TRIM ONLY).
And you're not answering my question. You've got five failure modes there (you didn't bold "In the event of temporary loss of all electrical control:"), only one of which is relevant to the case we're discussing and two or three of which have never actually cropped up on the line. From a piloting perspective the only significant failure mode that requires a different approach entirely is mechanical reversion (i.e USE MAN PITCH TRIM ONLY).
DW
Knowing what those modes mean is helpful, but not crucial. The only thing that *is* crucial is that outside Normal Law there are no protections and as such, more care must be taken.
Knowing what those modes mean is helpful, but not crucial. The only thing that *is* crucial is that outside Normal Law there are no protections and as such, more care must be taken.
DW
Quote originally RF4
And the main problem is, that you normally donīt fly that thing, but you are being flown while monitoring. Except when the sh*t hits the fan.
Quote originally RF4
And the main problem is, that you normally donīt fly that thing, but you are being flown while monitoring. Except when the sh*t hits the fan.
DW
That is the fault of the industry, not the aircraft or the systems. Even then what you're saying is untrue unless you take a very narrow definition of "flying" to mean direct surface connection, because the flight computers will do whatever the pilot requests them to do (just as their electro-mechanical/hydraulic predecessors did) unless what the pilot requests threatens to damage the aircraft.
That is the fault of the industry, not the aircraft or the systems. Even then what you're saying is untrue unless you take a very narrow definition of "flying" to mean direct surface connection, because the flight computers will do whatever the pilot requests them to do (just as their electro-mechanical/hydraulic predecessors did) unless what the pilot requests threatens to damage the aircraft.
When faced with a sudden failure the knowledge of the nature and detail of the failure and the consequences of failures is paramount. Under that view its best to keep things simple, limited to few cases to aid in a quick and effective decision making process.
At the moment it seems to be a graceful degradation (from the engineering point of view as you say), which keeps the system on the highest possible level, but it is prone to misunderstandings by the human monitor and operator called pilot. A gradual degradation with few and easy understandable steps could be easier understood and could reduce the error possibility.
Go back to the previous threads, how much we all discussed here the different laws and sublaws and their consequences to input and output systems (Autopilot, FBW-System, protections, flightcontrols...), how many wrong statements had been written about them, and we all learned from these errors.
But again, i only wanted to clarify, that the graceful degradation of the Flightlaws is not that easy to understand like you say here. My personal oppinion, all others are entiteled to a different one.
Last edited by RetiredF4; 23rd May 2012 at 14:14.
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So my case is based on: STARTLE (agree?), loss of scan, loss of orientation, and loss of the plot.....This in the first twenty seconds, max. The only save was for the PNF to take over. He didn't. The rest is merely interesting, but the game was over quickly. The PNF and later the Captain, failed, for whatever combination of reasons, to call off the jam, send the RightSeat to jump seat, and fly the plane.
Now, if you would admit that the startle factor doesn't necessarily need (as shown is another AF widebody from Caracas, which made it to Paris) another aircraft malfunction (beside those we already know i.e. pitot freezing & consequences), it would be terrific.
roulishollandais, I was sarcastic at one point, but didn't try to show too much cynism. Perhaps a translation issue? My concern was about the idea about asking pilots to fly manually in RVSM space: With current mean flying levels, I'm afraid it will lead to mid-airs (or airproxes, at last) far too often to be acceptable. I would prefer it was possible to have every crew in the airliner world being able to do this (pretty basic, when you think about it), but when it come to be reliable upon a long period of time, and detecting/alerting as soon as reliability cannot be assured, I'm sorry but we must face it : a computer (never tired, never distracted) do that better than a human being.
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Franzl
It all comes down to training and knowing you machine does it not? This removes any misunderstanding of the laws. Then you throw CRM into the mix and you have an solution
It all comes down to training and knowing you machine does it not? This removes any misunderstanding of the laws. Then you throw CRM into the mix and you have an solution
Absolutely correct.
But when we or the manufacturer comunicate like DW the asessment, that it flies in the gracefull degraded modes like in normal mode, then we will never get the management to improve the training and knowledge to the required standards.
But when we or the manufacturer comunicate like DW the asessment, that it flies in the gracefull degraded modes like in normal mode, then we will never get the management to improve the training and knowledge to the required standards.
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That's not what I said, and it's not what Airbus say either. What *I* said was that the Alternate flight law was designed to handle as as closely to Normal Law as possible despite the failures that caused the drop to Alternate.
Obviously it can't be exactly the same because there's a failure.
Obviously it can't be exactly the same because there's a failure.
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OC I'll put it as simplistically as you have....
Airbus: Oversold, Undersupported. Grasp>Reach.
Doze: "That's not what I said, and it's not what Airbus say either. What *I* said was that the Alternate flight law was designed to handle as as closely to Normal Law as possible despite the failures that caused the drop to Alternate.
In this paragraph is the heart of the flaw in the architecture.....
To wit: "Hide the problem"......
Airbus: Oversold, Undersupported. Grasp>Reach.
Doze: "That's not what I said, and it's not what Airbus say either. What *I* said was that the Alternate flight law was designed to handle as as closely to Normal Law as possible despite the failures that caused the drop to Alternate.
In this paragraph is the heart of the flaw in the architecture.....
To wit: "Hide the problem"......
Last edited by Lyman; 23rd May 2012 at 16:03.
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Originally Posted by Old Carthusian
It all comes down to training and knowing you machine does it not? This removes any misunderstanding of the laws.
DW Quote:
Originally Posted by RetiredF4
But when we or the manufacturer comunicate like DW the asessment, that it flies in the gracefull degraded modes like in normal mode.
Originally Posted by RetiredF4
But when we or the manufacturer comunicate like DW the asessment, that it flies in the gracefull degraded modes like in normal mode.
DW
That's not what I said, and it's not what Airbus say either. What *I* said was that the Alternate flight law was designed to handle as as closely to Normal Law as possible despite the failures that caused the drop to Alternate.
Obviously it can't be exactly the same because there's a failure.
That's not what I said, and it's not what Airbus say either. What *I* said was that the Alternate flight law was designed to handle as as closely to Normal Law as possible despite the failures that caused the drop to Alternate.
Obviously it can't be exactly the same because there's a failure.
How about your statement below? (Bolding by me)
DW
The point I was making was that you don't need to know the specifics as far as Alternate Law is concerned - fly the thing as you would normally fly it, just don't expect the protections to be there.
The point I was making was that you don't need to know the specifics as far as Alternate Law is concerned - fly the thing as you would normally fly it, just don't expect the protections to be there.
Last edited by RetiredF4; 23rd May 2012 at 16:12.
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No-one has addressed the point I made that the inputs made by the PF were wildly inappropriate for the circumstances, whatever the control law. Getting hung up on control laws and degradation distracts from the far more worrying fact that AF (and probably several other airlines) was routinely sending crews up in which two-thirds of the flight crew had no training in high-altitude manual handling.
The whole point of the flight-deck design in cost-saving terms was purely related to streamlining conversion training between types - it was never intended to give airlines an excuse to cut back on any other type of training.
@franzl - I think something might be lost in translation. "Fly ... as you would normally" is not the same as "It flies the same as in Normal Law" - the first statement refers to how the human should approach things ("Du sollst") and the latter describes the aircraft's behaviour ("Es verhält sich") - albeit inaccurately.
Last edited by DozyWannabe; 23rd May 2012 at 16:31.