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-   -   AF447 Thread No. 3 (https://www.pprune.org/tech-log/452836-af447-thread-no-3-a.html)

hetfield 1st June 2011 12:29

Victims' families want to ground A330/340 fleet.

Air-France-Absturz: Hinterbliebene wollen Airbus-Flotte stoppen - SPIEGEL ONLINE - Nachrichten - Panorama

tubby linton 1st June 2011 12:32

A33Zab,I have emailed the journalist from Flight about the article.I will let you know the basis of his story when I have it

RealQuax 1st June 2011 12:34

..there is no such thing as elevator trim.

takata 1st June 2011 12:34


Originally Posted by Lonewolf_50
takata, I'll suggest to you that pilots know that because that is part of flying.

Again, I was addressing (only) the specific case of reversing from Normal law to Alternate (not general flying skills here, this is type/law related). This could explain the initial oscillation in roll that would be fixed by re-trimming the rudder due to this axis protection being released as it went direct.
Take it easy.

MartinM 1st June 2011 12:37

Takata wrote:

I'm pretty convinced now that there was an unknown factor involving instruments that fooled the PF, hence more specifically the Right Hand Seat which is feeded by ADIRU2. Also, by deduction, the pilot flying was David Robert, 37, with 6,547 flying hrs including 4,479 on type. He was by far the more experienced A330 jockey on the deck and was PF from take-off. His reaction was immediate, he was not asleep, and he should have been fooled by something.
No.Incorrect. Co-Pilot No2 was PF starting 1:55 according to BAE report may. Taken from the CVR. He took over Captains seat, left at 1:59.


A 1 h 55, le commandant de bord réveille le second copilote et annonce « […] il va
prendre ma place ».

Entre 1 h 59 min 32 et 2 h 01 min 46 Le commandant de bord quitte le poste de pilotage.
PF had 800+ hrs on this type.
NPF was David Robert

At 2h11, the captain took again the pilot seat. This was already in the decent.

Vers 2 h 11 min 40 , le commandant de bord rentre dans le poste de pilotage.
I deliberately took the french version, as the english translation contains some differences

Denti 1st June 2011 12:48

But the captain wasn't the pilot flying if i read the report correct, he was the PNF on that sector and the copilot 2 took over his place, as PNF.

Meikleour 1st June 2011 12:48

MartinM: If I can make a small contribution to this thread. I have flown the A330 in ALT 2 LAW after a twin ADR incident due to icing conditions.
What surprised me was how "twitchy" the aircraft was, especially in roll. The handling was much harder than I had experienced in the simulator during training. We however continued to have valid ADI indications with which to fly attitude + power whilst trying to sort out the very numerous ECAM warnings plus alternating "Stall, stall" + overspeed warnings (spurious of course)
Why the crew should have applied pitch up inputs is a mystery to me unless it was a response to a perceived large overspeed but then why leave the power up?

As mentioned by other posters - the need to manually trim the THS forward is an area that is often seen to be missed by crew undertaking unusual attitude recovery training, especially from very high nose up attitudes and is, in my opinion, one of the few `real gotchas` about the aeroplane.

sensor_validation 1st June 2011 12:49

@MartinM

I'm with takata all the way - are we reading the same document?

takata 1st June 2011 12:50

Hi Martin,

Originally Posted by MartinM
No.Incorrect. Co-Pilot No2 was PF starting 1:55 according to BAE report may. Taken from the CVR. He took over Captains seat, left at 1:59.

There is nothing in the French report saying that.
. At take off, Captain is PNF from his LHS; FOx is PF from RHS.
. At 0159, Captain go to rest and FOy takes his place (LHS) as PNF.
. AP2 is engaged, meaning that the aircraft is flown from RHS.
=> If the PF was FO2 at take off, FO1 would have taken his RHS (but he didn't).
It means that the PF at take-off was FO1 from his RHS (David Robert).

The ambiguity (and press belief) is due to this sentence "le commandant de bord réveille le second copilote"
But it takes to be a French native speaker to understand correctly that it doesn't mean "2nd Officer" but the other co-pilote (as they are two on board, it could be either copilot).

beachbunny 1st June 2011 12:58

Correction?
 
Takata,

Quote: His reaction was immediate, he was not asleep, and he should have been fooled by something.

Do you not mean, "he should [B]not[B] have been fooled by something?

A thought has crossed my mind, bearing in mind that we are talking about iced up pitots, maybe static systems, could it be that their altimeters were not unwinding like one would imagine, with a 10,000 fpm descent, and that their VSIs were also not responding to the descent? Possibly even showing a climb, when they were actually descending.

As I've mentioned earlier, a prolonged nose down input should have brought them out of the stall, but why would you do that, if there was no indication that the sea was getting closer...

MartinM 1st June 2011 13:00


There is nothing in the French report saying that.
. At take off, Captain is PNF from his LHS; FOx is PF from RHS.
. At 0159, Captain go to rest and FOy takes his place (LHS) as PNF.
. AP2 is engaged, meaning that the aircraft is flown from RHS.
=> If the PF was FO2 at take off, FO1 would have taken his RHS (but he didn't).
It means that the PF at take-off was FO1 from his RHS (David Robert).

The ambiguity (and press belief) is due to this sentence "le commandant de bord réveille le second copilote"
But it takes to be a French native speaker to understand correctly that it doesn't mean "2nd Officer" but the other co-pilote (as they are two on board, it could be either copilot).
rgr on this. Missleading in the german and english translation and i misread this in my french knowledge.

tubby linton 1st June 2011 13:01

I just received this from the Flight journalist:

This information – that the aircraft did not switch into abnormal flight law – has been confirmed by the investigating authority.

ttcse 1st June 2011 13:08

Meikleuor
"Why the crew should have applied pitch up inputs is a mystery to me unless it was a response to a perceived large overspeed but then why leave the power up?"

I'm wondering if at that point they believed they were in a serious downdraft.

Also, the only transcript of events I've seen must be omitting cockpit conversations. There is too little talking.

spagiola 1st June 2011 13:08


Incorrect. Co-Pilot No2 was PF starting 1:55 according to BAE report may. Taken from the CVR. He took over Captains seat, left at 1:59.

Quote:
A 1 h 55, le commandant de bord réveille le second copilote et annonce « […] il va prendre ma place ».
First, "Prendre ma place" can refer simply to the captain's physical position, ie his seat, not necessarily to his role.

Second, you forget that the captain was PNF. So even if the new arrival did take over the captain's current role, he would have become PNF.

There's enough ambiguity in the French version that your interpretation is possible, but to this native French speaker it seems more natural to read the report as saying that the initial PF remained PF.

Note, for example that it is the PF that conducts the briefing for the new arrival.

BluJet 1st June 2011 13:10

New here as a writer. Read almost every article on this tech-log thread#3. Thank you, for all the good ones!

@takata
post #931
Your deduction concerning the PF omits that the 800hr F/O was not qualified to fly in the L/Hseat (see first BEAreport). So for me, it could have only been the 32year old, 800hr F/O who was PF.
your post #908 and #934
whereas I appreciate most of your posts and your efforts to get the"specialists" back to the ground I want to make a few comments.
We train to use the rudder(trim) mostly for engine out and crosswind landings on transport category aircraft. Especially after some accidents, where airplanes had been taken apart by misuse of rudder. I know the FCOM suggests to do so in some cases, but had that improved their situation? The chances of making it worse are much greater. (I totally agree with post #937).

I dont know whether you are pilot (maybe engineer?) but if you have a chance, watch pilots performing the F/CTL check on ground after engine start. you will often find that few are moving elevator only, respectively ailerons only when performing this check. In other words there is a good chance (especially under stress and during turbulence) that you also move parts of flight-controls which you did not intend to move in the first place. And, as you wrote, those ailerons are powerful in ALT2.
Please don't get me wrong! I really appreciate your work!



The friday BEA report really makes me sick, the new discussion about whether the aircraft was in ABNORM ATT LAW or not is a good example. If not, why did they not provide this information on friday?
A lawyer would probably state that this report would imply "circular reasoning".

sensor_validation 1st June 2011 13:14

@tubby

And the French BEA now put out official releases via a reporter based in London?

Machinbird 1st June 2011 13:14

Meikleour

MartinM: If I can make a small contribution to this thread. I have flown the A330 in ALT 2 LAW after a twin ADR incident due to icing conditions.
What surprised me was how "twitchy" the aircraft was, especially in roll. The handling was much harder than I had experienced in the simulator during training. We however continued to have valid ADI indications with which to fly attitude + power whilst trying to sort out the very numerous ECAM warnings plus alternating "Stall, stall" + overspeed warnings (spurious of course)
Why the crew should have applied pitch up inputs is a mystery to me unless it was a response to a perceived large overspeed but then why leave the power up?

Thank goodness. Someone with A330 with Alt 2 law experience.

Meikleour. If you had been handed the aircraft in Alt 2 law, with substantial lateral imbalance (probably due to a rudder trim change), how do you think the aircraft would have flown then?

takata 1st June 2011 13:15


Originally Posted by beachbunny
Do you not mean, "he should [B]not[B] have been fooled by something

Sorry, poorly expressed. I meant consequently, he was fooled by something, as of course, he should not have, being fully alert and experienced.
In fact, I'm thinking that his persistance to do the same mistake all the way down would not find an explanation if his possibly wrong initial reaction was not inverted at some point, when considering all the time it takes and the two other pilots.

Very puzzling. If the THS did not trim down, there was no nose down.
I have no explanation so far and I wonder if this is not the reason why the BEA is refraining from publishing a lot more up to this point. It could take them a very long work to sort all this mess out.

MartinM 1st June 2011 13:26

BlueJet wrote:

Your deduction concerning the PF omits that the 800hr F/O was not qualified to fly in the L/Hseat (see first BEAreport). So for me, it could have only been the 32year old, 800hr F/O who was PF.
your post #908 and #934
This literally confirms my assumption

PF was the Co-Pilot No.2 with 800hrs on an A330.

There is another part in this while dialog which made me assume that PF has less experience, which does not mean he was a bad pilot.

At some point in the CVR transscript it gives me the impression that the PNF knew better in what situation they were.

And from the ranking, it would make sense to me to sit the higher rated co-pilot on the captain seat.

grity 1st June 2011 13:29


Lonewolf 50 Themental and congnitive process, when you are doing this on instruments (which I presume AF 447 crew were, as it was night and the Wx was bad) is to set an attitude in balanced flight and trim to hold that attitude in all three axes. (Plural of axis)

What I was taught and used to teach was to trim nose and rudder first, aileron last, to avoid cross trimming, but such technique is probably model dependent.
i understand that this is a target way to continue the flight, trim to hold altitude and speed as before

but with high altitude und UAS is it not much saver due to more aerodynamic stability to set trim for an auto-stable slow descent (flightpath mayby -3 deg?) with not so much trust, lower risk of unexpected climb, searching a lower FL with a major speed range, thinking about the CG ..... is it not much more essential to recover stability than constant altitude

BOAC 1st June 2011 13:30

I am now of the view that the BEA 27 Mai release was bordering on mischievous - almost as if they were looking to see if they could fill PPRune with pages of posts (in which they succeeded).

Why did they miss out the obvious discussion early in the event when the a/c started climbing like a rocket above OPT and probably above MAXALT? Any pilot, even just out of training and on line, would know that that could well be be a one-way ticket to the bottom of the Atlantic, and so where is the "What on earth are you doing" from PNF or "I cannot control the attitude" from PF or whatever? Are we to infer from this omission that
a) It did not happen OR
b) That to tell us is less important than the CVR confirmation that they have duff airspeed, which we already know from ACARS?

What are the BEA playing at?

Last question for AB people - does the reported lack of abnormal law mean a software error here or is it possible the AoA vanes had gone west too? The altimeters/VSIs too? For heaven's sake, was the Pitot heat actually working?

MartinM 1st June 2011 13:33

Another irritating and concerning thing at FL100, when both pulled on the SS simultaneously, I have the bad feeling that they saw the ocean coming close. I think that was just a last try to save something without too much hope.

Back to the technical stuff. AFAIK there is only one SS active at a time. You have to push a button to take over.

Is Alternate Law 2 allowing dual SS input or were they eventually already degraded to mechanical law?

Clandestino 1st June 2011 13:40


Originally Posted by MartinM
All I try is to figure out what made him pull after disconnecting the AP.

The right person to answer that would be capt Marvin Renslow as he's the only one known to perform the similar feat. Unfortunately, neither he nor his F/O are able to tell us what were they thinking as their aeroplane pitched up and stalled.

It's debilitating fatigue, suckers!

@BOAC: 1. agree with your view on BEA "report", 2. We'll have to wait for proper report, with full DFDR traces and CVR transcript, to see whether it was simple software mess-up or not 3. pitot heat was almost certainly on - high altitude ice sticks to heated parts, like probes and engine compressors.

737-NG 1st June 2011 13:45

Translating from French means the Captain comes INTO the cockpit but he was no in his seat!

takata 1st June 2011 13:45

Hi BluJet,

Originally Posted by BluJet
Your deduction concerning the PF omits that the 800hr F/O was not qualified to fly in the L/Hseat (see first BEAreport). So for me, it could have only been the 32year old, 800hr F/O who was PF.

Yep, I didn't catch that!
About the rudder, I should have expressed something wrongly but I didn't remember what! Then, my intention was obviously not perfectly understood.
Thanks anyway for you nice comments and informative imput.

paull 1st June 2011 13:53

How much height would you need to fix it?
 
PNF took over at 2:13:32 + 15seconds, i.e. 41 seconds before the end and perhaps between 7000-7500 feet.
Even if you did all the right things, when is the latest you can act?
How would that differ if the trim was neutral?

Well, this is Tech-Log :)

Graybeard 1st June 2011 13:53


Meikleour

Join Date: Jul 2007
Location: uk
Posts: 161


..If I can make a small contribution to this thread. I have flown the A330 in ALT 2 LAW after a twin ADR incident due to icing conditions. ...

Was this event reported and investigated after landing? Do you have FDR traces that would help understand AF447?

Capn Bloggs 1st June 2011 13:55


Originally Posted by MartinM
Back to the technical stuff. AFAIK there is only one SS active at a time.

Wrong. They sum. Google Airbus Sidestick.

robertbartsch 1st June 2011 14:02

The new report is missing any discussion between the crew related to the stall condition. As written, it appears they did not know for 3.5 minutes that the plane was stalled.

Is that possible?

sensor_validation 1st June 2011 14:11

@Blujet, takata et al.

With respect to who was flying from where do you now challenge the previous 'agreement' between PJ2 and Lemurian summarized in this old post?

http://www.pprune.org/tech-log/44963...ml#post6452307

DozyWannabe 1st June 2011 14:15


Originally Posted by Capn Bloggs (Post 6487116)
Wrong. They sum. Google Airbus Sidestick.

They sum *if used together*, this is true. But using the sidesticks together is not normal procedure and the systems will notify the crew with a "DUAL INPUT" annunciation.

Correct procedure dictates that upon passing of control from one seat to the other, immediately following or simultaneous with the "I Have Control/My Aircraft" callout, the stick selector button at the base of the stick is pushed. There is no reason to have two pilots on the sidesticks at the same time.

The evidence so far suggests that but for a second or so, this procedure was followed correctly.

@BOAC : I think the BEA "note" was released purely to alleviate the press "leaks" that were proliferating prior to release. Far better for us internet folks to be speculating with a limited amount of real data (which I suspect is all that they had confirmed at the time) rather than trying to sift through a mountain of press twaddle, don't you agree?

BOAC 1st June 2011 14:18


Originally Posted by paull
How much height would you need to fix it?

- more than that. In my military days it was a given that if you were not starting a successful recovery from a spin (mentioned because of similar descent rates ONLY!) by 10,000 ft you ejected. I suspect it would have been significantly higher for this a/c - 10,000 fpm gives you 1 minute only and I suspect the wings would have come off or the g limited so it would have crashed form 10,000ft. Purely a ball park guess - if a correct attitude change had not been made by 20,000 ft it would be a done deal.

spagiola 1st June 2011 14:28


PNF took over at 2:13:32 + 15seconds, i.e. 41 seconds before the end and perhaps between 7000-7500 feet.
Even if you did all the right things, when is the latest you can act?
We are not told what, if anything, the new PF did after the handover, but the strange thing is that this handover does not appear to have changed much, as vertical velocity at impact (41 seconds later) was still over -10,000fpm.

BOAC 1st June 2011 14:29


Originally Posted by dozy
a mountain of press twaddle

- I have never considered the 'media' here - I am referring to the 'selective' release of inter-crew conversation from the CVR, no doubt, not the media.

RealQuax 1st June 2011 14:29

@MartinM, please! Respecting, that non-pilots and even non-experts can add good and valuable inputs to this discussion: Leave answers to questions about technical subtleties of the A330 to the ones who either fly her or know her intimately.

Me, having 10.000hrs+ on A330/A320 am still stunned about what happened there and am still learning a lot of specificities, which I didn't know yet about my aircraft and the environment, I am operating in.

As Regards those who criticise BEA for their restrictive publication-policy:
Having negotiated company agreements regarding data protection for my fellow pilot-brothers in my company and the association:

I pretty much appreciate the strictly factual way they publish: We see what crap newspapers and self-nominated experts already read out of these factual reports and publications. If it was me involved in such an accident, I would really appreciate that it is the real experts, officially tasked by the text, at least spirit of ICAO annex 13, who get the detailed informations, stick to the facts and publish only those after due consideration which explain what happened in order to help making aviation safer.

MartinM 1st June 2011 14:30

@Captn Bloggs: Thanks for the refresher.

There is no obvious advantage to go on dual-input


During normal operation both side sticks are active and associated signals are algebraically added; however, flight control parameters are not exceeded during dual side stick inputs. The pitch control of the electronic flight control system is a load demand system. In clean configuration, maximum pitch up command is +2.5 G and maximum down command is -1.0 G

BOAC 1st June 2011 14:30


Originally Posted by robertrbartsch
Is that possible?

- missed the last 50 pages?:ugh:

takata 1st June 2011 14:31


Originally Posted by sensor_validation
With respect to who was flying from where do you now challenge the previous 'agreement' between PJ2 and Lemurian summarized in this old post?

No. At first glance, this is how I deduced that the RHS would be occupied by the FO1 (David Robert) and Blujet shed a doubt on the LHS qualification issue.
From what Lemurian already said, based on AF operations, it was almost certain that FO1 would be PF or PNF (with Captain PF) always from RHS and that the FO2 would take the LHS at cruise as PNF when the FO1 was PF.

This was confirmed by PJ2 also:

Originally Posted by PJ2
Yes, understand - the procedures I am familiar with are the same, except perhaps that for the Relief Pilot position, AF uses First Officers who are licensed to sit in the RHS? Regardless, at some point, the F/Os doing the relief for one or the other two crew members will have to sit in the LHS but this would only be in cruise flight. By your statement I believe you mean that F/O's are not allowed to sit in the LHS for takeoff or landing, and that is the way I am familiar with. The Relief Pilot does not sit in either the LHS or RHS until the aircraft is in the Cruise phase of flight...that would be top-of-climb to top-of-descent.

Consequently, the LHS qualification for this part of the flight should not be taken into consideration: PF could actually have been FO1 (Robert) from RHS with FO2 (Bonin) as PNF from LHS, while the Captain was resting.

EDLB 1st June 2011 14:53


Even if you did all the right things, when is the latest you can act?
How would that differ if the trim was neutral?
If the THS would be in neutral position my gues is that they stood a chance even at 7500 feet MSL. The total velocity unfortunately mostly downward was enough to fly and create lift, if they only where able to get the nose down in the flight pass direction. Sort of in the downward part of a loop. Would not even be a real high G maneuver. They where only in a stall not in a spin.
Unfortunately the THS was still in a 13 degree upward position and if it takes a minute for the THS to get to neutral then they had no chance at all even at 15000 feet.

My 2 cents

rgbrock1 1st June 2011 14:56

RealQuax wrote:


Me, having 10.000hrs+ on A330/A320 am still stunned about what happened there and am still learning a lot of specificities, which I didn't know yet about my aircraft and the environment, I am operating in.
Sir. As captain of the A330 have you ever yourself experienced pitot tube icing and, if so, what happend and how did you react?


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