Air Asia Indonesia Lost Contact from Surabaya to Singapore
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I read that the FO was flying at the time of the crash, but I also read that the Captain took over, when they started to climb. This mixes things up. Do they mean that the Captain held the stick back until they stalled, or the FO? Maybe it wasn't the FO's fault after all? Maybe the leaked information is no good (who'da thought it?). I'd like to know if they tried using the apparently oft forgotten trim wheel to get their AoA under control.
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Out of curiosity - what is the 'French Quirk' described by Raanim and NoD?
Been flying the Bus for a couple of year now and never heard of it...
Been flying the Bus for a couple of year now and never heard of it...
The one later referred to it, when you go OP CLB, instead of smartly going to CLB power, and pitching for Climb Speed, it sometimes does nothing with the power, or even takes it off. It seems to be unsure of whether to "enter" the climb by leading with power or pitch? Some P2s fool it by winding the speed up for a bit, I just make some offensive remark about it's abilities and await it sorting it's life out (which it eventually does).
N O D. I have never heard of the Frenck Quirk, but I have seen it pitch for climb speed before adding power if you are going faster than climb speed. That is how I was taught to fly a light plane although it never made much sense.
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Originally Posted by NOD
The one later referred to it, when you go OP CLB, instead of smartly going to CLB power, and pitching for Climb Speed, it sometimes does nothing with the power, or even takes it off.
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One function of OP CLB is to maintain maximum climb thrust when A/THR is active
It wasn't be who brought it up BTW!
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NOD I think what you're referring to is when flying a higher selected speed than cost index climb speed in the FMGC whilst level, then getting a climb clearance and pulling open climb then managing the speed. It's your naughty FOs flying higher than company CI, increasing engine internal drag and wasting fuel. In this case it'll come back to idle. It gets me once every 6 months. Pushing EXPED then straight away pulling OPEN CLB or pushing CLB locks the thrust at CLB thrust and prevents this.
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Originally Posted by Gysbreght
I have been looking in vain for the maximum bank angle the AP uses. I thought it would be either 25 or 33 degrees. Do you know if there is such a limit?
If the AoB exceeds 45°, the AP will disconnect and the FD bars will be removed.
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I have been looking in vain for the maximum bank angle the AP uses. I thought it would be either 25 or 33 degrees. Do you know if there is such a limit?
However it seems quite happy to use up to 35deg to capture a Localizer
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Quote:
The one later referred to it, when you go OP CLB, instead of smartly going to CLB power, and pitching for Climb Speed, it sometimes does nothing with the power, or even takes it off.
What are you talking about ... One function of OP CLB is to maintain maximum climb thrust when A/THR is active.
The one later referred to it, when you go OP CLB, instead of smartly going to CLB power, and pitching for Climb Speed, it sometimes does nothing with the power, or even takes it off.
What are you talking about ... One function of OP CLB is to maintain maximum climb thrust when A/THR is active.
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"Veering left and wobbling" before the climb..
"Veering left and wobbling" before the climb..
Investigator: Co-pilot was flying AirAsia Flight 8501
Investigator: Co-pilot was flying AirAsia Flight 8501
Ertata Lanang Galih, a senior pilot and investigator, said after requesting permission to ascend, the plane was veering left and wobbling, CNN reported. Siswosuwarno said it then ascended to 37,400 feet in about 30 seconds, according to the broadcaster.
Hardly Never Not Unwilling
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[QUOTE] does the autopilot still have the "Expedite Climb" mode? [/QUOTE}
It does (actually a flight director mode) and it seeks to match climb thrust to green dot speed (roughly l/d max in the clean configuration). The engaged autopilot will grab on to the flight director and ride it up, but I don't think you'd ever see it command more than 4,000 fpm or so, even on the lightest 319.
I think I could rule out 'expedite climb' as a factor in this accident.
I agree that waiting till the investigation is complete before saying you know what happened is a good idea. But I feel pretty comfortable saying that a 6,000 fmp climb was not manually flown and involved some serious failure in the autoflight/reality interface.
It does (actually a flight director mode) and it seeks to match climb thrust to green dot speed (roughly l/d max in the clean configuration). The engaged autopilot will grab on to the flight director and ride it up, but I don't think you'd ever see it command more than 4,000 fpm or so, even on the lightest 319.
I think I could rule out 'expedite climb' as a factor in this accident.
I agree that waiting till the investigation is complete before saying you know what happened is a good idea. But I feel pretty comfortable saying that a 6,000 fmp climb was not manually flown and involved some serious failure in the autoflight/reality interface.
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More stuff of uncertain provenance:
AirLive.net: BREAKING Pilots of AirAsia #QZ8501 Disabled Critical Computers Moments Before AirAsia Crash
AirLive.net: BREAKING Pilots of AirAsia #QZ8501 Disabled Critical Computers Moments Before AirAsia Crash
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Originally Posted by NoD
So why sometimes does it take power off, or just do nothing, for 5-10s
But if you want to link a video to what you refer as a "French quirk" in the Airbus I'll be interested to watch it.
Originally Posted by Rananim
I read somewhere that when making a cruise climb in an Airbus and speed has been rolled back prior to climb THR set,that ATHR will actually command idle thrust.
I am used to FLCH/LVL CHG where full climb thrust is automatically commanded even if speed selector rolled back.
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Too bad the Indonesian Investigation Board refuses to indicate whether or not a full initial report on the crash will be released to the public.
Why am I not shocked.
Why am I not shocked.
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Trim and feel
When I first learnt to fly it was drummed into me that you used the controls to put the a/c where you wanted it and then trimmed out the stick forces - you did not use the trims to fly the a/c.
With hydraulic controls the manufacturers went to a lot of trouble to devise feel systems that told the pilot what he was doing. If you took the autopilot out and pulled the stick back then you would have to pull harder and harder to keep the nose up as the speed fell - there was a clue there!
Then along came FBW and we have a/c that no longer have feel but, worse still, trim the nose up as the speed falls with the a/p disconnected (sort of). Presumably someone decided that the feedback that feel provided was a waste of money or just impossible with a sidestick.
I flew t-tail jet airliners and we regularly hand-flew them because we enjoyed doing it and we were expected to be competent at it in the sim.
Incidentally I thought that pickle switches were used for dropping bombs.
With hydraulic controls the manufacturers went to a lot of trouble to devise feel systems that told the pilot what he was doing. If you took the autopilot out and pulled the stick back then you would have to pull harder and harder to keep the nose up as the speed fell - there was a clue there!
Then along came FBW and we have a/c that no longer have feel but, worse still, trim the nose up as the speed falls with the a/p disconnected (sort of). Presumably someone decided that the feedback that feel provided was a waste of money or just impossible with a sidestick.
I flew t-tail jet airliners and we regularly hand-flew them because we enjoyed doing it and we were expected to be competent at it in the sim.
Incidentally I thought that pickle switches were used for dropping bombs.
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Too bad the Indonesian Investigation Board refuses to indicate whether or not a full initial report on the crash will be released to the public.
It's possible, that the investigators just need more time to sort out why the computers were disabled prior to the incident, if that is indeed true. Why they were turned off, might not be evident at a glance.
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FDR - would the investigators please leak - "last recorded altitude"
I said very early on, when we first saw the ruptured pressure bulkhead, that the aircraft probably broke up, in the last few seconds, in the air, from overload, in a desperate pull-up.
I still think so, and I think the latest "information" could support that view.
The latest "information" - is that the "critical" computers were allegedly" switched off in the last few seconds.
That, if true, seems to me, to be consistent with a desperate last ditch attempt to force direct law.
How many seconds ? 5, 10, 15, 20 seconds ? The time is crucial.
Consider this hypothesis.
Out of control descending at around 12,000 feet per minute (to keep the numbers realisticly simple), which is 200 feet per second.
As best I can fathom, from weather reports at the time, local cloud base was probably about (verry rubbery) 1600 feet.
So, pop out of cloud - now visual, (it was just after local dawn) - 8 seconds to impact.
You, me, and every other pilot who has ever flown anything, are of course just going to sit there, fat dumb and happy, and just kiss our arses good-night.
Sure we will.
The other "information" that is out there, is interesting, not from what it said, but most pointedly, from what it did not say.
It is said that the fdr and cvr both stopped.
Two questions.
1. Did they stop simultaneously ?
(they were both mounted on the frames next to the missing ruptured sector of the pressure bulkhead).
(refer to the graphic showing the rupture outline on an installed bulkhead at post 1702 http://www.pprune.org/rumours-news/5...ml#post8819798)
2. What was the last recorded altitude ?
It will of couse be recorded as qnn, but we can convert it to local qnh from the met records.
Was it FL016, FL015, ..14, ..13, ..12, ..11, ..10, ..09, ..08, ....................... 01, ..00 ?
I may still be wrong of course.
I still think so, and I think the latest "information" could support that view.
The latest "information" - is that the "critical" computers were allegedly" switched off in the last few seconds.
That, if true, seems to me, to be consistent with a desperate last ditch attempt to force direct law.
How many seconds ? 5, 10, 15, 20 seconds ? The time is crucial.
Consider this hypothesis.
Out of control descending at around 12,000 feet per minute (to keep the numbers realisticly simple), which is 200 feet per second.
As best I can fathom, from weather reports at the time, local cloud base was probably about (verry rubbery) 1600 feet.
So, pop out of cloud - now visual, (it was just after local dawn) - 8 seconds to impact.
You, me, and every other pilot who has ever flown anything, are of course just going to sit there, fat dumb and happy, and just kiss our arses good-night.
Sure we will.
The other "information" that is out there, is interesting, not from what it said, but most pointedly, from what it did not say.
It is said that the fdr and cvr both stopped.
Two questions.
1. Did they stop simultaneously ?
(they were both mounted on the frames next to the missing ruptured sector of the pressure bulkhead).
(refer to the graphic showing the rupture outline on an installed bulkhead at post 1702 http://www.pprune.org/rumours-news/5...ml#post8819798)
2. What was the last recorded altitude ?
It will of couse be recorded as qnn, but we can convert it to local qnh from the met records.
Was it FL016, FL015, ..14, ..13, ..12, ..11, ..10, ..09, ..08, ....................... 01, ..00 ?
I may still be wrong of course.
Last edited by ventus45; 29th Jan 2015 at 21:16.