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-   -   Air Asia Indonesia Lost Contact from Surabaya to Singapore (https://www.pprune.org/rumours-news/553569-air-asia-indonesia-lost-contact-surabaya-singapore.html)

peekay4 26th Nov 2015 14:39

It is possibly relevant, but as a background, AD 2014-0217 was originally issued in mid-2014 (before the AirAsia accident) in response to the AA587 A300-600 accident in Queens -- referred to in the AD as "one accident on another aircraft type" -- and a second incident on an A319. The AD added logic to reduce tail plane stress and to activate a Stop Rudder Input Warning (SRIW) function.

The AD quoted above (2014-0217R1) was a revision to update the minimum FAC part numbers required to support SRIW. This revision was requested by Airbus because the original AD had left out a couple Service Bulletins. (The updated SBs were also issued before the AirAsia accident).

Now according to rumors... on the accident aircraft both FACs were shut-off simultaneously, possibly via circuit breakers. If true, then the above AD is a moot point really. The FACs can't provide protections if they are turned off.

So although the AirAsia accident might have involved rudder limits, the above AD was not released in response to this accident, and the promulgated changes even if implemented wouldn't have had any bearing on the accident's outcome.

Machinbird 26th Nov 2015 16:39


and to activate a conditional aural warning within the flight warning computer (FWC) to further protect against pilot induced rudder doublets.”
Great.:rolleyes:
Another sound that the pilot has to respond to immediately, probably under conditions of great stress.:mad:

peekay4 26th Nov 2015 17:17

It's "only" a warning... the FAC should automatically limit rudder loads regardless of pilot response.

airman1900 27th Nov 2015 12:45

From the BBC, 27 November 2015:

AirAsia shares slide on poor earnings results - BBC News


Next week, Indonesia's national transport safety board is expected to announce the findings of AirAsia's deadly crash that occurred in December 2014 ...

Data Guy 28th Nov 2015 06:55

Some FAC Rudder Faults
 
Just *Some FAC computer failure SDRs.


(*Data is limited because SDR non-reporting is still running at over 60 % for this year).

12 A-300 Series SDRs /Problem Descriptions / (Cause) FAC Computer / Part Number (P/N).

Briefs Only.See SDR Full Texts at FAA Query, Link > http://av-info.faa.gov/sdrx/Query.aspxJust enter SDR Number, and Hit Query.

3/20/14.SDR # and Link > USAA2014032100017 “Tail kicked, bumped multible times”. P/N B397BAM0513.
6/30/13.SDR # and Link > USAA2013070100015 “Banked, Felt in Rudder Pedals”. P/N B397BAM0513.
6/3/13. SDR # and Link > USAA2013060400023 “Uncommandedmomentary input”. P/N B397BAM0513.
12/7/12. SDR # and Link > USAA2012121000012 “Yawed – 5 seconds”.P/N B397BAM0513.
8/10/12. SDR # and Link > USAA2012081300019 “Fast uncommanded movement”. P/N B397BAM0513.
7/25/12. SDR # and Link > UALA2012072704071 “Uncommanded movement”. P/N B397BAM0513.
4/19/10. SDR # and Link > UALA2010041901293 “Substantial yaw”.P/N 3945128206.
3/19/11. SDR # and Link > UALA2011032101332 “Sudden yaw movement’. P/N B397BAM0513.
2/2/10.SDR # and Link > UALA2010020300427 “Yaw felt in cockpit”.P/N B397BAM0513.
4/14/09.SDR # and Link > CA090421011“Rudder kick, veered on runway”. P/N B397BAM0513.
5/13/07.SDR # and Link > NWAA071863251“Hard rudder kick”.P/NB397BAM0515.
12/3/02.SDR # and Link > AALA20021725 “Yawed Several Times”. P/NB471AAM7.Also see ASRS Report # 567765, - “61 PRIOR EVENTS”.


End --

Machinbird 30th Nov 2015 18:19

QZ8501 WARMUP
 
We must be getting close. The local news is in anticipation of the accident report:
AirAsia QZ8501 crash findings expected on Tuesday - Channel NewsAsia

peekay4 30th Nov 2015 18:27

Per earlier report (last page), the NTSC press conference is still scheduled for December 1, 2pm Jakarta time (less than 12 hours from now...)

wheels_down 1st Dec 2015 06:10

To sum up the report in three words.

Rubbish Training standards. In all corners of their business.

_Phoenix 1st Dec 2015 06:30

Again, blame the dead - flight crew action resulted in inability to control the aircraft ...

JAKARTA - REUTERS, Indonesian investigators said on Tuesday that crew action caused a loss of control and the stalling of an AirAsia passenger jet that crashed into the Java Sea last year, killing all 162 aboard.
The plane's flight control computer had a cracked solder joint that malfunctioned repeatedly, including four times during the flight, and 23 times the previous year.
"Subsequent flight crew action resulted in inability to control the aircraft ... causing the aircraft to depart from the normal flight envelope and enter a prolonged stall condition that was beyond the capability of the flight crew to recover," the national transport safety committee said in a statement.
Final report is released:
http://kemhubri.dephub.go.id/knkt/ntsc_home/ntsc.htm

marchino61 1st Dec 2015 06:49

Forensics
 
Wow!

I'm impressed - no joke! - that they can detect a cracked solder joint when a plane crashes into the sea with what was probably very high deceleration.

dr dre 1st Dec 2015 07:01

I think this quote from the report sums it up:


The Upset Recovery training was included in the aircraft operators training manual. The aircraft operator advised the KNKT that the flight crew had not been trained for the upset recovery training on Airbus A320, and this referred to FCTM Operational Philosophy: “The effectiveness of fly-by-wire architecture, and the existence of control laws, eliminates the need for upset recovery maneuvers to be trained on protected Airbus”. There was no evidence of DGCA findings for this incompliance of training.

peekay4 1st Dec 2015 07:14

Summary:
  • Aircraft had a history of numerous Rudder Travel Limiter Unit faults which were never resolved
  • During the accident flight, the crew received three consecutive Master Cautions related to the RTLUs, which they cleared via ECAM actions
  • After a fourth Master Caution, FAC 1 & 2 were reset by pulling the Circuit Breakers
  • The aircraft went to Alternate Law
  • Aircraft rolled 54 degrees left
  • FO applied sidestick input to roll right and pitch up
  • FO continued to pitch up as the aircraft zoomed to 38,000 ft at 11,000 fpm
  • Aircraft entered a stall
  • FO continued to apply maximum pitch up (until the end of recording)
  • Captain attempted to take over by pressing the left-sidestick priority button for 2 seconds (*)
  • DUAL INPUT activated and the aircraft continued to pitch up
  • Captain attempted another take over by pressing the sidestick priority button for 2 seconds (*)
  • Aircraft recorded lowest speed of 55 kts, 104 degrees left roll, and then descended at up to 20,000 fpm until the end of recording
(*) The sidestick priority button doesn't latch unless it is activated continuously for 40 seconds

ironbutt57 1st Dec 2015 07:20

"Push" vs "pull" seems to have contributed to the obvious confusion

PastTense 1st Dec 2015 07:28

"Issues such as flight approval considered did not contribute to the accident and was not investigated. The FDR data did not show any indication of the weather condition affecting the aircraft."

In the earlier discussion in this thread there was a feeling that bad weather was a significant factor.

ZFT 1st Dec 2015 07:28

wheels down


To sum up the report in three words.

Rubbish Training standards. In all corners of their business.
If we are honest, I don't think anyone has done a particularly good job with UPRT or extended stall envelope so far, whether it be regulators, OEMs, Training Organisations, TDMs or Airlines. Lots of talk , many committees etc these past years but not much concrete action.

Organisations such as ICATEE have been around for a long, long time now yet there is very limited progress at the delivered end of the training business.

How many crews today could really state they have received comprehensive UPRT or stall training? I would hazard a guess that not that many.

jcjeant 1st Dec 2015 07:40

Hi,

Summary:
Remake AF447
Not the same root cause .. but the same effects
Pull on the joystick with stall alarm all the way down ....
How many deaths will be needed for that ...

Right Way Up 1st Dec 2015 07:47

Resetting FACs by CB inflight......not sure I have seen that written down anywhere? :ugh:

tripilot 1st Dec 2015 08:02

I'm not an A'bus pilot (Boeing only)but I'd be keen to know what the QRH / ECAM response should have been to this repeated warning? I'm pretty sure it isn't to reset a CB in flight.

Cripple 1st Dec 2015 08:04


Originally Posted by Right Way Up (Post 9196923)
Resetting FACs by CB inflight......not sure I have seen that written down anywhere? :ugh:

Spot on. UPRT training (or lack of) is a red herring. Better UPRT could have allowed the crew to recover but there was no reason for the aircraft to end up in that position in the first place.

By use of this non standard cb reset on BOTH FACs, this crew (for whatever reason) put the a/c into ALTN LAW and their inputs subsequently put it into a position from which they could not recover.

In fact, not only is the FAC reset not included in the computer reset QRH table, the table also says (in a big red box) - WARNING DO NOT RESET MORE THAN ONE COMPUTER AT A TIME.

The RTLU fault is a non event. Following the ECAM drill would have stopped the nuisance cautions and the a/c would have been Cat 3A and perfectly flyable. Unless you need Cat 3B, why even try a reset? Especially after 3 previous faults that flight?

The aircraft remained perfectly flyable even after the crew actions disabled the FACs and after they lost control - at this point, UPRT became a potential factor - primarily for the FO though as it appears the CA was trying to make appropriate inputs to recover.

Ultimately though, if the crew had done nothing about the minor RTLU fault, the aircraft would not have crashed.

noske 1st Dec 2015 08:45


Originally Posted by tripilot
I'm not an A'bus pilot (Boeing only)but I'd be keen to know what the QRH / ECAM response should have been to this repeated warning?

The correct ECAM response is on page 15 of the report: reset both FACs, using the pushbuttons on the overhead panel.


Originally Posted by Cripple
The RTLU fault is a non event. Following the ECAM drill would have stopped the nuisance cautions and the a/c would have been Cat 3A and perfectly flyable.

Between 2300 and 2315, they suffered four failures of the RTLU, the time between the events decreasing from 9 to 4 and then 2 minutes. That's a lot of nuisance.


Originally Posted by Right Way Up
Resetting FACs by CB inflight......not sure I have seen that written down anywhere?

But when you consider the ground troubleshooting episode three days earlier that is described on pg. 21, it is understandable why the captain, in his growing frustration, decided to try it.

unworry 1st Dec 2015 08:53

@Cripple I wouldnt say its a red herring

Although clearly the crew contributed/created the upset, their inability to recover the plane - similar to AF447 - is of grave concern.



Originally Posted by peekay4
FO continued to apply maximum pitch up (until the end of recording)

:ouch:

Ranger One 1st Dec 2015 09:10

It shouldn't bloody matter how many computers you reset, in what order, or why, or what 'law' you end up in as a result.

A pair of ATPLs should be able to avoid stalling a basically serviceable aircraft into the bloody drink from FL380!

peekay4 1st Dec 2015 09:14


In fact, not only is the FAC reset not included in the computer reset QRH table, the table also says (in a big red box) - WARNING DO NOT RESET MORE THAN ONE COMPUTER AT A TIME.
As usual in most accidents, nothing is quite so simple.

1) The reset table in the QRH isn't limiting. The table only provides information about which computers are most prone to be reset. It does not mean other computers cannot be reset. The FAC is not listed among computers which are not allowed to be reset, and the caution against pulling certain CBs also do not list the FAC CBs.

2) The Captain did not reset both FACs at once. In fact he did them sequentially. FAC 1 was pulled at 2316:29 UTC and was re-energized by 2316:39. FAC 2 CB was only pulled seven seconds later, at 2316:46.

Unfortunately, even though FAC 1 had been re-energized, it was still inactive. Resetting the CB was not sufficient to reactivate the FAC, since the FAC's overhead pushbutton must also be toggled to OFF and then back to ON.

So even though the Captain had restored power to FAC 1, and its pushbutton was at the "ON" position, FAC 1 remained unavailable. When FAC 2 CB was pulled, the aircraft went into Alternate Law.

HundredPercentPlease 1st Dec 2015 09:15

Cripple,

There seem to be a few red herrings here. The important stuff seems to be:
  • They pulled the CBs (what were they thinking?).
  • Both watched the aircraft roll for 9 seconds to 54° without doing anything.
  • The FO zoom climbed with controlled (not full) backstick.
  • The CP is calling Pull Down repeatedly. The fatal language error?
  • From the stall, the CP is applying full roll with modulated pitch, the FO is applying full back stick with modulated roll.
  • The "stall stall" and "dual input" continue to the impact, with no effect on the crew.

The report is quick to point out that the FO is applying incorrect inputs, but reluctant to report that the CP is doing the same. They key graph is on page 51, with STKPC (decode: stick, pitch, capt).

I'm starting to think that we need to change the stall warning from "STALL STALL" "STALL whoop whoop PUSH DOWN". Or does the industry need a third full-backstick-until-impact event before we make changes?

plhought 1st Dec 2015 09:27


Originally Posted by Ranger One
It shouldn't bloody matter how many computers you reset, in what order, or why, or what 'law' you end up in as a result.

A pair of ATPLs should be able to avoid stalling a basically serviceable aircraft into the bloody drink from FL380!

+1 What he said.

oscarisapc 1st Dec 2015 09:32

I’m not an airline pilot but a medic. In the end result, this is a similar crash to AF447 in that there was a very distracted crew in an aeroplane that had its automatic protections off, who were then unable to recognise a pilot induced stall and kept the plane in a stalled condition until it crashed. I can’t believe that experienced pilots don’t know about stalling. There will be other human factors involved such as psychological barriers in a crisis to accepting that the familiar rules have just changed, and that a normally “unstallable” aeroplane might, on this occasion, be doing just that. This should be considered as a training issue.

HundredPercentPlease 1st Dec 2015 09:37


Originally Posted by Ranger One
A pair of ATPLs should be able to avoid stalling a basically serviceable aircraft

Of course they should. And no doubt this thread will gain many more posts saying the same thing.

But the constructive question is: why did two pilots, qualified to the levels the industry requires, fail to do what they were required to do?

Why?

That's the question that needs to be answered, and then the problem addressed. It's no good saying "idiots, move on".

Is there an issue with non-yoke inexperienced pilots just pulling up when in trouble (training conditioning from W/S, GPWS etc)? Are these problems caused by a complete lack of high altitude flight training? Is this a language/culture issue? Startle? Fatigue?

unworry 1st Dec 2015 09:56

Stall Warnings
 
from page 108

First Warning

Following the pitch up input on the right side stick, the aircraft continued climb then at 2316.56 the stall warning activated. ... the right side stick was at neutral then moved forward for two seconds. It caused the AOA decreased below 8°, and the aural stall warning stopped.
Second Warning

One second after the first stall warning ceased, the right side stick command was at 12° backward causing the aircraft pitch up and climbing at a rate up to 11,000 feet/minute.
The FDR recorded that after the first stall warning, the right side stick input was consistently backward. Could the PF become so fixated on levelling the wings that he was oblivious to pitch?

marchino61 1st Dec 2015 09:57

Hierarchy?
 
It's strange. So many times posters on pprune have pointed out accidents caused by the strictly hierarchical structure of Asian society.

Yet here we have an accident which could have been prevented by the captain telling the FO "I have control", instead of fighting between the two sidesticks.

Why?

unworry 1st Dec 2015 10:06

Dual Input
 

instead of fighting between the two sidesticks.
Of note in the report,


When both pilots move both sidesticks simultaneously in the same or opposite direction and neither takes priority, the system adds the signals algebraically.
When this occurred, the two green Side Stick Priority lights are ON and followed by “DUAL INPUT” voice message activation.
However, the CVR did not record “DUAL INPUT” voice message as it was suppressed by “STALL” voice warning.

Right Way Up 1st Dec 2015 10:09


But when you consider the ground troubleshooting episode three days earlier that is described on pg. 21, it is understandable why the captain, in his growing frustration, decided to try it.
I have to strongly disagree. He made what was an annoyance into a fatal accident by becoming a test pilot. It would be in the inflight reset list if it was a sensible procedure.

From the QRH

inflight,as a general rule, the crew must restrict computer resets to those listed in the table,or to those in applicable TDUs or OEBs. Before taking any action on other computers, the flight crew must consider and fully understand the consequences.
In this case if it was really annoying emergency cancel the caution then ground the aircraft after landing.

Siyouma 1st Dec 2015 10:14

Has anyone explored whether the FO in this accident and the FO of AF447 may have trained on the same programme given their nationalities? Unlikely but a slim possibility.

marchino61 1st Dec 2015 10:16


However, the CVR did not record “DUAL INPUT” voice message as it was suppressed by “STALL” voice warning.
Surely that should not be necessary? All the captain has to do is declare he has control of the aircraft. It's fairly obvious that he knew what to do and the FO didn't.

Could there be some unusual dynamic here, e.g. the Indonesian captain somehow feels inferior to the European FO? Surely not.

fab777 1st Dec 2015 10:22

because...
 

why did two pilots, qualified to the levels the industry requires, fail to do what they were required to do?
Because of the level of the industry.

Upset recovery training is new to the industry, post-AF447. As is the strong enphasis of the "I have control" magical words (think: proper task sharing and cross-cockpit communication), that may have saved that day.

HundredPercentPlease 1st Dec 2015 10:56

That's the point.

Is this the time where we have to have a long hard look at where pilots come from and what is "adequate" in terms of ability, training and experience? Or is it a function of the fact that aircraft now are so reliable, that exposure to things going wrong for real is so small that pilots are not able to cope?

In the past, aircraft were less reliable, so we all had exposure (horribly regular) to things going wrong. Now it is common to achieve command without a diversion or a circling approach. Let alone the a/p dumping you into a state with lots of untrimmed yaw.

My thoughts are that this has to be addressed in the sim. More sim time, and most importantly, less of the prescribed statutory "events" and more random stuff with a focus on initial actions. Once the startle is overcome and the initial quick diagnosis and initial actions done correctly, there is a much greater chance of a successful outcome.

Sim, sim, sim. Sadly though, the mantra is cost, cost, cost.

Swiss Cheese 1st Dec 2015 11:08

History repeating itself again....
 
I agree 100% with One Hundred Percent. The Coroner at the Air France 447 Inquest in 2013 highlighted a tendency for over-reliance on automation coupled with insufficient training. Deja vu.

HundredPercentPlease 1st Dec 2015 11:50

I would bet my last £1 that if put in a briefing classroom and asked the following questions, both pilots would give these answers:

Q. How do you recover from a stall?
A. Reduce the AoA by lowering the nose.

Q. How do you take control?
A. By pushing and holding the takeover pb, and saying "I have control".

Yet the startle, or fear, has resulted in an initial mess. 9 seconds is a long time to intervene when the aircraft banked 53° left. What was the thought process? Was it assumed that this was the a/p? When the a/p dropped out, did the FO read the FMAs? Did he do a micro-diagnosis? Did he see/say "Alternate Law"? Did he see the beta target?

Once in a mess, the fear has escalated (ref the captain's verbal comment) and recovery is 100 times harder.

It's not "recovery from unusual attitudes" that needs training, it's "recovery from an instant and unusual condition" that needs attention. How to approach this, the mental discipline required (as well as the operational discipline).

Curiously, our last sim cycle (A320) included "startle" and unusual attitude recovery. More to be done, industry-wide, I think.

Piltdown Man 1st Dec 2015 11:52

I believe Swiss and 100% are correct. Our modern world which includes cheap flights for all comes at a price - we will kill a few hundred every now and again. No part of the "system" we fly under can be absolved - including ATC with their pathetic noise maximisation procedures and prohibition of visual approaches. Everything we do is driven by cost - cheaper is perceived as being better. Our training is cut to the minimum prescribed, clowns in flight ops. departments prohibit things like manual flight and manual thrust and we spend our entire lives saving pennies. The same rot has moved into our technical departments. The clever little MBA whizz-kids have worked out how few spares we needs to carry and how little time we need to fix things so that engineers are nown under pressure to release aircraft they would prefer not to. And all of this is overseen by imbeciles like EASA (stress on the middle syllable).

We will have a kill a few more thousand and get the public really scared of flying cheaply before things will change.

PM

wanabee777 1st Dec 2015 11:57

That the FAA would certify a commercial aircraft designed with duel flight controls which have no tactile feedback between the two pilots is unconscionable!

fox niner 1st Dec 2015 12:12

Boeing driver here...

Does it really, I mean really.....take 40 bloody seconds to override the other sidestick?


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